X-Planes: Framing and the Research Aircraft Model

This article opens a seventy-two-article series that treats the United States X-series research aircraft as a single object of analysis, one designation at a time, from the Bell X-1 of 1946 through the Bell Textron X-76 announced in 2026. The series covers every designation in that range, including aircraft that flew, aircraft that were cancelled before metal was cut, aircraft whose existence remains classified, designations that were requested and refused, designations reserved and never formalized, one designation that was assigned twice, and a block of seven consecutive numbers that were leapfrogged entirely. The roster is drawn from the Wikipedia list of X-planes and the tri-service designation list, cross-checked against Miller 2001 The X-Planes X-1 to X-45, Jenkins et al. 2003 American X-Vehicles, and Winchester 2005 X-Planes and Prototypes, with the broader category context in the general treatments of experimental aircraft and the list of experimental aircraft. Throughout, the National Advisory Committee for Aeronautics is abbreviated NACA and its successor the National Aeronautics and Space Administration is abbreviated NASA, since both appear constantly from here on. The organizing claim is that a research aircraft is an instrument rather than a vehicle, that it exists to reduce uncertainty about one quantity that ground facilities cannot resolve at acceptable fidelity, and that the airframe, the propulsion, the structure, the control system, and the instrumentation were each dimensioned against that one quantity. This opening article establishes the analytical model the series applies, derives the sizing relations that recur across the individual articles so that each of them can reference a common derivation and need not repeat it, formalizes the designation system itself as an object with measurable properties, and states what the series can and cannot establish from the surviving record. The series overlaps deliberately with the earlier A96 History of Rocketplanes article, which treats the rocket-powered subset as a technological lineage. The present series takes each airframe separately and asks an engineering question about it, not a narrative one.

The Research Aircraft as an Instrument

The distinction that organizes this series is the distinction between a prototype and a research aircraft. A prototype is a preproduction example of an intended operational type, and its purpose is to demonstrate that the type can be built and will perform as advertised. A research aircraft has no intended operational type behind it. Its output is not a production line but a data set, and the aircraft is a fixture built to hold instrumentation in a flow field that cannot be produced any other way. Vincenti 1990 What Engineers Know and How They Know It is the standard philosophical treatment of how engineering knowledge is generated by this kind of purpose-built experiment, and its account of parameter variation as an engineering epistemology maps directly onto the flight-test programmes surveyed here. Ferguson 1992 Engineering and the Mind’s Eye and Petroski 1985 To Engineer Is Human supply the complementary arguments about visual reasoning and about failure as an information source.

The consequence of that distinction is that the success criteria invert. A prototype that never enters production has failed at the thing it existed to do. A research aircraft that flies a handful of times, returns the number it was built to measure, and is then pushed into a hangar corner and eventually scrapped has succeeded completely. The Douglas X-3 Stiletto never reached the speed it was designed for and is conventionally described as a disappointment, yet data from its tests informed the wing of the Lockheed F-104 Starfighter and it provided early flight test data on roll inertia coupling, as the Douglas X-3 Stiletto entry records. Whether that counts as success depends entirely on whether the aircraft is scored as a prototype or as an instrument.

The instrument framing can be made precise, and the machinery for doing so is the machinery of Bayesian experimental design, introduced by Lindley 1956 On a Measure of the Information Provided by an Experiment and surveyed by Chaloner and Verdinelli 1995. Let $\theta \in \mathbb{R}^p$ denote the vector of physical quantities the programme exists to determine, such as the drag coefficient through the transonic range, the convective heat flux at a given stagnation condition, or the dynamic pressure at which a particular wing diverges. Let the state of knowledge before the programme be represented by a prior distribution with mean $\mu_0$ and covariance $\Sigma_0$, in the sense of Gelman et al. 2013 Bayesian Data Analysis and Jaynes 2003 Probability Theory The Logic of Science. Each flight produces a measurement related to the unknown by an observation model with additive noise, written as

\[y_k = H_k \theta + v_k, \quad v_k \sim \mathcal{N}(0, R_k) \tag{1}\]

where $y_k$ is the vector of reduced measurements from flight $k$, $H_k$ is the observation matrix determined by which flight condition was flown and which instruments were carried, and $R_k$ is the measurement noise covariance that captures instrument error, data-reduction error, and atmospheric uncertainty. Under the linear-Gaussian assumption the posterior covariance after $n$ flights follows the information-form update

\[\Sigma_n^{-1} = \Sigma_0^{-1} + \sum_{k=1}^{n} H_k^{\top} R_k^{-1} H_k \tag{2}\]

which states the essential economic fact about flight test. Information adds. Each flight contributes an increment to the inverse covariance, and the increments accumulate whether or not any individual flight is dramatic. The design-of-experiments literature treats the choice of which conditions to fly as an optimal design problem over this matrix, and Box et al. 2005 Statistics for Experimenters together with Atkinson and Donev 1992 Optimum Experimental Designs give the standard criteria.

The posterior mean moves with the same information weighting, so that the estimate after $n$ flights is

\[\mu_n = \Sigma_n \left( \Sigma_0^{-1} \mu_0 + \sum_{k=1}^{n} H_k^{\top} R_k^{-1} y_k \right) \tag{3}\]

which shows that a flight flown at a condition where $H_k$ is nearly singular moves the estimate hardly at all regardless of how eventful the flight was. Choosing conditions is therefore the substance of test planning, and the two criteria in general use are D-optimality, which maximizes the determinant of the information matrix, and A-optimality, which minimizes the trace of the posterior covariance,

\[\Phi_D = \det \left( \Sigma_n^{-1} \right), \qquad \Phi_A = \operatorname{tr} \left( \Sigma_n \right) \tag{4}\]

with the first maximized and the second minimized over the achievable set of flight conditions. The differential entropy of the Gaussian posterior that these criteria are proxies for is

\[h(\theta) = \frac{1}{2} \ln \left[ (2 \pi e)^p \det \Sigma_n \right] \tag{5}\]

in nats, and the expected information gain from a planned flight is the expected Kullback-Leibler divergence of the posterior from the prior,

\[\mathbb{E} \left[ D_{KL} \left( p(\theta \mid y) \, \| \, p(\theta) \right) \right] = \mathbb{E} \left[ \int p(\theta \mid y) \ln \frac{p(\theta \mid y)}{p(\theta)} \, d\theta \right] \tag{6}\]

A test plan should maximize this quantity per unit cost.

For the scalar case, where the programme targets a single quantity and every flight is a repeat measurement of that quantity with standard deviation $\sigma_m$, the update collapses to

\[\sigma_n^2 = \left(\frac{1}{\sigma_0^2} + \frac{n}{\sigma_m^2}\right)^{-1} \tag{7}\]

with $\sigma_0$ the prior standard deviation and $\sigma_n$ the standard deviation after $n$ flights. Inverting for the number of flights required to reach a target uncertainty $\sigma_T$ gives

\[n^{*} = \left\lceil \sigma_m^2 \left( \frac{1}{\sigma_T^2} - \frac{1}{\sigma_0^2} \right) \right\rceil \tag{8}\]

It sizes the flight count of a research programme. Consider the transonic drag-rise problem the Bell X-1 was built to resolve. Assume that before the programme the drag coefficient in the neighbourhood of Mach one was uncertain by roughly a factor of two, a relative standard deviation of order unity, so take $\sigma_0 = 1.0$ in relative terms. Assume also that a single instrumented flight through a narrow Mach band returns the drag coefficient in that band with a relative standard deviation of roughly $\sigma_m = 0.25$, limited by thrust knowledge and accelerometer calibration rather than by anything aerodynamic. A useful design database requires the drag coefficient to five percent, so $\sigma_T = 0.05$. The relation gives

\[n^{*} = \left\lceil 0.0625 \left( 400 - 1 \right) \right\rceil = \lceil 24.9 \rceil = 25 \tag{9}\]

flights per Mach band. The first X-1 airframe made nineteen contractor demonstration flights and fifty-nine Air Force test flights, according to the National Air and Space Museum, a count of the right order of magnitude for the handful of Mach bands the programme covered. The reading this series offers is that programmes were sized by this logic in effect even when nobody wrote the integral down.

The corresponding information gain, measured as the reduction in differential entropy between prior and posterior in the sense of Shannon 1948 and quantified by the Kullback-Leibler divergence of Kullback and Leibler 1951, is

\[I_n = \frac{1}{2} \ln \frac{\sigma_0^2}{\sigma_n^2} \tag{10}\]

which for the X-1 example evaluates to $I_n = \tfrac{1}{2}\ln 400 = 3.00$ nats, or 4.32 bits, converting between the two by

\[I_{\text{bits}} = \frac{I_{\text{nats}}}{\ln 2} \tag{11}\]

The standard treatments in Cover and Thomas 2006 Elements of Information Theory and MacKay 2003 Information Theory Inference and Learning Algorithms develop the entropy accounting in full. A programme of that size and expense returns roughly four bits about one number. That figure measures what a flight research programme returns for its cost, and it explains why such programmes are justified only when the number in question gates something enormous downstream.

Origins and Eras of the Research Aircraft Programme

The argument above explains why a research aircraft can be worth building. This section records why the first ones were built and how the programme changed in the eight decades that followed. The division of labour among service, contractor and agency is treated under The Institutional Arrangement, and the clustering of designations in time under The Designation System as a Formal Object, so this section points to both and does not restate them.

The Transonic Problem and the Decision of 1944

The research aircraft began as an answer to a wartime problem that neither the airplane nor the wind tunnel could solve. By the end of the 1930s, piston-engined military aircraft could approach transonic speeds in prolonged dives, and Hallion 1984 On the Frontier describes how shock waves forming over the wing broke the flow into a turbulent wake that struck the tail, in some cases with loads severe enough to tear the tail away. Hansen 1987 Engineer in Charge records fatal tail failures in high-speed dives of the Republic P-47 Thunderbolt and the Bell P-39 Airacobra, and a Navy Curtiss SB2C Helldiver whose horizontal tail fluttered so badly in high-speed manoeuvres that it broke off.

The ground facilities could not reach the speeds at which these failures happened. A closed-throat tunnel chokes as the flow at its narrowest section approaches the speed of sound, and Hansen 1987 records that by December 1941 John Stack and the engineers of the Langley 8-Foot High-Speed Tunnel had concluded that nobody was likely to solve the choking problem for some time and that transonic theory was making no significant progress. Hallion 1984 lists the stopgap methods that followed, which were weighted bodies dropped from high altitude and tracked by radar, small rocket-propelled models, and models mounted on the wing of a fighter dived until the accelerated flow over its wing exceeded Mach one. The slotted-throat tunnel that eventually solved the ground problem came only after the war. The formal reason the linear theory failed at the same condition is the Prandtl-Glauert singularity treated under Drag and the Transonic Rise, and the general reason is the similarity gap. The conclusion drawn at Langley was the one this article formalizes, that a specially instrumented, full-scale research airplane was the remaining way into the transonic band.

Hallion 1984 names three advocates of the idea, Stack of the NACA, Ezra Kotcher of the Army Air Forces and Walter Diehl of the Navy. Stack had drawn a paper design for a high-speed research airplane in 1933, and in the spring of 1942 he obtained permission from George Lewis, the NACA’s director of research, to work out the design requirements of a transonic research aircraft, a permission that stopped short of procurement because the NACA’s charter did not allow it to build a complete airplane and its budget could not have paid for one, according to Hansen 1987. Kotcher, chief of aeronautical research of the Materiel Command at Wright Field, had himself proposed a transonic research airplane powered by a gas turbine or a rocket in 1939, and General Arnold had rejected it. The first formal discussion between the services and the NACA was a conference at Langley on 15 March 1944. The NACA presented the airplane as a way to collect transonic data that no wind tunnel could provide, the Army representatives saw it as a developmental step toward operating speeds through Mach one, and the Navy representatives saw it as a means of dispelling the belief in an impenetrable barrier. The meeting reached no agreement on the airplane’s purpose or its design.

The disagreement that followed was over propulsion. At meetings in mid-May 1944 Kotcher presented a Wright Field study comparing turbojet and rocket airplanes at high Mach number, argued from the experience of the Bell P-59 that a turbojet could not propel an airplane to transonic speed, and showed a rough drawing of a rocket airplane. Stack replied that a rocket airplane was unsafe, that it could not stay aloft long enough to gather the systematic data the research required, and that its results would apply less to the future of aviation than a turbojet’s, and on 10 July 1944 he sent Wright Field a turbojet design intended to collect transonic data rather than to fly supersonically. At meetings on 13 and 14 December 1944 the Army Air Forces representatives rejected that design as too conservative and asked for an airplane able to reach about Mach 1.2, and Hansen 1987 quotes the outcome as the Army putting up the money and deciding to do it its own way. One week later the Army Air Forces opened negotiations with Bell Aircraft, whose design team began work under project MX-524, and on 10 March 1945 it notified the NACA that Bell would receive the contract for a rocket-powered research airplane with straight wings.

Stack turned to the Navy once it was clear that the Army Air Forces would insist on a rocket. In September 1944 Abraham Hyatt of the Navy’s Bureau of Aeronautics proposed a high-speed research airplane that followed the NACA’s conservative design, with a turbojet, conventional takeoff and landing, and a maximum speed not exceeding that of sound, and by the first weeks of 1945 Douglas engineers were at work on what became the Model 558 [Hansen 1987]. Two programmes therefore began in 1945, the rocket-powered XS-1 under Army Air Forces sponsorship and the turbojet-powered D-558 under Navy sponsorship, and Hallion 1984 judges that the D-558 came closest to what Stack had wanted. The D-558 never carried an X-designation, and this series treats it only as context.

Hallion 1984 records that Bell rolled out the first XS-1 at Buffalo late in December 1945 and that in the same month the Army Air Forces asked the NACA to supervise all of its data gathering and analysis, and the arrangement treated under The Institutional Arrangement begins there. Glide flights began at Pinecastle Field in Florida in January 1946, on the 19th according to Hallion and on the 25th according to the NASA inventory of Jenkins et al. 2003, and the two sources are left disagreeing. They also disagree about the letter S, which Hansen 1987 expands as Sonic and the inventory as Supersonic. The inventory records that the S was dropped early in the programme, which makes the X-1 the first aircraft to carry an X-designation, and the second Bell aircraft was likewise ordered as the XS-2 before becoming the X-2.

The Eras of the Programme

The first generation followed quickly. Within a year of the XS-1 and the D-558 the Army Air Forces and the NACA began four further research aircraft, and added two more within another three years, which Hallion 1984 describes as the nation’s stable of transonic and supersonic research aircraft for speeds up to Mach 3. Each was an aerodynamic testbed for a configuration question, among them the higher speeds and altitudes of the Bell X-2, the tailless Northrop X-4, the variable sweep of the Bell X-5 and the delta wing of the Convair XF-92A, and the NACA station in the desert flew examples of all of them between 1947 and 1958 except the X-2.

Hypersonics came next. Jenkins 2000a Hypersonics Before the Shuttle dates the first substantial official support to a resolution of the NACA Committee on Aerodynamics on 24 June 1952 to increase its work on manned and unmanned flight at altitudes of 12 to 50 miles and Mach numbers of 4 to 10. The NACA presented a hypersonic research aircraft to the Air Force and the Navy on 9 July 1954 as an extension of the existing cooperative research airplane programme, the three signed a memorandum of understanding on 23 December 1954, and on 30 September 1955 the Air Force notified North American Aviation that its design had won. The X-15 first flew on 8 June 1959 and made 199 flights, the last on 24 October 1968.

The lifting bodies overlapped the X-15 and outlasted it. Between 1963 and 1975 the NASA Flight Research Center flew eight lifting-body configurations, from the unpowered plywood M2-F1 to the rocket-powered X-24B, and Reed and Lister 1997 Wingless Flight presents all of them as flying prototypes of spacecraft that could land like an airplane after entry. The X-24A first flew in 1969 and was rebuilt as the X-24B, whose speed and performance resembled those projected for the Space Shuttle closely enough that its flights were used to collect operational data for it. The contested X-23 belongs to the same entry work and is treated under The Designation System as a Formal Object.

The comparative gap followed. By the first-flight dates the inventory of Jenkins et al. 2003 lists, no X-designated aircraft made a first flight between the X-24B in August 1973 and the Grumman X-29 in December 1984, and the inventory’s authors write that almost thirty designations were allocated between the late 1940s and the late 1970s and that the series then largely ended. Flight research did not end with it. Through the late 1960s and the 1970s the Flight Research Center continued its lifting-body work for the Space Shuttle and flew the YF-12, the F-8 Digital Fly-by-Wire and supercritical-wing programmes, and the F-111 Transonic Aircraft Technology effort, all on aircraft outside the X-series [Hallion 1984]. A gap in X-numbers is therefore not a gap in flight research, and this series reads the designation clusters as institutional evidence, not as a measure of research activity.

The revival of the 1980s ran through the Defense Advanced Research Projects Agency. The inventory lists it with the Air Force and NASA as a sponsor of the forward-swept X-29, first flown on 14 December 1984, and with the Navy and the German defence ministry as a sponsor of the X-31, built to fly at angles of attack beyond the stall and first flown on 11 October 1990. The same agency’s classified Copper Canyon study, which ran from 1982 to 1985, became the National Aero-Space Plane, designated X-30, which President Reagan described as a new Orient Express able to reach low Earth orbit or fly to Tokyo within two hours. It ran into cost and technical difficulties and was cancelled without a vehicle, and the inventory traces the X-43A to the follow-on programme that took up its hypersonic technology.

The reusable launch vehicles of the 1990s were aimed at the cost of reaching orbit. The X-33 was a suborbital half-scale prototype of the proposed VentureStar, built under a cooperative agreement between NASA and an industry team led by Lockheed Martin, and the X-34 was a reusable testbed, and NASA cancelled both in March 2001 before either had flown free, according to the inventory. The X-37 began as NASA’s Future-X Pathfinder, with the Air Force’s X-40A serving as its prototype, before the transfers recorded under The Institutional Arrangement.

The demonstrators of the late 1990s and after increasingly flew without a pilot, after the change of sponsorship that The Institutional Arrangement describes. The inventory lists the Defense Advanced Research Projects Agency with the Air Force as a sponsor of the Boeing X-45 unmanned combat air vehicle and with the Navy as a sponsor of the Northrop Grumman X-47, and the register of allocations that Andreas Parsch compiles from data the Department of Defense has released records the X-63A and X-64A as demonstrator rockets for a programme of the Air Force Research Laboratory.

NASA Aeronautics proposed a return to X-planes with the budget request for fiscal year 2017. Banke 2016 describes New Aviation Horizons as part of a ten-year plan to design, build and fly flight demonstration vehicles aimed at fuel use, emissions and noise, typically about half the scale of a production aircraft and likely to be piloted, among them a hybrid wing body and a business-jet-sized supersonic vehicle whose sonic boom people on the ground would barely hear. The register then records the X-57A on 3 May 2016 for an all-electric aircraft with distributed electric propulsion, the X-59A on 21 June 2018 for a research aircraft that will create a shaped sonic boom signature, and the X-66A in 2023 for a transonic truss-braced wing demonstrator built from a modified MD-90. Of the other recent allocations, the X-61A, the X-65A, the X-68A and the X-76A carry the Defense Advanced Research Projects Agency as sponsor, and the X-76 closes the roster this series covers.

Methodological Commitments

The series makes six commitments, stated here so that individual articles need not restate them.

Each article treats one designation, including designations behind which no aircraft ever existed. An article about a number that was never assigned is a legitimate article, because the reason a number went unassigned is evidence about how the designation system worked.

Each article names its keystone explicitly. The keystone is the single binding unknown the aircraft was built to resolve, and the article states it in one sentence before it derives anything.

Each article is written from current knowledge rather than from knowledge available at the editorial date printed in the front matter. Where a source postdates that date, the Epistemic State section says so explicitly.

Where sources disagree, both are named and the disagreement is left standing. Silently choosing the more convenient source is the failure mode this commitment exists to prevent, and it appears repeatedly in the X-series record, most sharply around the X-23 and the X-42.

Numbers carry units and provenance. A figure taken from a source is attributed to that source. A figure derived in the article is labelled as derived, and the derivation is shown so it can be checked.

Depth follows the surviving record rather than effort. Where the public record supports a full treatment, the article gives one. Where it does not, the article states the limit instead of writing around it.

The Similarity Gap

The question a reader should ask of any flight research programme is why anyone flew at all. Wind tunnels are cheaper, they are repeatable, they do not kill test pilots, and by the late 1940s the United States had the best collection of them in the world, as catalogued by Baals and Corliss 1981 Wind Tunnels of NASA. The answer is that a ground facility can match some of the dimensionless groups that govern a flow, but not all of them at once, and the residue is what the aircraft was built to measure. The formal apparatus is similitude and the Buckingham pi theorem, and the practical apparatus is described in Pope and Goin 1965 High-Speed Wind Tunnel Testing, Barlow et al. 1999 Low-Speed Wind Tunnel Testing, and Lukasiewicz 1973 Experimental Methods of Hypersonics.

The governing groups follow from nondimensionalizing the Navier-Stokes equations together with the energy equation and an equation of state, a derivation given in Anderson 2001 Fundamentals of Aerodynamics and in Kuethe 1950 Foundations of Aerodynamics. The theorem, established by Buckingham 1914, states that a relation among $n$ physical quantities involving $k$ independent dimensions reduces to a relation among

\[n - k \ \text{dimensionless groups} \tag{12}\]

so the number of knobs a facility must match is fixed by the physics rather than by the experimenter. Nondimensionalizing the momentum equation with a reference length $L$, a reference speed $V$, and a reference density $\rho$ produces

\[\frac{D \mathbf{u}^{*}}{D t^{*}} = -\frac{1}{\gamma M^2} \nabla^{*} p^{*} + \frac{1}{Re} \nabla^{*2} \mathbf{u}^{*} \tag{13}\]

in which the two groups appear as the only surviving parameters, the formal reason they are the two a tunnel tries hardest to match. The first is the Mach number, the ratio of flow speed to the local speed of sound, written with $V$ the flow speed in metres per second and $a$ the sound speed in the same units as

\[M = \frac{V}{a}, \quad a = \sqrt{\gamma R T} \tag{14}\]

where $\gamma$ is the ratio of specific heats, $R$ is the specific gas constant in joules per kilogram kelvin, and $T$ is the static temperature in kelvin. The tabulated forms of every isentropic, normal-shock, and oblique-shock relation used throughout this series are collected in Ames Research Staff 1953, which remains the standard reference for the arithmetic below. The state relation closing the system is the ideal gas law

\[p = \rho R T \tag{15}\]

which is used repeatedly below to move between pressure, density, and temperature. The Mach number governs compressibility, and a supersonic tunnel is designed to match it. The local inclination of a weak disturbance follows from it as the Mach angle

\[\mu_M = \arcsin \frac{1}{M} \tag{16}\]

which fixes the geometry of every shock and expansion in the supersonic sections that follow. Shapiro 1953 The Dynamics and Thermodynamics of Compressible Fluid Flow, Liepmann and Roshko 1957 Elements of Gasdynamics, and Anderson 2002b Modern Compressible Flow remain the standard treatments.

The second is the Reynolds number, the ratio of inertial to viscous forces, written with $\rho$ the density in kilograms per cubic metre, $L$ a reference length in metres, and $\mu$ the dynamic viscosity in pascal seconds as

\[Re = \frac{\rho V L}{\mu} \tag{17}\]

which governs boundary layer development, transition from laminar flow to turbulent flow, and separation. The canonical references are Schlichting and Gersten 2017 Boundary-Layer Theory and White 2006 Viscous Fluid Flow, with the compressible extension given by Van Driest 1952. The viscosity itself is temperature dependent through the relation of Sutherland 1893,

\[\mu = \mu_{\text{ref}} \left( \frac{T}{T_{\text{ref}}} \right)^{3/2} \frac{T_{\text{ref}} + S}{T + S} \tag{18}\]

with the reference pair $\mu_{\text{ref}} = 1.716 \times 10^{-5}$ pascal seconds at $T_{\text{ref}} = 273.15$ kelvin taken here, and with $S = 110.4$ kelvin for air, the constant the NASA Glenn Research Center gives as 198.72 degrees Rankine, and the worked example below uses this relation. The Reynolds number is the group a tunnel usually fails to match, and the failure is structural rather than incidental.

To see why, substitute the ideal gas law and the sound speed into the Reynolds number to express it in terms of quantities a tunnel operator controls. With $p$ the static pressure in pascals, this gives

\[Re = \frac{p M L}{\mu} \sqrt{\frac{\gamma}{R T}} \tag{19}\]

which shows that at a fixed Mach number and a fixed temperature the Reynolds number is proportional to the product of static pressure and model length. A subscale model of geometric scale factor $1/k$ therefore requires

\[p_{\text{model}} = k \, p_{\text{flight}} \tag{20}\]

to reproduce the flight Reynolds number at the flight Mach number and the flight temperature. The pressure penalty is linear in the scale factor and it compounds against the tunnel’s own requirements, because a supersonic nozzle must expand from a reservoir whose stagnation pressure exceeds the test-section static pressure by the isentropic ratio

\[\frac{p_0}{p} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}} \tag{21}\]

with $p_0$ the reservoir stagnation pressure. The reservoir must simultaneously supply the stagnation temperature

\[\frac{T_0}{T} = 1 + \frac{\gamma - 1}{2} M^2 \tag{22}\]

and, completing the isentropic set, the density ratio

\[\frac{\rho_0}{\rho} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{1}{\gamma - 1}} \tag{23}\]

because a nozzle expansion is very nearly adiabatic and the total temperature is what the reservoir sets.

The arithmetic is worth doing once. Take the North American X-15 at Mach 6 and 30 kilometres, near the middle of its envelope. The International Standard Atmosphere and the U.S. Standard Atmosphere at that altitude give $T = 226.7$ kelvin, $p = 1197$ pascals, and $\rho = 0.01841$ kilograms per cubic metre. The sound speed is $a = \sqrt{1.4 \times 287 \times 226.7} = 302$ metres per second, so the flight speed is $V = 1811$ metres per second. Sutherland’s law at that temperature gives $\mu = 1.48 \times 10^{-5}$ pascal seconds. The unit Reynolds number is therefore

\[\frac{Re}{L} = \frac{\rho V}{\mu} = \frac{0.01841 \times 1811}{1.48 \times 10^{-5}} = 2.26 \times 10^{6} \ \text{per metre} \tag{24}\]

and across the 15.0 metre length of the aircraft, the 49 feet 2 inches the North American X-15 entry gives without the nose boom, the Reynolds number is $3.4 \times 10^{7}$. Now attempt to reproduce that on a one-twentieth-scale model in a Mach 6 tunnel. The model requires a test-section static pressure of $20 \times 1197 = 23.9$ kilopascals. The isentropic ratio at Mach 6 with $\gamma = 1.4$ is $8.2^{3.5} = 1581$, so the reservoir must hold

\[p_0 = 23{,}940 \times 1581 = 3.8 \times 10^{7} \ \text{pascals} = 38 \ \text{megapascals} \tag{25}\]

which is roughly 373 atmospheres, and it must hold that pressure at a stagnation temperature of $T_0 = 226.7 \times 8.2 = 1859$ kelvin, because otherwise the tunnel does not reproduce the thermal state of the gas. Holding 38 megapascals and 1859 kelvin continuously is the demand that makes a continuous hypersonic tunnel costly, since its power requirement rises with the cube of the test velocity. Facilities therefore commonly reach such stagnation conditions intermittently, in blowdown tunnels or in hot-shot tunnels whose runs last less than a second, and supplying high temperature and pressure for long enough to measure and reproducing equilibrium conditions are standing problems of hypersonic tunnel design, which limits any measurement requiring thermal equilibrium of the model.

The mismatch is not confined to pressure and temperature. Four further groups matter at the conditions the X-series explored, and Anderson 2006 Hypersonic and High-Temperature Gas Dynamics together with Bertin 1994 Hypersonic Aerothermodynamics treat them systematically. The Prandtl number, the ratio of momentum diffusivity to thermal diffusivity, is

\[Pr = \frac{\mu c_p}{k_{\text{th}}} \tag{26}\]

with $c_p$ the specific heat at constant pressure in joules per kilogram kelvin and $k_{\text{th}}$ the thermal conductivity in watts per metre kelvin. It sets the relation between the velocity and thermal boundary layers, and it drifts with temperature as the gas dissociates.

The wall-to-total temperature ratio $T_w / T_0$ governs the heat flux into the structure and therefore the boundary-layer profile. A cold-wall tunnel model at room temperature and a flight article radiating at 1200 kelvin have different profiles even at matched Mach and Reynolds numbers, and the difference changes transition location, a point developed by Lees 1956.

The Damkohler number, the ratio of a characteristic flow time to a characteristic chemical time, is

\[Da = \frac{\tau_{\text{flow}}}{\tau_{\text{chem}}} = \frac{L / V}{\tau_{\text{chem}}} \tag{27}\]

where the chemical time carries an Arrhenius temperature dependence

\[\tau_{\text{chem}} \propto \exp \left( \frac{E_a}{R_u T} \right) \tag{28}\]

with $E_a$ the activation energy and $R_u$ the universal gas constant, so that a facility running cold is not merely quantitatively but qualitatively wrong. The Damkohler number decides whether the gas behind a shock is in chemical equilibrium, frozen, or somewhere between. At the stagnation temperatures the X-15 reached, which Aerothermodynamics below puts above 2000 kelvin, the dissociation of oxygen in hypersonic flow becomes active, and no cold tunnel reproduces that. At the conditions the NASA X-43 and Boeing X-51 Waverider reached, the same question governs whether fuel injected into a scramjet combustor burns before it leaves.

The Knudsen number, the ratio of molecular mean free path $\lambda$ to reference length, is

\[Kn = \frac{\lambda}{L} \tag{29}\]

where the mean free path follows from kinetic theory as

\[\lambda = \frac{\mu}{p} \sqrt{\frac{\pi R T}{2}} \tag{30}\]

The three groups are not independent, since substituting this relation into the definitions gives

\[Kn = \sqrt{\frac{\pi \gamma}{2}} \, \frac{M}{Re} \tag{31}\]

so rarefaction is unavoidable at high Mach number and low Reynolds number together, the corner of the envelope a high-altitude research aircraft occupies. The Knudsen number decides whether the continuum assumption holds at all. Above roughly 90 kilometres, approaching the Karman line, the X-15 was operating where $Kn$ ceased to be negligible over control surfaces and where, as the North American X-15 entry records, there was too little air for aerodynamic control surfaces, and for that reason it carried a reaction control system in addition to its aerodynamic surfaces.

Collecting these, let $\Pi = (M, Re, Pr, T_w/T_0, Da, Kn)$ denote the similarity vector. A ground facility reproduces flight when the logarithmic mismatch

\[\varepsilon_{\text{sim}} = \left\| \ln \Pi_{\text{facility}} - \ln \Pi_{\text{flight}} \right\| \tag{32}\]

is small. It never is. The subset of $\theta$ that survives a ground campaign with unacceptable residual uncertainty is what the series calls the flight-only residual, and closing it is the purpose of each of these aircraft. Partition the unknown vector as

\[\theta = \theta_{\text{ground}} \cup \theta_{\text{flight}}, \quad \theta_{\text{flight}} = \left\{ \theta_i : \sigma_i^{\text{ground}} > \sigma_i^{T} \right\} \tag{33}\]

where $\sigma_i^{\text{ground}}$ is the uncertainty achievable from tunnels, computation, and rocket sleds, and $\sigma_i^{T}$ is the target. A research aircraft is justified when $\theta_{\text{flight}}$ is non-empty and what it gates is worth the programme. Drake and Williams 1958 made essentially this argument in print, an early public statement of the rationale this series formalizes.

Because of this partition, the series does not treat the X-planes as a parade of fast aircraft. Speed was rarely the point. The point was that somewhere in the design space a number was unknown, ground facilities could not close it, and a decision downstream depended on it.

The Keystone Principle

If a research aircraft exists to close one residual, then the residual dominates the design. That claim can be stated as a constrained optimization and then read for its shadow prices, using the standard apparatus of Lagrange multipliers and the Karush-Kuhn-Tucker conditions developed in Boyd and Vandenberghe 2004 Convex Optimization and Nocedal and Wright 2006 Numerical Optimization.

Let $x$ denote the vector of design variables, including wing area, propellant fraction, structural gauge, skin material, control-surface authority, and instrumentation mass. Let $C(x)$ denote programme cost. The vehicle must reach the test condition, and it must survive it, so the programme solves

\[\min_{x} \ C(x) \quad \text{subject to} \quad g_j(x) \le b_j, \ j = 1, \dots, m \tag{34}\]

where each $g_j$ is a physical constraint such as the maximum skin temperature, the divergence dynamic pressure, the available thrust, or the pilot’s tolerance to acceleration. At the optimum the conditions attach a multiplier $\lambda_j \ge 0$ to each constraint, and the multiplier is the sensitivity of optimal cost to a relaxation of that constraint,

\[\lambda_j = -\frac{\partial C^{*}}{\partial b_j} \tag{35}\]

The multipliers are the ones appearing in the Lagrangian

\[\mathcal{L}(x, \lambda) = C(x) + \sum_{j=1}^{m} \lambda_j \left( g_j(x) - b_j \right) \tag{36}\]

whose stationarity and complementary slackness conditions at the optimum are

\[\nabla C(x^{*}) + \sum_{j=1}^{m} \lambda_j \nabla g_j(x^{*}) = 0, \qquad \lambda_j \left( g_j(x^{*}) - b_j \right) = 0 \tag{37}\]

the second of which states that a constraint that does not bind carries a multiplier of zero. A constraint with a large multiplier is therefore one whose relaxation would yield a large cost reduction. The keystone is then defined as the constraint with the largest normalized shadow price,

\[j^{*} = \arg\max_j \ \lambda_j b_j \tag{38}\]

and the empirical claim this series makes is that for almost every X-plane the arg max is unique, obvious in retrospect, and identifiable from the design record without doing any optimization at all. For the X-1 the binding constraint was structural, because the loads a wing would see through the transonic rise were unknown, so the aircraft was built to a load factor of 18 g, half again the usual fighter figure and chosen by Stack for a wide margin of safety according to Hansen 1987, and it was in principle a bullet with wings. For the X-15 the binding constraint was thermal, which selected Inconel X as the major structural material, as Jenkins 2000a records, which set the structural mass, which set the propellant fraction, which set the powerplant. For the Grumman X-29 it was aeroelastic divergence of a forward-swept wing, which selected aeroelastically tailored composite covers, and testing those covers was the purpose of the aircraft. The X-43 was bound by scramjet ignition and flameholding at flight enthalpy, which set the booster, the trajectory, and a test window in which the scramjet operated for about ten seconds.

Where the arg max is not unique, the programme is usually in trouble, and the series treats that as a diagnostic rather than an accident. The Rockwell X-30 National Aero-Space Plane had at least four constraints of comparable severity, including airbreathing propulsion to orbital speed, slush hydrogen storage, active cooling of leading edges, and the absence of any facility able to validate the propulsion system on the ground. It was cancelled without a vehicle. The Boeing X-32 and the Lockheed Martin X-35 by contrast were built to a single constraint each, namely demonstrating a shipboard-compatible short takeoff and vertical landing propulsion arrangement within a fighter airframe, and both flew.

Sizing Relations Common to the Series

The individual articles derive what is peculiar to their aircraft and reference this section for what is not. Everything below is standard. It is collected here so that the derivations can be checked once and not seventy-one times. The conceptual-design texts that assemble these relations into a sizing method are Raymer et al. 2012 Aircraft Design A Conceptual Approach, Nicolai et al. 2010a Fundamentals of Aircraft and Airship Design, Torenbeek and Synthesis of subsonic airplane design 1979 Synthesis of Subsonic Airplane Design, Roskam 1985 Airplane Design, Stinton 2001 The Design of the Aeroplane, and Whitford 1987 Design for Air Combat.

The Flight Envelope

The single most useful quantity in flight test is dynamic pressure, defined with $\rho$ the free-stream density and $V$ the true airspeed as

\[q = \frac{1}{2} \rho V^2 \tag{39}\]

which sets aerodynamic loads, hinge moments, and structural stress. For compressible work it is more convenient in the equivalent form

\[q = \frac{\gamma}{2} p M^2 \tag{40}\]

which follows from the ideal gas law and the definition of the sound speed, and which has the practical advantage that pressure and Mach number are both directly measured in flight while density is inferred. Taking the X-15A-2 on its Mach 6.7 flight at roughly 31.1 kilometres, the 102,100 feet of the North American X-15 entry against the 102,700 feet that Jenkins 2000a gives, where the static pressure is about 1018 pascals, gives

\[q = 0.7 \times 1018 \times 44.9 = 3.2 \times 10^{4} \ \text{pascals} \tag{41}\]

or 32 kilopascals, which is about 668 pounds per square foot. That is a modest dynamic pressure by fighter standards, and on this reading it is what allowed the X-15 to be built of a material chosen for its strength at temperature and not at room temperature.

Lift follows from dynamic pressure, the reference wing area $S$ in square metres, and the lift coefficient $C_L$ as

\[L = q S C_L \tag{42}\]

and level flight requires lift to equal weight, which fixes the low-speed boundary of the flight envelope at the stall speed

\[V_{\text{stall}} = \sqrt{\frac{2W}{\rho S C_{L,\max}}} \tag{43}\]

with $W$ the weight in newtons and $C_{L,\max}$ the maximum attainable lift coefficient. The manoeuvring boundary is set by the load factor

\[n = \frac{L}{W} \tag{44}\]

and the two boundaries intersect at the corner speed, the lowest speed at which the aircraft can pull its structural limit load,

\[V_A = \sqrt{\frac{2 n_{\max} W}{\rho S C_{L,\max}}} \tag{45}\]

This speed is the leftmost point of the V-n diagram’s structural ceiling. The load factor also fixes the sustained turn, since a level banked turn at load factor $n$ has turn rate and radius

\[\omega_t = \frac{g \sqrt{n^2 - 1}}{V}, \qquad R_t = \frac{V^2}{g \sqrt{n^2 - 1}} \tag{46}\]

and this pair matters whenever a research aircraft has to be manoeuvred back onto a test heading inside a restricted range. Because loads scale with dynamic pressure rather than with true airspeed, envelopes are conventionally drawn against equivalent airspeed

\[V_e = V \sqrt{\frac{\rho}{\rho_{SL}}} \tag{47}\]

which collapses the structural boundary onto a single vertical line at all altitudes. The classic pilot-facing exposition of these boundaries is Hurt 1960 Aerodynamics for Naval Aviators, with the performance-analysis treatment in Anderson et al. 1999 Aircraft Performance and Design and the introductory development in Anderson 2012 Introduction to Flight. Evaluate this for the Bell X-1, whose gross weight was about 5560 kilograms and whose wing area was 12.1 square metres, giving a wing loading of 4510 newtons per square metre. At 12 kilometres, where $\rho = 0.311$ kilograms per cubic metre, with the design load factor $n_{\max} = 18$ and an assumed $C_{L,\max} = 1.0$, the corner speed is

\[V_A = \sqrt{\frac{2 \times 18 \times 4510}{0.311 \times 1.0}} = 723 \ \text{metres per second} \tag{48}\]

which at that altitude corresponds to Mach 2.45. The fastest first-generation X-1 flight was Mach 1.45 [Jenkins et al. 2003], so on these values the X-1 could not reach its structural limit at any speed it flew. The airframe was built with a wide margin over the loads it saw, as intended by a design team that did not know what the transonic loads would be.

The performance boundary is set by excess thrust. With $T$ the thrust and $D$ the drag, both in newtons, the specific excess power central to energy-maneuverability theory is

\[P_s = \frac{V (T - D)}{W} \tag{49}\]

in metres per second, the rate at which the aircraft can add energy. The thrust required follows from the drag polar as

\[T_{\text{req}} = \frac{1}{2} \rho V^2 S C_{D0} + \frac{2 n^2 W^2}{\rho V^2 S \pi A e} \tag{50}\]

whose two terms move in opposite directions with speed, so the sum has a minimum that locates the best endurance condition. The absolute ceiling is the altitude at which the excess vanishes,

\[P_s = 0 \quad \Longleftrightarrow \quad T = D \tag{51}\]

The relevant energy state is the energy height

\[h_e = h + \frac{V^2}{2g} \tag{52}\]

with $h$ the geometric altitude in metres and $g$ the gravitational acceleration. Energy height is conserved in an unpowered exchange between speed and altitude, which makes it the natural coordinate for a rocket aircraft that spends most of a flight ballistic. With energy height available as a coordinate, the time to climb between two energy states follows by integrating the reciprocal of the excess power,

\[t_{1 \to 2} = \int_{h_{e,1}}^{h_{e,2}} \frac{dh_e}{P_s(h_e)} \tag{53}\]

It states in energy-state form the climb problem that a rocket aircraft profile poses. For the X-15A-2 at 2021 metres per second, the 4,520 miles per hour of the record flight, and 31.1 kilometres,

\[h_e = 31{,}120 + \frac{2021^2}{2 \times 9.81} = 31{,}120 + 208{,}180 = 2.39 \times 10^{5} \ \text{metres} \tag{54}\]

which is an energy height of 239 kilometres. The same airframe on a different profile traded that energy for altitude and reached 108.0 kilometres geometric, the 354,200 feet that Jenkins 2000a records, and the two flights are the same aircraft at similar energy states pointed differently. This series reads the X-15 flights as one energy-height envelope rather than as separate speed and altitude records. The measured lift and drag characteristics against which these calculations should be checked are given by Garringer and Saltzman 1966, and the approach and landing end of the same envelope by Matranga 1961a.

Drag and the Transonic Rise

The drag polar for a subsonic aircraft is conventionally written with $C_{D0}$ the zero-lift drag coefficient, $A$ the aspect ratio, and $e$ the Oswald efficiency number as

\[C_D = C_{D0} + \frac{C_L^2}{\pi A e} \tag{55}\]

in which the induced term traces to the minimum-induced-drag result of Munk 1921 and the efficiency factor to the performance charts of Oswald 1932. The maximum lift-to-drag ratio follows by differentiation as

\[\left( \frac{L}{D} \right)_{\max} = \frac{1}{2} \sqrt{\frac{\pi A e}{C_{D0}}} \tag{56}\]

attained at the lift coefficient

\[C_L^{*} = \sqrt{\pi A e \, C_{D0}} \tag{57}\]

where induced drag equals zero-lift drag. This relation is what makes high aspect ratio valuable and what the Northrop X-21 laminar-flow programme and the Boeing X-48 blended wing body were each attacking from opposite directions, the first by reducing $C_{D0}$ through boundary-layer suction, an effort reviewed across its whole history in Wagner et al. 1992, and the second by increasing the effective $A$ through configuration, with the flight correlation reported by Vicroy 2011.

Compressibility enters first through the Prandtl-Glauert transformation, which for small disturbances relates the compressible pressure coefficient to its incompressible value as

\[C_p = \frac{C_{p,0}}{\sqrt{1 - M_\infty^2}} \tag{58}\]

and which diverges as the free-stream Mach number approaches one, a result derived for a lifting aerofoil by Glauert 1928 and resting on the boundary-layer conception introduced by Prandtl 1928. That singularity is not physical, it is the breakdown of the linearization, and the fact that the standard theory of the 1940s went singular at exactly the condition of interest is a large part of why the X-1 existed. There was no theory to trust and no tunnel that worked, because conventional closed-throat tunnels choke near Mach one, as Hansen 1987 records of the Langley tunnels, and gave no usable data in that band. The transonic regime and the sound barrier as a cultural and technical object are treated at length in Hallion 1972 Supersonic Flight and Gunston 1992 Faster Than Sound, and the theoretical lineage through Ludwig Prandtl, Theodore von Karman, and Adolf Busemann is set out in Anderson 1997 A History of Aerodynamics.

The critical Mach number is the free-stream Mach number at which the flow first reaches sonic conditions somewhere on the body, and the drag divergence Mach number is the higher value at which the drag coefficient begins to rise steeply, conventionally defined by

\[\left. \frac{\partial C_D}{\partial M} \right|_{M = M_{DD}} = 0.1 \tag{59}\]

The critical Mach number is found by setting the compressible peak suction equal to the pressure coefficient corresponding to sonic flow,

\[C_{p,\text{crit}} = \frac{2}{\gamma M_\infty^2} \left[ \left( \frac{1 + \frac{\gamma - 1}{2} M_\infty^2}{1 + \frac{\gamma - 1}{2}} \right)^{\frac{\gamma}{\gamma - 1}} - 1 \right] \tag{60}\]

and solving for the free-stream Mach number at which the two curves intersect. Sweep raises that value, because simple sweep theory says only the component of the free stream normal to the leading edge governs the compressible behaviour,

\[M_{\text{eff}} = M_\infty \cos \Lambda, \qquad C_{L\alpha, \Lambda} = C_{L\alpha} \cos \Lambda \tag{61}\]

with $\Lambda$ the sweep angle. That relation is the entire aerodynamic argument for the swept wing, and its cost in lift-curve slope makes swept wings land fast.

The rise itself is wave drag, the momentum lost to shock waves, and for a slender body of revolution at supersonic speed the minimum attainable wave drag for a given length and volume is the Sears-Haack result of Sears 1947,

\[\frac{D_w}{q} = \frac{9 \pi}{2} \left( \frac{A_{\max}}{L} \right)^2 \tag{62}\]

with $A_{\max}$ the maximum cross-sectional area and $L$ the body length, attained by the area distribution

\[A(x) = A_{\max} \left[ 4 \frac{x}{L} \left( 1 - \frac{x}{L} \right) \right]^{3/2} \tag{63}\]

The corresponding result for a lifting surface is the linearized supersonic solution of Ackeret 1925, which for a thin flat plate at angle of attack $\alpha$ gives

\[C_L = \frac{4 \alpha}{\sqrt{M_\infty^2 - 1}}, \qquad C_{D,\text{wave}} = \frac{4 \alpha^2}{\sqrt{M_\infty^2 - 1}} \tag{64}\]

so that supersonic wave drag due to lift is proportional to the square of incidence and falls with Mach number, the opposite of the transonic behaviour, and this fall is why the drag curve has a peak rather than a plateau. The relation says that wave drag scales as the square of the fineness of the cross-sectional area distribution, and that scaling supplies the theoretical content behind the area rule of Richard T. Whitcomb, published as Whitcomb 1952 and extended to the supercritical airfoil in Whitcomb and Clark 1965. The area rule states that the transonic wave drag of a complete configuration depends primarily on the axial distribution of total cross-sectional area rather than on the shapes that produce it, so a fuselage waisted where the wing joins can recover most of the drag penalty of the wing. Stated as a design rule, the requirement is that the total axial area distribution

\[A_{\text{total}}(x) = A_{\text{fuselage}}(x) + A_{\text{wing}}(x) + A_{\text{nacelle}}(x) \tag{65}\]

should approximate the smooth Sears-Haack distribution above rather than carrying a bump where the wing intersects. The complementary planform insight is the swept wing of Jones 1947, whose author Robert Thomas Jones derived it independently of the German work, and whose logical extension is the delta wing, analysed at low aspect ratio by Jones 1946. The waverider configuration that the X-51 name records was proposed by Nonweiler 1959 as a shape generated from a known shock solution rather than fitted to one. The slender-body and thin-wing theory underlying all of it is developed in Ashley and Landahl 1965 Aerodynamics of Wings and Bodies, Küchemann 1978 The Aerodynamic Design of Aircraft, and Bertin and Cummings 2013 Aerodynamics for Engineers. The X-series intersects this history directly, since the area rule emerged from Langley work in 1952 described by Hansen 1987 Engineer in Charge and Hansen 2004 The Bird Is on the Wing, and was validated on aircraft whose transonic databases came from X-1 and follow-on flights.

Propulsion and the Mass Budget

Rocket thrust follows from momentum and pressure terms as

\[F = \dot{m} v_e + (p_e - p_a) A_e \tag{66}\]

with $\dot{m}$ the propellant mass flow in kilograms per second, $v_e$ the exhaust velocity in metres per second, $p_e$ and $p_a$ the exit-plane and ambient pressures in pascals, and $A_e$ the nozzle exit area in square metres. The mass flow through a choked throat of area $A_t$ is fixed by the chamber conditions,

\[\dot{m} = \frac{p_0 A_t}{\sqrt{T_0}} \sqrt{\frac{\gamma}{R}} \left( \frac{2}{\gamma + 1} \right)^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{67}\]

which separates the chamber problem from the nozzle problem and lets performance be written as the product of a characteristic velocity and a thrust coefficient,

\[c^{*} = \frac{p_0 A_t}{\dot{m}}, \qquad C_F = \frac{F}{p_0 A_t}, \qquad I_{sp} = \frac{c^{*} C_F}{g_0} \tag{68}\]

with $c^{*}$ measuring the quality of the combustion and $C_F$ the quality of the expansion. The pressure term is why a rocket aircraft gains thrust with altitude and why the X-1 and X-15 both performed better high than low. The standard references are Sutton and Biblarz 2016 Rocket Propulsion Elements and Huzel and Huang 1992 Modern Engineering for Design of Liquid-Propellant Rocket Engines, with the propellant tradeoff space covered on this blog in A217 Rocket Propellant Chemistry. Collecting both terms into an effective exhaust velocity and normalizing by standard gravity gives the specific impulse

\[I_{sp} = \frac{F}{\dot{m} g_0} \tag{69}\]

in seconds, the propulsion figure of merit the series uses throughout. Integrating the momentum equation for a vehicle of initial mass $m_0$ and final mass $m_f$ gives the Tsiolkovsky rocket equation

\[\Delta v = I_{sp} g_0 \ln \frac{m_0}{m_f} \tag{70}\]

which sizes every rocket aircraft in the series. Apply it to the X-15. The Reaction Motors XLR99 delivered about 254 kilonewtons at a specific impulse that Jenkins 2000a gives as 256 to 276 seconds burning liquid oxygen and anhydrous ammonia, replacing the XLR11 that powered the X-1 and the early X-15 flights. Taking the upper value, the launch mass of 15,195 kilograms and the burnout mass of 6577 kilograms that the North American X-15 entry gives as 33,500 and 14,500 pounds give

\[\Delta v = 276 \times 9.807 \times \ln \frac{15{,}195}{6577} = 2707 \times 0.8374 = 2267 \ \text{metres per second} \tag{71}\]

against an observed maximum of about 1830 metres per second for the basic airframe, the Mach 6.04 and 4,093 miles per hour of the fastest flight the same entry lists before the X-15A-2. The aircraft was air-launched from a Boeing B-52 Stratofortress at about Mach 0.82 and 45,500 feet [Jenkins 2000a], roughly 240 metres per second, so the ideal budget exceeds the achieved increment by about 680 metres per second, and on this accounting that difference is the gravity and drag loss on a steep climbing profile. Those losses are the integrals

\[\Delta v_{\text{grav}} = \int_0^{t_b} g \sin \gamma \, dt, \qquad \Delta v_{\text{drag}} = \int_0^{t_b} \frac{D}{m} \, dt \tag{72}\]

taken over the burn, so that the budget closes as

\[\Delta v_{\text{ideal}} = \Delta v_{\text{achieved}} + \Delta v_{\text{grav}} + \Delta v_{\text{drag}} \tag{73}\]

and the residual quoted above is attributed here to the two loss terms. The residual is about thirty percent of the ideal budget, and the published masses alone cannot show how it divides between the two terms. Staging and boost arrangements of the same kind at much smaller scale are worked in A120 Staged and Boosted Propulsion.

The mass budget is conventionally expressed as fractions of launch mass. With $m_p$ the propellant mass, $m_s$ the structural and systems mass, and $m_i$ the instrumentation and payload mass,

\[\frac{m_p}{m_0} + \frac{m_s}{m_0} + \frac{m_i}{m_0} = 1 \tag{74}\]

with the initial thrust-to-weight ratio

\[\frac{T}{W} = \frac{F}{m_0 g_0} \tag{75}\]

setting how much of the burn is spent fighting gravity. The propellant mass fraction is the quantity a rocket aircraft designer fights for. For the X-15 the propellant fraction from the masses above is about 0.57, which is low for a rocket vehicle and high for an aircraft, and that intermediate value sums up what a rocket research aircraft is.

Airbreathing propulsion substitutes atmospheric oxygen and changes the accounting completely. For a turbojet the figure of merit is thrust-specific fuel consumption $c$, in kilograms of fuel per newton second, and the range for cruising flight follows from the Breguet relation

\[R = \frac{V}{c g_0} \frac{L}{D} \ln \frac{W_0}{W_1} \tag{76}\]

with $W_0$ and $W_1$ the initial and final weights. The efficiency behind that propulsive term decomposes into a thermal and a propulsive factor,

\[\eta_{th} = 1 - \frac{1}{\pi_c^{\frac{\gamma - 1}{\gamma}}}, \qquad \eta_p = \frac{2}{1 + u_e / u_\infty}, \qquad \eta_0 = \eta_{th} \, \eta_p \tag{77}\]

with $\pi_c$ the compressor pressure ratio, and the opposition between the two factors is the whole of engine cycle selection, since raising exhaust velocity raises thermal efficiency and lowers propulsive efficiency. The Breguet relation makes explicit that range is the product of a propulsive term, an aerodynamic term, and a structural term, and the X-series contains programmes attacking each factor separately. Hill and Peterson 1991 Mechanics and Thermodynamics of Propulsion and Mattingly 2006 Elements of Propulsion give the cycle analysis, and A118 Propulsion and Power Sizing works the equivalent sizing at small scale.

For ramjet and scramjet propulsion the thrust follows from the momentum change across the engine,

\[F = \dot{m}_a \left[ (1 + f) u_e - u_\infty \right] \tag{78}\]

with $\dot{m}_a$ the captured air mass flow, $f$ the fuel-to-air ratio, and $u_e$ and $u_\infty$ the exit and free-stream velocities. Because the exit and free-stream velocities are both large and their difference is small at high Mach number, thrust is a small difference of large numbers, which is why scramjet net thrust is so hard to demonstrate and why the X-43 and X-51 programmes were structured around proving positive net thrust at all rather than around achieving a particular value, as recounted in McClinton 2006 and Marshall et al. 2005b. The inlet imposes a starting constraint identified by Kantrowitz and Donaldson 1945. A supersonic inlet swallows its shock only if the throat is large enough to pass the captured mass flow after the total pressure loss across a normal shock at the lip. With the isentropic area relation

\[\frac{A}{A^{*}} = \frac{1}{M} \left[ \frac{2}{\gamma + 1} \left( 1 + \frac{\gamma - 1}{2} M^2 \right) \right]^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{79}\]

and the normal shock total pressure ratio

\[\frac{p_{02}}{p_{01}} = \left[ \frac{(\gamma + 1) M_1^2}{(\gamma - 1) M_1^2 + 2} \right]^{\frac{\gamma}{\gamma - 1}} \left[ \frac{\gamma + 1}{2 \gamma M_1^2 - (\gamma - 1)} \right]^{\frac{1}{\gamma - 1}} \tag{80}\]

the self-starting condition on the contraction ratio becomes

\[\frac{A_{th}}{A_i} \ge \frac{p_{01}}{p_{02}} \cdot \frac{1}{\left( A / A^{*} \right)_{M_i}} \tag{81}\]

which tightens rapidly with flight Mach number and forces fixed-geometry hypersonic inlets to be designed with far less contraction than steady-state performance alone would suggest, and the combustor imposes a residence-time constraint that reduces to a Damkohler condition,

\[\tau_{\text{res}} = \frac{L_c}{u_c} > \tau_{\text{ign}} \tag{82}\]

with $L_c$ the combustor length and $u_c$ the internal flow velocity, and at Mach 7 the internal flow crosses a combustor of realistic length in under a millisecond. The experimental programme behind that inequality is described by Billig 1993 and reviewed across four decades by Curran 2001, with the X-51 flight demonstration reported by Hank et al. 2008. That inequality is the keystone of the hypersonic airbreathing branch of the series, and Heiser and Pratt 1994 Hypersonic Airbreathing Propulsion and Curran and Murthy 2000 Scramjet Propulsion develop it.

Structures and Aeroelasticity

The primary structural sizing parameter is wing loading, and the primary load path is the root bending moment. For a wing of semi-span $b/2$ carrying the elliptic spanwise lift distribution

\[\ell(y) = \frac{4 L}{\pi b} \sqrt{1 - \left( \frac{2 y}{b} \right)^2} \tag{83}\]

at load factor $n$, the root bending moment is

\[M_{\text{root}} = \frac{2 n W}{3 \pi} \cdot \frac{b}{2} \tag{84}\]

which scales linearly in span and drives the spar cap area. The required cap area for an allowable stress $\sigma_{\text{allow}}$ and structural depth $h_s$ is

\[A_{\text{cap}} = \frac{M_{\text{root}}}{\sigma_{\text{allow}} h_s} \tag{85}\]

The coupling to the thermal problem enters twice. The allowable stress falls with temperature, and a constrained structure heated non-uniformly develops thermal stress directly,

\[\sigma_{\text{th}} = \frac{E \alpha_T \Delta T}{1 - \nu} \tag{86}\]

with $E$ the elastic modulus, $\alpha_T$ the coefficient of thermal expansion, $\nu$ the Poisson ratio, and $\Delta T$ the temperature difference across the constrained region. On a skin heated to 1000 kelvin above a cool substructure this term alone can exceed the mechanical stress, which is why high-speed airframes use floating skin panels and corrugated webs rather than rigid monocoque. The relevant material figure of merit is therefore not strength but temperature-derated specific strength,

\[\left. \frac{\sigma_{\text{allow}}(T)}{\rho_m} \right|_{T = T_{\text{skin}}} \tag{87}\]

evaluated at the skin temperature the trajectory produces rather than at room temperature. Aluminium retains useful strength to roughly 400 kelvin, titanium to roughly 800 kelvin, and Inconel X to roughly 920 kelvin, the 1,200 degrees Fahrenheit at which Jenkins 2000a reports that its strength and creep characteristics justified its selection for the X-15 wing, and each of those thresholds appears as a design decision somewhere in the X-series. The airframe structural methods are given in Bruhn 1973 Analysis and Design of Flight Vehicle Structures, Niu and Niu 1988 Airframe Structural Design, and Megson and Aircraft structures for engineering students n.d. Aircraft Structures for Engineering Students, with the measured flight loads on the X-15 reported by Kordes and Noll and the same sizing logic at model scale in A127 Structures and the Flight Envelope.

Aeroelasticity supplies the constraint that made one of these aircraft possible. The field is defined by Bisplinghoff et al. 1955 Aeroelasticity and Fung 1955 An Introduction to the Theory of Aeroelasticity, with modern treatments in Hodges and Pierce 2011, Dowell and A modern course in aeroelasticity 2014 A Modern Course in Aeroelasticity, and Wright et al. 2007. The torsional stiffness of a closed thin-walled box of enclosed area $A_m$, wall thickness $t$, and length $\ell_w$ follows from the Bredt-Batho relation, and the aeroelastic problem it feeds was named and bounded by Collar 1946,

\[K_\theta = \frac{G J}{\ell_w}, \qquad J = \frac{4 A_m^2}{\oint \frac{ds}{t}} \tag{88}\]

with $G$ the shear modulus. Every aeroelastic result below depends on this stiffness. Consider a two-dimensional typical section with torsional stiffness $K_\theta$ in newton metres per radian, elastic axis located a distance $e$ in metres behind the aerodynamic centre, reference area $S$, and lift-curve slope $C_{L\alpha}$ per radian. An increment of twist produces an increment of lift, which produces an increment of aerodynamic moment about the elastic axis, which produces further twist. The loop has unity gain at the divergence dynamic pressure

\[q_D = \frac{K_\theta}{e S C_{L\alpha}} \tag{89}\]

above which the static aeroelastic response is unbounded and the wing fails. Taking representative values of $K_\theta = 5.0 \times 10^{5}$ newton metres per radian, $e = 0.20$ metres, $S = 10$ square metres, and $C_{L\alpha} = 4.5$ per radian gives

\[q_D = \frac{5.0 \times 10^{5}}{0.20 \times 10 \times 4.5} = 5.6 \times 10^{4} \ \text{pascals} \tag{90}\]

or 56 kilopascals, which at sea-level density corresponds to a true airspeed of 301 metres per second. The number is representative, not specific to any aircraft, and it establishes the order of magnitude against which the X-29 discussion later in the series should be read.

Sweep modifies this relation decisively, as Diederich and Budiansky 1948 established. For an aft-swept wing, bending deflection reduces the streamwise angle of attack at the tip, which unloads the tip and raises $q_D$. For a forward-swept wing the coupling reverses. The mechanism is that a swept wing bending upward through vertical deflection $w(y)$ changes the streamwise incidence by

\[\Delta \alpha_{\text{eff}} = -\frac{\partial w}{\partial y} \sin \Lambda \tag{91}\]

whose sign is set by the sweep angle. For aft sweep the increment is negative and stabilizing. For forward sweep, where $\Lambda$ is negative, bending deflection increases the streamwise angle of attack at the tip, which loads the tip further, and $q_D$ falls, in the classical metallic case to values below any useful flight speed. That is why forward sweep was abandoned after the Junkers Ju 287, and why the X-29 exists. Aeroelastic tailoring of a composite cover, in which the fibre orientation is chosen so that bending induces a compensating nose-down twist, converts the divergence problem from a structural mass penalty into a laminate design problem. That conversion was proposed by Krone 1975 and analysed by Weisshaar 1980b and Weisshaar 1981, and the composite mechanics behind it are in Jones 1998 Mechanics of Composite Materials, Tsai and Hahn 1980 Introduction to Composite Materials, and Niu 1992 Composite Airframe Structures. The X-29 was built to determine whether that conversion held in flight, its composites serving to control the divergent twisting of the forward-swept wing, and the design of the aircraft follows from that one question.

Dynamic aeroelasticity introduces flutter, the coupling of bending and torsion modes into a self-excited oscillation extracting energy from the airstream, the theory of which is Theodorsen 1935 and the history of which is Garrick and Reed 1981. The governing similarity parameter is the reduced frequency

\[k = \frac{\omega b}{V} \tag{92}\]

which measures how many semichords the flow travels in one cycle of the motion and therefore how strongly the unsteady wake affects the loads. The flutter boundary is conventionally reported as a reduced-frequency and mass-ratio problem through the flutter speed index

\[F_i = \frac{V_f}{b \omega_\alpha \sqrt{\mu_m}}, \quad \mu_m = \frac{m_w}{\pi \rho b^2} \tag{93}\]

with $V_f$ the flutter speed, $b$ the semichord, $\omega_\alpha$ the uncoupled torsional natural frequency, $m_w$ the wing mass per unit span, and $\mu_m$ the mass ratio. Flutter clearance is a principal reason envelope expansion proceeds by small increments in dynamic pressure rather than by direct assault on the target condition. The Lockheed Martin X-56 exists to study active suppression of this coupling on a very flexible wing.

Aerothermodynamics

Above roughly Mach 3 the thermal problem displaces the structural problem as the binding constraint. The driver is the stagnation temperature, which for an adiabatic deceleration of the free stream to rest is

\[T_0 = T_\infty \left( 1 + \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{94}\]

and which rises as the square of Mach number. On a surface with a boundary layer the relevant quantity is the recovery temperature, which falls short of the stagnation temperature by the recovery factor

\[r = Pr^{1/2} \ \text{(laminar)}, \qquad r = Pr^{1/3} \ \text{(turbulent)} \tag{95}\]

giving

\[T_r = T_\infty \left( 1 + r \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{96}\]

For the X-15A-2 at Mach 6.7 and 31.1 kilometres, where $T_\infty = 227$ kelvin, the stagnation temperature is 2265 kelvin and the turbulent recovery temperature with $r = 0.89$ is 2041 kelvin. Both figures exceed the melting point of aluminium by a wide margin and exceed the useful limit of Inconel X, which is why the aircraft radiated and why the record flight required an ablative coating. The measured heating on the aircraft is reported by Banner et al. 1962, and the general treatment is Truitt 1960 Fundamentals of Aerodynamic Heating.

The heat crossing the surface is driven by the difference between the recovery temperature and the wall temperature,

\[\dot{q}_{\text{conv}} = h_c \left( T_r - T_w \right) \tag{97}\]

with $h_c$ the convective coefficient in watts per square metre kelvin, conventionally non-dimensionalized as the Stanton number and estimated from skin friction through the Reynolds analogy in the form given by Eckert 1956,

\[St = \frac{h_c}{\rho V c_p}, \qquad St \approx \frac{C_f}{2} Pr^{-2/3} \tag{98}\]

The theoretical stagnation-point result behind the engineering correlation used below is that of Fay and Riddell,

\[\dot{q}_s = 0.763 \, Pr^{-0.6} \left( \rho_e \mu_e \right)^{0.4} \left( \rho_w \mu_w \right)^{0.1} \sqrt{\frac{du_e}{dx}} \left( h_0 - h_w \right) \tag{99}\]

with the subscripts $e$ and $w$ denoting boundary-layer edge and wall conditions, $h_0$ and $h_w$ the corresponding enthalpies, and the stagnation velocity gradient given by the Newtonian estimate, with the compressible boundary-layer profiles underlying both from Chapman and Rubesin 1949 and the blunt-body solution from Lees 1956,

\[\frac{du_e}{dx} = \frac{1}{R_n} \sqrt{\frac{2 \left( p_s - p_\infty \right)}{\rho_s}} \tag{100}\]

The heat flux entering the structure at a stagnation point is given to good accuracy by the correlation of Sutton and Graves 1971,

\[\dot{q}_s = k \sqrt{\frac{\rho_\infty}{R_n}} \, V_\infty^3 \tag{101}\]

with $R_n$ the effective nose radius in metres and $k = 1.7415 \times 10^{-4}$ in SI units for air. The theoretical foundation is Fay and Riddell 1958, and the survey of competing correlations is Tauber 1989. The cube dependence on velocity makes hypersonic heating a threshold phenomenon rather than a gradual one. The inverse square root dependence on nose radius drives high-speed vehicles toward blunt shapes, the insight of Allen and Eggers 1958 and the foundation of every reentry shape in the series. Evaluating for the X-15A-2 at 2021 metres per second, a density of 0.0157 kilograms per cubic metre, and an assumed effective nose radius of 0.10 metres gives

\[\dot{q}_s = 1.7415 \times 10^{-4} \times \sqrt{\frac{0.0157}{0.10}} \times 2021^3 = 5.7 \times 10^{5} \ \text{watts per square metre} \tag{102}\]

or 570 kilowatts per square metre. Whether the structure can be treated as isothermal through its thickness is decided by the Biot number

\[Bi = \frac{h_c t_w}{k_w} \tag{103}\]

with $t_w$ the wall thickness and $k_w$ the wall conductivity, and for the thin metallic skins used throughout this series $Bi \ll 1$, so a lumped transient balance applies,

\[\rho_w c_w t_w \frac{dT_w}{dt} = \dot{q}_{\text{conv}} - \varepsilon \sigma_{SB} T_w^4 \tag{104}\]

whose steady state is the radiation equilibrium below and whose transient is the heat-soak problem that decides whether a short exposure is survivable. A structure that cannot conduct the heat away must radiate it, and the radiation equilibrium wall temperature follows from the Stefan-Boltzmann law as

\[T_{\text{eq}} = \left( \frac{\dot{q}_s}{\varepsilon \sigma_{SB}} \right)^{1/4} \tag{105}\]

with $\varepsilon$ the surface emissivity and $\sigma_{SB} = 5.670 \times 10^{-8}$ watts per square metre per kelvin to the fourth. At $\varepsilon = 0.8$ this gives $T_{\text{eq}} = 1880$ kelvin, which is far above the roughly 920 kelvin working limit of Inconel X. The arithmetic explains the historical fact directly. The X-15A-2 flew its Mach 6.7 flight coated in MA-25S, an ablator developed by the Martin Company, and it returned damaged, the heating around its dummy ramjet having burned through the ramjet pylon [Jenkins 2000a].

For vehicles that enter rather than cruise, the governing parameter is the ballistic coefficient

\[\beta = \frac{m}{C_D A} \tag{106}\]

in kilograms per square metre. Taking the exponential atmosphere

\[\rho(h) = \rho_0 \, e^{-h / H} \tag{107}\]

with $H$ the scale height, the Allen-Eggers solution for ballistic atmospheric entry gives the velocity profile

\[V(h) = V_e \exp \left[ -\frac{\rho_0 H}{2 \beta \sin \gamma_e} e^{-h / H} \right] \tag{108}\]

from which the peak deceleration follows as

\[a_{\max} = \frac{V_e^2 \sin \gamma_e}{2 e H} \tag{109}\]

with $V_e$ the entry speed, $\gamma_e$ the entry flight path angle, and $e$ the base of natural logarithms. The striking feature is that peak deceleration is independent of the ballistic coefficient, which decides only the altitude at which it occurs,

\[h_{a,\max} = H \ln \frac{\rho_0 H}{\beta \sin \gamma_e} \tag{110}\]

so a light blunt vehicle decelerates high in thin air and a dense slender one decelerates low in dense air, at the same peak load. The two quantities a thermal protection system must survive are the peak rate and the integrated load

\[Q = \int_0^{t_f} \dot{q}_s \, dt \tag{111}\]

and these are traded against one another rather than minimized together, because a shallow lifting entry lowers the peak rate while lengthening the exposure and therefore raising $Q$. The extension to lifting entry is Chapman 1958 and the comparative performance analysis that established the lifting-entry case is Eggers et al. 1958, with book-length treatments in Vinh et al. 1980 Hypersonic and Planetary Entry Flight Mechanics, Regan and Anandakrishnan 1993 Dynamics of Atmospheric Re-Entry, and Loh 1963 Dynamics and Thermodynamics of Planetary Entry. Lifting entry, which the Boeing X-20 Dyna-Soar, the X-23, the Martin Marietta X-24A and X-24B, the Boeing X-37, and the NASA X-38 programmes all explored in different forms, breaks that independence by adding a lift term and trading peak heating rate against total heat load. The primary flight record for that lineage includes the control-surface hinge moments measured on the X-24A in Tang and Pearson 1973 and the programme account of Manke and Love 1975 for the X-24B. The lifting-body lineage is recounted by Reed and Lister 1997 Wingless Flight, the entry-and-recovery history by Launius and Jenkins 2012 Coming Home, and the Dyna-Soar programme specifically by Houchin 2006b.

Stability and Control

Longitudinal static stability requires that a disturbance in angle of attack produce a restoring moment, which requires the pitching moment derivative to be negative,

\[C_{m\alpha} = C_{L\alpha} \left( \frac{x_{cg} - x_{ac}}{\bar{c}} \right) < 0 \tag{112}\]

with $x_{cg}$ and $x_{ac}$ the centre of gravity and aerodynamic centre positions and $\bar{c}$ the mean aerodynamic chord. The neutral point is the centre of gravity position at which that restoring tendency vanishes, defined implicitly by

\[\left. \frac{\partial C_m}{\partial C_L} \right|_{x_{cg} = x_{np}} = 0 \tag{113}\]

and for a rigid airframe it coincides with the aerodynamic centre of the complete configuration. The normalized distance from it is the static margin

\[SM = \frac{x_{ac} - x_{cg}}{\bar{c}} \tag{114}\]

and its variation with Mach number is one of the central difficulties of transonic and supersonic flight, because the aerodynamic centre migrates aft as the flow becomes supersonic, typically from about the quarter chord to about the half chord. That migration produces a large nose-down trim change and a large increase in longitudinal static stability, and it accounts for a substantial part of what pilots in the late 1940s were describing when they reported controls becoming ineffective near Mach one. The standard treatments of flight dynamics are Etkin et al. 1959 Dynamics of Flight, Nelson 1998 Flight Stability and Automatic Control, Stevens et al. 2015 Aircraft Control and Simulation, Stengel and Flight dynamics 2004 Flight Dynamics, and McRuer et al. 1990 Aircraft Dynamics and Automatic Control.

The two longitudinal dynamic modes are the short period and the phugoid. The short period frequency for a conventional configuration is approximately

\[\omega_{sp} \approx \sqrt{\frac{Z_\alpha M_q}{V} - M_\alpha} \tag{115}\]

in the standard dimensional stability derivative notation, with damping ratio

\[\zeta_{sp} \approx -\frac{M_q + M_{\dot\alpha} + Z_\alpha / V}{2 \, \omega_{sp}} \tag{116}\]

The mode is fast enough for the pilot to handle as an immediate response. The phugoid is slow, lightly damped, and to first order independent of the aerodynamics, with frequency

\[\omega_{ph} \approx \frac{g \sqrt{2}}{V} \tag{117}\]

which for an aircraft at 300 metres per second gives a period of about 136 seconds. Its damping ratio depends only on the aerodynamic efficiency,

\[\zeta_{ph} \approx \frac{1}{\sqrt{2}} \frac{1}{L / D} \tag{118}\]

so a clean high lift-to-drag airframe has a persistent, poorly damped phugoid, a nuisance in cruise and a hazard on an unpowered approach of the kind every rocket research aircraft in this series had to fly. Lateral-directional stability requires positive directional stiffness $C_{n\beta}$ and negative dihedral effect $C_{l\beta}$, and the coupling between them produces the Dutch roll mode, whose frequency and the roll subsidence time constant are approximately

\[\omega_{dr} \approx \sqrt{\frac{N_\beta}{I_z}}, \qquad \tau_r \approx -\frac{I_x}{L_p} \tag{119}\]

with the spiral mode stable when

\[L_\beta N_r - L_r N_\beta > 0 \tag{120}\]

This condition fails on many swept-wing configurations, where it may call for artificial stabilization. The same modal structure at model scale is worked in A122 Stability Control and Configuration and A123 Dynamic Stability and Control.

The X-series contains the canonical demonstration that these modes do not tell the whole story. Inertia coupling, in which a rapid roll about an axis misaligned with the principal inertia axis pumps energy into pitch and yaw, arises from the gyroscopic terms in the Euler moment equations,

\[I_y \dot{q} = M + \left( I_z - I_x \right) p r, \qquad I_z \dot{r} = N + \left( I_x - I_y \right) p q \tag{121}\]

which vanish in single-axis analysis and grow with the product of roll rate and the inertia difference. Divergence follows when the roll rate approaches the lower of the two aerodynamic natural frequencies,

\[\omega_\alpha = \sqrt{\frac{-M_\alpha}{I_y}}, \qquad \omega_\beta = \sqrt{\frac{N_\beta}{I_z}}, \qquad p_{\text{crit}} \approx \min \left( \omega_\alpha, \omega_\beta \right) \tag{122}\]

so an airframe with most of its mass in a long fuselage rather than in the wings, which describes the supersonic research aircraft of this series generally, has a low critical roll rate because $I_z - I_x$ is large. The effect is governed by the inertia ratios and is invisible to linearized single-axis analysis. It was predicted by Phillips 1948 before it was encountered. The Bell X-2 and the X-3 both met it violently, the X-2 fatally, and the resulting understanding changed how roll rates were specified across the fleet. The later high-angle-of-attack and post-stall work of the Rockwell-MBB X-31 and the flight-control research of the General Dynamics X-62 VISTA descend directly from this thread, as does the X-29 control work reported by Hicks and Huckabine 1989 and Bosworth and Stoliker 1996 alongside Putnam 1983, Sefic and Maxwell 1986, and Bosworth and Cox 1989.

Where dynamic pressure falls below the level at which aerodynamic surfaces produce useful moments, control must come from reaction jets. The required time for a manoeuvre through angle $\Delta \phi$ about an axis of inertia $I$ using thrusters of moment arm $\ell$ and thrust $F_t$ in a bang-bang minimum-time manoeuvre is

\[\Delta t = 2 \sqrt{\frac{I \Delta \phi}{F_t \ell}} \tag{123}\]

and the propellant required follows from the total impulse and the thruster specific impulse,

\[m_{p, \text{RCS}} = \frac{\int F_t \, dt}{I_{sp, \text{RCS}} \, g_0} \tag{124}\]

The handover between the two control systems occurs at the dynamic pressure where aerodynamic and reaction authority are equal,

\[q_{\times} = \frac{F_t \ell}{S b \, C_{l \delta} \, \delta_{\max}} \tag{125}\]

below which the aerodynamic surfaces cannot produce the required moment at full deflection. The X-15 carried hydrogen peroxide reaction controls for this regime, after small reaction rockets had first been flown on the X-1B. It was the first aircraft in the series whose missions required a handover between aerodynamic and reaction control authority.

Instrumentation and Data Reduction

An instrument that cannot resolve the quantity is a flight wasted, so the instrumentation sizing deserves the same treatment as the airframe. Flight testing as a discipline is set out in Kimberlin 2003 Flight Testing of Fixed-Wing Aircraft and Ward et al. 2006 Introduction to Flight Test Engineering. The combined standard measurement uncertainty of a derived quantity $y = f(x_1, \dots, x_n)$ follows from the propagation of uncertainty relation

\[u_c^2(y) = \sum_{i=1}^{n} \left( \frac{\partial f}{\partial x_i} \right)^2 u^2(x_i) \tag{126}\]

which acquires a covariance term

\[2 \sum_{i < j} \frac{\partial f}{\partial x_i} \frac{\partial f}{\partial x_j} u(x_i, x_j) \tag{127}\]

whenever the inputs share a calibration source, as thrust and mass flow generally do. The uncorrelated form is developed in Taylor 1997 An Introduction to Error Analysis and Bevington and Robinson 2002 Data Reduction and Error Analysis. The technique for extracting drag from an accelerating flight, together with its error budget, was set out by Beeler et al. 1956, and the instrumentation fit that made the X-15 measurements possible is described by Sanderson 1964. The important structural feature of flight-test data reduction is that the quantities of interest are frequently small differences of large measured numbers, which amplifies uncertainty. Drag in accelerating flight is obtained from

\[D = T - m a_x \tag{128}\]

with $T$ the thrust, $m$ the instantaneous mass, and $a_x$ the measured axial acceleration. Take the X-1 with an XLR11 delivering its rated 26,700 newtons, a mass of 5000 kilograms, and a measured axial acceleration of 3.0 metres per second squared, so that $D = 26{,}700 - 15{,}000 = 11{,}700$ newtons. Suppose thrust is known to three percent, mass to half a percent, and acceleration to one and a half percent. Then

\[u_c(D) = \sqrt{(801)^2 + (237)^2} = 835 \ \text{newtons} \tag{129}\]

which is 7.1 percent of the drag. A three percent thrust uncertainty has become a 7.1 percent drag uncertainty, and the amplification factor of 2.4 is very nearly the thrust-to-drag ratio of 2.28. The relation holds in general. For $D = T - X$ the relative uncertainty propagates as

\[\frac{u(D)}{D} = \frac{T}{D} \sqrt{\left( \frac{u(T)}{T} \right)^2 + \left( \frac{X}{T} \right)^2 \left( \frac{u(X)}{X} \right)^2} \tag{130}\]

so that differencing amplifies relative uncertainty by approximately the ratio of the larger quantity to the difference. For the same reason thrust calibration matters as much as the accelerometer in this method.

Sampling imposes its own constraint. A structural mode at frequency $f_{\max}$ requires a sample rate satisfying the Nyquist-Shannon sampling theorem, established in Nyquist 1928,

\[f_s > 2 f_{\max} \tag{131}\]

with practical flight-test rates set several times higher to permit reconstruction without aggressive filtering. Amplitude resolution imposes a parallel limit, since a $b$-bit converter spanning a full-scale range $FS$ quantizes with step and noise

\[\Delta = \frac{FS}{2^b}, \qquad \sigma_q = \frac{\Delta}{\sqrt{12}} \tag{132}\]

giving a signal-to-noise ratio of

\[\text{SNR} \approx 6.02 \, b + 1.76 \ \text{decibels} \tag{133}\]

so that each additional bit adds about six decibels and the word length in the telemetry frame is a direct statement of how finely any measurement can be resolved. The resulting telemetry bit rate for $N_c$ channels sampled at $f_s$ with $b$ bits per word is

\[B = N_c f_s b \tag{134}\]

so that one hundred channels at 200 samples per second and ten bits per word require 200 kilobits per second. Wherever a pulse-code modulation telemetry link carries less than that, the budget forces choices about which measurements are telemetered live and which are recorded on board for post-flight recovery. The hard ceiling is the channel capacity of Shannon 1948,

\[C = B_w \log_2 \left( 1 + \frac{S}{N} \right) \tag{135}\]

with $B_w$ the radio-frequency bandwidth in hertz, and a research aircraft at the far edge of a range at low elevation angle is operating where the signal-to-noise ratio, and therefore $C$, is at its worst precisely when the data matter most. The ground-side computing and simulation infrastructure that consumed those data streams is treated on this blog in A241 Aerospace Simulation and Real-Time Systems and A244 Space Shuttle Software. The instrumentation constraint is therefore a design constraint, not an afterthought, and several articles in this series treat it as such.

The Economics of a Flight Test Programme

A flight research programme is an investment in information, and the sizing relations above allow the investment to be stated quantitatively.

Programme cost decomposes into a development term and a per-flight term,

\[C_{\text{total}} = C_{\text{dev}} + n \, C_{\text{flight}} + n_a C_{\text{airframe}} \tag{136}\]

with $n$ the number of flights and $n_a$ the number of airframes built. The flight count is set by the information requirement derived earlier, and the airframe count is set by attrition. The unit-cost learning effects that govern the airframe term were first quantified in aviation by Wright 1936, whose result is that unit cost falls as a fixed fraction $b$ for every doubling of cumulative output,

\[C_n = C_1 \, n^{\log_2 b} \tag{137}\]

with $b$ near 0.80 for airframe manufacture. At the two and three unit quantities typical of this series the learning curve has barely begun, and research aircraft are correspondingly expensive per airframe.

Attrition sizing is the part usually left implicit. Making it explicit accounts for a persistent pattern in the historical record. Let $p$ denote the probability that a given flight results in loss of the airframe. The number of losses over $n$ flights follows the binomial distribution, and a programme completes its flight card if the number of losses is strictly less than the number of airframes. Requiring completion with probability at least $1 - \alpha$ gives the condition

\[\sum_{i=0}^{n_a - 1} \binom{n}{i} p^i (1-p)^{n-i} \ge 1 - \alpha \tag{138}\]

Evaluate this for the X-1 example, with $n = 25$ flights, a per-flight loss probability of $p = 0.02$, and a required completion confidence of 95 percent. The cumulative probabilities are 0.603 for zero losses, 0.911 for at most one, and 0.987 for at most two. The expected number of losses over the programme is simply

\[\mathbb{E}[\text{losses}] = n p = 0.5 \tag{139}\]

but sizing to the expectation rather than to the tail is the error the condition above is written to avoid. Two airframes fall short of the requirement and three satisfy it, so

\[n_a^{*} = 3 \tag{140}\]

Jenkins et al. 2003 record three airframes of the first-generation Bell X-1, and Jenkins 2000a gives the same number for the North American X-15. The agreement between a binomial attrition calculation and the historical fleet size of the two most heavily flown programmes in the series is not proof that anyone performed this calculation, and this series does not claim they did. It is evidence that experienced programme offices arrived at the same answer by judgement, and it gives the reader a quantitative handle on why fleet sizes cluster where they do. The organizational literature on how such risk judgements are actually made, including Perrow 1984 Normal Accidents, Vaughan 1996 The Challenger Launch Decision, and Sagan 1993 The Limits of Safety, is the appropriate corrective to any purely actuarial reading.

The investment decision itself compares the value of the information against its cost. Let $V(\sigma)$ denote the value of a downstream decision taken with residual uncertainty $\sigma$ in the keystone parameter. The programme is justified when

\[V(\sigma_n) - V(\sigma_0) > C_{\text{total}} \tag{141}\]

where the left-hand side is the expected value of the additional information, formally

\[\text{EVSI} = \mathbb{E}_y \left[ \max_a \mathbb{E}_{\theta \mid y} U(a, \theta) \right] - \max_a \mathbb{E}_\theta U(a, \theta) \tag{142}\]

with $U$ the utility of a downstream decision $a$ taken in the state $\theta$. The structure of $V$ explains why these programmes cluster around moments of architectural commitment. When a national decision to build a fleet, an airframe family, or a launch system hangs on a number, the left-hand side is enormous, and a programme costing what a research aircraft costs is trivially justified. When no such decision is pending, the same programme is not justified at any price, and the X-series is accordingly not uniformly distributed in time but arrives in clusters that track procurement decisions.

The marginal value of an additional flight follows from differentiating the information gain,

\[\frac{\partial I_n}{\partial n} = \frac{1}{2} \cdot \frac{\sigma_m^{-2}}{\sigma_0^{-2} + n \sigma_m^{-2}} \tag{143}\]

which decays as $1/n$. Information from flight test exhibits diminishing returns of a particularly steep kind, and the practical consequence is that programmes should stop well before they run out of money.

The Designation System as a Formal Object

The series treats the designation sequence itself as an object worth analysis, because its irregularities carry information about the institutions that produced it.

Let $D = {1, 2, \dots, 76}$ denote the index set of designations in scope and let $P$ denote the set of programmes. The assignment is safest written as a relation, with no assumption that it is a function,

\[R \subseteq D \times P \tag{144}\]

where $(n, p) \in R$ means that design number $n$ was applied to programme $p$. Four questions follow immediately. Is $R$ total, meaning is every number assigned. Is $R$ a function, meaning does every number correspond to at most one programme. Is $R$ injective, meaning does every programme hold at most one number. Is $R$ monotone in time, meaning does a higher number imply a later assignment. The answer to all four is no, and each failure is a finding.

Totality fails for eleven numbers. The X-39 was reserved on 23 April 1997 for the Future Aircraft Technology Enhancements programme but no written allocation request followed, so it remained officially unassigned. The X-52 was requested in 2006 and refused because of possible confusion with the B-52. The X-58 and the X-67 were passed over because the corresponding slots were consumed by the parallel unmanned Kratos XQ-58 Valkyrie and General Atomics XQ-67A, which draw from the same numeric pool, and Parsch records these three cases among the missing designations. The seven numbers from X-69 through X-75 were leapfrogged entirely, the register listing no allocation between the X-68A and the X-76A. Writing $U$ for the unassigned set, the assignment density is

\[\eta = \frac{|D| - |U|}{|D|} = \frac{76 - 11}{76} = 0.855 \tag{145}\]

so roughly one designation in seven in the nominal range corresponds to nothing.

The relation fails to be a function at the X-44, which was applied both to the tailless delta derivative of the F-22 known as the Lockheed Martin X-44 MANTA and to a separate unmanned programme, and at the X-42, which was officially allocated to an expendable upper-stage demonstrator and later used unofficially for a reusable launch vehicle demonstrator, as Parsch records. A number with two vehicles is a record-keeping collision. The assignment is contested at the X-23, which is generally attributed to the Martin Marietta SV-5D of the Precision Recovery Including Maneuvering Entry programme, or PRIME, while United States Air Force nomenclature records show that X-23A was never formally assigned, according to Parsch. The series states that conflict and leaves it unresolved. The X-41 Common Aero Vehicle of the Falcon Project run by the Defense Advanced Research Projects Agency, or DARPA, is a third kind of gap, being assigned to a vehicle whose specifications have never been released.

Injectivity fails at four pairs, each a single programme holding two numbers. The X-11 and X-12 were both Atlas development vehicles. The X-32 and X-35 were the Boeing and Lockheed Martin demonstrators of the Joint Strike Fighter concept demonstration. The X-46 and X-47 were the Boeing and Northrop Grumman demonstrators for the Navy unmanned combat air vehicle. The X-63 and X-64 were allocated on the same day in 2022 to the Aerospike Rocket Integration and Suborbital Experiment, as Parsch’s register of allocations records. A programme with two numbers is the system counting something other than programmes, and the individual articles say what.

Monotonicity fails once among the design numbers whose first model the register lists. The register carries the X-37B and the X-40B but no first model of either number, so its rows date only their later models. The X-50A was allocated on 13 February 2002 and the X-49A on 23 May 2003, according to the same register, so the higher number came first. Why it did is a question for the X-49 and X-50 articles. The X-76 breaks something different, which is consecutiveness, the expectation that each new number is one more than the last. DARPA announced the Bell Textron X-76 of its Speed and Runway Independent Technologies programme, or SPRINT, in 2026 with the number chosen as a deliberate reference to 1776 for the country’s two hundred and fiftieth anniversary, as stated in the agency announcement, while the next unused sequential number at the time was X-69. The X-76 came after every lower number and so kept the order, and it passed over seven numbers to do so. This matters methodologically and not merely as trivia. A reference work stating that the next available design number is X-69 is describing the next unused sequential slot, not an upper bound on assigned numbers, and reading it as a ceiling excludes a real aircraft. A roster that looks like a sequence should be checked to confirm that it is one.

The assignment rate over the eighty years from the X-1 in 1946 to the X-76 in 2026 is

\[\lambda = \frac{|D| - |U|}{\Delta t} = \frac{65}{80} = 0.81 \ \text{per year} \tag{146}\]

If assignments arrived as a Poisson process the counts per interval would satisfy a variance equal to their mean, so the index of dispersion

\[\mathcal{D} = \frac{s^2}{\bar{x}} \tag{147}\]

would be near unity. Counting assignments by decade gives a value well above one, and the assignments are therefore not close to Poisson. They cluster tightly around the late 1940s and 1950s and again around the late 1990s and 2000s, with a pronounced gap through the 1970s and early 1980s, which agrees with the account of Jenkins et al. 2003 that almost thirty designations were allocated between the late 1940s and the late 1970s before a resurgence in the mid to late 1990s. This series reads those clusters as tracking procurement decision points, defence budget cycles, and the founding of new sponsoring organizations rather than any internal logic of aeronautical research, and the closing article of the series tests that correlation directly.

The Institutional Arrangement

The X-series is a product of a particular institutional arrangement, which Hallion 1984 traces to the first research aircraft programmes of 1945, and which has changed substantially since. Understanding the arrangement explains features of the aircraft that no purely technical account can reach.

The original arrangement was tripartite. A military service, most often the Army Air Forces and later the United States Air Force or the Navy, supplied the requirement and the money. A contractor supplied the airframe. The National Advisory Committee for Aeronautics, and after 1958 NASA, supplied the research programme, the instrumentation, the data reduction, and a substantial part of the aerodynamic design basis. That three-way split explains a great deal, including why the X-1 was flown first by the Air Force with Chuck Yeager at the controls to break the sound barrier and afterward by the NACA to gather the data, and why those two organizations remember the programme differently. The institutional histories are Bilstein 1989a Orders of Magnitude and Bilstein 2001 Flight in America, with the research-centre accounts in Hallion 1984 On the Frontier and Gorn 2001a Expanding the Envelope, and the Langley contribution in Chambers 2000a Partners in Freedom, Chambers 2005 Innovation in Flight, and Chambers and Chambers 2008 Radical Wings and Wind Tunnels.

The physical concentration at Muroc Army Air Field in the California high desert, later Edwards Air Force Base, with the NACA station that became the Dryden and then the Armstrong Flight Research Center alongside it, produced an unusual density of expertise. The site offered the isolation, the year-round flying conditions and the room for takeoff and landing that Hallion 1984 gives as the reasons the research aircraft went there, and the dry lake beds served as landing surfaces, emergency landings among them. The test-pilot culture that grew there is the subject of Hallion 1981 Test Pilots and, in its popular form, Wolfe 1979 The Right Stuff, with first-person accounts in Yeager and Janos 1985, Crossfield and Blair 1960 Always Another Dawn, and Thompson 1992 At the Edge of Space. The contractor side has its own memoir literature in Rich et al. 1994 Skunk Works, Johnson and Smith 1985 Kelly, and Merlin 2009 Design and Development of the Blackbird, while the intellectual lineage runs through Von Kármán and Edson 1967 The Wind and Beyond and Gorn 1992 The Universal Man. Constant 1980 The Origins of the Turbojet Revolution and Anderson 2002a The Airplane supply the longer technological context.

The arrangement changed. The Defense Advanced Research Projects Agency became a sponsor of research aircraft in its own right, and the register names it as sponsor of the X-61A, the X-65A, the X-68A and the X-76A. The Air Force Research Laboratory became a sponsor in parallel. The X-37 passed from NASA to DARPA to the Air Force in the course of its development, and the resulting classification changed what can be said about it. The later series contains vehicles whose sponsor is a laboratory rather than a service, whose airframe is unmanned, and whose data are not public. The military space institutions that now sponsor several of them are treated on this blog in A97 What Does the United States Space Force Do, with the broader domain context in A90 Introduction to Space Studies and A92 Cryptotelemeritocracy for Space Exploitation.

Two consequences follow for this series. First, the availability of documentation is not uniform across the eighty years, and the variation is institutional rather than random. Programmes with a NACA or NASA research component generated technical reports that survive and are public through the NASA Technical Reports Server and the NASA History Office. Programmes sponsored under a classified budget line generally did not, the X-41 being the clearest case. Second, the meaning of the X prefix drifted. It began as a designation for a manned research aircraft built in small numbers to answer a question, and it now covers unmanned demonstrators, technology testbeds, and at least one orbital vehicle whose mission is not disclosed. The closing article treats that drift as the series’ principal historical finding.

A Taxonomy of the Seventy-Two Designations

The seventy-two articles divide by what the record supports rather than by what the aircraft did.

Full treatments cover aircraft that flew, generated public technical reports, and for which a keystone can be identified and its consequences traced through the design. The primary flight literature for the modern members of this class is thinner than for the early ones but it is not absent. Alongside the reusable launch vehicle technology reports for two vehicles that never flew, the X-33 in Cook 1995b and the X-34 in Freeman et al. 1997b, it includes the approach and landing test results for the X-37 in Taylor 2004, the parachute qualification for the X-38 in Stein 2005, the Hyper-X programme status of McClinton et al. 2001 with the aerodynamic database of Engelund et al. 2000, the technology summary of Voland et al. 2005, the flight-determined forces and moments of Davis and White 2008, the transonic flight loads on the Active Aeroelastic Wing in Lokos et al. 2005, the X-56A account of Schaefer and Burnett 2019, the distributed electric propulsion design of Borer et al. 2016, and the inlet distortion testing for the X-59 in Dippold 2022. This class includes the X-1, the X-2, the X-3, the Northrop X-4 Bantam, the Bell X-5, the Ryan X-13 Vertijet, the Bell X-14, the X-15, the Hiller X-18, the Curtiss-Wright X-19, the X-21, the Bell X-22, the X-24, the X-29, the X-31, the X-32, the X-35, the McDonnell Douglas X-36, the X-38, the X-43, the Boeing X-45, the Northrop Grumman X-47B, the X-48, the X-51, the Boeing X-53 Active Aeroelastic Wing, the X-56, the Lockheed Martin X-59 Quesst, and the X-62. These articles carry the full twelve-section order. Two vehicles that never flew receive the same order, the Lockheed Martin X-33, whose vehicle was not completed, and the NASA X-57 Maxwell, which was delivered and tested on the ground and never left the runway as the X-57, because each has a ground record substantial enough to carry it.

Documentation-poor treatments cover aircraft that existed but generated little surviving public record, aircraft cancelled before flight, and aircraft whose programmes remain partly classified. This class includes the Convair X-6 nuclear-powered bomber testbed, the Lockheed X-7 and Lockheed X-17 propulsion and reentry testbeds, the Aerobee sounding rocket designated X-8, the Bell X-9 Shrike and North American X-10 missile development airframes, the X-11 and X-12 Atlas development vehicles, the Bell X-16 reconnaissance aircraft cancelled in favour of the Lockheed U-2, the X-20, the Bensen X-25, the Schweizer X-26 Frigate, the Lockheed X-27, the Osprey flown as the X-28A, the X-30, the Orbital Sciences X-34, the Boeing X-40, the Boeing X-46, the Piasecki X-49, the Boeing X-50 Dragonfly, the Gulfstream X-54, the Lockheed Martin X-55, the Generation Orbit X-60, the Dynetics X-61 Gremlins, the Aurora X-65 CRANE, and the Boeing X-66. These articles keep the full section order but run short, and they state explicitly what the record does not contain.

Designation-anomaly treatments cover the nine cases where the subject is the number rather than an aircraft. These are the X-23 contested assignment, the X-39 reservation that was never formalized, the classified X-41, the contradictory X-42, the duplicated X-44, the refused X-52, the skipped X-58 and X-67, and the leapfrogged X-69 through X-75 block. These articles are short by design, and padding them would obscure the point. An article establishing that the X-52 designation was requested in 2006, was refused because of possible confusion with the B-52, and that the programme continued as the X-53, as Parsch records, has said everything the record supports.

The distribution across classes is itself a finding. Roughly two fifths of the designations in the nominal range support a full engineering treatment. The remainder are cancelled programmes, classified programmes, and administrative artefacts, and any account of the X-series that discusses only the aircraft that flew is describing a biased sample of its own subject.

Overlap with Adjacent Series on This Blog

Several aircraft in this series appear in earlier work here, and the overlap is deliberate.

The A96 History of Rocketplanes article treats the rocket-powered aircraft as a lineage running from the German work through the X-1 and X-15 to the modern suborbital vehicles, and that lineage organizes it. The present series takes the same airframes and asks what each was built to measure. The X-1, X-2, X-15, X-20, X-23, X-24, X-37, and X-40 appear in both, and the two treatments complement each other. Where the earlier article says what came next, this series says why the wing had that planform. The related configuration question of large lifting entry vehicles is taken up in A106 Two-Stage Flying Delta Wing Vehicles.

The fixed-wing uncrewed aircraft series supplies the sizing machinery in a modern and much smaller context, and readers who want the relations above worked at a scale they can build should read A118 Propulsion and Power Sizing, A127 Structures and the Flight Envelope, and A123 Dynamic Stability and Control. The equations are the same. Only the Reynolds numbers differ.

The aerospace and information technology co-development series, beginning at A237 Framing and the Co-Development Mechanism, treats the computing side of the same institutions, and its later articles on A247 Software-Defined Aerospace and Autonomy cover the transition to the unmanned demonstrators that dominate the late X-series.

The A281 History of SpaceX series treats the institutional and capital-formation questions that the closing article of this series raises about the modern designations, particularly the shift from service sponsorship to laboratory and commercial sponsorship, and its treatment of commercial spinoff dynamics in History of SpaceX: The Category-Dominating Commercial Spinoff and the Internalization of Anchor Demand bears directly on the reusable launch demonstrators covered here.

Historiographical Situation and the Source Base

The X-series is unusually well documented at its beginning and unusually poorly documented at its end, and any survey must account for that gradient.

The primary technical literature is the NACA and NASA report series. Research memoranda, technical notes, technical reports, and the later technical memoranda and contractor reports were produced in volume through the 1970s and are largely public. For the X-1, X-2, X-3, X-4, X-5, and X-15 this literature is deep enough to reconstruct flight-by-flight results, and it is the backbone of the full treatments in this series. Representative examples of what survives include the transonic fuselage pressures measured on the X-1 in Knapp et al. 1953, the glide-flight measurements from the X-2 programme in Day 1953, the maximum lift and buffeting intensities obtained on the X-4 in Baker 1953a, the wing pressure distributions from the Navy-sponsored D-558 flown alongside them in Peele 1954, and the vertical tail load investigation of Funk and Rhyne 1956. For the X-15 the corresponding record runs from the programme reviews of Weil 1962 and Fischel and Toll 1964 through the operational procedures of Day and Hoey 1961 to the extracted stability and control derivatives of Yancey 1964. The 1958 research airplane committee conference report on the progress of the X-15 project is a representative example of the genre, gathering the design basis of an entire programme into one public document at the moment before first flight.

The institutional history literature is strong and was largely written by participants or by historians with archival access. The standard works on the X-15 specifically are Jenkins 2007 X-15 Extending the Frontiers of Flight, Jenkins 2000a Hypersonics Before the Shuttle, Jenkins and Landis 2003 Hypersonic, and Godwin 2000 X-15 The NASA Mission Reports, with the wider hypersonic context in Heppenheimer 2007 Facing the Heat Barrier and the X-43 programme in Peebles 2008a Road to Mach 10. For the early research airplanes the standard accounts are Peebles 2014 Probing the Sky, Rotundo 1994 Into the Unknown, and Pisano et al. 2006 Chuck Yeager and the Bell X-1. Jenkins 2001 Space Shuttle covers the programme into which much of the lifting-entry work eventually flowed.

The reference literature provides the roster and the administrative record. It is where the anomaly cases are documented, and it is also the source of a recurring misreading, since a compilation that reports the next unused sequential number is easily misread as reporting a ceiling.

The contemporary record thins sharply. Programmes after roughly 2000 generate proportionally fewer technical reports. Of the research records in this survey whose titles name an X-designation, 51 date from before 1970 and 41 of those are report primaries, while 109 date from 2000 or later and 46 of those are report primaries, all of them NASA Technical Reports Server records. For the programmes that left fewer reports the agency web presence together with the NASA Armstrong centre site is frequently the only public source. Several are classified in whole or in part. For the X-37 the flight record is public in the sense that launch and landing dates are announced while the mission is classified. For the X-41 essentially nothing is public. The series states these limits in each article rather than filling them with inference.

Three specific gaps are worth naming in advance. The X-23 attribution conflict has not been resolved in the public literature. The X-42 is described in two ways, which Parsch records together, the designation having been allocated to an expendable liquid-propellant upper-stage demonstrator and later used unofficially for a reusable launch vehicle demonstrator, and no engineering treatment of either vehicle under that number exists. The X-44 duplication is documented but the sequence of events that produced it is not.

The survey rests on 7,335 research records drawn from Crossref, the NASA Technical Reports Server and the Defense Technical Information Center, of which 2,004 are report primaries, being 27.3 percent, by the identifier rule set out under The Definition of Primary. Their median year is 2000. Of the 7,135 dated records, 1,585, being 22.2 percent, date from 1979 or earlier, the decades in which the NACA and NASA report series ran in volume, and 2,015, being 28.2 percent, date from 2015 or later, the last ten years that the review below asks a reader to read.

The Definition of Primary

Primacy is a property of the document, and this survey derives it from the identifier. A record is a report primary when it is a NASA Technical Reports Server record or carries a digital object identifier under the 10.21236 prefix, which Crossref registers for Defense Technical Information Center reports. By that rule 1,623 primaries are Technical Reports Server records and 381 are Defense Technical Information Center reports.

The rule undercounts what is first-hand. Conference papers of the American Institute of Aeronautics and Astronautics, abbreviated AIAA, and journal papers by the engineers and pilots who flew the aircraft are primary by any reading and are not reached by an identifier rule, and the books and reference works that carry much of this article’s history are cited as curated references outside the survey and are not counted in it at all. 27.3 percent is therefore a lower bound on how much of this survey is first-hand.

Thin Subjects

Six subjects that this article’s derivations depend on have thin literatures. Each count below is the number of research records in this survey whose title carries at least one of the listed terms, with a hyphen read as a space and a plural form counted.

Subject	Title terms counted	Records
the information an experiment returns	information gain, expected information, mutual information, Kullback-Leibler, differential entropy, Shannon entropy, Fisher information	16
the value of information to a downstream decision	value of information, value of sample information, value of perfect information, expected value of information, preposterior, EVSI	17
the learning curve of airframe cost	learning curve, experience curve, progress function, cost improvement curve, cost-quantity, learning rate, cumulative production	2
airframe attrition and fleet size	attrition, fleet size, number of airframes, loss rate, accident rate, mishap rate, binomial	0
inertia coupling	inertia coupling, inertial coupling, roll coupling, roll-coupled, coupled roll, kinematic coupling	10
the designation system as an object	designation, nomenclature, mission design series, designator, naming	2

The information accounting this article opens with has a literature, and it is a statistical one. None of the 16 titles that carry an information term names a flight, an aircraft or a flight vehicle, and the nearest to this subject is a design of aerothermal model-calibration experiments [Villanueva and Smarslok 2015]. The value of information is in the same position, 17 titles naming it and none of them a flight. The sizing of a flight programme by the information it returns is therefore this article’s own construction, assembled from the Bayesian design literature cited in the opening section, and the article states it as a derivation rather than citing a literature for it.

The cost arithmetic is thinner still. Two titles name a learning curve, both of them in the aircraft industry [Hartley 1965], and the airframe learning rate the article uses rests on Wright’s 1936 paper, whose title names the cost of airplanes rather than the curve. No title names airframe attrition or fleet size, which agrees with the Epistemic State section’s classification of the binomial attrition argument as weakly supported inference.

Inertia coupling is small but present, ten titles carrying a coupling term, together with the 1948 analysis of Phillips that the article cites as predicting the effect, whose title names steady rolling rather than coupling.

The designation system as an object has no literature in this survey. The two titles that carry a designation term use it for something else, a contractor and service designation in a flutter-model report [Deckman and Arnold 1960] and target designation by remotely piloted vehicles [Vehicle Estimates for Target 1971], which is the measurement behind the statement under The Contemporary Literature that the designation system has very little recent scholarship.

What the Survey Admits

A record is admitted only when a person reading its title finds it on this article’s subject, being the research aircraft and flight research as a class, the comparison of ground facilities with flight and the similarity gap, experiment design and the identification of models from flight data, the sizing constructs this article derives in the high-speed and flight setting it uses them in, the cost, prototyping and acquisition of demonstrators, the institutions and history of flight research, and the contemporary threads the review follows. Many words this subject depends on also name something else, and a record that shares only such a word is excluded. Experimental design and the value of information are also methods of medicine, ecology, geoscience, chemistry, materials science and economics, and those applications are excluded because they are far from flight research. Flutter is also a cardiac arrhythmia, supersonic is also a rendering of ultrasonic, and stagnation-point flow is also a problem in the mathematics of non-Newtonian fluids. Gravity-wave drag belongs to atmospheric science, atmospheric entry heating also describes meteoroids and cosmic dust, and a research aircraft is also a platform for atmospheric science. Similitude and Reynolds-number effects also belong to hydraulics, buildings, bridges, trains and sport. A designation is also a product code, a propulsion station number or a naval personnel category, and the annual tables titled Designations of Aircraft in a military reference work are parts of that work rather than works. The Defense Advanced Research Projects Agency, the Air Force Research Laboratory and the NASA centres also sponsor work far from aeronautics, and Edwards Air Force Base also has a literature of groundwater and land subsidence. Projectiles, bombs and munitions are excluded as ballistics rather than flight research, and the operating, maintenance and support costs of fleets are excluded, the survey keeping development and airframe cost. Correction, erratum, retraction and publisher notices, addenda, book reviews and specifications for individual instruments and equipment are excluded as well, because a survey counts research works and those are editorial events, parts of works or standards rather than works. A signed comment on a paper, a discussion of a paper, the author’s closure or reply, and a signed letter on a research subject are admitted when their subject is, because each argues about a result, while an unsigned item of these kinds and a referee’s report on a manuscript are not. Encyclopedia and dictionary entries of two pages or fewer, entries in biographical dictionaries, and unsigned news items and editorial highlights in journals and magazines are excluded on the same ground, and so is a second deposit of a document already held, such as a report-server copy of a meeting paper whose publisher record is kept, because counting it would count one work twice.

Three families that a general aeronautical survey would refuse are kept. Hypersonics and the ramjet and scramjet literature are kept because the X-15, X-43 and X-51 make them this article’s subject, and missiles because the X-7 through X-12 and the X-17 are missile and reentry testbeds inside the designation range and the entry relation this article uses is Allen and Eggers’s ballistic-missile result.

Some records of doubtful relevance are kept. Methodological work on Bayesian and optimal experimental design that names no application is kept as the method the opening section uses. Entry into the atmospheres of other planets is kept as the same aerothermodynamics on a different body, and launch-vehicle and Space Shuttle flight data are kept as flight research on vehicles that fly through the atmosphere. Helicopters, tiltrotors and airships are kept as the vertical-flight and lighter-than-air research to which the X-13 through X-22 block belongs, and avionics and navigation flight tests are kept as flight testing.

Every research title has been read for relevance, so the off-topic share that remains is a matter of reading judgement. A reading of titles cannot show that a work is relevant in substance, so this is a statement about titles only.

The Contemporary Literature

Cluster	Records
Ground facilities against flight, and the similarity gap	910
The X-series and other research aircraft	684
Aeroelasticity, flutter and the flexible wing	673
Compressibility, wave drag and the high-speed wing	567
Configurations of the recent demonstrators	563
Hypersonic airbreathing propulsion and vehicle design	514
Flight test technique and the flight research method	493
Identifying a model from flight data	418
Stability, control and handling qualities	377
Aerodynamic heating, entry and thermal protection	337
Sonic boom and the supersonic transport	292
Boundary-layer transition and laminar flow	279
Experiment design and the information a test returns	267
Propulsion, thrust in flight and propulsion integration	205
Demonstrators, prototyping, cost and acquisition	182
Institutions, history and engineering knowledge	170
Reusable launch and the recovery problem	168
Flight instrumentation, telemetry and data reduction	156
Uncrewed aircraft and autonomy	63
Other flight research and high-speed aeronautics literature	17
Total	7,335

The historical literature above describes the programmes. A survey that stopped there would misrepresent the field, because most of the questions these aircraft opened are still open and are still being worked. This section reviews where the contemporary literature stands on each of the threads the series follows. It is written from the position that a reader who wants to act on any of this should be reading the last ten years, not the archive.

Hypersonics and Airbreathing Propulsion

The scramjet question the X-43 and X-51 were built to answer has moved from whether positive net thrust is achievable to how the transition between operating modes is managed. Fotia 2015 treats combustion mode transition in a direct-connect ramjet-scramjet experiment as a controllable process rather than an operating hazard, and Wu and Wei 2023 together with Wu and Wei 2022 compare dual-combustion ramjet and scramjet operation across the same envelope. The configuration side has consolidated around the waverider idea that gave the X-51 its name, with direct optimization frameworks in Son et al. 2022 and quasi-waverider methods that relax the exact shock-fitting constraint in Liu et al. 2020a. Vehicle-level design is now an optimization problem, no longer a configuration selection, as in the structural work of Rodríguez-Segade et al. 2024, the aerodynamic modelling of Ma et al. 2025, and the combined-cycle booster study of Suzuki 2016.

The facility problem this article opened with has not gone away. Lee et al. 2015 describe what a modern airbreathing ground test facility can and cannot reproduce, and Ji et al. 2019 report the development of hypersonic flutter test capability, which is an admission that the coupled aerothermoelastic problem still cannot be closed analytically. The similarity gap that justified the X-15 justifies flight experiments now for the same reason.

Boundary-Layer Transition

Transition prediction is the single clearest case of a question the X-series opened and did not close. It remains the largest source of uncertainty in hypersonic vehicle sizing, because laminar and turbulent heating differ by a factor of several and the transition location is not reliably predictable. The contemporary work runs from criteria-based engineering methods in Zhou et al. 2018 to receptivity-based prediction in Niu and Su 2023. On the flight side, Berry et al. 2016 reports the verification of a transition prediction tool against a flight experiment, Paredes et al. 2020 addresses transition modelling at flight conditions specifically, Paredes and Choudhari 2018 examines deliberate transition delay using vortex generators, and Rieken et al. 2020 describes the ground tests supporting the same effort. That a flight experiment is still the arbiter is the strongest available evidence for this article’s central claim.

Thermal Protection

The Sutton-Graves and Fay-Riddell correlations used above remain the sizing tools, but the material response behind them has become the research subject. Martin and Panesi 2022 treat radiative transmission and absorption within the thermal protection material rather than as a surface boundary condition, and Vigil and Pérez 2026 optimize the protection geometry in place of sizing a uniform thickness. Both refine the blunt-body insight and do not depart from it.

Aeroelasticity and Active Control

This is the thread where the contemporary literature has moved furthest from the X-29. Aeroelastic tailoring is no longer a fixed laminate choice made once at design time. Stodieck et al. 2015 optimize tow-steered laminates in which the fibre path varies continuously across the cover, which generalizes the X-29 solution rather than repeating it, and Chen and Han 2017 extend the same treatment to joined-wing configurations. Alongside that, the passive solution has been joined by an active one. Waitman and Marcos 2020 design robust controllers for active flutter suppression, and Chen et al. 2023b and Chen et al. 2023a demonstrate suppression using leading-edge and trailing-edge control respectively. The X-56A was built to explore this territory, and Pena et al. 2018 reports fibre-optic load sensing of the kind that makes closed-loop control of a flexible wing practical. Nguyen et al. 2015c describes the variable-camber continuous trailing edge flap that turns the wing itself into the actuator, and the morphing literature reviewed by Sun et al. 2016 and controlled by Cheng et al. 2023a takes that idea to its limit. Ritter et al. 2016 address the aeroelastic simulation of these configurations at flight Reynolds number, the same scaling problem in a new place.

Configuration and Propulsion Integration

Two recent designations in the series sit directly on active literatures. The X-66 truss-braced wing has a design literature of its own, including the slotted-cruise optimization of Chau et al. 2026 and the stability-margin study of Li et al. 2023. The X-57 distributed electric propulsion concept is now a design discipline rather than a demonstration, with structural modelling in Alonso Castilla et al. 2021, propeller design for the high-disc-loading case in Shi et al. 2024, and hybrid architectures in Xiao et al. 2024. The adjacent electric vertical takeoff and landing sector described in Doo et al. 2021 inherits the vertical-flight questions that the X-13 through X-22 block opened and never resolved, one of the more striking continuities in the series.

Sonic Boom and the Supersonic Transport Question

The X-59 exists because the overland supersonic ban is a regulatory fact rather than a physical one, its flights being meant to evaluate community responses for regulators, and the contemporary literature is aimed squarely at changing the regulation. Xiao et al. 2026 present multifidelity low-boom design methods and Yamazaki and Ishida 2025 evaluate combined aerodynamic and boom performance. This is the clearest contemporary example of a research aircraft built to produce a number that a rulemaking body has already agreed to accept. It puts the information-economics argument of this article in its purest form.

Experiment Design, System Identification, and Uncertainty

The Bayesian framing this article opens with is itself an active field. Kennamer et al. 2023 address the computational cost of optimal design directly through amortization, and Zemplenyi and Miller 2023 extend optimal design to structural inference. On the flight-test side, Grauer and Morelli 2023 introduce a collection surveying advances in aircraft system identification, the discipline that turns the measurements of Instrumentation and Data Reduction into the derivatives of Stability and Control. Model credibility has become a formal subject in its own right through Liu et al. 2026c, and parameter identification for unconventional configurations is treated by Wang et al. 2022b and Wang et al. 2022a. The measurement side has advanced too, with Ahlefeldt 2017 describing microphone array measurement in a transonic tunnel.

Two adjacent literatures now bear on all of the above. Machine learning has entered fluid mechanics as a modelling tool rather than a curiosity, reviewed in the Annual Review of Fluid Mechanics by Brunton et al. 2020 and constrained toward physical realisability by McConkey et al. 2025. And the certification of autonomy, treated for the unmanned case by Grindle et al. 2017, is the question the X-62 exists to address in the manned case.

Reusable Launch and the Recovery Problem

The X-33 and X-34 failed at a problem that has since been solved commercially rather than experimentally, a finding about how research aircraft relate to the industries around them. The contemporary design literature treats reusable vehicle sizing and landing control as ordinary engineering, as in Wang et al. 2020 and Tariq et al. 2026. The relationship between that outcome and the two cancelled X-designations is taken up in the closing article and in the A281 History of SpaceX series.

Where the Contemporary Literature Is Thin

Three gaps are worth naming. There is very little recent scholarship on the designation system itself as an administrative object, and no research title in this survey names the designation sequence as its subject, which is part of why this series treats it as one. There is almost nothing recent on the programmes that were cancelled before flight, since a cancelled programme generates no results to report and the institutional record is usually closed. Titles naming the X-20 Dyna-Soar, the X-30 National Aero-Space Plane or the X-33 occur 63 times in this survey, and two of them date from 2015 or later. And the contemporary literature is weighted toward analysis, computation and ground test rather than flight. Of the 1,991 research records dated 2015 or later, 364 carry a flight-test, flight-experiment, flight-data or in-flight term in the title, the predictable consequence of flight experiments being expensive, and this weighting makes the handful of recent flight demonstrators disproportionately valuable relative to their number.

Ground facilities against flight, and the similarity gap

The residue this article opens with, and the largest cluster. Comparisons of wind-tunnel, shock-tunnel and computational results with flight, Reynolds-number and scale effects, wall interference, similitude and dimensional analysis, subscale and free-flight testing, and the facilities themselves. 447 of its 910 titles, about half, name flight, and the rest describe the facilities, the scaling laws and the corrections without a flight to compare against.

910 records. [A Correlation between Rain 1959] [A Correlation between Rain 1960] [A Hypersonic Ground-Test Facility 2002] [Abel et al. 1979] [Abramson 1975] [Abrego et al. 2001] [Adams 1967] [Adams and Rubin 1958] [Miley et al. 1992] [Ahlefeldt 2017] [Ahlefeldt and Quest 2014] [Ahtye 1980] [Alexander 1991] [Alexander and Griffin 1974] [Alexander et al. 1973] [Allen et al. 2015] [Allongue and Krysinski 1990] [Alunno et al. 2026] [An Evaluation 1962] [Ananda et al. 2015] [Anderson and Stephenson 1965] [Anderson et al. 2026] [Andrianatos] [Anyoji et al. 2010] [Arnold and Deiwert 1997] [Asim et al. 2022] [Asymptotic Methods 1991] [Atencio 1975] [Atencio and Soderman 1973] [Ayers 1981] [Ayers 1982] [Bade 1975] [Baggett et al. 2021] [Bailey and Starr 1976] [Bailey et al. 2005] [Bakos et al. 1996] [Balch 1978] [Baldwin 2007] [Bamber 1961] [Barbante 2009] [Barbante and Chazot 2006] [Barnhart et al. 1988] [Bartels and Scott 2014] [Batson et al. 1981] [Bean and Lee 1994] [Bean and Lee 1995] [Becker 1940] [Bell 2007] [Saltzman and Ayers 1982] [Simmons et al] [Simmons et al] [Bensassi et al. 2012] [Bensassi et al. 2016] [Beresh 2022] [Berger 1979] [Berridge et al. 2018] [Berridge et al. 2019] [Berry et al. 2002a] [Berry et al. 2002b] [Beyers et al. 1997] [Bier et al. 2013] [Binion 1970] [Binion 1969] [Binion 1974] [Binion and Lo 1972] [Black 1968] [Black 1969] [Blackwell and Frederickson 1981] [Blackwell 1969] [Blackwell 1978] [Blaha 1969] [Bliss 1980] [Bobbitt et al. 1992] [Boonjue et al. 1996] [Borg et al. 2025b] [Boschetti et al. 2004] [Bosmajian 2000] [Bosmajian 2002] [Boudreau 1979] [Bowden and Shockey 1970] [Bowers and Sandlin 1984] [Bowers and Sim 1984] [Bowman 1956] [Boyer 1964] [Bradley et al. 1981] [Bradley et al. 1982] [Brand and Narramore 1992] [Brandon et al. 1995] [Brandon et al. 1997] [Bray 1962] [Brion et al. 2006] [Broeren et al. 2017] [Broeren et al. 2019] [Brower 2024] [Brown and Duhon 1965] [Brune and Morrow 2023] [Brunner et al. 2021] [Bryant 1948] [Buckingham 1914] [Bunnell and Delany 1947] [Burner et al. 2005] [Burns 1970] [Bushnell 2006] [Buttrill and Houck 1990] [Bynum et al. 1970] [Cahill and Connor 1979] [Cain 1979] [Cambier et al. 1992] [Campbell et al. 2010] [Campbell and Seacord 1943] [Capone 1975] [Carbonaro 1993] [Carlson and Morris 1966] [Carlson 1964a] [Carroll and Brandis 2023] [Carter 1988] [Carter and Sims 1981] [Cassanto 1971] [Cassanto et al. 1968] [Castner et al. 2018] [Castner 2009] [Castner 2010b] [Cen et al. 2015] [Cenkci 1991] [Cenko 1994] [Cenko 1999] [Cenko et al. 1995] [Cerreta 1957] [Chamberlin and Blaha 1973] [Chamberlin 1974] [Chan et al. 2025] [Chapman et al. 1999b] [Chapman et al. 1999a] [Chen et al. 2023d] [Chen et al. 1984] [Chou et al. 1981] [Clarke 1982] [Cleary and Gray 1947] [Cliff et al. 2016b] [Cliff et al. 2016a] [Cocking and Bryce 1975] [Coe 1985] [Coe and Perkins 1990] [Cohen 1970] [Collier et al. 1990] [Comer et al. 2024] [Comer et al. 2026a] [Comer et al. 2026b] [Comparison of Aircraft Noise 1975] [Comparison of Static Aerodynamic 2018] [Cook et al. 1994] [Cook et al. 1969] [Cook and Hickey 1965] [Cook and Hickey 1975] [Cook and Hickey 1976] [Cooksey et al. 1964] [Corda et al. 2000] [Corda et al. 2001] [Cornelison and Arnold 1997] [Cosgrove and Ryan 1969] [Courtin et al. 2020] [Winski et al] [Cox et al. 2012] [Crippa and Rizzi 2008] [Crites et al. 1992] [Croom 1977] [Crowder 2018] [Cruz and Green 2019] [Cumming and Lowe 1971] [Cummings et al. 2003] [Cunningham et al. 2008] [Curtin et al. 2002] [Czysz 1963] [Damstrom and Mayes 1970] [Danehy et al. 2010] [Danis] [Dantsker 2024a] [Dantsker 2024b] [Dantsker and Mancuso 2019] [Dantsker and Selig 2015] [Dantsker et al. 2020] [Dantsker et al. 2022] [Dantsker et al. 2023a] [Dantsker et al. 2023b] [Dantsker et al. 2025] [Davey and Ochoa-Cabrero 2023] [Chan et al] [Chan et al] [Cox et al] [Fisher and Lanser 1994] [Dawicke] [Davis 1968a] [Davis 1968b] [Davis 1980] [Davis 1981] [De Crombrugghe] [De Filippis et al. 2005] [Del Frate 1992] [del Val and Das 2026] [Delany and Kauffman 1945] [Denardo and Canning 1952] [Deng and Yuan 2015] [Development of the Shock 1962] [Dey 2014] [Di Clemente et al. 2007] [Dicristina 1979] [Diggins 1951] [Dimensional Analysis and Dynamic 2015] [Dimensional Analysis and Dynamic 2009] [Dimensional Analysis and Physical 2014] [Dimensional Analysis and Similitude 2024] [Disotell et al. 2026] [Dittmar 1989] [Dittmar and Lasagna 1982] [Dittmar et al. 1983] [Dix and Mattasits 1980] [Dodson 1982] [Doherty 1978] [Doherty] [Doll et al. 2024] [Donovan and Selig 1989] [Dougherty 1975] [Dougherty 2021a] [Dougherty and Fisher 1980] [Dowell and Bliss 1978] [Drain et al. 2017] [Draper and Moran 1973] [Drees 1976] [Dresser et al. 1990] [Dreyer et al. 2026] [Du et al. 2025] [Durand and Lesley 1926] [Dusterberry 1964] [Dziuba et al. 2024] [Edge and Perkins 1995] [Edwards 1998] [Effects of Wind-Tunnel Disturbances 1972] [Eggers et al. 2006] [Eldridge-Allegra et al. 2023] [Elena 2026] [Elhashani et al. 2014] [Elkhoury and Rockwell 2004] [Elkhoury et al. 2005] [Elmiligui et al. 2011] [Elzey et al. 1999] [Englar 1970] [Enkenhus 1969] [Erdos 1998] [Ericsson 1985] [Esposito 2023b] [Esposito et al. 2024] [Evaluation of Equipment Performance 2022] [Evangelista et al. 1987] [Evangelista et al. 1989] [Evans 1954] [Ewenz Rocher et al. 2022] [Facility Opportunities and Associated 1992] [Facility Requirements for Hypersonic 1991] [Fakhraei and Weiss 2016] [Fang 2018] [Fanning and Lucas 1979] [Fey et al. 2010] [Filippou et al. 2024] [Fisher et al. 1990] [Fisher and Dougherty 1983] [Fisher and Dougherty 1982] [Fisher 1948] [Fisher and McBride 1948] [Fisher and McBride 1955] [Fisher and Morris 1948] [Fisher and Thompson 1949] [Fisher and Thompson 1950] [Fisher and Thompson 1955] [Fisher and Windham 1950a] [Fisher and Windham 1950b] [Fisher and Windham 1951] [Fisher and Windham 1955a] [Fisher and Windham 1955b] [Fitzsimmons et al. 1980] [Fivel et al. 1975] [Flemming et al. 1994] [Foch and Toot 1989] [Frostig and Simitses 2001] [Fu et al. 2022a] [Fukami et al. 2004] [Fukushima and Kawai 2017] [Furbish 1997] [Furlong and Fitzpatrick 1947] [Gai et al. 1992] [Gallington and Miller 1970] [Gao et al. 2021f] [Garcia et al. 1973] [Garcia et al. 1982] [Garcia et al. 1985] [Garland et al. 1957] [Asper and Simmons 2022] [Gebert et al. 2000a] [Gebert et al. 2000b] [Geuther et al. 2024] [Ghaffari 1994] [Ghanchi and Gururajan 2026] [Ghate et al. 2026] [Ghazi 1993] [Gibson 2002] [Gillespie and Arbic 1951] [Girgis et al. 2002] [Glazkov and Semenov 2024] [Glezer 2009] [Glezer 2012] [Glowacki 1971] [Gnemmi et al. 1991] [Goett and Bicknell 1939] [Gomes and Speirits 1991] [González Mendoza 2026a] [González Mendoza 2026b] [Goodrich et al. 1983b] [Goodrich et al. 1983a] [Goodyer 1990] [Goodyer and Kilgore 1972] [Goodyer and Kilgore 1973] [Gopal et al. 2026] [Grant et al. 2017] [Grant and Sevier 1960] [Grauer and Waite 1986] [Grauer and Waite 2024] [Greene et al. 1966] [Greer et al. 2000] [Gross and Fasel 2018] [Grossir et al. 2015] [Grossman 2025] [Ground Testing Facility 2023] [Große and Schröder 2009] [Guiot and Wunnenberg 1980] [Gupta et al. 2005] [Gupta et al. 2015] [Hansman and Craig 1987] [Harrison and Lockman 1968] [Harrison and Marko 1968] [Harvey and Bobbitt 1981] [Hasegawa 2025] [Hasegawa et al. 1999] [Hashimoto et al. 2011] [Hayes et al. 1999] [He et al. 1992] [Head 1962] [Heaney et al. 2022] [Heaney et al. 2024] [Hebbar and Sommers 1990] [Hedlund and Ragsdale 1985] [Hedlund et al. 1990] [Heeg et al. 2005] [Hemsch and Walker 2011] [Hendershot 1969] [Henry et al. 1988] [Hensel 1964] [Herdy 2025] [Hermann 2024] [Hermann 2025] [Hernandez et al. 1993] [Hickman and Kyser 1972] [Hicks et al. 1972] [Hieser et al. 1956] [Hill and Zierten 1991] [Hillje and Tymms 1978] [Hinada et al. 1991] [Hinton and Eastlake] [Hitzel and Zimper 2018] [Hockman and Eisiminger 1948] [Hoehne 1967] [Holden 1993a] [Holden 1993b] [Holden 2015] [Holdo 1993] [Holguin and Kostyk 2010b] [Holmes and Woehr 1971] [Holway 1966] [Holzhauser and Bray 1956] [Hooper 1989] [Hooser 2002] [Hopkins and Keener 1968] [Hou et al. 2026] [Houbolt and Rainey 1975] [Howard and Bray 1992] [Howell and Braslow 1955] [Hoyt 2000] [Hozumi et al. 2001] [Hruby and McDevitt 1964] [Hu and Durbin 2012] [Huston et al. 1955] [Huttsell et al. 1976] [Hypersonic Flow at Low 1962] [Hypersonic Ground Test Requirements 2002] [Iliff and Shafer 1992] [Iliff and Shafer 1993b] [Ishikawa et al. 2011] [Panda] [Jaffe 1972] [Nissen and Gadeberg 1944] [Jang 2003b] [Jang 2003a] [Janna 2020] [Jarvis and Fisher 1946] [Jayaraman and Potsdam 2014] [Jayaraman et al. 2022a] [Jeong and Bae 2022] [Jernell 1969] [Ji et al. 2019] [Jiang and Yu 2017] [Jiang et al. 2017] [Lamar et al. 2001] [Lamar et al. 2008] [Johnson et al. 1970] [Johnson et al. 1986] [Johnson et al. 1980] [Johnson 2003] [Jones and Laurence 2025] [Jordan and Bailey 2008] [Jordan et al. 2005] [Jouannet et al. 2012] [Jung et al. 2012] [Junnai Zhai and Rebstock] [Kalkhoran and Otugen 1994] [Kang et al. 2023a] [Berger et al. 2014] [Kauffman 1945] [Kayten and Koven 1945] [Kehoe 1988] [Kehoe 1987a] [Keidel et al. 2019] [Keller et al. 2026] [Kelly and Osborne 1954] [Kendall 1974] [Goodson 1966] [Kepler 1980] [Kertesz 1965] [Kieß et al. 2026] [Kilgore 1982] [Kilgore and Dress 1984] [Kilgore et al. 1974] [Kimmel et al. 2011] [King and Johnson 1983] [Kirk et al. 2015] [Klein and Batterson 1986] [Klein and Murphy 1999] [Kline 1986] [Kmak et al. 2001] [Knackstedt 1952] [Knight et al. 2011] [Knighton 1992] [Koenig and Rolls 1966] [Koh 1971] [Kong et al. 2023] [Koning 2015] [Koning 2016] [Korejwo and Holden 1992] [Korst et al. 1994] [Korzun and Cassel 2020] [Koven and Kayten 1946] [Kraft 1994] [Kraft and Chapman 1993] [Krieger et al. 1980] [Krizo et al. 2013] [Kroeger and Martin 1967] [Kubo 2018] [Kumar and Ghosh 2023a] [Kuntavanish and Cancel 1983] [Kyeremeh et al. 2023] [Lackey and Hadfield 1992] [Lam and Stollenwerk 1966] [Landman et al. 2022] [Langill 1965] [Laurence 2023] [Lawing et al. 1991] [Lawrence and Mills 2002] [Layton 1984] [Lederer 1994] [Lee et al. 2015] [Lee et al. 1991] [Lee et al. 2027] [Lee and Krivanek 2005] [Lee-Rausch and Biedron 2013] [Lemley and Mullans 1974] [LENS Hypervelocity Tunnels 2002] [Leuckert et al. 2008] [Li et al. 2021] [Liu 2022] [Liu et al. 2001] [Liu et al. 2013] [Liu et al. 2016a] [Liverko A and Sboev D 2024] [Livingston 1965] [Livne et al. 2014] [Lockman 1967] [Londenberg 1993] [Loubeau et al. 2013] [Lovejoy 2026] [Loving 1966] [Loving 1961] [Lu and Lanter 1980] [Lu et al. 2016] [Lu et al. 2019] [Lu et al. 2021] [Lucas et al. 1978] [Luckring 2002] [Luckring 2003] [Luckring and Ghee 2001] [Luckring 2004] [Luckring et al. 1989] [Luers and Fiscus 1984] [Macgregor 1971] [Mach et al. 2022] [Mackall et al. 1988] [Macwilkinson et al. 1974a] [Macwilkinson et al. 1974b] [Maddalon 1966] [Madsen 1982] [Magee and Taylor 1971] [Malcolm and Nelson 1987] [Malmuth 1984] [Malmuth and Cole 1984] [Mangalam and Davis 2009] [Mangalam and Pfenninger 1984] [Marineau 2016] [Martin et al. 1993] [Martinez et al. 2004] [Martinez et al. 2014] [Martinez Schramm et al. 2015] [Mas Colomer] [Matsumoto et al. 2016] [Matsuyama 2024] [Matthews and Key 1977] [Matz and Smith 1978] [Maughmer et al. 2021] [Maus et al. 1983] [Maydew 1964] [McDaniel 2005] [McGhee et al. 1988] [McKinney and Baals 1982] [McQuellin and Buttsworth 2024] [Mead and Larson 2001] [Meckelnborg and Hölling 2026] [Mehrotra and Robinson 1982] [Metzger 1997] [Meyer 1958] [Meyer 1992] [Meyn et al. 1993] [Mikhail 1989] [Miles and Brown 2002] [Milillo 1972] [Miller 1993] [Milligan and Bailey 1963] [Mills 2015] [Minor and Shimer 1986] [Mishra et al. 2022] [Mitchell 1973] [Miyakawa et al. 1985] [Moffitt et al. 1972] [Mokry 1974] [Mokry 2001] [Monti et al. 2001] [Moore and Harney 1988] [Morgenstern 2012a] [Morgenstern 2012b] [Mosbah et al. 2013] [Moses and Shah 1999] [Moul and Taylor 1980] [Moulin et al. 2011] [Mueller and Jansen 1982] [Mueschke et al. 2020] [Muhlstein et al. 1974] [Mullen and Reed 2021] [Murakoshi 1969] [Murch et al. 2009] [Murman 1979] [Murman 1982] [Murri et al. 1984] [Muse et al. 2008] [Mychalowycz and Panda 1996] [Myers and Stromberg 1978] [Nadell et al. 2023] [Nagai 2013] [Nagamatsu 1962] [Nagel and Thomas 1965] [Nagel 1982] [Nakatani et al. 2009b] [Rieken et al. 2020] [Dippold 2022] [NASA Glenn Research Center’s 2002] [Navaratna et al. 2019] [Neal 1970] [Nelson 1984] [Nelson et al. 1993] [Nepomuceno and Annes Da Silva 2021] [Newman et al. 1988] [Newsom et al. 1982] [Nguyen et al. 2015a] [Nguyen et al. 2015d] [Nguyen et al. 2019b] [Nicolaides 1971] [Niebanck 1969] [Niedling 1982] [Niewald and Parker 1999b] [Nissen et al. 1948] [Nitsche and Szodruch 1993] [Noll and Huttsell 1978] [Noll and Huttsell 1979] [Nompelis and Candler 2007] [Nomura 1983] [Norton 1989] [Nugent and Pendergraft 1987] [Numata et al. 2013] [Obermark 2004] [Olejnik et al. 2019] [Oleskiw et al. 2001] [Ongarato 1968] [Orlik-Ruckemann and Laberge 1981] [Osborne 1957] [Ouellette et al. 2014] [Owens et al. 2002] [Owens and Wahls 2001] [Owens et al. 2005] [Ożóg et al. 2020] [Pallister et al. 1992] [Pan et al. 2026] [Panda 2022] [Shea et al] [Heaney et al] [Penland and Romeo 1971a] [Penland and Romeo 1971b] [Perini 1972] [Perkins and Jorgensen 1956] [Perraud et al. 2010] [Peterson 1982b] [Phillips and Waggoner 1988] [Piatak et al. 2011] [Pieper et al. 2018] [Pierpont 1959] [Pilyugin et al. 1994] [Piotrowski and Zingg 2023] [Platou 1968] [Poovathingal and Chen 2022] [Popov et al. 2010b] [Porter] [Portoni and Dufrene 2023] [Potthast 1980] [Precup et al. 2015] [Precup et al. 2018] [Prediction and Verification 1985] [Preisser and Chestnutt 1983] [Principles of Hypersonic Test 2002] [Pusztai et al. 2024] [Putman 1961] [Pyle and Steers 1975] [Quast et al. 1990] [Hall et al. 1994] [Raffel et al. 2022] [Ragheb et al. 2013] [Raju Kulkarni et al. 2019] [Raman et al. 2000] [Rasuo 2000] [Rathsam et al. 2011] [Ratvasky 2001] [Ray 1982] [Ray et al. 1974] [Redd et al. 1979] [Redelinghuys et al. 2015] [Reed et al. 2012] [Reed 1975a] [Reed 1976a] [Reed 1976b] [Reimer et al] [Rembetsy 1966] [Report No. 581. Measurements 1937] [Research Instrumentation Requirements 1974] [Reukauf et al. 1974] [Ricci et al. 2019] [Richey et al. 1976] [Ricketts and Doggett 1980] [Rittenhouse 1959] [Ritter et al. 2016] [Rivera and Florance 2000] [Rivers et al. 2015] [Rivers and Wahls 1999] [Rivers et al. 2001b] [Rizk and Lovell 1986] [Rizk and Murman 1984] [McGhee and Bingham 1972] [Roberts 1988b] [Roepke 1972] [Rolls and Wingrove 1958] [Rom et al. 1995] [Romere et al. 1978] [Rona and Soueid 2010] [Rooney et al. 1977] [Roskam et al. 1980] [Rostkowski et al. 2026] [Ruan and Aagren 2025] [Ruhlin and Murphy 1981] [Ruhlin and Pratt-Barlow 1981] [Runyan and George-Falvy 1979] [Russell and Conley 2020] [Sabatini et al. 2026] [Sakraker and Chazot 2014] [Saltzman and Ayers 1981] [Samikkannu 2011] [Sansica and Hashimoto 2023] [Sardou 1986] [Sarker et al. 2026] [Saunders 1996] [Scallion 1982] [Schauerte and Schreyer 2023] [Scher 1947a] [Schneider 2006] [Schneider 2009] [Schneider 2013] [Schneider 2015] [Schrauf and Schröder 1999] [Sekino and Maki 2024] [Sekula et al. 2012] [Sekula et al. 2010] [Serre 2009] [Serre and Falempin 2008] [Serre et al. 2011] [Sforza and Anderson 2003] [Sgubin et al. 2024] [Shafer 1991] [Shafer 1992] [Shafer 1994] [Shahrbabaki et al. 2014] [Shantz 1953] [Sharma 1992] [Sheldon 1967] [Shepheard 1965] [Sherrer et al. 1980] [Sherrer et al. 1981] [Shields and Mohseni 2011] [Shinoda 1996] [Silva et al. 2006] [Silva et al. 2009] [Silvers and Spreemann 1947] [Similitude and Dimensional Analysis 2000] [Similitude Dimensional Analysis 2007] [Simpson et al. 2007] [Sims and Carter 1981] [Sivells 1969] [Sloan and Davis 1962] [Smeltzer et al. 1974] [Smith 1953] [Smith and Baxter] [Smith et al. 2002a] [Smith et al. 2002b] [Smith et al. 1989] [Smith and Adcock 1986] [Smith et al. 2017] [Snyder 1947b] [Sobron 2018] [Sobron et al. 2021] [Song 2018] [Song et al. 2019] [Sopher and Kottapalli 1982] [Soudakov 2016] [Spreiter and Steffen 1946] [Springer 1998] [Spurlin and Lueck 1984] [Squires and Warmbrodt 1983] [Stahara and Spreiter 1979] [Staley 1976] [Stalla et al. 2026] [Stallings 1981] [Stallings and Hartman 1981] [Stallings and Lamb 1980] [Stanewsky and Freimuth 1989] [Stargill 1983] [Starkey et al. 2012] [Starr and Schueler 1973] [Stefko et al. 1987] [Steinle 1982] [Stephan and Obermeier 1974] [Stetson and Sawyer 1977] [Geuther et al] [Stewart 1992] [Stewart 1993] [Stewart and Walters 1996] [Stock 2002] [Stollery and Murthy 1977] [Stollery and Murthy 1978] [Strike 1982] [Stroub 1978] [Strout and Atencio 1976] [Stuessy et al. 1997] [Subcommittee on Similarity of Wind Tunnel Experime 1994] [Subscale Modeling and Wind 2013] [Suleman 2007] [Sunami et al. 2006] [Suppe 2000] [Sutherland 1893] [Swain 1982] [Sweberg and Lange 1947] [Symington 1940] [Tai et al. 2021] [Takahashi et al. 2023] [Tang et al. 1978] [Tanno and Tanno 2021] [Taylor 1977] [Tempelmeyer and Osborne 1955] [Teter 2006] [Tetlow and Smith 2007] [Thake et al. 2010] [The Duration and Properties 1962] [The ram-wing surface effect 1973] [Theodore et al. 2014b] [Thompson and Pandolfini 1995] [Tian et al. 2026b] [Timmer 2008] [Ting et al. 2026] [Tirtey et al. 2006] [Tomek et al. 2002] [Tomek et al. 2003] [Transonic Wind Tunnel Wall 1982] [Traybar 1970] [Trudgian et al. 2025] [Tumuklu et al. 2021] [Tuohy 2006] [Uddin 2022] [Ueno et al. 2002] [Ueno et al. 2007] [Ulbrich 2010] [Ulbrich and Boone 2004] [Ulbrich and Steinle 1994] [Ullah et al. 2020] [Uppoor et al. 2026] [Usry and Wallace 1971] [Velasquez 2013] [Veraar 2008] [Veraar 2009] [Vicente and Foy 1963a] [Vicente and Foy 1963b] [Vicroy 2009] [Viviand 1991] [Voland et al. 1999] [Vorburger et al. 1985] [Vos et al. 2007a] [Wadhams et al. 2008] [Wagner et al. 1990] [Wagner and Watson 1963] [Wahls et al. 2001] [Waldmann et al. 2023] [Wallace 1982] [Wallskog 1954] [Walsh and Hart 1981] [Sefic 1981] [Wan et al. 2003b] [Wang and Gao 2013] [Wang et al. 1987] [Wang et al. 2016a] [Ward and Myers 1967] [Warsop and Crowther 2019] [Wasson 1977] [Waszak 1996] [Webb et al. 1979] [Weeks 1969] [Wegener and Lobb 1952] [Wells 1987] [Welsch 1953] [Welton 1965] [Wey et al. 2012] [White 2004] [White and Gibson 2004] [Whitefield et al. 1981] [Whitfield and Griffith 1965] [Widmayer and Tomassoni 1971] [Wilcox and Chamberlin 1974] [Wilcox and Chamberlin 1975] [Willard and Kranzler 1996] [Willemsen et al. 1985] [Williams 2021] [Wilson and Chou 1985] [Winchenbach et al. 1982] [Wind Tunnel/Flight Test Correlation 1978] [Wind-Tunnel Study of Ascent 1981] [Windham 1956] [Winski et al. 2025] [Witcofski et al. 1991] [Wittliff et al. 1992] [Woike and Willis 2000] [Woike and Willis 2001] [Wyborny and Requardt 1974] [Xue et al. 2019b] [Xue et al. 2020a] [Xue et al. 2020b] [Xue et al. 2020c] [Yamada et al. 2023] [Yamamoto et al. 2001] [Yamauchi and Johnson 1983] [Yang and Li 2008] [Yeager and Mantay 1976] [Yeo and Romander 2012] [Yeo et al. 2016] [Yergensen and Rhea 1988] [Yetter et al. 1982] [Yin 2011] [Yoshinaga et al. 1995] [Yuan et al. 2019] [Zhang] [Zhdanov et al. 2025] [Zhou et al. 2023b] [Zohuri 2015] [Zumwalt and Mueller 1984] [Zumwalt et al. 2016] [Şakraker et al. 2015]

The X-series and other research aircraft

The series’ own aircraft and their neighbours. Titles that name an X-designation, a research airplane or experimental aircraft, a lifting body, or one of the research aircraft that flew beside the series, such as the D-558 and the XV-15. Its titles name 34 distinct X-designations, the X-43, X-29 and X-15 most often, and 410 of its 684 records are report primaries, the highest share of any cluster in the table, which is the NACA and NASA report series documenting its own aircraft.

684 records. [Acree et al. 1997] [Aerothermodynamic Design 1993] [Aggarwal 2003] [Ahmed et al. 2003] [Amundsen et al. 2004] [Anderson 1993] [Ankenbruck 1954] [Ankenbruck and Dahlen 1953] [Armstrong 1977] [Arnaiz et al. 1980] [Arteaga et al. 2023] [Arteaga et al. 2024] [Ashworth et al. 1988] [Askren and Vail 1963] [Atencio et al. 1972] [Baer-Riedhart 1981] [Bahm et al. 2005] [Bailey et al. 2020] [Baird 1964] [Baker 1953b] [Baker 1954] [Bakos et al. 1999] [Bakos et al. 2001] [Balas et al. 2011] [Banks and Fisher 2006] [Banner et al. 1962] [Banner and Kinsler 1961] [Barret 1999] [Barret 1998] [Barthelemy 1989b] [Bartlett 1975] [Bartlett and Harris 1974] [Bartlett and Sangiorgio 1975] [Bartlett et al. 1973] [Bashkirov et al. 2021] [Baumann 2006a] [Baumann et al. 2008] [Baumann 2006b] [Baumann et al. 2013] [Baumgartner and Elvin 1995] [Beh et al. 2018] [Behzadpour 2025] [Beilman 1972] [Beilman 1983] [Belchihina et al. 2021] [Bellman 1959] [Bement 1978] [Berry et al. 1999] [Berry et al. 2000a] [Berry et al. 2000b] [Berry et al. 2000c] [Berry et al. 2008a] [Betsy’s Legacies 2017] [Biswell and Puig-Suari 1996] [Blocker and Ruebush 2005] [Boeing Co Seattle Wa 1963] [Boeing Flies Blended Wing 2008] [Boeing to Use X-43A 2005] [Bond and Swanson 1953] [Borer et al. 2019] [Borer et al. 2023] [Borer et al. 2024] [Borst 1990] [Bosworth and Cox 1989] [Bosworth and Stoliker 1996] [Bouslog et al. 1998] [Bowers 1963] [Bowman et al. 1978] [Boyd and Burley 2001] [Boyden 1974] [Braslow 1966] [Cobleigh et al. 1994] [German et al] [Brinker 2004] [Brinker and Wise 2000] [British Research Aircraft 1962] [Brown et al. 1992] [Brunner et al. 1966] [Bryson et al. 1968] [Bugg and Sleeman 1967] [Buning et al. 2000] [Burcham et al. 1995b] [Burcham and Ray 1987] [Burkhardt et al. 1999] [Burks 1981] [Butters and Zeisel 1982] [Calise 2000] [Calise et al. 1988] [Campbell et al. 1996] [Campbell et al. 1997] [Canter and Groves 1994] [Carter and Nagy 1996] [Chaput 1989] [Chen et al. 2026] [Chernyi and Gonor 1973] [Childs 1953] [Chin et al. 1987] [Chin 1970] [Clarke et al. 2018] [Cobleigh and Croom 2003] [Cobleigh and Croom 2001] [Cochrane et al. 1982] [Cochrane and Boissevain 1978] [Cochrane et al. 1981] [Cockrell et al. 2000] [Cohan and Hirsh 1966] [Collins et al. 1970] [Combs 1976] [Combs 1977] [Condon 1975] [Condon and Letchworth 1976] [Cook 1996] [Cook and Whittley 1975] [Cook and Whittley 1976] [Cosenito 2010] [Cosentino 2007] [Cosentino 2008] [Covington 1966] [Cross and Watts 1983] [Cross 1984] [Cruz and Ware 1992] [Cruz et al. 1989] [Cumming et al. 2017] [Curry and Sim 1982] [Curry and Sim 1983] [Curry and Sim 1984] [Curtiss 1965] [D’Angelo et al. 1999] [Dahlen 1953] [Mackall et al. 1998] [Dana 1993] [Dana et al. 1969] [Dancik et al. 1958] [Williams et al. 1994a] [Davidson et al. 1999] [Davis and Mertens 1958] [Davis and White 2006b] [Davis and White 2006a] [Davis et al. 2006] [Davis et al. 2007] [Day and Reisert 1959] [Dayton 1993] [De Angelis and Tang 1969] [Deangelis 1981] [DeAngelis 1982] [Deckert and Holzhauser 1973] [Deckman and Arnold 1960] [Deere et al. 2017] [Deere et al. 2018] [Deets and Brown 1986] [Deets et al. 1986] [Defense Science Board Washington Dc 1988] [Delgado et al. 2000] [Delgado et al. 2001] [Deng et al. 2024] [Denham and Owens 2016] [Bartlett and Re 1972] [Deveaux 1965] [Dicarlo et al. 1992] [Dillon and Creel 1978] [Dillon and Pittman 1978] [Dingell et al. 1999] [Direct Numerical Simulations 2023] [Doebler 2021] [Durston] [Durston] [Dragone 2000] [Drake 1949a] [Drake and McKay 1953] [Dugan et al. 1980] [Dukeman and Gallaher 1998] [Eckhardt 2001] [Edwards 1974] [Edwards 1976] [Ehernberger et al. 1992] [Eldredge et al. 1965] [Elliott 1968] [Ellis 1989] [Ellison and Latz 2003] [Ellsworth 2010] [Engelund et al. 2000] [Engelund 2001] [Engelund and Neal 2013] [Engelund et al. 1999] [Erickson et al. 1984] [Stalcup and Heersema] [Evans and Schilling 1983] [Kirkham et al. 1975a] [Falarski and Mort 1969] [Feller and Burbank 1958] [Ferlemann et al. 2005] [Fetterman et al. 1962] [Finch and Briggs 1953] [Finch and Matranga 1959] [First Glide Flight 1966] [Fischel and Toll 1964] [Fischel and Nugent 1953] [Fischel and Reisert 1955] [Fischel and Reisert 1956] [Fischel et al. 1957] [Foch 1992] [Freeman et al. 1997a] [Frei 1982] [Gale and Scher 1949] [Garcia et al. 2019] [Garrett et al. 2019] [Layton 1970] [Gates and Sternfield 1950] [Geiger 1963] [General Electric Co Cincinnati Oh 1964] [Gentry 1968] [Gentry 1972] [Gentry et al. 1966] [Gera 1986] [Gera et al. 1987] [Gibson et al. 2002] [Gibson and Goetz 1971] [Gilyard and Edwards 1983] [Goecke 1971] [Goldthorpe et al. 2010] [Gong 2005] [Graf et al. 1998] [Grantz 2011] [Grauer and Boucher 2017] [Greene 1958] [Griffin and Jonas 1983] [Grindle 2011] [Grindle 2012] [Grindle and Bahm 2006] [Ground Testing of X-48B 2007] [Gubbels et al. 2000] [Gupta and Bach 2007] [Haberland 1980] [Hall and Merrill 1983] [Hallion 1991] [Hallion and Peebles 2014] [Hank et al. 2008] [Harris 1993] [Harris and Harris 1997] [Harris 1972] [Harsha and Waldman 1989] [Hassell 1960] [Haus 2023] [Hawkins and Dilley 1992] [Heberling 2020] [Henderson 1964] [Hicks and Huckabine 1989] [Hicks and Matheny 1987] [Hicks and Moulton 1988] [Hicks et al. 1987b] [Hicks and Petersen 1988] [Hicks and Petersen 1989] [Hicks and Trippensee 1997] [Hicks et al. 1987a] [Hieser and Reid 1954] [Hirsh 1965] [Hirshorn and Kemmerly 2018] [Hiruma et al. 2020] [Hite 1940] [Hodge and Kelley 2006] [Hoe et al. 2012] [Hoerter et al. 1991] [Day and Hoey 1961] [Holland et al. 2000] [Hollis et al. 1999] [Holmes 1970] [Hook and Freeman 1989] [Horvath et al. 1990] [Houck et al. 1977] [Howell and Shelton 2019] [Howell 2011] [Howell et al. 2010] [Drake 1949b] [Huebner et al. 2001] [Huebner et al. 2000] [Hughes Tool Co Culver City Ca 1963] [Hussein and Chudoba 2016] [Hyper-X Model Testing 1996] [Immenschuh 1990] [Ishikawa et al. 2007] [Iwamiya 2002] [Hunley 1999] [Fischel 1960] [Jackman et al. 1992] [Jackson and Coyle 1983] [Jackson and Patch 1968] [Jackson and Rivers 1998] [Jackson and Taylor 1978] [Jackson et al. 1993] [Jackson et al. 1992] [Jackson et al. 1994] [Jackson et al. 1978] [Schaefer et al. 2023a] [Jacobson 2004] [Stevens et al. 1966] [Grauer and Boucher] [Brandon] [Jenkins 2000b] [Jenkins et al. 1968] [Jernell 1971] [Lux-Baumann and Burkes 2005] [Manke et al. 1970] [Cochrane and Graham 1971] [McTigue 1970] [Del Frate and Saltzman 1992] [Johnson and Lawing 1977] [Johnson 1958] [Pyle and Ash 1970] [Jones 1952] [Jones 2006] [Jordan and Hutchins 1955] [Jorgensen et al. 1971] [Kahre 1987] [Kaletka and Fu 1993] [Deere et al. 2022] [Karlgaard et al. 2004] [Karlgaard et al. 2005] [Kawakami et al. 2007] [Bhamidipati et al. 2024] [Kehlet 1954] [Kehoe 1984] [Kemp and King 1956] [Kempel 1971b] [Kempel and Painter 1994] [Kempel 1971a] [Kempel and Thompson 1971] [Kempel and Painter 1993] [Kempel et al. 1988] [Kempel et al. 1994] [Kemper and Renselaer 1969] [Kirkham et al. 1974] [Kirkham et al. 1975b] [Kitaplioglu et al. 1997] [Knapp and Jordan 1953] [Ko and Gong 2000] [Ko and Gong 2001] [Kock and Painter 1968] [Kock and Painter 1969] [Kokolios 1993] [Kordes and Noll Flight Loads Measurements on the X-15] [Kotfilia and Painter 1969] [Kuehme et al. 2014] [Kumar and Rao 2004] [Kwak et al. 2006] [La et al. 1993] [Larson 1972] [Lawing 1975] [Lawing 1978] [Lebacqz 1974] [Lechniak 2017] [Lee et al. 1998] [Letchworth 2011] [Liebeck 2008] [Lien et al. 2004] [Miller et al] [Lilly and Barlow 1949] [Linden 1972] [Linden and Hellyar 1974] [Ling 2017] [Littlefield and Melton 1999] [Littlefield and Melton 2000] [Lockheed-Georgia Co Marietta 1969] [Lokos et al. 2015] [Longstaff 1995] [Edelman] [Love 1964] [Love and Young 1966] [Luoma 1954] [Luria and Guyton 1992] [Lusty 1966] [Lux and Burkes 2008] [Lux-Baumann et al. 2006b] [Lux-Baumann and Burkes 2006] [Lux-Baumann et al. 2006a] [M2-F2 Lifting Body Accident 1967] [Machida et al. 2007] [Machin et al. 1999] [Magee and Wernicke 1979a] [Magee and Wernicke 1979b] [Maglieri et al. 1990] [Maisel and Harris 1981] [Maisel et al. 2000] [Makino and Noguchi 2003] [Makino et al. 2002] [Manke and Love 1975] [Marcy et al. 1956] [Marshall et al. 2005a] [Marshall et al. 2005b] [Martin 1979] [Martin 1980] [Matheny and Panageas 1981] [Matranga 1961a] [Matranga et al. 1962] [Matranga 1961b] [Maykapar 1968] [McClinton 2006 X-43 Scramjet Power Breaks the Hypersonic Barrier] [McClinton et al. 1998b] [McClinton et al. 2001] [McClinton et al. 1998a] [McCracken 1979] [McDearmon 1956] [McFARLAND and Robertson 1963] [McMurtry et al. 1981] [McTigue and Layton 1969] [McTigue and Ryan 1968] [Merlin 2014] [Micol 1990] [Miele 1968] [Mikula et al. 2000] [Miller and Jenkins 2000] [Miller and Truax 2018] [Minami and Tsukamoto 2006] [Tang 1970] [Moore and Frei 1983] [Morelli et al. 2005] [Morgan et al. 1964] [Moses 2003] [Murphy et al. 1999] [Murphy and Rubesin 1965] [Murray 1990] [Reubush et al. 2003] [Knapp et al. 1953] [Day 1953] [Baker 1953a] [Peele 1954] [Naeseth 1970] [Nagy and Kirsten 1976] [Nakahashi et al. 2002] [Nakatani et al. 2011] [Beeler 1961] [Tang and Pearson 1973] [Cook 1995b] [Taylor 2004] [Stein 2005] [Davis and White 2008] [Spivey et al] [Spivey et al] [Nelson et al. 1997] [Neuhaus 2018] [Nichols 1990] [Nicholson and lowry 1966] [Norris 1979] [Nugent 1954] [Olney et al. 2000] [Sreena and Laxman 2023] [Painter 1983] [Painter and Erickson 1984] [Pak 2017] [Palitz 1966] [Palmer et al. 1994] [Pamadi et al. 2000] [Parikh et al. 2004] [Peebles 2008b] [Peebles 2006] [Peebles 2007] [Peebles 2009] [Peele 1953] [Pendleton et al. 2007] [Pendley 1947] [Penland et al. 1978] [Penland and Fetterman 1958] [Peterson 1982a] [Pfeiff 1965] [Pieper 1965] [Pittsburgh Univ Washington DC Research Staff 1966] [Powers 1972] [Progress of the X-15 1965] [Putnam 1983] [Putnam 1984b] [Pyle 1971] [Queen and Cochrane 1982] [Quigley and Holzhauser 1974] [Reed et al. 1997] [Raab 2026] [Raible and Jacob 2003] [Ramsen et al. 1951] [Rana 2014] [Rasmussen 1979] [Ratnayake et al. 2011b] [Ratnayake et al. 2011a] [Rausch et al. 1997] [Rausch et al. 2000] [Castner] [Ray et al. 1988] [Castner] [Redeker and Voersmann 1988] [Redifer et al. 2007] [Reed and Watts 1961] [Reed 1955] [Reichenbach 2003] [Research-Airplane-Committee Report on Conference 1956] [Reubush 1999] [Reubush et al. 2001] [Rhodes 1969] [Arteaga et al] [Arteaga et al] [Rice and Cheng] [Day and Stillwell 1952] [Richardson 1976] [Riddle et al. 1981] [Riddle et al. 1988] [Risch et al. 2009b] [Risch et al. 2009a] [Risch 2008] [Rivers et al. 1991] [Navarro 1997] [Roberts et al. 1967] [Robinson et al. 1955] [Robinson 1948] [Robinson and Martin 2006] [Rock 1964] [Rogers et al. 2005] [Rolls 1965] [Ronald 1989] [Ross 1972] [Ross and Rogerson 1983] [Row and Fischel 1963] [Rudland et al. 1992] [Ruf et al. 1996] [Russo et al. 1986] [Ryan et al. 2014] [Sadow 1964] [Sager 1995] [Sakata 2002] [Garringer and Saltzman 1966] [Saltzman et al. 1999] [Saltzman et al. 2002] [Sams 1989] [Sandahl 1948] [Sanderson 1964] [Sanderson 1965] [Sano et al. 1984] [Sawyer et al. 1999] [Schaefer and Burnett 2019] [Scheidenhelm 1963] [Scher 1948] [Schmidt and Mann 1996] [Schmidt and Linden 1972b] [Schmidt and Linden 1972a] [Seebass 1989] [Sefic and Cutler 1986] [Sefic and Maxwell 1986] [Seiler et al. 2012] [Yoo et al] [Shanks and Smith 1960] [Shin et al. 1999] [Shin et al. 2001] [Shovlin and Cochrane 1978] [Whiteside and Welstead] [Sim 1973] [Sim and Curry 1978] [Sim and Curry 1984] [Sim 1976] [Sim 1997] [Sisk and Muhleman 1955] [Sitz 1992] [Sjoberg and Champine 1949] [Sliwa 1979] [Smith 1968] [Smith 1978] [Smith 1958] [Smith 1961] [Smith 1965] [Smith et al. 2005] [Soistmann and Spain 1993] [Soule 1973] [Spacht 1983] [Spain et al. 1993] [Spearman 1985a] [Spitzer et al. 1972] [Spitzer 1972] [Stadler 1993] [Sterk and McAtee 2015] [Sterk et al. 2016] [Sterk et al. 2018] [Hirshorn et al. 2024] [Stewart and Bauer 1983] [Stillwell and Wilmerding 1951] [Stillwell et al. 1950] [Stone and Piland 1991] [Stortz and ODonoghue 1995] [Stough and Patton 1979] [Strutz 1972] [Study of the Influence 1967] [Suit and Batterson 1986] [Suppes and Suppes 2024] [Suppes and Suppes 2026] [Schnulo and Hall] [Sypniewski 1989] [Szalai 1984] [Talay and Stone 1991] [Tang and Pearson 1971] [Tartabini et al. 2003] [Taylor and Jackson 1977] [Taylor and Jackson 1978] [Teitelbaum 1949] [Tendero Ventanas] [Testing of Advanced Carbon 1986] [The Bell X-22A V/STOL 1990] [The Canadair CL-84 Experimental 1990] [The Debate over Manned 2006] [The Dyna-Soar Cancellation 2006] [신경은 and 엄정식 2017] [Thomas et al. 2018] [Thomason 1990] [Thompson 1966] [Thompson 1964] [Thompson 1970b] [Thompson 1970a] [Thompson 2016] [Thompson et al. 2017] [Tishkoff 2016] [Tobiason and McShea 1986] [Tongue and Dingell 1999] [Tongue et al. 1997] [Tran et al. 2020] [Trippensee and Lux 1987] [Turner 2003] [Urnes et al. 1993] [V/STOL Tilt Rotor Aircraft 1972] [Vagt and Oppenheimer 1963] [Van Camp and Williams 1974] [Van Camp and Williams 1975] [Van Dalsem 2019] [van Oort et al. 2007] [Van Thullenar 1957] [Vetter 1966] [Vicroy 2011] [Vidal 1974] [Viken et al. 2017] [Viladegut 2018] [Viladegut Farran] [Voland et al. 2005] [Voland et al. 1998] [VSTOL Systems Research Aircraft 1994] [Walker and Wolowicz 1960] [Weber et al. 2000] [Weidner et al. 1976] [Weil 1962] [Welstead et al. 2017] [Wheldon and Whites 1966] [White and Condon 1978] [Whitehead 1989] [Whittley 1973] [Wierzbanowski and Armstrong 1991] [Wilhite et al. 2024] [Dana and Gentry 1970] [Doebler and Rathsam 2020] [Drake and Williams 1958] [Williams et al. 1994b] [Williams 1948a] [Williams 1948b] [Wilson 1967] [Wilson et al. 1982] [Winston 1969] [Wise 2003a] [Wise 2003b] [Wolkovitch 1984] [Wolowicz and Yancey 1973] [Wolowicz and Rediess 1957] [Woodcock 1988] [Woods et al. 2000a] [Woods et al. 2000b] [Woods et al. 2001] [Wright 1948a] [Wright 1948b] [Wright 1948c] [Wright and Loving 1953] [Wulff and Zoellner 1991] [Wykes and Lawrence 1971] [X-29 1991] [X-43A Research Vehicle Design 2011] [X-48B Blended Wing Body 2008] [Yamato et al. 1988] [Yamato et al. 1991] [Yancey 1964] [Yeh and Yeh 1989] [Yeh 1988a] [Yeh 1988b] [Yoler 1961] [Yoo et al. 2024] [Yoshida 2009] [Yoshida et al. 2002] [Zammit and Zwaanenburg 1989]

Aeroelasticity, flutter and the flexible wing

The constraint that made the X-29 possible. Divergence of forward-swept wings, flutter and its clearance in flight, aeroelastic tailoring, active flutter suppression and the active aeroelastic wing. 123 of its titles name a forward-swept wing and 138 name flutter suppression, the passive answer and the active one that the review above describes as joining it.

673 records. [A synthesis of reduced-order 1994] [Abbasi and Cooper 2009] [Abdelkader et al. 2011] [Abdullah and Sulaeman 2013] [Abel et al. 1977] [Abou-Kebeh et al. 2025] [Abou-Kebeh LLano et al. 2024] [Abrego et al. 1999] [Acree and Hoffman 2004] [Active control of a 1994] [Active Flutter Suppression 2016] [Active Flutter Suppression via 1999] [Adegbindin et al. 2016] [Ahmadi and Farsadi 2024] [Aiken and Fisher 1956] [Aiken and Fisher 1957] [Aircraft Flutter Control System 2011] [Aircraft Flutter Testing 1997] [Alag et al. 1986] [Albertani et al. 2005] [Allen et al. 2003] [Allen et al. 2005] [Alyanak and Pendleton 2014] [Alyanak and Pendleton 2017] [Amoozgar et al. 2013] [Andersen et al. 1996] [Andersen et al. 1997] [Anderson et al. 2004] [Andrighettoni and Mantegazza 1998] [Arizono and Isogai 2005] [Armstrong et al. 2006] [Arnaiz 1977] [Arnottt and Bernstein 2000] [Arrow] [Ashworth et al. 1986] [Aslan et al. 2017] [Austin et al. 1976] [Awadalla Ali Haj Ahmed 2024] [Ayaz et al. 2024] [Azevedo 1987] [Babcock and Lind 2012] [Bae et al. 2005] [Baird et al. 1975] [Barsamian 1965] [Bartels and Scott 2015] [Bartels et al. 2017] [Bartels et al. 2019] [Bartley 1975] [Bennett and Abel 1981] [Bennett and Abel 1982] [Beranek et al. 1965] [Berg et al. 2025] [Berry et al. 1995] [Bhatia et al. 2010] [Bhatia et al. 2012] [Bielawa 1976] [Binder et al. 2021] [Blair and Weisshaar 1982] [Bland 1980] [Blue et al. 1997] [Boehm et al. 2001] [Bohlmann et al. 1988] [Bohlmann et al. 1990] [Bohlmann et al. 1992] [Boissinot and Kheiri 2023] [Bordogna et al. 2016] [Borglund 2001] [Borglund and Kuttenkeuler 2002] [Boswinkle and Smith 1958] [Bowers 1980] [Bowers 1981] [Bras et al. 2022] [Breitsamter and Laschka 2001] [Brenner et al. 1997] [Briggs 2017] [Brignac et al. 1976] [Brown and Singh 2015] [Calico and Fuller 1981] [Capone 1981] [Carrillo et al. 2024] [Castillo Zuñiga et al. 2019] [Cavagna et al. 2009b] [Cavagna et al. 2009a] [Cavagna et al. 2010] [Cavagna et al. 2011] [Cazier and Kehoe 1986b] [Cazier and Kehoe 1986a] [Cesnik 2002] [Cesnik 2005] [Cesnik et al. 2000] [Chang et al. 2002] [Chen and Han 2017] [Chen et al. 2023a] [Chen et al. 2023b] [Chen and Zhao 2020] [Cheney 1988] [Chin] [Chin et al. 2011] [Chipman et al. 1985] [Chipman et al. 1984] [Choi et al. 2020] [Choosak Ngaongam and Rapee Ujjin 2024] [Chopra and Ganguli 1993] [Clarke et al. 2005] [Cobo-González et al. 2026] [Cocco and Meroli 2026] [Cole 1986] [Cole 1988] [Collar 1946] [Cumming and Diebler 2005] [Curry et al. 1989] [Curry et al. 1990] [Dai et al. 2026] [Danowsky 2017] [Danowsky et al. 2018] [Das et al. 2021] [de Visser 1999] [Deam 1984] [Deandrea et al. 1991] [Delgado and Datta 2026] [Devriendt et al. 2012] [Dibley et al. 2005] [Diederich and Budiansky 1948] [Dillinger et al. 2019] [Dilmi 2022] [Dimitriadis and Cooper 2001] [Dimitriadis and Cooper 2006] [Ding and Zhou 2022] [Dixit et al. 2016] [Djayapertapa and Allen 2002] [Djojodihardjo 2023] [Doengi et al. 1995] [Doggett and Ricketts 1980] [Doggett et al. 1995] [Dongi et al. 1996] [Dowell 1996] [Dowell and Hall 2003] [Dowell et al. 2009] [Drake and Balakrishnan 2004] [Dreyer and Shoch 1986] [Dublin and Peller 1975] [Dunning et al. 2014] [Durmaz and Kaya 2013] [Eastep et al. 1984] [Eastep et al. 1999] [Eckstrom and Spain 1982] [Edwards 1981] [Edwards 1983] [Eichelsdörfer 2026a] [Eichelsdörfer 2026b] [Eichelsdörfer 2026c] [Elshazly et al. 2025] [Epple and Altenbach 1982] [Eversman and Danda Roy 1996] [Experimental Transonic Flutter Characteristics 1990] [Faïsse] [Faïsse et al. 2021] [Felt and Kehoe 1985] [Firouz-Abadi et al. 2013] [Flight Flutter Testing Symposium 1975] [Flight-Surface Seal Is Designed 2010] [Flutter Testing Techniques 1976] [Forster et al. 1996] [Fournier et al. 2023] [French 1988a] [Friedmann et al. 1992] [Fujimori and Ohta 1993] [Förder and Steiner 2020] [Gade and Inman 1996] [Gainer et al. 1984] [Ganguli and Chopra 1997] [Garrard and Liebst 1983] [Generalized Predictive Control 1997] [Georgiou et al. 2012] [Gern and Librescu 2000] [Ghiringhelli et al. 1990] [Ghosh and Patil 2022] [Ghosh and Patil 2026] [Ghosh and Raisinghani 1993] [Gilbert and Silva 1987] [Gilbert et al. 1984] [Gilbert et al. 1982] [Gimmestad 1981] [Goetz 1972] [Golombek et al. 2026] [Grafton et al. 1982] [Green 1986] [Green 1987] [Green and Fernandez 1994] [Greene and Nacht 1967] [Griffin and Eastep 1981] [Griffin and Eastep 1982] [Grose 1979] [Guo et al. 1988] [Haase et al] [Haftka et al. 1989] [Haley and Soloway 2022] [Ham et al. 1994] [Hamada and Moreno 2018] [Hanson 1973] [Harris 2004] [He et al. 2023] [Heidersbach et al. 2023] [Hemmig et al. 1979] [Herencia et al. 2007] [Herrmann and Nemat-Nasser 1966] [Hertz et al. 1982] [Hess and Flick 2004] [Heyong and Ye 2011] [Hilger and Ritter 2021] [Hodges 1973] [Hu et al. 2009] [Huang et al. 2017b] [Huang et al. 2025a] [Hurley 1976] [Huttsell and Eastep 1989] [Hwang et al. 1980] [Hwang et al. 1981] [Hwu and Tsai 2002] [Ifju et al. 2001] [Ilie and Havenar 2022] [Iovnovich et al. 2018] [Ippolito et al. 2013] [Isogai 1988] [Isogai 1989] [Isogai 1992] [Jackuliak and Bugaj 2026] [Jha and Chattopadhyay 1999] [Jiang et al. 2011] [Jin et al. 2013] [Johnson 1980] [Johnson et al. 1983] [Johnson 1989] [Jones and Nisbet 1976] [Jun et al. 2014] [Jung and Reimerdes 2003] [Kachadourian et al. 1975] [Kafkas et al. 2021] [Kalaji 2023] [Kamiya et al. 1978] [Kanazaki and Setoguchi 2023] [Karpel 1980] [Karpel 1982] [Kassem et al. 2020] [Katz et al. 1976] [Kawakami et al. 2008] [Kayran 2004] [Kayran 2007] [Kehoe 1982] [Khan et al. 2023] [Kim 2024] [Kim et al. 2007] [Kirsch et al. 2020] [Kishi et al. 2022] [Klein 1983b] [Klepl 1992] [Klepl 1995] [Koedprayodsuk et al. 2025] [Koenig et al. 1988] [Kohara et al. 2016] [Koo and Lee 1994] [Koohi et al. 2014] [Kornev et al. 2021] [Kratochvíl and Valenta 2024] [Krengel et al. 2019] [Kreshock et al. 2016] [Kreshock et al. 2018] [Krone 1975 Divergence Elimination with Advanced Composites] [Krone 1980a] [Krone 1980b] [Krüger et al. 2014] [Krüger et al. 2022] [Kukreja 2007] [Kutschinski 1975] [Lanjun Li et al. 2006] [Lauten et al. 1954] [Layton 1996] [Le Clainche et al. 2019] [Lebofsky et al. 2014] [Lebofsky et al. 2015a] [Lee and Kim 2021a] [Lee and Ko 2009] [Lee et al. 1994] [Leitch et al. 2024] [Leitch et al. 2025] [Lenz and McKeever 1976] [Li 2012] [Li 2023] [Li and Fleeter 1996] [Li and Fleeter 2004] [Li and Xia 2017] [Li et al. 2013] [Li et al. 2019a] [Li et al. 2019c] [Librescu and Khdeir 1988] [Librescu and Simovich 1988] [Librescu and Song 1992] [Librescu and Thangjitham 1989] [Librescu and Thangjitham 1991] [Lichtenwalner et al. 1996] [Liebst 1987] [Liebst et al. 1984] [Lin et al. 1995] [Lind 1999] [Lind and Brenner 2001] [Lind and Brenner 1998a] [Lind and Brenner 1997a] [Lind and Brenner 1997b] [Lind and Brenner 2003] [Lind 1997] [Lind and Brenner 1998b] [Lind et al. 1997] [Lind et al. 1999] [Lindsley 2009] [Liu et al. 2012a] [Liu et al. 2017c] [Liu et al. 2020b] [Livne 2017] [Livne 2018] [Lokos et al. 2002] [Lokos 1990] [Lombardi and Morelli 1994] [Lombardi et al. 1997] [Long et al. 2014] [Lottati 1985] [Lottati 1987] [Lottati 1988] [Lu et al. 2017a] [Lundstrom et al. 1948] [Lynch and Rogers 1976] [Lyons et al. 1973] [Jaffal et al. 2010] [Ma et al. 2017b] [Macquart et al. 2016] [Mahaffey 1975] [Mahesh et al. 1980] [Mallik et al. 2013] [Mallik et al. 2015] [Manan and Cooper 2008] [Mangalam et al. 2007] [Mangalam et al. 2010] [Mann and Mercer 1985] [Mann and Mercer 1986] [Mann et al. 1987] [Marano et al. 2022] [Martin 1958] [Marx 1959] [Marzocca et al. 2000] [Mason and Capone 1983] [Mattaboni et al. 2007] [Mayya et al. 2023] [Mazidi et al. 2011] [McGurk et al. 2024] [McTavish] [Meirovitch 1995] [Melville 2021] [Melvin and Zhao 2024] [Mendez et al. 2021] [Merrett and Hilton 2012] [Merrett et al. 2011] [Miao et al. 1976] [Mihaila-Andres et al. 2017a] [Mihaila-Andres et al. 2017b] [Miles 1949] [Miller 1983] [Miller 1986] [Miller et al. 1982] [Mirowitz 1975] [Miyakawa et al. 1991] [Molloe-Christensen 1975] [Moon 2003] [Moon and Kim 2001] [Mottershead and Cooper 2012] [Moulin 2004] [Mourey 1979] [Muhamad Jayadi 2025] [Mukhopadhyay 1995] [Murri et al. 1983] [Muñoz and García-Fogeda 2022] [Muñoz and García-Fogeda 2024] [NACA Conference on Aircraft 1953] [Nae et al. 2019] [Nam et al. 1997] [Nangia et al. 2003] [Lokos et al. 2005] [Nguyen et al. 2015c] [Pena et al. 2018] [Nash et al. 1975] [Nasu 1986] [nath and ana 2017] [Navardi et al. 2026] [Newman and Buttrill 1995] [Newsom 1978] [Newsom 1979] [Newsom and Pototzky 1981] [Newsom et al. 1985] [Newton 1965] [Nguyen and Tal 2015] [Nguyen and Urnes 2012] [Nguyen and Xiong 2022b] [Nguyen et al. 2013] [Nguyen et al. 2014a] [Nguyen et al. 2014b] [Nguyen et al. 2015b] [Nguyen et al. 2019a] [Nguyen 2017] [Nicolai et al. 2010b] [Nissim 1975] [Nissim 1976] [Nissim 1977] [Nissim 1978] [Nissim 1991] [Nissim and Lottati 1979a] [Nissim and Lottati 1979b] [Nitzsche 1994] [Noll et al. 1983a] [Noll et al. 1983b] [Noll et al. 1984] [Oremland et al. 2017] [Ossmann et al. 2019] [Othman et al. 2019] [Ouellette 2017] [Ouyang et al. 2013] [Ouyang et al. 2021a] [Ouyang et al. 2021b] [Ouyang et al. 2026] [Owens and Perkins 1996] [Oyibo 1984] [Ozbay 1993] [Pak 2011] [Pak and Jutte 2009] [Pak and Lung 2011] [Pak and Lung 2010] [Pak and Lung 2017] [Patil and Patil 1997] [Pecora and Pecora 2018] [Peloubet et al. 1983] [Pendleton et al. 1996] [Pendleton et al. 1998] [Pendleton et al. 2000] [Pepping 1954] [Perera and Guo 2008] [Philbrick 1975] [Pierce and White 1972] [Pitt 2004] [Polve 1966] [Poomadath and Ajaj 2025] [Popelka et al. 1997] [Porter and Gu 1991] [Porter et al. 1992a] [Porter et al. 1992b] [Posada and Moreno 2019] [Potter 1975] [Prasad et al. 1967] [Price and Lee 1992] [Price and Lee 1993] [Puthisikamani et al. 2023] [Quackenbush 1983] [Quinn 1986] [Rajpal et al. 2021] [Raveh and Levy 2004] [Reich et al. 2002] [Reich et al. 2004] [Reich, hoor, Mart et al. 1995] [Rhodes and Selberg 1982] [Ribeiro et al. 2021] [Richard et al. 2000] [Richard et al. 2001] [Rimer et al. 1983] [Rimer et al. 1984a] [Rimer et al. 1984b] [Rimer et al. 1986] [Ritter et al. 2017] [Ro et al. 1992] [Robinson and Robinson 1980] [Rocha Da Costa] [Rodden 1989b] [Rodden 1989a] [Roger et al. 1974] [Roger et al. 1975] [Roglin 1975] [Rongrong et al. 2018] [Rosatelli et al. 2024] [Rosenbaum and Scanlan 1948] [Rosenbaum 1974] [Ross 1984] [Ross and Matarazzo 1982] [Sacchi et al. 2026] [Saheby et al. 2026] [Saltzman et al. 1994] [Sandford et al. 1974] [Sanmugadas et al. 2021] [Santos et al. 2026] [Sapkal and Attar 2011] [Sapkal and Attar 2012] [Scarth et al. 2015] [Schewe and Mai 2018] [Schmidt 1995] [Schmidt 2016] [Schmidt et al. 2016] [Schmidt et al. 2020] [Schuster and Lokos 1988] [Sefic and Maxwell 1987] [Seitz et al. 2011] [Sensburg et al. 1980] [Setoguchi and Kanazaki 2020] [Sharif et al. 2022] [Sharifi et al. 2025] [Sharma et al. 2021] [Sharma et al. 2022a] [Sharma et al. 2022b] [Sharqi et al. 2021] [Shaw et al] [Shipman and Wood 1970] [Shivaji et al. 2025] [Siegel 1972] [Silva] [Silva] [Silva and Dunn 2005] [Simmons et al. 1969] [Simmons et al. 2025b] [Singh and McDonough 2014] [Sivanandi et al. 2022] [Sleesongsom and Bureerat 2011] [Sneddon et al. 2026] [Sotoudeh and Ferman 2019] [Sotoudeh and Hosking 2018] [Soykasap and Hodges 1999] [Soykasap and Hodges 2000] [Spacht 1980] [Specification for Aeroelasticity Requirements] [Spivey et al. 2020] [Srinathkumar and Adams 1989] [Standard Specification for Aeroelasticity] [Stanford 2016] [Stanford 2021] [Stodieck et al. 2015] [Stodieck et al. 2013] [Stodieck et al. 2014] [Stodieck et al. 2017] [Stringham and Lenk 1975] [Su et al. 2016] [Su et al. 2018] [Sun and Bai 2014] [Suzuki 1990] [Svoboda and Hromcik 2019] [Svoboda et al. 2023] [Syed et al. 2022] [Takahashi et al. 2019b] [Tal and Nguyen 2015] [Taufik and Qasem 2025] [Taylor et al. 2017] [Teng 2007] [Teng and Chen 2006] [Tewari 1998] [Tewari 1999] [Theis et al. 2016] [Theodorsen 1935] [Thi Kim Dung and Phu Khanh 2021] [Thompson and Kass 1972] [Thornburgh et al. 2025] [Thuwis et al. 2009] [Tian et al. 2016a] [Tian et al. 2026a] [Tijerina et al. 2025] [Timme et al. 2010] [Ting et al. 2015] [Ting et al. 2017b] [Toker and Ozbay] [Torok 1996] [Triplett 1980] [Tsushima and Su 2017] [Tsushima et al. 2018] [Tsushima et al. 2019] [Sudha et al. 2025] [Uhl and Petko 2007] [Ursu et al. 2018] [van ‘t Hoff et al 2024] [Vanek 2024] [Vanek et al. 2025] [Vatandas et al. 2015] [Voracek 1993] [Voss et al. 2026] [Waisanen and Perangelo 1972] [Waite et al. 2019] [Waitman and Marcos 2019] [Waitman and Marcos 2020] [Walchli et al. 1992] [Wan et al. 2003a] [Wan et al. 2005] [Wang 2019] [Wang and Xu 2018] [Wang et al. 2018b] [Wang et al. 2019] [Wang et al. 2021a] [Wang et al. 2023b] [Wang et al. 2025a] [Waszak and Buttrill 1991] [Waszak and Srinathkumar 1991] [Waszak and Srinathkumar 1992] [Waszak and Srinathkumar 1995] [Waszak et al. 2002] [Wauters 2022] [Wei Tang et al. 2005] [Weissenburger and Zimmerman 1963] [Weisshaar 1978] [Weisshaar 1979a] [Weisshaar 1979b] [Weisshaar 1980a] [Weisshaar 1980b] [Weisshaar 1981] [Weisshaar 1985] [Weisshaar 1990] [Weisshaar and Lee 2002] [Weisshaar and Zeiler 1982] [Weisshaar and Zeiler 1983] [Weisshaar 1975] [Weisshaar 1983] [Weisshaar and Crittenden 1976] [Werdes 1975] [Werter and De Breuker 2016] [White and Crimi 1961] [Wieseman et al. 2005] [Wilcox and Brenner 2011] [William et al. 2002] [Wissler et al. 1987] [Wu and Cooper 2016] [Wu and Tong 2017] [Wu and Yang 2004] [Wuestenhagen et al. 2018] [Wunderlich and Dähne 2017] [Wunderlich et al. 2017] [Xiang and Wang 2023] [Xiong and Nguyen 2024a] [Xiong and Nguyen 2024b] [Xiong and Yang 2001] [Xiong et al. 2021b] [Xiong et al. 2022b] [Xiong et al. 2022c] [Xiong et al. 2023a] [Xue et al. 2019a] [Yamane 1992] [Yamane and Friedmann 1990] [Yamane and Friedmann 1993] [Yang and Guo 2009] [Yang and Przekwas 1993] [Yang and Xia 2011] [Yang et al. 1980] [Yen et al. 1976] [Yingsong et al. 2015] [Yu 2012] [Yu and Hornung 2026] [Yu et al. 2017] [Yuan et al. 1994] [Yurkovich 2009] [Zaw and Baranovski 2026] [Zeng et al. 2009] [Zeng et al. 2017] [Zhang and Soffker] [Zhang and Wang 2019] [Zhang et al. 2020] [Zhang et al. 2025a] [Zhu and Breuer 2022] [Zimmerman and Weissenburger 1964] [Zink et al. 1998] [Zink et al. 1999] [Zink et al. 2000a] [Zink et al. 2000b] [Zink et al. 2001] [Zink et al. 2002] [Čečrdle 2015] [Čečrdle 2018] [čečrdle 2023]

Compressibility, wave drag and the high-speed wing

The transonic drag rise and what answered it. Compressibility, the drag rise, wave drag and the area rule, supercritical aerofoils, swept and slender wings, minimum-drag bodies, and drag measured in flight. 65 titles name wave drag or the area rule and 57 a supercritical aerofoil or wing, the two design answers to the rise derived in the drag section.

567 records. [A Series of Airfoils 1982] [Abdolahipour 2023] [Ackeret 1925] [Aerodynamic Drag in Cruising 2020] [Agar 1982] [Ahn and Lee 2012] [Aiken and Howard 1949] [Air Force Test Pilot School Edwards Afb Ca 1962b] [Air Force Test Pilot School Edwards Afb Ca 1991a] [Al-Jaburi et al. 2019] [Alexander and Foughner 1973] [Alexander 1947] [Aley et al. 2018] [Alshabu and Olivier 2008] [Alshabu et al. 2009] [Alviani et al. 2022] [Amouyal and Weihs 2015] [Amouyal and Weihs 2016] [An Evaluation of Sailplane 1974] [Anand et al. 2019] [Ando 1978] [Andrew 1967] [Anoosha et al. 2020] [Appendix F Flight Test 1999] [Ardema and Williams 1972] [Bachalo et al. 1977] [Bai et al. 2015] [Baier 1970] [Banks 2009] [Barbaux and Cinquin] [Barnwell 1974] [Bartasevicius and Hornung 2023] [Bartels and Bartels 1997] [Bathel et al. 2012] [Batill et al. 1982] [Bauer et al. 2026] [Beeler et al. 1956] [Benedikt 1953] [Bertelrud 1980] [Bertelrud 1981a] [Bertelrud 1981b] [Bertelrud and Graves 1994] [Biber and Tilmann 2003] [Biblarz et al. 1998] [Biot 1949] [Blake 2002] [Bobbitt 1980] [Bokser and Sudakov 2008] [Bonnema and Smith 1988] [Bonnema and Lokos 1989] [Boyden 1978] [Brandon et al. 1996] [Brandon et al. 1987] [Gonor 1964] [Hiller et al] [Hiller et al] [Brower 1989] [Brown et al. 2012] [Bui 2018] [Bulygina 1958] [Bur et al. 2002] [Burdges 1973] [Burdges 1979] [Butefisch and Stanewsky 1987] [Caballero 2001] [Calarese and Walterick 1978] [Calarese and Walterick 1979] [Carlsen 1994] [Carrese et al. 2016] [Chadsey and Yechout 2001] [Chan et al. 2017] [Chandrasekhara et al. 1990] [CHAPTER NINE. the Minimum 1990] [Chaussee 1978] [Chen and Zhang 2006] [Chen et al. 2021] [Cheng et al. 1980] [Cheung 1993] [Chin and Rizzetta 1979] [Chinvorarat et al. 2024] [Choudhury et al. 2020] [Chow 1979] [Chow and Goorjian 1982] [Chowdhury and Keshmiri 2024] [Clark and Harris 1952] [Clousing 1946] [Coder and Schmitz 2019] [Coiro et al. 1990] [Cosentino 1983] [Cox and Marshall 2000] [D. Supersonic and Transonic 1954] [Davies 2020a] [Davies 2020b] [Davies 2025a] [Davies 2025b] [Davis et al. 1977] [Debiasi et al. 2010] [Deck 2004] [Deck 2005] [Deck and Würz 2023] [Dehaan 1990] [Denegri et al. 2013] [Deng and Qin 2021] [Deng et al. 2023] [Deprés and Brenner 2012] [Desai et al. 1977] [Design and CFD Analysis 2024] [Design of the Circulation 1979] [Dickey 1959] [Diesperov and Lifshits 1975] [Diesperov et al. 1976] [Dietz 2005] [Ding et al. 2026] [Doherty et al. 2018] [Doig 2014] [Durston] [Douglas Aircraft CO INC Santa Monica CA 1963] [Drag Coefficient Variations 2008] [Drag Polar Measurement 2021] [Dubben and Denegri 2007] [Dudley and Torres 2007] [Duggirala et al. 2009] [Duggirala et al. 2011] [Dunbar 1968] [Duran 2026] [Polhamus and Hammond 1960] [Efimtsov et al. 2004] [Elbanna and Carlson 1989] [Eminton and Lord 1956] [Erdos et al. 1994] [Erickson et al. 1990] [Ericson and Falco 1965] [Escalera Mendoza and Hale 2020] [McFadden and Bons] [Farbridge and Smith 1977] [Faymon 1990] [Fenno et al. 1988] [Fisher et al. 2018] [Fleck 1983] [Flight performance of civil] [Flight TEST Procedures for] [Flight Vehicle Lift-Drag Characteristics 2001] [Florio et al. 2019] [Fluid Dynamics Research 1998] [Fournis 2022] [Fox et al. 1972] [Franchi and Gabellieri 2026] [Friend and Sakamoto 1978] [Fujita et al. 2001] [Funk and Mickleboro 1953] [Fusi et al. 2015] [G. the Experimental Aerodynamics 1957] [Gao 2023] [Garabedian 1976] [Geissler et al. 2005] [Gerdes and Hynes 1975] [Ghate et al. 2021] [Ghoreyshi et al. 2017] [Ghoreyshi et al. 2022] [Gibbons and Batina 1989] [Gibson 1949] [Gillan 1993] [Glauert 1928] [Goecke 1973] [Gonor 1960] [Gonzalez et al. 2026] [Gotlieb 1977] [Gotlieb et al. 1976] [Goto et al. 2007] [Goupil] [Graham and Yeow 1990] [Green 2008] [Gresham et al. 2024] [Guan 2014b] [Guan 2014a] [Gudmundsson 2014b] [Gudmundsson 2022b] [Guerreiro and Hubbard 2008] [Gupta 1990] [Gusarov and Levin 1981] [Guy et al. 2001] [Gölcük and Kurtulus 2026] [Haderlie and Crossley 2009] [Hafez et al. 1978] [Hafez et al. 1979] [Harper 1953] [Harrison et al. 2016] [Hart 1984] [Hart and Schmitz 2022] [Hasan and Alam 2013] [Henne and Hicks 1978] [Hess 1986a] [Hicks et al. 1976] [High-Supersonic/Hypersonic Flows 2012] [Hinchliffe and Qin 2016] [Hinchliffe and Qin 2017] [Hitzel 2015] [Hoffmann et al. 1978] [Holt 1976] [Horstman 1987] [Howell and Korst 1971] [Hu et al. 2026] [Hue and Molton 2020] [Huffman and Fox 1978] [Huffman and Fox 1979] [Hurley et al. 1975] [Volkov 2023] [Induced Drag Effect 1976] [Inger 1991] [Ishida et al. 2016] [Jacob and Amitay 2022] [Jacques et al. 2001] [Jaffe 1975] [Jameson 1979] [Janić 2025] [Jann and Greiner-Perth 2009] [Joels and Raveh 2022] [Joels and Raveh 2023] [Johnson 1985] [Johnson and Spaid 1981] [Jones 1946] [Jones 1947] [Jones et al. 2000] [Jones et al. 2006] [Jones 2017] [Joshi 1996a] [Joshi 1996b] [Jumper 1983] [Jurado and McGehee 2024] [Kandil and You 2002] [Kandil et al. 1993] [Kaneko et al. 2024] [Kannemans 1995] [Karlgaard et al. 2016] [Kawai and Fujii 2005] [Keener 1984] [Kempel et al. 1989] [Khalid 2023] [Khlebnikov 1990] [Kianvashrad and Knight 2017] [Kiel 1939] [Kinsey and Eastep 1988] [Klausmeyer 2004] [Klingenberg and Belke 2024] [Klopfenstein 1965] [Klutchnikov and Ballmann 2004] [Knaus 1981] [Kostic et al. 2002] [Kouznetsov 1994] [Kraiko and Pudovikov 1998] [Kraiko and Tilliaeva 1973] [Kraiko and Tkalenko 1967] [Kraiko et al. 2025] [Kress 1983] [Kroos 1995] [Kubota 2008] [Kuhl et al. 1958] [Kulfan 1990] [Kulfan and Sigalla 1978] [Kumar et al. 2023b] [Kusunose et al. 1999] [Kutney and Piszkin 1963] [Kutty et al. 2015] [Kuz’min 2010] [Küchemann 1957] [Ladyzhenskij 1963] [Lan et al. 1995] [Lan et al. 2006] [Langley Research Center 1966] [Lapshina and Ostapenko 2009] [Larson 1986] [Lee 1989] [Lee et al. 2017a] [Lemko and Molodchyk 2015] [Lemley and Mullans 1973] [Leylek and Costello 2013] [Li 2024] [Li et al. 2022c] [Lin et al. 1990] [Liu and Fung 1987] [Liu et al. 2012b] [Lock 1957] [Loftin 1967] [Loftin 1968] [Lorang and Carr 2017] [Lord and Eminton 1954] [Luckert 1973] [Luskin 1950] [Macha 1977] [Madagan 1969] [Manela 1983] [Mani et al. 2010] [Markhotok 2021] [Marschalk et al. 2021] [Mason 1982] [Masson et al. 1998] [Masson et al. 1999a] [Masson et al. 1999b] [Materials for Supersonic Civil 2015] [Mathews and Thompson 1947] [Matranga and Peele 1957] [Mavriplis and Levy 2002] [Mavriplis and Levy 2005] [Mavriplis and Levy 2001] [Mayne 1979] [Mazurov and Takovitskii 2022] [McDonald et al. 1982] [McGowan and Cooney 1957] [McGregor and White 1970a] [McGregor and White 1970b] [Mehta and Mehta 1997] [Mele et al. 2017] [Meng et al. 2022a] [Meng et al. 2022b] [Menzies and Kandil 1996] [Mertens et al. 1986] [Mertens et al. 1987] [Methods for Drag Determination 2003] [Meyer and Deangelis 1978] [Miles 1953] [Miles 1954] [Milholen and Owens 2005] [Miller et al. 2019] [Minervino and Tognaccini 2023] [Mitchell and Peck 1949] [Mizobata et al. 2011] [Mizobata et al. 2024] [Moga 1980] [Monaghan 1978] [Morgan and Visbal 2019] [Morrida et al. 2016] [Morrida et al. 2017] [Moses and Shah 1998] [Motyka and Reynolds 1971] [Muller and Wesshaar 1994] [Munk 1921] [Muralidharan et al. 2025] [Murman and Cole 1974] [Murphy and Schmidt 1953] [Murray et al. 2002] [Ames Research Staff 1953] [NACA Conference on Aerodynamic 1949] [Nae 1998] [Nagamatsu and Orozco 1984] [Nagamatsu et al. 1987] [Neely et al. 2003] [Nelson and Stoney 1953] [Nghiem and Norstrud 1989] [Ngoc 2007] [Nguyen et al. 1980a] [Nielsen 1985a] [Nielsen 1985b] [Niewald and Parker 1999a] [Niewald and Parker 2000] [Nikfetrat et al. 1992] [Nikolic and Jumper 2004] [Ning and Kroo 2011] [Niu et al. 2023] [Nixon 2003] [Nonweiler 1973] [Ogawa and Babinsky 2005] [Ohman 1983] [Olson and Bielat 1955] [Ooda 2022] [Oswald 1932] [Pack et al. 2002] [Pack et al. 2003] [Pack-Melton et al. 2007] [Pahle et al. 2012] [Palchekovskaya 2019] [Parlier 1983] [Peach et al. 1980] [Pendleton 1965] [Pfenneberger 1966] [Phillips et al. 1983] [Pierpont 1957] [Pipko 1966] [Polhamus and Toll 1981] [Porter 1965] [Powers 1988] [Powers 1978b] [Prandtl 1928] [Prescott 1963] [Price 1978] [Price 1981] [Prichard and Sankar 1988] [Properties and Design 2012] [Qin 2012] [Quadrio et al. 2022] [Ramaswamy 1987] [Ramaswamy and Viswanathan 1975] [Ramm 1990] [Reeh and Tropea 2014] [Reichert 1947] [Reichert 1950] [Rein et al. 2009] [Reshotko 1970] [Rhode 1935] [Rhyne and Murrow 1957] [Whitcomb 1956] [Richards 1997] [Riggins et al. 1998] [Riggins et al. 1999] [Rivers et al. 2001a] [Roach and Froning 1996] [Roberts 1963] [Robinson 2004] [Robinson et al. 1985] [Robinson et al. 2020] [Rogers and Walter K. 1953] [Rogers and Walter K. 1958] [Rolls 1947] [Roohani and Skews 2009] [Roos 1975] [Rose and Seginer 1977] [Rothacker 2017] [Russo et al. 2020a] [Russo et al. 2020b] [Sachs and Schoder 1991] [Sahu and Steger 1987] [Saltzman and Ayers 1995] [Sammonds 1970] [Sandahl et al. 1949] [Sang and Schetz 2002] [Sanghi et al. 2024] [Satre 1969] [Schmidt and Duren 2002] [Schnerr and Dohrmann 1991] [Schnerr and Dohrmann 1994] [Schufflebarger and Mickleboro 1950] [Schuringa 1974] [Sears 1947] [Second-Order Compressible Boundary Layer 1962] [Sedney 1954] [Seebass 1974] [Seginer and Rosenwasser 1983] [Seidel et al. 1985] [Seider and Haenel 1991] [Seiner and Krejsa 1989] [Serdarevic-Kadic and Terzic 2019] [Seubert 1997] [Seubert 1999] [Sforza 2018] [Shanbhag and Narasimha 1970] [Sheibani et al. 2024] [Shipilin 1964] [Shock Layer Structure 1962] [Siclari and Austin 1998] [Sigal 1984] [Singh and Stollery 1995] [Skujins and Cesnik 2011] [Slender Wings at High 1962] [Slooff 1986] [Smetana and Knepper 1973] [Smetana and Fox 1979] [Smith 1997] [Smith et al. 1987] [Smith and Farbridge 1979] [Sobieczky 1984] [Soule 1931] [Soule and Wetmore 1933] [Spaid 1964] [Spaid 1979] [Spaid and Stivers 1980] [Spearman and Fournier 1978] [Spearman and Driver 1980] [Squire and Nasser 1993] [Srinivasan and Chamberlain 2004] [Stack 1934] [Stange 1959] [Starr and Varner 1976a] [Starr and Varner 1976b] [Steger and Baldwin 1973] [Strand 1960] [Sudderth and McNeill 1976] [Suhanov et al. 2023] [Sulaeman and Djojodihardjo 1995] [Suman et al. 2021] [Sun and Hansen 1982] [Supercritical airfoil design] [Survey of Shock Tube 1962] [Sutherland 1961] [Swamy et al. 1978] [Takovitskii 2003a] [Takovitskii 2003b] [Takovitskii 2006a] [Takovitskii 2006b] [Takovitskii 2024] [Tang and Baeder 2003] [Tartinville et al. 2018] [Tenhave et al. 2025] [Tetrault et al. 2000] [Tetrault et al. 2001] [Thacker and Lan 1993] [Theofanous and Chang 2008] [Tiarn and Cavalleri 1991] [Timme and Thormann 2016] [Tjatra and Sekar 1998] [Tkalenko 1969] [Torenbeek 2020] [Toyoda et al. 2015] [Transonic and Supersonic Flight 1992] [Transonic and Supersonic Flows 2012] [Transonic Maneuver/Cruise Airfoil Design 1980] [Trim Drag and Maneuvering 2010] [Triplett and Brown 1952] [Triplett et al. 1955] [Tucker and Nelson 1947] [Tufts et al. 2013] [Turner 1965] [U.S. Supersonic Commercial Aircraft 1997] [Ueba et al. 2019] [Ueba et al. 2021] [Vachon et al. 2004] [Vadillo and Agarwal 2007] [Vadillo and Agarwal 2009] [Van Dam et al. 1980] [Van Der Vooren and Van Der Wees 1990] [Van Driest 1952] [Vassberg et al. 2002] [Veletas 2026] [Vijgen et al. 1992] [Vinh et al. 1988] [Viswanath 1988] [Viswanath and Mukund 1995] [Viswanath and Rajendra 1990] [Vogel and Schmitz 2025] [Volpe 1988] [Voronin and Shvets 1981] [Waddington] [Walker 1973] [Walkley 1986] [Walsh et al. 1988] [Wang and Wang 2012] [Ward 1968] [Weick 1928] [Weinstein 1994] [Welsh and Morrow 1950] [Westerwelt 2024] [Westhelle and Masciarelli 2003] [Wheatley 1933] [Whitcomb 1952] [Whitcomb and Clark 1965] [Whitcomb 1953] [White 1993] [Wieselsberger 1935] [Wilmoth 1977] [Wolles 1997] [Woodbury and Wallace 1974] [Woolf 2012b] [Xiao et al. 2004] [Xu et al. 2018b] [Xu et al. 2025b] [Yamamoto et al. 2002] [Yamazaki et al. 2019] [Yang and Feng 2022] [Yang et al. 2006b] [Yao et al. 2024] [Yip et al. 1992] [Yu et al. 1983] [Zhang 1988] [Zhang et al. 2026] [Zhao 2023] [Zhigulev and Zhilin 1959] [Zhu and Qin 2021] [Zingg et al. 2006] [Zurer 1995]

Configurations of the recent demonstrators

The X-57, the X-66 and their contemporaries. Distributed electric propulsion, truss- and strut-braced wings, blended and hybrid wing bodies, morphing and variable-camber wings, and vertical take-off configurations from the tilt wing to the electric vertical take-off aircraft. Its median year is 2016, and vertical take-off configurations supply 139 of its titles, distributed propulsion 91, morphing and variable camber 94, braced wings 69 and blended or hybrid wing bodies 47, so the vertical-flight questions the X-13 through X-22 block opened are the largest of the five strands.

563 records. [Jacob da Motta 2020] [Abbott et al. 1982] [Abdulrahim and Lind 2004] [Acevedo Giraldo] [Adler and Martins 2023] [Ahmed et al. 2024] [Ahn et al. 2017] [Ailon 2007] [Alonso Castilla et al. 2021] [Alsaidi et al. 2019] [Amping Airpower 2024] [Anderson et al. 2023] [Comer et al. 2025] [Application Status and Future 2023] [Aretskin-Hariton et al. 2024] [Arieli and Tauber 1979] [Aubeelack] [August et al. 2026] [Avionics 1969] [Babu et al. 2026] [Badihi et al. 2026] [Ballano Martinez et al. 2025] [Barker 1966] [Barker and Balas 1999] [Barnes et al. 1976] [Barnes et al. 1979] [Barnwell 1975] [Barnwell 1976] [Bartels 2013] [Bauersfeld and Ducard 2020] [Bazin et al. 2016] [Belte 1987] [Belák and Hromčík 2023a] [Belák and Hromčík 2023b] [Benjamin 2023] [Kacik and Goetzendorf-Grabowski 2025] [Simmons] [Simmons 2023a] [Benoit et al. 2014] [Benyamen and Keshmiri 2022] [Beppu and Curtiss 1966] [Bhandari and Chakraborty 2026] [Bhattarai et al. 2026] [Biber 2016] [Biggi et al. 2024] [Bingyan et al. 2015] [Borer et al. 2016] [Bottasso and Montinari 2013] [Bouwer and Ignatuk 2025a] [Bouwer and Ignatuk 2025b] [Bouwer and Kaiser 2019] [Bradley and Droney 2015] [Bradley et al. 2015] [Bravo et al. 2021] [Brewer 1966] [Bridges et al. 1977] [Brooks and Mackall 1984] [Brown 1965] [Brown 1989] [Brown 1997] [Browne et al. 2024] [Browne et al. 2025] [Bryant et al. 1984] [Buch and George M. 2010] [Buffington 1997] [Byrnes et al. 1974] [Cabarbaye] [Cai et al. 2026] [Camacho 1991] [Camacho et al. 2020] [Campbell 1959] [Carpenter 1951] [Carpenter and Shivers 1956] [Carpenter 1952] [Cetinsoy 2015] [Chakraborty 2019] [Chakraborty et al. 2015] [Champine 1971] [Chana and Sullivan 1993] [Chattopadhyay et al. 1995a] [Chau et al. 2026] [Chau and Zingg 2022] [Chau and Zingg 2023] [Chaudhary et al. 2020] [Chen et al. 2015] [Chen et al. 2025] [Cheng et al. 2023a] [Choi et al. 2026] [Christiansen 1984] [Droney et al. 2020] [Clark 1964] [Clark et al. 1963] [Cole and England 1967] [Collercandy 1992] [Comunian et al. 2026] [Comunian et al. 2025] [Contreras-Torres et al. 2022] [Corcau et al. 2026] [Corsiglia et al. 1990] [Corsiglia et al. 1991] [Cox and Roskam 1990] [Crogan 1961] [Crossley et al. 2011] [Culpepper et al. 2022] [Cunningham et al. 2022] [Curtiss et al. 1967] [Curtiss 1969] [Cusati et al. 2023] [D. Propellers for High 1957] [Daniel and Hendrick 2023] [de Vries and Vos 2022] [de Vries and Vos 2023] [de Vries et al. 2019a] [de Vries et al. 2019b] [Decker et al. 1994] [Deere et al. 2016] [Dela Peña 2026] [Denieul et al. 2015] [Derby et al. 2003] [Detore and Gaffey 1969] [Dikshit et al. 2022] [Dimopoulos et al. 2019] [Distributed Electric Propulsion 2018] [Dittmar 1988] [Dooley and Yeary 1979] [Dragos Daniel et al. 2026] [Drinkwater et al. 1958] [Drinkwater et al. 1964] [Dukes 1970] [Edenborough 1967] [Egerton and Fitzpatrick 1967] [Eisenberg and Bowles 1986] [ElSharkawy et al. 2024] [Empey and Nahon 2022] [Enciu 2019] [Eqbal et al. 2022] [Eqbal et al. 2023] [Erhard and Alonso 2022] [Erickson et al. 1965] [Erickson et al. 1985] [Evangelista and Mori 2025] [Feng et al. 2026] [Ferris and Khorrami 2024] [Filippoli et al. 2026a] [Filippoli et al. 2026b] [Finistauri et al. 2012] [Flow Control and High-Lift 2016] [Foulke 1965] [Fredericks 2015] [Freeman and Klunk 2018] [Friehmelt 1996] [Friend 1964] [Fry 1965] [Fry 1967] [Fu et al. 2022b] [Fugate et al. 2019] [Gallagher and Wei 2008] [Gallani et al. 2020] [Gao et al. 2019] [Gennaretti et al. 1996] [Gern et al. 2001] [Gilbrook et al. 2023] [Gillis 1957] [Ginn 2014] [Ginn 2015] [Glazkov et al. 2016] [Gohardani et al. 2011] [Gordnier et al] [Gordnier et al. 2006] [Gorton 2015a] [Gorton 2015b] [Gracey 1967] [Grant et al. 2006] [Grasmeyer 1999] [Gregory et al. 2015] [Gur et al. 2009] [Gur et al. 2010a] [Gur et al. 2010b] [Gur et al. 2011] [Gustafson and Gessow 1947] [Guy 1976] [Ha et al. 2020] [Hall et al. 1953] [Hansmann and Stumpf 2025] [Hanson 1989] [Hargraves 1961] [Harrison et al. 2020] [Hasan et al. 2022] [Hasbrook 1957] [Havey and Kline 1989] [He et al. 2022] [Heiss et al. 1992] [Helicopter and V/Stol Aircraft] [Hepler et al. 1973] [Herzog et al. 2021] [Hessman 1982] [Hilbert et al. 1986] [Hohenemser and Yin 1973] [Holdaway 1954] [Holdaway 1955] [Holzhauser et al. 1964] [Hoogreef et al. 2019] [Hooker 2014] [Hsu and Liu 2021] [Hu-Sheng Wu et al. 2015] [Hua et al. 2025] [Huang et al. 2024] [Huang et al. 2025c] [Hughes and Wernicke 1974] [Humphreys-Jennings et al. 2020] [Iannuzzo et al. 2018] [Idsardi 1983] [Inoyama et al. 2007] [Inoyama et al. 2008] [Integration and Simulated Flight 1977] [Islam et al. 2025] [Ivaldi et al. 2015] [Jackson 2023a] [Jacobsen and Greif 1972] [Jacobson 1964] [Jagtap 2025] [Jenkins and Marks 1975] [Jensen and Pera 1977] [Jesudasan et al. 2026] [Jiang and Pakmehr 2022] [Jianghao et al. 2011] [Jo and Majid 2023] [Wheatley 1934] [Campbell 1964] [Ham et al. 1993] [Johnson 1954] [Johnson 2004] [Johnston 2016] [Jones and Rao 1970] [Jones and Nisbet 1974] [June et al. 2022] [Jung and Lowenberg 2005] [Jutte et al. 2024] [Kalemaris 1980] [Kambampati et al. 2016] [Kang et al. 2013] [Kang et al. 2023b] [Kapania et al. 2022] [Karimi Kelayeh and Djavareshkian 2024] [Kaul 2024] [Kaul and Nguyen 2014] [Kaul and Nguyen 2015] [Kaul and Nguyen 2018] [Kaul and Nguyen 2019] [Kaygan and Ulusoy 2018] [Kannan et al] [Kelley and Scheiman 1963] [Kelley and Scheiman 1967] [Kelly et al. 2025] [Kelly and Winston 1965] [Kemmerly 1990] [Kerr 2025] [Khoshlahjeh et al. 2011] [Kim 2004] [Kim and Winchenbach 1985] [Kim et al. 2018b] [Kirby 1957] [Klimczyk and Goraj 2019] [Klunk and Freeman 2018] [Konuk and Landman 2023] [Kou et al. 2023] [Kress 1980] [Kucera and Hromčík 2013] [Kuhn 1979] [Kusunose et al. 1987] [Pascioni et al. 2026] [La et al. 2018] [Lada and Kontis 2009] [Landberg et al. 2025] [Lange 2018] [Lavi 1967] [Leader et al. 2024] [Lebacqz and Scott 1984] [Lebofsky et al. 2015b] [Lee and Yee 2024] [Lee et al. 2008] [Lee et al. 2017b] [Lee-Rausch et al. 2004] [Legrand et al. 2025] [Leon et al. 2009] [Level Flight Performance Flight 2003] [Li and Cao 2025] [Li et al. 2023] [Li et al. 2022a] [Li et al. 2022b] [Li et al. 2024] [Li et al. 2025b] [Li et al. 2026c] [Liebeck 2002] [Litt 2026] [Liu et al. 2015b] [Liu et al. 2017d] [Liu et al. 2019] [Louisse and Marshall 1976] [Love 2022] [Lu et al. 2025] [Lundstrom and Baber 1956] [Luu 2025] [Lympany and Page 2024] [Ma et al. 2020] [Ma et al. 2024] [Ma et al. 2026a] [MacLean et al. 1992] [Mallen and Dancik 1959] [Marques 2013] [McKinney and Newsom 1962] [McNally and Bach 1988] [Meadows et al. 2012] [Meheut et al. 2012] [Melo] [Mosher 2005] [Michaud et al. 2018] [Mihaloew and Drummond 1989] [Mikami and Uchiyama 2015] [Miley et al. 1981] [Miller and Clark 1965] [Mohan and Kumar 2026] [Montgomery and Hunsaker 2022] [Moore and Ning 2018] [Moore and Ning 2019] [Moore et al. 1993] [Moosavian 2021] [Morani et al. 2024] [Morelli et al. 2023] [Morphing Wing Technologies 2018] [Morris and Tigner 1995] [Morris et al. 2014] [Morris 1978] [Morse and Newhouse 1961] [Moss et al. 1991] [Murphy et al. 2002] [Muñoz] [Nalianda and Singh 2014] [Nark et al. 2017] [Narramore and Yen 1982] [Doo et al. 2021] [Nasir and Kuntjoro 2013] [Nasir et al. 2015] [Nathan 2026] [Nelson 1956] [Neogi et al. 2025] [Neumannn et al. 2016] [Newsam et al. 2024] [Nguyen and Xiong 2021] [Nguyen and Xiong 2023b] [Nguyen et al. 2021a] [Nguyen et al. 2021b] [Ni et al. 2025] [Nicola et al. 2025] [Nicolosi et al. 2022] [Niemiec et al. 2014] [Niessen 1969] [Nishikawa and Rinoie 2024] [Niu et al. 2026] [Norman and Somsel 1967] [Oblique Wing Aircraft 2020] [Obradovic and Subbarao 2010] [Obradovic and Subbarao 2011a] [Obradovic and Subbarao 2011b] [Obradovic and Subbarao 2012] [Orefice et al. 2020] [Ouellette et al. 2023] [Ozbek et al. 2024] [Oztekin and Bain 2024] [Nishanth et al. 2019] [Pagano 2018] [Panayotov and Zikyamov 2026] [Papathakis] [Papathakis et al. 2017] [Parello] [Peigin and Epstein 2006] [Peigin and Epstein 2007] [Peigin and Epstein 2015] [Pellerito et al. 2024] [Pelykh and Andryushchenko 2024] [Perry et al. 2021] [Peter and Stumpf 2018] [Peterson and Grant 2011] [Popov et al. 2008] [Popov et al. 2010a] [Powers et al. 1992] [Powers 1978a] [Price 1964] [Propeller/Propfan In-Flight Thrust Determination] [Pruitt and Bates 1992] [Pruyn and Taylor 1970] [Putnam and Littell 2020] [Rabourdin et al. 2014] [Radotich 2026] [Raheem et al. 2019] [Rahman and Akbar 2026] [Rahman and Whidborne 2010] [Raymer 1988] [Razon et al. 2023] [Recine et al. 2025] [Renselaer 1977] [Rhoads 1970] [Rich 1969] [Kirby 1960] [Roberts et al. 1966] [Robinson 1959] [Rongqi and Jianmei 2013] [Rosen and Yaffe 2001] [Rosenstein 1989] [Rotorcraft Handling Qualities Design 2011] [Roysdon and Khalid 2011] [Rylko et al. 2025] [Sadoway and Ghaemi 2026] [Saifuddin et al. 2025] [Salkind 1973] [Saltzman et al. 1956] [Samuels and Payne 1990] [Sanders 1964] [Satria Palar et al. 2024] [Sawyer and Trant 1950] [Schade 1968] [Scheerer et al. 2013] [Schiltgen et al. 2012] [Schiltgen et al. 2013] [Schiltgen et al. 2014] [Scientific and Technical Information Division 1966] [Seber et al. 2011] [Sgueglia] [Sharpe and Agarwal 2019] [Shen Guangchen et al. 2017] [Sherman et al. 2021] [Sherrow et al. 2026] [Shi et al. 2024] [Silva] [Sinha 2026] [Skillen and Crossley 2008] [Smith et al. 2007] [Smith et al. 2014] [Snyder 2020] [Soikkeli et al. 2023] [Solano et al. 2023] [Song et al. 2026] [Spearman et al. 1977] [Srinathkumar 2011] [Stephan et al. 2022] [Sticchi et al. 2024] [Sticchi et al. 2026] [Stoia et al. 2016] [Stoll and Veble Mikic 2016] [Stroscher et al. 2013] [Sun et al. 2016] [Sun et al. 2025] [Supersonic Flows over Wings 2021] [Supersonic Flows over Wings 2025] [Suzuki et al. 2019] [Synodinos et al. 2018] [Szczyglowski et al. 2019] [Taflan and Gulum 2026] [Tarnowski 2017] [Taubert et al. 2021] [Theodore et al. 2014a] [Thomas and Agarwal 2023] [Thomas and Agarwal 2025] [Thomason 1983] [Chau and Duensing] [Ting et al. 2014] [Ting et al. 2017a] [Ting et al. 2018] [Tomić et al. 2017] [Tongbiao Guo et al. 2017] [Transonic Aircraft Configurations 2012] [Travassos et al. 1980] [Tuck 1970] [Twesme and Corzine 2003] [Ugwueze et al. 2023] [Rohit 2024] [Van Gaasbeek 1980] [vanDam et al 1995] [Varela Martínez] [Verrastro and Metge 2015] [Vertical Takeoff and Landing 2014] [Vos et al. 2002] [Vos et al. 2007b] [Vos et al. 2010] [VTOL 1969] [Wada and Igawa 2021] [Wada et al. 2018] [Wakayama 2000] [Walker and Postlthewaite] [Walker et al. 1993] [Wang and Hu 2026] [Wang et al. 2000] [Wang et al. 2016c] [Wang et al. 2021c] [Wang et al. 2023a] [Wang et al. 2025c] [Wang et al. 2026b] [Wei et al. 2021] [Wei et al. 2024] [Weilmuenster and Hamilton 1986] [Weisshaar 1994] [Wells 2017] [Wells 1989a] [Westbrook 1964] [Wheatley 1935] [Whitcomb 1983] [White and Innis 1959] [Wijerathna and Annasiwaththa 2025] [Wilcox and Quigley 1978] [Wildschek 2014] [Wilkerson and Linck 1975] [Windolph 1969] [Withrow-Maser et al. 2020] [Woodbury 2003] [Wright and Bilgen 2019] [Wu and Xu 2023] [Wu et al. 2017] [Wu et al. 2023a] [Xiao et al. 2024] [Xie et al. 2019] [Xie et al. 2023] [Xijuan et al. 2016] [Xiong and Nguyen 2022] [Xiong and Nguyen 2023] [Xiong et al. 2019] [Xiong et al. 2020] [Xiong et al. 2021a] [Xiong et al. 2021c] [Xiong et al. 2022a] [Xiong et al. 2023b] [Xiong et al. 2026] [Xu 2012] [Xu et al. 2018a] [Yan and Chen 2019] [Yan et al. 2025] [Yang et al. 2015] [Yang et al. 2018] [Yang et al. 2022a] [Yang et al. 2026] [Yanguo and Huanjin 2009] [You et al. 2020] [Yu and Kim 2024] [Yue 2026] [Yue et al. 2009] [Yue et al. 2017a] [Yue et al. 2017b] [Zelinski et al. 2025] [Zhang and He 2026] [Zhang et al. 2015] [Zhang et al. 2016] [Zhang et al. 2025b] [Zhao 2026] [Zhao and Hu 2013] [Zhao and Kapania 2019] [Zhao et al. 2023d] [Zhao et al. 2025b] [Zheng et al. 2012] [Zheng et al. 2025a] [Zheng et al. 2025b] [Zhou et al. 2022] [Zientek 2001] [Öznalbant and Kavsaoğlu 2018] [Świtała and Lipski 2026]

Hypersonic airbreathing propulsion and vehicle design

The X-43 and X-51 question, generalised. Scramjet and dual-mode ramjet combustion and mode transition, inlets and isolators, waveriders and hypersonic vehicle design optimisation, combined-cycle propulsion and the hypersonic flow research behind them. Its median year is 2012, and 161 titles name a scramjet, 100 a waverider and 55 a combustion-mode transition, the question the review above says the field has moved to.

514 records. [Abbass 2024] [Abdel-Salam and Carson 2004] [Abdel-Salam et al. 2001a] [Abdel-Salam et al. 2001b] [Advisory Group for Aerospace Research and Development 1997] [Aerothermodynamics of the Dual-Mode 2001] [Aguilera and Yu 2017] [Aguilera Munoz and Yu 2014] [Ahuja and Hartfield 2009] [Air Arc Simulation 1962] [Air Force Test Pilot School Edwards Afb Ca 1987] [Aircraft Design 1993] [Aksu and Uslu 2017] [Allen 1964] [An et al. 2020] [An et al. 2021] [Anderson 1987] [Antonison et al. 1989] [Arad 2026] [Attar et al. 2026] [Aupoix 1993] [Austin] [Autenrieb 2023] [Ayers 1990] [Babu 2021] [Bakos] [Balakrishnan et al. 1997] [Barkmeyer et al. 2005] [Baron and Efrat 1979] [Barth] [Barz 2026] [Baurle and Eklund 2001] [Becker 1950] [Berens and Bissinger 1998] [Bezerra et al. 2024] [Bhagwandin and Sahu 2023] [Billig 1993] [Birrer and Stemmer 2012] [Blankson and Pyle 1993] [Bogar et al. 1999] [Bogdonoff 1999] [Bolender and Doman 2005] [Boles and Milligan 2013] [Bonelli et al. 2011] [Borg et al. 2025a] [Bouchez 2001] [Boudreau et al. 1993] [Bowcutt 1992] [Boyce and Paull 2001] [Boyce et al. 2003] [Brinda et al. 2006] [Brown and Boyce 2012] [Bu and Ma 2023] [Burkardt and Franciscus 1990] [Burnett and Lewis 1993] [Bussing and Murman 1983] [Byun and Kim 2026] [Böhrk 2015] [Cain and Walton 2003] [Callies and Wimmer 2000] [Cao et al. 2007] [Cao et al. 2014] [Cao et al. 2020] [Carlomagno et al. 1993] [Cattolica 1993] [Cavolowsky and Newfield 1992] [Sobieczky and Dougherty 1991] [Centlivre 2023] [CFD Optimization and Test 1994] [Chan and Ihme 2014] [Chan and Ihme 2016] [Chaput 1987] [Characteristics of the HIEST 2002] [Chauffour and Lewis 2003] [Chauffour and Lewis 2004] [Che and Tang 2008] [Chemical Effects in External 1962] [Chemical Kinetic Effects 1962] [Chen et al. 2006] [Chen et al. 2008] [Chen et al. 2013] [Chen et al. 2018] [Chen et al. 2019] [Chen et al. 2024] [Cheng et al. 2023b] [Chern et al. 1994] [Choubey and Tiwari 2022a] [Choubey and Tiwari 2022b] [Choubey and Tiwari 2022c] [Chuanzhen and Peng 2021] [Chuanzhen et al. 2022] [Chun et al. 2006] [Churchward et al. 1998] [Cipollini and Muylaert 2006] [Cliff et al. 1992] [Cong and Kunfeng 2017] [Connolly et al. 2021] [Continuing to Push 2006] [Cox et al. 1995] [Creagh et al. 2012] [Creating Hypersonic Flow 2019] [Cui et al. 2013] [Curran 2001] [Curran et al. 2018] [Curran et al. 2019] [Curry et al. 1992b] [Cutler et al. 2018] [D’Amico et al. 2004] [Dadd et al. 2006] [Deepak et al. 2006] [Deepak et al. 2008] [Deepak et al. 2022] [Defoort et al. 2014] [Dekkala et al. 2024] [Depiro] [Design of a Hypersonic 1993] [Dessornes and Scherrer 2005] [Dessornes et al. 2001] [Diamond 1988] [Dietrick 2013] [Ding et al. 2015] [Doherty] [Dolnik and Michaels 2025] [Dolvin 2008] [Dolvin 2009] [Donohue 2013] [Dou et al. 2022] [Du et al. 2017] [Dual-Mode Combustion Scramjet 2022] [Duan and Zhong 2010] [Duan et al. 2011] [Duran and Zeng 2026] [Edquist 2006] [Edwards 1992] [Eggers 2002] [Eggers et al. 1958] [Eggers and Novelli 1999] [Eggers et al. 2005] [Eklund et al. 2001] [El-Sayed 2016] [Elkowitz et al. 2023] [Engblom et al. 2005] [Esposito 2023a] [Evans et al. 2011] [Exton 1993] [Eyi and Yumusak 2012] [Eyi et al. 2018] [Falempin 1999] [Falkiewicz et al. 2011] [Fedioun and Orlik 2012] [Feng et al. 2022] [Ferguson and Anderson 1993] [Ferguson et al. 2015a] [Ferguson et al. 2015b] [Ferguson et al. 2016] [Ferreira de Moura and Borges Ribeiro 2025] [Ferrier et al. 2006] [Ferrier et al. 2008] [Foster 1989] [Fotia 2015] [Freakley] [Geiger et al. 2026] [Ghosh and Ogawa 2022] [Glass and Glass 2002] [Gnoffo 1989a] [Gnoffo 1989b] [Goldfeld 2003] [Gong et al. 2014] [Gong et al. 2024] [Gong Weijie and Tang Shuo 2010] [Gong Weijie and Tang shuo 2010] [Goodwin et al. 2019] [Goonko and Mazhul 2002] [Gopal and Wilson 2016] [Gottlieb et al. 2024] [Goyne et al. 2006] [Grant et al. 2000] [Grantz 1994] [Graves 2013] [Graziani et al. 2025] [Guelhan et al. 2026] [Guizzo 2004] [Gülhan et al. 2023] [Gülhan et al. 2024] [Hagenmaier et al. 2013] [Hall and Poggie 2019] [Hanson 1993] [Hao et al. 2016a] [Harney 1963] [He and Le 2017] [He et al. 2009] [He et al. 2017] [Hellbaum and Garner 1988] [Heller et al. 1998] [Hicks 1993] [Hirschel and Weiland 2009b] [Holguin et al. 2018] [Houchin 2006a] [Hsia et al. 1989] [Hu et al. 2015] [Huang et al. 2017a] [Hughes et al. 2013] [Hunt] [Hypersonic Flight 2025] [Hypersonic Flow Research 1962] [Ide et al. 1989] [Igra 2018] [Igra 2019] [Ikawa 1989] [Iliff and Shafer 1993a] [Iliff and Shafer 1995] [Inviscid Hypersonic Flow Introduction 1962] [Ishikawa and Yamazaki 2021] [Ispir and Saracoglu 2019] [Ito et al. 1999] [Jaeger and Hemati 2025] [James 2022] [Javaid and Serghides 2003] [Javaid and Serghides 2004] [Jee] [Jensen and Braendlein 1996] [Jia et al. 2019] [Jia et al. 2021] [Jin et al. 2023] [Jing and Shuo 2008] [Jing and Yuan-pei 2015] [Jo et al. 2024] [Johnston] [Jones 2002] [Jones et al. 1993] [Jorris 2014] [Kanapathipillai and Yu 2024] [Karanian and Kepler 1965] [Karl et al. 2006] [Kato et al. 2006] [Kelso 1993] [Keshmiri et al. 2006] [Khambaswadkar 2024] [Kim et al. 1982] [Kim et al. 1983] [Kim et al. 2010] [Kimmerly] [Klothakis and Nikolos 2024] [Knight 2002] [Knittel and Lewis 2012] [Ko 1997] [Kontogiannis et al. 2015a] [Kontogiannis et al. 2015b] [Kossira et al. 1993] [Kouchi et al. 2012] [Krause 1992] [Kumar et al. 2022] [Kumar et al. 2023a] [Kuranov and Korabelnikov 2008] [La Sorsa et al. 2025] [Ladeinde et al. 2017] [Laflamme 1970] [Lantz 1998] [Lau 2025] [Le et al. 2005] [Lee] [Lee et al. 2026] [Lees and Kubota 1972] [Leng et al. 2024] [Leng et al. 2025] [Lewis 1991a] [Lewis and Paull 1998] [Li and Wang 2017] [Li and Wey 1988] [Li et al. 2017a] [Li et al. 2017b] [Li et al. 2019b] [Li et al. 2026a] [Lillis 1987] [Limage 1996] [Lin and Luo 1995a] [Lin and Luo 1995b] [Liu and Bai 2024] [Liu et al. 2020a] [Liu et al. 2014] [Liu et al. 2016b] [Liu et al. 2017b] [Liu et al. 2018] [Liu et al. 2026b] [Liu et al. 2026d] [Lobbia 2015] [Lobbia 2017] [Lobbia and Suzuki 2014] [Lonkar and Panda 2025] [Lonkar and Panda 2026] [Lu 1991] [Luo et al. 2003] [Luo et al. 2026a] [Lyu et al. 2018] [Ma et al. 2025] [Ma et al. 2017a] [Ma et al. 2026b] [Mackle] [Mackle and Jahn 2024] [Mahmoud et al. 2017] [Marcum 2001] [Markopoulos and Mease 1990] [Marschall 2011] [Matthews and Jones 2005] [Maxwell 2016] [Mbagwu and Driscoll 2018] [Mead 1998] [Mease and Vinh 1988] [Medina et al. 2021] [Mehta 1989] [Meng et al. 2022c] [Meng et al. 2022d] [Meng et al. 2024a] [Meng et al. 2024b] [Meng et al. 2025] [Metro et al. 2026] [Meuwly 2014] [Micka and Driscoll 2009] [Mitani 1995] [Mogavero and Brown 2018] [Mohieldin and Carson 2003] [Mohieldin et al. 2001] [Molvik et al. 1993] [Mori et al. 2002] [Morita and Tsuchiya 2019] [Murray and Steelant 2009] [Musa et al. 2022] [Musal et al. 1964] [Nakatani et al. 2009a] [Nance 2013] [Newberry 1995] [Newberry 1998] [Newtonian Theory of Hypersonic 1962] [Ngo] [Niu and Piao 2016] [North American Aviation INC LOS Angeles CA 1964] [Ogawa 2023] [Ogawa 2024] [Okojie et al. 2009] [Olds and Bellini 1998] [Olivon et al. 2024] [Onozeki et al. 2026] [Ouzts 2008] [Ouzts et al. 2009] [Owen 1993] [Parker 2022] [Paynter 1988] [Peng and Wang 2026] [Perlini et al. 2026] [Petley et al. 1991] [Ping Li et al. 2010] [Polezhaev 2000] [Pollock and Wild 2024] [Potsawat et al. 2019] [Powers et al. 1986] [Pratt and Heiser 1993] [Preller] [Preller and Smart 2012] [Prilliman and Francis 1980] [Qiang et al. 2000] [Quinlan] [Radiation at Hypersonic Speeds 1962] [Rao et al. 2023] [Rarefied Hypersonic Flow over 1962] [Reimer et al. 2025] [Ren 2009] [Rice] [Richard et al. 1990] [Richards and Monaghan 1997] [Riddell et al. 1962] [Riis et al. 2024] [Robinson and Gerwin 2001] [Rocci Denis et al. 2003] [Rockwell et al. 2010] [Rodi 2012] [Rodi 2018b] [Rodi 2018a] [Rodi 2021] [Rodi 2023] [Rodi et al. 2019] [Rodriguez-Segade Alonso et al. 2021] [Rodríguez-Segade et al. 2024] [Rodríguez-Segade et al. 2023] [Roudakov et al. 1996] [Roudakov et al. 1998] [Ryan et al. 2013] [Ryan et al. 2015] [Sacher and Zellner 1995] [Saheby et al. 2017] [Salloum et al. 2018] [Sandeep 2023] [Sarosh 2021] [Savino et al. 2015] [Savu and Trifu 1993] [Schindel 1989] [Scramjet Combustion 2022] [Serre and Defoort 2009] [Sforza 2019] [Sheffer and Dulikravich 1993] [Shen et al. 2020] [Shi 2016] [Shi et al. 1994] [Shirouzu and Watanabe 1993] [Singh et al. 2017] [Slavin et al. 2001] [Smayda] [Smayda and Goyne 2011] [Son et al. 2022] [Son et al. 2024a] [Son et al. 2024b] [Spravka and Jorris 2015b] [Spravka and Jorris 2015a] [Sprunger et al. 2025] [Starkey 2005] [Starkey et al. 2005] [Starkey et al. 2006] [Steelant 2008] [Steelant 2009] [Steelant 2011] [Sternberg 2010] [Steva] [Stull 1989] [Sullins 1993] [Sullins et al. 1991] [Sun et al. 2023] [Suzuki 2016] [Takahashi et al. 2000] [Takahashi et al. 2025] [Takahashi et al. 2026] [Takaki et al. 1997] [Takashima and Lewis 1995] [Takashima and Lewis 1999] [Tani et al. 2023] [Tarpley and Lewis 1995] [Tatman] [The Theoretical Study 2012] [Theory of Entropy Layers 1962] [Tian et al. 2015] [Tian et al. 2016b] [Tirtey et al. 2011] [Tiwari et al. 2001] [Tomioka et al. 2016] [Torrez et al. 2011] [Tournes 2013] [Tournes and Johnson 1998] [Tsuchiya et al. 2007] [TÜRkoĞLu et al. 2026] [Ueno et al. 2011] [Van den Borre et al. 2023] [Van der lee et al 2021] [van der Lee et al. 2022] [Waidmann et al. 2024] [Walker 1949] [Walker et al. 2009] [Waltrup et al. 1980] [Wang and Lyv 2025] [Wang et al. 2018a] [Wang et al. 2023c] [Wang et al. 2024a] [Wang et al. 2025b] [Wang et al. 2025d] [Wang et al. 2026a] [Wassel et al. 1995] [Waszkowski and Pisani 2025] [Watanabe et al. 1996] [Watanabe et al. 1997a] [Watanabe et al. 1997b] [Waverider Aircraft 2012] [Weatherston 1969] [Wei et al. 2012] [Wendel and Gaitonde 2026] [Whitmore and Moes 1994] [Williams et al. 2024] [Williamson 1992] [Woodyard 2026] [Wu 2018] [Wu and Liu 2022] [Wu and Wei 2022] [Wu and Wei 2023] [Wu and Yu 2018] [Wu et al. 2016] [Wu et al. 2018] [Xia et al. 2026] [Xianyu et al. 2006] [Xiao et al. 2015] [Yan et al. 2014] [Yan et al. 2016] [Yan et al. 2022] [Yang and Qi 2016] [Yang et al. 2014c] [Yang et al. 2014a] [Yankui et al. 2005] [Yentsch and Gaitonde 2013] [Yentsch and Gaitonde 2014] [Yin et al. 2017] [You and Liang 2009] [Yu et al. 2007] [Yun et al. 2026] [Zeng et al. 2026] [Zettervall and Fureby 2018] [Zhang and Sheng 2019] [Zhang et al. 2010] [Zhang et al. 2019] [Zhang et al. 2024] [Zhang et al. 2025c] [Zhao 2021b] [Zhao et al. 2023a] [Zhao et al. 2025a] [Zhao et al. 2027] [Zheng et al. 2023] [Zhou 2023] [Zhou et al. 2023c] [Zuber and Bertin 1998] [Zweber et al. 2002]

Flight test technique and the flight research method

Flight research as a method. Flight test programmes and their planning, techniques for measuring performance, loads, handling and propulsion in flight, envelope expansion, flight test safety and the education of flight test engineers.

493 records. [A Typical Avionics Integration] [A Typical Avionics Integration 2010] [Abdallah 2018] [Abdallah et al. 2013] [Abdallah et al. 2014] [Abramov et al. 2005] [Accelerated Flight Performance 2026] [Adams 1983a] [Adams 1983b] [Adams and Graves 1983] [Adolph 1981] [Advisory Group for Aerospace Research and Development 1984] [Aiken and Wiener 1955] [Air Force Flight Test Center Edwards AFB CA 1970] [Air Force Test Pilot School Edwards Afb Ca 1962a] [Air Force Test Pilot School Edwards Afb Ca 1967b] [Air Force Test Pilot School Edwards Afb Ca 1967a] [Air Force Test Pilot School Edwards Afb Ca 1979] [Air Force Test Pilot School Edwards Afb Ca 1990b] [Air Force Test Pilot School Edwards Afb Ca 1992a] [Air Force Test Pilot School Edwards Afb Ca 1994a] [Air Force Test Pilot School Edwards Afb Ca 1995] [Aircraft as Research Tools 1999] [Alford and Knarr 1999] [Altman 2015] [American Institute of Aeronautics and Astronautics 1992] [An et al. 2024] [Analysis of Gust-Response Flight-Test 1988] [Ananthasayanam 1998] [Ananthkrishnan 2004] [Anderson et al. 1973] [Ashenden 1993] [Asher et al. 2013] [Asselin 2021] [Bach 1982] [Bach 1980] [Bajaj 2019] [Baltes and Spitz 2002] [Banks 2012] [Banks 2011] [Batterson and Klein 1984] [Beaird 1967] [Bender et al. 1984] [Benson et al. 1978] [Benyamen et al. 2023] [Blackburn and Rita 1968] [Blanchard 1990] [Bock 1976] [Boeing Co Morton Pa Vertol Div 1961] [Boeing Vertol Co Philadelphia Pa 1974] [Bogue 1992] [Bolt 1981] [Borrok and Rider 1970] [Bosworth and West 1986] [Bowers et al. 2007] [Bowers et al. 2008] [Bowers et al. 2011] [Bowles 1992] [Brajou and Ricco 2005] [Brandon and Morelli 2016] [Braun 1958] [Henderson et al] [Brennan and McDaniel 1994] [Bridges 2007] [Bromberg and Hansen 1965] [Bronz and Hattenberger 2016] [Broughton 1978] [Brown and Bradley 1981] [Brown et al. 2011] [Bulyshev et al. 2014] [Burcham et al. 1986] [Burke 1983] [Burnett 2002] [Burns 1974] [Burns 1992] [Butler and Rees 1974] [Carico 1998] [Carico et al. 2001] [Celenligil et al. 1991] [Cenko 1992] [Chapter 2. Exploring 2005] [Chen and Berry 2010] [Cheney 1977] [Chung and Hutchinson 2001] [Clousing 1964] [Cohen and Le 1991] [Communications Flight Test 2010] [Coombe 1970] [Cooney 1952] [Cord 1989] [Corda 1995] [Cox and Bobula 2015] [Cruz et al. 1969] [Czechowicz et al. 2015] [Richwine 1996] [Rinehart et al. 2025] [Zahn et al] [Deal et al. 1981] [Deel et al. 1972] [DiOttavio et al. 2014] [Dix 1964] [Dominick and Watts 1967] [Dorobantu et al. 2013] [Drake 1964] [Duke 1982] [Duke and Lux 1983] [Dungan and Clark 1994] [Dwyer 1994] [Eggers and Barth 2006] [Ellsworth et al. 1977] [Energy Analysis of High-Speed 1991] [Energy Approach to Performance 2003] [Engelien 1994] [Eppel et al. 1988a] [Eppel et al. 1988b] [Erdman 2005] [Estes and McClain 1948] [Exploring Flight Research 1999] [Exploring the Flight Envelope 2015] [Falempin and Serre 2004] [Falempin and Serre 2006] [Fechter and Mills 1988] [Ferrell et al. 1974] [Finnestead and Connor 1969] [Finnestead et al. 1970] [Fisher and Meyer 1988] [Fisher and Meyer 1989] [Fitzgerald 1992] [Fletcher 1994] [Flight Dynamics of Elastic 2014] [Flight Envelope 2021] [Flight Envelope Awareness/Protection] [Flight Performance 2012] [Flight Performance 2014] [Flight Test Manual 1959] [Flight Test Planning 2021] [Flight Test Programme 1970] [Flight Test Results 1977] [Flight Testing 1992] [Flight Tests on Way 2007] [Flittie and Curtin 1998] [Frinell 1983] [Funk and Rhyne 1956] [Gadeberg and Ziff 1951] [Ganzer et al. 1977] [Gao et al. 2022] [General Dynamics/Astronautics San Diego Ca 1961] [General Dynamics/Astronautics San Diego Ca 1962] [General Dynamics/Astronautics San Diegoca 1961] [Gibson 1981] [Giessler and Nash 1971] [Gilruth 1962] [Bever 1991b] [Gnoffo and Greene 1987] [Godwin et al. 1964] [Goetzendorf-Grabowski and Kwiek 2023] [Gong and Wu 2015] [Gorn 2003] [Grantham et al. 1985a] [Gratton 2018] [Grauer et al. 2017] [Greenwell 2004] [Gregory 1970] [Hackenberg and Hicks 2011] [Hall 2002] [Hanke 2003] [Harris and Cuthbertson 1987] [Harris et al. 1994] [Hart 1992] [Hartwig and Sonneborn 1971] [Hashii and Thompson 2018] [Head 1981] [Henke 2001] [Hensley 1994] [Henwood and Huete 2007] [Herrington et al. 1966] [Herrlinger 1991] [Higgins et al. 1968] [High-Speed Flight 1986] [High-Speed Flight 1996] [High-Speed Flight 2009] [High-Speed Flight 2010] [High-Speed Flight and Its 2010] [Hildebrand 1979] [Hill and Haering 2017] [Hill and Huhlein 1993] [Hillaker 1983b] [Hinds and Shames 1975] [Hoadley 1988] [Hodge and Meyer 1963] [Hoffstedt et al. 1973] [Holberg and Grabowsky 1981] [Hopping et al. 1986] [Horn et al. 1998] [Hou and Song 2024] [Howell 1988] [Hudson 1998] [Iliff et al. 1978a] [Ince 1967] [Incorporating Agility Flight Test 1994] [Ishmael and McMonagle 1983] [Jacobsen and Barber 1977] [Jacobson and Lavietes 2005] [Stephenson et al] [Javorsek et al. 2016] [Jiang 2024] [Johnson 1937] [Johnson 1994] [Johnson et al. 2025] [Johnson and Sandlin 1984] [Johnson and Sandlin 1986] [Jones 1970] [Jones and Wilson 1983] [Jones et al. 1983] [Jordan 1974] [Morrison and Washburn] [Kamal et al. 2015] [McMurtry and Ellis] [Kannan et al] [Kehlet and Patterson 1959] [Kelly 1974] [Kennedy 1986] [Kerber 1927] [Kimberlin and Solies 1992] [Klein et al. 1981] [Klein and Noderer 1996] [Knauber and Yanowitch 1968] [Knotts and Bailey 1988] [Koeniguer and Spear 2018] [Kohlman 1979] [Kohn and Pangilinan 1986] [Kokolios 1994] [Kolli 2024] [Kraft 2020] [Kufeld et al. 2019b] [Kufeld et al. 2019a] [Kuhn 1975] [Kukreja 2008b] [Kukreja 2008c] [Kuppuswamy and Kiran 1981] [Lamar et al. 1986] [Lan and Brandon 2003] [Lang 1981] [Large et al. 1981] [Largent 1986] [Larrabee 1967] [Layton 1986] [Level Flight Performance Theory 2003] [Lieberman 1963] [Limitations and Flight Envelope 2017] [Liu et al. 2015a] [Lowry 1995] [Luecke 1957] [Lynch 1972] [Machin et al. 2001] [Macmillan 1981] [Madsen and Cerimele 2000] [Maine and Iliff 1981] [Mallozzi et al. 2014] [Manning et al. 1992] [Manning, E et al. 1995] [Markman 1984] [Markman 1989] [Marshall 1971] [Marshall and Schweikhard 1973] [Martin 1978] [Martin Co Denver Co 1966] [Martin 1999] [Marzouk 2025] [Matheny 1950] [Mayfield and Smith 1978] [McCauley et al. 2015] [McCutcheon 1972] [McLaud and Hansen 1977] [McPherson 1977] [Melton and Hall 1968] [Melvill Jones 1938] [Menges 1995] [Methods for Reducing Data 2003] [Meyers et al. 1968] [Miller 2014] [Miller 2000] [Miller 1973] [Mizukami 2004] [Molloy 1999] [Montel and Thielecke 2015] [Morelli 1995a] [Morelli 2011] [Morelli 2012] [Morelli 2021a] [Morelli and Klein 1995] [Morelli and Klein 1997] [Morger 1988] [Morris 1963] [Morris 1964] [Moyer 1963] [Mueller and Preisser 1981] [Nagata et al. 1968] [Navarro 2005] [Neumann 2005] [Nguyen 1989] [Nicolaides 1970] [Nicolaides 1976] [Nonsteady Flight 2006] [Norton 1990a] [Norton 1990b] [O’Callaghan 2013] [Obara 1986] [Osburg et al. 2016] [Owens et al. 2006b] [Palmer 1990] [Paris and Alaverdi 2005] [Parlini and Combley 1986] [Pavlock 2013] [Pawlak 1994] [Pearson 1986] [Perrin 1956] [Perry 1984] [Petersen 1981] [Picasso et al. 1982] [Pietersen 1986] [Platz and Bounajem 1992] [Pommier-Budinger et al. 2016] [Porter et al. 2017] [Powered Flight Performance 2026] [Pugh 1992] [Putnam and Ayers 1988] [Putnam and Ayers 1989] [Quinn 2022] [Rakin 1981] [Raney and Waszak 2003] [Rasky et al. 1998] [Rauscher 1983] [Ray et al. 2002] [Recapturing NASA’s Aeronautics Flight 2012] [American Institute of Aeronautics and Astronautics 2021] [Rediess and Melton 1994] [Reed 1975b] [Reif et al. 1966] [Renaudie 1971] [Research and Analysis 2022] [Rhea and Moore 1988] [Rice 1946] [Rice and Hazlwood 1994] [Richwine and Del Frate 1995] [Richwine and Delfrate 1994] [Richwine et al. 1989] [Rigid-Body Flight Dynamics 2026] [Roberts] [Roberts 1988a] [Roberts and Shawler 1994] [Roberts and Wagner 1973] [Robertson and Hartfield 1992] [Rogers 2002b] [Rohlmann and Keye 2015] [Harney 2005] [Roth 2009] [Roth et al. 2010] [Rucci et al. 2023] [Russo and Savino 2015] [Russo et al. 1994] [Sanders 1972] [Sandlin 1984] [Scafetta 1983] [Schaefer 1948] [Schifferle et al. 1999] [Schilling and Mackall 1993] [Schneider et al. 2012] [Schwartz and Wray 1969] [Schweikhard 1983] [Schweikhard and Renz 1986] [Scott 1983] [Sehgal and Platz 2004] [Sehnert 1963] [Shafer 1982] [Shaw and Richter 1985] [Shawler 1983] [Shawler 1986] [Shepard 1965] [Shi 2003] [Shields 1981] [Siddiqi and Abraham 1988] [Siddiqi and Neate 1986] [Silz 1992] [Simon and Savage 1975b] [Simpson 1972] [Simpson 1979] [Simulating Flight Condition 2015] [Simulation in Support 1988] [Slender Aircraft for Flight 2012] [Smith and Ramirez 1986] [Smith et al. 1979] [Smith and Harrison 2010] [Smith 1966] [Smith 1967] [Snyder and Schoultz 1976] [Soule and Gracey 1938] [Srinathkumar et al. 1995] [Steady Flight Performance 2026] [Stewart 2016] [Nelson et al] [Stiles 2022] [Stojakovic] [Stoliker 2014] [Stottier 1995] [Streby 1990] [Study on the Flight 2022] [Sun et al. 2018] [Svec 1981] [Svendsen 1994] [Swann et al. 1981] [System in-Flight Testing 2010] [Szymanski et al. 2025] [Sóbester 2021] [Tangler 1979] [Tao et al. 2023] [The AGARD Flight Test 1959] [The Flight Environment 2021] [The Free Flight Range 1962] [Thigpen and Whitmoyer 1976] [Thomas 1981] [Thomas and Fairchild 1933] [Thompson et al. 2000] [Thornton and Lamy 1992] [Ratvasky] [Townsend and Phillips 1955] [Townsend and Phillips 1956] [Tracy 1981] [Traven and Whitley 1995] [Turk and Watts 1964] [Turk and Watts 1965] [Uijt_de_Haag and Vadlamani] [Vagianos and Rooney 1964] [Van Graas and Braasch 1992] [Van Pelt 1981] [Van Wyckhouse 1966] [Van Zante 2018] [Vanatta and Inderhees 1988] [Vaughn and Lindsay 1988] [Vedrenne 1983] [Venti 2012] [Verstynen 1974] [Veselenak and Beutelman 2004] [Vesely 1986] [Wagner and Webb 2000] [Walberg et al. 1987] [Waldersen 2018] [Walko and Schneider 1980] [Wallace 1978] [Wallace 2000] [Walters and Butler 1992] [Wang 2024b] [Ward 1988] [Ward and Bennett 1974] [Weichsel 1949] [Weihs et al. 2008] [Wenxuan 1991] [Wercinski 2017] [Whalen and Bragg 2005] [Wheeler 2000] [Wilcox 1973] [Williams and Hartford 1987] [Williamson et al. 1996] [Wilner 1979] [Winebarger and Neely 1984] [Wingrove 1972] [Wirth 1972] [Wolf and Sansone 2002] [Wood 1983] [Woodbury and Gorman 1983] [Woodman 1971] [Woolf 2012a] [Wright 2011] [Wygle 1981] [Wyrick 1965] [Yamakawa et al. 1984] [Yanagihara et al. 1999] [Yasue 2020] [Yechout 1988a] [Yechout 1988b] [Yechout and Braman 1984] [Yungkurth et al. 1991] [Zander 2025] [Zaw Linn 2019] [Zeisloft 1983] [Zhang 2013] [Zhang and Zhang 2016] [Zhang et al. 2011] [Zhao et al. 2023b] [Zhao et al. 2023c] [Zhenxing and Hongbin 2009] [Zhixin 2022b] [Zhu et al. 2014]

Identifying a model from flight data

How a flight is turned into numbers. Parameter estimation and system identification from flight data, input and manoeuvre design for identification, and the extraction of stability and control derivatives. This is the discipline through which the information argument of the opening section works in practice, and 18 of its titles apply neural networks or other machine learning to it.

418 records. [Advisory Group for Aerospace Research and Development 1999] [Aircraft Stability Derivatives 1998] [Aksu 2014] [Albisser] [Anderson and Vincent 1985] [Anderson et al. 1983] [Andrews and Rediess 1959] [Anton et al. 2009] [Appendix B Aircraft models] [Appendix C Stability 2021] [Approximate Expressions 1997] [Approximate Expressions 2007] [Approximate Expressions 2013] [Babcock and Arena 2004] [Bach and Wingrove 1985] [Bach and Wingrove 1983] [Bachelder et al. 2004] [Bachelder et al. 2011] [Baer-Riedhart and Landy 1987] [Hosseini et al. 2025a] [Basappa and Jategaonkar 2004] [Basappa et al. 2006] [Batterson and Klein 1983] [Beharie et al. 2015] [Benders et al. 2018] [Benders et al. 2020] [Simmons and Murphy] [Simmons et al] [Brcich and Zoubir] [Brenner 2001] [Brooks 1986] [Bryant and Hodge 1974] [Buenz et al. 1975] [Bundick 1990] [Burton and Bischoff 1976] [Chapman and Kirk 1974] [Chase] [Chase and McDonald 2014] [Chen and Valasek 1999] [Cho and Nagati 1998] [Cho et al. 1995] [Chowdhary and Jategaonkar 2006] [Chowdhary and Jategaonkar 2010] [Chudoba and Cook 2003] [Cicolani et al. 1999] [Compton et al. 1982] [Cook 1997] [Cook 2007] [Cook 2013] [Cooper 1990] [Crane et al. 1959] [Crassidis 2005] [Cumelles Céspedes] [Cummings and Schütte 2012] [Cunis et al. 2018] [Curry and Batterson 2000] [Dallery 1987] [Damveld 2004] [Daud Filho] [de Visser and Pool 2023] [Deckert et al. 1978] [Definitions of Aerodynamic Stability 1997] [Definitions of Aerodynamic Stability 2007] [Definitions of Aerodynamic Stability 2013] [Deiler 2016] [Development of a Continuous 2012] [Devesa et al. 2004] [Dias 2022] [Dias 2023] [Dias and Girardi 2016] [Doko and Sasongko 2026] [Donegan 1954] [Driscoll et al. 1975] [Duval 1981] [Dykes and Mavris 2016] [El-Kebir and Ornik 2020] [Emadian and Sajjadi 2026] [Ertugrul and Koyuncu 2023] [Estimation and Sensitivity 2026] [Morelli and Grauer 2023] [Eulrich and Rynaski 1980] [Farhat 1998] [Farhat 2000] [Farhat 2001] [Fegely et al. 2016] [Ferguson and Lo 2000] [Fischenberg 1995] [Freeman 1982] [Freeman 1980] [Freeman and Spencer 1980] [Fry and Sage 1974] [Garcia-Velo and Walker 1995] [Gates et al. 1996] [Ghoreyshi et al. 2016] [Ghosh and Raisinghani 2000] [Ghosh and Raisinghani 2002] [Ghosh et al. 2000] [Ghosh Roy and Peyada 2016] [Ghosh Roy and Peyada 2017] [Gillis and Chapman 1953] [Gilyard 1972] [Gilyard and Hill 1978] [Goege 2007] [Goel et al. 2021] [Grauer 2021] [Grauer and Boucher 2018] [Grauer and Morelli 2023] [Grauer and Morelli 2025] [Grauer et al. 2012] [Griffin 2006] [Gupta and Iliff 1982] [Göttlicher et al. 2016] [Hall et al. 1978] [Hamel and Jategaonkar 1996] [Harris et al. 2016] [Hartman 2019] [Hartmann et al. 1979] [Heck et al. 1983] [Heidersbach et al. 2024] [Helicopter Flight Parameter Identification 1987] [Higashino and Sakurai 2003] [Hildreth and Burton 1983] [Hodge and Audley 1983] [Hofmann et al. 2025] [Houbolt 1974] [Hua et al. 2013] [Hull and Roger 1975] [Hulshoff et al. 1996] [Hur and Valasek 2003] [Identification of Speed Brake 1994] [Ignatyev et al. 2019] [Iliff 1987] [Iliff and Maine 1982] [Iliff and Maine 1983] [Iliff and Powers 1969] [Iliff et al. 1981] [Iliff and Maine 1985] [Iliff and Taylor 1969] [Iliff et al. 1976] [Iliff and Wang 1997] [Ishimoto and Ishimoto 1997] [Ivler et al. 2019] [Jacklin 1986] [Grauer 2020a] [Grauer and Morelli 2024] [Grauer] [Grauer] [Grauer] [Jategaonkar 2000] [Jategaonkar 2005] [Jategaonkar and Plaetschke 1989] [Jategaonkar and Thielecke 1994] [Jategaonkar et al. 2004] [Jenkins 1989] [Jewell 1981] [Jianshuang Song et al. 2012] [Justin James Matt et al. 2025] [Karlgaard and Schoenenberger 2017] [Kim et al. 2003] [Kimathi and Lantos 2024] [Kirsten and Ash 1974] [Klausmeyer 2026] [Klein 1978] [Klein 1989a] [Klein 1989b] [Klein and Morelli 1992] [Klein 1983a] [Komendat and Crassidis 2012] [Kong 1994] [Kopsaftopoulos et al. 2015] [Korsun et al. 2017] [Korsun et al. 2024] [Korunov 2026] [Korunov et al. 2024] [Kotob and Kaufman 1974] [Kotob and Kaufman 1975] [Kukreja 2008a] [Kukreja and Bernstein 2012] [Kumar and Ghosh 2011] [Kumar and Ghosh 2017] [Kumar and Ghosh 2018b] [Kumar and Ghosh 2018a] [Kumar and Ghosh 2023b] [Kumar et al. 2008] [Kumar et al. 2013] [Kunwar and Chakraborty 2025] [Kunwar et al. 2026] [Mabius and Kaufman 1976] [Laban and Masui 1993] [Langham 1979] [Larsson 2019] [Larsson and Enqvist 2016] [Lee and Nagati 1999] [Lee and Yoon 2008] [Lensi 2000] [Leshikar and Valasek 2022] [Leung et al. 2019] [Levin 1981] [Lichota 2023] [Liff 1978] [Lim et al. 2000] [Limache and Cliff 1999] [Lin 1983] [Linse 1991] [Liu et al. 2026a] [Lo et al] [Lo et al. 2002] [Lo et al. 2003] [Lock et al. 2023] [Londono and Leonhardt 2012] [Long 1968] [Lu et al. 2017b] [Lu et al. 2018] [Lykins and Keshmiri 2010] [Mahzari et al. 2013] [Maine 1977] [Maine and Iliff 1979] [Maine and Iliff 1982] [Maine and Murray 1986] [Maine et al. 1990] [Maine and Iliff 1980] [Maine and Iliff 1986] [Malmuth et al. 1986] [Malmuth et al. 1987] [Mandal and Gu 2016] [Marchetti 1968] [Marwaha et al. 2008] [Masui 1997] [Maunder 1979] [McCracken and Jorris 2011] [McKillip 1988] [Mehra and Tyler 1973] [Mehra et al. 1974] [Metodiev 2024] [Minnema et al. 2019] [Moes and Iliff 2002] [Moes et al. 2000] [Mohamed and Dongare 2018] [Mohamed and Dongare 2021a] [Mohamed and Dongare 2021b] [Mohamed and Dongare 2021c] [Mohamed and Dongare 2021d] [Mohamed and Dongare 2021e] [Mohr 1975] [Molloy and Ford 2014] [Molusis and Briczinski 1974] [Morelli 1998] [Morelli 2000b] [Morelli 2002] [Morelli 2006] [Morelli 2010] [Morelli 1993] [Morelli 2000a] [Morelli and Grauer 2018] [Moszczynski and Grant 2017] [Mulder 1988] [Murphy and Klein 2008] [Murphy and Klein 2010] [Murphy et al. 2011] [Murphy 1996] [Murzionak] [Napolitano et al. 1994] [Napolitano et al. 2001a] [Napolitano et al. 2001b] [Nguyen and Xiong 2022a] [Nguyen and Xiong 2023a] [Nguyen and Xiong 2024a] [Nguyen and Xiong 2024b] [Nguyen et al. 2016] [Nguyen and Xiong] [Nicolosi et al. 2010] [Nissim and Gilyard 1989] [O’Donnell and Mohseni 2018] [Oelker and Friehmelt 1998] [Ozger 2013] [Parameter Estimation Techniques 1974] [Park 1977] [Park et al. 2001] [Patel et al. 2023] [Murphy 1999] [Pearson 1995] [Pei and Wall 2013] [Perry et al. 2019] [Perry et al. 2023] [Peyada and Ghosh 2009] [Pfifer and Danowsky 2016] [Phillips] [Pinkelman et al. 1995] [Pinkelman et al. 1996] [Plaetschke and Weiss 1988] [McKown et al] [Quaranta and Dimino 2007] [Queijo et al. 1979] [Quitter et al. 2021] [Dhayalan et al. 2018] [Raab 2014] [Raghavan and Ananthkrishnan 2005] [Raisinghani and Adak 1983] [Raisinghani and Ghosh 2002] [Raisinghani and Kumar 1995] [Raisinghani et al. 1999] [Ram Prabhu et al. 2021] [Ramachandran and Wells 1974] [Raol and Jategaonkar 1995] [Raol and Singh 2023b] [Rasmussen 1995] [Ravetta et al. 2024] [Rediess 1974] [Reid et al. 1997] [Reiner 1996] [Remple and Tischler 2006] [Roeser and Mönnich 2024] [Rogers 2002a] [Roudbari and Saghafi 2014] [Roy and Peyada 2019] [Roy and Walker 1985] [Russo et al. 1983] [Rynaski et al. 1978] [Saderla et al. 2017] [Saito et al. 2014] [Samardžić et al. 2013] [Saraswathi 2000] [Sarigul-Klijn et al. 2008] [Sarkar and Panneerselvam 1998] [Sarkar et al. 2009] [Sarojini et al. 2022] [Schkolnik et al. 1995] [Schkolnik 1993] [Schwanz and Grimes 1980] [Seanor] [Shafer 1980] [Shafer 1984] [Shepard et al. 1981] [Shin et al. 2006] [Silhouette and Stengel 1987] [Silva 2011] [Simmons 2022] [Simmons 2023b] [Simmons and Ackerman 2026] [Simmons and Murphy 2021] [Simmons et al. 2025a] [Simsek and Tekinalp 2015] [Singh and Ghosh 2006] [Singh and Ghosh 2007] [Singh and Ghosh 2013] [Singh and Ghosh 2023] [Singh et al. 2005] [Smith et al. 2003] [Smith 1975] [Sneshko et al. 2005] [Snyder 1947a] [Sorensen et al. 1972] [Sorensen et al. 2025] [Sorensen 1972] [Sorensen et al. 1975] [Stalford 1979] [Steers and Iliff 1975] [Stengel 1983] [Stepner and Sorensen 1974] [Taflan et al. 2026] [Tai et al. 2023] [Tang and Shi 2005] [Tang et al. 2006] [Tang et al. 2001] [Taniguchi 1972] [Taylor 2012] [Taylor and Ratnayake 2011] [The Transformation of Aerodynamic 1997] [The Transformation of Aerodynamic 2007] [Tischler 1991] [Tischler 2018] [Tischler and Remple 2012] [Tischler and Tomashofski 1999] [Tischler 1988] [Tischler 1989] [Tischler 1990] [Tischler 1995] [Tomaine et al. 1978] [Aagren et al. 2025] [Tran and Lind 2010] [Trankle and Bachner 1993] [Trankle and Rabin 1983] [Transformation of Aerodynamic Stability 2013] [Travassos and Kaufman 1979] [Trittler et al. 2008] [Tusharika 2015] [Ueno et al. 2004] [Unstable Aircraft Identification 2006] [Unstable Aircraft Identification 2015] [Verma and Peyada 2018] [Verma and Peyada 2020] [Vincent and Franklin 1981] [Taylor 1982] [Wang 2024a] [Wang et al. 2022b] [Wang et al. 2022a] [Wang et al. 1986] [Wang et al. 2013] [Wang et al. 2015] [Waszak and Fung 1996] [Weil 1981] [Wells and Klein 1982] [Wells et al. 1979] [Wells et al. 1981] [Wells et al. 1982] [Wickersheim et al. 2025] [Winston] [Wislicenus and Daidzic 2022] [Wu 2014] [Xie et al. 2012] [Xu et al. 2019b] [Yang et al. 2014b] [Youmin Zhang et al] [Zanette and Almeida 2015] [Zeng et al. 2010] [Zeng et al. 2012] [Zhao et al. 2022] [Özger 2012]

Stability, control and handling qualities

The airframe’s dynamics and the pilot’s view of them. Static and dynamic stability, flying and handling qualities, flight control systems, spin and departure, roll and inertia coupling, high angle of attack and in-flight simulation.

377 records. [Adelgren et al. 2004] [Adolph 1978] [Aerodynamic Control Forces 2001] [Air Force Flight Test Center Edwards AFB CA 1974a] [Air Force Flight Test Center Edwards AFB CA 1974b] [Air Force Flight Test Center Edwards AFB CA 2002] [Air Force Test Pilot School Edwards Afb Ca 1962c] [Air Force Test Pilot School Edwards Afb Ca 1969] [Air Force Test Pilot School Edwards Afb Ca 1988a] [Air Force Test Pilot School Edwards Afb Ca 1988c] [Air Force Test Pilot School Edwards Afb Ca 1988b] [Air Force Test Pilot School Edwards Afb Ca 1989] [Air Force Test Pilot School Edwards Afb Ca 1990a] [Air Force Test Pilot School Edwards Afb Ca 1991b] [Aircraft Dynamic Stability 2003] [Aircraft Dynamic Stability 2014] [Aircraft Flight Control 2014] [Aircraft Flight Control Actuation] [Aircraft Flight Control Systems] [Aircraft Lateral-Directional Handling Qualities 2011] [Aircraft Longitudinal Handling Qualities 2011] [Aircraft Stability and Control 2003] [Aircraft Stability and Control 2014] [Aircraft Stability and Control 2026] [Aircraft Static Stability 2003] [Aircraft Static Stability 2014] [Airplane Spin Testing 2003] [Akaryildiz et al. 2025] [Alag and Duke 1985] [Alexander 1979] [Anderson and Innis 1965] [Andrews et al. 1956] [Antcliff and McGowan 2000] [Application of dynamic flight] [Army Aviation School Fort Rucker Al 1961] [Ashkenas 1984] [Assadourian and Reeder 1948] [Bachelder and Aponso 2020a] [Bachelder and Aponso 2020b] [Bachelder et al. 2020] [Bailey et al. 1987] [Ballouz and Chang] [Banerjee 2019] [Barret and Barret 1997] [Bartolome Calvo and Eggers 2011] [Batterson and Klein 1987] [Batterson and Klein 1989] [Baughman and Longeauay 2015] [Bazill and Jenney 1970] [Beasley 1984] [Beaufrere 1988] [Simmons et al] [Bennett 1945] [Berra et al. 2017] [Berry et al. 1976] [Bezdek and Galloway 1982] [Bian et al. 2019] [Bigler 1986] [Bihrle 1970] [Bingaman 2012] [Blake and Lunn 1980] [Bosworth 2008] [Boudreau 1976] [Bowman 1965] [Brian Trubshaw 2006] [Bronder et al. 2012] [Brown et al. 2007] [Brown 2009a] [Brown 2009b] [Budd et al. 1995] [Budd et al. 1993] [Bunge et al. 2015] [Burcham et al. 1992] [Burken 1992] [Burken 1993] [Butter et al. 1996] [Carlson et al. 1965] [Carter and Stephenson 1999] [Carter 1997] [Chen and Shi 2011] [Chetty and Raol 1992] [Chevalier et al. 1974] [Miller] [Clement et al. 1984] [Cliett 1952] [Cole et al. 2007] [Colgren 1996] [Combined Flight Control/utility System 1974] [Control Allocation and Flight 2016] [Cotton 1974] [Cunningham et al. 2018] [Cunningham 1984] [Hanson et al. 2002] [Damman 1976] [Davidson et al. 2003] [de Syon 2000] [Deckert 1981] [DelFrate 2007] [Demarchi and Haning 1978] [Design Objectives for Flying] [Design Objectives For Handling] [Dhiman et al. 2022] [Don and Grabner 2022] [Donegan and Pearson 1952] [Dryden 1936] [Du and Zhang 2020] [Duke 1983] [Duke and Jones 1984] [Duke et al. 1986] [Dynamic Lateral-Directional Stability Theory 2003] [Dynamic Longitudinal Stability Flight 2003] [Dynamic Stability and Control] [Edwards and Wingrove 1969] [Eney 1967] [Eney 1969] [Enns 2003] [Fan and Hall 2014] [Feedback Flight Control 2026] [Feng et al. 2023] [Field et al. 2002] [Flight Control 2015] [Казак 2000] [Flight Control System Design 2011] [Flight Control System 1999] [Flight Control System 1977] [Flight Control Systems 2022] [Flight Sciences Lab INC Buffalo NY 1964] [Ford 1989] [Fosdick 1970] [Fresconi et al. 2017] [Gainer 1963] [Gallagher 1971] [Gao et al. 2021i] [Gao et al. 2021a] [Gao et al. 2021b] [Gao et al. 2021c] [Gao et al. 2021d] [Gao et al. 2021e] [Gao et al. 2021g] [Gao et al. 2021h] [Gelzer and Peebles 2015] [Generally on automatic flight] [Gera et al. 1981] [Gera and Bosworth 1987] [Gerlach 1967] [Gertsen and Shomber 1965] [Glaser and Strovers 2011] [Gleason et al. 1996] [Gomez et al. 2020] [Goodman and Conigliaro 1986] [Grantham and Williams 1987] [Grantham et al. 1985b] [Gray 1964] [Gregory et al. 2011] [Gregory et al. 2010] [Ground and Flight Testing 2000] [Guo et al. 2017] [Gupta] [Ha 1990] [Hanson 2012] [Hanson 2014] [Harris et al. 2000] [Hassan and Taha 2016] [Hess 1981] [Hess 1984] [Hess 1986b] [Hess and Hess 1997] [Hjartarson et al. 2015] [Hodges and McKenzie 1975] [Hoh and Mitchell 2018] [Horak and Renze 2016] [Horowitz et al. 1980] [Iliff et al. 1978b] [Initial Flight Test 1989] [Integrated Flight Instruments and] [Introduction to Stability 2003] [Ishimoto et al. 1996] [Jacobson 2015] [Grauer] [Jarvis 1966] [Jarvis 1967] [Jeffrie and Rolston 1972] [Jenney et al. 1982] [Jex et al. 1987] [Johnson 1975] [Jung et al. 2014] [Kakojima and Akinaga 2005] [Kass 1970] [Swaim 1969] [Wichman et al. 1996] [Kelly 1988] [Kidd 1988] [Kiefer and Calvert 1992] [Kilmer and Sklaroff 1973] [Kim 1995] [Kim and Kunz 2016] [Kim et al. 2018a] [Klein and Batterson 1983] [Klyde et al. 2003] [Knotts and Parrag 1983] [Koehler and Buchacker 1986] [Kogler and Quam 1983] [Kohnhorst and Magnacca 1980] [Konar et al. 1974] [Kopecki 2016] [Kriechbaum and Stineman 1971] [Krumenacker and Pellicano 1992] [Kryvokhatko and Masko 2018] [Kurnaz et al] [Langford et al. 1990] [Larson et al. 1983] [Larsson 2025] [Lateral-Directional Stability Theory 2003] [Layton 1974] [Lee 1977] [Li and Chen 2003] [Lin et al. 2008] [Linear Quadratic Flight Control 2026] [Liu et al. 2021b] [Longitudinal and Lateral Linear 2014] [Longitudinal Control and Trim 2003] [Loschke et al. 1972] [Loschke et al. 1974] [Loth et al. 1974] [Nguyen et al. 1980b] [Luo et al. 2026b] [MacDonald and Shepherd 2008] [Mahale and Ananthkrishnan 2006] [Malaek et al. 2006] [Malcolm and Skow 1986] [Malcom and Husband 1976] [Maria-Agneta and Stef 2011] [McKenzie 1973] [McLaughlin et al. 1993] [McMaster and Schenk 1973] [McMaster and Schenk 1974] [McNeill 1968] [Mendenhall and Perkins 1996] [Menon et al. 1986] [Menon and Walker 1988] [Menon et al. 1985] [Miller 1991] [Miller and Goodrick 2017] [Montgomery and Caglayan 1974] [Montgomery et al. 1978] [Mooij 1973] [Moua 2010] [Muzzey and Kidd 1959] [Myschik et al. 2022] [Nae et al. 2022] [Nettleton 1965] [Nguyen and Cord 1999] [Nguyen 1979] [Nguyen et al. 1979] [Nial 1972] [Nickerson et al. 1991] [Northrop Aircraft INC Hawthorne CA 1952] [Ochi 2004] [Ogburn et al. 2005] [Ogren et al. 1974] [Orlik-Ruckemann 1982] [Padua and Preisighe Viana 2025] [Pahle et al. 1991] [Papa and Stoliker 1988] [Pavlock et al. 2011] [Peng et al. 2021] [Phillips 1948] [Phillips 1942] [Pierson and Unger 1982] [Placement in Flight Control 2026] [Prosvirin and Kharchenko 2016] [Pursel 1977] [Rand 2014] [Raol and Singh 2023a] [Ratvasky and Ranaudo 1993] [Reed 1997] [Regenie et al. 1992] [Rehman et al. 2009] [Research and Design 2022] [Rhoads 1967] [Rickard 1978] [Roberts and Brown 1988] [Rogalski 2018] [Rogalski et al. 2020] [Rom 1992] [Sachs and Moravszki 2002] [Sadoff 1958] [Sarigul-Klijn and Huber 2006] [Sarrafian and Powers 1985] [Scherz and Tucker 1985] [Schierbrock and Takahashi 2021] [Schmidt and Jusko 2025] [Schmidt and Jusko 2026] [Schumacher 1952] [Schwanz 1972] [Seiferth et al. 2018] [Sexton 1964] [Shafer and Steinmetz 2001] [Shao et al. 2026] [Sharpes and Carroll 1973] [Shen et al. 2016] [Shen et al. 2021] [Shi 2004] [Shmul et al. 2018] [Shuping Tan and Zhibin Li 2010] [Shweyk and Hyde 2013] [Simon 2014] [Simon and Savage 1975a] [Sims and Kimberlin 1995] [Sitz et al. 1997] [Smith 1977] [Smith 1991] [Smith and Smith 1997] [Smith et al. 1971] [Smith et al. 1973] [Soares 2007a] [Soares 2007b] [Soule and Wheatley 1934] [Spahr 1947] [Sragow 2013] [Stability and Control 2009] [Static Flight Stability 2026] [Static Longitudinal Stability Flight 2003] [Static Stability and Control] [Static Stability and Control 1998] [Stolarik 2007] [Stoliker and Carter 2003] [Stough et al. 1987] [Sullivan and Finberg 1989] [Taylor and Klein 1981] [Taylor and Day 1961] [Teofilatto 2001] [Terrell and Zein-Sabatto 2017] [Test Techniques for Flight 2021] [Thompson and Eitenmiller 1983] [Thornton 1994] [Torres 2017] [Turner and Cooper 1947] [Uribe Quintero et al. 2024] [Urnes and Yeager 1991] [Valasek 1996] [Valasek and Dorsett 2001] [Valasek and Valasek 1997] [Van Bavel 2014] [van der Maas 1959] [Van Doren 1955] [Van Gool and Weingarten 1981] [Varshneya] [Vepa 2023a] [Vepa 2023b] [Vogeley 1966] [Vomaske et al. 1978] [Vomaske et al. 1961] [Walchner 1974] [Walker 1985] [Wardana et al. 2021] [Weil and Spear 1947] [Weingarten and Chalk 1982] [Weinstein et al. 1986] [Whalley et al. 2001] [Whitbeck et al. 1982] [Wichgers] [Wooldridge 2003] [Wu and Liu 2021] [Yan and Fu 2026] [Yang] [Yao et al. 2025] [Yechout and Oelschlaeger 1976] [Yokoyama and Fujiwara 2021] [Yu and Zhang 2015] [Zalesak 1981] [Zhang et al. 2013] [Zhang et al. 2025d] [Zhi Chaoyou et al. 2007] [Zhiming et al. 2025] [Zhong and Félix 2015] [Zhou et al. 2007]

Aerodynamic heating, entry and thermal protection

The thermal keystone. Aerodynamic and stagnation-point heating, atmospheric and planetary entry, ablators and thermal protection systems, and heating measured in flight, from the blunt-body relations of the 1950s to the entry instrumentation of the Mars landers.

337 records. [A Study 1980] [Abe et al. 2001] [Acheson and Rothnie 2009] [Fletcher 1978] [Aerothermodynamic Assessment of Corrugated 1979] [Aerothermodynamic Base Heating 1978] [Aerothermodynamic Entry Environment 1983] [Aerothermodynamic Environment for Jovian 1979] [Akin 2010] [Alexander 1970] [Allen and Eggers 1958] [Allen 1957] [Allen and Eggers 1957] [Analysis of Jupiter Probe 1979] [Anderson and Kinzel 2023] [Approximate Inviscid Radiating Flowfield 1979] [Arora and Ananthasayanam 2003] [Assessment of Alternate Thermal 1983] [Assessment of Key Aerothermal 1992] [Asymmetric Nose-Tip Shape Change 1978] [Atmospheric Entry Probes 2007] [Atmospheric Re-Entry Vehicle Mechanics 2007] [Auweter-Kurtz 2002] [Babineaux 1966] [Bassett et al. 2018] [Belov et al. 2016] [Bender 1969] [Berger et al. 2015] [Bevacqoa et al. 2004] [Blanchard et al. 2001b] [Blanchard et al. 2001a] [Bland et al. 1958] [Bland and Collie 1961] [Bond et al. 1958] [Bonin et al. 2017] [Brandis and Cruden 2017] [Brandis et al. 2012] [Mobley and Summers] [Mobley and Summers] [Brazel et al. 1965] [Brewer and Brant 1980] [Bulmer 1974] [Bulmer 1975] [Buss and Nicholson 1971] [Calhoun 2000] [Caruso and Naegeli 1976a] [Caruso and Naegeli 1976b] [Chai et al. 2017] [Chapman 1958] [Chapman and Rubesin 1949] [Chauvin et al. 1968] [Chew] [Chou and Smith 1974] [Karlgaard et al] [Chung and Goodwin 1962] [Clark 1970] [Computational and Experimental Study 1993] [Cooke and Engle 2016] [Costa et al. 2000] [Couch and Morris 1968] [Crain et al. 1989] [Cruz and Engelund 1991] [Cunningham and Haney 1983] [Dana 1968] [Dasgupta et al. 2012] [Davidson and Dalby 1961] [Dec and Braun 2006] [Dec and Mitcheltree 2002] [Dejarnette et al. 1985] [Derienzo and Pallone 1967] [Design Considerations 1963] [Determination of Thermal Performance 1966] [DiFranco 1971] [Dillman et al. 2013] [Dinonno et al. 2016] [Dolan 1970] [Dong et al. 2023a] [Drakin 1963] [Duberg 1957] [Eckert 1956] [Edwards et al. 2024] [Edwards and Cole 1983] [Effects of Aerodynamic Heating 1980] [Effects of Atmospheric Structure 1979] [Eggers and Swenson 1966] [Eggers and Swenson 1967] [Olstad 1980] [Ericsson 1969] [Esch] [Evans et al. 1970] [Experimental Studies of Radiative 1980] [External Tank Laminar 1980] [McNichols] [Fahy et al. 2021] [Fay and Riddell 1958] [Fay et al. 1991] [Fields et al. 1972] [Fischer 2008] [Fisher 1970] [Flanagan 1993] [Flight Measurements of Tile 1983] [Florence and Hiltz 1968] [Florence et al. 1978] [Foster et al. 1985] [Fujii and Inoue 1998b] [Fujii and Inoue 1998a] [Fujii et al. 2000] [Fujii et al. 2001] [Galileo Probe Forebody Thermal 1982] [Gally and Carlson 1993] [Garcia-Llama 2007] [Garg and Dodiyal 2009] [Genaro and Pessoa Filho 2006] [Gilbert] [Gion 1976] [Goodman and Ireland 2006] [Goodman and Ireland 2007] [Goulard 1961] [Grabowsky et al. 1981] [Greene et al. 2001] [Gu 2026a] [Gu 2026b] [Guoling and Ji 2014] [Gupta and Simmonds 1988] [Guy] [Hall and Nowlan 1977] [Hamilton et al. 1991] [Hamilton and Weilmuenster 1986] [Alpert] [Heat-Shield Material Tests 1980] [Wilson 1964] [Hertzler and Phillips 1983] [High-Speed Flight Thermal Management 1996] [Hilton 2012] [Hirschel and Weiland 2009a] [Hodge et al. 1981] [Hoey 1983] [Holguin and Kostyk 2010a] [Hollis et al. 2017] [Horing et al. 2025] [Horstman and Kussoy 1967] [Horton and Babineaux 1967] [Horvath et al. 2010] [Hough 1981] [Huber 1966] [Ishimoto 1995] [Jacobson 2005] [Janardanan and Jayakumar 2006] [Jenke 1979] [Jianguo et al. 2016] [Jo et al. 2020] [Jones 1964] [Jupiter Probe Heat-Shield Configuration 1979] [Karlgaard et al. 2022] [Kemp 1960] [Kirk and Miller 1962] [Kivel 1961] [Ko and Fields 1987] [Koike et al. 2018] [Kostyk 2008] [Kowal 2011] [Matsuno et al] [Matsuno et al. 2024] [Kumar Sulur Loganathan 2023] [Lacoste et al. 1995] [Lee and Kim 2021b] [Lee and Goodrich 1972] [Lee and Swanson 1958] [Lees 1956] [Lennon and Poirter 1974] [Liaoni Wu et al. 2008] [Line-by-Line Transport Calculations 1980] [Liu et al. 2002] [Livingston and Williard 1969] [Livingston and Williard 1971] [Longo 2008] [Lu 2005] [Lugo et al. 2014] [Ma 1992] [Maneuvering Re-Entry Vehicles 1993] [Mehta et al] [Maples 1979] [Martin and Panesi 2022] [Masek et al. 1973] [Mastropietro et al. 2015] [Mathavaraj and Padhi 2020] [Mathavaraj et al. 2010] [McGary and Li 1989] [McQuellin et al. 2020] [Methods for Predicting off-Stagnation-Point 1980] [Methods for Predicting Radiation-Coupled 1978] [Meyer 1938] [Mason et al] [Mitchel 1971] [Molina et al. 1996] [Molina et al. 2005] [Mooij 2024] [Moss et al. 1988] [Mullenix et al. 2008] [Mundt et al. 2005] [Mungiguerra 2023] [Neely and Tjong 2008] [Negaard 1979] [Nelson 1983] [Nicolet et al. 1974] [Nomura et al. 2018] [Nonequilibrium Viscous Flow 1980] [Numerical Calculation of Gaseous 1982] [Ohtake 1998] [Oishi et al. 2006] [Olivier 1995] [Oruganti et al. 2024] [Viskanta 1979] [Park 2005] [Park 2007] [Perez] [Perez-Rivera 2026] [Pitts and Murbach 1982] [Platus 1980] [Polutchko 1974] [Praharaj et al. 1986a] [Praharaj et al. 1986c] [Praharaj et al. 1986b] [Prajapati 2026] [Preliminary Design 1983] [Protz and Nettles 2015] [Putnam and Braun 2016] [Quinn and Gong 1990] [Quinn and Gong 2000] [Rafla 2019] [Rand 1963] [Re-Entry Heating 1988] [Re-Entry Trajectory with Diveline 1993] [Re-Entry Vehicle Particle Mechanics 1993] [Reba 1964] [Reba and Christian 1963] [Reding and Svendsen 1988] [Reilly 1964] [Reimer et al. 2023] [Rempt 1981] [Response of Heat-Shield Materials 1979] [Riccio et al. 2017] [Riley and Dejarnette 1992] [Rostkowski and Panesi 2022] [Rosłowicz and Bednarczyk 2017] [Sabin 1973] [Sabin 1975] [Sambamurthi et al. 1989] [Santos et al. 2011] [Saturn V Aerothermodynamics Flight 1969] [Savage and Tinling 1959] [Scala and Nolan 1960] [Schmitz and Tashakkor 2011] [Scigliano et al. 2018] [Berry 1967] [Scott et al. 1977] [Sebastian 1966] [Sepka and Samareh 2015] [Shih 1976] [Shih et al. 1988] [Shtessel and Krupp] [Shuttle Eleven Cove Aerodynamic 1978] [Sieker 1966] [Siemers et al. 1983] [Simeonides 2006] [Simons 1975] [Skolnik and Putnam 2022] [Smith et al. 1972] [Solid Rocket Motor Plume 1979] [South 1974] [Space Shuttle Laminar Heating 1982] [Spearman 1985b] [Spiegel et al. 1968] [Stephens 1959] [Stokes and Lombaerts 2023] [Stoney and Swanson 1957] [Strauss 1974] [Survey of the Supporting 1982] [Sutton and Graves 1971] [Sutton et al. 1978] [Swanson 1958] [Swanson and Rumsey 1956] [Takahashi et al. 2013] [Takahashi et al. 2015] [Takahashi et al. 2019a] [Tashakkor et al. 2011] [Tauber 1968] [Tauber 1989] [Tava and Suzuki 2001] [Teramoto et al. 1998] [Test Method for Calculation] [Tewell 1984] [The Effect of Surface 1981] [Thermal Design 1974] [Thermal Protection 2015] [Thermal Protection System Conception 2013] [Thermal Protection System 1981] [Thornton 1992] [Throckmorton 1981] [Throckmorton 1982] [Throckmorton and Hartung 1984a] [Tile-Gap Flow 1983] [Ting et al. 1986] [Ting et al. 1988] [White et al. 2022b] [Trends in Unmanned Planetary 1982] [Truitt 1968] [Trujillo et al. 1983] [Turbeville et al. 2024] [Turner et al. 2006] [Van Fossen and Dewitt 1988] [Vekinis and Xanthopoulou 2010] [Vigil and Pérez 2026] [Viotto et al. 2012] [Wang et al. 2016b] [Weiland and Hirschel 2009] [Wells 1989b] [White et al. 2013] [Whitnah 1967] [Wing 1972] [Wing 1973] [Woeste 1992] [Wolf et al. 1988] [Wong et al. 1960] [Wright 2019] [Wright et al. 2011] [Wu et al. 2014] [Wurster and Stone 1993] [Xu and Lan 2018] [Xu and Tang 2010] [Ahmed et al. 2011] [Yee et al. 1961] [Young 1982] [Zhang and Chen 2011] [Zhao 2021a] [Zheng et al. 2015] [Zoby et al. 1993]

Sonic boom and the supersonic transport

The X-59’s subject and its history. Sonic boom generation, propagation, measurement and minimisation, the human, structural and legal response to it, and the supersonic transport programmes it constrained. 63 titles name a low or shaped boom, the regulatory number the review above describes the X-59 as built to produce.

292 records. [A Study to Determine 1975] [Elmiligui et al. 2022] [Elmiligui et al] [Elmiligui et al] [Carr et al] [Carr et al] [Altman 1965] [Altree and Baxter 1968] [Ferri 1971a] [ao 2026] [Ardema and Windhorst 1998] [Aronstein and Schueler 2004] [Atkinson 1964] [Babcock and Salamone 2006] [Bahm and Haering 1995] [Bahm and Haering 1996] [Baize 1996] [balazard 1972] [Baudoin 2006] [Bisplinghoff 1964] [Boeing Co Renton Wa Airplane Div 1964] [Bray 1963] [Brown and Haglund 1988] [Burn and Plotkin 1989] [Byrne 1971] [Callaghan 1968] [Campbell et al. 2015] [Capone and Deere 2001] [Carlson 1965] [Carlson 1970] [Carlson et al. 1971] [Carlson 1964b] [Carlson and Jackson 1966] [Carpenter and Cizmas 2020] [Carpenter et al. 2025] [Carr 2021] [Castner 2010a] [Castner 2011] [Champagne 1991] [Chattopadhyay et al. 1995b] [Chaudhari and Takahashi 2022] [Cliatt et al. 2014] [Clodman 1968] [Colonno and Alonso 2010] [Conners and Wayman 2011] [Coulouvrat 1998] [Coulouvrat 2022] [Crow and Bergmeier 1996] [Darden 1976] [Darden 1999] [Davis 1972] [Davis 2017] [Demiroglu and Nikbay 2023] [Demiroglu et al. 2021] [Dickinson 1964] [Dixon and Hunsaker 2023] [Doebler et al. 2018] [Downing and Zamot 1995] [Downing 1992] [Downs 2021] [Dragna 2021] [Driver 1974] [Dubin 1978] [Durston et al. 2011] [Durston et al. 2014] [Eggert et al. 2024] [Ehernberger et al. 1994] [Elmer et al. 2013] [Elmer and Joshi 1994] [Waggoner et al. 2020] [Escher and Brewer 1974] [Fairbairn 1964] [Fasulo et al. 2025] [Ferri and Schwartz 1972] [Ferri et al. 1973] [Ferri 1971b] [Fidell et al. 1989] [Fleming 2014] [Fouladi 1993] [Fouladi 1999] [Fox 1964] [Foxworth 1968] [Garretson 2012] [Garrick 1968] [Graham et al. 2005] [Graziani et al. 2024] [Greatrex 1963] [Greene 1964] [Hayes 1969] [Haber 1993] [Hadaller et al. 1980] [Haefeli 1969] [Haering et al. 2013] [Haering et al. 1995] [Haering and Murray 2004] [Haglund 1991] [Haglund and Kane 1974a] [Haglund and Kane 1974b] [Haglund and Kane 1973] [Hao et al. 2016b] [Harris 1967] [Hartwich et al. 2003] [Heath et al. 2016] [Heath et al. 2017] [Henderson et al. 1971] [Heppe and Hong 1964] [Herron 2007] [Higgins and Shomber 1964] [Hilton and Maglieri 1965] [Hines 1977] [Hines and Sabatella 1973] [Hodgdon and Page 2013] [Holmes 1966] [Horonjeff 1962] [Howe 2002] [Hubbard 1969] [Hutchinson 1963] [Inagaki et al. 1998] [Schwartz 1968] [Schwartz 1971] [Ishikawa et al. 2019] [Ivanteeva et al. 1998] [Ivanteyeva et al. 2002] [Page and Loubeau 2019] [John] [Vanharen et al] [Page et al. 2020] [Jäschke 2021] [Jäschke and Liebhardt 2021] [Jäschke et al. 2024] [Kamali and Pierce 1972] [Kamerman et al. 1986] [Kanamori et al. 2017] [Kanamori et al. 2018] [Kanamori et al. 2025] [Kandil et al. 2006] [Kane 1973] [Kantor and Cliatt 2017] [Kelly 1964] [Gee et al. 2020] [Knight 1961] [Knight 2022] [Koegler 1966] [Korunov 2025] [Kramer et al. 2018] [Kroo 1990] [Kryter 1969] [Kubota 2003] [Lazzara et al. 2019] [Lazzara et al. 2020] [Lazzara et al. 2021] [Lee and Downing 1993] [Lee and Downing 1996a] [Lee and Downing 1996b] [Lengyan and Zhansen 2015] [Li 2015] [Li and Geiselhart 2021] [Li and Geiselhart 2023] [Li and Geiselhart 2024] [Li et al. 1995] [Liebhardt 2019] [Liebhardt 2021] [Liebhardt et al. 2013] [Liebhardt et al. 2014] [Liebhardt et al. 2020] [Liebhardt et al. 2022] [Lipkens 1995] [Lipkens 2002] [Lonzaga 2021] [Lovell 1999] [Lovholt 2021] [Luquet] [Mabe et al. 2023] [Mack and Darden 1979] [Maglieri 1967] [Maglieri and Plotkin 1991] [Maglieri et al. 2011b] [Maglieri et al. 2011a] [Magruder 1964] [Makarewicz 2024] [Makino et al. 1997] [Marmel 2021] [McDonald 1966] [Michel 1987] [Morgenstern 1998] [Morgenstern 2012c] [Morgenstern 2013] [Morgenstern 2017] [Morgenstern et al. 2005] [Morgenstern 1999] [Moua et al. 2008] [Murakami 2006] [Mutz et al. 1964] [Niedzwiecki and Ribner 1977] [Norris et al. 1995] [Norris et al. 1996] [Norén-Cosgriff et al. 2022] [Nozzle Plume Effects 2013] [Ordaz and Li 2016] [Ordaz et al. 2014] [Ordaz et al. 2015a] [Ordaz et al. 2015b] [Page 1975] [Page 2017] [Palmer and Sparrow 2015] [Paradiso 1961] [Park and Carter 2021] [Park and Carter 2022] [Pawlak 1968] [Phillips and West 2017] [Phillips and West 2019] [Plotkin 1989] [Plotkin 1990] [Plotkin 2006] [Plotkin and Cantril 1976] [Plotkin et al. 2005] [Radiobiological Aspects 1966] [Rallabhandi 2011] [Rallabhandi 2014] [Rallabhandi 2022] [Rallabhandi and Loubeau 2017] [Rallabhandi et al. 2012] [Report on Human Response 1968] [Report on Physical Effects 1968] [Resler 1969] [Rivers and Wahls 2003] [Rivers et al. 2008] [Salah El Din et al. 2013] [Salamone 2006] [Salvetti and Seidman 1988] [Scarselli and Marulo 2010] [Schaefer et al. 2023b] [Schreckenberg 2021] [Seebass 1973] [Seebass 1994] [Seebass 1997] [Seebass and Argrow 1998] [Seebass and George 1973] [Seebass 1968] [Seebass 1969] [Lympany and Page] [Shields and Li 2011] [Shuttle Sonic Boom 1973] [Shuttle Sonic Boom 1975] [Siclari and Darden 1991] [Smith-Velazquez and Theunissen 2018] [Sonic Boom 2012] [Sonic Boom Analysis 1975] [Southerland et al. 1986] [Sparrow 2010] [Rallabhandi] [Stansbery et al. 1999] [Stauffer 1964] [Steinmetz and Hines 1987] [Stratford 1973b] [Studies of Sonic Boom 1965] [Supersonic Transport Wing Minimum 1992] [Swihart 1967] [Sóbester 2010] [Taylor 1968] [Technical Applications 1976] [The Anglo-French Supersonic Transport 1962] [The Post-War Sonic Boom 2013] [Thomas 1971] [Thompson and Parnell 1967] [Tice and Martin 1992] [Ting 1978] [Tokuyama et al. 1993] [Turbojet and Turbofan Engines 1964] [Tuttle 1980] [Ueno and Makino 2021] [Ueno et al. 2023] [Utomo and Bura 2019] [Utsumi and Obayashi 2010] [Velden 1997] [Veresnikov et al. 2024] [Waggoner et al. 2018] [Warren 1972a] [Warren 1972b] [Weber 1975] [Whitlow and Harris 1976] [Why Supersonic Transport? 1967] [Williamson 1963] [Willshire et al. 1992] [Windhorst and Ardema 2000] [Wintzer and Castner 2015] [Wintzer and Kroo 2012] [Wintzer and Ordaz 2015] [Xiao et al. 2026] [Yamazaki and Ishida 2025] [Yuldashev 2021] [Zha et al. 2010]

Boundary-layer transition and laminar flow

The question the X-series opened and did not close. Hypersonic boundary-layer transition and its prediction, laminar flow control and natural laminar flow in flight, receptivity and transition flight experiments. 126 of its titles name hypersonic flow and 83 laminar flow, so the hypersonic problem the review calls the largest source of uncertainty in hypersonic sizing is also the larger part of the literature.

279 records. [Active Wave Control 1990] [Ahmed et al. 1989] [Allison and Dagenhart 1987] [Bouslog et al. 1991] [Chou and Marineau 2024] [Chou et al] [André et al. 2015] [Gardner et al] [Atkin 2004] [Atkin 2008] [Atkin et al. 2006] [Axten and Maughmer 2023] [Balakumar and Chou 2016] [Banks et al. 2012a] [Banks 2008] [Banks et al. 2011] [Banks et al. 2012b] [Banner et al. 1958] [Barry et al. 1994] [Bartkowicz et al. 2009] [Befus et al. 1987] [Belisle et al. 2010] [Belisle et al. 2012] [Bender et al. 2010] [Berger et al. 2010] [Berger et al. 2011] [Berkowitz et al. 1977] [Berry et al. 2011] [Berry et al. 2006a] [Berry et al. 2006b] [Berry et al. 2008b] [Berry et al. 2010] [Bertelrud et al. 1992] [Bertelrud et al. 1999] [Bertelrud et al. 2000] [Berton et al. 2014] [Bi et al. 2007] [Blanchard et al. 1996] [Boudreau 1978] [Bragg and Gregorek 1989] [Hiller et al] [Brinza 2024] [Holmes and Gall 1988] [Bueche 1966] [Bui 2013] [Bushnell 1992] [Carpenter et al. 2018] [Chaplin 2013] [Chauvin and Speegle 1957] [Chen et al. 2023c] [Chokani 2000] [Collier 1993] [Corke and Bowersox 2018] [Croom and Holmes 1985] [Croom et al. 1987] [Crouch 2008] [Davis and Fischer 1983] [Davis et al. 1986] [de Paula et al. 2025] [Deem and Murphy 1965] [Demetriades 1975] [Dirling et al. 1975] [Donelli et al. 2005] [Donelli et al. 2009] [Dong and Zhong 1998] [Drake and Solomon 2010] [Duan et al. 2012] [Dungan et al. 2026] [Dunlap and Kuethe 1961] [Dwivedi and Sidharth 2026] [Edwards 1961] [Eppink and Wlezien 2011] [Fehrs and Kaiser 2025] [First Laminar Flow Flight 1992] [Fischer 1969] [Fischer and Vemuru 1991] [Fischer et al. 1983] [Fisher and Cobleigh 1994] [Fisher and Peterson 1978] [Freudinger and Kehoe 1990] [Fu and Wang 2007] [Fuhrmann 1993] [Fujii 2005] [Gajoni et al. 2026] [Godil and Bertelrud 1992] [Gosse et al. 2014] [Graber et al. 1968] [Groot et al. 2020] [Haans et al. 2004] [Hader and Fasel 2021] [Hader and Fasel 2024] [Hader et al. 2020] [Han and Cao 2019] [Harvey and Pride 1982] [Hastings et al. 1986] [Hefner 1992] [Henderson 1967] [Heston et al. 2021] [Hill and Borg 2024] [Hollis 2008] [Holmes and Obara 1992] [Holmes et al. 1986] [Hong and Jung 2024] [Horstmann et al. 1990] [Hoskin et al. 2024] [Huang et al. 2025b] [Husmeier and Fasel 2007] [Hybrid Laminar Flow Flight 1999] [Introduction to the Virtual 2026] [Jaffe and Prislin 1966] [Jeong et al. 2026] [Jiang et al. 2026] [Johnsen et al. 2016] [Johnson and Candler 1999] [Johnson et al. 1997] [Johnson et al. 2008] [Johnston and Candler 2023] [Johnston et al. 2026] [Karpuk and Mosca 2024] [Kehoe 1987b] [Keller 2019] [Kim and Lee 2025] [Kimmel 1999] [Kimmel 2003] [Kimmel and Poggie 1997] [Kimmel et al. 2003] [Kirk 2016] [Kuntz and Potter 2007] [Kuntz and Potter 2008] [McGinley et al. 2006] [Runyan and Steers 1980] [LaGraff 2007] [Laminar Flow Control Wing 1999] [Lampropoulos et al. 2025] [Lange 1984] [Larson 1968] [Lau 2007] [Laurence et al. 2014] [Lee 2024] [Lee et al. 1990] [Lei and Zhong 2011] [Lei and Zhong 2012] [Li et al. 2011] [Li et al. 2012] [Liechty et al. 2006b] [Liechty et al. 2006a] [Lin and Miller 2025] [Liu et al. 2021a] [Lombardi et al. 1996] [Low Drag Airfoil Design 1980] [Lynde et al. 2021] [Maddalon and Wagner 1969] [Maddalon et al. 1989] [Maestrello et al. 1986] [Malik 1987] [Malik 2000] [Malik et al. 1990] [Manuel and Doty 1991] [Mao and Cao 2014] [Denison et al. 2023] [Marshall 2000] [Martellucci 1964] [Martellucci et al. 1972] [Maslov 2001] [Maslov and Mironov 2000] [Mavriplis et al. 2020] [Meersman et al. 2022] [Melander and Candler 2024] [Methel et al. 2025] [Minier and Suit 1988] [Miró Miró] [Mori et al. 2024] [Murakami et al. 1995] [Murthy and Rose 1977] [Murthy and Steinle 1986] [Nagamatsu and Sheer 1964] [Nagamatsu et al. 1965] [Nagel 1967] [Stetson 1990] [Wagner et al. 1992] [Berry et al. 2016] [Paredes and Choudhari 2018] [Paredes et al. 2020] [Barnwell and Hussaini 1992] [Nguyen et al. 2023] [Nicotra et al. 2026] [Niu and Su 2023] [Obara et al. 1986] [Obara and Holmes 1985] [Obara et al. 1990] [Obara et al. 1991] [Orlik et al. 2009] [Ort and Dosch 2019] [Oz and Kara 2024] [Ozawa and Bruce 2025] [Palmer et al. 2013] [Paredes et al. 2021] [Patrick 2019] [Perkins et al. 2022] [Perkins et al. 2023] [Pfenninger and Bacon 1961] [Pinna and Rambaud 2013] [Pätzold et al. 2013] [DiviaHarshaVardini et al. 2023] [Ramnath 1969] [Redeker et al. 1990] [Reeh and Tropea 2015] [Ren et al. 2014] [Riedel and Sitzmann 1997] [Riley and McNamara 2016] [Roback et al. 1996] [Roberts et al. 2012] [Ryan-Simmons and Agarwal 2024] [Sakamoto et al. 2023] [Saric 2010] [Saric and Reed 2004] [Saric et al. 2015] [Schneider 1998] [Schneider 1999] [Schneider 2007] [Schneider 2008b] [Schneider 2008a] [Schuelein 2008] [Sheetz 1965] [Shiplyuk et al. 2012] [Shrestha and Candler 2018] [Shrestha et al. 2017] [Sidharth and Dwivedi 2026] [Sidorenko et al. 2015] [Snodgrass 1955] [Softley 1969] [Somers 1992] [Spanos 2009] [Stemmer 2005] [Stetson 1983] [Stetson 1986] [Stetson 1992] [Stilla 1993] [Stilla 1994] [Streett 2003] [Subbareddy and Candler 2011] [Swanson and Daniel 2016] [Tang et al. 2010] [Tani 1952] [Tauber and Wilkins 1966] [Throckmorton and Hartung 1984b] [Tirtey et al. 2008] [Tirtey et al. 2009] [Tokugawa and Yoshida 2006] [Osses 2020] [Transonic Flight Test 1994] [Tu et al. 2021] [Tucker et al. 2014a] [Tucker et al. 2016a] [Unnikrishnan and Gaitonde 2018] [Vu and Candler 2026] [Wagner et al. 1988] [Wang and Josyula 2016] [Ward and Miley 1983] [Wentz et al. 1985] [Wentz and Nyenhuis 1984] [Winston 1970] [Wood 1968] [Wurster 1981] [Xiao and Yang 2025] [Xu et al. 2019a] [Yang et al. 2021] [Ye et al. 2017] [Yeo and Liu 2018] [Young and Fielding 2001] [Zhao 2015] [Zhao et al. 2017] [Zhao et al. 2026] [Zhong 2000] [Zhong 2009] [Zhou et al. 2018] [Zhou et al. 2015b] [Zhu 2022] [Zou and Zhong 2026]

Experiment design and the information a test returns

The Bayesian framing, as a literature. Bayesian and optimal experimental design, expected information gain, the value of information, input and manoeuvre design for parameter estimation, and uncertainty quantification and model validation. It is the youngest cluster in the table, with a median year of 2017, and 81 of its 267 titles, fewer than a third, name a flight, an aircraft or another flight vehicle, which measures how far the method and its flight-test application have stayed apart.

267 records. [Abbas and Hazen 2025] [Agrell and Dahl 2021] [Air Force Test Pilot School Edwards Afb Ca 1994b] [Alex and Lijo 2021] [Alexanderian 2021] [Alexanderian and Maio 2026] [Alexanderian et al. 2016] [Anderson et al] [Ao and Li 2024] [Argyris and Papadimitriou 2016] [Argyris and Papadimitriou 2017] [Ashenafi et al. 2022] [Attia et al. 2025] [Banerjee and Corbetta 2021] [Bania and Wójcik 2025] [Banks and Rehm 2014] [Bansal 2019] [Bartuska et al. 2022] [Bartuska et al. 2024] [Bayard 1993] [Bayard 1992] [Bayesian Experimental Design 2014] [Bayesian optimal experimental design] [Bayesian uncertainty quantification and] [Beck et al. 2018] [Bellosta et al. 2021] [Ben-Haim 2006] [Bever 1992] [Blanchard and Sapsis 2021] [Bo et al. 2007] [Bock et al] [Buchanan and Crosby 1983] [Busetto et al. 2009] [Bynum and Baurle 2011] [Capellari et al. 2016] [Carlon et al. 2022] [Carlon et al. 2023] [Catanach 2025] [Catanach and Callahan 2024] [Catanach and Das 2024] [Chaloner 1984] [Chaloner and Verdinelli 1995] [Chapter 5 the Value 2004] [Cheng and Huan 2026] [Chowdhary et al. 2026] [Coles and Prange 2012] [Coons and Huan 2025] [D-Optimal Designs for Exponential] [D-Optimal Designs for Rational] [Danowsky et al. 2012] [de Carvalho Dantas Maia et al. 2025] [Dean 1982] [Dehideniya] [Deshpande and Rivera 2013] [Design of Experiments 2016] [Dong et al. 2025] [Dougherty] [Drovandi and Tran 2018] [Du and Wang 2024] [Duong et al. 2023] [E- and c-Optimal Designs] [Englezou et al. 2022] [Eulrich et al. 1978] [Exact Optimal Designs 2011] [Farrow 2013] [Fehrs and Helm 2025] [Fischer 2005] [Functional Approach to Optimal 2006] [Fundamentals of the Optimal] [George et al. 2022] [Go and Chen 2025a] [Go and Chen 2025b] [Gottu Mukkula and Paulen 2016] [Grauer 2018] [Grimm et al. 2023] [Gupta et al. 1976] [Gupta and Hall 1975] [Haering and Plotkin 2013] [Han and Kim 2011] [Hosseini and Holzapfel 2022] [Hosseini et al. 2025b] [Huan and Banovic 2024] [Huan and Marzouk 2013] [Hull 2026] [Hyde et al. 2014] [INDES User’s Guide Multistep 1979] [Iollo] [Jackson 2023b] [Jaiswal and Honnappa 2020] [Jakeman 2023] [Jakeman 2024] [Jakowluk 2014] [Jakowluk 2018] [Jakowluk 2019] [James McGree] [Grauer and Boucher 2020] [Jauberthie et al] [Jauberthie et al. 2003] [Jauberthie et al. 2006] [Jauberthie et al. 2018] [Jayaraman et al. 2022b] [Jeong and Jo 2026] [Jeun and Whittaker 2002] [Jiang and Li 2018] [Jiang and Zhao 2021] [Jianhong 2025] [Jones et al. 2016] [Jung and Baeder 2019] [Matt] [Matt and Altamirano 2026] [Matt 2024] [Matt and Altamirano 2025] [Kamalov 2017] [Keesman 2015] [Keesman 2018] [Keisler 2004] [Keisler and Brodfuehrer 2009] [Kennamer et al. 2023] [Key Ideas in Experimental 2016] [Khodja et al. 2010] [Kidd 1965] [Kidd 1966] [Kim] [Kimmel et al. 1996] [Klein 1990] [Klein et al. 2026] [Kleinegesse et al. 2021] [Koval and Nicholson 2025] [Kraft 2018] [Kulkarni and Suh 2005] [Kullback and Leibler 1951] [Kurdi et al. 2007] [Lawrence] [Lepsien et al. 2025] [Li and Zhou 2016] [Li et al. 2017c] [Li et al. 2026b] [Lichota 2016] [Lichota et al. 2016] [Lichota et al. 2017] [Licitra et al. 2018] [Lindley 1956] [Liu et al. 2026c] [Lohr 1995] [Lopez-Toledo and Athans 1974] [Lu and Huang 1992] [Lu and Yeh 1993] [Lu et al. 1995] [López-Fidalgo 2023] [M10 Maximum entropy sampling 1996] [Man et al. 2016] [Mason 2013] [Mayr et al. 2015] [McClinton et al. 2002] [McFarland and Riha 2009] [Mehra 1974] [Mehra and Eupta 1975] [Merkhofer 1975] [Michek et al. 2024] [Moes et al. 2006] [Moes et al. 2003] [Morelli 2003] [Morelli 2008] [Morelli 2009] [Morelli 2021b] [Morelli 2021c] [Morelli 1991] [Morelli 1995b] [Morelli 1997] [Murphy and Landman 2015] [Müller 2005] [Neto et al. 2009] [Ng and Qureshi 1981] [Nguyen et al. 2020] [Numerical search for D-optimal 2022] [Oladyshkin and Nowak 2019] [Oliveira et al. 2024] [Omran et al. 2008] [Optimal experiment design for 2022] [Optimal input signals for 2022, 5 Optimal input signals for linea] [Optimal input signals for 2022, 7 Optimal input signals for DPS t] [Ozger 2007] [Panchal et al. 2007] [Panchal et al. 2009] [Pandey and Herrmann 2021] [Papadimitriou and Argyris 2017] [Parsa et al. 2025] [Phillips and Landman 2016] [Plotkin and Maglieri 2013] [Prangle et al. 2023] [Qi and Baker 2026] [Qian et al. 2014] [Qian et al. 2016] [Qureshi and Ng 1982] [RafajŁOwicz 1982] [Rafajłowicz 2022] [Ratvasky et al. 2007] [Rauk and Faya 2022] [Rothery et al. 2023] [Russell 2018] [Sadraoui et al. 2026] [Saetti and Rogers 2020] [Salis Brasil Neto et al. 2006] [Sandig 2024] [Santos and Cunha 2024] [Santosa and Anderson 2022] [Sebastiani and Wynn 2000] [Senkel et al. 2013] [Sensitivity and Value 2023] [Shannon 1948] [Sharpe and Hansman 2024] [Shen and Huan 2023] [Siddiqui et al. 2024] [Sivia 2006] [Smith 1996] [Smith 1995] [Smith et al. 2004] [Sousa et al. 2021] [Stepner and Mehra 1973] [Structured Risk Management 2011] [Sun and Sun 2015] [Tang et al. 2015] [Taylor et al. 2010] [Terejanu et al. 2013] [The Expected Fisher Information 2022] [Thumati and Schoen 2005] [Trotta et al. 2009] [Tsilifis et al. 2017] [Tucker et al. 2014b] [Tucker et al. 2016b] [Tulsyan et al. 2012] [Usman Hafeez et al. 2013] [Vallone] [van den Brandt and de Visser 2018] [van der Linden et al] [Vaughn et al. 2012] [Vernon 1993] [Villanueva and Smarslok 2015] [Voracek et al. 2002] [Harrison 2021] [Wahlberg et al. 2010] [Waite 2018] [Walsh et al. 2017] [Wang et al. 2018c] [Wang et al. 2024b] [Waterhouse] [Weiss et al. 2022] [Wetmore 1947] [White et al. 2022a] [White et al. 2022c] [White et al. 2023] [White et al. 2024b] [Willier et al. 2024] [Wizsa 2019] [Wizsa et al. 2020] [Wu et al. 2023b] [Wu et al. 2023d] [Wu et al. 2023c] [Xu and Liao 2020] [Yavuztürk et al. 2017] [Yoko 2024] [Yoon et al. 2010] [Youmin et al] [Zemplenyi and Miller 2023] [Zeng and Kukreja 2013] [Zhong et al. 2026] [Zonta et al. 2013]

Propulsion, thrust in flight and propulsion integration

The engine as the quantity a drag measurement depends on. Rocket and jet propulsion for research aircraft, inlets, nozzles and their integration with the airframe, thrust determined in flight, propulsion-controlled aircraft, and the engine as a flight research subject on testbeds such as the F-15.

205 records. [A Technology and Operations 1993] [Abada et al. 2024] [Abercrombie 1979] [Abernethy et al. 1986] [Advanced Ducted Propulsor In-Flight] [Air Force Test Pilot School Edwards Afb Ca 1992b] [Airfoil Static-Pressure Thrust 1990] [Andrews 1996] [Andrisani and Jones 1994] [Astakhov et al. 2024] [Atesoglu and Özgören 2006] [Atesoglu and Özgören 2007] [Aujogue] [Bartasevicius et al. 2022] [Battiston et al. 2022] [Bawa and Michalski 2025] [Beheim 1982] [Bellin and Brooks 1983] [Berry and Gilyard 1973] [Blanchard 1953] [Borg 2001] [Braman et al. 1983] [Brilliant and Bauer 1977] [Bronz et al. 2017] [Brown 2004] [Brown 1944] [Bruno 2023] [Bull and Bridges 1983] [Bullard 1967] [Burcham et al. 1995a] [Burcham et al. 1994] [Burcham et al. 1996] [Burcham et al. 1997a] [Burcham et al. 1997b] [Burcham et al. 2004] [Burcham and Burken 1994] [Burcham and Pappas 1996] [Burcham et al. 1981] [Burcham et al. 1983] [Burger 1983] [Burley 1970] [Bursey and Dickinson 1990] [Cale 1982] [Carman 1970] [Carroll and Cox 1983] [Chandler and Chisholm 1993] [Chaowanapreecha and Rattanagraikanakorn 2023] [Chun and Swanson 1964] [Cicala and Miele 1956] [Clough 1990] [Compton and Abdol-Hamid 1990] [Computational Analysis of Combustion 1981] [Conners 1989] [Conners and Sims 1998] [Coons 1986] [Craig and Reich 1981] [Cumming and Kim 2018] [Cutright and Braasch] [Davidson 1964] [Davison 1963] [Destarac and van der Vooren 2004] [Diskin and Northam 1987] [Drag and Propulsive Efficiency 1990] [Dutton and Addy 1980] [Elliott and Furgurson 1978] [Ellis and Brown 1943] [Emo and Gustus] [Ennix et al. 1993] [Falempin et al. 1995] [Flight Characteristics of Quad 2014] [Flight 2026] [Flynn et al. 2009] [Foreman 1963] [Foss and Swihart 1956] [Franciscus 1983] [Fullerton 1993] [Gal-Or 2001] [Gallagher 1968] [Gong et al. 2017] [Gove 1929] [Hernandez and Burcham 1988] [Curran and Murthy 1991] [Holmes et al. 1980] [Hughes 1981] [Hughes and Johnson 1972] [Hunter and D’Amico 2024] [In-Flight Thrust Determination] [In-Flight Thrust Determination for] [Integrated Propulsion Technology Demonstrator. 1994] [Jahn 2023] [Stewart et al. 1992] [James 1981] [Jankiewicz 2026] [Jansen et al. 2017] [Jet Thrust Measurement 2003] [Johnson and Painter 1976] [Jones et al. 2013] [Jones and Bui 2012] [Jones et al. 2014] [June et al. 2024] [Kantrowitz and Donaldson 1945] [Karabacak and Turan 2023] [Karlgaard et al. 2018] [Khalid and Faherty 1990] [Kim and Lee 2021] [Kimura et al. 2003] [Krivec et al. 1984] [Kurth et al. 2015] [Lacerda Montes et al. 2025] [Lederer 1996] [Linderman et al. 1974] [Lozino-Lozinsky et al. 1996] [Gowtham et al. 2022] [Macpherson 1962] [Madzsar et al. 1994] [Maine et al. 1994] [Malyuta et al. 2019] [Marmie et al. 2015] [Martos et al. 2011] [Massuger 1940] [Mauldin 1946] [McVey et al. 1969] [Merceruio] [Mickola 1961] [Miele 1955] [Miele 1957] [Miele 1959] [Mishra et al. 2019] [Mitcham et al. 1951] [Mixson et al. 1984] [Montgomery and Garrard 2005] [Moulden et al. 1974] [Muller and Gasko 1967] [Myers and Walsh 1988] [Nark and Jones 2019] [Nichols 1988] [Nugent et al. 1983] [Okninski et al. 2016] [Palumbo et al. 2003] [Patent for Rocket Airplane 1931] [Peters 1985] [Picard and Whitley 2002] [Piecewicz and Kindsvogel 1943] [Planeaux 1991] [Plant et al. 1980] [Poll and Schumann 2024] [Post et al. 2011] [Propulsion Systems from Takeoff 1991] [Qaumi 2021] [Ratnayake 2010] [Ray 1994] [Ray et al. 1992] [Reinhardt 1948] [Rezy 1980] [ROCKET-POWERED AIRCRAFT 2017] [Rooney and Wilt 1985] [Rosenberg and Schuch 1983] [Rubin 1971] [Ruetten 2018] [Thomas et al] [Thomas et al] [Saltzman 1957] [Sanders and Callaghan 1956] [Schenck 1949] [Smit and Gorrell 2026] [Solies 1992] [Sonneveldt et al. 2019] [St. John and Frederick 2013] [Stanly 1950] [Starkey et al. 2014] [Steer 2000] [Steppert and Epple 2017] [Stern and Peracchio 1989] [Stevens 1950] [Subsonic/Transonic/Supersonic Nozzle Flows 1986] [Taguchi et al. 2009] [Taguchi et al. 2012] [Tang and Chase 2008] [Thompson 2022] [Time-Dependent In-Flight Thrust Determination] [Tsohas and Heister 2010] [Uncertainty of In-Flight Thrust] [Vadyak et al. 1979] [Vinh and Medepalli 1994] [Walsh 1992] [Walsh 1993] [Ward and Miley 1984] [Ward et al. 1985] [Watson and Hardy 1983] [Welsh 1952] [White 1944] [Whitfield and Blackburn 1965] [Williams 1965] [Williams and Hunt 1980] [Wong et al. 2019] [Woodfield 1970] [Woodward and Loeffler 1993] [Yang et al. 2022b] [Yechout and Schweikhard 1984] [You et al. 2017] [Yun et al. 2019] [Zafirov 2010] [Zhang et al. 2017b] [Zhang et al. 2023] [Zhuang et al. 2025]

Demonstrators, prototyping, cost and acquisition

The programme as an investment. Airframe cost-estimating relationships, life-cycle and development cost, design to cost, prototyping and technology demonstrators, and the budget documents of the services that buy them.

182 records. [A Comparison of Cost 1977] [A Preliminary Estimate 1970] [Abell 1989] [Abou Khalil] [Adams 1974] [Adams and Hinders 1974] [Aircraft Cost Considerations 2010] [Aircraft Engine Life Cycle] [Alford 2004] [Allel et al. 2023] [Anderson et al. 2016] [Arent and Falatko 1992] [Arnold 1981] [Ascani et al. 1980] [Balaram et al. 2018] [Ball 2013] [Bao and Chen 2023] [Barham 1994] [Beltramo 1985] [Bennett 1991] [Blackwell and Millott 2008] [Bornemisza 1990] [Brandeau 1978] [Brown 1981] [Brunner 1996] [Burnside 2012] [Bush 1965] [Recine et al] [Carlyle 1976] [Carten 1978] [Carter et al. 2013] [Chase and McKinney 2005] [Cheng et al. 2025] [Cherry 1975] [Clark 1980] [Clarke and Roskam 1982] [Clarke et al. 1982] [Coker et al. 1978] [Comey et al. 1978] [Cost of Aircraft 2016] [Cost-Estimating Relationships for Aircraft 1972] [Culy 1995] [Czysz and Murthy 1996] [Daniel and Ramusat 2005] [Davis 1989] [Deepa and Gupta 2023] [Defense Science Board Washington Dc 1993] [Dehennis 2025] [Deng and Yeh 2009] [Deng and Yeh 2010] [Deng and Yeh 2011] [Department of the Air 1980] [Department of the Air 1986] [Department of the Air 1990] [Department of the Air 1991] [Department of the Air 1994] [Donelson et al. 1989] [Dougherty 2018] [Draper et al. 1983] [Duke et al. 1988] [Duke et al. 1989] [ECO Demonstrator Begins Flight 2018] [Ecodemonstrator Flight Test Program 2020] [Eglin et al. 2025] [Eliassen 1965] [Erhard et al. 2021] [Etesse 1979] [Etherington 1988] [Evans and Sonntag 1963] [Ferretto¹ et al. 2024] [Fielding and Jones 2000] [Finchum 1974] [Fitzsimmons 1996] [Freuler and Hoffmann 1977] [Freund et al. 2008] [Fuel Cell Demonstrator Aeroplane 2007] [Gallagher and Fellers 1983] [Garman and Andrisani 2003] [Gindin and Darom 1996] [Bever 1981] [Green 1980] [Greer 2010] [Gudmundsson 2014a] [Gudmundsson 2022a] [Ha et al. 2017] [Hang 2015] [Harle 1979] [Hartley 1965] [Harvey and Ryan 2012] [Haynes et al. 2025] [Herkes et al. 2006] [Hillaker 1983a] [Hinrichsen and Bautista 2001] [Hoffman 1971] [Horowitz et al. 2014] [Howard et al. 1989] [Improving Acquisition and Sustainment 2023] [Iscold 2008] [Jategaonkar et al. 2005] [Jensen 2016] [Johnson 1990] [Juhasz et al. 2020] [Kenyon 1974] [Kish et al. 2017] [Klein et al. 2016] [Klingenberg et al. 2026] [Kreutz 1970] [Lang and Pitzer 1980] [Lappos and Phelps 1991] [Lewerenz 1987] [Lightweight Low-Cost Flight Test 2007] [Logan 1974] [London and Sumrall 1999] [Low Cost Cargo Aircraft 1960] [Lu et al. 2015] [Mach et al. 2007] [Malloy et al. 2010] [Marchinski 1974] [Martínez Morán 2018] [Marx 1983] [Marx et al. 1995] [Marx et al. 1998] [McCarthy et al. 2018] [Melgaard 1986] [Mogfhadam and Farsi 1995] [Monterzino et al. 2010] [Moorhouse 1990] [Morgenfeld 1992] [Muraoka et al. 2009] [Niazi et al. 2006] [Ohta et al. 1984] [Owens et al. 2006a] [Parametric Flyaway Cost Estimating 2024] [Pausder et al. 2000] [Pérez Rus and Le Gal 2024] [Reed et al. 1982] [Renz et al. 1981] [Robinson 1995] [Rocket Powered Prototypes 1998] [Rosenthal 1982] [Rosenthal and Brandeau 1983] [Rydlo et al. 2013] [Rzucidło 2006] [Shang et al. 2025] [Shawler 1981] [Simmons et al. 2023] [Skelly 1989] [Smith et al. 2011] [Sobrón Rueda 2021] [Srijayantha 1983] [Stahl et al. 1984] [Stekler 1982] [Stewart and Campion 1980] [Stratford 1973a] [Summary of Current Economic 1970] [Sun 2026] [Talmage 2008] [Thokala et al. 2012] [Thrall 1975] [Tihansky 1976] [Tirovolis and Serghides 2005] [Tom et al. 2009] [Trainelli and Rolando 2011] [Waddoups 1983] [Wang et al. 2021b] [Wernicke 1980] [White et al. 2024a] [Why do Aircraft Cost] [Why Do Aircraft Cost 1999] [Wilson 2012] [Womer and Gulledge 1983] [Womer and Marcotte 1986] [Woodrow et al. 2013] [Wright 1936] [Xu et al. 2026] [Yang 2021a] [Yates 1964] [Yates 1965] [Younossi et al. 2001] [Yu et al. 2023] [Zammit Mangion et al. 2024] [Zhixin 2022a]

Institutions, history and engineering knowledge

The arrangement and its historians. Histories of the NACA, NASA and their research centres, of flight research and of particular research programmes, centre overviews, test pilots, and the nature of engineering knowledge. Dryden and Armstrong, two names for one flight research centre, appear in 37 of its titles against 20 for Langley, so the centre at which most of this series flew is also the one whose own history is most often written.

170 records. [A Brief History 1978] [Aircraft Tire History] [Akens et al. 1965] [Altitude Wind Tunnel 2008] [Anderson 1976] [Anderson 1981] [Anderson 2000] [Anderton 1978] [Aviation History and UAS] [Ayar and Guleren 2019] [Bilstein and Wallace 1998] [Bilstein 1989b] [Aponso 2019] [Blanchard et al. 1980] [Bohn-Meyer et al. 2005] [Bohn-Meyer et al. 2004] [Bosworth 2006] [Bosworth 2010] [Braslow 1999b] [Braslow 1999a] [Henderson and Huff 2021] [Burns 2004] [Burns 2022] [Burns 2026] [Burns and Bruckner 2006] [Burns et al. 2007] [Campbell 2025] [Carroll 2025] [Cobham and Langley 1940] [Cole et al. 2006] [Costa and Arteaga 2011] [Cusimano and Johnson 1994] [Day 1997] [de Try 2004] [Dees and Moua 2010] [DelFrate 2008] [Deng et al. 2022] [Dodson 2005] [Dommett and Wright 2001] [Hartman 1970] [Ehresman 1981] [El-Sayed 2024a] [El-Sayed 2024b] [El-Sayed 2024c] [Emme 1976] [Ennix-Sandhu 2006] [Eppley 1963] [Fields 1978] [Fisher 1999] [Fisher 2007] [Fisher and Parcel 2007] [Flomenhoft 1994] [Fotia et al. 2019] [Frye et al. 2004] [Garrick and Reed 1981] [Gibbings 1982] [Goraj et al. 2007] [Gorn 2001b] [Gustafson 1956] [Gustafson 1970e] [Gustafson 1970b] [Gustafson 1970c] [Gustafson 1970a] [Gustafson 1970d] [Gustafson 1970f] [Hallion 1984] [Hamer and Mayo 1953] [Hansen et al. 2004] [Hansen et al. 2005] [Henderson et al. 1952] [Hicks 1992] [Higham 1963] [History of Aircraft & 2022] [History of Commercial Aircraft] [History of Supersonic Transport 2020] [Hodges et al. 2016] [Hollmann 1993] [Holubik 1988] [Horn 2008] [Hudson et al. 2018] [Hylton et al. 2012] [Jackel 2020] [Jackson 1953] [Jackson et al. 2004] [Johns 1984] [Johnston and Sawyer 1988] [Jones et al. 2024] [Chambers 2000b] [Chambers 2003] [Kehoe 1995] [Mort 2020] [Klein 2002] [Koppes 1989] [Koppes and Anderson 1977] [Koppes and Hansen 1989] [Kostyk 2011] [Kostyk 2007] [Kryvokon 2018] [Wallace 1996] [Langley 1971] [Lappos 2020] [Lau et al. 2009] [Leary 2002] [Levinson 1987] [Lewis 1991b] [Lincoln and Elliott 1994] [Lux et al. 2007] [Martinez 2012] [Meyer 2007] [Miller 2007a] [Miller 2007b] [Montoro et al. 2023] [Murphy and Klein 2005] [Murrow et al. 1989] [Dougherty] [NACA/NASA History at Dryden 1990] [NASA Langley Research Center 2022] [Navarro 2009] [Neal and Flick 2017] [Negaard 1980] [Norlin 1995] [Nugent and Takahashi 2026] [Mack 1998] [Pfenninger and Vemuru 1992] [Phillips 1998] [Portree 1998] [Powell and Shyy 2013] [Powers 1997] [Pugsley 1987] [Putnam 1984a] [Ratnayake 2009] [Ratnayake 2007] [Reubush 1992] [Ricketts 1990] [Riebe and Kuhn 1973] [Roland and Becker 1983] [Roland 1984] [Samuel et al. 2018] [Schultz 2003] [Schyfter 2013] [Sharipkhojaevic 2025] [Sorenson 1971] [SpaceShipOne 2008] [Spearman 2003] [Spearman 2004] [Spearman 2005] [Spearman 2009] [Spearman 2012] [Spearman 1981] [Springer 1994] [Stephenson 1999] [Swassing 2008] [Sweetman 1990] [Talmage 1947] [Talty and Caughlin 1988] [Tatarewicz and Hansen 1996] [Technology Demonstrator Close Air 2023] [Thomson 2024] [Thomson 2025] [Titan II Research 2002] [Torenbeek 2016] [Tow 2010] [Versa Power Boeing 2011] [Walan and Lydecker 2023] [Wang and Iliff 2004] [Ward 1984] [Wolfe and Bakalyar 2011] [Xie 2024] [Zahm 1921] [Zubrin and Clapp 1996]

Reusable launch and the recovery problem

The problem the X-33 and X-34 met, later solved outside the series. Reusable launch vehicle design and operations, approach, landing and vertical recovery, guidance for the unpowered return, and the programmes from the Space Shuttle orbiter to the commercial vehicles.

168 records. [Agarwalla 2025] [Al Bakri] [AL-Bakri and Kluever 2017] [Allen et al. 1994] [Andrews 1998] [Arora et al. 2003] [Barthelemy 1989a] [Baumann and Bisbee] [Benton 1990] [Berman 1947] [Birkeland and Meuser 1999] [Bjarke and Ehernberger 1989] [Bogue and Erbland 1992] [Bradford et al. 2000] [Brevault et al. 2019] [Burchett] [Campbell et al. 2009] [Caplin] [Chase 1979] [Coakley] [Cook 1995a] [Cooke 1980a] [Cooke 1980b] [Cooke 1982] [Crawford and Thomas 2006] [Culp and Cooke 1982] [Curry et al. 1992a] [Cusick and Kontis 2019] [Daniel et al. 2004] [Der Kiureghian 2001] [Devanath and Beebi 2016] [Dods and Hanly 1972] [Dong et al. 2023b] [Dorsey et al. 2000] [Du] [Dumbacher and Klevatt 1994] [Edwards et al. 2010] [Eggers 2003] [Elias and Knutson 1995] [Elvin 1996] [Fallon et al. 1999] [Ferrandon 1997] [Ferrandon 1998] [Findlay et al. 1984] [French 1988b] [Fujii et al. 2003] [Gage and Vander Kam 2003] [Gardinier and Taylor 1999] [Gong et al. 1987] [Green et al. 1983] [Guadagnini et al. 2023] [Hagopian 2002] [Hameed and Bindu 2019] [Hannum and Berkopec 1989] [Hao et al. 2017] [Hellman et al. 2010] [Hertzfeld 2000] [Hillje and Nelson 1981] [Hunt 1989] [Igreja and Lemos 2022] [Ishimoto et al. 2005] [Jacobson 1952] [Jategaonkar et al. 2006] [Jiang and Ordonez 2008] [Johnson and Servidio 2008] [Johnson and Sorenson 2006] [Junaid R and Beebi M 2015] [June et al. 2025] [Jung et al. 2025] [Kalden 2007] [Kaplan 2002] [Karel 1967] [Khamlak 2026] [Kiehn 2020] [Kim et al. 2026] [Kirsten 1985] [Kluever and Neal 2015] [Knapp 1999] [Kohrs 1982] [Komar and Christenson 1996] [Krishnan and Sajikumar 2023] [Larsen 2000] [Larsen 2003] [Larsen 2005] [Letchworth and Letchworth 2000] [Li and Hu 2018] [Li et al. 2025a] [Li et al. 2026d] [Liu et al. 2017a] [Logsdon and Williamson 1997] [Marlow 2003] [Martin 2006] [Martin et al. 2024] [Mathews et al. 1948] [McCandless and Cruz 1985] [McClure 1998] [McConnaughey et al. 1995] [Mendenhall et al. 1997] [Merlet 1954] [Meyerson 1998] [Miotto and LePome 2003] [Mo et al. 2022] [Mobley 1999] [Molina et al. 2009] [Moore et al. 1980] [Morris 1995] [Mosley 1972] [Myers et al. 1984] [Nair and Kukreja 2025] [Freeman et al. 1997b] [Noneman 2002] [Nugroho et al. 2024] [Numerical Optimization on Approach 2016] [Pidvysotskyi 2021] [Pruett et al. 1981] [Purcell et al. 2025] [Rasky et al. 2006] [Redondo Gutierrez et al. 2022] [Response Analysis of Landing 2026] [Reusable Launch Vehicle 1995] [Reusable Launch Vehicle Landing 2026] [Rey 2000] [Rooney 2003] [Hameed and Bindu 2021] [Saturn 5 Launch Vehicle 1971] [Scher 1947b] [Schmitt and Burchett 2004] [Singh et al. 2024] [Sivan and Pandian 2018] [Smith 1974] [Spencer 1999] [Staniszewski 1999] [Su and Wang 2015] [Suit and Schiess 1985] [Suit 1986] [Suit 1989] [Suit and Schiess 1988] [Sun] [Tariq et al. 2026] [Tetlow et al. 2000] [Thies 2022] [Throckmorton 1989] [Trevino et al. 2012] [Tsukamoto et al. 2003] [Tuohy 1998] [Urschel and Cox 2003] [Vaicaitis 1994] [Wang et al. 2020] [Wang et al. 2022c] [Wangu and Mouyos 1998] [Weilmuenster and Hamilton 1982] [Wetzel] [Wierzbanowski and Ramasubramanian 2020] [Wright 1989] [Xu et al. 2016] [Xu et al. 2025a] [Yamanaka 2003] [Yang et al. 2006a] [Yue et al. 2018] [Yue et al. 2019] [Yue et al. 2022a] [Yue et al. 2022b] [Zhang et al. 2017a] [Zhang et al. 2018] [Zhang et al. 2021] [Zhang et al. 2025e] [Zhao et al. 2020] [Zimpfer 1999]

Flight instrumentation, telemetry and data reduction

The instrument inside the instrument. Flight test instrumentation systems, telemetry, air-data systems and their calibration, sensors and fibre-optic strain sensing, and the reduction of recorded flight data.

156 records. [Pool and Bosman 1974] [Boztug et al. 2026] [Ali 2026] [Johnson et al] [Aiken and See 1951] [Air Force Test Pilot School Edwards Afb Ca 1990c] [Air Force Test Pilot School Edwards Afb Ca 1993] [Aircraft and Flight Test 2021] [Alich and Castillo 2007] [Allen and Hofbeck 1986] [Doan et al. 2020] [Bachalo et al. 1990] [Bai et al. 2019] [Bailey et al. 1996] [Bekar et al. 2025] [Bendix Corp York Pa 1963] [Blanchard 1989] [Blanchard 1991] [Bleimeyer 1981] [Blue and Crawford 1997] [Borek and Richardson 1969] [Brotherhood 1975] [Bufalino 1995] [Calloway 1986] [Campbell and Kresge 2003] [Carnahan et al. 1975] [Chan 2018] [Coskun and Genc 2021] [Crowther and Lamont 2001] [Crounse 2005] [Demo 1986] [Erol et al. 2004] [Design Validation and Verification 2026] [Dickhudt 1983] [Durbin 1959] [Schwegler - Lanl and Place - Honeywell 2000] [Fantini 1998] [Farmer 1974] [Filipovic and Dikic 2011] [Fitz and Stattel 1965] [Flight Test Instrumentation 1965] [Frederick and Ratnayake 2010] [Frederick and Ratnayake 2011] [Friehmelt and Jost 2000] [Garoutte and Bryan 1983] [Gerlach 1965] [Gilyard and Belte 1974] [Bever 1984] [Bever 1986] [Bever 1991a] [Grafe et al. 2026] [Gregorek et al. 1977] [Gruber et al. 2009] [Guelhan et al. 2012] [Haering 1993] [Hager 1955] [Hamory and Murray 1992] [Hamory and Murray 1993] [Hang 2017] [Harney et al. 1983] [Harney and Richardson 1968] [Harpold and Reber 1966] [Head-up Displays and Air 1988] [Helffer et al. 2014] [High-Altitude Long-Endurance HALE Sensor 2026] [Hobbs and Page 2011] [Hon Man Chan et al. 2015] [Horton et al. 1966] [Howland 1953] [Huebner et al. 2009] [Hui and Collins 2001] [Hyde and Massie 1993] [Jacobsen 1974] [Jann and Yakimenko 2015] [Jarvinen and Bruce 1976] [Jentink and Bogue 2005] [Klun et al. 2020] [Johnston et al. 1998] [Jurado and McGehee 2019] [Kao and Anderson 1981] [Karns et al. 2017] [Knoblach 1974] [Knoedler et al] [Knoedler et al. 1996] [Kohlman et al. 1987] [Kosmos and Greenwell 1980] [Kurkjian 1947] [Lamy 1983] [Leach and Hui 2001] [Lee et al. 2019] [Lyöri et al. 2007] [Machnik et al. 2022] [Madhusudana Rao et al. 2014] [Mahindra 1983] [Mannai 1962] [Mayer and Chalfant 2023] [Mennebeuf et al. 2024] [Milne and Martos 2012] [Monteil 2024] [Morrell et al. 1988] [Nash 1981] [Nash 1982] [Naval Air Test Center Patuxent River MD 1963] [Niehaus 1962] [Nyquist 1928] [Olhausen 1975] [Rus et al. 2026] [Palomino 2022] [Parameswaran and Jategaonkar 2004] [Paris and Alaverdi 1998] [Parks and Wingrove 1977] [Parlini 1983] [Borek and Pool 1994] [Ratvasky and Van Zante 1999] [Reeves et al. 1960] [Reichle 1965] [Rhoads 1952] [Ricciardi and Minwalla 2016] [Roh et al. 2006] [Rooker 1970] [Sabatini 2014] [Sandoz et al. 2024] [Schafer 1962] [Schuster 2009] [Shlien 1991] [Song et al. 2024] [Space Vehicle Sa-6 Telemetry 1965] [Stelmach 2012] [Strapp et al. 2011] [Strock 1983] [Swanson et al. 2018] [Tambova et al. 2026] [Teets 2016] [Ratvasky et al] [Ratvasky et al. 2024] [Atkins et al] [Young] [Tsoubanos 1979] [Vasconcelos et al. 2011] [Cuda 2022] [Véras et al. 2022] [Try et al. 2020] [Waldersen and Schnarr 2017] [Walker and Kaufman 1977] [Warner and Moran 1979] [Westphal et al. 2006] [Widnall and Grundy 1974] [Wilkin Perry 1943] [Benson et al] [Wilson] [Wolf and Bossert 2001] [Meineke and Urry 1992] [Work et al. 2019] [Yang 2021b] [Yang 2021c] [Zyluk and Sibilski 2015]

Uncrewed aircraft and autonomy

The late X-series without a pilot. Unmanned combat air vehicles, the operation and flight testing of uncrewed aircraft, and their integration and autonomy.

63 records. [Abdulrahim 2019] [Ashokkumar 2023] [Bauer 2007] [Bauer 2009] [Bauer 2008] [Beeharry and Ramful 2024] [Blevins et al. 2022] [Cosentino 2006] [Cosentino 2009] [Costello et al. 2021] [Cox 2009] [Dantsker et al. 2019] [Zahn et al] [Dawkins et al. 2018] [De Wagter and Meulenbeld 2019] [Dickes et al. 2002] [Elkhoury 2008] [Feng and Yan 2017] [Flight Test Data Analysis 2016] [Fu Li et al. 2008] [Further Development and Flight 1994] [Gordnier et al. 2007] [In-Flight Demo of Multiple 2007] [Jorris et al. 2011] [Kim et al. 2015] [Larrabee] [Leylek and Costello 2015] [Lima Filho et al. 2021] [Lin 2002] [McKinnis et al. 2021] [Michalowski and Varano 2017] [Minwalla et al. 2016] [Mustopa 2022] [Grindle et al. 2017] [Okuhara et al. 2022] [Opromolla 2020] [Pestana 2010] [Petersen et al. 2004] [Practice for Methods to] [Prasad and Unnikrishnan 2006] [Qinkun Xiao et al. 2006] [Sabatini 2013] [Soltmann and Hall 2017] [Standard Practice for Methods] [Suminsby 2002] [Szilder and McIlwain 2012] [Taranto and Abdulrahim 2023] [Tekinalp and Cavus 2012] [Tianyuan and Xiongqing 2009] [UAV Flight Testing 2021] [Vallespin et al. 2011] [van Rooij and Cummings 2018] [van Rooij et al. 2018] [Vehicle Estimates for Target 1971] [Vicroy et al. 2012] [Wills 2015a] [Wills 2015b] [Wyatt 2003] [Xi et al. 2023] [Xu and Keshmiri 2021] [Zeitler et al. 2018] [Zhou et al. 2015a] [Zhou et al. 2023a]

Other flight research and high-speed aeronautics literature

The residual, reported and not hidden. On-subject records that fall in no cluster above, being 17 titles on standard-atmosphere tables, machine learning in fluid mechanics, subsonic research-aircraft and transport concepts, icing research and the aerodynamic problems of manned space vehicles. A residual this small is a property of a gate that admits only titles naming this article’s subjects, so almost every admitted title falls under one of the headings above.

17 records. [Atmospheric Model 1993] [Kock et al. 1978] [Bradley and Droney 2011] [Bradley and Droney 2012] [Brunton et al. 2020] [Chambers and Reed 1993] [Cruise and Climb of] [Fitzgerald et al. 1994] [International Standard Atmosphere ISA 2017] [Landis 2001] [McConkey et al. 2025] [Nonweiler 1959] [Northrop Aircraft INC Hawthorne CA 1953] [Reinmann et al. 1982] [Stough and Nolmes 1987] [Thelander 1965] [Williams 1978]

Where the Framing Breaks Down

The instrument model is productive, but it is not universally correct. Four failure modes are stated here at the outset so that individual articles can invoke them by name.

The model assumes a keystone exists. Some designations were assigned to vehicles that had no research question at all, being either what Jenkins et al. 2003 call essentially prototypes of future operational aircraft or technology demonstrators assembled from existing components to show an integration rather than to measure anything. For those the keystone section of the article template is a forced fit, and the article says so.

The model assumes the keystone was identified correctly at the time. Several programmes were built around a question that turned out not to be the binding one. The X-3 was built to investigate sustained supersonic flight with a low-aspect-ratio wing, could not exceed Mach one in level flight, and instead met roll inertia coupling, which on this reading was its most valuable result. Treating the X-3 through its stated keystone misses what it actually contributed.

The model treats the aircraft as the unit of analysis. For some programmes the unit is properly the facility, the test technique, or the analytical method, and the aircraft is incidental. The X-21 laminar flow programme is better understood as a study of manufacturing tolerance and surface contamination than as an aircraft programme, and its negative result, the slots plugged by debris, insects and rain that the Northrop X-21 entry records, was about dirt rather than about aerodynamics.

The model assumes a programme is scored on information returned. Some X-designations may have existed to sustain an industrial capability, to keep a design team employed between production contracts, or to establish a claim on a budget line. Those are real purposes and the information framing does not capture them. The articles covering the more recent designations return to this point repeatedly, because the proportion of programmes with a non-informational purpose appears to rise over the period covered.

Epistemic State

This section follows the analytical essay convention used throughout this blog and sorts the claims above by the kind of support they have.

Established historical fact includes the existence, sponsorship, and gross characteristics of the aircraft named here, the tripartite institutional arrangement of service, contractor, and NACA or NASA, the physical concentration at Muroc and Edwards, the fleet sizes of three airframes each for the X-1 and X-15, the X-15A-2 use of MA-25S ablative coating on the Mach 6.7 flight, the refusal of the X-52 designation in 2006 over confusion with the B-52, and the 2026 announcement of the Bell Textron X-76 with the number chosen as a reference to 1776. These are documented in the sources cited and are not in dispute.

Established engineering analysis includes every equation in the sizing sections. The similarity groups, the Prandtl-Glauert relation, the Sears-Haack wave drag result, the Tsiolkovsky relation, the typical-section divergence dynamic pressure, the Sutton-Graves stagnation heating correlation, the Allen-Eggers entry solution, and the uncertainty propagation relation are all standard results with settled derivations, and the reader should treat them as textbook rather than as claims of this article. The worked numerical examples are the author’s arithmetic applied to published input values, and they are labelled as derived where they appear.

Inference includes the interpretation of any particular aircraft through a single keystone. That the X-15 was thermally driven and the X-29 aeroelastically driven is a reading of the design record rather than a statement any programme office made in those terms. The reading is defensible, but it remains a reading.

Weakly supported inference includes the binomial attrition calculation reproducing the historical fleet size of three. Two data points agreeing with a calculation is not evidence that the calculation describes the decision process, and no claim is made that any programme office performed it. The agreement is offered as a quantitative intuition and nothing more.

Contested and unresolved in the public record are the X-23 designation attribution, the character of the X-42, and the sequence of events that produced the X-44 duplication. This series does not resolve any of them and states the conflict in each case.

Outside the public record entirely are the specifications and results of the X-41 and the mission content of the X-37 flights. Where this series discusses them it is describing the shape of the gap rather than its contents.

A note on sources is also owed. Three research citations point at search endpoints of the NASA Technical Reports Server rather than at fixed document identifiers, which is a weaker form of citation because a search endpoint cannot return a not-found response for a query that matches nothing. Every cited work is one the author has reason to believe exists. Every hand-chosen research citation carrying a digital object identifier, 62 in all, has been resolved through Crossref and checked against author and title, every hand-chosen citation of a NASA Technical Reports Server record has been checked against the server’s own author and title, and the survey’s other research records carry the identifiers that Crossref and the reports server return for them and are cited for their titles. The reader should treat the search-endpoint citations as pointers to a literature and not as verified links to particular editions.

Finally, a note on temporal position. This article carries an editorial date of 2025-10-06 and is written from knowledge current at the time of writing, which includes the 2026 announcement of the X-76 and developments in the X-59, X-65, X-66, and X-68 programmes that postdate the editorial date. That is a deliberate choice for a survey series, stated here so that the reader need not discover it.

Out of Scope

The series does not cover the X-designations of the pre-1946 United States system, the parallel unmanned XQ- series except where it consumed numbers from the same pool, foreign research aircraft except where they bear directly on a United States programme, lifting-body designations outside the X-series such as the M2-F1 and HL-10 except as context for the X-24, the D-558 series flown alongside the early X-planes under Navy sponsorship, or the research aircraft carrying NASA rather than military designations.

It does not attempt a unified aerodynamic theory of high-speed flight, a complete history of any sponsoring institution, a treatment of test pilot selection and training, or an assessment of the programmes against contemporary alternatives that were never designated.

It does not resolve classified questions through inference from open sources. Where the record stops, the articles stop.

Series Roadmap

The seventy-two articles run in designation order from the X-1 to the X-76, one per day, with this framing article opening and a synthesis article closing. The designation order is not chronological, because assignment is not monotone in time, and the articles say so where the discrepancy matters.

The early block from the X-1 through the X-5 covers the transonic and early supersonic research aircraft, and the instrument model is clearest there. The X-6 through X-12 block covers propulsion testbeds and missile development airframes, several of which are documentation-poor. The X-13 through X-22 block is dominated by vertical takeoff and landing experiments, which form the largest thematic cluster in the series. The X-23 through X-24 pair covers lifting-body entry. Small and unusual airframes at the edge of what the designation was meant for fill the X-25 through X-28 block. The 1980s configuration experiments occupy the X-29 through X-31 block. The X-32 through X-38 block covers the 1990s, when the designation was applied to large procurement demonstrators and reusable launch technology. The X-39 through X-51 block spans the transition to unmanned vehicles and hypersonic airbreathing propulsion, and it contains four of the nine anomaly cases. The X-52 through X-62 block covers the modern configuration and control demonstrators. The X-63 through X-76 block covers the current programmes, where the record is thinnest and the sponsorship is most varied.

The closing article returns to the questions raised here. What the designation became, why the clusters fall where they do, why the parallel unmanned series consumed numbers from the same pool, and whether the instrument model still describes what an X-designation means.

Conclusion

A research aircraft is a machine built to measure one thing that cannot be measured any other way, and the argument of this series is that everything else about such an aircraft follows from that one thing. The similarity gap establishes that ground facilities leave a residue. The keystone principle establishes that the residue dominates the design. The sizing relations establish how it propagates into wing area, skin material, propellant fraction, control authority, and instrumentation. The information economics establish why the programmes exist when they exist and why they cluster where they cluster.

The designation system carries its own evidence. It is not total, not a function, not injective, and not monotone, and each of those failures records an institutional fact. A number reserved and never formalized records a programme that lost its sponsor. A number refused records a nomenclature authority exercising judgement. A number consumed by a parallel unmanned series records the moment the uncrewed vehicles became numerous enough to compete for the same pool. A number chosen for an anniversary records an agency doing something other than counting.

Seventy-one articles follow. The next one takes the aircraft that started it, the Bell X-1, and asks what the transonic drag rise actually was and what it cost to find out.

Equations

This section collects the 147 display equations of the article in the order they appear, each under its number and reproduced exactly as it stands in the text. A title in bold names an established result, and a title in italics beginning with the word Bespoke names a construction made for this analysis. Of the 147, 127 are established and 20 are bespoke. Each equation uses the units of the International System stated in its section, with information measured in nats unless converted to bits, and several letters are reused across sections, so $\mu$, $\lambda$, $e$, $b$, $S$, $R$ and $T$ each change meaning between sections and are read from the nearest prose.

Equation 1, Linear Gaussian Observation Model. Each flight returns a measurement that is a linear function of the unknown parameter vector plus zero-mean Gaussian noise with a known covariance. Bayesian experimental design Lindley 1956 Chaloner and Verdinelli 1995

\[y_k = H_k \theta + v_k, \quad v_k \sim \mathcal{N}(0, R_k) \tag{1}\]

Equation 2, Information-Form Posterior Covariance Update. Under the linear Gaussian model the inverse posterior covariance is the inverse prior covariance plus one information increment from each flight.

\[\Sigma_n^{-1} = \Sigma_0^{-1} + \sum_{k=1}^{n} H_k^{\top} R_k^{-1} H_k \tag{2}\]

Equation 3, Information-Weighted Posterior Mean. The posterior mean combines the prior mean and every measurement, each weighted by the information it carries.

\[\mu_n = \Sigma_n \left( \Sigma_0^{-1} \mu_0 + \sum_{k=1}^{n} H_k^{\top} R_k^{-1} y_k \right) \tag{3}\]

Equation 4, D-Optimal and A-Optimal Design Criteria. D-optimality maximises the determinant of the information matrix and A-optimality minimises the trace of the posterior covariance. Atkinson and Donev 1992

\[\Phi_D = \det \left( \Sigma_n^{-1} \right), \qquad \Phi_A = \operatorname{tr} \left( \Sigma_n \right) \tag{4}\]

Equation 5, Differential Entropy of a Gaussian Posterior. The differential entropy of a multivariate Gaussian depends only on its dimension and the determinant of its covariance.

\[h(\theta) = \frac{1}{2} \ln \left[ (2 \pi e)^p \det \Sigma_n \right] \tag{5}\]

Equation 6, Expected Information Gain of an Experiment. The expected information gain of a planned flight is the expected Kullback-Leibler divergence of the posterior from the prior.

\[\mathbb{E} \left[ D_{KL} \left( p(\theta \mid y) \, \| \, p(\theta) \right) \right] = \mathbb{E} \left[ \int p(\theta \mid y) \ln \frac{p(\theta \mid y)}{p(\theta)} \, d\theta \right] \tag{6}\]

Equation 7, Scalar Posterior Variance after Repeated Measurements. For a single quantity measured repeatedly with equal noise, the posterior precision is the prior precision plus one measurement precision per flight.

\[\sigma_n^2 = \left(\frac{1}{\sigma_0^2} + \frac{n}{\sigma_m^2}\right)^{-1} \tag{7}\]

Equation 8, Flight Count Required to Reach a Target Uncertainty. Inverting the scalar update and rounding up gives the smallest number of flights that brings the posterior standard deviation to the target.

\[n^{*} = \left\lceil \sigma_m^2 \left( \frac{1}{\sigma_T^2} - \frac{1}{\sigma_0^2} \right) \right\rceil \tag{8}\]

Equation 9, Bespoke Flight Count for the Transonic Drag Problem. The required flight count per Mach band follows from assumed relative uncertainties of $1.0$ before the programme, $0.25$ per flight and a target of $0.05$, values the article chose to illustrate the X-1.

\[n^{*} = \left\lceil 0.0625 \left( 400 - 1 \right) \right\rceil = \lceil 24.9 \rceil = 25 \tag{9}\]

Equation 10, Information Gain as Entropy Reduction. For a scalar Gaussian the information gained is half the logarithm of the ratio of prior to posterior variance. Shannon 1948 Kullback-Leibler divergence

\[I_n = \frac{1}{2} \ln \frac{\sigma_0^2}{\sigma_n^2} \tag{10}\]

Equation 11, Conversion from Nats to Bits. An information quantity in nats is divided by the natural logarithm of two to express it in bits. Cover and Thomas 2006

\[I_{\text{bits}} = \frac{I_{\text{nats}}}{\ln 2} \tag{11}\]

Equation 12, Buckingham Pi Theorem Group Count. A relation among $n$ physical quantities involving $k$ independent dimensions reduces to a relation among $n - k$ dimensionless groups. Buckingham 1914

\[n - k \ \text{dimensionless groups} \tag{12}\]

Equation 13, Nondimensional Momentum Equation. Scaling the momentum equation by a reference length, speed and density leaves the Mach and Reynolds numbers as its only parameters. Anderson 2001

\[\frac{D \mathbf{u}^{*}}{D t^{*}} = -\frac{1}{\gamma M^2} \nabla^{*} p^{*} + \frac{1}{Re} \nabla^{*2} \mathbf{u}^{*} \tag{13}\]

Equation 14, Mach Number and Speed of Sound. The Mach number is the ratio of flow speed to the speed of sound, which for an ideal gas depends on the ratio of specific heats and the temperature. Mach number speed of sound

\[M = \frac{V}{a}, \quad a = \sqrt{\gamma R T} \tag{14}\]

Equation 15, Ideal Gas Law. The ideal gas law relates static pressure to density and temperature through the specific gas constant.

\[p = \rho R T \tag{15}\]

Equation 16, Mach Angle. A weak disturbance in supersonic flow propagates along a cone whose half-angle is the inverse sine of the reciprocal Mach number. Shapiro 1953 Liepmann and Roshko 1957

\[\mu_M = \arcsin \frac{1}{M} \tag{16}\]

Equation 17, Reynolds Number. The Reynolds number is the ratio of inertial to viscous forces formed from density, speed, a reference length and the dynamic viscosity. Reynolds number

\[Re = \frac{\rho V L}{\mu} \tag{17}\]

Equation 18, Sutherland Viscosity Law. The dynamic viscosity of a gas varies with temperature through a reference pair and the Sutherland constant. Sutherland 1893 NASA Glenn Research Center

\[\mu = \mu_{\text{ref}} \left( \frac{T}{T_{\text{ref}}} \right)^{3/2} \frac{T_{\text{ref}} + S}{T + S} \tag{18}\]

Equation 19, Reynolds Number in Terms of Pressure and Mach Number. Substituting the ideal gas law and the sound speed shows that at fixed Mach number and temperature the Reynolds number is proportional to static pressure times length.

\[Re = \frac{p M L}{\mu} \sqrt{\frac{\gamma}{R T}} \tag{19}\]

Equation 20, Test-Section Pressure Required by a Subscale Model. A model at geometric scale $1/k$ must run at $k$ times the flight static pressure to match the flight Reynolds number at the flight Mach number and temperature.

\[p_{\text{model}} = k \, p_{\text{flight}} \tag{20}\]

Equation 21, Isentropic Stagnation Pressure Ratio. The ratio of stagnation to static pressure in isentropic flow is a power of the stagnation temperature ratio fixed by the ratio of specific heats. Ames Research Staff 1953

\[\frac{p_0}{p} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}} \tag{21}\]

Equation 22, Stagnation Temperature Ratio. The ratio of stagnation to static temperature grows with the square of the Mach number for an adiabatic deceleration. stagnation temperature

\[\frac{T_0}{T} = 1 + \frac{\gamma - 1}{2} M^2 \tag{22}\]

Equation 23, Isentropic Stagnation Density Ratio. The ratio of stagnation to static density completes the isentropic set as a power of the stagnation temperature ratio. Ames Research Staff 1953

\[\frac{\rho_0}{\rho} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{1}{\gamma - 1}} \tag{23}\]

Equation 24, Unit Reynolds Number of the X-15 at Mach 6 and 30 Kilometres. The unit Reynolds number is evaluated with standard atmosphere density and temperature at 30 kilometres and the corresponding Mach 6 flight speed. International Standard Atmosphere U.S. Standard Atmosphere

\[\frac{Re}{L} = \frac{\rho V}{\mu} = \frac{0.01841 \times 1811}{1.48 \times 10^{-5}} = 2.26 \times 10^{6} \ \text{per metre} \tag{24}\]

Equation 25, Bespoke Reservoir Pressure for a One-Twentieth-Scale Model. The reservoir pressure follows from the isentropic ratio at Mach 6 applied to a hypothetical model at one-twentieth scale, a scale the article chose to show the size of the pressure penalty.

\[p_0 = 23{,}940 \times 1581 = 3.8 \times 10^{7} \ \text{pascals} = 38 \ \text{megapascals} \tag{25}\]

Equation 26, Prandtl Number. The Prandtl number is the ratio of momentum diffusivity to thermal diffusivity. Prandtl number

\[Pr = \frac{\mu c_p}{k_{\text{th}}} \tag{26}\]

Equation 27, Damkohler Number. The Damkohler number is the ratio of a characteristic flow time to a characteristic chemical time. Damkohler number

\[Da = \frac{\tau_{\text{flow}}}{\tau_{\text{chem}}} = \frac{L / V}{\tau_{\text{chem}}} \tag{27}\]

Equation 28, Arrhenius Dependence of Chemical Time. The characteristic chemical time varies exponentially with the ratio of activation energy to the product of the universal gas constant and temperature.

\[\tau_{\text{chem}} \propto \exp \left( \frac{E_a}{R_u T} \right) \tag{28}\]

Equation 29, Knudsen Number. The Knudsen number is the ratio of the molecular mean free path to a reference length. Knudsen number

\[Kn = \frac{\lambda}{L} \tag{29}\]

Equation 30, Kinetic-Theory Mean Free Path. Kinetic theory gives the mean free path in terms of viscosity, pressure and temperature.

\[\lambda = \frac{\mu}{p} \sqrt{\frac{\pi R T}{2}} \tag{30}\]

Equation 31, Knudsen Number from Mach and Reynolds Numbers. Substituting the mean free path into the definitions shows that the Knudsen number is proportional to the ratio of Mach number to Reynolds number.

\[Kn = \sqrt{\frac{\pi \gamma}{2}} \, \frac{M}{Re} \tag{31}\]

Equation 32, Bespoke Logarithmic Similarity Mismatch. The article measures how far a facility falls from flight as the norm of the difference between the logarithms of the facility and flight similarity vectors.

\[\varepsilon_{\text{sim}} = \left\| \ln \Pi_{\text{facility}} - \ln \Pi_{\text{flight}} \right\| \tag{32}\]

Equation 33, Bespoke Partition into Ground and Flight-Only Unknowns. The article defines the flight-only residual as the components of the unknown vector whose best achievable ground uncertainty exceeds the target. Drake and Williams 1958

\[\theta = \theta_{\text{ground}} \cup \theta_{\text{flight}}, \quad \theta_{\text{flight}} = \left\{ \theta_i : \sigma_i^{\text{ground}} > \sigma_i^{T} \right\} \tag{33}\]

Equation 34, Constrained Programme Cost Minimisation. Programme cost is minimised over the design variables subject to inequality constraints on the physical limits the vehicle must respect.

\[\min_{x} \ C(x) \quad \text{subject to} \quad g_j(x) \le b_j, \ j = 1, \dots, m \tag{34}\]

Equation 35, Lagrange Multiplier as Shadow Price. At the optimum each multiplier equals the negative sensitivity of the optimal cost to a relaxation of its constraint bound.

\[\lambda_j = -\frac{\partial C^{*}}{\partial b_j} \tag{35}\]

Equation 36, Lagrangian of the Programme Problem. The Lagrangian adds to the cost each constraint violation weighted by its multiplier.

\[\mathcal{L}(x, \lambda) = C(x) + \sum_{j=1}^{m} \lambda_j \left( g_j(x) - b_j \right) \tag{36}\]

Equation 37, Stationarity and Complementary Slackness. At the optimum the cost gradient is balanced by the weighted constraint gradients, and a constraint that does not bind carries a zero multiplier.

\[\nabla C(x^{*}) + \sum_{j=1}^{m} \lambda_j \nabla g_j(x^{*}) = 0, \qquad \lambda_j \left( g_j(x^{*}) - b_j \right) = 0 \tag{37}\]

Equation 38, Bespoke Keystone as the Largest Normalised Shadow Price. The article defines the keystone as the constraint whose multiplier times its bound is largest, a normalisation it chose so that constraints in different units can be compared.

\[j^{*} = \arg\max_j \ \lambda_j b_j \tag{38}\]

Equation 39, Dynamic Pressure. Dynamic pressure is half the product of free-stream density and the square of true airspeed. dynamic pressure

\[q = \frac{1}{2} \rho V^2 \tag{39}\]

Equation 40, Dynamic Pressure in Terms of Mach Number. The ideal gas law and the sound speed rewrite dynamic pressure as a product of static pressure and the square of the Mach number.

\[q = \frac{\gamma}{2} p M^2 \tag{40}\]

Equation 41, Dynamic Pressure of the X-15A-2 at Mach 6.7. The compressible form is evaluated at the Mach 6.7 record flight with a static pressure of about 1018 pascals. North American X-15

\[q = 0.7 \times 1018 \times 44.9 = 3.2 \times 10^{4} \ \text{pascals} \tag{41}\]

Equation 42, Lift Equation. Lift is the product of dynamic pressure, reference wing area and lift coefficient. lift coefficient

\[L = q S C_L \tag{42}\]

Equation 43, Stall Speed. Setting lift equal to weight at the maximum lift coefficient gives the lowest speed of level flight. stall

\[V_{\text{stall}} = \sqrt{\frac{2W}{\rho S C_{L,\max}}} \tag{43}\]

Equation 44, Load Factor. The load factor is the ratio of lift to weight.

\[n = \frac{L}{W} \tag{44}\]

Equation 45, Corner Speed. The corner speed is the lowest speed at which the maximum lift coefficient produces the structural limit load factor.

\[V_A = \sqrt{\frac{2 n_{\max} W}{\rho S C_{L,\max}}} \tag{45}\]

Equation 46, Turn Rate and Radius at a Given Load Factor. A level banked turn at load factor $n$ has a turn rate and radius fixed by the speed and the horizontal component of lift.

\[\omega_t = \frac{g \sqrt{n^2 - 1}}{V}, \qquad R_t = \frac{V^2}{g \sqrt{n^2 - 1}} \tag{46}\]

Equation 47, Equivalent Airspeed. Equivalent airspeed scales true airspeed by the square root of the density ratio, so that equal equivalent airspeeds give equal dynamic pressures.

\[V_e = V \sqrt{\frac{\rho}{\rho_{SL}}} \tag{47}\]

Equation 48, Bespoke Corner Speed of the Bell X-1. The corner speed is evaluated at 12 kilometres with the design load factor of 18 and a maximum lift coefficient of 1.0 that the article assumes. Bell X-1

\[V_A = \sqrt{\frac{2 \times 18 \times 4510}{0.311 \times 1.0}} = 723 \ \text{metres per second} \tag{48}\]

Equation 49, Specific Excess Power. Specific excess power is the excess of thrust over drag times speed divided by weight, the rate at which the aircraft can add energy height. energy-maneuverability theory

\[P_s = \frac{V (T - D)}{W} \tag{49}\]

Equation 50, Thrust Required from the Parabolic Drag Polar. The thrust required in flight at load factor $n$ is the sum of a zero-lift term rising with speed and an induced term falling with speed.

\[T_{\text{req}} = \frac{1}{2} \rho V^2 S C_{D0} + \frac{2 n^2 W^2}{\rho V^2 S \pi A e} \tag{50}\]

Equation 51, Absolute Ceiling Condition. Specific excess power vanishes where thrust equals drag, which defines the absolute ceiling.

\[P_s = 0 \quad \Longleftrightarrow \quad T = D \tag{51}\]

Equation 52, Energy Height. Energy height is the geometric altitude plus the kinetic energy per unit weight.

\[h_e = h + \frac{V^2}{2g} \tag{52}\]

Equation 53, Minimum-Time Climb Integral. The time between two energy states is the integral of the reciprocal of specific excess power over energy height.

\[t_{1 \to 2} = \int_{h_{e,1}}^{h_{e,2}} \frac{dh_e}{P_s(h_e)} \tag{53}\]

Equation 54, Energy Height of the X-15A-2 Record Flight. The energy height is evaluated at the record speed of 2021 metres per second and an altitude of 31.1 kilometres. North American X-15

\[h_e = 31{,}120 + \frac{2021^2}{2 \times 9.81} = 31{,}120 + 208{,}180 = 2.39 \times 10^{5} \ \text{metres} \tag{54}\]

Equation 55, Parabolic Drag Polar. The drag coefficient is the zero-lift drag coefficient plus an induced term proportional to the square of the lift coefficient. drag polar Munk 1921 Oswald 1932

\[C_D = C_{D0} + \frac{C_L^2}{\pi A e} \tag{55}\]

Equation 56, Maximum Lift-to-Drag Ratio. Differentiating the parabolic polar gives the maximum lift-to-drag ratio in terms of aspect ratio, Oswald efficiency and zero-lift drag. lift-to-drag ratio

\[\left( \frac{L}{D} \right)_{\max} = \frac{1}{2} \sqrt{\frac{\pi A e}{C_{D0}}} \tag{56}\]

Equation 57, Lift Coefficient for Maximum Lift-to-Drag Ratio. The maximum lift-to-drag ratio occurs at the lift coefficient at which induced drag equals zero-lift drag.

\[C_L^{*} = \sqrt{\pi A e \, C_{D0}} \tag{57}\]

Equation 58, Prandtl-Glauert Compressibility Correction. The small-disturbance compressible pressure coefficient is the incompressible value divided by the square root of one minus the square of the Mach number. Prandtl-Glauert transformation Glauert 1928

\[C_p = \frac{C_{p,0}}{\sqrt{1 - M_\infty^2}} \tag{58}\]

Equation 59, Drag Divergence Mach Number Criterion. The drag divergence Mach number is conventionally the Mach number at which the slope of drag coefficient against Mach number reaches one tenth. drag divergence Mach number

\[\left. \frac{\partial C_D}{\partial M} \right|_{M = M_{DD}} = 0.1 \tag{59}\]

Equation 60, Critical Pressure Coefficient. The pressure coefficient at which the local flow becomes sonic follows from the isentropic relations as a function of the free-stream Mach number.

\[C_{p,\text{crit}} = \frac{2}{\gamma M_\infty^2} \left[ \left( \frac{1 + \frac{\gamma - 1}{2} M_\infty^2}{1 + \frac{\gamma - 1}{2}} \right)^{\frac{\gamma}{\gamma - 1}} - 1 \right] \tag{60}\]

Equation 61, Simple Sweep Theory. Only the component of the free stream normal to the leading edge governs the compressible behaviour, which reduces the effective Mach number and the lift-curve slope by the cosine of the sweep angle.

\[M_{\text{eff}} = M_\infty \cos \Lambda, \qquad C_{L\alpha, \Lambda} = C_{L\alpha} \cos \Lambda \tag{61}\]

Equation 62, Sears-Haack Minimum Wave Drag. The minimum supersonic wave drag of a slender body of given length and maximum area is proportional to the square of the ratio of that area to the length. Sears-Haack Sears 1947

\[\frac{D_w}{q} = \frac{9 \pi}{2} \left( \frac{A_{\max}}{L} \right)^2 \tag{62}\]

Equation 63, Sears-Haack Area Distribution. The minimum wave drag is attained by a cross-sectional area distribution that is a three-halves power of a parabola in the axial coordinate. Sears 1947

\[A(x) = A_{\max} \left[ 4 \frac{x}{L} \left( 1 - \frac{x}{L} \right) \right]^{3/2} \tag{63}\]

Equation 64, Ackeret Linearised Supersonic Flat Plate. Linearised supersonic theory gives a lift coefficient proportional to incidence and a wave drag due to lift proportional to its square, both falling with Mach number. Ackeret 1925

\[C_L = \frac{4 \alpha}{\sqrt{M_\infty^2 - 1}}, \qquad C_{D,\text{wave}} = \frac{4 \alpha^2}{\sqrt{M_\infty^2 - 1}} \tag{64}\]

Equation 65, Whitcomb Area Rule. The transonic wave drag of a configuration depends primarily on the total axial distribution of cross-sectional area summed over fuselage, wing and nacelles. area rule Whitcomb 1952

\[A_{\text{total}}(x) = A_{\text{fuselage}}(x) + A_{\text{wing}}(x) + A_{\text{nacelle}}(x) \tag{65}\]

Equation 66, Rocket Thrust. Rocket thrust is the momentum flux of the exhaust plus the pressure difference between the nozzle exit and ambient acting over the exit area.

\[F = \dot{m} v_e + (p_e - p_a) A_e \tag{66}\]

Equation 67, Choked Throat Mass Flow. The mass flow through a choked nozzle throat is fixed by the chamber pressure and temperature, the throat area and the gas properties.

\[\dot{m} = \frac{p_0 A_t}{\sqrt{T_0}} \sqrt{\frac{\gamma}{R}} \left( \frac{2}{\gamma + 1} \right)^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{67}\]

Equation 68, Characteristic Velocity, Thrust Coefficient and Specific Impulse. Performance separates into a characteristic velocity measuring combustion and a thrust coefficient measuring expansion, whose product over standard gravity is the specific impulse. Sutton and Biblarz 2016 Huzel and Huang 1992

\[c^{*} = \frac{p_0 A_t}{\dot{m}}, \qquad C_F = \frac{F}{p_0 A_t}, \qquad I_{sp} = \frac{c^{*} C_F}{g_0} \tag{68}\]

Equation 69, Specific Impulse. Specific impulse is the thrust per unit propellant weight flow, expressed in seconds. specific impulse

\[I_{sp} = \frac{F}{\dot{m} g_0} \tag{69}\]

Equation 70, Tsiolkovsky Rocket Equation. The ideal velocity increment is the effective exhaust speed times the logarithm of the ratio of initial to final mass. Tsiolkovsky rocket equation

\[\Delta v = I_{sp} g_0 \ln \frac{m_0}{m_f} \tag{70}\]

Equation 71, Bespoke Ideal Velocity Increment of the X-15. The rocket equation is evaluated with the upper end of the quoted range of specific impulse for the XLR99 and the published launch and burnout masses, which gives an ideal increment with no losses. Jenkins 2000a North American X-15

\[\Delta v = 276 \times 9.807 \times \ln \frac{15{,}195}{6577} = 2707 \times 0.8374 = 2267 \ \text{metres per second} \tag{71}\]

Equation 72, Gravity and Drag Loss Integrals. The gravity loss integrates the component of gravity along the flight path and the drag loss integrates drag per unit mass over the burn.

\[\Delta v_{\text{grav}} = \int_0^{t_b} g \sin \gamma \, dt, \qquad \Delta v_{\text{drag}} = \int_0^{t_b} \frac{D}{m} \, dt \tag{72}\]

Equation 73, Bespoke Velocity Budget Closure. The article closes the budget by assigning the whole difference between the ideal and achieved increments to gravity and drag losses.

\[\Delta v_{\text{ideal}} = \Delta v_{\text{achieved}} + \Delta v_{\text{grav}} + \Delta v_{\text{drag}} \tag{73}\]

Equation 74, Launch Mass Fractions. The propellant, structural and instrumentation fractions of launch mass sum to one.

\[\frac{m_p}{m_0} + \frac{m_s}{m_0} + \frac{m_i}{m_0} = 1 \tag{74}\]

Equation 75, Initial Thrust-to-Weight Ratio. The initial thrust-to-weight ratio is the thrust divided by the launch weight.

\[\frac{T}{W} = \frac{F}{m_0 g_0} \tag{75}\]

Equation 76, Breguet Range Equation. Cruise range is the product of a propulsive term, the lift-to-drag ratio and the logarithm of the ratio of initial to final weight. range

\[R = \frac{V}{c g_0} \frac{L}{D} \ln \frac{W_0}{W_1} \tag{76}\]

Equation 77, Thermal, Propulsive and Overall Efficiency. The ideal Brayton thermal efficiency rises with compressor pressure ratio, the propulsive efficiency falls as exhaust speed exceeds flight speed, and their product is the overall efficiency. Hill and Peterson 1991

\[\eta_{th} = 1 - \frac{1}{\pi_c^{\frac{\gamma - 1}{\gamma}}}, \qquad \eta_p = \frac{2}{1 + u_e / u_\infty}, \qquad \eta_0 = \eta_{th} \, \eta_p \tag{77}\]

Equation 78, Airbreathing Net Thrust. The net thrust of a ramjet or scramjet is the captured air mass flow times the gain in momentum from inlet to exit including the added fuel. ramjet

\[F = \dot{m}_a \left[ (1 + f) u_e - u_\infty \right] \tag{78}\]

Equation 79, Isentropic Area-Mach Relation. The ratio of a duct area to its sonic throat area is a function of the local Mach number alone in isentropic flow.

\[\frac{A}{A^{*}} = \frac{1}{M} \left[ \frac{2}{\gamma + 1} \left( 1 + \frac{\gamma - 1}{2} M^2 \right) \right]^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{79}\]

Equation 80, Normal Shock Total Pressure Ratio. The ratio of total pressures across a normal shock is a function of the upstream Mach number alone.

\[\frac{p_{02}}{p_{01}} = \left[ \frac{(\gamma + 1) M_1^2}{(\gamma - 1) M_1^2 + 2} \right]^{\frac{\gamma}{\gamma - 1}} \left[ \frac{\gamma + 1}{2 \gamma M_1^2 - (\gamma - 1)} \right]^{\frac{1}{\gamma - 1}} \tag{80}\]

Equation 81, Kantrowitz Inlet Starting Limit. An inlet starts only when its throat-to-capture area ratio is large enough to pass the captured flow after a normal-shock total pressure loss. Kantrowitz and Donaldson 1945

\[\frac{A_{th}}{A_i} \ge \frac{p_{01}}{p_{02}} \cdot \frac{1}{\left( A / A^{*} \right)_{M_i}} \tag{81}\]

Equation 82, Combustor Residence Time Condition. Combustion completes only when the residence time of the flow in the combustor exceeds the ignition time, a Damkohler condition.

\[\tau_{\text{res}} = \frac{L_c}{u_c} > \tau_{\text{ign}} \tag{82}\]

Equation 83, Elliptic Spanwise Lift Distribution. The elliptic distribution gives the lift per unit span as a function of spanwise position for a total lift $L$ and span $b$.

\[\ell(y) = \frac{4 L}{\pi b} \sqrt{1 - \left( \frac{2 y}{b} \right)^2} \tag{83}\]

Equation 84, Root Bending Moment of an Elliptically Loaded Wing. The root bending moment is the semispan lift times the distance of its centroid from the root, which is linear in span and load factor.

\[M_{\text{root}} = \frac{2 n W}{3 \pi} \cdot \frac{b}{2} \tag{84}\]

Equation 85, Required Spar Cap Area. The spar cap area is the root bending moment divided by the product of the allowable stress and the structural depth.

\[A_{\text{cap}} = \frac{M_{\text{root}}}{\sigma_{\text{allow}} h_s} \tag{85}\]

Equation 86, Thermal Stress of a Constrained Plate. A plate constrained in its plane and heated by $\Delta T$ develops a stress set by the elastic modulus, the expansion coefficient and the Poisson ratio.

\[\sigma_{\text{th}} = \frac{E \alpha_T \Delta T}{1 - \nu} \tag{86}\]

Equation 87, Temperature-Derated Specific Strength. The material index is the allowable stress divided by density, evaluated at the skin temperature the trajectory produces.

\[\left. \frac{\sigma_{\text{allow}}(T)}{\rho_m} \right|_{T = T_{\text{skin}}} \tag{87}\]

Equation 88, Bredt-Batho Torsional Stiffness. The torsional constant of a closed thin-walled section is four times the square of its enclosed area divided by the contour integral of reciprocal wall thickness.

\[K_\theta = \frac{G J}{\ell_w}, \qquad J = \frac{4 A_m^2}{\oint \frac{ds}{t}} \tag{88}\]

Equation 89, Torsional Divergence Dynamic Pressure. A typical section diverges at the dynamic pressure at which the aerodynamic twisting moment per unit twist equals the torsional stiffness.

\[q_D = \frac{K_\theta}{e S C_{L\alpha}} \tag{89}\]

Equation 90, Bespoke Divergence Dynamic Pressure for Representative Values. The divergence dynamic pressure is evaluated for stiffness, offset, area and lift-curve slope that the article chose as representative and not specific to any aircraft.

\[q_D = \frac{5.0 \times 10^{5}}{0.20 \times 10 \times 4.5} = 5.6 \times 10^{4} \ \text{pascals} \tag{90}\]

Equation 91, Bending-Torsion Coupling of a Swept Wing. Upward bending of a swept wing changes the streamwise incidence in proportion to the bending slope and the sine of the sweep angle. Diederich and Budiansky 1948

\[\Delta \alpha_{\text{eff}} = -\frac{\partial w}{\partial y} \sin \Lambda \tag{91}\]

Equation 92, Reduced Frequency. The reduced frequency is the angular frequency times the semichord divided by the flow speed. Theodorsen 1935

\[k = \frac{\omega b}{V} \tag{92}\]

Equation 93, Flutter Speed Index and Mass Ratio. The flutter speed is normalised by the semichord, the torsional natural frequency and the square root of the ratio of wing mass to the mass of surrounding air.

\[F_i = \frac{V_f}{b \omega_\alpha \sqrt{\mu_m}}, \quad \mu_m = \frac{m_w}{\pi \rho b^2} \tag{93}\]

Equation 94, Adiabatic Stagnation Temperature. Decelerating the free stream adiabatically to rest raises its temperature by a factor that grows with the square of the Mach number.

\[T_0 = T_\infty \left( 1 + \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{94}\]

Equation 95, Laminar and Turbulent Recovery Factors. The recovery factor is approximately the square root of the Prandtl number for a laminar boundary layer and its cube root for a turbulent one.

\[r = Pr^{1/2} \ \text{(laminar)}, \qquad r = Pr^{1/3} \ \text{(turbulent)} \tag{95}\]

Equation 96, Recovery Temperature. The recovery temperature is the free-stream temperature raised by the recovery factor times the stagnation rise.

\[T_r = T_\infty \left( 1 + r \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{96}\]

Equation 97, Convective Heat Flux. The convective heat flux is the heat transfer coefficient times the difference between the recovery and wall temperatures.

\[\dot{q}_{\text{conv}} = h_c \left( T_r - T_w \right) \tag{97}\]

Equation 98, Stanton Number and the Reynolds Analogy. The Stanton number normalises the heat transfer coefficient, and the Reynolds analogy relates it to half the skin friction coefficient corrected by the Prandtl number. Eckert 1956

\[St = \frac{h_c}{\rho V c_p}, \qquad St \approx \frac{C_f}{2} Pr^{-2/3} \tag{98}\]

Equation 99, Fay-Riddell Stagnation-Point Heat Flux. The stagnation-point heat flux depends on edge and wall density-viscosity products, the stagnation velocity gradient and the enthalpy difference across the boundary layer. Fay and Riddell 1958

\[\dot{q}_s = 0.763 \, Pr^{-0.6} \left( \rho_e \mu_e \right)^{0.4} \left( \rho_w \mu_w \right)^{0.1} \sqrt{\frac{du_e}{dx}} \left( h_0 - h_w \right) \tag{99}\]

Equation 100, Newtonian Stagnation Velocity Gradient. The velocity gradient at a blunt stagnation point follows from the Newtonian pressure difference and the nose radius.

\[\frac{du_e}{dx} = \frac{1}{R_n} \sqrt{\frac{2 \left( p_s - p_\infty \right)}{\rho_s}} \tag{100}\]

Equation 101, Sutton-Graves Stagnation-Point Heating Correlation. The stagnation-point heat flux scales with the square root of density over nose radius and the cube of velocity. Sutton and Graves 1971

\[\dot{q}_s = k \sqrt{\frac{\rho_\infty}{R_n}} \, V_\infty^3 \tag{101}\]

Equation 102, Bespoke Stagnation Heat Flux of the X-15A-2. The Sutton-Graves correlation is evaluated at the record speed and density with an effective nose radius of 0.10 metres that the article assumes.

\[\dot{q}_s = 1.7415 \times 10^{-4} \times \sqrt{\frac{0.0157}{0.10}} \times 2021^3 = 5.7 \times 10^{5} \ \text{watts per square metre} \tag{102}\]

Equation 103, Biot Number. The Biot number compares conduction resistance through the wall with convection resistance at its surface.

\[Bi = \frac{h_c t_w}{k_w} \tag{103}\]

Equation 104, Lumped Transient Wall Heat Balance. A thin wall with small Biot number stores heat at the rate convection delivers it less the rate it radiates.

\[\rho_w c_w t_w \frac{dT_w}{dt} = \dot{q}_{\text{conv}} - \varepsilon \sigma_{SB} T_w^4 \tag{104}\]

Equation 105, Radiation Equilibrium Wall Temperature. A wall that conducts no heat away settles at the temperature at which it radiates what it absorbs. Stefan-Boltzmann law

\[T_{\text{eq}} = \left( \frac{\dot{q}_s}{\varepsilon \sigma_{SB}} \right)^{1/4} \tag{105}\]

Equation 106, Ballistic Coefficient. The ballistic coefficient is the mass divided by the product of drag coefficient and reference area. ballistic coefficient

\[\beta = \frac{m}{C_D A} \tag{106}\]

Equation 107, Exponential Atmosphere. Density falls exponentially with altitude over a constant scale height.

\[\rho(h) = \rho_0 \, e^{-h / H} \tag{107}\]

Equation 108, Allen-Eggers Ballistic Entry Velocity. Ballistic entry at constant flight path angle through an exponential atmosphere gives velocity as a double exponential in altitude. Allen and Eggers 1958

\[V(h) = V_e \exp \left[ -\frac{\rho_0 H}{2 \beta \sin \gamma_e} e^{-h / H} \right] \tag{108}\]

Equation 109, Allen-Eggers Peak Deceleration. The peak deceleration of ballistic entry depends on entry speed, flight path angle and scale height but not on the ballistic coefficient. Allen and Eggers 1958

\[a_{\max} = \frac{V_e^2 \sin \gamma_e}{2 e H} \tag{109}\]

Equation 110, Altitude of Peak Deceleration. The ballistic coefficient fixes only the altitude at which the peak deceleration occurs.

\[h_{a,\max} = H \ln \frac{\rho_0 H}{\beta \sin \gamma_e} \tag{110}\]

Equation 111, Integrated Heat Load. The heat load is the time integral of the stagnation-point heat flux over the entry.

\[Q = \int_0^{t_f} \dot{q}_s \, dt \tag{111}\]

Equation 112, Longitudinal Static Stability Criterion. Static stability requires a negative pitching moment slope, which holds when the centre of gravity lies ahead of the aerodynamic centre.

\[C_{m\alpha} = C_{L\alpha} \left( \frac{x_{cg} - x_{ac}}{\bar{c}} \right) < 0 \tag{112}\]

Equation 113, Neutral Point. The neutral point is the centre of gravity position at which the pitching moment no longer varies with lift coefficient.

\[\left. \frac{\partial C_m}{\partial C_L} \right|_{x_{cg} = x_{np}} = 0 \tag{113}\]

Equation 114, Static Margin. The static margin is the distance from the centre of gravity to the aerodynamic centre in units of the mean aerodynamic chord. longitudinal static stability

\[SM = \frac{x_{ac} - x_{cg}}{\bar{c}} \tag{114}\]

Equation 115, Short-Period Natural Frequency. The short-period frequency is approximated from the dimensional pitch and heave stability derivatives.

\[\omega_{sp} \approx \sqrt{\frac{Z_\alpha M_q}{V} - M_\alpha} \tag{115}\]

Equation 116, Short-Period Damping Ratio. The short-period damping ratio is approximated from the pitch damping, the angle of attack rate derivative and the heave derivative.

\[\zeta_{sp} \approx -\frac{M_q + M_{\dot\alpha} + Z_\alpha / V}{2 \, \omega_{sp}} \tag{116}\]

Equation 117, Lanchester Phugoid Frequency. To first order the phugoid frequency is the square root of two times gravity divided by speed, independent of the aerodynamics. phugoid

\[\omega_{ph} \approx \frac{g \sqrt{2}}{V} \tag{117}\]

Equation 118, Phugoid Damping Ratio. To first order the phugoid damping ratio is inversely proportional to the lift-to-drag ratio.

\[\zeta_{ph} \approx \frac{1}{\sqrt{2}} \frac{1}{L / D} \tag{118}\]

Equation 119, Dutch Roll Frequency and Roll Subsidence Time Constant. The Dutch roll frequency follows from the directional stiffness and yaw inertia, and the roll time constant from the roll inertia and roll damping. Dutch roll

\[\omega_{dr} \approx \sqrt{\frac{N_\beta}{I_z}}, \qquad \tau_r \approx -\frac{I_x}{L_p} \tag{119}\]

Equation 120, Spiral Stability Condition. The spiral mode is stable when the product of the dihedral effect and yaw damping exceeds the product of roll due to yaw rate and directional stiffness.

\[L_\beta N_r - L_r N_\beta > 0 \tag{120}\]

Equation 121, Gyroscopic Terms of the Euler Moment Equations. The pitch and yaw moment equations contain products of body rates and inertia differences that couple roll into pitch and yaw. Inertia coupling

\[I_y \dot{q} = M + \left( I_z - I_x \right) p r, \qquad I_z \dot{r} = N + \left( I_x - I_y \right) p q \tag{121}\]

Equation 122, Critical Roll Rate for Inertia Coupling. Divergence follows when the roll rate approaches the lower of the pitch and yaw natural frequencies. Phillips 1948

\[\omega_\alpha = \sqrt{\frac{-M_\alpha}{I_y}}, \qquad \omega_\beta = \sqrt{\frac{N_\beta}{I_z}}, \qquad p_{\text{crit}} \approx \min \left( \omega_\alpha, \omega_\beta \right) \tag{122}\]

Equation 123, Minimum-Time Bang-Bang Manoeuvre. A rest-to-rest rotation through $\Delta \phi$ with full thrust for half the time and full reverse thrust for the other half takes a time set by inertia, angle and control moment.

\[\Delta t = 2 \sqrt{\frac{I \Delta \phi}{F_t \ell}} \tag{123}\]

Equation 124, Reaction Control Propellant Mass. The propellant required is the total thruster impulse divided by the specific impulse of the thrusters times standard gravity.

\[m_{p, \text{RCS}} = \frac{\int F_t \, dt}{I_{sp, \text{RCS}} \, g_0} \tag{124}\]

Equation 125, Bespoke Aerodynamic to Reaction Control Handover Pressure. The article places the handover at the dynamic pressure at which the thruster moment equals the aerodynamic rolling moment at full control deflection.

\[q_{\times} = \frac{F_t \ell}{S b \, C_{l \delta} \, \delta_{\max}} \tag{125}\]

Equation 126, Combined Standard Uncertainty. For uncorrelated inputs the variance of a derived quantity is the sum of squared sensitivities times the input variances. propagation of uncertainty measurement uncertainty

\[u_c^2(y) = \sum_{i=1}^{n} \left( \frac{\partial f}{\partial x_i} \right)^2 u^2(x_i) \tag{126}\]

Equation 127, Covariance Term of Uncertainty Propagation. Correlated inputs add twice the sum over pairs of sensitivity products times the input covariances.

\[2 \sum_{i < j} \frac{\partial f}{\partial x_i} \frac{\partial f}{\partial x_j} u(x_i, x_j) \tag{127}\]

Equation 128, Drag from Accelerating Flight. Drag is thrust less the product of instantaneous mass and measured axial acceleration. Beeler et al. 1956

\[D = T - m a_x \tag{128}\]

Equation 129, Bespoke Drag Uncertainty of the X-1 Example. The combined uncertainty is evaluated for supposed uncertainties of three percent in thrust, half a percent in mass and one and a half percent in acceleration, values the article chose for illustration.

\[u_c(D) = \sqrt{(801)^2 + (237)^2} = 835 \ \text{newtons} \tag{129}\]

Equation 130, Relative Uncertainty of a Difference. Differencing two measured quantities amplifies the relative uncertainty by approximately the ratio of the larger quantity to the difference.

\[\frac{u(D)}{D} = \frac{T}{D} \sqrt{\left( \frac{u(T)}{T} \right)^2 + \left( \frac{X}{T} \right)^2 \left( \frac{u(X)}{X} \right)^2} \tag{130}\]

Equation 131, Nyquist Sampling Criterion. A signal containing frequencies up to $f_{\max}$ must be sampled at more than twice that frequency. Nyquist-Shannon sampling theorem Nyquist 1928

\[f_s > 2 f_{\max} \tag{131}\]

Equation 132, Quantisation Step and Quantisation Noise. A converter with $b$ bits over a full-scale range has a step of that range divided by $2^b$ and a noise standard deviation of the step divided by the square root of twelve.

\[\Delta = \frac{FS}{2^b}, \qquad \sigma_q = \frac{\Delta}{\sqrt{12}} \tag{132}\]

Equation 133, Signal-to-Noise Ratio of an Ideal Converter. Each bit of word length adds about six decibels to the signal-to-noise ratio of a full-scale sine wave.

\[\text{SNR} \approx 6.02 \, b + 1.76 \ \text{decibels} \tag{133}\]

Equation 134, Telemetry Bit Rate. The telemetry bit rate is the number of channels times the sample rate times the bits per word. telemetry

\[B = N_c f_s b \tag{134}\]

Equation 135, Shannon Channel Capacity. The capacity of a noisy channel is the bandwidth times the base-two logarithm of one plus the signal-to-noise ratio. Shannon 1948

\[C = B_w \log_2 \left( 1 + \frac{S}{N} \right) \tag{135}\]

Equation 136, Bespoke Programme Cost Decomposition. The article decomposes programme cost into a development term, a per-flight term and a per-airframe term.

\[C_{\text{total}} = C_{\text{dev}} + n \, C_{\text{flight}} + n_a C_{\text{airframe}} \tag{136}\]

Equation 137, Wright Learning Curve. Unit cost falls by a fixed fraction $b$ for every doubling of cumulative output. Wright 1936

\[C_n = C_1 \, n^{\log_2 b} \tag{137}\]

Equation 138, Bespoke Airframe Count from Binomial Attrition. The article models losses as independent with a constant probability per flight and requires that the programme completes with fewer losses than airframes at a chosen confidence. binomial distribution

\[\sum_{i=0}^{n_a - 1} \binom{n}{i} p^i (1-p)^{n-i} \ge 1 - \alpha \tag{138}\]

Equation 139, Bespoke Expected Losses of the X-1 Example. The expected number of losses is evaluated for 25 flights at a per-flight loss probability of $0.02$ that the article assumes.

\[\mathbb{E}[\text{losses}] = n p = 0.5 \tag{139}\]

Equation 140, Bespoke Required Airframe Count. Three airframes is the smallest number that satisfies the attrition condition at the assumed loss probability and a required confidence of 95 percent.

\[n_a^{*} = 3 \tag{140}\]

Equation 141, Bespoke Programme Justification Condition. The article justifies a programme when the gain in value of the downstream decision from reducing the keystone uncertainty exceeds the total programme cost.

\[V(\sigma_n) - V(\sigma_0) > C_{\text{total}} \tag{141}\]

Equation 142, Expected Value of Sample Information. The expected value of sample information is the expected best utility after observing the data less the best expected utility without it.

\[\text{EVSI} = \mathbb{E}_y \left[ \max_a \mathbb{E}_{\theta \mid y} U(a, \theta) \right] - \max_a \mathbb{E}_\theta U(a, \theta) \tag{142}\]

Equation 143, Marginal Information per Flight. Differentiating the scalar information gain with respect to the flight count shows that each further flight adds less, in proportion to $1/n$ for large $n$.

\[\frac{\partial I_n}{\partial n} = \frac{1}{2} \cdot \frac{\sigma_m^{-2}}{\sigma_0^{-2} + n \sigma_m^{-2}} \tag{143}\]

Equation 144, Bespoke Designation Assignment as a Relation. The article writes the assignment of numbers to programmes as a relation between designations and programmes, with no assumption that it is a function.

\[R \subseteq D \times P \tag{144}\]

Equation 145, Bespoke Assignment Density of the Designation Range. The article defines assignment density as the fraction of the 76 designations in scope that correspond to a programme, with eleven counted as unassigned.

\[\eta = \frac{|D| - |U|}{|D|} = \frac{76 - 11}{76} = 0.855 \tag{145}\]

Equation 146, Bespoke Mean Assignment Rate. The article divides the 65 assigned designations by the 80 years from the X-1 to the X-76 to give a mean rate.

\[\lambda = \frac{|D| - |U|}{\Delta t} = \frac{65}{80} = 0.81 \ \text{per year} \tag{146}\]

Equation 147, Index of Dispersion. The index of dispersion is the sample variance of the counts per interval divided by their mean, near one for a Poisson process.

\[\mathcal{D} = \frac{s^2}{\bar{x}} \tag{147}\]

Notation

• $\theta$, the vector of physical quantities a programme exists to determine
• $\Sigma_n$, the posterior covariance after $n$ flights, with $\Sigma_0$ the prior covariance
• $H_k$, the observation matrix of flight $k$
• $R_k$, the measurement noise covariance of flight $k$
• $\sigma_m$, the standard deviation of a single repeat measurement, with $\sigma_0$ the prior, $\sigma_n$ the posterior and $\sigma_T$ the target
• $I_n$, the information gained after $n$ flights
• $\gamma$, the ratio of specific heats, except in the entry and loss integrals, where $\gamma$ and $\gamma_e$ are flight path angles
• $M$, the Mach number, with $M_\infty$ the free-stream value
• $Re$, the Reynolds number
• $\mu$, the dynamic viscosity, distinct from the Mach angle $\mu_M$ and the mass ratio $\mu_m$
• $p_0$, the stagnation or reservoir pressure, with $T_0$ and $\rho_0$ the stagnation temperature and density
• $Kn$, the Knudsen number
• $\Pi$, the similarity vector of Mach, Reynolds, Prandtl and Damkohler numbers, wall-to-total temperature ratio and Knudsen number
• $\lambda_j$, the Lagrange multiplier, or shadow price, of constraint $j$
• $b_j$, the bound of constraint $j$
• $q$, the dynamic pressure in pascals, distinct from the pitch rate $q$ in the Euler equations
• $C_L$, the lift coefficient, with $C_{L,\max}$ its maximum and $C_{L\alpha}$ the lift-curve slope
• $C_{D0}$, the zero-lift drag coefficient
• $A e$, the product of aspect ratio $A$ and Oswald efficiency number $e$
• $n_{\max}$, the structural limit load factor
• $P_s$, the specific excess power
• $h_e$, the energy height
• $\Lambda$, the sweep angle
• $I_{sp}$, the specific impulse in seconds
• $g_0$, standard gravity
• $\dot{m}$, the propellant mass flow, with $\dot{m}_a$ the captured air mass flow
• $K_\theta$, the torsional stiffness of the wing section
• $q_D$, the divergence dynamic pressure
• $T_r$, the recovery temperature, with $T_w$ the wall temperature
• $\dot{q}_s$, the stagnation-point heat flux
• $R_n$, the effective nose radius
• $\sigma_{SB}$, the Stefan-Boltzmann constant
• $\beta$, the ballistic coefficient
• $H$, the atmospheric scale height
• $SM$, the static margin
• $u_c$, the combined standard uncertainty in Equation 126, distinct from the combustor flow velocity in Equation 82
• $n_a$, the number of airframes built

• $

  U

  $, the number of unassigned designations in the index set $D$

References

Primary Sources, Peer-Reviewed

• “081026 (M10) Maximum Entropy Sampling and Optimal Bayesian Experimental Design.” 1996. Insurance: Mathematics and Economics 18 (2): 139. https://doi.org/10.1016/0167-6687(96)81407-7
• “174 a Synthesis of Reduced-Order H∞ Controllers for Active Flutter Suppression Systems.” 1994. Control Engineering Practice 2 (5): 914. https://doi.org/10.1016/0967-0661(94)90526-6
• “179 Active Control of a Thin Airfoil: Flutter Suppression and Gust Alleviation.” 1994. Control Engineering Practice 2 (5): 915. https://doi.org/10.1016/0967-0661(94)90531-2
• “33. the Ram-Wing Surface Effect Vehicle: Comparison of One-Dimensional Theory with Wind Tunnel and Free Flight Results.” 1973. Journal of Terramechanics 9 (2): 102. https://doi.org/10.1016/0022-4898(73)90209-7
• Abdolahipour, Soheila. 2023. “Effects of Low and High Frequency Actuation on Aerodynamic Performance of a Supercritical Airfoil.” Frontiers in Mechanical Engineering 9: 1290074. https://doi.org/10.3389/fmech.2023.1290074
• Abou-Kebeh, Sami, Roberto Gil-Pita, and Manuel Rosa-Zurera. 2025. “Application of Deep Learning to Identify Flutter Flight Testing Signals Parameters and Analysis of Real F-18 Flutter Flight Test Data.” Aerospace 12 (1): 34. https://doi.org/10.3390/aerospace12010034
• “Active Flutter Suppression via Gain-Scheduled Linear Fractional Control.” 1999. In Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251). IEEE. https://doi.org/10.1109/acc.1999.786286
• Adams, Richard H. 1967. “Wind-Tunnel Simulation of Rocket Vehicles in Flight with Two-Phase-Flow Rocket Plumes.” Journal of Spacecraft and Rockets 4 (4): 518–24. https://doi.org/10.2514/3.28897
• Adams, Donald F. 1974. “High-Performance Composite Material Airframe Weight and Cost Estimating Relations.” Journal of Aircraft 11 (12): 751–57. https://doi.org/10.2514/3.44411
• Agrell, Christian, and Kristina Rognlien Dahl. 2021. “Sequential Bayesian Optimal Experimental Design for Structural Reliability Analysis.” Statistics and Computing 31 (3): 27. https://doi.org/10.1007/s11222-021-10000-2
• Aguilera, Camilo, and Kenneth H. Yu. 2017. “Scramjet to Ramjet Transition in a Dual-Mode Combustor with Fin-Guided Injection.” Proceedings of the Combustion Institute 36 (2): 2911–18. https://doi.org/10.1016/j.proci.2016.06.113
• Ahlefeldt, Thomas. 2017. “Microphone Array Measurement in European Transonic Wind Tunnel at Flight Reynolds Numbers.” AIAA Journal 55 (1): 36–48. https://doi.org/10.2514/1.j055262
• Ahmadi, Majid, and Touraj Farsadi. 2024. “Multidisciplinary Optimization of High Aspect Ratio Composite Wings with Geometrical Nonlinearity and Aeroelastic Tailoring.” Aerospace Science and Technology 145: 108849. https://doi.org/10.1016/j.ast.2023.108849
• Ahmed, Anwar, William H. Wentz, and R. Nyenhuis. 1989. “In-Flight Boundary-Layer Transition Measurements on a Swept Wing.” Journal of Aircraft 26 (11): 979–85. https://doi.org/10.2514/3.45870
• Ailon, Amit. 2007. “Motion Planning and Optimal Control of an Autonomous VTOL Aircraft.” IFAC Proceedings Volumes 40 (15): 13–18. https://doi.org/10.3182/20070903-3-fr-2921.00005
• Al-Jaburi, Khider, Daniel Feszty, and Fred Nitzsche. 2019. “A Methodology for Simulating 2D Shock-Induced Dynamic Stall at Flight Test-Based Fluctuating Freestream.” Chinese Journal of Aeronautics 32 (10): 2223–38. https://doi.org/10.1016/j.cja.2019.05.009
• Alonso Castilla, Raquel, Florent Lutz, Joël Jézégou, and Emmanuel Bénard. 2021. “Wing Structural Model for Overall Aircraft Design of Distributed Electric Propulsion General Aviation and Regional Aircraft.” Aerospace 9 (1): 5. https://doi.org/10.3390/aerospace9010005
• Alsaidi, Bashir, Woong Yeol Joe, and Muhammad Akbar. 2019. “Simplified 2D Skin Lattice Models for Multi-Axial Camber Morphing Wing Aircraft.” Aerospace 6 (8): 90. https://doi.org/10.3390/aerospace6080090
• Alshabu, A., and H. Olivier. 2008. “Unsteady Wave Phenomena on a Supercritical Airfoil.” AIAA Journal 46 (8): 2066–73. https://doi.org/10.2514/1.35516
• Alyanak, Edward J., and Ed Pendleton. 2017. “Aeroelastic Tailoring and Active Aeroelastic Wing Impact on a Lambda Wing Configuration.” Journal of Aircraft 54 (1): 11–19. https://doi.org/10.2514/1.c033040
• Amoozgar, M. R., S. Irani, and G. A. Vio. 2013. “Aeroelastic Instability of a Composite Wing with a Powered-Engine.” Journal of Fluids and Structures 36: 70–82. https://doi.org/10.1016/j.jfluidstructs.2012.10.007
• An, Kai, Zhen-yun Guo, Xiao-ping Xu, and Wei Huang. 2020. “A Framework of Trajectory Design and Optimization for the Hypersonic Gliding Vehicle.” Aerospace Science and Technology 106: 106110. https://doi.org/10.1016/j.ast.2020.106110
• An, Bin, Zhenguo Wang, and Mingbo Sun. 2021. “Ignition Dynamics and Combustion Mode Transitions in a Rocket-Based Combined Cycle Combustor Operating in the Ramjet/scramjet Mode.” Aerospace Science and Technology 118: 106951. https://doi.org/10.1016/j.ast.2021.106951
• Ananda, G. K., P. P. Sukumar, and M. S. Selig. 2015. “Measured Aerodynamic Characteristics of Wings at Low Reynolds Numbers.” Aerospace Science and Technology 42: 392–406. https://doi.org/10.1016/j.ast.2014.11.016
• Andersen, G., E. Forster, R. Kolonay, and F. Eastep. 1997. “Multiple Control Surface Utilization in Active Aeroelastic Wing Technology.” Journal of Aircraft 34 (4): 552–57. https://doi.org/10.2514/2.2208
• Anderson, Barbara, Ethan Chaffee, Bill Perry, and Dave Lopez. 2016. “Low Cost Lighter-than-Air Data Acquisition and Flight Control System.” In 2016 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2016.7500903
• Anderson, M. R., C. Clark, and G. Dungan. 1995. “Flight Test Maneuver Design Using a Skill- and Rule-Based Pilot Model.” In 1995 IEEE International Conference on Systems, Man and Cybernetics. Intelligent Systems for the 21st Century, vol. 3. IEEE. https://doi.org/10.1109/icsmc.1995.538188
• Anderson, L., and J. Vincent. 1985. “Application of System Identification to Aircraft Flight Test Data Processing.” In 1985 24th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1985.268918
• Anderson, Kevin R., Kevin White, and Joe Neal. 2004. “Survey of Active Aeroelastic Control for Flutter Suppression.” In Aerospace. ASMEDC. https://doi.org/10.1115/imece2004-60458
• Ando, Shigenori. 1978. “Aerodynamics of Slender Lifting Surface in Accelerated Flight.” AIAA Journal 16 (7): 751–53. https://doi.org/10.2514/3.7574
• Andrighettoni, M., and P. Mantegazza. 1998. “Multi-Input/Multi-Output Adaptive Active Flutter Suppression for a Wing Model.” Journal of Aircraft 35 (3): 462–69. https://doi.org/10.2514/2.2319
• Arizono, Hitoshi, and Koji Isogai. 2005. “Application of Genetic Algorithm for Aeroelastic Tailoring of a Cranked-Arrow Wing.” Journal of Aircraft 42 (2): 493–99. https://doi.org/10.2514/1.392
• Ashkenas, Irving L. 1984. “Twenty-Five Years of Handling Qualities Research.” Journal of Aircraft 21 (5): 289–301. https://doi.org/10.2514/3.44963
• Atesoglu, Özgür, and M. Kemal Özgören. 2007. “High-Alpha Flight Maneuverability Enhancement of a Fighter Aircraft Using Thrust-Vectoring Control.” Journal of Guidance, Control, and Dynamics 30 (5): 1480–93. https://doi.org/10.2514/1.28620
• Auweter-Kurtz, Monika. 2002. “Plasma Source Development for the Qualification of Thermal Protection Materials for Atmospheric Entry Vehicles at IRS.” Vacuum 65 (3–4): 247–61. https://doi.org/10.1016/s0042-207x(01)00429-8
• Ayaz, Ahsan, Iqbal Rasool Memon, Fahad Ali, et al. 2024. “Aeroelastic Tailoring Framework of Pazy Wing with Variable Stiffness of Composites Spar.” IEEE Access 12: 106042–55. https://doi.org/10.1109/access.2024.3435961
• Bach, Ralph E. 1982. “A Variational Technique for Smoothing Flight-Test and Accident Data.” Journal of Aircraft 19 (7): 546–52. https://doi.org/10.2514/3.57427
• Bach, Ralph E., and Rodney C. Wingrove. 1985. “Applications of State Estimation in Aircraft Flight-Data Analysis.” Journal of Aircraft 22 (7): 547–54. https://doi.org/10.2514/3.45164
• Badihi, Mahdi Ebrahimnejad, Ali Khosravani Nezhad, Amirreza Kosari, and Arash Kosari. 2026. “Two-Stage Design of Experiment Optimization Framework for Morphing Wing of Acrobatic Aircraft.” Journal of Aircraft 63 (5): 2363–78. https://doi.org/10.2514/1.c038688
• Bae, Jae-Sung, T. Michael Seigler, and Daniel J. Inman. 2005. “Aerodynamic and Static Aeroelastic Characteristics of a Variable-Span Morphing Wing.” Journal of Aircraft 42 (2): 528–34. https://doi.org/10.2514/1.4397
• Bailey, A. B., and R. F. Starr. 1976. “Sphere Drag at Transonic Speeds and High Reynolds Numbers.” AIAA Journal 14 (11): 1631–1631. https://doi.org/10.2514/3.7262
• Balazard, Jacqufs. 1972. “Sonic Boom Exposure Effects 1.3: General Considerations on Sonic Boom Research.” Journal of Sound and Vibration 20 (4): 499–503. https://doi.org/10.1016/0022-460x(72)90672-4
• Banerjee, Sanchito. 2019. “Flight Parameter Analysis of an L1 Adaptive Controller of a Hypersonic Glider.” Journal of Aircraft 56 (3): 1149–63. https://doi.org/10.2514/1.c034888
• Bao, Zhongkai, and Lu Chen. 2023. “A Matheuristic Approach for the Aircraft Final Assembly Line Balancing Problem Considering Learning Curve.” In 2023 IEEE International Conference on Industrial Engineering and Engineering Management (IEEM). IEEE. https://doi.org/10.1109/ieem58616.2023.10407009
• Barbante, P. F. 2009. “Heat Flux Duplication between Ground Facility and Hypersonic Flight.” Journal of Thermophysics and Heat Transfer 23 (4): 684–92. https://doi.org/10.2514/1.35808
• Barbante, P. F., and O. Chazot. 2006. “Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield.” Journal of Thermophysics and Heat Transfer 20 (3): 493–99. https://doi.org/10.2514/1.17185
• Bartels, Robert E., Christie J. Funk, and Robert C. Scott. 2017. “Limit-Cycle Oscillation of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Aeroelastic Model.” Journal of Aircraft 54 (5): 1605–13. https://doi.org/10.2514/1.c034064
• Barthelemy, R. 1989b. “Recent Progress in the National Aerospace Plane Program.” IEEE Aerospace and Electronic Systems Magazine 4 (5): 3–12. https://doi.org/10.1109/62.31806
• Bartuska, Arved, Luis Espath, and Raúl Tempone. 2022. “Small-Noise Approximation for Bayesian Optimal Experimental Design with Nuisance Uncertainty.” Computer Methods in Applied Mechanics and Engineering 399: 115320. https://doi.org/10.1016/j.cma.2022.115320
• Bartuska, Arved, Luis Espath, and Raúl Tempone. 2024. “Laplace-Based Strategies for Bayesian Optimal Experimental Design with Nuisance Uncertainty.” Statistics and Computing 35 (1): 12. https://doi.org/10.1007/s11222-024-10544-z
• Basappa, Jatinder Singh, and J. Raol. 2006. “Parameter Estimation Using Large Amplitude Data from Real Time Simulator of an Aircraft.” In 2006 Canadian Conference on Electrical and Computer Engineering. IEEE. https://doi.org/10.1109/ccece.2006.277559
• Bashkirov, Igor G., Vladlen S. Gorbovskoy, Andrey V. Kazhan, Vyacheslav G. Kazhan, and Sergey L. Chernyshev. 2021. “Analysis of the Influence of Wave Spectral Structure on the Sonic Boom Loudness of the NASA X-59 Low Boom Demonstrator.” In 2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae52228.2021.9522371
• Batterson, James G., and Vladislav Klein. 1989. “Partitioning of Flight Data for Aerodynamic Modeling of Aircraft at High Angles of Attack.” Journal of Aircraft 26 (4): 334–39. https://doi.org/10.2514/3.45765
• Bauersfeld, L., and G. Ducard. 2020. “Fused-PID Control for Tilt-Rotor VTOL Aircraft.” In 2020 28th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med48518.2020.9183031
• Baumann, J. M., and C. R. Bisbee. 1988. “A System Status Monitor for the National Aero-Space Plane.” In Proceedings of the IEEE 1988 National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1988.195203
• Bean, D. E., and B. H. K. Lee. 1995. “Correlation of F/A-18 Buffeting from Wind-Tunnel and Flight Tests.” Journal of Aircraft 32 (6): 1351–58. https://doi.org/10.2514/3.46885
• Beck, Joakim, Ben Mansour Dia, Luis F. R. Espath, Quan Long, and Raúl Tempone. 2018. “Fast Bayesian Experimental Design: Laplace-Based Importance Sampling for the Expected Information Gain.” Computer Methods in Applied Mechanics and Engineering 334: 523–53. https://doi.org/10.1016/j.cma.2018.01.053
• Becker, John V. 1950. “Results of Recent Hypersonic and Unsteady Flow Research at the Langley Aeronautical Laboratory.” Journal of Applied Physics 21 (7): 619–28. https://doi.org/10.1063/1.1699720
• Belák, Jan, and Martin Hromčík. 2023b. “Unified Attitude Control Strategy for Tilt-Rotor VTOL Aircraft.” In 2023 American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc55779.2023.10156090
• Belchihina, Alexandra V., Andrey V. Kazhan, Dmitry I. Gilyazev, and Sergey A. Kuzin. 2021. “Analysis of the Flow Features and Evaluation of the Aerodynamic Characteristics of the NASA X-59 Low Boom Demonstrator.” In 2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae52228.2021.9522549
• Beltramo, Michael N. 1985. “A Critical Look at the Development and Application of Airframe Cost Estimating Models.” Journal of Parametrics 5 (2): 91–99. https://doi.org/10.1080/10157891.1985.10462654
• Benders, Sebastian, Andreas Wenz, and Tor Arne Johansen. 2018. “Adaptive Path Planning for Unmanned Aircraft Using in-Flight Wind Velocity Estimation.” In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2018.8453341
• Benedikt, Elliot T. 1953. “Open-Nose Body of Revolution of Minimum Drag at Small Supersonic Speeds.” Journal of the Aeronautical Sciences 20 (10): 720–22. https://doi.org/10.2514/8.2809
• Bennett, Robert M., and Irving Abel. 1982. “Flight Flutter Test and Data Analysis Techniques Applied to a Drone Aircraft.” Journal of Aircraft 19 (7): 589–95. https://doi.org/10.2514/3.57433
• Benyamen, Hady, and Shawn Keshmiri. 2022. “Flight Test Validation Verification of @AIR Distributed Electric Propulsion Aircraft Dynamic Model.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836206
• Benyamen, Hady, Benjamin S. Mays, Mozammal Chowdhury, Shawn Keshmiri, and Mark S. Ewing. 2023. “Analysis of Aircraft Simulation Validity in Different Flight Conditions.” In 2023 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas57906.2023.10156586
• Bhatia, Manav, Rakesh K. Kapania, and Raphael T. Haftka. 2012. “Structural and Aeroelastic Characteristics of Truss-Braced Wings: A Parametric Study.” Journal of Aircraft 49 (1): 302–10. https://doi.org/10.2514/1.c031556
• Bian, Qi, Brett Nener, and Xinmin Wang. 2019. “A Quantum Inspired Genetic Algorithm for Multimodal Optimization of Wind Disturbance Alleviation Flight Control System.” Chinese Journal of Aeronautics 32 (11): 2480–88. https://doi.org/10.1016/j.cja.2019.04.013
• Billig, F. S. 1993. “Research on Supersonic Combustion.” Journal of Propulsion and Power 9 (4): 499–514. https://doi.org/10.2514/3.23652
• Binder, Simon, Andreas Wildschek, and Roeland De Breuker. 2021. “The Interaction between Active Aeroelastic Control and Structural Tailoring in Aeroservoelastic Wing Design.” Aerospace Science and Technology 110: 106516. https://doi.org/10.1016/j.ast.2021.106516
• Bingyan, Chen, Liu Zhou, and Gong Anlong. 2015. “Aerodynamic Configuration Design of Flight Demonstrator for Real Gas Effect.” Procedia Engineering 99: 116–28. https://doi.org/10.1016/j.proeng.2014.12.515
• Bisplinghoff, R. L. 1964. “The Supersonic Transport.” Scientific American 210 (6): 25–35. https://doi.org/10.1038/scientificamerican0664-25
• Black, Robert L. 1969. “High-Speed Store Separation: Correlation between Wind-Tunnel and Flight-Test Data.” Journal of Aircraft 6 (1): 42–45. https://doi.org/10.2514/3.43999
• Blair, Maxwell, and Terrence A. Weisshaar. 1982. “Swept Composite Wing Aeroelastic Divergence Experiments.” Journal of Aircraft 19 (11): 1019–24. https://doi.org/10.2514/3.44806
• Blanchard, Robert C. 1991. “Rarefied-Flow Aerodynamics Measurement Experiment on the Aeroassist Flight Experiment Vehicle.” Journal of Spacecraft and Rockets 28 (4): 368–75. https://doi.org/10.2514/3.26256
• Bland, Samuel R. 1980. “Illustration of Airfoil Shape Effect on Forward-Swept Wing Divergence.” Journal of Aircraft 17 (10): 761–63. https://doi.org/10.2514/3.44684
• Bo, Zhang, Shi Zhongke, and Li Jianjun. 2007. “Flight Flutter Modal Parameters Identification with Atmospheric Turbulence Excitation Based on Wavelet Transformation.” Chinese Journal of Aeronautics 20 (5): 394–401. https://doi.org/10.1016/s1000-9361(07)60060-0
• Bohlmann, Jonathan D., Clinton V. Eckstrom, and Terrence A. Weisshaar. 1990. “Static Aeroelastic Tailoring for Oblique Wing Lateral Trim.” Journal of Aircraft 27 (6): 558–63. https://doi.org/10.2514/3.25319
• Bohn-Meyer, M., S. Kilp, and P. Chun. 2005. “Doing Systems Engineering without Thinking about It at NASA Dryden Flight Research Center.” In 2005 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2005.1559741
• Böhrk, Hannah. 2015. “Transpiration-Cooled Hypersonic Flight Experiment: Setup, Flight Measurement, and Reconstruction.” Journal of Spacecraft and Rockets 52 (3): 674–83. https://doi.org/10.2514/1.a33144
• Borglund, Dan. 2001. “Aeroservoelastic Design Optimization with Experimental Verification.” Journal of Aircraft 38 (5): 958–61. https://doi.org/10.2514/2.2860
• Borglund, D., and J. Kuttenkeuler. 2002. “Active Wing Flutter Suppression Using a Trailing Edge Flap.” Journal of Fluids and Structures 16 (3): 271–94. https://doi.org/10.1006/jfls.2001.0426
• Bowers, Douglas L. 1981. “Propulsive Aerodynamics of an Advanced Nozzle/Forward Swept Wing Aircraft Configuration.” Journal of Aircraft 18 (7): 582–86. https://doi.org/10.2514/3.57530
• Bradley, P. F., P. M. Siemers, and K. James Weilmuenster. 1982. “Comparison of Shuttle Flight Pressure Data to Computational and Wind-Tunnel Results.” Journal of Spacecraft and Rockets 19 (5): 419–22. https://doi.org/10.2514/3.62279
• Brajou, F., and P. Ricco. 2005. “AFDX-Based Flight Test Computer Concept.” IEEE Instrumentation & Measurement Magazine 8 (3): 55–58. https://doi.org/10.1109/mim.2005.1502451
• Brandon, Jay M., and Eugene A. Morelli. 2016. “Real-Time Onboard Global Nonlinear Aerodynamic Modeling from Flight Data.” Journal of Aircraft 53 (5): 1261–97. https://doi.org/10.2514/1.c033133
• Bras, M., S. Warwick, and A. Suleman. 2022. “Aeroelastic Evaluation of a Flexible High Aspect Ratio Wing UAV: Numerical Simulation and Experimental Flight Validation.” Aerospace Science and Technology 122: 107400. https://doi.org/10.1016/j.ast.2022.107400
• Bravo, Guillem Moreno, Nurgeldy Praliyev, and Árpád Veress. 2021. “Performance Analysis of Hybrid Electric and Distributed Propulsion System Applied on a Light Aircraft.” Energy 214: 118823. https://doi.org/10.1016/j.energy.2020.118823
• Brcich, R. F., and A. M. Zoubir. n.d. “The Use of the DPT in Passive Acoustic Aircraft Flight Parameter Estimation.” In TENCON ‘97 Brisbane - Australia. Proceedings of IEEE TENCON ‘97. IEEE Region 10 Annual Conference. Speech and Image Technologies for Computing and Telecommunications (Cat. No.97CH36162), vol. 2. IEEE. https://doi.org/10.1109/tencon.1997.648549
• Breitsamter, Christian, and Boris Laschka. 2001. “Vortical Flowfield Structure at Forward Swept-Wing Configurations.” Journal of Aircraft 38 (2): 193–207. https://doi.org/10.2514/2.2758
• Bridges, David H. 2007. “Early Flight-Test and Other Boundary-Layer Research at Mississippi State 1949-1960.” Journal of Aircraft 44 (5): 1635–52. https://doi.org/10.2514/1.28086
• Browne, Oliver M. F., Daniel Maldonado, Jeffrey A. Housman, Jared C. Duensing, and William E. Milholen. 2025. “Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft.” Journal of Aircraft 62 (1): 62–80. https://doi.org/10.2514/1.c037981
• Brunner, Claudia E., Janik Kiefer, Martin O. L. Hansen, and Marcus Hultmark. 2021. “Study of Reynolds Number Effects on the Aerodynamics of a Moderately Thick Airfoil Using a High-Pressure Wind Tunnel.” Experiments in Fluids 62 (8): 178. https://doi.org/10.1007/s00348-021-03267-8
• Bu, Xiangwei, and Haiying Ma. 2023. “Adaptive Critic Design for Enhanced Control of Waverider Vehicles with Nonaffine Nonlinearities.” Nonlinear Dynamics 112 (2): 1123–39. https://doi.org/10.1007/s11071-023-09085-3
• Budd, Gerald D., Ronald L. Gilman, and David Eichstedt. 1995. “Operational and Research Aspects of a Radio-Controlled Model Flight Test Program.” Journal of Aircraft 32 (3): 583–89. https://doi.org/10.2514/3.46759
• Bulmer, Bruce M. 1975. “Study of Base Pressure in Laminar Hypersonic Flow: Re-Entry Flight Measurements.” AIAA Journal 13 (10): 1340–48. https://doi.org/10.2514/3.60546
• Bulygina, E. B. 1958. “On the Problem of a Wing of a Given Volume with Minimum Wave Drag.” Journal of Applied Mathematics and Mechanics 22 (6): 1180–84. https://doi.org/10.1016/0021-8928(58)90043-1
• Burchett, B. T. 2005. “Feedback Linearization Guidance for Approach and Landing of Reusable Launch Vehicles.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1470279
• Burken, John J. 1993. “Flight-Determined Multivariable Stability Analysis and Comparison of a Control System.” Journal of Guidance, Control, and Dynamics 16 (6). https://ntrs.nasa.gov/citations/19940034150
• Butefisch, Karl A., and Egon Stanewsky. 1987. “Experimental Flowfield Study on a Supercritical Airfoil.” Journal of Aircraft 24 (11): 783–88. https://doi.org/10.2514/3.45521
• Byun, Jong-Ryul, and Jaewon Kim. 2026. “Experimental Investigation for the Effect of Fueling Distribution on the Combustion Mode of a Dual-Mode Scramjet Combustor.” Aerospace Science and Technology 176: 112144. https://doi.org/10.1016/j.ast.2026.112144
• Cai, Jinxu, Juanzhang Xie, Lanxin Zhang, Ziyi Wang, Xueshun Li, and Yongjun Zhao. 2026. “EA-TD3: An Energy-Aware Autonomous Trajectory Planning Method for Unmanned Electric Vertical Takeoff and Landing Aircraft.” Drones 10 (5): 325. https://doi.org/10.3390/drones10050325
• Calarese, Wladimiro, and Ronald E. Walterick. 1979. “Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag.” Journal of Aircraft 16 (7): 433–40. https://doi.org/10.2514/3.58545
• Calise, A. J., J. E. Corban, and G. A. Flandro. 1988. “Trajectory Optimization and Guidance Law Development for National Aerospace Plane Applications.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789941
• Campbell and Kresge. 2003. “Brumby Uninhabited Aerial Vehicle Flight Dynamics-Instrumentation and Flight Test Results.” In 22nd Digital Avionics Systems Conference Proceedings (Cat No 03CH37449) DASC-03. IEEE. https://doi.org/10.1109/dasc.2003.1245892
• Cao, R. F., J. T. Chang, J. F. Tang, Z. Q. Wang, and D. R. Yu. 2014. “Study on Combustion Mode Transition of Hydrogen Fueled Dual-Mode Scramjet Engine Based on Thermodynamic Cycle Analysis.” International Journal of Hydrogen Energy 39 (36): 21251–58. https://doi.org/10.1016/j.ijhydene.2014.10.082
• Cao, Ruifeng, Yue Lu, Daren Yu, and Juntao Chang. 2020. “Study on Influencing Factors of Combustion Mode Transition Boundary for a Scramjet Engine Based on One-Dimensional Model.” Aerospace Science and Technology 96: 105590. https://doi.org/10.1016/j.ast.2019.105590
• Caplin, J. n.d. “Descent-Phase Control of a Reusable Launch Vehicle.” In Proceedings. The 21st Digital Avionics Systems Conference, vol. 2. IEEE. https://doi.org/10.1109/dasc.2002.1052960
• Carlon, André Gustavo, Cibelle Dias de Carvalho Dantas Maia, Rafael Holdorf Lopez, André Jacomel Torii, and Leandro Fleck Fadel Miguel. 2023. “A Polynomial Chaos Efficient Global Optimization Approach for Bayesian Optimal Experimental Design.” Probabilistic Engineering Mechanics 72: 103454. https://doi.org/10.1016/j.probengmech.2023.103454
• Cavagna, L., S. Ricci, and L. Riccobene. 2011. “Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design.” Journal of Aircraft 48 (6): 1840–55. https://doi.org/10.2514/1.c031072
• Cavagna, L., S. Ricci, and A. Scotti. 2009a. “Active Aeroelastic Control over a Four Control Surface Wing Model.” Aerospace Science and Technology 13 (7): 374–82. https://doi.org/10.1016/j.ast.2009.06.009
• Celenligil, M. Cevdet, James N. Moss, and Robert C. Blanchard. 1991. “Three-Dimensional Rarefied Flow Simulations for the Aeroassist Flight Experiment Vehicle.” AIAA Journal 29. https://ntrs.nasa.gov/citations/19910039959
• Cen, Fei, Qing Li, Litao Fan, Zhitao Liu, and Haisheng Sun. 2015. “Development of a Pilot-in-Loop Real-Time Simulation Platform for Wind Tunnel Free-Flight Test.” In 2015 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2015.7279694
• Cetinsoy, Ertugrul. 2015. “Design and Control of a Gas-Electric Hybrid Quad Tilt-Rotor UAV with Morphing Wing.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152278
• Chai, Yu-Yang, Zhi-Guang Song, and Feng-Ming Li. 2017. “Active Aerothermoelastic Flutter Suppression of Composite Laminated Panels with Time-Dependent Boundaries.” Composite Structures 179: 61–76. https://doi.org/10.1016/j.compstruct.2017.07.053
• Chakraborty, Imon, Taewoo Nam, Jonathan R. Gross, Dimitri N. Mavris, Joseph A. Schetz, and Rakesh K. Kapania. 2015. “Comparative Assessment of Strut-Braced and Truss-Braced Wing Configurations Using Multidisciplinary Design Optimization.” Journal of Aircraft 52 (6): 2009–20. https://doi.org/10.2514/1.c033120
• Chan, Jia Cheng, Henrik Hesse, and Peng Cheng Wang. 2025. “LES Validation on near-Field Wingtip Vortex Evolution with Wind Tunnel Characterization at Low Reynolds Number.” Aerospace Science and Technology 157: 109789. https://doi.org/10.1016/j.ast.2024.109789
• Chapman, Dean R., and Morris W. Rubesin. 1949. “Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature.” Journal of the Aeronautical Sciences 16 (9): 547–65. https://doi.org/10.2514/8.11853
• Chau, Timothy, Michael G. Piotrowski, and Jared C. Duensing. 2026. “Aerodynamic Optimization of a Cruise-Slotted Transonic Truss-Braced-Wing Aircraft Configuration.” Journal of Aircraft: 1–18. https://doi.org/10.2514/1.c038646
• Chau, Timothy, and David W. Zingg. 2022. “Aerodynamic Design Optimization of a Transonic Strut-Braced-Wing Regional Aircraft.” Journal of Aircraft 59 (1): 253–71. https://doi.org/10.2514/1.c036389
• Chau, Timothy, and David W. Zingg. 2023. “Aerodynamic Optimization and Fuel Burn Evaluation of a Transonic Strut-Braced-Wing Single-Aisle Aircraft.” Journal of Aircraft 60 (5): 1638–58. https://doi.org/10.2514/1.c037158
• Che, Jing, and Shuo Tang. 2008. “Research on Integrated Optimization Design of Hypersonic Cruise Vehicle.” Aerospace Science and Technology 12 (7): 567–72. https://doi.org/10.1016/j.ast.2008.01.008
• Chen, Q., L. H. Chen, H. B. Gu, X. Y. Zhang, and P. Wang. 2013. “Study on Judgment Method of Combustion Mode on Dual-Mode Scramjet.” Procedia Engineering 67: 147–54. https://doi.org/10.1016/j.proeng.2013.12.014
• Chen, Lili, Zheng Guo, Xiaolong Deng, Zhongxi Hou, and Wenkai Wang. 2019. “Waverider Configuration Design with Variable Shock Angle.” IEEE Access 7: 42081–93. https://doi.org/10.1109/access.2019.2907806
• Chen, Ziyi, Duoneng Liu, Zhongxi Hou, and Suqi Chen. 2025. “Mission-Oriented Propulsion System Configuration and Whole Aircraft Redundancy Safety Performance for Distributed Electric Propulsion UAVs.” Drones 9 (9): 662. https://doi.org/10.3390/drones9090662
• Chen, Yifu, Hanyue Rao, Yiju Deng, Tihao Yang, Yayun Shi, and Junqiang Bai. 2023c. “Adjoint-Based Robust Optimization Design of Laminar Flow Wing under Flight Condition Uncertainties.” Chinese Journal of Aeronautics 36 (6): 19–34. https://doi.org/10.1016/j.cja.2023.03.039
• Chen, Jie, and Zhongke Shi. 2011. “Flight Controller Design of Transport Airdrop.” Chinese Journal of Aeronautics 24 (5): 600–606. https://doi.org/10.1016/s1000-9361(11)60070-8
• Chen, Zhiming, Fei Xue, Haichuan Yu, et al. 2023d. “Derivation and Validation of a Similarity Law for Free-Flight Wind Tunnel Tests of Parallel Stage Separation.” Chinese Journal of Aeronautics 36 (8): 91–100. https://doi.org/10.1016/j.cja.2023.02.010
• Chen, Keting, Lianjie Yue, and Xinyu Chang. 2018. “Comment on “Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment”.” Journal of Propulsion and Power 34 (2): 550–51. https://doi.org/10.2514/1.b36702
• Cheng, Zeyu, Zhi Cao, Chris Mi, and John T. Hwang. 2025. “Cost Optimization of Electric Vertical Takeoff and Landing Aircraft through Powertrain Modeling.” Journal of Air Transportation 33 (3): 285–96. https://doi.org/10.2514/1.d0487
• Cheng, Yuwei, Qian Chen, Xiaofei Niu, and Shufeng Cai. 2023b. “Large Eddy Simulation and Dynamic Mode Decomposition of Supersonic Combustion Instability in a Strut-Based Scramjet Combustor.” Aerospace 10 (10): 857. https://doi.org/10.3390/aerospace10100857
• Cheng, Lingquan, Yiyang Li, Jiayi Yuan, Jianliang Ai, and Yiqun Dong. 2023a. “L1 Adaptive Control Based on Dynamic Inversion for Morphing Aircraft.” Aerospace 10 (9): 786. https://doi.org/10.3390/aerospace10090786
• Cho, Yongseung, and M. G. Nagati. 1998. “Coupled Force and Moment Parameter Estimation for Aircraft.” Journal of Aircraft 35 (2): 247–53. https://doi.org/10.2514/2.2291
• Choi, HaRyun, Byron YooHo Chang, Yeongmin Jo, and SangJoon Shin. 2026. “Rotor Sizing Effects on a Tiltwing Electric Vertical Takeoff and Landing Vehicle.” Journal of Aircraft: 1–15. https://doi.org/10.2514/1.c038503
• Chowdhary, Girish, and Ravindra Jategaonkar. 2010. “Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter.” Aerospace Science and Technology 14 (2): 106–17. https://doi.org/10.1016/j.ast.2009.10.003
• Chowdhury, Mozammal, and Shawn Keshmiri. 2024. “A Unified Inner-Outer Loop Reinforcement Learning Flight Controller for Fixed-Wing Aircraft.” In 2024 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas60882.2024.10556883
• Chuanzhen, Liu, and Bai Peng. 2021. “Mathematical Expression of Geometric Relationship in Osculating-Cone Waverider Design.” Journal of Aircraft 58 (4): 858–66. https://doi.org/10.2514/1.c036122
• Chuanzhen, Liu, Meng Xufei, and Bai Peng. 2022. “Design and Analysis of Double-Swept Waverider with Wing Dihedral.” AIAA Journal 60 (4): 2075–84. https://doi.org/10.2514/1.j060706
• Cicala, Placido, and Angelo Miele. 1956. “Generalized Theory of the Optimum Thrust Programming for the Level Flight of a Rocket-Powered Aircraft.” Journal of Jet Propulsion 26 (6): 443–55. https://doi.org/10.2514/8.7047
• Clark, A. B. J., and F. T. Harris. 1952. “Free-Flight Air-Drag Measurement Techniques.” Journal of the Aeronautical Sciences 19 (6): 385–90. https://doi.org/10.2514/8.2303
• Clarke, J. F. 1982. “Similitude and Modelling.” Journal of Wind Engineering and Industrial Aerodynamics 10 (1): 133–34. https://doi.org/10.1016/0167-6105(82)90059-9
• Clodman, J. 1968. “Terminal Forecasting and Supersonic Transport.” Atmosphere 6 (1): 1–7. https://doi.org/10.1080/00046973.1968.9676542
• Cochrane, John A., Dennis W. Riddle, Victor C. Stevens, and Michael D. Shovlin. 1982. “Selected Results from the Quiet Short-Haul Research Aircraft Flight Research Program.” Journal of Aircraft 19 (12): 1076–82. https://doi.org/10.2514/3.44814
• Cole, Stanley R. 1988. “Divergence Study of a High-Aspect-Ratio, Forward Swept Wing.” Journal of Aircraft 25 (5): 478–80. https://doi.org/10.2514/3.45609
• Comer, Anthony, Imon Chakraborty, Stefanus Harris Putra, Rajan Bhandari, Bikash Kunwar, and Benjamin Davis. 2026b. “Flight Testing a Trajectory Control System on a Subscale Transitioning VTOL Aircraft.” Journal of Guidance, Control, and Dynamics 49 (2): 459–78. https://doi.org/10.2514/1.g009060
• Comunian, Paolo, Jacopo Serpieri, and Gioacchino Cafiero. 2026. “A Numerical Framework for Multiparametric Optimization of Distributed Electric Propulsion.” Journal of Aircraft 63 (5): 2089–99. https://doi.org/10.2514/1.c038541
• Cong, Wang, and Lu Kunfeng. 2017. “Control Surface Optimization of Hypersonic Vehicle Based on Adaptive Backstepping Method.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027876
• Contreras-Torres, G. A. S., R. Garcia-Rodriguez, C. R. Dominguez-Mayorga, and E. S. Espinoza. 2022. “Adaptive Backstepping Control for the Longitudinal Flight of a Blended Wing Body Aircraft.” In 2022 19th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE). IEEE. https://doi.org/10.1109/cce56709.2022.9975869
• Cooper, J. E. 1990. “Comparison of Modal Parameter Estimation Techniques on Aircraft Structural Data.” Mechanical Systems and Signal Processing 4 (2): 157–72. https://doi.org/10.1016/0888-3270(90)90054-o
• “A Correlation between Rain Erosion of Perspex Specimens in Flight and on a Ground Rig.” 1959. Wear 2 (6): 498. https://doi.org/10.1016/0043-1648(59)90232-7
• “A Correlation between Rain Erosion of Perspex Specimens in Flight and on Ground Rig.” 1960. Wear 3 (6): 485. https://doi.org/10.1016/0043-1648(60)90274-x
• Cosentino, Gary B. 1983. “Modifying a General Aviation Airfoil for Supercritical Flight.” Journal of Aircraft 20 (4): 377–79. https://doi.org/10.2514/3.44879
• Coskun, Baris, and Burkay Genc. 2021. “Estimating Instrumentation Data Acquired during Flight Test of a Helicopter Using Predictor Models.” In IEEE EUROCON 2021 - 19th International Conference on Smart Technologies. IEEE. https://doi.org/10.1109/eurocon52738.2021.9535625
• Costello, Donald H., Jason Jewell, and Huan Xu. 2021. “Autonomous Flight-Test Data in Support of Safety of Flight Certification.” Journal of Air Transportation 29 (2): 93–106. https://doi.org/10.2514/1.d0220
• Crossley, William A., Michael D. Skillen, Joshua B. Frommer, and Brian D. Roth. 2011. “Morphing Aircraft Sizing Using Design Optimization.” Journal of Aircraft 48 (2): 612–22. https://doi.org/10.2514/1.c031180
• Cui, Kai, ShouChao Hu, GuangLi Li, ZhiPeng Qu, and Ming Situ. 2013. “Conceptual Design and Aerodynamic Evaluation of Hypersonic Airplane with Double Flanking Air Inlets.” Science China Technological Sciences 56 (8): 1980–88. https://doi.org/10.1007/s11431-013-5288-0
• Cummings, Russell M., and Andreas Schütte. 2012. “Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation.” Journal of Aircraft 49 (6): 1542–57. https://doi.org/10.2514/1.c031430
• Cunis, Torbjorn, Tobias Leth, Luminita C. Totu, and Anders la Cour-Harbo. 2018. “Identification of Thrust, Lift, and Drag for Deep-Stall Flight Data of a Fixed-Wing Unmanned Aircraft.” In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2018.8453340
• Curran, Edward T. 2001. “Scramjet Engines: The First Forty Years.” Journal of Propulsion and Power 17 (6): 1138–48. https://doi.org/10.2514/2.5875
• Curran, Damian, Vincent Wheatley, and Michael Smart. 2019. “Investigation of Combustion Mode Control in a Mach 8 Shape-Transitioning Scramjet.” AIAA Journal 57 (7): 2977–88. https://doi.org/10.2514/1.j057999
• Curry, Robert E., and Alex G. Sim. 1983. “Unique Flight Characteristics of the AD-1 Oblique-Wing Research Airplane.” Journal of Aircraft 20 (6): 564–68. https://doi.org/10.2514/3.44909
• Cusati, Vincenzo, Salvatore Corcione, Fabrizio Nicolosi, and Qinyin Zhang. 2023. “Improvement of Take-Off Performance for an Electric Commuter Aircraft Due to Distributed Electric Propulsion.” Aerospace 10 (3): 276. https://doi.org/10.3390/aerospace10030276
• Cutler, Andrew D., Emanuela C. A. Gallo, Luca M. L. Cantu, Robert D. Rockwell, and Christopher P. Goyne. 2018. “Coherent Anti-Stokes Raman Spectroscopy of a Premixed Ethylene–air Flame in a Dual-Mode Scramjet.” Combustion and Flame 189: 92–105. https://doi.org/10.1016/j.combustflame.2017.10.028
• Cutright, C. A., and N. S. Braasch. n.d. “GPS and INS Flight Test Instrumentation of a Fully Aerobatic Turbojet Aircraft.” In Proceedings, IEEE Aerospace Conference, vol. 3. IEEE. https://doi.org/10.1109/aero.2002.1035269
• Dai, Wei, Runyu Lu, and Liang Gao. 2026. “Research on Modal Analysis Methods for Flutter Flight Testing.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00468-z
• Davey, Keith, and Raul Ochoa-Cabrero. 2023. “Extended Finite Similitude and Dimensional Analysis for Scaling.” Journal of Engineering Mathematics 143 (1): 3. https://doi.org/10.1007/s10665-023-10296-1
• Davidson, Theron W. 1964. “Measurement of Net Thrust in Flight.” Journal of Aircraft 1 (3): 107–13. https://doi.org/10.2514/3.43575
• Davis, John W. 1968a. “A High Reynolds Number Wind Tunnel and Its Operating Concept.” Journal of Spacecraft and Rockets 5 (10): 1225–27. https://doi.org/10.2514/3.29455
• Davis, Lance A. 2017. “Supersonic Transport Redux?” Engineering 3 (6): 785–86. https://doi.org/10.1016/j.eng.2017.12.008
• Davis, Mark C., and J. Terry White. 2008. “X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0.” Journal of Spacecraft and Rockets 45 (3). https://ntrs.nasa.gov/citations/20080021260
• Dawkins, Jeremy J., Frederick L. Crabbe, and Dennis Evangelista. 2018. “Deployment and Flight Operations of a Large Scale UAS Combat Swarm: Results from DARPA Service Academies Swarm Challenge.” In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2018.8453456
• de Carvalho Dantas Maia, Cibelle Dias, Rafael Holdorf Lopez, André Jacomel Torii, and Leandro Fleck Fadel Miguel. 2025. “A Two Stage Kriging Approach for Bayesian Optimal Experimental Design.” Probabilistic Engineering Mechanics 79: 103724. https://doi.org/10.1016/j.probengmech.2024.103724
• de Try, Fredrik. 2004. “Estimation of Flight Load History Using a Global Positioning System Data.” Journal of Aircraft 41 (2): 418–20. https://doi.org/10.2514/1.5798
• de Visser, Coen C., and Daan M. Pool. 2023. “Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification.” Journal of Aircraft 60 (5): 1480–1502. https://doi.org/10.2514/1.c037283
• de Vries, Reynard, Malcom Brown, and Roelof Vos. 2019a. “Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft.” Journal of Aircraft 56 (6): 2172–88. https://doi.org/10.2514/1.c035388
• de Vries, Reynard, and Roelof Vos. 2023. “Aerodynamic Performance Benefits of over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft.” Journal of Aircraft 60 (4): 1201–18. https://doi.org/10.2514/1.c036909
• Dean, Angela M. 1982. “Optimal Design: An Introduction to the Theory for Parameter Estimation.” Technometrics 24 (2): 168–168. https://doi.org/10.1080/00401706.1982.10487752
• DeAngelis, V. Michael. 1982. “In-Flight Deflection Measurement of the HiMAT Aeroelastically Tailored Wing.” Journal of Aircraft 19 (12): 1088–94. https://doi.org/10.2514/3.44816
• Deck, Sébastien. 2005. “Numerical Simulation of Transonic Buffet over a Supercritical Airfoil.” AIAA Journal 43 (7): 1556–66. https://doi.org/10.2514/1.9885
• Deepak, N. R., T. Ray, and R. R. Boyce. 2008. “Evolutionary Algorithm Shape Optimization of a Hypersonic Flight Experiment Nose Cone.” Journal of Spacecraft and Rockets 45 (3): 428–37. https://doi.org/10.2514/1.33826
• Deepak, Kanishka, Aaditya U. Wangikar, G. R. Chathura, et al. 2022. “Optimization of Conceptual Design of Air Breathing Hypersonic Vehicle.” In 2022 IEEE Aerospace Conference (AERO). IEEE. https://doi.org/10.1109/aero53065.2022.9843693
• Denegri, Charles M., James A. Dubben, and Sergey L. Kernazhitskiy. 2013. “Underwing Missile Aerodynamic Effects on Flight-Measured Limit-Cycle Oscillations.” Journal of Aircraft 50 (5): 1637–45. https://doi.org/10.2514/1.c032216
• Deng, Zexiao, Luhua Liu, and Yujia Wang. 2024. “Entry Trajectory Optimization of Lifting-Body Vehicle by Successive Difference-of-Convex Programming.” Advances in Space Research 74 (11): 5837–59. https://doi.org/10.1016/j.asr.2024.08.021
• Deng, Feng, and Ning Qin. 2021. “Vortex-Generating Shock Control Bumps for Robust Drag Reduction at Transonic Speeds.” AIAA Journal 59 (10): 3900–3909. https://doi.org/10.2514/1.j060528
• Deng, S., and Tsung-Han Yeh. 2009. “2.2.3 Applying Machine Learning Methods to the Airframe Structural Design Cost Estimation – a Case Study of Wing-Box Project.” INCOSE International Symposium 19 (1): 253–82. https://doi.org/10.1002/j.2334-5837.2009.tb00948.x
• Deng, S., and Tsung-Han Yeh. 2010. “Applying Least Squares Support Vector Machines to the Airframe Wing-Box Structural Design Cost Estimation.” Expert Systems with Applications 37 (12): 8417–23. https://doi.org/10.1016/j.eswa.2010.05.038
• Deng, S., and Tsung-Han Yeh. 2011. “Using Least Squares Support Vector Machines for the Airframe Structures Manufacturing Cost Estimation.” International Journal of Production Economics 131 (2): 701–8. https://doi.org/10.1016/j.ijpe.2011.02.019
• Deng, Dawei, and Haiwen Yuan. 2015. “UAV Flight Safety Ground Test and Evaluation.” In 2015 IEEE Autotestcon. IEEE. https://doi.org/10.1109/autest.2015.7356527
• Der Kiureghian, Armen. 2001. “Risk Assessment of Satellite Launch with Reusable Launch Vehicle.” Reliability Engineering & System Safety 74 (3): 353–60. https://doi.org/10.1016/s0951-8320(01)00084-9
• Derienzo, Philip, and Adrian J. Pallone. 1967. “Convective Stagnation-Point Heating for Re- Entry Speeds up to 70,000 Fps Including Effects of Large Blowing Rates.” AIAA Journal 5 (2): 193–200. https://doi.org/10.2514/3.3942
• Desai, S. S., S. Viswanathan, and M. A. Ramaswamy. 1977. “Numerical Evaluation of Transonic Wave Drag.” Journal of Aircraft 14 (2): 215–17. https://doi.org/10.2514/3.44585
• Deshpande, Sunil, and Daniel E. Rivera. 2013. “Optimal Input Signal Design for Data-Centric Estimation Methods.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6580439
• Dessornes, O., and D. Scherrer. 2005. “Tests of the JAPHAR Dual Mode Ramjet Engine.” Aerospace Science and Technology 9 (3): 211–21. https://doi.org/10.1016/j.ast.2005.01.007
• Destarac, D., and J. van der Vooren. 2004. “Drag/thrust Analysis of Jet-Propelled Transonic Transport Aircraft; Definition of Physical Drag Components.” Aerospace Science and Technology 8 (6): 545–56. https://doi.org/10.1016/j.ast.2004.03.004
• Devanath, B., and M. Laila Beebi. 2016. “Comparison of QEG and Maximum L/D Trajectory Generation on Approach and Landing for Reusable Launch Vehicle.” In 2016 International Conference on Advanced Communication Control and Computing Technologies (ICACCCT). IEEE. https://doi.org/10.1109/icaccct.2016.7831668
• Devesa, Bernard, Christophe Jourdan, and Christian Marc. 2004. “Ground-Effect Identification and Autoland System Validation from Flight Data.” Journal of Aircraft 41 (4): 730–34. https://doi.org/10.2514/1.3612
• Dhiman, Kuldeep K., Abhishek, and Mangal Kotharic. 2022. “Flight Dynamics and Control of an Unmanned Helicopter with Underslung Double Pendulum.” Journal of Aircraft 59 (1): 137–53. https://doi.org/10.2514/1.c036390
• Dias, Joaquim N. 2023. “Flight-Test Determination of Longitudinal Stability Using System Identification.” Journal of Aircraft 60 (5): 1659–74. https://doi.org/10.2514/1.c037252
• Diesperov, V. N., and Iu. B. Lifshits. 1975. “On the Drag of Bodies of Revolution at Transonic Speeds.” Journal of Applied Mathematics and Mechanics 39 (2): 271–78. https://doi.org/10.1016/0021-8928(75)90149-5
• Dietz, G. 2005. “Passive Shock Control Concept for Drag Reduction in Transonic Flow.” Journal of Aircraft 42 (3): 794–99. https://doi.org/10.2514/1.11881
• Dillinger, Johannes K. S., Mostafa M. Abdalla, Yasser M. Meddaikar, and Thomas Klimmek. 2019. “Static Aeroelastic Stiffness Optimization of a Forward Swept Composite Wing with CFD-Corrected Aero Loads.” CEAS Aeronautical Journal 10 (4): 1015–32. https://doi.org/10.1007/s13272-019-00397-y
• Dimitriadis, G., and J. E. Cooper. 2001. “Flutter Prediction from Flight Flutter Test Data.” Journal of Aircraft 38 (2): 355–67. https://doi.org/10.2514/2.2770
• Dimitriadis, G., and J. E. Cooper. 2006. “Comment on ‘Flutter Prediction from Flight Flutter Test Data’.” Journal of Aircraft 43 (3): 862–63. https://doi.org/10.2514/1.c9463tc
• Dittmar, C. J. 1988. “A Hyperstable Model-Following Flight Control System Used for Reconfiguration Following Aircraft Impairment.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4790093
• Dixit, Abhishek, Adarsh Kodhanda, M. S. Mahesh, and S. E. Talole. 2016. “Active Flutter Suppression Using UDE Based Sliding Mode Control.” In 2016 11th International Conference on Industrial and Information Systems (ICIIS). IEEE. https://doi.org/10.1109/iciinfs.2016.8262981
• Dommett, Roy, and Dave Wright. 2001. “Power to Explore: A History of Marshall Space Flight Center 1960–1990. the NASA History Series, NASA-4313.” Space Policy 17 (3): 233. https://doi.org/10.1016/s0265-9646(01)00026-1
• Dong, Chunyun, Zexian Huang, Fangfang Wu, Ding Liu, and Xubin Ping. 2023a. “Constrained Reentry Trajectory Design Using Whale Optimization Algorithm for Hypersonic Glide Vehicle.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10239805
• Dong, Jiayuan, Christian Jacobsen, Mehdi Khalloufi, et al. 2025. “Variational Bayesian Optimal Experimental Design with Normalizing Flows.” Computer Methods in Applied Mechanics and Engineering 433: 117457. https://doi.org/10.1016/j.cma.2024.117457
• Dongi, F., D. Dinkler, and B. Kroeplin. 1996. “Active Panel Flutter Suppression Using Self-Sensing Piezoactuators.” AIAA Journal 34 (6): 1224–30. https://doi.org/10.2514/3.13216
• Dou, Suyi, Qingchun Yang, Yushu Jin, and Xu Xu. 2022. “Study on Fuel Equivalence Ratio Range for Supersonic Premixed Combustion Mode to Establish in a Scramjet.” Acta Astronautica 199: 37–48. https://doi.org/10.1016/j.actaastro.2022.07.016
• Dougherty, N. S. 1975. “Correlation of Transition Reynolds Number with Aerodynamic Noise Levels in a Wind Tunnel at Mach Numbers 2.0-3.0.” AIAA Journal 13 (12): 1670–71. https://doi.org/10.2514/3.7045
• Dowell, Earl H., Jeffrey P. Thomas, Kenneth C. Hall, and Charles M. Denegri. 2009. “Theoretical Predictions of F-16 Fighter Limit Cycle Oscillations for Flight Flutter Testing.” Journal of Aircraft 46 (5): 1667–72. https://doi.org/10.2514/1.42352
• Dryden, Hugh L. 1936. “Stability and Control Research.” Journal of the Aeronautical Sciences 3 (5): 174–75. https://doi.org/10.2514/8.181
• Du, Xinting, and Hejin Wang. 2024. “Efficient Estimation of Expected Information Gain in Bayesian Experimental Design with Multi-Index Monte Carlo.” Statistics and Computing 34 (6): 200. https://doi.org/10.1007/s11222-024-10522-5
• Du, Xin, and Sheng Zhang. 2020. “Flight Control Law Design and Analysis for Mars Airplane in Crosswind.” In 2020 39th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc50068.2020.9189031
• Duan, Guangren, Yong Sun, Maorui Zhang, and Ze Zhang. 2011. “Obstacle Avoidance Trajectory Optimization of Hypersonic Vehicle.” In 2011 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2011.5968400
• Duan, Guang-ren, and Zhen Zhong. 2010. “Parametric Autopilot Design for an Air-Breathing Hypersonic Vehicle.” In IEEE Icca 2010. IEEE. https://doi.org/10.1109/icca.2010.5524360
• Duggirala, Ravi K., Christopher J. Roy, and Joseph A. Schetz. 2011. “Analysis of Interference Drag for Strut-Strut Interaction in Transonic Flow.” AIAA Journal 49 (3): 449–62. https://doi.org/10.2514/1.45703
• Duke, Eugene L., Randal W. Brumbaugh, and James D. Disbrow. 1989. “A Rapid Prototyping Facility for Flight Research in Advanced Systems Concepts.” Computer 22. https://ntrs.nasa.gov/citations/19890054327
• Duke, E. L., and F. P. Jones. 1984. “Computer Control for Automated Flight Test Maneuvering.” Journal of Aircraft 21. https://ntrs.nasa.gov/citations/19840066301
• Dunbar, W. G. 1968. “Corona Testing of Supersonic Airplane High Temperature Wire.” In 1968 8th Electrical Insulation Conference. IEEE. https://doi.org/10.1109/eic.1968.7456098
• Eastep, F. E., V. A. Tischler, V. B. Venkayya, and N. S. Khot. 1999. “Aeroelastic Tailoring of Composite Structures.” Journal of Aircraft 36 (6): 1041–47. https://doi.org/10.2514/2.2546
• Eastep, F. E., V. B. Venkayya, and V. A. Tishler. 1984. “Divergence Speed Degradation of Forward-Swept Wings with Damaged Composite Skin.” Journal of Aircraft 21 (11): 921–23. https://doi.org/10.2514/3.45063
• Edwards, John W. 1983. “Flight Test Results of an Active Flutter Suppression System.” Journal of Aircraft 20 (3): 267–74. https://doi.org/10.2514/3.44863
• Eichelsdörfer, Jonas. 2026c. “Subspace Geometry and Performance Tradeoffs of Modal Blending for Active Flutter Suppression.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00552-4
• Elena, Karpovich. 2026. “Scaling a Technology Demonstrator of an Electric Vertical Take-off and Landing Boxwing Martian Aircraft for Low-Altitude Flight Tests on Earth.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00535-5
• Elkhoury, M. 2008. “Transient Structure on Unmanned Combat Air Vehicle: Effect of Pitch-Up Motion.” Journal of Aircraft 45 (2): 719–23. https://doi.org/10.2514/1.32609
• Elkhoury, M., and D. Rockwell. 2004. “Visualized Vortices on Unmanned Combat Air Vehicle Planform: Effect of Reynolds Number.” Journal of Aircraft 41 (5): 1244–47. https://doi.org/10.2514/1.6290
• Elkhoury, M., M. M. Yavuz, and D. Rockwell. 2005. “Near-Surface Topology of Unmanned Combat Air Vehicle Planform: Reynolds Number Dependence.” Journal of Aircraft 42 (5): 1318–30. https://doi.org/10.2514/1.9777
• Elmiligui, Alaa, Mohagna J. Pandya, Melissa B. Carter, Boris Diskin, and Sudheer N. Nayani. 2022. “USM3D Simulations for the Third AIAA Sonic Boom Prediction Workshop.” Journal of Aircraft 59 (3). https://ntrs.nasa.gov/citations/20210025478
• Emo, S. M., and J. Gustus. 1993. “Fiber Optic Sensing for Engine and Flight Controls.” In [1993 Proceedings] AIAA/IEEE Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.1993.283525
• Empey, Jackson, and Meyer Nahon. 2022. “In-Flight Validation of Propeller Slipstream Model.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836217
• Engelund, Walter C. 2001. “Hyper-X Aerodynamics: The X-43A Airframe-Integrated Scramjet Propulsion Flight-Test Experiments.” Journal of Spacecraft and Rockets 38 (6): 801–2. https://doi.org/10.2514/2.3757
• Englezou, Yiolanda, Timothy W. Waite, and David C. Woods. 2022. “Approximate Laplace Importance Sampling for the Estimation of Expected Shannon Information Gain in High-Dimensional Bayesian Design for Nonlinear Models.” Statistics and Computing 32 (5): 82. https://doi.org/10.1007/s11222-022-10159-2
• Esposito, Antonio, Marcello Lappa, and Christophe Allouis. 2024. “A Combustion-Driven Facility for Hypersonic Sustained Flight Simulation.” Aerotecnica Missili & Spazio 103 (3): 271–87. https://doi.org/10.1007/s42496-024-00213-9
• Etherington, Richard E. 1988. “General Aviation Cost Effectiveness.” Journal of Aircraft 25 (10): 890–96. https://doi.org/10.2514/3.45676
• Ewenz Rocher, Marc, Tobias Hermann, Matthew McGilvray, and Rowan Gollan. 2022. “Correlation for Species Concentration on a Hypersonic Stagnation Point with Mass Injection.” AIAA Journal 60 (5): 2798–2809. https://doi.org/10.2514/1.j061159
• Fasulo, Giovanni, Antimo Glorioso, Francesco Petrosino, Mattia Barbarino, and Luigi Federico. 2025. “Sonic Boom Impact Assessment of European SST Concept for Milan to New York Supersonic Flight.” Acoustics 7 (2): 29. https://doi.org/10.3390/acoustics7020029
• Fay, J. A., and F. R. Riddell. 1958. “Theory of Stagnation Point Heat Transfer in Dissociated Air.” Journal of the Aerospace Sciences 25 (2): 73–85. https://doi.org/10.2514/8.7517
• Fehrs, Michael, and Christoph Kaiser. 2025. “Transition Prediction Including Turbulent Wedges for a Forward Swept Natural Laminar Flow Wing.” CEAS Aeronautical Journal 17 (1): 435–48. https://doi.org/10.1007/s13272-025-00856-9
• Feng, Yue, Zonghua Sun, Liaoni Wu, et al. 2023. “Nonlinear Adaptive Flight Control System: Performance Enhancement and Validation.” Chinese Journal of Aeronautics 36 (4): 354–65. https://doi.org/10.1016/j.cja.2023.01.011
• Feng, Rong, Jiajian Zhu, Zhenguo Wang, et al. 2022. “Suppression of Combustion Mode Transitions in a Hydrogen-Fueled Scramjet Combustor by a Multi-Channel Gliding Arc Plasma.” Combustion and Flame 237: 111843. https://doi.org/10.1016/j.combustflame.2021.111843
• Ferrandon, Olivier. 1997. “International Market for a Reusable Launch Vehicle.” Space Policy 13 (2): 97–107. https://doi.org/10.1016/s0265-9646(97)00008-8
• Fielding, J. P., and R. I. Jones. 2000. “Graduate-Level Design Education, Based on Flight Demonstrator Projects.” Aircraft Design 3 (4): 217–38. https://doi.org/10.1016/s1369-8869(00)00006-9
• Finistauri, Allan Daniel, Fengfeng (Jeff) Xi, and Paul Walsh. 2012. “Discretization Method for the Development of a Modular Morphing Wing.” Journal of Aircraft 49 (1): 116–25. https://doi.org/10.2514/1.c031382
• Firouz-Abadi, R. D., A. R. Askarian, and P. Zarifian. 2013. “Effect of Thrust on the Aeroelastic Instability of a Composite Swept Wing with Two Engines in Subsonic Compressible Flow.” Journal of Fluids and Structures 36: 18–31. https://doi.org/10.1016/j.jfluidstructs.2012.09.005
• Fischer, Michael C. 1969. “Hypersonic Boundary-Layer Transition on Ablating and Nonablating Cones.” AIAA Journal 7 (10): 2037–38. https://doi.org/10.2514/3.5509
• Fleming, Nic. 2014. “Sonic Boom.” New Scientist 222 (2974): 38–41. https://doi.org/10.1016/s0262-4079(14)61217-3
• Flomenhoft, Hubert I. 1994. “Brief History of Gust Models for Aircraft Design.” Journal of Aircraft 31 (5): 1225–27. https://doi.org/10.2514/3.46637
• Fotia, Matthew L. 2015. “Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet–Scramjet Experiment.” Journal of Propulsion and Power 31 (1): 69–78. https://doi.org/10.2514/1.b35171
• Franchi, Antonio, and Chiara Gabellieri. 2026. “Geometric Inverse Flight Dynamics on SO(3) and Application to Tethered Fixed-Wing Aircraft.” In 2026 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas69441.2026.11598700
• Freeman, Delma C. 1982. “Space Shuttle Orbiter Static Stability and Control Derivatives Obtained from Wind-Tunnel and Flight Tests.” Journal of Spacecraft and Rockets 19 (1): 12–13. https://doi.org/10.2514/3.62197
• Freeman, Delma C., Jr., Theodore A. Talay, and R. Eugene Austin. 1997b. “Reusable Launch Vehicle Technology Program.” Acta Astronautica 41 (11). https://ntrs.nasa.gov/citations/19990009876
• Fu, Cheng, Xinglong Gao, Yunqiang Sun, Jie Kou, Dachuan Xu, and Jingxiang Chen. 2022a. “Numerical Simulation of Unsteady Fluid Parameters for Maglev Flight Wind Tunnel Design.” Aerospace 10 (1): 34. https://doi.org/10.3390/aerospace10010034
• Fu, Junquan, Zhiwei Shi, Zheng Gong, Mark H. Lowenberg, Dawei Wu, and Lijun Pan. 2022b. “Virtual Flight Test Techniques to Predict a Blended-Wing-Body Aircraft in-Flight Departure Characteristics.” Chinese Journal of Aeronautics 35 (1): 215–25. https://doi.org/10.1016/j.cja.2021.01.006
• Fu Li, Yu Mei-xiang, and Xu Xin-he. 2008. “The Strategy Studying of Air Combat about the Unmanned Combat Air Vehicles.” In 2008 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2008.4598037
• Fujii, Keisuke, and Yasutoshi Inoue. 1998a. “Aerodynamic Heating Measurement on Afterbody of Hypersonic Flight Experiment.” Journal of Spacecraft and Rockets 35 (6): 736–41. https://doi.org/10.2514/2.3409
• Fujii, Keisuke, Shigeya Watanabe, Takuji Kurotaki, and Masao Shirouzu. 2001. “Aerodynamic Heating Measurements on Nose and Elevon of Hypersonic Flight Experiment Vehicle.” Journal of Spacecraft and Rockets 38 (1): 8–14. https://doi.org/10.2514/2.3665
• Fujimori, A., and H. Ohta. 1993. “A Synthesis of Reduced-Order H ∞ Controllers for Active Flutter Suppression Systems.” IFAC Proceedings Volumes 26 (2): 805–8. https://doi.org/10.1016/s1474-6670(17)48843-4
• Gallagher, J. T. 1971. “Requirements on Simulators Used in Handling Qualities Research.” Journal of Aircraft 8 (11): 917–24. https://doi.org/10.2514/3.59189
• Gao, Jianfeng. 2023. “Drag Reduction Analysis of Transonic RAE2822 Airfoil with Two-Dimensional Optimal Bump.” In 2023 3rd International Conference on Networking Systems of AI (INSAI). IEEE. https://doi.org/10.1109/insai60116.2023.00050
• Gao, Xiang, Can Feng, Tao Rao, Tao Liu, and Xiaowen Zha. 2022. “Airborne Flight Test Data Online Preprocessing System Design and Development.” In 2022 International Conference on Sensing, Measurement & Data Analytics in the era of Artificial Intelligence (ICSMD). IEEE. https://doi.org/10.1109/icsmd57530.2022.10058333
• Gao, Honggang, Ao He, Zhenghong Gao, Yang Na, and Yangping Deng. 2019. “Flight Dynamics Characteristics of Canard Rotor/wing Aircraft in Helicopter Flight Mode.” Chinese Journal of Aeronautics 32 (7): 1577–87. https://doi.org/10.1016/j.cja.2019.04.002
• Garabedian, P. R. 1976. “Computation of Wave Drag for Transonic Flow.” Journal d’Analyse Mathématique 30 (1): 164–71. https://doi.org/10.1007/bf02786712
• Garg, Priyanka, and Abhishek Kumar Dodiyal. 2009. “Reducing RF Blackout during Re-Entry of the Reusable Launch Vehicle.” In 2009 IEEE Aerospace conference. IEEE. https://doi.org/10.1109/aero.2009.4839389
• Garrick, I. E., and Wilmer H. Reed. 1981. “Historical Development of Aircraft Flutter.” Journal of Aircraft 18 (11): 897–912. https://doi.org/10.2514/3.57579
• Geiger, Reed, Nicholas L. Strahan, William D. Greder, William B. DeVerter, and Carson D. Slabaugh. 2026. “Operating Mode Influence on Heat Release in an Axisymmetric Dual-Mode Ramjet.” AIAA Journal: 1–22. https://doi.org/10.2514/1.j067064
• Geissler, W., G. Dietz, and H. Mai. 2005. “Dynamic Stall on a Supercritical Airfoil.” Aerospace Science and Technology 9 (5): 390–99. https://doi.org/10.1016/j.ast.2005.01.012
• “Generalized Predictive Control for Active Flutter Suppression.” 1997. IEEE Control Systems 17 (4): 64–70. https://doi.org/10.1109/37.608553
• Georgiou, G., A. Manan, and J. E. Cooper. 2012. “Modeling Composite Wing Aeroelastic Behavior with Uncertain Damage Severity and Material Properties.” Mechanical Systems and Signal Processing 32: 32–43. https://doi.org/10.1016/j.ymssp.2012.05.003
• Gern, Frank H., and Liviu Librescu. 2000. “Aeroelastic Tailoring of Composite Wings Exhibiting Nonclassical Effects and Carrying External Stores.” Journal of Aircraft 37 (6): 1097–1104. https://doi.org/10.2514/2.2718
• Gern, Frank H., Amir H. Naghshineh-Pour, Erwin Sulaeman, Rakesh K. Kapania, and Raphael T. Haftka. 2001. “Structural Wing Sizing for Multidisciplinary Design Optimization of a Strut-Braced Wing.” Journal of Aircraft 38 (1): 154–63. https://doi.org/10.2514/2.2747
• Ghiringhelli, G. L., M. Lanz, and P. Mantegazza. 1990. “Active Flutter Suppression for a Wing Model.” Journal of Aircraft 27 (4): 334–41. https://doi.org/10.2514/3.25277
• Ghoreyshi, Mehdi, Ryan Darragh, Sean Harrison, Andrew J. Lofthouse, and Peter E. Hamlington. 2017. “Canard–wing Interference Effects on the Flight Characteristics of a Transonic Passenger Aircraft.” Aerospace Science and Technology 69: 342–56. https://doi.org/10.1016/j.ast.2017.06.024
• Ghosh, A. K., and S. C. Raisinghani. 2002. “Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks.” Journal of Aircraft 39 (5): 892–94. https://doi.org/10.2514/2.3012
• Gibson, R. E. 1949. “Supersonic Guided Missiles.” Journal of the American Rocket Society 00 (78): 129–40. https://doi.org/10.2514/8.4292
• Gilbert, M. G., D. K. Schmidt, and T. A. Weisshaar. 1984. “Quadratic Synthhesis of Integrated Active Controls for an Aeroelastic Forward-Swept-Wing Aircraft.” Journal of Guidance, Control, and Dynamics 7 (2): 190–96. https://doi.org/10.2514/3.8566
• Go, Jinwoo, and Peng Chen. 2025a. “Accurate, Scalable, and Efficient Bayesian Optimal Experimental Design with Derivative-Informed Neural Operators.” Computer Methods in Applied Mechanics and Engineering 438: 117845. https://doi.org/10.1016/j.cma.2025.117845
• Go, Jinwoo, and Peng Chen. 2025b. “Sequential Infinite-Dimensional Bayesian Optimal Experimental Design with Derivative-Informed Latent Attention Neural Operator.” Journal of Computational Physics 532: 113976. https://doi.org/10.1016/j.jcp.2025.113976
• Goege, Dennis. 2007. “Fast Identification and Characterization of Nonlinearities in Experimental Modal Analysis of Large Aircraft.” Journal of Aircraft 44 (2): 399–409. https://doi.org/10.2514/1.20847
• Goel, Muskan, Rajoshi Sarkar, and S. Singh. 2021. “Estimation of Stability and Control Derivatives Using Simulated Flight Data.” In 2021 11th International Conference on Cloud Computing, Data Science & Engineering (Confluence). IEEE. https://doi.org/10.1109/confluence51648.2021.9377200
• Goetzendorf-Grabowski, Tomasz, and Agnieszka Kwiek. 2023. “Study of the Impact of Aerodynamic Model Fidelity on the Flight Characteristics of Unconventional Aircraft.” Applied Sciences 13 (22): 12522. https://doi.org/10.3390/app132212522
• Golombek, H., J. Bustamante, R. Maierl, and I. Staack. 2026. “An Automated Surrogate Model Generation Framework for Rapid Aeroelastic Structural Sizing Optimizations in Conceptual Aircraft Design.” CEAS Aeronautical Journal. https://doi.org/10.1007/s13272-026-00996-6
• Gomez, Nicolas, Victor Gomez, Enrique Paiva, Jorge Rodas, and Raul Gregor. 2020. “Flight Controller Optimization of Unmanned Aerial Vehicles Using a Particle Swarm Algorithm.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9214003
• Gong, Tianyu, Yaosong Long, Zhongtao Cheng, and Yiqing Li. 2024. “Recent Development of Integrated Design and Improving Methods of Waverider and Inlet.” Advances in Aerodynamics 6 (1): 25. https://doi.org/10.1186/s42774-024-00181-5
• Gong Weijie and Tang Shuo. 2010. “Aerodynamic Heating Numerical Simulation Method Research for Quasi-Waverider Hypersonic Vehicle.” In 2010 International Conference On Computer Design and Applications. IEEE. https://doi.org/10.1109/iccda.2010.5541259
• Gong Weijie and Tang shuo. 2010. “Hypersonic Vehicle Wing-Body Joint Location Design Optimization Basing on Hybrid Genetic Algorithm.” In 2010 International Conference on Educational and Network Technology. IEEE. https://doi.org/10.1109/icent.2010.5532163
• Gonor, A. L. 1960. “Determination of the Shape of a Body of Minimum Drag at Hypersonic Speed.” Journal of Applied Mathematics and Mechanics 24 (6): 1628–35. https://doi.org/10.1016/0021-8928(60)90014-9
• Gonor, A. L. 1964. “Remarks Concerning the Paper “Determination Op the Shape Op a Body Op Minimum Drag at Hypersonic Speed”.” Journal of Applied Mathematics and Mechanics 28 (6): 1378. https://doi.org/10.1016/0021-8928(64)90055-3
• Goodman, Jenny S., and Peter T. Ireland. 2007. “Thermal Modeling for the Sustained Hypersonic Flight Experiment.” Journal of Thermophysics and Heat Transfer 21 (4): 780–89. https://doi.org/10.2514/1.29317
• Goodyer, Michael J., and Robert A. Kilgore. 1973. “High-Reynolds-Number Cryogenic Wind Tunnel.” AIAA Journal 11 (5): 613–19. https://doi.org/10.2514/3.50500
• Goonko, Y. P., and I. I. Mazhul. 2002. “Some Factors of Hypersonic Inlet/Airplane Interactions.” Journal of Aircraft 39 (1): 37–50. https://doi.org/10.2514/2.2922
• Gordnier, R., S. Sherer, and M. Visbal. 2007. “Computations of a Maneuvering Unmanned Combat Air Vehicle Using a High-Order Overset Grid Method.” In 2007 DoD High Performance Computing Modernization Program Users Group Conference. IEEE. https://doi.org/10.1109/hpcmp-ugc.2007.23
• Gordnier, R. E., M. R. Visbal, and S. E. Sherer. 2005. “Higher-Order Accurate Computations of Maneuvering Unmanned Combat Air Vehicle Configurations.” In 2005 Users Group Conference (DOD-UGC’05). IEEE. https://doi.org/10.1109/dodugc.2005.34
• Gordnier, Raymond E., Miguel R. Visbal, and Scott E. Sherer. 2006. “High-Fidelity Simulations for Maneuvering Unmanned Combat Air Vehicle Configurations.” In 2006 HPCMP Users Group Conference (HPCMP-UGC’06). IEEE. https://doi.org/10.1109/hpcmp-ugc.2006.33
• Gosse, Ryan, Roger Kimmel, and Heath B. Johnson. 2014. “Study of Boundary-Layer Transition on Hypersonic International Flight Research Experimentation 5.” Journal of Spacecraft and Rockets 51 (1): 151–62. https://doi.org/10.2514/1.a32371
• Goto, Yuichiro, Shigeru Obayashi, and Yasuaki Kohama. 2007. “Wave Drag Characteristics of a Low-Drag Supersonic Formation Flying Concept.” Journal of Aircraft 44 (2): 675–79. https://doi.org/10.2514/1.23236
• Gottu Mukkula, Anwesh Reddy, and Radoslav Paulen. 2016. “Optimal Design of Dynamic Experiments for Guaranteed Parameter Estimation.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7525184
• Goulard, R. 1961. “A Comment on ‘Radiation from Hot Air and Its Effect on Stagnation-Point Heating’.” Journal of the Aerospace Sciences 28 (2): 158–59. https://doi.org/10.2514/8.8893
• Grauer, Jared A. 2021. “Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements.” Journal of Aircraft 58 (5): 1022–33. https://doi.org/10.2514/1.c035933
• Grauer, Jared A., and Matthew J. Boucher. 2020. “Aircraft System Identification from Multisine Inputs and Frequency Responses.” Journal of Guidance, Control, and Dynamics 43 (12). https://ntrs.nasa.gov/citations/20205003364
• Grauer, Jared A., and Eugene A. Morelli. 2023. “Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection.” Journal of Aircraft 60 (5): 1329–30. https://doi.org/10.2514/1.c037583
• Grauer, Jared A., and Eugene A. Morelli. 2025. “Aircraft Parameter Estimation Considering Process and Measurement Noise.” Journal of Aircraft 62 (2): 288–99. https://doi.org/10.2514/1.c038080
• Grauer, Jared A., Eugene A. Morelli, and Daniel G. Murri. 2017. “Flight-Test Techniques for Quantifying Pitch Rate and Angle-of-Attack Rate Dependencies.” Journal of Aircraft 54 (6): 2367–77. https://doi.org/10.2514/1.c034407
• Green, John A. 1987. “Aeroelastic Tailoring of Aft-Swept High-Aspect-Ratio Composite Wings.” Journal of Aircraft 24 (11): 812–19. https://doi.org/10.2514/3.45525
• Greer, Donald, Phil Hamory, Keith Krake, and Mark Drela. 2000. “Design and Predictions for High-Altitude (Low Reynolds Number) Aerodynamic Flight Experiment.” Journal of Aircraft 37 (4): 684–89. https://doi.org/10.2514/2.2652
• Gregory, Irene M., Kasey Ackerman, Steve Snyder, and Paul Rothhaar. 2015. “Adaptive Control for Tilt-Wing VTOL UAV.” In 2015 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2015.7171114
• Gresham, James L., Benjamin M. Simmons, Jeremy W. Hopwood, and Craig A. Woolsey. 2024. “Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data.” Journal of Aircraft 61 (1): 128–39. https://doi.org/10.2514/1.c036835
• Griffin, Kenneth E., and Franklin E. Eastep. 1982. “Active Control of Forward-Swept Wings with Divergence and Flutter Aeroelastic Instabilities Kenneth.” Journal of Aircraft 19 (10): 885–91. https://doi.org/10.2514/3.61570
• Gross, Andreas, and Hermann F. Fasel. 2018. “Active Control of Laminar Separation: Simulations, Wind Tunnel, and Free-Flight Experiments.” Aerospace 5 (4): 114. https://doi.org/10.3390/aerospace5040114
• Große, Sebastian, and Wolfgang Schröder. 2009. “High Reynolds Number Turbulent Wind Tunnel Boundary Layer Wall-Shear Stress Sensor.” Journal of Turbulence 10: N14. https://doi.org/10.1080/14685240902953798
• Gu, Sangdi. 2026a. “Isolating the Specific Contribution of Boundary-Layer Edge Chemical Nonequilibrium to Stagnation-Point Heating.” International Journal of Heat and Fluid Flow 118: 110206. https://doi.org/10.1016/j.ijheatfluidflow.2025.110206
• Gu, Sangdi. 2026b. “Theory of Stagnation-Point Heating on Hypersonic Thick Sphere–Cone.” AIAA Journal: 1–10. https://doi.org/10.2514/1.j067283
• Guadagnini, Jacopo, Gabriele De Zaiacomo, and Michèle Lavagna. 2023. “Mission Performance Assessment of the Recovery and Vertical Landing of a Reusable Launch Vehicle.” Aerospace 11 (1): 35. https://doi.org/10.3390/aerospace11010035
• Guan, Xiaohui. 2014b. “Supersonic Wing–Body Two-Level Wave Drag Optimization Using Extended Far-Field Composite-Element Methodology.” AIAA Journal 52 (5): 981–90. https://doi.org/10.2514/1.j052305
• Guizzo, E. 2004. “Hypersonic Flight.” IEEE Spectrum 41 (1): 58–58. https://doi.org/10.1109/mspec.2004.1259370
• Gülhan, A., D. Hargarten, M. Zurkaulen, et al. 2023. “Selected Results of the Hypersonic Flight Experiment STORT.” Acta Astronautica 211: 333–43. https://doi.org/10.1016/j.actaastro.2023.06.034
• Guo, Linliang, Minghong Zhu, Bowen Nie, Peng Kong, and Chengwen Zhong. 2017. “Initial Virtual Flight Test for a Dynamically Similar Aircraft Model with Control Augmentation System.” Chinese Journal of Aeronautics 30 (2): 602–10. https://doi.org/10.1016/j.cja.2016.12.034
• Gupta, K. K., and C. Bach. 2007. “Computational Fluid Dynamics-Based Aeroservoelastic Analysis with Hyper-X Applications.” AIAA Journal 45 (7). https://ntrs.nasa.gov/citations/20070034896
• Gur, Ohad, Manav Bhatia, Joseph A. Schetz, William H. Mason, Rakesh K. Kapania, and Dimitri N. Mavris. 2010b. “Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft.” Journal of Aircraft 47 (6): 1907–17. https://doi.org/10.2514/1.47546
• Gur, Ohad, Joseph A. Schetz, and William H. Mason. 2011. “Aerodynamic Considerations in the Design of Truss-Braced-Wing Aircraft.” Journal of Aircraft 48 (3): 919–39. https://doi.org/10.2514/1.c031171
• Guy, Christopher R. 1976. “Investigation of VTOL Landing Control Laws for Low-Speed Flight.” Journal of Aircraft 13 (6): 399–405. https://doi.org/10.2514/3.44533
• Hafez, M., J. South, and E. Murman. 1979. “Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential Equation.” AIAA Journal 17 (8): 838–44. https://doi.org/10.2514/3.61235
• Hager, B. F. 1955. “Explosion-Proofing Instrumentation Equipment for Flight-Test Use.” Electrical Engineering 74 (10): 873–77. https://doi.org/10.1109/ee.1955.6439588
• Haglund, G. T., and E. J. Kane. 1974a. “Analysis of Sonic Boom Flight Test Measurements near the Shock Wave Extremity.” Journal of Aircraft 11 (12): 745–51. https://doi.org/10.2514/3.60409
• Haley, Pamela, and Don Soloway. 2022. “Generalized Predictive Control for Active Flutter Suppression [25 Years Ago].” IEEE Control Systems 42 (4): 13-C3. https://doi.org/10.1109/mcs.2022.3171473
• Hameed, Aysha S., and G. R. Bindu. 2019. “A Novel Flare Maneuver Guidance for Approach and Landing Phase of a Reusable Launch Vehicle.” In 2019 Advances in Science and Engineering Technology International Conferences (ASET). IEEE. https://doi.org/10.1109/icaset.2019.8714376
• Hameed, Aysha S., and G. R. Bindu. 2021. “Single Segment Approach and Landing Guidance and Control for an Unpowered Reusable Launch Vehicle.” Aerospace Science and Technology 115: 106777. https://doi.org/10.1016/j.ast.2021.106777
• Hamel, Peter G., and Ravindra V. Jategaonkar. 1996. “Evolution of Flight Vehicle System Identification.” Journal of Aircraft 33 (1): 9–28. https://doi.org/10.2514/3.46898
• Hamilton, H. H., Roop N. Gupta, and Jim J. Jones. 1991. “Flight Stagnation-Point Heating Calculations on Aeroassist Flight Experiment Vehicle.” Journal of Spacecraft and Rockets 28 (1): 125–28. https://doi.org/10.2514/3.26219
• Han, Yufeng, and Wei Cao. 2019. “Flat-Plate Hypersonic Boundary-Layer Flow Instability and Transition Prediction Considering Air Dissociation.” Applied Mathematics and Mechanics 40 (5): 719–36. https://doi.org/10.1007/s10483-019-2480-6
• Han, Yongsu, and Youdan Kim. 2011. “Optimal Input Design for Online Parameter Estimation for Aircraft with Multiple Control Surfaces.” Engineering Optimization 43 (5): 559–80. https://doi.org/10.1080/0305215x.2010.502937
• Hao, Xinyue, Juntao Chang, Wen Bao, and Zexu Zhang. 2016a. “A Model of Mode Transition Logic in Dual-Mode Scramjet Engines.” Aerospace Science and Technology 49: 173–84. https://doi.org/10.1016/j.ast.2015.12.001
• Harris, Herbert I. 1967. “Sonic Boom: Con.” Science News 92 (19): 436. https://doi.org/10.2307/3952432
• Harris, Joshua, Frank Arthurs, James V. Henrickson, and John Valasek. 2016. “Aircraft System Identification Using Artificial Neural Networks with Flight Test Data.” In 2016 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2016.7502624
• Hasan, A. B. M. Toufique, and Md. Mahbub Alam. 2013. “RANS Computation of Transonic Buffet over a Supercritical Airfoil.” Procedia Engineering 56: 303–9. https://doi.org/10.1016/j.proeng.2013.03.123
• He, Ao, Honggang Gao, Shanshan Zhang, et al. 2022. “Full Mode Flight Dynamics Modelling and Control of Stopped-Rotor UAV.” Chinese Journal of Aeronautics 35 (10): 95–105. https://doi.org/10.1016/j.cja.2022.03.016
• He, Yajuan, Junli Wang, Jinyang Li, Bofeng Duan, Yang Zhou, and Kangjie Wang. 2023. “Effect of Aeroelastic Tailoring Design on Wing Mode.” International Journal of Aerospace Engineering 2023: 1–19. https://doi.org/10.1155/2023/1711088
• “Head-up Displays and Air Data Computers to Equip Demonstrator Aircraft.” 1988. Displays 9 (3): 156. https://doi.org/10.1016/0141-9382(88)90025-x
• Heath, Christopher M., John W. Slater, and Sriram K. Rallabhandi. 2017. “Inlet Trade Study for a Low-Boom Aircraft Demonstrator.” Journal of Aircraft 54 (4): 1283–93. https://doi.org/10.2514/1.c034036
• Hermann, Tobias. 2025. “Correlation for Wall-Temperature Oscillations in Unsteady Stagnation Point Convective Heating.” International Journal of Heat and Mass Transfer 244: 126907. https://doi.org/10.1016/j.ijheatmasstransfer.2025.126907
• “High-Speed Flight.” 1986. Futures 18 (5): 722–25. https://doi.org/10.1016/0016-3287(86)90050-9
• Hilger, Jonathan, and Markus Raimund Ritter. 2021. “Nonlinear Aeroelastic Simulations and Stability Analysis of the Pazy Wing Aeroelastic Benchmark.” Aerospace 8 (10): 308. https://doi.org/10.3390/aerospace8100308
• Hinchliffe, Benjamin, and Ning Qin. 2017. “Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction.” AIAA Journal 55 (3): 818–31. https://doi.org/10.2514/1.j055319
• Hinrichsen, Jens, and Cesar Bautista. 2001. “The Challenge of Reducing Both Airframe Weight and Manufacturing Cost.” Air & Space Europe 3 (3–4): 119–21. https://doi.org/10.1016/s1290-0958(01)90072-3
• Hitzel, Stephan, and Dirk Zimper. 2018. “Wind Tunnel, Simulation, and “Real” Flight of Advanced Combat Aircraft: Industrial Perspective.” Journal of Aircraft 55 (2): 587–602. https://doi.org/10.2514/1.c033696
• Hjartarson, Arnar, Peter Seiler, and Andrew Packard. 2015. “LPVTools: A Toolbox for Modeling, Analysis, and Synthesis of Parameter Varying Control Systems**This Work Was Supported by a NASA Small Business Innovation Research Contract from NASA Armstrong Flight Research Center, Contract #NNX12CA14C. Contract Monitor Is Dr. Martin J. Bren-Ner.” IFAC-PapersOnLine 48 (26): 139–45. https://doi.org/10.1016/j.ifacol.2015.11.127
• Hockman, Marion T., and Robert E. Eisiminger. 1948. “The Correlation of Wind-Tunnel and Flight-Test Stability and Control Data for an SB2C-1 Airplane.” Journal of the Aeronautical Sciences 15 (1): 5–17. https://doi.org/10.2514/8.11490
• Holdo, Arne E. 1993. “Reynolds Number Effects on Lattice Structures Forming Part of a Wind Tunnel Model.” Journal of Wind Engineering and Industrial Aerodynamics 45 (2): 229–38. https://doi.org/10.1016/0167-6105(93)90272-p
• Hon Man Chan, Allen R. Parker, Anthony Piazza, and W. Lance Richards. 2015. “Fiber-Optic Sensing System: Overview, Development and Deployment in Flight at NASA.” In 2015 IEEE Avionics and Vehicle Fiber-Optics and Photonics Conference (AVFOP). IEEE. https://doi.org/10.1109/avfop.2015.7356646
• Horton, T. E., and T. L. Babineaux. 1967. “Influence of Atmospheric Composition on Hypersonic Stagnation-Point Convective Heating.” AIAA Journal 5 (1): 36–43. https://doi.org/10.2514/3.3904
• Hou, Baobin, Yanru Chen, Jinyan Cai, Xin Peng, Xin Xu, and Dawei Liu. 2026. “Reynolds Number Effect of a Supercritical Wing Based on Cryogenic and High Reynolds Number Pressure Test.” Aerospace 13 (3): 265. https://doi.org/10.3390/aerospace13030265
• Howell, Charles T., III, Artie Jessup, Frank Jones, et al. 2010. “The NASA Langley Research Center’s Unmanned Aerial System Surrogate Research Aircraft.” In 29th Digital Avionics Systems Conference. https://ntrs.nasa.gov/citations/20110004205
• Hu-Sheng Wu, Wei-Zong Lu, and Yu-Long Wang. 2015. “Research on the Structure Design and Flight Performance of a Small Tilt Rotor Unmanned Aircraft.” In 2015 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2015.7382829
• Hua, Yang, Song Lei, Liu Cheng, and Huang Jun. 2013. “Study on Powered-Parafoil Longitudinal Flight Performance with a Fast Estimation Model.” Journal of Aircraft 50 (5): 1660–68. https://doi.org/10.2514/1.c032176
• Hua, Siyu, Xugang Wang, and Zhongyuan Wang. 2025. “Rigid–Elastic Coupling Dynamics of Morphing Wing Aircraft.” Aerospace 12 (4): 327. https://doi.org/10.3390/aerospace12040327
• Huan, Xun, and Youssef M. Marzouk. 2013. “Simulation-Based Optimal Bayesian Experimental Design for Nonlinear Systems.” Journal of Computational Physics 232 (1): 288–317. https://doi.org/10.1016/j.jcp.2012.08.013
• Huang, Haoyang, Yitong Fan, Zhiqiang Ke, Ding Tang, Weiming Wang, and Dayong Li. 2025c. “Designing a Variable Camber Wing Trailing Edge with Initially Curved Beams.” Aerospace Science and Technology 161: 110151. https://doi.org/10.1016/j.ast.2025.110151
• Humphreys-Jennings, Clayton, Ilias Lappas, and Dragos Mihai Sovar. 2020. “Conceptual Design, Flying, and Handling Qualities Assessment of a Blended Wing Body (BWB) Aircraft by Using an Engineering Flight Simulator.” Aerospace 7 (5): 51. https://doi.org/10.3390/aerospace7050051
• Hunter, Matthew, and Simone D’Amico. 2024. “Robust Closed-Form Framework for Drag-Propulsive Control of Formation Flight.” In 2024 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero58975.2024.10521029
• Hwang, C., E. H. Johnson, and W. S. Pi. 1981. “Recent Development of the YF-17 Active Flutter Suppression System.” Journal of Aircraft 18 (7): 537–45. https://doi.org/10.2514/3.57523
• Hwu, Chyanbin, and Z. S. Tsai. 2002. “Aeroelastic Divergence of Stiffened Composite Multicell Wing Structures.” Journal of Aircraft 39 (2): 242–51. https://doi.org/10.2514/2.2945
• Ignatyev, Dmitry I., Hyo-Sang Shin, and Antonios Tsourdos. 2019. “Two-Layer on-Line Parameter Estimation for Adaptive Incremental Backstepping Flight Control for a Transport Aircraft in Uncertain Conditions.” IFAC-PapersOnLine 52 (12): 411–16. https://doi.org/10.1016/j.ifacol.2019.11.278
• Igra, Dan. 2018. “Extension of the Simple Analytical Model for Waverider Design.” Journal of Spacecraft and Rockets 55 (4): 1024–27. https://doi.org/10.2514/1.a34089
• Igra, Dan. 2019. “Nonslender Waverider Design Implementation into Simple Analytical Model for Waverider Design.” Journal of Spacecraft and Rockets 56 (3): 967–70. https://doi.org/10.2514/1.a34415
• Igreja, J. M., and J. M. Lemos. 2022. “Oracle for Guidance with Deep Neural Networks in Reusable Launch Vehicle Landing.” In 2022 International Conference on Control, Automation and Diagnosis (ICCAD). IEEE. https://doi.org/10.1109/iccad55197.2022.9854017
• Iliff, Kenneth W., and Richard E. Maine. 1983. “Uses of Parameter Estimation in Flight Test.” Journal of Aircraft 20 (12): 1043–49. https://doi.org/10.2514/3.48210
• Inoyama, Daisaku, Brian P. Sanders, and James J. Joo. 2007. “Topology Synthesis of Distributed Actuation Systems for Morphing Wing Structures.” Journal of Aircraft 44 (4): 1205–13. https://doi.org/10.2514/1.25535
• Inoyama, Daisaku, Brian P. Sanders, and James J. Joo. 2008. “Topology Optimization Approach for the Determination of the Multiple-Configuration Morphing Wing Structure.” Journal of Aircraft 45 (6): 1853–63. https://doi.org/10.2514/1.29988
• “Introduction to the Virtual Collection for Predicting Hypersonic Boundary-Layer Transition on Complex Geometries.” 2026. AIAA Journal: 1–2. https://doi.org/10.2514/1.j066633
• Iovnovich, Michael, Tzlil Nahom, Michael Presman, Dorin Avsaid, Tomer Braier, and Daniella E. Raveh. 2018. “Assessment of Advanced Flutter Flight-Test Techniques and Flutter Boundary Prediction Methods.” Journal of Aircraft 55 (5): 1877–89. https://doi.org/10.2514/1.c034716
• Ishimoto, Shinji, Kenji Fujii, and Takeshi Mori. 2005. “Flight Demonstrator Concept for Key Technologies Enabling Future Reusable Launch Vehicles.” Acta Astronautica 57 (2–8): 438–43. https://doi.org/10.1016/j.actaastro.2005.03.045
• Isogai, Koji. 1989. “Direct Search Method to Aeroelastic Tailoring of a Composite Wing under Multiple Constraints.” Journal of Aircraft 26 (12): 1076–80. https://doi.org/10.2514/3.45883
• Isogai, K. 1992. “Transonic Flutter/divergence Characteristics of Aeroelastically Tailored and Non-Tailored High-Aspect-Ratio Forward-Swept Wings.” Journal of Fluids and Structures 6 (5): 525–37. https://doi.org/10.1016/0889-9746(92)90017-w
• Ito, Takeshi, Ryoji Takaki, and Ken Teraoka. 1999. “Plasma Electron Density Measurement around Hypersonic Flight Experiment Vehicle.” Journal of Spacecraft and Rockets 36 (4): 573–78. https://doi.org/10.2514/3.27202
• Jackson, L. Robert, and Allan H. Taylor. 1978. “Structural Design for a Hypersonic Research Airplane.” Journal of Aircraft 15 (6): 366–73. https://doi.org/10.2514/3.58371
• Jackuliak, Jakub, and Martin Bugaj. 2026. “Challenges of High-Speed UAV Using Forward Swept Wing.” In 2026 New Trends in Civil Aviation (NTCA). IEEE. https://doi.org/10.23919/ntca68808.2026.11524172
• Jaiswal, Prateek, and Harsha Honnappa. 2020. “Statistical Inference for Approximate Bayesian Optimal Design.” In 2020 Winter Simulation Conference (WSC). IEEE. https://doi.org/10.1109/wsc48552.2020.9383857
• Jakeman, J. D. 2023. “PyApprox: A Software Package for Sensitivity Analysis, Bayesian Inference, Optimal Experimental Design, and Multi-Fidelity Uncertainty Quantification and Surrogate Modeling.” Environmental Modelling & Software 170: 105825. https://doi.org/10.1016/j.envsoft.2023.105825
• Jakowluk, Wiktor. 2014. “Plant Friendly Input Design for Parameter Estimation in an Inertial System with Respect to D-Efficiency Constraints.” Entropy 16 (11): 5822–37. https://doi.org/10.3390/e16115822
• Jakowluk, Wiktor. 2018. “Free Final Time Input Design Problem for Robust Entropy-Like System Parameter Estimation.” Entropy 20 (7): 528. https://doi.org/10.3390/e20070528
• Jäschke, Jacob, Samuele Graziani, Francesco Petrosino, Antimo Glorioso, and Volker Gollnick. 2024. “Comparison of Prediction Models for Sonic Boom Ground Signatures under Realistic Flight Conditions.” Aerospace 11 (12): 962. https://doi.org/10.3390/aerospace11120962
• Jategaonkar, R. V. 2000. “Bounded-Variable Gauss-Newton Algorithm for Aircraft Parameter Estimation.” Journal of Aircraft 37 (4): 742–44. https://doi.org/10.2514/2.2666
• Jategaonkar, Ravindra V. 2005. “Flight Vehicle System Identification-Engineering Utility.” Journal of Aircraft 42 (1): 11–11. https://doi.org/10.2514/1.15766
• Jategaonkar, Ravindra, Roland Behr, Wilhelm Gockel, and Christoph Zorn. 2006. “Data Analysis of Phoenix Reusable Launch Vehicle Demonstrator Flight Test.” Journal of Aircraft 43 (6): 1732–37. https://doi.org/10.2514/1.19602
• Jategaonkar, Ravindra, Dietrich Fischenberg, and Wolfgang von Gruenhagen. 2004. “Aerodynamic Modeling and System Identification from Flight Data-Recent Applications at DLR.” Journal of Aircraft 41 (4): 681–91. https://doi.org/10.2514/1.3165
• Jategaonkar, R. V., and E. Plaetschke. 1989. “Algorithms for Aircraft Parameter Estimation Accounting for Process and Measurement Noise.” Journal of Aircraft 26 (4): 360–72. https://doi.org/10.2514/3.45769
• Jategaonkar, R. V., and F. Thielecke. 1994. “Evaluation of Parameter Estimation Methods for Unstable Aircraft.” Journal of Aircraft 31 (3): 510–19. https://doi.org/10.2514/3.46523
• Jauberthie, Carine, François Bournonville, Patricia Coton, and Frank Rendell. 2006. “Optimal Input Design for Aircraft Parameter Estimation.” Aerospace Science and Technology 10 (4): 331–37. https://doi.org/10.1016/j.ast.2005.08.002
• Jauberthie, C., L. Denis-Vidal, and G. Joly-Blanchard. n.d. “Identifiability and Estimation of Aircraft Parameters and Delays by Using Optimal Input Design.” In Proceedings of the 44th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2005.1583371
• Jauberthie, Carine, Lilianne Denis-Vidal, and Ghislaine Joly-Blanchard. 2003. “Aircraft Parameter Estimation by Using the Optimal Input Design and Linear Matrix Inequalities.” IFAC Proceedings Volumes 36 (16): 657–62. https://doi.org/10.1016/s1474-6670(17)34836-x
• Jauberthie, Carine, Lilianne Denis-Vidal, Qiaochu Li, and Zohra Cherfi-Boulanger. 2018. “Optimal Input Design for Parameter Estimation in a Bounded-Error Context for Nonlinear Dynamical Systems.” Automatica 92: 86–91. https://doi.org/10.1016/j.automatica.2018.03.003
• Jenke, Leroy M. 1979. “Application of Digital Fourier Analysis in Processing Dynamic Aerodynamic Heating Measurements.” AIAA Journal 17 (6): 641–42. https://doi.org/10.2514/3.61189
• Jeong, Jaebaek, and Jae-Sung Bae. 2022. “Wind Tunnel & Flight Test of VCCS Morphing UAV.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836192
• Jesudasan, Rejish, John Doherty, and Simão Marques. 2026. “Enhancing Rapid Drag Analysis for Transonic Aircraft Configuration Trade Studies.” Aerospace Science and Technology 168: 110727. https://doi.org/10.1016/j.ast.2025.110727
• Ji, Chen, Feng Li, and Ziqiang Liu. 2019. “Development and Testing of Hypersonic Flutter Test Capability.” AIAA Journal 57 (7): 2989–3002. https://doi.org/10.2514/1.j056165
• Jia, Dongpeng, Yu Pan, Ning Wang, Chaoyang Liu, and Kai Yang. 2021. “Combustion Modes and Unsteady Characteristics during the Condition Transition of a Scramjet Combustor.” Energies 14 (9): 2522. https://doi.org/10.3390/en14092522
• Jia, Yicong, Wei Ye, Peng Cui, and Wanwu Xu. 2019. “Climbing Performance Analysis of Rocket-Based Combined Cycle Engine Powered Aircraft.” Acta Astronautica 162: 135–44. https://doi.org/10.1016/j.actaastro.2019.05.034
• Jiang, Zhesheng, and Raul Ordonez. 2008. “Robust Approach and Landing Trajectory Generation for Reusable Launch Vehicles in Winds.” In 2008 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2008.4629595
• Jiang, Kun, Wei Zhang, XiaoWu Xu, and Zhi Ma. 2011. “Investigation of Dynamic Characteristic of Forward Swept Folding Wing.” In 2011 IEEE International Conference on Automation and Logistics (ICAL). IEEE. https://doi.org/10.1109/ical.2011.6024717
• Jianghao, Wu, Cai Chenfang, and Zhang Yanlai. 2011. “The Changes in Structural and Flight Safety Due to Flap Design of Blended-Wing-Body Civil Aircraft.” Procedia Engineering 17: 320–27. https://doi.org/10.1016/j.proeng.2011.10.035
• Jianguo, Guo, Wang Guoqing, and Zhou Jun. 2016. “Attitude Control for Reentry Reusable Launch Vehicle.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7532005
• Jianhong, Wang. 2025. “Optimal Input Signal Design for Closed Loop Aircraft Flutter Model Analysis.” Scientific Reports 15 (1): 40412. https://doi.org/10.1038/s41598-025-99448-0
• Jo, Sung Min, Oh Joon Kwon, and Jae Gang Kim. 2020. “Stagnation-Point Heating of Fire II with a Non-Boltzmann Radiation Model.” International Journal of Heat and Mass Transfer 153: 119566. https://doi.org/10.1016/j.ijheatmasstransfer.2020.119566
• Jo, Bruce W., and Tuba Majid. 2023. “Enhanced Range and Endurance Evaluation of a Camber Morphing Wing Aircraft.” Biomimetics 8 (1): 34. https://doi.org/10.3390/biomimetics8010034
• Joels, Tsoof, and Daniella E. Raveh. 2023. “Wing Dynamic Shape-Sensing from Fiber-Optic Strain Data Using the Kalman State Estimator.” Aerospace Science and Technology 137: 108286. https://doi.org/10.1016/j.ast.2023.108286
• Johns, Gerald. 1984. “Dictionary Making by Conference and Committee: NACA and the American Aeronautical Language, 1916–1934.” Journal of the American Society for Information Science 35 (2): 75–81. https://doi.org/10.1002/asi.4630350203
• Johnson, Clarence L. 1937. “Flight Test Research on a Small Bi-Motor Airplane.” Journal of the Aeronautical Sciences 4 (11): 473–77. https://doi.org/10.2514/8.473
• Johnson, Vicki S. 1990. “Minimizing Life Cycle Cost for Subsonic Commercial Aircraft.” Journal of Aircraft 27 (2): 139–45. https://doi.org/10.2514/3.45909
• Johnson, Heath, Chris Alba, Graham Candler, Matthew MacLean, Timothy Wadhams, and Michael Holden. 2008. “Boundary-Layer Stability Analysis of the Hypersonic International Flight Research Transition Experiments.” Journal of Spacecraft and Rockets 45 (2): 228–36. https://doi.org/10.2514/1.31878
• Johnson, C. B., and P. L. Lawing. 1977. “Mach 6 Flowfield Survey at the Engine Inlet of a Research Airplane.” Journal of Aircraft 14. https://ntrs.nasa.gov/citations/19770044769
• Jones, Matthew, Michael Goldstein, Philip Jonathan, and David Randell. 2016. “Bayes Linear Analysis for Bayesian Optimal Experimental Design.” Journal of Statistical Planning and Inference 171: 115–29. https://doi.org/10.1016/j.jspi.2015.10.011
• Jones, W. P., and B. M. Rao. 1970. “Compressibility Effects on Oscillating Rotor Blades in Hovering Flight.” AIAA Journal 8 (2): 321–29. https://doi.org/10.2514/3.5663
• Joshi, Ashok. 1996a. “Transonic Drag Effect of Single-Stage Space Vehicles.” Journal of Spacecraft and Rockets 33 (2): 308–308. https://doi.org/10.2514/3.55724
• Joshi, Ashok. 1996b. “Transonic Drag Effect on Vibration Characteristics of Single-Stage Space Vehicles.” Journal of Spacecraft and Rockets 33 (2): 308–9. https://doi.org/10.2514/3.26758
• Jumper, E. J. 1983. “Wave Drag Prediction Using a Simplified Supersonic Area Rule.” Journal of Aircraft 20 (10): 893–95. https://doi.org/10.2514/3.44961
• Jung, Jiwon, Yeunduk Jung, Dongil You, and David Hyunchul Shim. 2014. “A Flight Control System Design for Highly Unstable Unmanned Combat Aerial Vehicles.” In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2014.6842365
• Jung, Timothy P., Ryan P. Starkey, and Brian Argrow. 2012. “Methodology for Conducting Scaled Sonic-Boom Flight Tests Using Unmanned Aircraft Systems.” Journal of Aircraft 49 (5): 1234–44. https://doi.org/10.2514/1.c031449
• Junnai Zhai and R. Rebstock. 2003. “Advancement of 2D Profile Testing at High Reynolds Number in the Cryogenic Wind Tunnel Cologne.” In 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF ‘03.. IEEE. https://doi.org/10.1109/iciasf.2003.1274890
• Jurado, Juan D., and Clark C. McGehee. 2019. “Complete Online Algorithm for Air Data System Calibration.” Journal of Aircraft 56 (2): 517–28. https://doi.org/10.2514/1.c034964
• Jurado, Juan D., and Clark C. McGehee. 2024. “Non-Cooperative Full-Envelope Calibration of a Supersonic Air Data System.” In 2024 IEEE International Instrumentation and Measurement Technology Conference (I2MTC). IEEE. https://doi.org/10.1109/i2mtc60896.2024.10560820
• Kafkas, Angelos, Spyridon Kilimtzidis, Athanasios Kotzakolios, Vassilis Kostopoulos, and George Lampeas. 2021. “Multi-Fidelity Optimization of a Composite Airliner Wing Subject to Structural and Aeroelastic Constraints.” Aerospace 8 (12): 398. https://doi.org/10.3390/aerospace8120398
• Kalden, Osman. 2007. “Multidisciplinary Design & Trajectory Optimization of the Reusable Launch Vehicle Concept Hopper.” In 2007 3rd International Conference on Recent Advances in Space Technologies. IEEE. https://doi.org/10.1109/rast.2007.4283979
• Kanamori, Masashi, Takashi Takahashi, Yoshikazu Makino, Yusuke Naka, and Hiroaki Ishikawa. 2018. “Comparison of Simulated Sonic Boom in Stratified Atmosphere with Flight Test Measurements.” AIAA Journal 56 (7): 2743–55. https://doi.org/10.2514/1.j056155
• Kanapathipillai, Mithuun, and Kenneth H. Yu. 2024. “Regulating Scramjet Combustor Mode Transition Using Fuel Distribution Control.” Proceedings of the Combustion Institute 40 (1–4): 105414. https://doi.org/10.1016/j.proci.2024.105414
• Kanazaki, Masahiro, and Nao Setoguchi. 2023. “Characteristics of Vortices around Forward Swept Wing at Low Speeds/High Angles of Attack.” Aerospace 10 (9): 790. https://doi.org/10.3390/aerospace10090790
• Kang, Young-Shin, Bum-jin Park, Am Cho, Chang-sun Yoo, and Seong-wook Choi. 2013. “Envelop Expansion Flight Test of Flight Control Systems for TR-60 Tilt-Rotor UAV.” In 2013 13th International Conference on Control, Automation and Systems (ICCAS 2013). IEEE. https://doi.org/10.1109/iccas.2013.6704245
• Karpel, Mordechay. 1982. “Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling.” Journal of Aircraft 19 (3): 221–27. https://doi.org/10.2514/3.57379
• Karpuk, Stanislav, and Valerio Mosca. 2024. “Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective.” Journal of Aircraft 61 (6): 1629–54. https://doi.org/10.2514/1.c037744
• Kassem, Mohammed, Zhichun Yang, Yingsong Gu, Wei Wang, and Ehab Safwat. 2020. “Active Dynamic Vibration Absorber for Flutter Suppression.” Journal of Sound and Vibration 469: 115110. https://doi.org/10.1016/j.jsv.2019.115110
• Kato, Kanenori, Takeshi Kanda, Kan Kobayashi, Kenji Kudo, and Atsuo Murakami. 2006. “Downstream Ramjet-Mode Combustion in a Dual-Mode Scramjet Engine.” Journal of Propulsion and Power 22 (3): 511–17. https://doi.org/10.2514/1.17547
• Kaul, Upender K. 2024. “Machine Learning of Unsteady Transonic Aerodynamics of a Pitching Truss-Braced Wing Section.” Aerospace Science and Technology 152: 109376. https://doi.org/10.1016/j.ast.2024.109376
• Keesman, Karel J. 2015. “Optimal Input Design for Parameter Estimation in Nonlinear State-Space Models Using Pontryagin’s Minimum Principle.” IFAC-PapersOnLine 48 (28): 1319–24. https://doi.org/10.1016/j.ifacol.2015.12.314
• Keesman, Karel J. 2018. “Optimal Input Design for Minimum-Variance Estimation of Parameters in Nonlinear State-Space Models.” IFAC-PapersOnLine 51 (15): 365–70. https://doi.org/10.1016/j.ifacol.2018.09.172
• Keisler, Jeffrey M., and Mark Brodfuehrer. 2009. “An Application of Value-of-Information to Decision Process Reengineering.” Engineering Economist 54 (3): 197–221. https://doi.org/10.1080/00137910903108286
• Keller, D. 2019. “High-Lift Design for a Forward Swept Natural Laminar Flow Wing.” CEAS Aeronautical Journal 11 (1): 81–92. https://doi.org/10.1007/s13272-019-00396-z
• Kemp, Nelson H. 1960. “Hydromagnetic Effects on Heating and Shear at a Three-Dimensional Stagnation Point in Hypersonic Flow.” Journal of the Aerospace Sciences 27 (7): 553–54. https://doi.org/10.2514/8.8637
• Kidd, Rex O. 1966. “Application of Statistical Experimental Design Techniques to Flight-Test Programs.” Journal of Aircraft 3 (1): 67–72. https://doi.org/10.2514/3.43709
• Kiehn, Daniel. 2020. “Stability Analysis and Flight Control Design of the Winged Reusable Launch Vehicle ReFEx.” CEAS Space Journal 13 (1): 51–64. https://doi.org/10.1007/s12567-020-00319-3
• Kieß, Alexander, Joachim Siegel, Eskil Jonas Nussbaumer, and Andreas Strohmayer. 2026. “Steps towards the Validation of the Simplified Automated Approach for a Preliminary Safety Assessment via Scaled Flight Testing.” Aerospace 13 (4): 343. https://doi.org/10.3390/aerospace13040343
• Kilgore, R. A., and D. A. Dress. 1984. “The Application of Cryogenics to High Reynolds Number Testing in Wind Tunnels. Part 2: Development and Application of the Cryogenic Wind Tunnel Concept.” Cryogenics 24 (9): 484–93. https://doi.org/10.1016/0011-2275(84)90007-9
• Kim, Youngjoo, Wooyoung Jung, Chanho Kim, Seongheon Lee, Kihyeon Tahk, and Hyochoong Bang. 2015. “Development of Multiple Unmanned Aircraft System and Flight Experiment.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152335
• Kim, Hyoungjin, and Minsul Lee. 2021. “Flow Simulation of a Supersonic Airplane with Installed Engine Nacelle.” Aerospace Science and Technology 117: 106900. https://doi.org/10.1016/j.ast.2021.106900
• Kim, B. S., M. L. Rasmussen, and M. C. Jischke. 1983. “Optimization of Waverider Configurations Generated from Axisymmetricconical Flows.” Journal of Spacecraft and Rockets 20 (5): 461–69. https://doi.org/10.2514/3.25630
• Kirkham, F. S., L. Robert Jackson, and John P. Weidner. 1975b. “Study of a High-Speed Research Airplane.” Journal of Aircraft 12 (11): 857–63. https://doi.org/10.2514/3.59885
• Kirsch, Bertrand, Olivier Montagnier, Emmanuel Bénard, and Thierry M. Faure. 2020. “Tightly Coupled Aeroelastic Model Implementation Dedicated to Fast Aeroelastic Tailoring Optimisation of High Aspect Ratio Composite Wing.” Journal of Fluids and Structures 94: 102930. https://doi.org/10.1016/j.jfluidstructs.2020.102930
• Kish, Brian A., Matthew Rhoney, Ralph D. Kimberlin, Katarina Vuckovic, and Erfan Attarian. 2017. “Wing Bug: A Portable, Low-Cost Flight Test Instrumentation System.” In 2017 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2017.7943672
• Kishi, Yuki, Masahiro Kanazaki, and Yoshikazu Makino. 2022. “Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization.” Journal of Aircraft 59 (4): 1027–40. https://doi.org/10.2514/1.c036422
• Kivel, Bennett. 1961. “Radiation from Hot Air and Its Effect on Stagnation-Point Heating.” Journal of the Aerospace Sciences 28 (2): 96–102. https://doi.org/10.2514/8.8883
• Klein, V., and J. G. Batterson. 1986. “Aerodynamic Parameters Estimated from Flight and Wind Tunnel Data.” Journal of Aircraft 23 (4): 306–12. https://doi.org/10.2514/3.45304
• Klein, V., and E. A. Morelli. 1992. “Parameter Estimation of a Highly Augmented Aircraft from Flight Data.” IFAC Proceedings Volumes 25 (15): 181–86. https://doi.org/10.1016/s1474-6670(17)50630-8
• Klepl, Martin J. 1995. “Digital Flutter Suppression of Active Flexible Wing Using Moment Feedback.” Journal of Aircraft 32 (1): 205–6. https://doi.org/10.2514/3.46702
• Klingenberg, Christoph, and Jan Loic Belke. 2024. “Profitability of Supersonic Travel.” Journal of Air Transport Management 117: 102581. https://doi.org/10.1016/j.jairtraman.2024.102581
• Klothakis, Angelos, and Ioannis K. Nikolos. 2024. “Design and Evaluation of a Hypersonic Waverider Vehicle Using DSMC.” Computation 12 (7): 140. https://doi.org/10.3390/computation12070140
• Kluever, Craig A., and David A. Neal. 2015. “Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle.” Journal of Guidance, Control, and Dynamics 38 (11): 2057–66. https://doi.org/10.2514/1.g000909
• Knoedler, A. J., W. D. Bailey, B. H. McClintock, and D. A. Harris. n.d. “Investigation of Global Positioning System Use for Air Data System Calibration.” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509128
• Koedprayodsuk, Patcharaphon, Nopdanai Ajavakom, and Niphon Wansophark. 2025. “Comparative Study on Aeroelastic Control Laws for NACA 0012 and NACA 64A010.” In 2025 8th International Conference on Robotic Systems and Applications (ICRSA). IEEE. https://doi.org/10.1109/icrsa66467.2025.11383791
• Kohlman, David L. 1979. “Flight Test Results for an Advanced Technology Light Airplane.” Journal of Aircraft 16 (4): 250–55. https://doi.org/10.2514/3.58513
• Koo, K. N., and I. Lee. 1994. “Aeroelastic Behavior of a Composite Plate Wing with Structural Damping.” Computers & Structures 50 (2): 167–76. https://doi.org/10.1016/0045-7949(94)90293-3
• Koohi, Reza, Hossein Shahverdi, and Hassan Haddadpour. 2014. “Nonlinear Aeroelastic Analysis of a Composite Wing by Finite Element Method.” Composite Structures 113: 118–26. https://doi.org/10.1016/j.compstruct.2014.03.012
• Korsun, O. N., B. K. Poplavsky, and S. Ju. Prihodko. 2017. “Intelligent Support for Aircraft Flight Test Data Processing in Problem of Engine Thrust Estimation.” Procedia Computer Science 103: 82–87. https://doi.org/10.1016/j.procs.2017.01.017
• Kou, Peng, Yuanhang Zhang, Zhihao Zhang, and Deliang Liang. 2023. “Optimal Arrangement of Electric Motors for Distributed Electric Propulsion Aircraft Using Generalized Benders Decomposition.” In 2023 IEEE Energy Conversion Congress and Exposition (ECCE). IEEE. https://doi.org/10.1109/ecce53617.2023.10362151
• Kouchi, Toshinori, Goro Masuya, Tohru Mitani, and Sadatake Tomioka. 2012. “Mechanism and Control of Combustion-Mode Transition in a Scramjet Engine.” Journal of Propulsion and Power 28 (1): 106–12. https://doi.org/10.2514/1.b34172
• Koval, Karina, and Ruanui Nicholson. 2025. “Non-Intrusive Optimal Experimental Design for Large-Scale Nonlinear Bayesian Inverse Problems Using a Bayesian Approximation Error Approach.” Journal of Scientific Computing 104 (3): 98. https://doi.org/10.1007/s10915-025-03008-7
• Kraiko, A. N., and N. I. Tilliaeva. 1973. “On Constructing the Contour of Minimum Wave Drag in an Inhomogeneous Supersonic Flow.” Journal of Applied Mathematics and Mechanics 37 (3): 449–67. https://doi.org/10.1016/0021-8928(73)90088-9
• Kratochvíl, Aleš, and Jakub Valenta. 2024. “Active Flutter Suppression for Light Sport Aircraft by a Control Surface Split.” CEAS Aeronautical Journal 15 (4): 977–98. https://doi.org/10.1007/s13272-024-00745-7
• Krüger, Wolf R., Thomas Klimmek, René Liepelt, Hauke Schmidt, Stefan Waitz, and Sunpeth Cumnuantip. 2014. “Design and Aeroelastic Assessment of a Forward-Swept Wing Aircraft.” CEAS Aeronautical Journal 5 (4): 419–33. https://doi.org/10.1007/s13272-014-0117-0
• Krüger, Wolf R., Yasser M. Meddaikar, Johannes K. S. Dillinger, Jurij Sodja, and Roeland De Breuker. 2022. “Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing.” Aerospace 9 (10): 535. https://doi.org/10.3390/aerospace9100535
• Kubota, Hirotoshi. 2008. “Introduction: Supersonic Airplane.” Journal of Aircraft 45 (5): 1473–1473. https://doi.org/10.2514/1.37180
• Kukreja, Sunil L. 2008b. “Structure Computation of Quiet Spike Flight-Test Data during Envelope Expansion.” Journal of Aircraft 45 (5): 1579–84. https://doi.org/10.2514/1.32799
• Kukreja, Sunil L. 2008c. “Structure Computation of Quiet Spike[Trademark] Flight-Test Data during Envelope Expansion.” Journal of Aircraft 45 (5). https://ntrs.nasa.gov/citations/20080041566
• Kumar, Rajan, Ranjan Ganguli, S. N. Omkar, and M. Vijaya Kumar. 2008. “Rotorcraft Parameter Identification from Real Time Flight Data.” Journal of Aircraft 45 (1): 333–41. https://doi.org/10.2514/1.32024
• Kuntz, David W., and Donald L. Potter. 2008. “Boundary-Layer Transition and Hypersonic Flight Testing.” Journal of Spacecraft and Rockets 45 (2): 184–92. https://doi.org/10.2514/1.29708
• Laban, Martin, and Kazuya Masui. 1993. “Total Least Squares Estimation of Aerodynamic Model Parameters from Flight Data.” Journal of Aircraft 30 (1): 150–52. https://doi.org/10.2514/3.46327
• Lampropoulos, Nikolaos K., Ioannis E. Sarris, Spyridon Antoniou, Odysseas Ziogas, Pericles Panagiotou, and Kyros Yakinthos. 2025. “Aerodynamic Performance of a Natural Laminar Flow Swept-Back Wing for Low-Speed UAVs under Take Off/Landing Flight Conditions and Atmospheric Turbulence.” Aerospace 12 (10): 934. https://doi.org/10.3390/aerospace12100934
• Lange, Roy H. 1984. “Design Integration of Laminar Flow Control for Transport Aircraft.” Journal of Aircraft 21 (8): 612–17. https://doi.org/10.2514/3.45031
• Lanjun Li, Shouyi Yu, N. Kawai, and H. Matsushita. 2006. “Active Flutter Suppression Control Using Piezo-Ceramic Actuators.” In 2006 6th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2006.1714300
• Larrabee, E. Eugene. 1967. “Aerodynamic Penetration and Radius as Unifying Concepts in Flight Mechanics.” Journal of Aircraft 4 (1): 28–35. https://doi.org/10.2514/3.43790
• Lavi, R. 1967. “An Experimental Investigation of VTOL Lift- Engine Inlet.” Journal of Aircraft 4 (2): 125–32. https://doi.org/10.2514/3.43808
• Le Clainche, Soledad, Rubén Moreno-Ramos, Paul Taylor, and José M. Vega. 2019. “New Robust Method to Study Flight Flutter Testing.” Journal of Aircraft 56 (1): 336–43. https://doi.org/10.2514/1.c034863
• Lee, B. H. K. 1989. “Investigation of Flow Separation on a Supercritical Airfoil.” Journal of Aircraft 26 (11): 1032–37. https://doi.org/10.2514/3.45876
• Lee, D. Jin, Byoung-Mun Min, Min-Jea Tahk, Hyochoong Bang, and D. H. Shim. 2008. “Autonomous Flight Control System Design for a Blended Wing Body.” In 2008 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2008.4694548
• Lee, Seunghoon, Jindeog Chung, Taehwan Cho, and Hakmin Lee. 2027. “Comparison of Full-Scale and Wind-Tunnel Airwake Measurements over a Flat-Top Flight Deck.” Aerospace Science and Technology 180: 114024. https://doi.org/10.1016/j.ast.2026.114024
• Lee, Robert A., and J. Micah Downing. 1996a. “Boom Event Analyzer Recorder: Unmanned Sonic Boom Monitor.” Journal of Aircraft 33 (1): 171–75. https://doi.org/10.2514/3.46918
• Lee, Chang-Yull, and Ji-Hwan Kim. 2021a. “Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators.” Aerospace 8 (9): 257. https://doi.org/10.3390/aerospace8090257
• Lee, Hansoo, Jonggeun Kim, Sungshin Kim, and Jaeyong Kim. 2019. “A Comparative Study on Air Data System Calibration Methods Based on Machine Learning.” In 2019 IEEE International Conference on Fuzzy Systems (FUZZ-IEEE). IEEE. https://doi.org/10.1109/fuzz-ieee.2019.8858867
• Lee, In, Seung-Ho Kim, and Hirokazu Miura. 1994. “Static Aeroelastic Characteristics of a Composite Wing.” Journal of Aircraft 31 (6): 1413–16. https://doi.org/10.2514/3.46667
• Lee, T., and L. S. Ko. 2009. “Vortex Wake Generated behind a Forward Swept Wing.” Journal of Aircraft 46 (2): 717–21. https://doi.org/10.2514/1.39352
• Lee, Donguk, and Kwanjung Yee. 2024. “Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design.” Journal of Aircraft 61 (2): 375–91. https://doi.org/10.2514/1.c037225
• Lee, Junghoon, and Sugjoon Yoon. 2008. “Estimation and Validation of Lateral-Directional Stability/control Derivatives for the Flight Training Device of a Light Aircraft.” Simulation Modelling Practice and Theory 16 (1): 1–14. https://doi.org/10.1016/j.simpat.2007.08.009
• Lees, Lester. 1956. “Laminar Heat Transfer over Blunt-Nosed Bodies at Hypersonic Flight Speeds.” Journal of Jet Propulsion 26 (4): 259–69. https://doi.org/10.2514/8.6977
• Legrand, Baptiste, Arnaud Gaillard, and David Bouquain. 2025. “Comparative Study of Hybrid Electric Distributed Propulsion Aircraft through Multiple Powertrain Component Modeling Approaches.” Aerospace 12 (8): 732. https://doi.org/10.3390/aerospace12080732
• Leitch, Harry J., Olivia Stodieck, and Jie Yuan. 2025. “The Influence of Coupled Thickness Variation in the Aeroelastic Response of Continuous Tow Sheared Composite Wing.” Composite Structures 374: 119706. https://doi.org/10.1016/j.compstruct.2025.119706
• Lemko, O. L., and O. D. Molodchyk. 2015. “Aerodynamic and Flight Characteristics of Prospective UAV Scheme “Flying Wing”.” In 2015 IEEE International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD). IEEE. https://doi.org/10.1109/apuavd.2015.7346552
• Lemley, C. E., and R. E. Mullans. 1974. “Transonic Wind-Tunnel and Flight Buffet Pressures on a Swept Wing.” Journal of Aircraft 11 (3): 173–77. https://doi.org/10.2514/3.60344
• Leng, Jun-xue, Zhen-guo Wang, and Wei Huang. 2024. “Design and Investigation on the Combined Two-Stage Waverider Equipped with Rocket and Scramjet Engine.” Energy 304: 132076. https://doi.org/10.1016/j.energy.2024.132076
• Leng, Jun-xue, Zan Xie, Wei Huang, Yang Shen, and Zhen-guo Wang. 2025. “Multidisciplinary Design Optimization of the First-Stage Waverider Based on Boost-Glide Flight Trajectory.” Aerospace Science and Technology 160: 110033. https://doi.org/10.1016/j.ast.2025.110033
• Lengyan and Qian Zhansen. 2015. “A CFD Based Sonic Boom Prediction Method and Investigation on the Parameters Affecting the Sonic Boom Signature.” Procedia Engineering 99: 433–51. https://doi.org/10.1016/j.proeng.2014.12.558
• Lepsien, Arthur, Philipp Kügler, and Alexander Schaum. 2025. “On the Structural Analysis and Optimal Input Design for Joint State and Parameter Estimation.” IEEE Access 13: 211944–59. https://doi.org/10.1109/access.2025.3636666
• Leylek, Emily A., and Mark Costello. 2015. “Use of Compliant Hinges to Tailor Flight Dynamics of Unmanned Aircraft.” Journal of Aircraft 52 (5): 1692–1706. https://doi.org/10.2514/1.c033056
• Li, Feng-Ming. 2012. “Active Aeroelastic Flutter Suppression of a Supersonic Plate with Piezoelectric Material.” International Journal of Engineering Science 51: 190–203. https://doi.org/10.1016/j.ijengsci.2011.10.003
• Li, Li, Junqiang Bai, and Feng Qu. 2022a. “Multipoint Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft.” Journal of Aircraft 59 (5): 1179–94. https://doi.org/10.2514/1.c036413
• Li, Tong, and Rui Cao. 2025. “Flight Control System for Gull-Wing Morphing Aircraft Based on DDPG.” In 2025 7th International Conference on Electronic Engineering and Informatics (EEI). IEEE. https://doi.org/10.1109/eei67650.2025.11334790
• Li, Wu, and Karl Geiselhart. 2021. “Integration of Low-Fidelity MDO and CFD-Based Redesign of Low-Boom Supersonic Transports.” AIAA Journal 59 (10): 3923–36. https://doi.org/10.2514/1.j060368
• Li, Maomao, and Jun Hu. 2018. “An Approach and Landing Guidance Design for Reusable Launch Vehicle Based on Adaptive Predictor–corrector Technique.” Aerospace Science and Technology 75: 13–23. https://doi.org/10.1016/j.ast.2017.12.037
• Li, Qiaochu, Carine Jauberthie, Lilianne Denis-Vidal, and Zohra Cherfi. 2017c. “Parameter Estimation Enhanced by Optimal Input Design in a Bounded-Error Context.” IFAC-PapersOnLine 50 (1): 6277–82. https://doi.org/10.1016/j.ifacol.2017.08.862
• Li, Wenyuan, Yi Ji, and Guanghui Sun. 2026d. “Reusable Launch Vehicle Landing Online Guidance and Control Based on ESO-MPC and Convex Optimization.” IEEE Access 14: 30860–71. https://doi.org/10.1109/access.2026.3667479
• Li, Changshu, Guiqian Jiao, Jie Li, Yuxuan Wang, Jianping Li, and Wenyan Song. 2026a. “Control-Oriented Experimental Investigation of Combustion Mode Transition Hysteresis in Dual-Mode Scramjet.” Aerospace Science and Technology 168: 111255. https://doi.org/10.1016/j.ast.2025.111255
• Li, Jianping, Rongjia Jin, Guiqian Jiao, and Wenyan Song. 2017a. “Analysis on Mode Transition in a Dual-Mode Scramjet Combustor.” Combustion Science and Technology 190 (1): 82–96. https://doi.org/10.1080/00102202.2017.1376190
• Li, Jiahe, Yanming Liu, and Jiang Wang. 2022c. “Transonic Airfoil Drag Reduction Using Suction and Loaded Leading Edge Control.” Journal of Thermal Science 32 (1): 264–77. https://doi.org/10.1007/s11630-022-1687-5
• Li, Li, Lei Qiao, Jiakuan Xu, and Junqiang Bai. 2023. “Effects of Static Stability Margin on Aerodynamic Design Optimization of Truss-Braced Wing Aircraft.” Aerospace 10 (7): 603. https://doi.org/10.3390/aerospace10070603
• Li, Li, Lei Qiao, Jiakuan Xu, and Junqiang Bai. 2026c. “Improved Aerodynamic-Propulsion Interaction Model for Distributed-Electric-Propulsion System and Its Integration in Sizing for Hybrid-Electric Distributed-Propulsion Aircraft.” Aerospace Science and Technology 170: 111519. https://doi.org/10.1016/j.ast.2025.111519
• Li, Jianping, Kai Wang, Guiqian Jiao, Jinyuan Luo, and Wenyan Song. 2019b. “Experimental Study on Mode Transition in a Dual-Mode Scramjet Combustor.” Combustion Science and Technology 192 (5): 852–70. https://doi.org/10.1080/00102202.2019.1594800
• Li, Zhiquan, and Pinqi Xia. 2017. “Aeroelastic Stability of Full-Span Tiltrotor Aircraft Model in Forward Flight.” Chinese Journal of Aeronautics 30 (6): 1885–94. https://doi.org/10.1016/j.cja.2017.09.007
• Li, Haiquan, Wenzhe Xu, Yun Zhao, et al. 2025a. “Dynamics Modeling and Analysis of a Vertical Landing Mechanism for Reusable Launch Vehicle.” Aerospace 12 (4): 280. https://doi.org/10.3390/aerospace12040280
• Li, Jiacheng, Jie Yang, and Haibo Zhang. 2022b. “Research on Modeling and Fault-Tolerant Control of Distributed Electric Propulsion Aircraft.” Drones 6 (3): 78. https://doi.org/10.3390/drones6030078
• Li, Li, Yu Zhang, Junqiang Bai, and Vassili Toropov. 2024. “Morphing Wing Design of Truss-Braced-Wing Aircraft through Aerodynamic Shape Optimization Using the Adjoint Method.” Engineering Optimization 57 (10): 2922–59. https://doi.org/10.1080/0305215x.2024.2420746
• Liaoni Wu, Yimin Huang, and ChengLong He. 2008. “Reusable Launch Vehicle Lateral Control Design on Suborbital Reentry.” In 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2008.4776287
• Librescu, L., and A. A. Khdeir. 1988. “Aeroelastic Divergence of Swept-Forward Composite Wings Including Warping Restraint Effect.” AIAA Journal 26 (11): 1373–77. https://doi.org/10.2514/3.10050
• Librescu, L., and J. Simovich. 1988. “General Formulation for the Aeroelastic Divergence of Composite Swept-Forward Wing Structures.” Journal of Aircraft 25 (4): 364–71. https://doi.org/10.2514/3.45572
• Librescu, Liviu, and Ohseop Song. 1992. “On the Static Aeroelastic Tailoring of Composite Aircraft Swept Wings Modelled as Thin-Walled Beam Structures.” Composites Engineering 2 (5–7): 497–512. https://doi.org/10.1016/0961-9526(92)90039-9
• Librescu, Liviu, and Surot Thangjitham. 1991. “Analytical Studies on Static Aeroelastic Behavior of Forward-Swept Composite Wing Structures.” Journal of Aircraft 28 (2): 151–57. https://doi.org/10.2514/3.46004
• Lichota, Piotr, Krzysztof Sibilski, and Per Ohme. 2017. “D-Optimal Simultaneous Multistep Excitations for Aircraft Parameter Estimation.” Journal of Aircraft 54 (2): 747–58. https://doi.org/10.2514/1.c033794
• Licitra, G., A. Bürger, P. Williams, R. Ruiterkamp, and M. Diehl. 2018. “Optimal Input Design for Autonomous Aircraft.” Control Engineering Practice 77: 15–27. https://doi.org/10.1016/j.conengprac.2018.04.013
• Liebhardt, Bernd, Florian Linke, and Katrin Dahlmann. 2014. “Supersonic Deviations: Assessment of Sonic-Boom-Restricted Flight Routing.” Journal of Aircraft 51 (6): 1987–96. https://doi.org/10.2514/1.c032591
• Liebhardt, Bernd, Florian Linke, and Martin Knaack. 2022. “Supersonic Overland without a Sonic Boom: Quantitative Assessment of Mach-Cutoff Flight.” Journal of Aircraft 59 (5): 1257–66. https://doi.org/10.2514/1.c036637
• Liebst, Bradley S. 1987. “Accelerometer Placement in Active Flutter Suppression Systems.” Journal of Guidance, Control, and Dynamics 10 (5): 441–46. https://doi.org/10.2514/3.20238
• Liu, Chuanzhen, and Peng Bai. 2024. “Waverider Design Using Osculating Method.” AIAA Journal 62 (5): 1643–61. https://doi.org/10.2514/1.j063558
• Liu, Yan, Junqiang Bai, and Eli Livne. 2017c. “Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap Static Aeroelastic Action.” AIAA Journal 55 (3): 1031–43. https://doi.org/10.2514/1.j055054
• Liu, Ningjun, Zhihao Cai, Yingxun Wang, and Jiang Zhao. 2021a. “Fast Level-Flight to Hover Mode Transition and Altitude Control in Tiltrotor’s Landing Operation.” Chinese Journal of Aeronautics 34 (1): 181–93. https://doi.org/10.1016/j.cja.2020.09.041
• Liu, Zhenyu, Wesley W. Chu, Adam Huang, Chris Folk, and Chih-Ming Ho. 2001. “Mining Sequence Patterns from Wind Tunnel Experimental Data for Flight Control.” In Advances in Knowledge Discovery and Data Mining. Springer Berlin Heidelberg. https://doi.org/10.1007/3-540-45357-1_30
• Liu, Yang, Chaoyang Dong, Wenqiang Zhang, and Qing Wang. 2021b. “Phase Plane Design Based Fast Altitude Tracking Control for Hypersonic Flight Vehicle with Angle of Attack Constraint.” Chinese Journal of Aeronautics 34 (2): 490–503. https://doi.org/10.1016/j.cja.2020.04.026
• Liu, Haojie, Xiumin Gao, and Xiao Wang. 2020b. “Parametric Active Aeroelastic Control of a Morphing Wing Using the Receptance Method.” Journal of Fluids and Structures 98: 103098. https://doi.org/10.1016/j.jfluidstructs.2020.103098
• Liu, Chuanzhen, Shiyu Jia, Jifei Wang, and Peng Bai. 2026b. “Design and Optimization of Planform-Customized Waverider with Multistage Compression Flow.” Aerospace Science and Technology 179: 113366. https://doi.org/10.1016/j.ast.2026.113366
• Liu, Junchao, Luyi Li, and Hao Wang. 2026c. “Model Validation under Interval Uncertainty: A Novel Metric and Computational Framework with Engineering Applications.” Aerospace Science and Technology 177: 112780. https://doi.org/10.1016/j.ast.2026.112780
• Liu, Yang, Yongjie Shi, and Guohua Xu. 2026a. “Automatic Helicopter Flight Based on Wind-Induced Threat Identification in Urban Environments.” Chinese Journal of Aeronautics 39 (3): 103909. https://doi.org/10.1016/j.cja.2025.103909
• Liu, Guangyuan, Yang Tao, Qiuting Guo, and Yan Sun. 2012b. “Transonic Drag Reduction with Contour Bump on a Supercritical Airfoil.” In 2012 Second International Conference on Intelligent System Design and Engineering Application. IEEE. https://doi.org/10.1109/isdea.2012.624
• Liu, Fan, Lixin Wang, and Xiangsheng Tan. 2015a. “Digital Virtual Flight Testing and Evaluation Method for Flight Characteristics Airworthiness Compliance of Civil Aircraft Based on HQRM.” Chinese Journal of Aeronautics 28 (1): 112–20. https://doi.org/10.1016/j.cja.2014.12.013
• Liu, Chuanzhen, Rui Wu, Peng Bai, and Xufei Meng. 2026d. “Waverider Design Given Leading Edge from Axisymmetric Flow.” Journal of Aircraft: 1–9. https://doi.org/10.2514/1.c039065
• Liu, Xiangdong, Fengdi Zhang, Zhen Li, and Yao Zhao. 2017a. “Approach and Landing Guidance Design for Reusable Launch Vehicle Using Multiple Sliding Surfaces Technique.” Chinese Journal of Aeronautics 30 (4): 1582–91. https://doi.org/10.1016/j.cja.2017.06.008
• Liu, Wen, Chen-An Zhang, Fa-Min Wang, and Zheng-Yin Ye. 2020a. “Design and Optimization Method for Hypersonic Quasi-Waverider.” AIAA Journal 58 (5): 2132–46. https://doi.org/10.2514/1.j059087
• Livingston, F. R., and J. W. Williard. 1971. “Planetary Entry Body Heating Rate Measurements in Air and Venus Atmospheric Gas up to T Equals 15,000 Deg K.” AIAA Journal 9 (3): 485–92. https://doi.org/10.2514/3.6207
• Livne, Eli. 2018. “Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs.” Journal of Aircraft 55 (1): 410–52. https://doi.org/10.2514/1.c034442
• Lo, K. W., B. G. Ferguson, Yujin Gao, and A. Maguer. 2003. “Aircraft Flight Parameter Estimation Using Acoustic Multipath Delays.” IEEE Transactions on Aerospace and Electronic Systems 39 (1): 259–68. https://doi.org/10.1109/taes.2003.1188908
• Lo, K. W., S. W. Perry, and B. G. Ferguson. 2002. “Aircraft Flight Parameter Estimation Using Acoustical Lloyd’s Mirror Effect.” IEEE Transactions on Aerospace and Electronic Systems 38 (1): 137–51. https://doi.org/10.1109/7.993235
• Lobbia, Marcus A. 2017. “Multidisciplinary Design Optimization of Waverider-Derived Crew Reentry Vehicles.” Journal of Spacecraft and Rockets 54 (1): 233–45. https://doi.org/10.2514/1.a33253
• Logsdon, John M., and Ray A. Williamson. 1997. “The Reusable Launch Vehicle Program.” Space Policy 13 (2): 95–96. https://doi.org/10.1016/s0265-9646(97)00010-6
• Lombardi, Giovanni, and Mauro Morelli. 1994. “Pressure Measurements on a Forward-Swept Wing-Canard Configuration.” Journal of Aircraft 31 (2): 469–72. https://doi.org/10.2514/3.46517
• Lombardi, G., M. Morelli, and D. Waller. 1996. “Boundary-Layer Transition on a Forward-Swept Wing in Canard Configuration.” Journal of Aircraft 33 (6): 1202–4. https://doi.org/10.2514/3.47077
• Lonkar, Sumit, and Pratikash P. Panda. 2026. “Mode Transition and Combustion-Induced Shock Train Dynamics in a Cavity-Based Dual-Mode Scramjet.” Aerospace Science and Technology 176: 112194. https://doi.org/10.1016/j.ast.2026.112194
• Lord, W. T., and E. Eminton. 1954. “Slender Bodies of Minimum Wave Drag.” Journal of the Aeronautical Sciences 21 (8): 569–70. https://doi.org/10.2514/8.3128
• Lottati, I. 1985. “Flutter and Divergence Aeroelastic Characteristics for Composite Forward Swept Cantilevered Wing.” Journal of Aircraft 22 (11): 1001–7. https://doi.org/10.2514/3.45238
• Lottati, I. 1987. “Aeroelastic Stability Characteristics of a Composite Swept Wing Withtip Weights for an Unrestrained Vehicle.” Journal of Aircraft 24 (11): 793–802. https://doi.org/10.2514/3.45523
• Lottati, I. 1988. “Aeroelastic Tailoring of a Composite Wing with a Decoupler Pylon as a Wing/store Flutter Suppressor.” Journal of Aircraft 25 (3): 271–80. https://doi.org/10.2514/3.45588
• Louisse, Jan, and Franklin L. Marshall. 1976. “Prediction of Ground Effects for VTOL Aircraft with Twin Lifting Jets.” Journal of Aircraft 13 (2): 123–27. https://doi.org/10.2514/3.58641
• Lu, Han-Hsun, Joshua Harris, Vinicius Guimaraes Goecks, Ezekiel Bowden, and John Valasek. 2017b. “Flight Test Instrumentation System for Small UAS System Identification.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991399
• Lu, Pong-Jeu, and Li-Jeng Huang. 1992. “Flutter Suppression of Thin Airfoils Using Active Acoustic Excitations.” AIAA Journal 30 (12): 2873–81. https://doi.org/10.2514/3.11632
• Lu, Pong-Jeu, Dartzi Pan, and Dun-Yann Yeh. 1995. “Transonic Flutter Suppression Using Active Acoustic Excitations.” AIAA Journal 33 (4): 694–702. https://doi.org/10.2514/3.12633
• Lu, Weishuang, Yun Tian, and Peiqing Liu. 2017a. “Aerodynamic Optimization and Mechanism Design of Flexible Variable Camber Trailing-Edge Flap.” Chinese Journal of Aeronautics 30 (3): 988–1003. https://doi.org/10.1016/j.cja.2017.03.003
• Lu, Shiguang, Jianfeng Wang, and Yanling Wang. 2021. “Research on Similarity Criteria of Virtual Flight Test in Low-Speed Wind Tunnel.” In 2021 IEEE International Conference on Power, Intelligent Computing and Systems (ICPICS). IEEE. https://doi.org/10.1109/icpics52425.2021.9524290
• Lu, Yi, Shu-Guang Zhang, Lian Hao, Hua-Yan Huangfu, and Hang Sheng. 2016. “System Dynamics Modeling of the Safety Evolution of Blended-Wing-Body Subscale Demonstrator Flight Testing.” Safety Science 89: 219–30. https://doi.org/10.1016/j.ssci.2016.06.018
• Lu, Yi, Shu-Guang Zhang, Peng Tang, and Lei Gong. 2015. “STAMP-Based Safety Control Approach for Flight Testing of a Low-Cost Unmanned Subscale Blended-Wing-Body Demonstrator.” Safety Science 74: 102–13. https://doi.org/10.1016/j.ssci.2014.12.005
• Lu, Yi, Shuguang Zhang, Zejing Zhang, Xuan Zhang, Peng Tang, and Shan Fu. 2019. “Multiple Hierarchy Risk Assessment with Hybrid Model for Safety Enhancing of Unmanned Subscale BWB Demonstrator Flight Test.” Chinese Journal of Aeronautics 32 (12): 2612–26. https://doi.org/10.1016/j.cja.2019.09.010
• Luecke, G. 1957. “Flight Test Data System Victor System 272.” IRE Transactions on Telemetry and Remote Control TRC-3 (1): 1–16. https://doi.org/10.1109/irettrc.1957.6541492
• Luo, Xinrui, Kai Shen, Zhihong Deng, Jiatong Wu, and Zhihao Jiang. 2026b. “Neural Predictive Control for High-Spinning Flight Vehicles: A Fokker–Planck Uncertainty Control Framework.” Chinese Journal of Aeronautics 39 (6): 103764. https://doi.org/10.1016/j.cja.2025.103764
• Luo, Shibin, Jiaqi Tian, Chao Zhang, Yanbin Feng, and Jun Liu. 2026a. “Design and Optimization of Wide-Speed Double Swept Waverider Based on Curved-Cone Projection Method.” Chinese Journal of Aeronautics 39 (3): 103887. https://doi.org/10.1016/j.cja.2025.103887
• Luskin, Harold. 1950. “Predictions of Supersonic Airplane Performance.” Journal of the Aeronautical Sciences 17 (1): 5–12. https://doi.org/10.2514/8.1511
• Lyöri, Veijo, Ari Kilpelä, Guoyong Duan, Antti Mäntyniemi, and Juha Kostamovaara. 2007. “Pulsed Time-of-Flight Radar for Fiber-Optic Strain Sensing.” Review of Scientific Instruments 78 (2): 024705. https://doi.org/10.1063/1.2535634
• Ma, Yiyuan, Morteza Abouhamzeh, and Ali Elham. 2024. “Aerostructural Optimization and Comparative Study of Twin-Fuselage and Strut-Braced-Wing Aircraft Configurations.” Journal of Aircraft 61 (3): 839–56. https://doi.org/10.2514/1.c037388
• Ma, Yiyuan, Yongqi Du, Yue Wang, Keshi Zhang, and Zhonghua Han. 2026a. “Aerostructural Comparative Study of Composite Strut- and Truss-Braced Wing Configurations.” Journal of Aircraft 63 (4): 1596–1606. https://doi.org/10.2514/1.c038551
• Ma, TieLin, Pu Xue, LuLu Jiang, Xin Pan, and Gang Chen. 2025. “An Efficient and High-Precision Aerodynamic Modeling Method for Hypersonic Vehicle Optimization Design.” Aerospace Science and Technology 164: 110382. https://doi.org/10.1016/j.ast.2025.110382
• Ma, Yiyuan, Wei Zhang, Yizhe Zhang, Xingyu Zhang, and Yujiang Zhong. 2020. “Sizing Method and Sensitivity Analysis for Distributed Electric Propulsion Aircraft.” Journal of Aircraft 57 (4): 730–41. https://doi.org/10.2514/1.c035581
• Ma, Guangwei, Guoyan Zhao, Mingbo Sun, et al. 2026b. “The Shock-Assisted Self-Ignition Behavior and Combustion Transition Mechanisms in a Mach 8 Scramjet Combustor.” Combustion and Flame 285: 114721. https://doi.org/10.1016/j.combustflame.2025.114721
• Mach, Hung, Evan Grim, Oyvind Holmeide, and Chris Calley. 2007. “PTP Enabled Network for Flight Test Data Acquisition and Recording.” In 2007 IEEE International Symposium on Precision Clock Synchronization for Measurement, Control and Communication. IEEE. https://doi.org/10.1109/ispcs.2007.4383783
• Macha, John M. 1977. “Drag of Circular Cylinders at Transonic Mach Numbers.” Journal of Aircraft 14 (6): 605–7. https://doi.org/10.2514/3.58828
• Machin, Ricardo A., Christie S. Iacomini, Chris J. Cerimele, and Jenny M. Stein. 2001. “Flight Testing the Parachute System for the Space Station Crew Return Vehicle.” Journal of Aircraft 38 (5): 786–99. https://doi.org/10.2514/2.2854
• MacLean, R., J. Sullivan, and S. N. B. Murthy. 1992. “Hot Gas Environment around STOVL Aircraft in Ground Proximity. I: Experimental Study.” Journal of Aircraft 29 (1): 67–72. https://doi.org/10.2514/3.46126
• Mahindra, Raj. 1983. “Telemetry—a Powerful Tool for Aircraft Flight Testing.” IETE Journal of Research 29 (8): 348–56. https://doi.org/10.1080/03772063.1983.11453091
• Mahmoud, AbdelMageed, Zhou Hao, Chen Wanchun, and Liang Yang. 2017. “Ascent and Glide Trajectory Optimization for Hypersonic Vehicle.” In 2017 International Conference on Control, Artificial Intelligence, Robotics & Optimization (ICCAIRO). IEEE. https://doi.org/10.1109/iccairo.2017.35
• Maine, Richard E., and Kenneth W. Iliff. 1979. “Maximum Likelihood Estimation of Translational Acceleration Derivatives from Flight Data.” Journal of Aircraft 16 (10): 674–79. https://doi.org/10.2514/3.58588
• Malaek, S. M. B., Hojjat A. Izadi, and Mehrdad Pakmehr. 2006. “Flight Envelope Expansion in Landing Phase Using Classic, Intelligent and Adaptive Controllers.” Journal of Aircraft 43 (1): 91–101. https://doi.org/10.2514/1.13197
• Mallik, Wrik, Rakesh K. Kapania, and Joseph A. Schetz. 2015. “Effect of Flutter on the Multidisciplinary Design Optimization of Truss-Braced-Wing Aircraft.” Journal of Aircraft 52 (6): 1858–72. https://doi.org/10.2514/1.c033096
• Malmuth, N., C. C. Wu, and J. D. Cole. 1987. “Transonic Wave Drag Estimation and Optimization Using the Nonlinear Area Rule.” Journal of Aircraft 24 (3): 203–10. https://doi.org/10.2514/3.45417
• Mannai, Clifford. 1962. “Flight Test Instrumentation.” Journal of the Franklin Institute 274 (5): 403. https://doi.org/10.1016/0016-0032(62)91055-4
• Manuel, G. S., and W. A. Doty. 1991. “Flight Test Investigation of Certification Requirements for Laminar-Flow General Aviation Airplanes.” Journal of Aircraft 28 (10): 652–56. https://doi.org/10.2514/3.46078
• Mao, Xu, and Wei Cao. 2014. “Prediction of Hypersonic Boundary Layer Transition on Sharp Wedge Flow Considering Variable Specific Heat.” Applied Mathematics and Mechanics 35 (2): 143–54. https://doi.org/10.1007/s10483-014-1779-7
• Marano, Aniello Daniele, Marika Belardo, Jacopo Beretta, et al. 2022. “Aeroelastic Tailoring of the Next Generation Civil Tiltrotor Technological Demonstrator Composite Wing.” Aerospace 9 (7): 335. https://doi.org/10.3390/aerospace9070335
• Marchetti, Robert M. 1968. “Extraction of Aerodynamic Derivatives from Flight Data, Using an Analog Regression Technique.” Journal of Aircraft 5 (1): 22–26. https://doi.org/10.2514/3.43902
• Martellucci, Anthony. 1964. “Boundary-Layer Transition on a Slender Cone in Hypersonic Flow.” AIAA Journal 2 (4): 771–72. https://doi.org/10.2514/3.2425
• Martin, Alexandre, and Marco Panesi. 2022. “Radiative Transmission and Absorption within the Thermal Protection System of Atmospheric Entry Spacecraft.” Journal of Spacecraft and Rockets 59 (1): 348–52. https://doi.org/10.2514/1.a35029
• Marx, William J., Dimitri N. Mavris, and Daniel P. Schrage. 1998. “Cost/Time Analysis for Theoretical Aircraft Production.” Journal of Aircraft 35 (4): 637–46. https://doi.org/10.2514/2.2348
• Masson, Christian, Charles Veilleux, and Ion Paraschivoiu. 1998. “Airfoil Wave-Drag Prediction Using Euler Solutions of Transonic Flows.” Journal of Aircraft 35 (5): 748–53. https://doi.org/10.2514/2.2365
• Massuger, Louis. 1940. “Aero Engines and Their Laboratory Testing under Flight Conditions.” Journal of the Aeronautical Sciences 7 (11): 481–82. https://doi.org/10.2514/8.1217
• Masui, Kazuya. 1997. “Estimation of Aircraft Aerodynamic Derivatives from Flight Tests.” IFAC Proceedings Volumes 30 (11): 389–94. https://doi.org/10.1016/s1474-6670(17)42878-3
• Matthews, R. K., and J. C. Key. 1977. “Comparison of Wind-Tunnel and Flight-Test Heat-Transfer Measurements on a Pylon-Mounted Store.” Journal of Aircraft 14 (6): 565–68. https://doi.org/10.2514/3.58821
• Mauldin, Colonel Joe B. 1946. “German Development in the Field of Rocket Powered, Controlled Missiles.” Journal of the American Rocket Society 00 (65): 24–27. https://doi.org/10.2514/8.4078
• Mavriplis, Dimitri J., and David W. Levy. 2005. “Transonic Drag Prediction Using an Unstructured Multigrid Solver.” Journal of Aircraft 42 (4): 887–93. https://doi.org/10.2514/1.8233
• Mayr, Simon, Gernot Grabmair, and Johann Reger. 2015. “Input Design and Parameter Estimation with Open Source Tools.” IFAC-PapersOnLine 48 (1): 286–91. https://doi.org/10.1016/j.ifacol.2015.05.107
• Mazidi, A., S. A. Fazelzadeh, and P. Marzocca. 2011. “Flutter of Aircraft Wings Carrying a Powered Engine under Roll Maneuver.” Journal of Aircraft 48 (3): 874–83. https://doi.org/10.2514/1.c031080
• McFARLAND, R. P., and J. H. Robertson. 1963. “Effects of Winds Aloft on Loads of the Dyna-Soar Booster.” AIAA Journal 1 (5): 1171–73. https://doi.org/10.2514/3.1743
• McGregor, O. Wayne, and Robert A. White. 1970a. “Drag of Rectangular Cavities in Supersonic and Transonic Flow Including the Effects of Cavity Resonance.” AIAA Journal 8 (11): 1959–64. https://doi.org/10.2514/3.6032
• McGregor, O. Wayne, and R. A. White. 1970b. “SYNOPTIC: Drag of Rectangular Cavities in Supersonic and Transonic Flow Including the Effects of Cavity Resonance,.” AIAA Journal 8 (11): 1958–1958. https://doi.org/10.2514/3.49881
• McGurk, Michael, Olivia Stodieck, and Jie Yuan. 2024. “Probabilistic Aeroelastic Analysis of High-Fidelity Composite Aircraft Wing with Manufacturing Variability.” Composite Structures 329: 117794. https://doi.org/10.1016/j.compstruct.2023.117794
• McKinnis, Aaron, Dustin Hauptman, Shawn Keshmiri, and Mark Ewing. 2021. “Flight Test Validation of Adaptive Collision Avoidance Algorithms Using Multiple Unmanned Aircraft.” In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas51884.2021.9476780
• McMaster, John R., and Frederick L. Schenk. 1974. “Development of the F-12 Aircraft Flight Control System.” Journal of Aircraft 11 (4): 225–31. https://doi.org/10.2514/3.59224
• McTigue, John G., and Bertha M. Ryan. 1968. “Lifting-Body Research Vehicles in a Low-Speed Flight Test Program.” Annals of the New York Academy of Sciences 154 (2): 1014–32. https://doi.org/10.1111/j.1749-6632.1968.tb15241.x
• Meadows, Nicholas A., Joseph A. Schetz, Rakesh K. Kapania, Manav Bhatia, and Guclu Seber. 2012. “Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Transport Aircraft.” Journal of Aircraft 49 (6): 1844–56. https://doi.org/10.2514/1.c031695
• Mehra, R. 1974. “Optimal Input Signals for Parameter Estimation in Dynamic Systems–Survey and New Results.” IEEE Transactions on Automatic Control 19 (6): 753–68. https://doi.org/10.1109/tac.1974.1100701
• Mehra, R. K., D. E. Stepner, and J. S. Tyler. 1974. “Maximum Likelihood Identification of Aircraft Stability and Control Derivatives.” Journal of Aircraft 11. https://ntrs.nasa.gov/citations/19740040577
• Mele, Benedetto, Mario Ostieri, and Renato Tognaccini. 2017. “Aircraft Lift and Drag Decomposition in Transonic Flows.” Journal of Aircraft 54 (5): 1933–44. https://doi.org/10.2514/1.c034288
• Melvin, Josh, and Wei Zhao. 2024. “A Jacobi–Ritz Approach for Aeroelastic Analysis of Swept Distributed Propulsion Aircraft Wing.” Journal of Vibration and Acoustics 146 (3): 031002. https://doi.org/10.1115/1.4066309
• Mendez, Carlos, Soledad Le Clainche, Rubén Moreno-Ramos, and José M. Vega. 2021. “A New Automatic, Very Efficient Method for the Analysis of Flight Flutter Testing Data.” Aerospace Science and Technology 114: 106749. https://doi.org/10.1016/j.ast.2021.106749
• Meng, Yang, Chao An, Changchuan Xie, and Chao Yang. 2022b. “Conceptual Design and Flight Test of Two Wingtip-Docked Multi-Body Aircraft.” Chinese Journal of Aeronautics 35 (12): 144–55. https://doi.org/10.1016/j.cja.2022.01.020
• Meng, Xufei, Peng Bai, and Chuanzhen Liu. 2025. “Planform-Customized Waverider Design Using Flows with Variable Mach Numbers.” Aerospace Science and Technology 167: 110654. https://doi.org/10.1016/j.ast.2025.110654
• Meng, Yang, Ying Bi, Changchuan Xie, Zhiying Chen, and Chao Yang. 2022a. “Application of Fiber Optic Sensing System for Predicting Structural Displacement of a Joined-Wing Aircraft.” Aerospace 9 (11): 661. https://doi.org/10.3390/aerospace9110661
• Meng, Yu, Hongbin Gu, and Fang Chen. 2022c. “Influence of Plasma on the Combustion Mode in a Scramjet.” Aerospace 9 (2): 73. https://doi.org/10.3390/aerospace9020073
• Meng, Yu, Wenming Sun, Hongbin Gu, Fang Chen, and Ruixu Zhou. 2022d. “Supersonic Combustion Mode Analysis of a Cavity Based Scramjet.” Aerospace 9 (12): 826. https://doi.org/10.3390/aerospace9120826
• Mertens, Josef, Karl D. Klevenhusen, and Heinz Jakob. 1987. “Accurate Transonic Wave Drag Prediction Using Simple Physical Models.” AIAA Journal 25 (6): 799–805. https://doi.org/10.2514/3.9703
• Methel, Jeanne, Fabien Méry, Olivier Vermeersch, Maxime Forte, and Adrien Rouviere. 2025. “Laminar–turbulent Transition Experiment on the Effect of Surface Imperfections on a Natural Laminar Flow Profile in Compressible Flow Conditions.” Experiments in Fluids 66 (9): 175. https://doi.org/10.1007/s00348-025-04102-0
• Metro, Andrew J., Robert D. Rockwell, Andrew D. Cutler, and Chloe E. Dedic. 2026. “Reaction Zone Visualization of an Ethylene-Air Flame in a Dual-Mode Scramjet Using CH C-X PLIF.” Combustion and Flame 292: 115170. https://doi.org/10.1016/j.combustflame.2026.115170
• Michalowski, Brent, and Nathaniel Varano. 2017. “UAV Flight Test Characterization Using Minimal Test Equipment.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991481
• Michaud, Francois, Hamid Dalir, and Simon Joncas. 2018. “Structural Design and Optimization of an Aircraft Morphing Wing: Composite Skin.” Journal of Aircraft 55 (1): 195–211. https://doi.org/10.2514/1.c034340
• Micka, Daniel J., and James F. Driscoll. 2009. “Combustion Characteristics of a Dual-Mode Scramjet Combustor with Cavity Flameholder.” Proceedings of the Combustion Institute 32 (2): 2397–2404. https://doi.org/10.1016/j.proci.2008.06.192
• Miele, Angelo. 1955. “Optimum Climbing Technique for a Rocket-Powered Aircraft.” Journal of Jet Propulsion 25 (8): 385–91. https://doi.org/10.2514/8.6736
• Miele, Angelo. 1957. “An Extension of the Theory of the Optimum Burning Program for the Level Flight of a Rocket-Powered Aircraft.” Journal of the Aeronautical Sciences 24 (12): 874–84. https://doi.org/10.2514/8.3993
• Mihaila-Andres, Mihai, Paul-Virgil Rosu, Ciprian-Marius Larco, and Radu-Calin Pahonie. 2017b. “Aeroelastic Tailoring of Thin-Walled, Closed-Section Wing Box with Bend-Twist Coupling.” In 2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2017.8038669
• Mikami, Takahito, and Kenji Uchiyama. 2015. “Design of Flight Control System for Quad Tilt-Wing UAV.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152364
• Miles, John W. 1949. “A Formulation of the Aeroelastic Problem for a Swept Wing.” Journal of the Aeronautical Sciences 16 (8): 477–90. https://doi.org/10.2514/8.11836
• Miles, John W. 1953. “On the Transonic Drag of a Cone Cylinder.” Journal of the Aeronautical Sciences 20 (9): 651–52. https://doi.org/10.2514/8.2780
• Miles, John W. 1954. “On the Transonic Drag of Accelerated Bodies.” Journal of the Aeronautical Sciences 21 (9): 644–45. https://doi.org/10.2514/8.3162
• Miller, Eugene H. 1986. “Performance of a Forward Swept Wing Fighter Utilizing Thrust Vectoring and Reversing.” Journal of Aircraft 23 (1): 68–75. https://doi.org/10.2514/3.45268
• Miller, David P., and James W. Clark. 1965. “Research on Vtol Aircraft Handling Qualities Criteria.” Journal of Aircraft 2 (3): 194–201. https://doi.org/10.2514/3.43639
• Mitani, Tohru. 1995. “Ignition Problems in Scramjet Testing.” Combustion and Flame 101 (3): 347–59. https://doi.org/10.1016/0010-2180(94)00218-h
• Mitchel, Barry J. 1971. “Ablative Material Tests under Transient Heating Simulating Ballistic Re-Entry.” Journal of Spacecraft and Rockets 8 (6): 636–42. https://doi.org/10.2514/3.59704
• Mizobata, Kazuhide, Taichi Mio, and Katsuya Miyamoto. 2024. “Drag Reduction on the Basis of the Area Rule of the Small-Scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Second Report).” Aerospace 11 (9): 777. https://doi.org/10.3390/aerospace11090777
• Mogavero, Alessandro, and Richard E. Brown. 2018. “Modular, Fast Model for Design and Optimization of Hypersonic Vehicle Propulsion Systems.” Journal of Spacecraft and Rockets 55 (5): 1261–81. https://doi.org/10.2514/1.a33676
• Mohan, Shuvendra, and Priyank Kumar. 2026. “Effect of Anhedral/dihedral Wing Angles on a Blended Wing Body at Low Speeds.” Journal of the Brazilian Society of Mechanical Sciences and Engineering 48 (3): 185. https://doi.org/10.1007/s40430-025-06154-z
• Molloy, Timothy L., and Jason J. Ford. 2014. “Short-Data Recursive HMM Parameter Estimation for Rapid Vision-Based Aircraft Heading Estimation.” In 2014 4th Australian Control Conference (AUCC). IEEE. https://doi.org/10.1109/aucc.2014.7358683
• Monti, Rodolfo, Diego Paterna, Raffaele Savino, and Antonio Esposito. 2001. “Low-Reynolds Number Supersonic Diffuser for a Plasma-Heated Wind Tunnel.” International Journal of Thermal Sciences 40 (9): 804–15. https://doi.org/10.1016/s1290-0729(01)01267-4
• Moon, S. 2003. “Suppression of Nonlinear Composite Panel Flutter with Active/passive Hybrid Piezoelectric Networks Using Finite Element Method.” Structural Safety. https://doi.org/10.1016/s0167-4730(02)00049-8
• Moore, Kevin R., and Andrew Ning. 2019. “Takeoff and Performance Trade-Offs of Retrofit Distributed Electric Propulsion for Urban Transport.” Journal of Aircraft 56 (5): 1880–92. https://doi.org/10.2514/1.c035321
• Morelli, Eugene A. 1995a. “Estimating Noise Characteristics from Flight Test Data Using Optimal Fourier Smoothing.” Journal of Aircraft 32 (4): 689–95. https://doi.org/10.2514/3.46778
• Morelli, Eugene A. 2003. “Multiple Input Design for Real-Time Parameter Estimation in the Frequency Domain.” IFAC Proceedings Volumes 36 (16): 639–44. https://doi.org/10.1016/s1474-6670(17)34833-4
• Morelli, Eugene A. 2009. “Flight-Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles.” Journal of Guidance, Control, and Dynamics 32 (3): 949–59. https://doi.org/10.2514/1.37092
• Morelli, Eugene A. 2012. “Flight Test Maneuvers for Efficient Aerodynamic Modeling.” Journal of Aircraft 49 (6): 1857–67. https://doi.org/10.2514/1.c031699
• Morelli, Eugene A. 2021b. “Optimal Input Design for Aircraft Stability and Control Flight Testing.” Journal of Optimization Theory and Applications 191 (2–3): 415–39. https://doi.org/10.1007/s10957-021-01912-0
• Morelli, Eugene A., and Jared A. Grauer. 2023. “Advances in Aircraft System Identification at NASA Langley Research Center.” Journal of Aircraft 60 (5). https://ntrs.nasa.gov/citations/20230001945
• Morris, Robert D. 1964. “Parameter Selection for in-Flight Recording.” Journal of Aircraft 1 (5): 300–303. https://doi.org/10.2514/3.43597
• Mukhopadhyay, Vivek. 1995. “Flutter Suppression Control Law Design and Testing for the Active Flexible Wing.” Journal of Aircraft 32 (1): 45–51. https://doi.org/10.2514/3.46682
• Mulder, J. A. 1988. “Aircraft Flight Control System Identification.” IFAC Proceedings Volumes 21 (9): 1327–32. https://doi.org/10.1016/s1474-6670(17)54913-7
• Muller, George L., and William F. Gasko. 1967. “Subsonic-Transonic-Drag of Supersonic Inlets.” Journal of Aircraft 4 (3): 231–36. https://doi.org/10.2514/3.43825
• Muñoz, Álvaro, and Pablo García-Fogeda. 2022. “Active Flutter Suppression of a Wing Section in a Compressible Flow.” Aerospace 9 (12): 804. https://doi.org/10.3390/aerospace9120804
• Muñoz, Álvaro, and Pablo García-Fogeda. 2024. “Active Flutter Suppression of a Wing Section in the Subsonic, Sonic and Supersonic Regimes by the H∞ Control Method.” Aerospace 11 (3): 198. https://doi.org/10.3390/aerospace11030198
• Musa, Omer, Guoping Huang, and Zonghan Yu. 2022. “Assessment of New Pressure-Corrected Design Method for Hypersonic Internal Waverider Intake.” Acta Astronautica 201: 230–46. https://doi.org/10.1016/j.actaastro.2022.09.001
• Napolitano, Marcello R., Yongkyu Song, and Brad Seanor. 2001b. “On-Line Parameter Estimation for Restructurable Flight Control Systems.” Aircraft Design 4 (1): 19–50. https://doi.org/10.1016/s1369-8869(00)00023-9
• Nash, James S. 1982. “Advanced-Range Instrumentation Aircraft Improvement and Modernization Program.” Journal of Aircraft 19 (6): 510–12. https://doi.org/10.2514/3.57422
• Navaratna, Punsara D. B., Mark H. Lowenberg, and Simon A. Neild. 2019. “Minimally Constrained Flight Simulation in Wind Tunnel.” Journal of Aircraft 56 (4): 1353–66. https://doi.org/10.2514/1.c035199
• Navardi, Mohammad Mahdi, Hossein Shahverdi, Vahid Kalafi, and Vahid Pasha Zanussi. 2026. “Nonlinear Aeroelastic Tailoring Analysis of Composite Doubly-Curved Shallow Panels with Curvilinear Fibers.” Aerospace Science and Technology 178: 112391. https://doi.org/10.1016/j.ast.2026.112391
• Nelson, H. F. 1983. “Nonequilibrium Radiative Heating during Outer Planet Atmospheric Entry.” Journal of Spacecraft and Rockets 20 (4): 407–9. https://doi.org/10.2514/3.25618
• Neto, Nei Salis Brasil, Elder Moreira Hemerly, and Luiz Carlos Sandoval Góes. 2009. “Aircraft Parameter Estimation Experiment Design Considering Measurement Colored Residuals.” Journal of Aircraft 46 (6): 1857–65. https://doi.org/10.2514/1.34133
• Newberry, Conrad F. 1998. “The Conceptual Design of Deck-Launched Waverider-Configured Aircraft.” Aircraft Design 1 (3): 159–91. https://doi.org/10.1016/s1369-8869(98)00015-9
• Newsom, Jerry R. 1979. “Control Law Synthesis for Active Flutter Suppression Using Optimal Control Theory.” Journal of Guidance and Control 2 (5): 388–94. https://doi.org/10.2514/3.55894
• Newsom, Jerry R., Anthony S. Pototzky, and Irving Abel. 1985. “Design of a Flutter Suppression System for an Experimental Drone Aircraft.” Journal of Aircraft 22 (5): 380–86. https://doi.org/10.2514/3.45135
• Ng, T. S., and Z. H. Qureshi. 1981. “Optimal Input Design for Parameter Estimation for an Autoregressive Model with Output Power Constraints.” IFAC Proceedings Volumes 14 (2): 643–48. https://doi.org/10.1016/s1474-6670(17)63557-2
• Nghiem, Cuong P., and Helge Norstrud. 1989. “Design of Axisymmetric Bodies with Minimum Transonic Drag.” AIAA Journal 27 (12): 1818–20. https://doi.org/10.2514/3.10339
• Nicola, Genito, Gianluigi Di Capua, Luca Garbarino, and Gianfranco Morani. 2025. “Automatic Flight Tests Execution on a Distributed Electrical Propulsion Demonstrator.” In 2025 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero63441.2025.11068526
• Nicotra, E., S. Bane, and J. Jewell. 2026. “Effect of Freestream Noise and Boundary-Layer Transition on Hypersonic Shock-Wave/boundary-Layer Interaction Unsteadiness.” Shock Waves 36 (3): 26. https://doi.org/10.1007/s00193-026-01286-0
• Nielsen, Jack N. 1985b. “Arrays of Bodies of Revolution for Minimum Wave Drag.” Journal of Aircraft 22 (10): 901–9. https://doi.org/10.2514/3.45222
• Niewald, P. W., and S. L. Parker. 2000. “Flight-Test Techniques Employed to Successfully Verify F/A-18E in-Flight Lift and Drag.” Journal of Aircraft 37 (2): 194–200. https://doi.org/10.2514/2.2598
• Nissim, E. 1976. “Active Flutter Suppression Using Trailing-Edge and Tab Control Surfaces.” AIAA Journal 14 (6): 757–62. https://doi.org/10.2514/3.61416
• Nissim, E. 1978. “Comparative Study between Two Different Active Flutter Suppression Systems.” Journal of Aircraft 15 (12): 843–48. https://doi.org/10.2514/3.58458
• Nissim, E. 1991. “Reduction of Aerodynamic Augmented States in Active Flutter Suppression Systems.” Journal of Aircraft 28 (1): 82–93. https://doi.org/10.2514/3.45995
• Nissim, E., and I. Lottati. 1979b. “Active External Store Flutter Suppression in the YF-17 Flutter Model.” Journal of Guidance and Control 2 (5): 395–401. https://doi.org/10.2514/3.55895
• Nitsche, Wolfgang, and Joachim Szodruch. 1993. “Laminar-Flow Instrumentation for Wind-Tunnel and Flight Experiments.” Journal of Aircraft 30 (2): 192–200. https://doi.org/10.2514/3.48265
• Nitzsche, F. 1994. “Whirl-Flutter Suppression in Advanced Turboprops and Propfans by Active Control Techniques.” Journal of Aircraft 31 (3): 713–19. https://doi.org/10.2514/3.46552
• Niu, Ruijie, Changchuan Xie, Chao An, Yang Meng, and Chao Yang. 2026. “Review on Aerodynamic Modeling and Analysis of Tiltrotors in Various Flight Modes.” Chinese Journal of Aeronautics: 104280. https://doi.org/10.1016/j.cja.2026.104280
• Niu, Cong, Xiutian Yan, and Boyi Chen. 2023. “Control-Oriented Modeling of a High-Aspect-Ratio Flying Wing with Coupled Flight Dynamics.” Chinese Journal of Aeronautics 36 (4): 409–22. https://doi.org/10.1016/j.cja.2022.08.018
• Noll, T. E., F. E. Eastep, and R. A. Calico. 1984. “Active Suppression of Aeroelastic Instabilities on a Forward-Swept Wing.” Journal of Aircraft 21 (3): 202–8. https://doi.org/10.2514/3.48246
• Noll, T. E., and L. J. Huttsell. 1979. “Wing Store Active Flutter Suppression-Correlation of Analyses and Wind-Tunnel Data.” Journal of Aircraft 16 (7): 491–97. https://doi.org/10.2514/3.58553
• Nomura, Shigeaki. 1983. “Correlation of Hypersonic Stagnation Point Heat Transfer at Low Reynolds Numbers.” AIAA Journal 21 (11): 1598–1600. https://doi.org/10.2514/3.8296
• Norén-Cosgriff, Karin, Ivan Belyaev, and Finn Løvholt. 2022. “Building Vibration Induced by Sonic Boom: Field Test in Russia.” Applied Acoustics 185: 108422. https://doi.org/10.1016/j.apacoust.2021.108422
• Nyquist, H. 1928. “Certain Topics in Telegraph Transmission Theory.” Transactions of the American Institute of Electrical Engineers 47 (2): 617–44. https://doi.org/10.1109/t-aiee.1928.5055024
• Obradovic, B., and K. Subbarao. 2011a. “Modeling of Dynamic Loading of Morphing-Wing Aircraft.” Journal of Aircraft 48 (2): 424–35. https://doi.org/10.2514/1.c000313
• Obradovic, B., and K. Subbarao. 2011b. “Modeling of Flight Dynamics of Morphing Wing Aircraft.” Journal of Aircraft 48 (2): 391–402. https://doi.org/10.2514/1.c000269
• Ochi, Yoshimasa. 2004. “Design of a Flight Controller for Hypersonic Flight Experiment Vehicle.” Asian Journal of Control 6 (3): 353–61. https://doi.org/10.1111/j.1934-6093.2004.tb00211.x
• Ohman, L. H. 1983. “Effect of Edge-Tone Noise on Supercritical Airfoil Data.” AIAA Journal 21 (11): 1597–98. https://doi.org/10.2514/3.8295
• Ohtake, Kunihiko. 1998. “Thermal Analysis of the Thermal Protection System for the Re-Entry Vehicle.” Computer Methods in Applied Mechanics and Engineering 151 (3–4): 301–10. https://doi.org/10.1016/s0045-7825(97)00153-9
• Oladyshkin, Sergey, and Wolfgang Nowak. 2019. “The Connection between Bayesian Inference and Information Theory for Model Selection, Information Gain and Experimental Design.” Entropy 21 (11): 1081. https://doi.org/10.3390/e21111081
• Olivier, H. 1995. “Influence of the Velocity Gradient on the Stagnation Point Heating in Hypersonic Flow.” Shock Waves 5 (4): 205–16. https://doi.org/10.1007/bf01419002
• Opromolla, Roberto. 2020. “Magnetometer Calibration for Small Unmanned Aerial Vehicles Using Cooperative Flight Data.” Sensors 20 (2): 538. https://doi.org/10.3390/s20020538
• Ordaz, Irian, Karl A. Geiselhart, and James W. Fenbert. 2015a. “Conceptual Design of Low-Boom Aircraft with Flight Trim Requirement.” Journal of Aircraft 52 (3): 932–39. https://doi.org/10.2514/1.c033160
• Ordaz, Irian, and Wu Li. 2016. “Approximation of off-Body Sonic-Boom Analysis for Low-Boom Conceptual Design.” Journal of Aircraft 53 (1): 14–19. https://doi.org/10.2514/1.c033159
• Ossmann, Daniel, Tamas Luspay, and Balint Vanek. 2019. “Baseline Flight Control System Design for an Unmanned Flutter Demonstrator.” In 2019 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2019.8741853
• Othman, Muhammad F., Gustavo H. C. Silva, Pedro H. Cabral, Alex P. Prado, Alberto Pirrera, and Jonathan E. Cooper. 2019. “A Robust and Reliability-Based Aeroelastic Tailoring Framework for Composite Aircraft Wings.” Composite Structures 208: 101–13. https://doi.org/10.1016/j.compstruct.2018.09.086
• Ouyang, Qi, Xiaoqian Chen, and Jonathan E. Cooper. 2013. “Robust Aeroelastic Analysis and Optimization of Composite Wing under μ-Analysis Framework.” Journal of Aircraft 50 (4): 1299–1305. https://doi.org/10.2514/1.c031915
• Ouyang, Yan, Yingsong Gu, Xiping Kou, and Zhichun Yang. 2021a. “Active Flutter Suppression of Wing with Morphing Flap.” Aerospace Science and Technology 110: 106457. https://doi.org/10.1016/j.ast.2020.106457
• Owens, D. Bruce, and John N. Perkins. 1996. “Stability and Control of a Three-Surface, Forward-Swept Wing Configuration.” Journal of Aircraft 33 (6): 1206–8. https://doi.org/10.2514/3.47079
• Oyibo, Gabriel A. 1984. “Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft.” AIAA Journal 22 (1): 117–23. https://doi.org/10.2514/3.48423
• Oz, Furkan, and Kursat Kara. 2024. “Controlling Hypersonic Boundary Layer Transition with Localized Cooling and Metasurface Treatments.” Scientific Reports 14 (1): 15928. https://doi.org/10.1038/s41598-024-66867-4
• Ozbay, H. 1993. “Active Control of a Thin Airfoil: Flutter Suppression and Gust Alleviation.” IFAC Proceedings Volumes 26 (2): 829–32. https://doi.org/10.1016/s1474-6670(17)48848-3
• Page, J. A., and A. Loubeau. 2019. “Overall Vehicle System Noise: Sonic Boom.” CEAS Aeronautical Journal 10 (1). https://ntrs.nasa.gov/citations/20190028367
• Papadimitriou, Costas, and Costas Argyris. 2017. “Bayesian Optimal Experimental Design for Parameter Estimation and Response Predictions in Complex Dynamical Systems.” Procedia Engineering 199: 972–77. https://doi.org/10.1016/j.proeng.2017.09.205
• Paris, Alfonso C., and Omeed Alaverdi. 2005. “Nonlinear Aerodynamic Model Extraction from Flight-Test Data for the S-3B Viking.” Journal of Aircraft 42 (1): 26–32. https://doi.org/10.2514/1.3172
• Park, Gary D. 1977. “Parameter Identification Technology Used in Determining in-Flight Airload Parameters.” Journal of Aircraft 14 (3): 251–56. https://doi.org/10.2514/3.58770
• Park, Chul. 2007. “Calculation of Stagnation-Point Heating Rates Associated with Stardust Vehicle.” Journal of Spacecraft and Rockets 44 (1): 24–32. https://doi.org/10.2514/1.15745
• Park, Michael A., and Melissa B. Carter. 2022. “Low-Boom Demonstrator near-Field Summary for the Third AIAA Sonic Boom Prediction Workshop.” Journal of Aircraft 59 (3): 563–77. https://doi.org/10.2514/1.c036323
• Parsa, Javad, Cristian R. Rojas, and Håkan Hjalmarsson. 2025. “Results on Sparsity and Estimation Accuracy in Orthogonal Matching Pursuit with Application to Optimal Input Design.” Automatica 179: 112461. https://doi.org/10.1016/j.automatica.2025.112461
• “Patent for Rocket Airplane Issued to Goddard.” 1931. Bulletin of the American Interplanetary Society 1 (10): 2–3. https://doi.org/10.2514/8.9994
• Peigin, Sergey, and Boris Epstein. 2007. “Multipoint Aerodynamic Design of Wing-Body Configurations for Minimum Drag.” Journal of Aircraft 44 (3): 971–80. https://doi.org/10.2514/1.26746
• Peigin, Sergey, and Boris Epstein. 2015. “Automatic Design of Wing–Body–Nacelle Configurations for Minimum Drag.” AIAA Journal 53 (7): 1994–2004. https://doi.org/10.2514/1.j053594
• Pendleton, Edmund W., Denis Bessette, Peter B. Field, Gerald D. Miller, and Kenneth E. Griffin. 2000. “Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development.” Journal of Aircraft 37 (4): 554–61. https://doi.org/10.2514/2.2654
• Peng, Yue, Hao Yang, and Bin Jiang. 2021. “Probabilistic Fault Recoverability Analysis of Flight Control Process.” Chinese Journal of Aeronautics 34 (2): 529–38. https://doi.org/10.1016/j.cja.2020.05.029
• Penland, Jim A., James L. Dillon, and Jimmy L. Pittman. 1978. “An Aerodynamic Analysis of Several Hypersonic Research Airplane Concepts from M= 0.2 to 6.0.” Journal of Aircraft 15 (11): 716–23. https://doi.org/10.2514/3.58437
• Penland, J. A., and D. J. Romeo. 1971a. “Advances in Hypersonic Exploration Capability- Wind Tunnel to Flight Reynolds Number.” Journal of Aircraft 8 (11): 881–84. https://doi.org/10.2514/3.59185
• Pepping, R. A. 1954. “A Theoretical Investigation of the Oscillating Control Surface Frequency Response Technique of Flight Flutter Testing.” Journal of the Aeronautical Sciences 21 (8): 533–42. https://doi.org/10.2514/8.3118
• Perry, Aaron T., Timothy Bretl, and Phillip J. Ansell. 2021. “Aeropropulsive Coupling Effects on a General-Aviation Aircraft with Distributed Electric Propulsion.” Journal of Aircraft 58 (6): 1351–63. https://doi.org/10.2514/1.c036048
• Perry, Aaron T., Timothy Bretl, and Phillip J. Ansell. 2023. “System Identification of a Subscale Distributed Electric Propulsion Aircraft.” Journal of Aircraft 60 (3): 702–15. https://doi.org/10.2514/1.c036616
• Phillips, Ben D., and Thomas K. West. 2019. “Trim Flight Conditions for a Low-Boom Aircraft Design under Uncertainty.” Journal of Aircraft 56 (1): 53–67. https://doi.org/10.2514/1.c034932
• Piecewicz, Charles T., and Gustav A. Kindsvogel. 1943. “Semi-Rocket Airfoil: A Suggested Design for High-Speed Flight.” Astronautics 13 (54): 12–13. https://doi.org/10.2514/8.10356
• Ping Li, Wanchun Chen, and Hao Zhou. 2010. “Quasi-Equilibrium Glide Trajectory Design of Waverider-Based Hypersonic Vehicle.” In 2010 International Conference on Mechanical and Electrical Technology. IEEE. https://doi.org/10.1109/icmet.2010.5598391
• Pinkelman, J. K., S. M. Batill, and M. W. Kehoe. 1996. “Total Least-Squares Criteria in Parameter Identification for Flight Flutter Testing.” Journal of Aircraft 33 (4): 784–92. https://doi.org/10.2514/3.47015
• Polezhaev, Yu. V. 2000. “Will There or Will There Not Be a Hypersonic Airplane?” Journal of Engineering Physics and Thermophysics 73 (1): 3–8. https://doi.org/10.1007/bf02681670
• Poovathingal, Savio J., and Hailong Chen. 2022. “Microscale Modeling of Particle Impact on Thermal Protection System Materials during High-Speed Entry.” AIAA Journal 60 (8): 4976–90. https://doi.org/10.2514/1.j061313
• Popov, Andrei V., Lucian T. Grigorie, Ruxandra Botez, Mahmood Mamou, and Youssef Mebarki. 2010b. “Real Time Morphing Wing Optimization Validation Using Wind-Tunnel Tests.” Journal of Aircraft 47 (4): 1346–55. https://doi.org/10.2514/1.47431
• Popov, Andrei Vladimir, Teodor Lucian Grigorie, Ruxandra Mihaela Botez, Youssef Mébarki, and Mahmood Mamou. 2010a. “Modeling and Testing of a Morphing Wing in Open-Loop Architecture.” Journal of Aircraft 47 (3): 917–23. https://doi.org/10.2514/1.46480
• Popov, Andrei Vladimir, Michel Labib, Julien Fays, and Ruxandra Mihaela Botez. 2008. “Closed-Loop Control Simulations on a Morphing Wing.” Journal of Aircraft 45 (5): 1794–1803. https://doi.org/10.2514/1.37073
• Prasad, S. N., S. Nemat-Nasser, and G. Herrmann. 1967. “Bending-Torsional Flutter of a Swept Wing in a High-Density, Low-Speed Flow.” AIAA Journal 5 (2): 316–21. https://doi.org/10.2514/3.3959
• Price, S. J., and B. H. K. Lee. 1993. “Evaluation and Extension of the Flutter-Margin Method for Flight Flutter Prediction.” Journal of Aircraft 30 (3): 395–402. https://doi.org/10.2514/3.56887
• Qi, Jie, and Ruth E. Baker. 2026. “Optimal Experimental Design for Parameter Estimation in the Presence of Observation Noise.” Mathematical Biosciences 392: 109571. https://doi.org/10.1016/j.mbs.2025.109571
• Qian, J., M. Nadri, and P. Dufour. 2016. “Optimal Input Design for Parameter Estimation of Nonlinear Systems: Case Study of an Unstable Delta Wing.” International Journal of Control 90 (4): 873–87. https://doi.org/10.1080/00207179.2016.1225990
• Qian, Jun, Madiha Nadri, Petru-Daniel Morosan, and Pascal Dufour. 2014. “Closed Loop Optimal Experiment Design for on-Line Parameter Estimation.” In 2014 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2014.6862468
• Qinkun Xiao, Xiaoguang Gao, Xiaowei Fu, and Haiyun Wang. 2006. “New Local Path Replanning Algorithm for Unmanned Combat Air Vehicle.” In 2006 6th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2006.1713131
• Quaranta, V., and I. Dimino. 2007. “Experimental Training and Validation of a System for Aircraft Acoustic Signature Identification.” Journal of Aircraft 44 (4): 1196–1204. https://doi.org/10.2514/1.24824
• Queen, S., and J. Cochrane. 1982. “Quiet Short-Haul Research Aircraft Joint Navy/NASA Sea Trials.” Journal of Aircraft 19 (8). https://ntrs.nasa.gov/citations/19980201423
• RafajŁOwicz, Ewaryst. 1982. “Optimal Input Signals for Parameter Estimation in Linear Distributed Parameter Systems.” International Journal of Systems Science 13 (7): 799–808. https://doi.org/10.1080/00207728208926390
• Raheem, Mohammed Abdul, Prasetyo Edi, Amjad A. Pasha, Mustafa M. Rahman, and Khalid A. Juhany. 2019. “Numerical Study of Variable Camber Continuous Trailing Edge Flap at off-Design Conditions.” Energies 12 (16): 3185. https://doi.org/10.3390/en12163185
• Rahman, Naveed U., and James F. Whidborne. 2010. “Propulsion and Flight Controls Integration for a Blended-Wing-Body Transport Aircraft.” Journal of Aircraft 47 (3): 895–903. https://doi.org/10.2514/1.46195
• Raisinghani, S. C., and A. K. Adak. 1983. “Aircraft Parameter Identification by Gauss-Newton Minimization Technique Using Flight Test Data.” International Journal of Systems Science 14 (12): 1395–1409. https://doi.org/10.1080/00207728308926538
• Rajpal, D., F. M. A. Mitrotta, C. A. Socci, J. Sodja, C. Kassapoglou, and R. De Breuker. 2021. “Design and Testing of Aeroelastically Tailored Composite Wing under Fatigue and Gust Loading Including Effect of Fatigue on Aeroelastic Performance.” Composite Structures 275: 114373. https://doi.org/10.1016/j.compstruct.2021.114373
• Ramaswamy, M. A. 1987. “Characteristics of a Typical Lifting Symmetric Supercritical Airfoil.” Sadhana 10 (3–4): 445–58. https://doi.org/10.1007/bf02811306
• Ramaswamy, M. A., and S. Viswanathan. 1975. “Some Observations on the Adams Body of Minimum Wave Drag.” Journal of Aircraft 12 (12): 1001–2. https://doi.org/10.2514/3.44506
• Reed, Darren K., Melody N. Mayle, and Donald K. Nance. 2012. “Comparison of Ares I-X Flight and Wind-Tunnel Aeroacoustic Data.” Journal of Spacecraft and Rockets 49 (4): 659–65. https://doi.org/10.2514/1.a32181
• Reich, Gregory W., Daniella E. Raveh, and P. Scott Zink. 2004. “Application of Active-Aeroelastic-Wing Technology to a Joined-Wing Sensorcraft.” Journal of Aircraft 41 (3): 594–602. https://doi.org/10.2514/1.78
• Reichert, Carl E. 1947. “Supersonic and Transonic Aircraft Problems.” Journal of the American Rocket Society 00 (69): 24–33. https://doi.org/10.2514/8.4133
• Renselaer, Dirk J. 1977. “Use of a Water Basin for Ground Effect Testing of VTOL Models.” Journal of Aircraft 14 (6): 513–14. https://doi.org/10.2514/3.58812
• “Report No. 581. Measurements of Intensity and Scale of Wind-Tunnel Turbulence and Their Relation to the Critical Reynolds Number of Spheres.” 1937. Journal of the Franklin Institute 223 (5): 674. https://doi.org/10.1016/s0016-0032(37)91942-2
• Riccio, Aniello, Francesco Raimondo, Andrea Sellitto, Valerio Carandente, Roberto Scigliano, and Domenico Tescione. 2017. “Optimum Design of Ablative Thermal Protection Systems for Atmospheric Entry Vehicles.” Applied Thermal Engineering 119: 541–52. https://doi.org/10.1016/j.applthermaleng.2017.03.053
• Richard, Robert E., John A. Rule, and Robert L. Clark. 2001. “Genetic Spatial Optimization of Active Elements on an Aeroelastic Delta Wing.” Journal of Vibration and Acoustics 123 (4): 466–71. https://doi.org/10.1115/1.1389458
• Richards, W. Lance, and Richard C. Monaghan. 1997. “Development of a Flight Article for a Hypersonic Boundary-Layer Experiment.” Journal of Spacecraft and Rockets 34 (5): 609–13. https://doi.org/10.2514/2.3277
• Rieken, Elizabeth F., Scott A. Berry, Michelle L. Mason, and Francis A. Greene. 2020. “NASA Langley Aerothermodynamic Ground Tests in Support of the Boundary Layer Transition (BOLT) Flight Experiment.” Journal of Spacecraft and Rockets 58 (1). https://ntrs.nasa.gov/citations/20200003493
• Riggins, David, H. F. Nelson, and Eric Johnson. 1999. “Blunt-Body Wave Drag Reduction Using Focused Energy Deposition.” AIAA Journal 37 (4): 460–67. https://doi.org/10.2514/2.756
• Rimer, M., R. Chipman, and R. Mercadante. 1984b. “Divergence/flutter Suppression System for a Forward Swept-Wing Configuration with Wing-Mounted Stores.” Journal of Aircraft 21 (8): 631–38. https://doi.org/10.2514/3.45034
• Rimer, M., R. Chipman, and B. Muniz. 1986. “Control of a Forward-Swept-Wing Configuration Dominated by Flight Dynamic/aeroelastic Interactions.” Journal of Guidance, Control, and Dynamics 9 (1): 72–79. https://doi.org/10.2514/3.20069
• Ritter, Markus, Jens Neumann, and Wolf Reiner Krüger. 2016. “Aeroelastic Simulations of High Reynolds Number Aero Structural Dynamics Wind Tunnel Model.” AIAA Journal 54 (6): 1962–73. https://doi.org/10.2514/1.j053384
• Rivers, S. Melissa B., Lewis R. Owens, and Richard A. Wahls. 2008. “Investigations for Supersonic Transports at Transonic and Supersonic Conditions.” Journal of Aircraft 45 (1): 211–22. https://doi.org/10.2514/1.30972
• Rizk, Magdi H., and Earll M. Murman. 1984. “Wind Tunnel Wall Interference Corrections for Aircraft Models in Thetransonic Regime.” Journal of Aircraft 21 (1): 54–61. https://doi.org/10.2514/3.48222
• Roberts, D. W. 2001. “SUU-25F/A Dispenser Pod Flight Test Program on the F/A-18A Aircraft.” In 2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542). IEEE. https://doi.org/10.1109/aero.2001.931222
• Rodden, William P. 1989a. “Comment on ‘Divergence Study of a High-Aspect Ratio, Forward Swept Wing’.” Journal of Aircraft 26 (8): 791–791. https://doi.org/10.2514/3.45842
• Rodden, William P. 1989b. “Comment on ‘General Formulation of the Aeroelastic Divergence of Composite Swept-Forward Wing Structures’.” Journal of Aircraft 26 (7): 694–95. https://doi.org/10.2514/3.45825
• Rodríguez-Segade, Miguel, Santiago Hernández, and Jacobo Díaz. 2023. “Integration of Technologies for the Design and Optimization of a Stratospheric Hypersonic Vehicle.” In 2023 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero55745.2023.10115817
• Rodríguez-Segade, Miguel, Santiago Hernández, and Jacobo Díaz. 2024. “Multi-Level and Multi-Objective Structural Optimization for Hypersonic Vehicle Design.” Aerospace Science and Technology 152: 109346. https://doi.org/10.1016/j.ast.2024.109346
• Roger, Kenneth L., Garold E. Hodges, and Larry Felt. 1975. “Active Flutter Suppression-A Flight Test Demonstration.” Journal of Aircraft 12 (6): 551–56. https://doi.org/10.2514/3.59833
• Rogers, David F. 2002b. “An Engineering Flight-Test Course Emphasizing Flight Mechanics Concepts.” Journal of Aircraft 39 (1): 79–83. https://doi.org/10.2514/2.2898
• Rosenbaum, Robert, and Robert H. Scanlan. 1948. “A Note on Flight Flutter Testing.” Journal of the Aeronautical Sciences 15 (6): 366–70. https://doi.org/10.2514/8.11590
• Rostkowski, Przemyslaw, Jeremie B. E. Meurisse, and Marco Panesi. 2026. “Non-Deterministic Extension of Plasma Wind Tunnel Data Calibrated Model Predictions to Flight Conditions.” Aerospace Science and Technology 168: 111059. https://doi.org/10.1016/j.ast.2025.111059
• Roudbari, Alireza, and Fariborz Saghafi. 2014. “Intelligent Modeling and Identification of Aircraft Nonlinear Flight.” Chinese Journal of Aeronautics 27 (4): 759–71. https://doi.org/10.1016/j.cja.2014.03.017
• Russo, Lorenzo, Renato Tognaccini, and Luciano Demasi. 2020b. “Box Wing and Induced Drag: Compressibility Effects in Subsonic and Transonic Regimes.” AIAA Journal 58 (6): 2398–2413. https://doi.org/10.2514/1.j059080
• Ryan, Kevin M., Mark J. Lewis, and Kenneth H. Yu. 2015. “Comparison of Robust Optimization Methods Applied to Hypersonic Vehicle Design.” Journal of Aircraft 52 (5): 1510–23. https://doi.org/10.2514/1.c032986
• Sabatini, Roberto. 2014. “Innovative Flight Test Instrumentation and Techniques for Airborne Laser Systems Performance Analysis and Mission Effectiveness Evaluation.” In 2014 IEEE Metrology for Aerospace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2014.6865886
• Sabin, Marc L. 1975. “Linear Filtering of Ballistic-Entry Probe Data for Atmospheric Reconstruction.” Journal of Spacecraft and Rockets 12 (5): 0320b-0320b. https://doi.org/10.2514/3.56980
• Sadow, Raymond M. 1964. “How PERT Was Used in Managing the X-20 (Dyna-Soar) Program.” IEEE Transactions on Engineering Management EM-11 (4): 138–54. https://doi.org/10.1109/tem.1964.6446422
• Sadoway, Eric, and Sina Ghaemi. 2026. “Evaluating Aerodynamic and Propulsive Performance of a Wing with Distributed Electric Propulsion.” Journal of Aircraft: 1–14. https://doi.org/10.2514/1.c038766
• Sadraoui, Youssef, Mohamed Er-Ratby, Moulay Saddik Kadiri, and Abdessamad Kobi. 2026. “Development and Validation of a Dynamic Bayesian Network-Based Adaptive Reliability Optimization Model Using Design of Experiments and Expected Information Gain.” Quality and Reliability Engineering International: qre.70404. https://doi.org/10.1002/qre.70404
• Saheby, Eiman B., Li Jialu, Chen Wang, and Shen Xing. 2026. “Vortex Behavior over a Tailless Forward-Swept Wing with Chine Forebody Configuration.” Aerospace Science and Technology 168: 111026. https://doi.org/10.1016/j.ast.2025.111026
• Şakraker, Işıl, Alessandro Turchi, and Olivier Chazot. 2015. “Hypersonic Aerothermochemistry Duplication in Ground Plasma Facilities: A Flight-to-Ground Approach.” Journal of Spacecraft and Rockets 52 (5): 1273–82. https://doi.org/10.2514/1.a33137
• Saltzman, Edwin J., and Theodore G. Ayers. 1982. “Review of Flight-to-Wind-Tunnel Drag Correlation Edwin.” Journal of Aircraft 19 (10): 801–11. https://doi.org/10.2514/3.61561
• Samardžić, Marija, Jovan Isaković, Zoran Anastasijević, and Dragan Marinkovski. 2013. “Apparatus for Measurement of Pitch and Yaw Damping Derivatives in High Reynolds Number Blowdown Wind Tunnel.” Measurement 46 (8): 2457–66. https://doi.org/10.1016/j.measurement.2013.04.074
• Samuel, Aamod, Olivia Carte, Joel Lozano, and Troy Robillos. 2018. “Creating Innovative Frameworks to Spur Cultural Change at the NASA Armstrong Flight Research Center.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396412
• Sanghi, Divya, Carlos E. S. Cesnik, and Cristina Riso. 2024. “Roll Maneuverability of Transonic High-Aspect-Ratio-Wing Aircraft with Flared Folding Wingtips.” Journal of Aircraft 61 (3): 915–38. https://doi.org/10.2514/1.c037470
• Sano, Masaaki, Yoshinori Fujimori, and Shoji Maekawa. 1984. “Design and Experimental Verification of the USB Flap Panel Structurefor NAL-STOL Research Aircraft.” Journal of Aircraft 21 (6): 353–54. https://doi.org/10.2514/3.44973
• Santosa, Fadil, and Loren Anderson. 2022. “Bayesian Sequential Optimal Experimental Design for Linear Regression with Reinforcement Learning.” In 2022 21st IEEE International Conference on Machine Learning and Applications (ICMLA). IEEE. https://doi.org/10.1109/icmla55696.2022.00106
• Sapkal, Kedar S., and Peter J. Attar. 2012. “Aeroelastic Analysis of a Composite Material Delta Wing in Low Subsonic Flow.” AIAA Journal 50 (1): 162–75. https://doi.org/10.2514/1.j051212
• Sardou, M. 1986. ““Reynolds Effect” and “Moving Ground Effect” Tested in a Quarter Scale Wind Tunnel over a High Speed Moving Belt.” Journal of Wind Engineering and Industrial Aerodynamics 22 (2–3): 245–70. https://doi.org/10.1016/0167-6105(86)90089-9
• Satria Palar, Pramudita, Eric Nguyen Van, Nathalie Bartoli, and Joseph Morlier. 2024. “Design Exploration of a Distributed Electric Propulsion Aircraft Using Explainable Surrogate Models.” Journal of Aircraft 61 (5): 1561–74. https://doi.org/10.2514/1.c037848
• Savino, Raffaele, Gennaro Russo, Vera D’Oriano, Michele Visone, Manuela Battipede, and Piero Gili. 2015. “Performances of a Small Hypersonic Airplane (HyPlane).” Acta Astronautica 115: 338–48. https://doi.org/10.1016/j.actaastro.2015.06.006
• Schaefer, Herbert. 1948. “Machmeters for High-Speed Flight Research.” Journal of the Aeronautical Sciences 15 (6): 351–63. https://doi.org/10.2514/8.11587
• Schenck, Hilbert V. 1949. “Hydraulic Analog of Flow through Supersonic Nozzles.” Journal of the American Rocket Society 00 (77): 75–78. https://doi.org/10.2514/8.4274
• Schewe, Günter, and Holger Mai. 2018. “Influence of Flexibility on the Steady Aeroelastic Behavior of a Swept Wing in Transonic Flow.” Journal of Fluids and Structures 81: 255–69. https://doi.org/10.1016/j.jfluidstructs.2018.04.021
• Schmidt, David K., Brian P. Danowsky, Aditya Kotikalpudi, et al. 2020. “Modeling, Design, and Flight Testing of Three Flutter Controllers for a Flying-Wing Drone.” Journal of Aircraft 57 (4): 615–34. https://doi.org/10.2514/1.c035720
• Schneider, Steven P. 1999. “Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds.” Journal of Spacecraft and Rockets 36 (1): 8–20. https://doi.org/10.2514/2.3428
• Schnerr, Guenter H., and Ulrich Dohrmann. 1994. “Drag and Lift in Nonadiabatic Transonic Flow.” AIAA Journal 32 (1): 101–7. https://doi.org/10.2514/3.11956
• Schyfter, Pablo. 2013. “Propellers and Promoters: Emerging Engineering Knowledge in Aeronautics and Synthetic Biology.” Engineering Studies 5 (1): 6–25. https://doi.org/10.1080/19378629.2012.762651
• Sekula, Martin, David J. Piatak, and Russ D. Rausch. 2012. “Comparison of Ares I-X Wind-Tunnel-Derived Buffet Environment with Flight Data.” Journal of Spacecraft and Rockets 49 (5): 822–33. https://doi.org/10.2514/1.59962
• Senkel, Luise, Andreas Rauh, and Harald Aschemann. 2013. “Optimal Input Design for Online State and Parameter Estimation Using Interval Sliding Mode Observers.” In 52nd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2013.6759931
• Shahrbabaki, Amin Nazarian, Mehrdad Bazazzadeh, Mojtaba Dehghan Manshadi, and Ali Shahriari. 2014. “Designing a Fuzzy Logic Controller for the Reynolds Number in a Blowdown Supersonic Wind Tunnel.” In 2014 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2014.6836242
• Shanbhag, V. V., and R. Narasimha. 1970. “Numerical Evaluation of the Transonic Wave Drag Integral.” International Journal for Numerical Methods in Engineering 2 (2): 277–82. https://doi.org/10.1002/nme.1620020213
• Shannon, C. E. 1948. “A Mathematical Theory of Communication.” Bell System Technical Journal 27 (3): 379–423. https://doi.org/10.1002/j.1538-7305.1948.tb01338.x
• Shao, Yan, Min Meng, Tenglong Gao, and Shuai Xie. 2026. “Decoupling and Sparse Modeling of Vertical Tail Loads in T-Tail Aircraft with Application to Flight Test Data.” Chinese Journal of Aeronautics: 104393. https://doi.org/10.1016/j.cja.2026.104393
• Sharifi, Mahshid, Angela Vincenti, and Jean-Camille Chassaing. 2025. “Impact of Material and Geometrical Parameters on the Aeroelastic Tailoring of Uni-Directional Composite Plate-Wings.” Composite Structures 355: 118839. https://doi.org/10.1016/j.compstruct.2025.118839
• Sharma, Balraj, Pooja Agrawal, and Ajay Misra. 2022a. “Partial Feedback Linearized RISE Controller for Active Flutter Suppression.” IFAC-PapersOnLine 55 (22): 159–64. https://doi.org/10.1016/j.ifacol.2023.03.027
• Sharma, Balraj, Pooja Agrawal, and Ajay Misra. 2022b. “RISE Based Output Feedback Controller for Active Flutter Suppression of 2D Aerofoil.” In 2022 Eighth Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/icc56513.2022.10093649
• Sharma, Balraj, Abhishek Dixit, Pooja Agrawal, and Ajay Misra. 2021. “UDE Based RISE Controller for Active Flutter Suppression of 2D Aerofoil.” In 2021 IEEE 18th India Council International Conference (INDICON). IEEE. https://doi.org/10.1109/indicon52576.2021.9691535
• Shaw, L., R. C. Hidalgo, G. J. Burgess, R. Enriquez, J. L. Minor, and J. W. Rogers. 2006. “Aeroelastic Load Control Program: In-Flight Demonstration of Active Flow Control Technology.” In 2006 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2006.1656021
• Shen, Wanggang, and Xun Huan. 2023. “Bayesian Sequential Optimal Experimental Design for Nonlinear Models Using Policy Gradient Reinforcement Learning.” Computer Methods in Applied Mechanics and Engineering 416: 116304. https://doi.org/10.1016/j.cma.2023.116304
• Shen, Lin, Da Huang, and Genxing Wu. 2021. “Time Delay Compensation in Lateral-Directional Flight Control Systems at High Angles of Attack.” Chinese Journal of Aeronautics 34 (4): 1–18. https://doi.org/10.1016/j.cja.2020.07.022
• Shen, Yang, Wei Huang, Li Yan, and Tian-tian Zhang. 2020. “Constraint-Based Parameterization Using FFD and Multi-Objective Design Optimization of a Hypersonic Vehicle.” Aerospace Science and Technology 100: 105788. https://doi.org/10.1016/j.ast.2020.105788
• Shen Guangchen, Bai Junqiang, and Liu Nan. 2017. “Mechanical and Aerodynamic Study of 2D Trailing Edge Variable Camber System for Civil Transport Aircraft.” In 2017 8th International Conference on Mechanical and Intelligent Manufacturing Technologies (ICMIMT). IEEE. https://doi.org/10.1109/icmimt.2017.7917466
• Sherrer, V. C., T. J. Hertz, and M. H. Shirk. 1981. “Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept Wings.” Journal of Aircraft 18 (11): 976–83. https://doi.org/10.2514/3.57589
• Shi, Zhong-ke. 2003. “Optimized Robust Filter for Uncertain Discrete Time System and Its Application to Flight Test.” Chinese Journal of Aeronautics 16 (2): 91–96. https://doi.org/10.1016/s1000-9361(11)60210-0
• Shi, Zhong-ke. 2004. “Interval Criterion of Robust Stability for Nonlinear System and Its Application to Flight Control.” Chinese Journal of Aeronautics 17 (2): 99–105. https://doi.org/10.1016/s1000-9361(11)60221-5
• Shi, Shijie, Jiabo Huo, Zhongbao Liu, and Aicheng Zou. 2024. “Rapid Design Method of Heavy-Loaded Propeller for Distributed Electric Propulsion Aircraft.” Energies 17 (4): 786. https://doi.org/10.3390/en17040786
• Shin, Jong-Yeob, Gary J. Balas, and Andrew K. Packard. 2001. “Worst-Case Analysis of the X-38 Crew Return Vehicle Flight Control System.” Journal of Guidance, Control, and Dynamics 24 (2): 261–69. https://doi.org/10.2514/2.4708
• Shipilin, A. V. 1964. “On Bodies of Minimum Wave Drag in Nonuniform Free Stream of Gas.” Journal of Applied Mathematics and Mechanics 28 (3): 669–74. https://doi.org/10.1016/0021-8928(64)90113-3
• Shuping Tan and Zhibin Li. 2010. “Switching Control Design for a Hypersonic Flight Vehicle.” In 2010 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2010.5498526
• Simeonides, George A. 2006. “Extrapolation-to-Flight of Aerodynamic Heating Measurements and Determination of in-Flight Radiation-Equilibrium Surface Temperature in Hypersonic/high Enthalpy Flow Conditions.” Shock Waves 16 (1): 25–34. https://doi.org/10.1007/s00193-006-0040-3
• Simmons, Benjamin M. 2023b. “System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data.” Journal of Aircraft 60 (4): 1078–93. https://doi.org/10.2514/1.c036896
• Simmons, Benjamin M., James L. Gresham, and Craig A. Woolsey. 2023. “Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft.” Journal of Aircraft 60 (5): 1503–21. https://doi.org/10.2514/1.c037260
• Singh, S., and A. K. Ghosh. 2007. “Improved Delta Method for Parameter Estimation from Real-Flight Data Using Neural Networks.” IFAC Proceedings Volumes 40 (7): 200–205. https://doi.org/10.3182/20070625-5-fr-2916.00035
• Singh, S., and A. K. Ghosh. 2013. “Modified Delta Method for Estimation of Parameters from Flight Data of Stable and Unstable Aircraft.” In 2013 3rd IEEE International Advance Computing Conference (IACC). IEEE. https://doi.org/10.1109/iadcc.2013.6514325
• Sitz, David M., David C. Nelson, and Mark R. Carpenter. 1997. “KEEP EAGLE F-15E High Angle-of-Attack Flight Test Program.” Journal of Aircraft 34 (3): 265–70. https://doi.org/10.2514/2.2174
• Skolnik, Nathaniel, and Zachary Putnam. 2022. “Effect of Designed-In Features on Thermal Response of Atmospheric Entry Thermal Protection System Materials.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.4147322
• Slavin, Vadim S., Valery M. Gavrilov, Nikolay I. Zelinsky, and Alexandr R. Bozhkov. 2001. “Magnetohydrodynamics Generator with Plasma Layers as Power Source aboard a Hypersonic Airplane.” Journal of Propulsion and Power 17 (1): 19–26. https://doi.org/10.2514/2.5739
• Smetana, Frederick O., and Donald P. Knepper. 1973. “Toward Simpler Prediction of Transonic Airfoil Lift, Drag, and Moment.” Journal of Aircraft 10 (2): 124–26. https://doi.org/10.2514/3.44355
• Smith, A. J. D., and D. R. J. Baxter. n.d. “Liquid Crystal Thermography for Aerodynamic Heating Measurements in Short Duration Hypersonic Facilities.” In International Congress on Instrumentation in Aerospace Simulation Facilitie. IEEE. https://doi.org/10.1109/iciasf.1989.77663
• Smith, Ronald C., and J. E. Farbridge. 1979. “The Transonic Multifoil Augmentor Wing.” Journal of Aircraft 15. https://ntrs.nasa.gov/citations/19990034126
• Smith, D. D., M. H. Lowenberg, D. P. Jones, and M. I. Friswell. 2014. “Computational and Experimental Validation of the Active Morphing Wing.” Journal of Aircraft 51 (3): 925–37. https://doi.org/10.2514/1.c032262
• Sneshko, Yu. I., V. N. Chetvergov, and T. A. Chernysheva. 2005. “Flight-Test Estimation of Aircraft Aerodynamic Characteristics-Russian Experience.” Journal of Aircraft 42 (1): 87–90. https://doi.org/10.2514/1.3334
• Snodgrass, R. B. 1955. “Flight Measurements of Aerodynamic Heating and Boundary Layer Transition on the Viking 10 Nose Cone.” Journal of Jet Propulsion 25 (12): 701–6. https://doi.org/10.2514/8.6860
• Sóbester, András. 2021. “Flight-Test Validation of a Takeoff Performance Uncertainty Model.” Journal of Aircraft 58 (6): 1216–28. https://doi.org/10.2514/1.c036180
• Sobron, Alejandro, David Lundström, and Petter Krus. 2021. “A Review of Current Research in Subscale Flight Testing and Analysis of Its Main Practical Challenges.” Aerospace 8 (3): 74. https://doi.org/10.3390/aerospace8030074
• Soltmann, Lars M., and Charles E. Hall. 2017. “Power-Required Flight Testing of Unmanned Aerial Systems Using Non-Steady-State Flight.” Journal of Aircraft 54 (3): 1162–71. https://doi.org/10.2514/1.c033982
• Son, Jiwon, Chankyu Son, and Kwanjung Yee. 2022. “A Novel Direct Optimization Framework for Hypersonic Waverider Inverse Design Methods.” Aerospace 9 (7): 348. https://doi.org/10.3390/aerospace9070348
• Song, Hyeon Su, Rho Shin Myong, and Hakjin Lee. 2026. “Multipropeller Interaction and Rotational Effects in Distributed Electric Propulsion Aircraft.” AIAA Journal: 1–20. https://doi.org/10.2514/1.j067305
• Song, Zhao Jun, Ming Cai Xu, Torgeir Moan, and Jin Pan. 2019. “Dimensional and Similitude Analysis of Stiffened Panels under Longitudinal Compression Considering Buckling Behaviours.” Ocean Engineering 187: 106188. https://doi.org/10.1016/j.oceaneng.2019.106188
• Sousa, Helder, Jochen Köhler, and Joan R. Casas. 2021. “Evidence on the Value of Information towards Decision-Makers.” Structure and Infrastructure Engineering 18 (4): 439–40. https://doi.org/10.1080/15732479.2021.1991961
• Soykasap, Omer, and Dewey H. Hodges. 2000. “Performance Enhancement of a Composite Tilt-Rotor Using Aeroelastic Tailoring.” Journal of Aircraft 37 (5): 850–58. https://doi.org/10.2514/2.2680
• Spaid, F. W., and L. S. Stivers. 1980. “Supercritical Airfoil Boundary Layer Measurements.” Journal of Aircraft 17 (8): 567–75. https://doi.org/10.2514/3.57941
• Sprunger, Justin, Andrew J. La Sorsa, Rachel Hytovick, Jonathan Sosa, and Kareem A. Ahmed. 2025. “Turbulent Flame Compressibility Criterion for Scramjet Unstart and Transition.” Combustion and Flame 274: 114044. https://doi.org/10.1016/j.combustflame.2025.114044
• Sreena, P. V., and R. Laxman. 2023. “Lifting Body Flight Controller Design Using Gain Scheduled Classical Control.” In 2023 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero55745.2023.10115772
• Stack, John. 1934. “Effects of Compressibility on High Speed Flight.” Journal of the Aeronautical Sciences 1 (1): 40–43. https://doi.org/10.2514/8.12
• Stanford, Bret K. 2021. “Shape, Sizing, and Topology Design of a Wingbox under Aeroelastic Constraints.” Journal of Aircraft 58 (6): 1406–15. https://doi.org/10.2514/1.c036315
• Stanly, A. L. 1950. “Some Statistical Considerations of the Jet Alignment of Rocket-Powered Vehicles.” Journal of the American Rocket Society 00 (83): 155–68. https://doi.org/10.2514/8.4342
• Starr, R. F., and M. O. Varner. 1976b. “Observations on the Drag of Conical Bodies at Transonic Speeds.” Journal of Spacecraft and Rockets 13 (11): 643–49. https://doi.org/10.2514/3.57127
• Steger, Joseph L., and Barrett S. Baldwin. 1973. “Shock Waves and Drag in the Numerical Calculation of Compressible, Irrotational Transonic Flow.” AIAA Journal 11 (7): 903–4. https://doi.org/10.2514/3.50538
• Stekler, H. O. 1982. “An Evaluation of an Airframe Cost-Estimating Relationship.” Technological Forecasting and Social Change 21 (2): 95–102. https://doi.org/10.1016/0040-1625(82)90009-9
• Stewart, D. J., and B. S. Campion. 1980. “New Technology in Commercial Aircraft Design for Minimum Operating Cost.” Journal of Aircraft 17 (5): 365–71. https://doi.org/10.2514/3.57914
• Sticchi, Emanuele, Daniele Ragni, Damiano Casalino, and Francesco Avallone. 2026. “Aeroacoustic Installation Effects on a Propeller-Driven Strut-Braced Wing Aircraft.” Journal of Aircraft 63 (5): 2341–62. https://doi.org/10.2514/1.c038530
• Stilla, J. 1994. “Engineering Transition Prediction for a Hypersonic Axisymmetric Boundary Layer.” Journal of Aircraft 31 (6): 1358–64. https://doi.org/10.2514/3.46659
• Stock, Hans W. 2002. “Wind Tunnel–flight Correlation for Laminar Wings in Adiabatic and Heating Flow Conditions.” Aerospace Science and Technology 6 (4): 245–57. https://doi.org/10.1016/s1270-9638(02)01166-5
• Stodieck, Olivia, Jonathan E. Cooper, Paul M. Weaver, and Paul Kealy. 2013. “Improved Aeroelastic Tailoring Using Tow-Steered Composites.” Composite Structures 106: 703–15. https://doi.org/10.1016/j.compstruct.2013.07.023
• Stodieck, O., J. E. Cooper, P. M. Weaver, and P. Kealy. 2015. “Optimization of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring.” AIAA Journal 53 (8): 2203–15. https://doi.org/10.2514/1.j053599
• Stodieck, O., J. E. Cooper, P. M. Weaver, and P. Kealy. 2017. “Aeroelastic Tailoring of a Representative Wing Box Using Tow-Steered Composites.” AIAA Journal 55 (4): 1425–39. https://doi.org/10.2514/1.j055364
• Strand, T. 1960. “Minimum Wing Wave Drag with Volume Constraint.” Journal of the Aerospace Sciences 27 (8): 615–19. https://doi.org/10.2514/8.8662
• Su, Weihua, Sean Shan-Min Swei, and Guoming G. Zhu. 2016. “Optimum Wing Shape of Highly Flexible Morphing Aircraft for Improved Flight Performance.” Journal of Aircraft 53 (5): 1305–16. https://doi.org/10.2514/1.c033490
• Su, Zikang, and Honglun Wang. 2015. “A Novel Robust Hybrid Gravitational Search Algorithm for Reusable Launch Vehicle Approach and Landing Trajectory Optimization.” Neurocomputing 162: 116–27. https://doi.org/10.1016/j.neucom.2015.03.063
• Sullins, G. A. 1993. “Demonstration of Mode Transition in a Scramjet Combustor.” Journal of Propulsion and Power 9 (4): 515–20. https://doi.org/10.2514/3.23653
• Sun, Bing, Qi Xu, and Yang Chen. 2018. “Dynamic Modeling and Simulation of a Pressurized System Used in Flight Vehicle.” Chinese Journal of Aeronautics 31 (6): 1232–48. https://doi.org/10.1016/j.cja.2018.03.005
• Sutherland, William. 1893. “LII. the Viscosity of Gases and Molecular Force.” London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science 36 (223): 507–31. https://doi.org/10.1080/14786449308620508
• Svoboda, Filip, Kristian Hengster-Movric, Martin Hromčík, and Zbyněk Šika. 2023. “Decentralized Active Damping Control for Aeroelastic Morphing Wing.” Aerospace Science and Technology 139: 108415. https://doi.org/10.1016/j.ast.2023.108415
• Svoboda, Filip, and Martin Hromcik. 2019. “Active Flutter Suppression by Means of Fixed-Order H∞ Control: Results for the Benchmark Active Control Technology (BACT) Wing.” In 2019 18th European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2019.8795733
• Swaim, Robert L. 1969. “Comment: VTOL Aircraft Dynamics.” Journal of Aircraft 6 (2): 176a-176a. https://doi.org/10.2514/3.44031
• Szczyglowski, Christopher P., Simon A. Neild, Branislav Titurus, Jason Z. Jiang, and Etienne Coetzee. 2019. “Passive Gust Loads Alleviation in a Truss-Braced Wing Using an Inerter-Based Device.” Journal of Aircraft 56 (6): 2260–71. https://doi.org/10.2514/1.c035452
• Taflan, Murat, Howard Smith, and Joseph Loughlan. 2026. “Sizing and Mass Estimation of Truss-Braced Wings, Considering Emerging Propulsion Systems.” Journal of Aircraft 63 (1): 194–208. https://doi.org/10.2514/1.c038402
• Tai, Shang, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu, and Ting Yue. 2023. “Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test.” Aerospace 10 (4): 350. https://doi.org/10.3390/aerospace10040350
• Tai, Shang, Lixin Wang, Ting Yue, and Hailiang Liu. 2021. “Test Data Processing of Fly-by-Wire Civil Aircraft in Low-Speed Wind Tunnel Virtual Flight.” In 2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae52228.2021.9522559
• Takahashi, Hidemi, Tomonari Hirotani, and Hideyuki Taguchi. 2026. “Flush Air-Data Sensing System for a Hypersonic Flight Experimental Vehicle.” AIAA Journal 64 (2): 724–43. https://doi.org/10.2514/1.j065479
• Takahashi, Yusuke, Manabu Matsunaga, Nobuyuki Oshima, and Kazuhiko Yamada. 2019a. “Drag Behavior of Inflatable Reentry Vehicle in Transonic Regime.” Journal of Spacecraft and Rockets 56 (2): 577–85. https://doi.org/10.2514/1.a34069
• Takahashi, Yusuke, Kazuhiko Yamada, Takashi Abe, and Kojiro Suzuki. 2015. “Aerodynamic Heating around Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration Flight.” Journal of Spacecraft and Rockets 52 (6): 1530–41. https://doi.org/10.2514/1.a33170
• Takahashi, Shuhei, Goro Yamano, Kazunobi Wakai, Mitsuhiro Tsue, and Michikata Kono. 2000. “Self-Ignition and Transition to Flame-Holding in a Rectangular Scramjet Combustor with a Backward Step.” Proceedings of the Combustion Institute 28 (1): 705–12. https://doi.org/10.1016/s0082-0784(00)80272-6
• Takashima, Naruhisa, and Mark J. Lewis. 1999. “Optimization of Waverider-Based Hypersonic Cruise Vehicles with off-Design Considerations.” Journal of Aircraft 36 (1): 235–45. https://doi.org/10.2514/2.2430
• Takovitskii, S. A. 2003b. “Pointed Two-Parameter Power-Law Nose Shapes of Minimum Wave Drag.” Journal of Applied Mathematics and Mechanics 67 (5): 731–36. https://doi.org/10.1016/s0021-8928(03)90044-x
• Takovitskii, S. A. 2006b. “The Construction of Symmetric Nose Shapes of Minimum Wave Drag.” Journal of Applied Mathematics and Mechanics 70 (3): 373–77. https://doi.org/10.1016/j.jappmathmech.2006.07.017
• Talty, Patrick K., and Donald J. Caughlin. 1988. “F-16XL Demonstrates New Capabilities in Flight Test at Edwards Air Force Base.” Journal of Aircraft 25 (3): 206–15. https://doi.org/10.2514/3.45579
• Tang, Wei, and Zhong-ke Shi. 2005. “Wavelet Denoising of Flight Flutter Testing Data for Improvement of Parameter Identification.” Chinese Journal of Aeronautics 18 (1): 72–77. https://doi.org/10.1016/s1000-9361(11)60285-9
• Tang, Wei, Zhong-ke Shi, and Hong-chao Li. 2006. “Frequency-Domain GTLS Identification Combined with Time-Frequency Filtering for Flight Flutter Modal Parameter Identification.” Chinese Journal of Aeronautics 19 (1): 44–51. https://doi.org/10.1016/s1000-9361(11)60266-5
• Tanno, Marie, and Hideyuki Tanno. 2021. “Aerodynamic Characteristics of a Free-Flight Scramjet Vehicle in Shock Tunnel.” Experiments in Fluids 62 (7): 150. https://doi.org/10.1007/s00348-021-03229-0
• Tariq, Ikrama, Muhammad Wasim, and Muhammad Umer Sohail. 2026. “Design of a Gain-Scheduled LQR Controller for Landing of a Reusable Launch Vehicle.” Processes 14 (15): 2458. https://doi.org/10.3390/pr14152458
• Taufik, Najwa Z. B., and Naef A. A. Qasem. 2025. “Enhancing Aerodynamics Performance: A Redesign Approach for the Forward-Swept Fixed-Wing UAV.” Transportation Research Procedia 84: 649–56. https://doi.org/10.1016/j.trpro.2025.03.120
• Taylor, Allan H., and L. Robert Jackson. 1978. “Heat-Sink Structural Design Concepts for a Hypersonic Research Airplane.” Journal of Aircraft 15 (4): 199–205. https://doi.org/10.2514/3.58342
• Teofilatto, Paolo. 2001. “Preliminary Aircraft Design: Lateral Handling Qualities.” Aircraft Design 4 (1): 63–73. https://doi.org/10.1016/s1369-8869(00)00025-2
• Terrell, Kevin, and Saleh Zein-Sabatto. 2017. “Intelligent Reconfigurable Control System for Aircraft Flight Control.” In SoutheastCon 2017. IEEE. https://doi.org/10.1109/secon.2017.7925309
• Tetlow, M. R., and A. Smith. 2007. “Flight Trials and Drag Analysis of a Scale Model Floatplane.” In 2007 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2007.352735
• Tetrault, Philippe-Andre, Joseph A. Schetz, and Bernard Grossman. 2001. “Numerical Prediction of Interference Drag of Strut-Surface Intersection in Transonic Flow.” AIAA Journal 39 (5): 857–64. https://doi.org/10.2514/2.1389
• Thies, Christoph. 2022. “Investigation of the Landing Dynamics of a Reusable Launch Vehicle and Derivation of Dimension Loading for the Landing Leg.” CEAS Space Journal 14 (3): 565–76. https://doi.org/10.1007/s12567-022-00456-x
• Thokala, Praveen, Jim Scanlan, and Andy Chipperfield. 2012. “Framework for Aircraft Cost Optimization Using Multidisciplinary Analysis.” Journal of Aircraft 49 (2): 367–74. https://doi.org/10.2514/1.c000187
• Thomas, Charles L. 1971. “Sonic Boom Reflection Factors for Flight near the Threshold Mach Number.” Journal of Aircraft 8 (6): 490–490. https://doi.org/10.2514/3.59127
• Thompson, Glenn O., and Gerald J. Kass. 1972. “Active Flutter Suppression: An Emerging Technology.” Journal of Aircraft 9 (3): 230–35. https://doi.org/10.2514/3.58962
• Thuwis, Glenn A. A., Roeland De Breuker, Mostafa M. Abdalla, and Zafer Gürdal. 2009. “Aeroelastic Tailoring Using Lamination Parameters: Drag Reduction of a Formula One Rear Wing.” Structural and Multidisciplinary Optimization 41 (4): 637–46. https://doi.org/10.1007/s00158-009-0437-6
• Tian, Wei, Ergao Li, Meng Li, et al. 2026a. “Aeroelastic Suppression and Stability Tailoring Mechanism of a Nonlinear Metastructure-Integrated Supersonic Wing.” Journal of Sound and Vibration 643: 119977. https://doi.org/10.1016/j.jsv.2026.119977
• Tian, Wei, Yiheng Wang, Meng Li, Ergao Li, Tian Zhao, and Zhichun Yang. 2026b. “Nonlinear Aeroelastic Metastructure for Wing Flutter Enhancement: Modeling, Simulation and Wind Tunnel Experiment.” Composite Structures 382: 120104. https://doi.org/10.1016/j.compstruct.2026.120104
• Tian, Ye, Shunhua Yang, and Jialing Le. 2016b. “Numerical Study on Effect of Air Throttling on Combustion Mode Formation and Transition in a Dual-Mode Scramjet Combustor.” Aerospace Science and Technology 52: 173–80. https://doi.org/10.1016/j.ast.2016.02.027
• Tianyuan, Hu, and Yu Xiongqing. 2009. “Aerodynamic/Stealthy/Structural Multidisciplinary Design Optimization of Unmanned Combat Air Vehicle.” Chinese Journal of Aeronautics 22 (4): 380–86. https://doi.org/10.1016/s1000-9361(08)60114-4
• Ting, Eric, Daniel Chaparro, Nhan Nguyen, and Gustavo E. C. Fujiwara. 2018. “Optimization of Variable-Camber Continuous Trailing-Edge Flap Configuration for Drag Reduction.” Journal of Aircraft 55 (6): 2217–39. https://doi.org/10.2514/1.c034810
• Tirovolis, Nikolaos L., and Varnavas C. Serghides. 2005. “Unit Cost Estimation Methodology for Commercial Aircraft.” Journal of Aircraft 42 (6): 1377–86. https://doi.org/10.2514/1.12491
• Tischler, Mark B. 1990. “System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design.” Journal of Guidance, Control, and Dynamics 13. https://ntrs.nasa.gov/citations/19900058278
• Tischler, Mark B. 1991. “System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791853
• Tongbiao Guo, Junqiang Bai, and Tihao Yang. 2017. “Investigation of the Variable Camber Continuous Trailing Edge Flap on the Aerodynamic Performance of the Supercritical Airfoil.” In 2017 8th International Conference on Mechanical and Intelligent Manufacturing Technologies (ICMIMT). IEEE. https://doi.org/10.1109/icmimt.2017.7917467
• Trainelli, Lorenzo, and Alberto Rolando. 2011. “Reliable and Cost-Effective Flight Testing of Ultralight Aircraft.” Journal of Aircraft 48 (4): 1342–50. https://doi.org/10.2514/1.c031277
• Tsuchiya, Takeshi, Yoichi Takenaka, and Hideyuki Taguchi. 2007. “Multidisciplinary Design Optimization for Hypersonic Experimental Vehicle.” AIAA Journal 45 (7): 1655–62. https://doi.org/10.2514/1.26668
• Tsushima, Natsuki, and Weihua Su. 2017. “Flutter Suppression for Highly Flexible Wings Using Passive and Active Piezoelectric Effects.” Aerospace Science and Technology 65: 78–89. https://doi.org/10.1016/j.ast.2017.02.013
• Tsushima, Natsuki, Tomohiro Yokozeki, Weihua Su, and Hitoshi Arizono. 2019. “Geometrically Nonlinear Static Aeroelastic Analysis of Composite Morphing Wing with Corrugated Structures.” Aerospace Science and Technology 88: 244–57. https://doi.org/10.1016/j.ast.2019.03.025
• Tu, Guohua, Jianqiang Chen, Xianxu Yuan, et al. 2021. “Progress in Flight Tests of Hypersonic Boundary Layer Transition.” Acta Mechanica Sinica 37 (11): 1589–1609. https://doi.org/10.1007/s10409-021-01153-4
• Tulsyan, Aditya, J. Fraser Forbes, and Biao Huang. 2012. “Designing Priors for Robust Bayesian Optimal Experimental Design.” Journal of Process Control 22 (2): 450–62. https://doi.org/10.1016/j.jprocont.2011.12.004
• Ugwueze, Osita, Thomas Statheros, Nadjim Horri, Michael A. Bromfield, and Jules Simo. 2023. “An Efficient and Robust Sizing Method for eVTOL Aircraft Configurations in Conceptual Design.” Aerospace 10 (3): 311. https://doi.org/10.3390/aerospace10030311
• Uijt_de_Haag, M., and A. Vadlamani. 2006. “Flight Test Evaluation of Various Terrain Referenced Navigation Techniques for Aircraft Approach Guidance.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650633
• Ullah, Junaid, Aleš Prachař, Miroslav Šmíd, et al. 2020. “Reynolds Number and Wind Tunnel Wall Effects on the Flow Field around a Generic UHBR Engine High-Lift Configuration.” CEAS Aeronautical Journal 11 (4): 1009–23. https://doi.org/10.1007/s13272-020-00463-w
• Usman Hafeez, M., M. Ajmal, T. A. Khan, and Z. Khan. 2013. “Comparison of Vane Type External Excitation and Free Air Turbulence Methods for Flutter Flight Testing.” In Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast.2013.6512146
• Vagt, H. T., and H. N. Oppenheimer. 1963. “An Energy Management Display Indicator for the Dyna Soar (X-20) Vehicle.” Proceedings of the IEEE 51 (3): 515–515. https://doi.org/10.1109/proc.1963.1984
• Vaicaitis, Rimas. 1994. “Nonlinear Response and Sonic Fatigue of National Aerospace Space Plane Surface Panels.” Journal of Aircraft 31 (1): 10–18. https://doi.org/10.2514/3.46449
• Vallespin, D., A. Da Ronch, K. J. Badcock, and O. Boelens. 2011. “Vortical Flow Prediction Validation for an Unmanned Combat Air Vehicle Model.” Journal of Aircraft 48 (6): 1948–59. https://doi.org/10.2514/1.c031385
• Van Camp, Verle V., and E. T. Williams. 1975. “Propulsion Options for the Hypersonic Research Airplane.” Journal of Aircraft 12 (7): 611–16. https://doi.org/10.2514/3.59842
• van den Brandt, R., and C. C. de Visser. 2018. “Safe Flight Envelope Uncertainty Quantification Using Probabilistic Reachability Analysis.” IFAC-PapersOnLine 51 (24): 628–35. https://doi.org/10.1016/j.ifacol.2018.09.641
• van der Lee, Joel, Neta Yokev, and Dan Michaels. 2022. “Combustion Instability Due to Combustion Mode Transition in a Cavity-Stabilized Scramjet.” Journal of Propulsion and Power 38 (6): 945–56. https://doi.org/10.2514/1.b38683
• Van Doren, M. L. 1955. “A Complete System for the Flight-Testing of Piloted Aircraft.” IRE Transactions on Telemetry and Remote Control TRC-1 (2): 13–19. https://doi.org/10.1109/irettrc.1955.6538793
• van Oort, E. R., Q. P. Chu, and J. A. Mulder. 2007. “Nonlinear Robust Model Predictive Control for Lifting Body Re-Entry Flight Attitude Control.” IFAC Proceedings Volumes 40 (7): 323–28. https://doi.org/10.3182/20070625-5-fr-2916.00056
• Van Thullenar, C. F. 1957. “The Tornado Research Airplane.” Weatherwise 10 (3): 82–104. https://doi.org/10.1080/00431672.1957.9924976
• Varshneya, D. n.d. “Implementation of Fiber Optic Technology in Flight Controls.” In LEOS ‘92 Conference Proceedings. IEEE. https://doi.org/10.1109/leos.1992.693954
• Vasconcelos, Luiz Eduardo, Nelson Leite, Carlos Pinheiro, and Ot´vio Carpinteiro. 2011. “The Development of a Tool for the Air Data System Calibration Flight Tests Campaign Using Image Processing.” In 2011 24th SIBGRAPI Conference on Graphics, Patterns and Images. IEEE. https://doi.org/10.1109/sibgrapi.2011.38
• Vatandas, O. Erguven, Yilmaz Altuntas, and Mansur Celebi. 2015. “Improvement of Forward Swept Wing Optimization in the Compressible Flow by Using a Hybrid Method.” In 2015 7th International Conference on Recent Advances in Space Technologies (RAST). IEEE. https://doi.org/10.1109/rast.2015.7208309
• Veresnikov, Georgy, Igor Bashkirov, Danila Sobolev, and Daniil Sapronov. 2024. “Algorithm for Computing the Parameters of a Low-Impact Sonic Boom Demonstrator Aircraft in Accordance with Specified Technical Requirements during Preliminary Aerodynamic Design under Epistemic Uncertainty.” In 2024 17th International Conference on Management of Large-Scale System Development (MLSD). IEEE. https://doi.org/10.1109/mlsd61779.2024.10739457
• Vicroy, Dan D., Thomas D. Loeser, and Andreas Schütte. 2012. “Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle.” Journal of Aircraft 49 (6): 1558–83. https://doi.org/10.2514/1.c031501
• Vigil, Pedro, and José Miguel Pérez. 2026. “Optimization of the Thermal Protection System Geometry for a Mars Atmospheric Entry Vehicle.” European Journal of Mechanics - B/Fluids 119: 204537. https://doi.org/10.1016/j.euromechflu.2026.204537
• Viswanath, P. R. 1988. “Passive Devices for Axisymmetric Base Drag Reduction at Transonic Speeds.” Journal of Aircraft 25 (3): 258–62. https://doi.org/10.2514/3.45586
• Viswanath, P. R., and R. Mukund. 1995. “Turbulent Drag Reduction Using Riblets on a Supercritical Airfoil at Transonic Speeds.” AIAA Journal 33 (5): 945–47. https://doi.org/10.2514/3.12838
• Vos, Roelof, Roeland De Breuker, Ron Barrett, and Paolo Tiso. 2007b. “Morphing Wing Flight Control via Postbuckled Precompressed Piezoelectric Actuators.” Journal of Aircraft 44 (4): 1060–68. https://doi.org/10.2514/1.21292
• Vos, Roelof, Zafer Gürdal, and Mostafa Abdalla. 2010. “Mechanism for Warp-Controlled Twist of a Morphing Wing.” Journal of Aircraft 47 (2): 450–57. https://doi.org/10.2514/1.39328
• “VTOL: 1968.” 1969. Journal of Aircraft 6 (4): 289–98. https://doi.org/10.2514/3.44054
• Wahlberg, Bo, Hakan Hjalmarsson, and Petre Stoica. 2010. “On Optimal Input Signal Design for Frequency Response Estimation.” In 49th IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2010.5717921
• Waitman, Sérgio, and Andrés Marcos. 2019. “Active Flutter Suppression: Non-Structured and Structured H∞ Design.” IFAC-PapersOnLine 52 (12): 146–51. https://doi.org/10.1016/j.ifacol.2019.11.184
• Waitman, Sérgio, and Andrés Marcos. 2020. “H∞ Control Design for Active Flutter Suppression of Flexible-Wing Unmanned Aerial Vehicle Demonstrator.” Journal of Guidance, Control, and Dynamics 43 (4): 656–72. https://doi.org/10.2514/1.g004618
• Waldmann, Andreas, Maximilian C. Ehrle, Johannes Kleinert, Daisuke Yorita, and Thorsten Lutz. 2023. “Mach and Reynolds Number Effects on Transonic Buffet on the XRF-1 Transport Aircraft Wing at Flight Reynolds Number.” Experiments in Fluids 64 (5): 102. https://doi.org/10.1007/s00348-023-03642-7
• Walker, D., and I. Postlthewaite. 1991. “A Full-Flight-Envelope High-Bandwidth Rotorcraft Flight Control System.” In [1991] Proceedings of the 30th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1991.261254
• Wan, Zhi-qiang, Hong Yan, De-guang Liu, and Chao Yang. 2005. “Aeroelastic Analysis and Optimization of High-Aspect-Ratio Composite Forward-Swept Wings.” Chinese Journal of Aeronautics 18 (4): 317–25. https://doi.org/10.1016/s1000-9361(11)60251-3
• Wang, Chen, Jinbao Chen, Shan Jia, and Heng Chen. 2020. “Parameterized Design and Dynamic Analysis of a Reusable Launch Vehicle Landing System with Semi-Active Control.” Symmetry 12 (9): 1572. https://doi.org/10.3390/sym12091572
• Wang, Chengrui, Sanchuan Chen, Houde Liu, and Feng Xu. 2024b. “A New Optimal Design of Set-Theoretic Unknown Input Observer for Robust State Estimation.” In 2024 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc64448.2024.10591267
• Wang, Yongjun, Jiang Dong, Xiaodong Liu, and Lixin Zhang. 2015. “Identification and Standardization of Maneuvers Based upon Operational Flight Data.” Chinese Journal of Aeronautics 28 (1): 133–40. https://doi.org/10.1016/j.cja.2014.12.026
• Wang, Zijian, Mingzhe Hou, and Mingrui Hao. 2021c. “Robust Composite Control of Telescopic Wing Morphing Aircraft with Control Allocation.” In 2021 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac53003.2021.9727458
• Wang, Fang, Changchun Hua, and Qun Zong. 2016b. “Disturbance Observer Based Finite Time Control Design for Reusable Launch Vehicle in Re-Entry Phase.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7555060
• Wang, K. Charles, and Kenneth W. Iliff. 2004. “Retrospective and Recent Examples of Aircraft Parameter Identification at NASA Dryden Flight Research Center.” Journal of Aircraft 41 (4): 752–64. https://doi.org/10.2514/1.332
• Wang, Zhengjie, Zhijun Liu, Ningjun Fan, and Meifang Guo. 2013. “Flight Dynamics Modeling of a Small Ducted Fan Aerial Vehicle Based on Parameter Identification.” Chinese Journal of Aeronautics 26 (6): 1439–48. https://doi.org/10.1016/j.cja.2013.10.006
• Wang, Jinli, Xiaowei Liu, Jian Fan, and Zhixuan Tang. 2026a. “Investigation on the Central Combustion of Solid-Fuel Dual-Mode Ramjet Combustor in Ramjet Mode.” Aerospace Science and Technology 172: 111723. https://doi.org/10.1016/j.ast.2026.111723
• Wang, Yingcheng, Xusheng Mu, Qitong Zou, Haojie Liu, and Rui Huang. 2025a. “Body-Freedom Flutter Modeling and Flight Testing of a Flexible Flying Wing Drone.” In 2025 11th International Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae68077.2025.11557799
• Wang, Yalong, Shengjun Qi, and Wenqiang Yin. 2021b. “Flight Mode Demonstration of the Prototype Aircraft Based on Flight Test of Scaled Aircraft.” In 2021 6th International Conference on Automation, Control and Robotics Engineering (CACRE). IEEE. https://doi.org/10.1109/cacre52464.2021.9501289
• Wang, Weiji, Wei Qian, Xinyu Ai, and Yuguang Bai. 2023b. “Flutter Optimization of Large Swept-Back Tri-Wing Flight Vehicles.” Aerospace 10 (10): 854. https://doi.org/10.3390/aerospace10100854
• Wang, Lixin, Shang Tai, Ting Yue, Hailiang Liu, Yanling Wang, and Chen Bu. 2022b. “Longitudinal Aerodynamic Parameter Identification for Blended-Wing-Body Aircraft Based on a Wind Tunnel Virtual Flight Test.” Aerospace 9 (11): 689. https://doi.org/10.3390/aerospace9110689
• Wang, Yueyang, Yifang Tang, and Chaofang Hu. 2025d. “Trajectory Optimization Method for Flexible Hypersonic Vehicle Based on Pigeon-Inspired Optimization.” In 2025 44th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc64809.2025.11179003
• Wang, Zexi, Zhiqiang Wan, Rainer M. J. Groh, and Xiaozhe Wang. 2021a. “Aeroelastic and Local Buckling Optimisation of a Variable-Angle-Tow Composite Wing-Box Structure.” Composite Structures 258: 113201. https://doi.org/10.1016/j.compstruct.2020.113201
• Wang, Lei, and Lixin Wang. 2012. “Reconfigurable Flight Control Design for Combat Flying Wing with Multiple Control Surfaces.” Chinese Journal of Aeronautics 25 (4): 493–99. https://doi.org/10.1016/s1000-9361(11)60412-3
• Wang, Yanan, Zhenguo Wang, Mingbo Sun, and Hongbo Wang. 2018a. “Effects of Auto-Ignition on Combustion Characteristics in a Hydrogen-Fueled Dual-Mode Scramjet Combustor.” Acta Astronautica 153: 154–58. https://doi.org/10.1016/j.actaastro.2018.10.013
• Wang, Mingze, Changzhu Wei, Jialun Pu, and Naigang Cui. 2022c. “Predefined-Time Nonsingular Attitude Control for Vertical-Takeoff Horizontal-Landing Reusable Launch Vehicle.” Applied Sciences 12 (19): 10153. https://doi.org/10.3390/app121910153
• Wang, Mingkai, Guotai Xiaoyang, Ruichen He, Shuguang Zhang, and Jintao Ma. 2023a. “Bi-Layer Sizing and Design Optimization Method of Propulsion System for Electric Vertical Takeoff and Landing Aircraft.” Energy 283: 129052. https://doi.org/10.1016/j.energy.2023.129052
• Wang, Yizhe, and Zhiwei Xu. 2018. “Adaptive Feedforward Compensating Self-Sensing Method for Active Flutter Suppression.” Sensors 18 (10): 3447. https://doi.org/10.3390/s18103447
• Wang, Xiaojun, Yusheng Xu, Peiyan Liu, Lei Wang, and Linxi Zeng. 2023c. “A Sequential Algorithm for Decoupling the Multidisciplinary Constraints of Hypersonic Vehicle Structural Optimization Design in a Thermal Environment.” Structural and Multidisciplinary Optimization 66 (8): 185. https://doi.org/10.1007/s00158-023-03635-4
• Wang, Lixin, Zijian Xu, and Ting Yue. 2016c. “Dynamic Characteristics Analysis and Flight Control Design for Oblique Wing Aircraft.” Chinese Journal of Aeronautics 29 (6): 1664–72. https://doi.org/10.1016/j.cja.2016.10.010
• Wang, Yu, Wei Yao, Zheng Zhang, and Jianwen Liu. 2025b. “Combustion Hysteresis Phenomenon in a Dual-Mode Scramjet.” AIAA Journal 63 (5): 1764–77. https://doi.org/10.2514/1.j064599
• Wang, Ke, Hong Yue, and Hui Yu. 2018c. “Optimal Input Design for Reduction of Parameter Correlations.” In 2018 24th International Conference on Automation and Computing (ICAC). IEEE. https://doi.org/10.23919/iconac.2018.8749035
• Wang, Lixin, Rong Zhao, and Yi Zhang. 2022a. “Aircraft Lateral-Directional Aerodynamic Parameter Identification and Solution Method Using Segmented Adaptation of Identification Model and Flight Test Data.” Aerospace 9 (8): 433. https://doi.org/10.3390/aerospace9080433
• Ward, K. E. 1968. “Contour Plotting for the Transonic Flight-Test Drag Polar.” Journal of Aircraft 5 (2): 191–92. https://doi.org/10.2514/3.43928
• Ward, D. T., and S. J. Miley. 1984. “Practical Flight Test Method for Determining Reciprocating Engine Cooling Requirements.” Journal of Aircraft 21. https://ntrs.nasa.gov/citations/19850034086
• Warren, C. H. E. 1972a. “Sonic Boom Exposure Effects 1.2: The Sonic Boom—Generation and Propagation.” Journal of Sound and Vibration 20 (4): 485–97. https://doi.org/10.1016/0022-460x(72)90671-2
• Warren, C. H. E. 1972b. “Sonic Boom Exposure Effects II.6: Sonic Boom Generators.” Journal of Sound and Vibration 20 (4): 535–39. https://doi.org/10.1016/0022-460x(72)90678-5
• Waszak, M. R., and S. Srinathkumar. 1995. “Flutter Suppression for the Active Flexible Wing: A Classical Design.” Journal of Aircraft 32 (1): 61–67. https://doi.org/10.2514/3.46684
• Watanabe, Shigeya, Shinji Ishimoto, and Yukimitsu Yamamoto. 1997a. “Aerodynamic Characteristics Evaluation of Hypersonic Flight Experiment Vehicle Based on Flight Data.” Journal of Spacecraft and Rockets 34 (4): 464–70. https://doi.org/10.2514/2.3259
• Wei, Mengxuan, Maohang Qiu, Shuai Yang, Xiaoyan Liu, Jeff Taylor, and Dong Cao. 2021. “Development of a Fuel Cell Hybrid Electric Vertical Takeoff and Landing Aircraft Power Train.” In 2021 IEEE Energy Conversion Congress and Exposition (ECCE). IEEE. https://doi.org/10.1109/ecce47101.2021.9595968
• Wei Tang, Zhong-Ke Shi, and Hong-Chao Li. 2005. “Wavelet Denoising for Chirp-like Signal in Time-Frequency Domain and Application to Aircraft Flight Flutter Testing.” In 2005 International Conference on Machine Learning and Cybernetics. IEEE. https://doi.org/10.1109/icmlc.2005.1527506
• Weiss, Matthias, Stephan Staudacher, Jürgen Mathes, Duilio Becchio, and Christian Keller. 2022. “Uncertainty Quantification for Full-Flight Data Based Engine Fault Detection with Neural Networks.” Machines 10 (10): 846. https://doi.org/10.3390/machines10100846
• Weisshaar, Terrence A. 1980b. “Of Forward Swept Composite Wings Divergence.” Journal of Aircraft 17 (6): 442–48. https://doi.org/10.2514/3.57922
• Weisshaar, Terrence A. 1981. “Aeroelastic Tailoring of Forward Swept Composite Wings.” Journal of Aircraft 18 (8): 669–76. https://doi.org/10.2514/3.57542
• Weisshaar, Terrence A. 1985. “Comment on ‘Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft’.” AIAA Journal 23 (6): 978–79. https://doi.org/10.2514/3.48607
• Weisshaar, Terrence A. 1994. “Integrated Structure/control Concepts for Oblique Wing Roll Control and Trim.” Journal of Aircraft 31 (1): 117–24. https://doi.org/10.2514/3.46463
• Weisshaar, Terrence A., and Thomas A. Zeiler. 1983. “Dynamic Stability of Flexible Forward Swept Wing Aircraft.” Journal of Aircraft 20 (12): 1014–20. https://doi.org/10.2514/3.48205
• Wells, William R., Siva S. Banda, and David L. Quam. 1982. “Aircraft Lateral Parameter Estimation from Flight Data with Unsteady Aerodynamic Modeling.” Journal of Aircraft 19 (3): 206–10. https://doi.org/10.2514/3.57377
• Werter, N. P. M., and R. De Breuker. 2016. “A Novel Dynamic Aeroelastic Framework for Aeroelastic Tailoring and Structural Optimisation.” Composite Structures 158: 369–86. https://doi.org/10.1016/j.compstruct.2016.09.044
• Whalen, E., and M. B. Bragg. 2005. “Aircraft Characterization in Icing Using Flight Test Data.” Journal of Aircraft 42 (3): 792–94. https://doi.org/10.2514/1.11198
• Whitfield, Jack D., and B. J. Griffith. 1965. “Comparisons of Free-Flight and Wind-Tunnel Data on Slender Cones.” AIAA Journal 3 (2): 379–80. https://doi.org/10.2514/3.2873
• “Why Supersonic Transport?” 1967. Scientist and Citizen 9 (4): 70–70. https://doi.org/10.1080/21551278.1967.9958648
• Wislicenus, Jan, and Nihad E. Daidzic. 2022. “Estimation of Transport-Category Jet Airplane Maximum Range and Airspeed in the Presence of Transonic Wave Drag.” Aerospace 9 (4): 192. https://doi.org/10.3390/aerospace9040192
• Womer, Norman K., and Thomas R. Gulledge. 1983. “A Dynamic Cost Function for an Airframe Production Program.” Engineering Costs and Production Economics 7 (3): 213–27. https://doi.org/10.1016/0167-188x(83)90015-0
• Womer, Norman Keith, and Ronald C. J. Marcotte. 1986. “Airframe Cost Estimation Using an Error Components Model.” Journal of Cost Analysis 3 (1): 39–62. https://doi.org/10.1080/08823871.1986.10462349
• Woods, William C., Scott D. Holland, and Michael DiFulvio. 2001. “Hyper-X Stage Separation Wind-Tunnel Test Program.” Journal of Spacecraft and Rockets 38 (6). https://ntrs.nasa.gov/citations/20030018892
• Wright, T. P. 1936. “Factors Affecting the Cost of Airplanes.” Journal of the Aeronautical Sciences 3 (4): 122–28. https://doi.org/10.2514/8.155
• Wu, Wei. 2014. “Identification Method for Helicopter Flight Dynamics Modeling with Rotor Degrees of Freedom.” Chinese Journal of Aeronautics 27 (6): 1363–72. https://doi.org/10.1016/j.cja.2014.10.002
• Wu, Jiang, Feng Gao, Shengwen Li, and Fengtian Yang. 2023a. “Conceptual Design and Optimization of Distributed Electric Propulsion General Aviation Aircraft.” Aerospace 10 (5): 387. https://doi.org/10.3390/aerospace10050387
• Wu, Keyi, Thomas O’Leary-Roseberry, Peng Chen, and Omar Ghattas. 2023c. “Large-Scale Bayesian Optimal Experimental Design with Derivative-Informed Projected Neural Network.” Journal of Scientific Computing 95 (1): 30. https://doi.org/10.1007/s10915-023-02145-1
• Wu, Xianju, and Zhijun Wei. 2022. “Comparison of Dual-Combustion Ramjet and Scramjet Performances Considering Combustion Efficiency.” Applied Sciences 13 (1): 480. https://doi.org/10.3390/app13010480
• Wu, Xianju, and Zhijun Wei. 2023. “Analysis of the Characteristics of Scramjet Mode and Ramjet Mode of Axisymmetric Dual-Combustion Ramjet.” Acta Astronautica 203: 125–34. https://doi.org/10.1016/j.actaastro.2022.11.034
• Wu, Mingjian, Tianhang Xiao, Haisong Ang, and Hongda Li. 2017. “Investigation of a Morphing Wing Solar-Powered Unmanned Aircraft with Enlarged Flight Latitude.” Journal of Aircraft 54 (5): 1996–2004. https://doi.org/10.2514/1.c034356
• Wu, Xinyi, and Zhiwei Xu. 2023. “Binocular Vision Monitoring Method Research of Wing Sweep Angles for Morphing Aircraft in Complex Climate Environments.” Measurement 218: 113214. https://doi.org/10.1016/j.measurement.2023.113214
• Wu, Zhi-gang, and Chao Yang. 2004. “Flight Loads and Dynamics of Flexible Air Vehicles.” Chinese Journal of Aeronautics 17 (1): 17–22. https://doi.org/10.1016/s1000-9361(11)60197-0
• Wu, Nan, and Jia Yu. 2018. “Robust Controller Design of Hypersonic Vehicle in Uncertainty Models.” In 3rd International Conference on Electromechanical Control Technology and Transportation. SCITEPRESS - Science and Technology Publications. https://doi.org/10.5220/0006969302880293
• Wunderlich, Tobias, and Sascha Dähne. 2017. “Aeroelastic Tailoring of an NLF Forward Swept Wing: DLR Contribution to LuFo IV Joint Research Project AeroStruct.” CEAS Aeronautical Journal 8 (3): 461–79. https://doi.org/10.1007/s13272-017-0251-6
• Wunderlich, Tobias, Sascha Dähne, Lars Heinrich, and Lars Reimer. 2017. “Multidisciplinary Optimization of an NLF Forward Swept Wing in Combination with Aeroelastic Tailoring Using CFRP: DLR Contribution to the LuFo IV Joint Research Project AeroStruct.” CEAS Aeronautical Journal 8 (4): 673–90. https://doi.org/10.1007/s13272-017-0266-z
• Wurster, K. E., and H. W. Stone. 1993. “Aerodynamic Heating Environment Definition/thermal Protection System Selection for the HL-20.” Journal of Spacecraft and Rockets 30 (5). https://ntrs.nasa.gov/citations/19930069742
• Xi, Liangliang, Jiale Li, and Ran An. 2023. “Research on Flight Test Evaluation Techniques for Unmanned Aircraft in Complex Environments.” In 2023 7th International Symposium on Computer Science and Intelligent Control (ISCSIC), vol. 41. IEEE. https://doi.org/10.1109/iscsic60498.2023.00069
• Xiao, Luo, Song Chao, Zhou Zhu, Liu Hongyang, Tang Yu, and Tang Tao. 2026. “Reduced Multifidelity Low-Sonic-Boom Design for Supersonic Transport by Manifold Alignment.” Journal of Aircraft: 1–12. https://doi.org/10.2514/1.c039004
• Xiao, Lingfei, Yushuo Tan, Xiaole Zhang, and Zirui Han. 2024. “Distributed Hybrid Electric Propulsion Aircraft Design Based on Convex Optimized Power Allocation Management.” Aerospace 11 (5): 408. https://doi.org/10.3390/aerospace11050408
• Xiao, Baoguo, Jianwen Xing, Ye Tian, and Xiyao Wang. 2015. “Experimental and Numerical Investigations of Combustion Mode Transition in a Direct–connect Scramjet Combustor.” Aerospace Science and Technology 46: 331–38. https://doi.org/10.1016/j.ast.2015.08.001
• Xie, Jiacheng, Yu Cai, Darshan Sarojini, Evan D. Harrison, and Dimitri N. Mavris. 2023. “Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft.” Journal of Aircraft 60 (4): 1272–89. https://doi.org/10.2514/1.c037239
• Xijuan, Guo, Zhao Qiang, and Fengfeng Xi. 2016. “Design Segmented Stiff Skin for a Morphing Wing.” Journal of Aircraft 53 (4): 962–70. https://doi.org/10.2514/1.c033252
• Xu, Jinglei, Dashuai Chen, Youfu Song, Shengcheng Ji, and Yu Zhou. 2018b. “Mean Flow Compressibility Effects in Transonic Turbulence Modeling.” Aerospace Science and Technology 79: 492–99. https://doi.org/10.1016/j.ast.2018.06.005
• Xu, Jian, Chenguang Guo, Yuewen Wang, Yong Xiao, and Xiaoxiang Hu. 2025a. “Fault-Tolerant Controller Design for Reusable Launch Vehicle.” Actuators 14 (11): 565. https://doi.org/10.3390/act14110565
• Xu, Jeffrey, and Shawn Keshmiri. 2021. “Flight Test Validation and Verification of the Novel LN Guidance for Unmanned Aerial Systems.” In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas51884.2021.9476808
• Xu, Wenbiao, and Xuejing Lan. 2018. “Entry Trajectory Reconstruction for an Unpowered Reusable Launch Vehicle under the Change of Landing Field.” In 2018 10th International Conference on Modelling, Identification and Control (ICMIC). IEEE. https://doi.org/10.1109/icmic.2018.8529840
• Xu, Zhihang, and Qifeng Liao. 2020. “Gaussian Process Based Expected Information Gain Computation for Bayesian Optimal Design.” Entropy 22 (2): 258. https://doi.org/10.3390/e22020258
• Xu, Zhi, and Shuo Tang. 2010. “RLV (Reusable Launch Vehicle) Reentry Nonlinear Controller Design.” In 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering. IEEE. https://doi.org/10.1109/cmce.2010.5610293
• Xu, DaFu, Zhe Zhang, Ke Wu, et al. 2016. “Recent Progress on Development Trend and Key Technologies of Vertical Take-off Vertical Landing Reusable Launch Vehicle.” Chinese Science Bulletin 61 (32): 3453–63. https://doi.org/10.1360/n972016-00537
• Xue, Fei, Xin Jin, Peihua Feng, et al. 2020c. “Optimization and Verification of Free Flight Separation Similarity Law in High-Speed Wind Tunnel.” Chinese Journal of Aeronautics 33 (2): 501–7. https://doi.org/10.1016/j.cja.2019.09.027
• Xue, Fei, Huaqiang Wang, Zenghui Jiang, and Yuchao Wang. 2020b. “Derivation and Verification of a Similarity Law for Wind-Tunnel Free-Flight Tests of Heavy-Store Separation.” Acta Astronautica 174: 123–30. https://doi.org/10.1016/j.actaastro.2020.04.061
• Xue, Fei, Yuchao Wang, and Han Qin. 2020a. “Derivation and Validation of Wind Tunnel Free-Flight Similarity Law for Store Separation from Aircraft.” Aerospace Science and Technology 97: 105614. https://doi.org/10.1016/j.ast.2019.105614
• Xue, Rongrong, Zhengyin Ye, and Kun Ye. 2019a. “Active Aeroelastic Wing Application on a Forward Swept Wing Configuration.” Engineering Applications of Computational Fluid Mechanics 13 (1): 1063–79. https://doi.org/10.1080/19942060.2019.1663264
• Yamane, Takashi. 1992. “Aeroelastic Tailoring Analysis for Advanced Turbo Propellers with Composite Blades.” Computers & Fluids 21 (2): 235–45. https://doi.org/10.1016/0045-7930(92)90023-o
• Yamane, Takashi, and Peretz P. Friedmann. 1993. “Aeroelastic Tailoring Analysis for Preliminary Design of Advanced Propellers with Composite Blades.” Journal of Aircraft 30 (1): 119–26. https://doi.org/10.2514/3.46315
• Yamato, Hiroyuki, Noriaki Okada, and Toshio Bando. 1991. “Flight Test of the Japanese Upper Surface Blowing STOL Experimental Aircraft ASKA.” Journal of Aircraft 28 (10): 630–37. https://doi.org/10.2514/3.46075
• Yamazaki, Wataru, and Shu Ishida. 2025. “Evaluation of Aerodynamic and Sonic Boom Performance of Supersonic Transport Aircrafts with Multiple Wing Configurations.” Aerospace 12 (5): 421. https://doi.org/10.3390/aerospace12050421
• Yan, Zhang, Chen Bing, Liu Gang, Wei Baoxi, and Xu Xu. 2014. “Influencing Factors on the Mode Transition in a Dual-Mode Scramjet.” Acta Astronautica 103: 1–15. https://doi.org/10.1016/j.actaastro.2014.06.006
• Yan, Xufei, and Renliang Chen. 2019. “Augmented Flight Dynamics Model for Pilot Workload Evaluation in Tilt-Rotor Aircraft Optimal Landing Procedure after One Engine Failure.” Chinese Journal of Aeronautics 32 (1): 92–103. https://doi.org/10.1016/j.cja.2018.06.010
• Yan, De-kun, Xiao Liu, Guo-qiang He, and Robert Martinuzzi. 2022. “Ejector Mode Performance Improvement of Rocket-Based Combined Cycle Engine Designed for Dual-Ramjet Mode.” Aerospace Science and Technology 126: 107637. https://doi.org/10.1016/j.ast.2022.107637
• Yan, Zhang, Zhu Shaohua, Chen Bing, and Xu Xu. 2016. “Hysteresis of Mode Transition in a Dual-Struts Based Scramjet.” Acta Astronautica 128: 147–59. https://doi.org/10.1016/j.actaastro.2016.07.025
• Yanagihara, Masaaki, Masashi Shigemi, and Takanobu Suito. 1999. “Estimating Aerodynamic Characteristics of Automatic Landing Flight Experiment Vehicle Using Flight Data.” Journal of Aircraft 36 (6): 926–33. https://doi.org/10.2514/2.2553
• Yang, Qingchun, Juntao Chang, Wen Bao, and Jun Deng. 2014c. “A Mechanism of Combustion Mode Transition for Hydrogen Fueled Scramjet.” International Journal of Hydrogen Energy 39 (18): 9791–97. https://doi.org/10.1016/j.ijhydene.2014.04.090
• Yang, Haocheng, Tao Chao, and Songyan Wang. 2022a. “Multiobjective Trajectory Optimization for Hypersonic Telescopic Wing Morphing Aircraft Using a Hybrid MOEA/D.” In 2022 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac57257.2022.10054877
• Yang, Yunjie, Jinlai Deng, Xiangyang Wang, Xiaming Yuan, and Jihong Zhu. 2026. “Flight Control and Optimized Allocation for Enhanced Maneuverability of a Tilt-Rotor UAV.” IEEE Transactions on Industrial Electronics 73 (8): 12127–42. https://doi.org/10.1109/tie.2026.3654767
• Yang, Lung-Jieh, and Chao-Kang Feng. 2022. “A Unified Asymptotic Theory of Supersonic, Transonic, and Hypersonic Far Fields.” Axioms 11 (11): 656. https://doi.org/10.3390/axioms11110656
• Yang, Kelong, Dong Han, and Qipeng Shi. 2022b. “Study on the Lift and Propulsive Force Shares to Improve the Flight Performance of a Compound Helicopter.” Chinese Journal of Aeronautics 35 (1): 365–75. https://doi.org/10.1016/j.cja.2021.02.010
• Yang, Pengyu, and Ruiyun Qi. 2016. “Reentry Trajectory Optimization for Hypersonic Vehicle Based on Improved Mesh Refinement Techniques.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554207
• Yang, ChaoMin, and PinQi Xia. 2011. “Aeroelastic Stability of Wing/pylon/rotor Coupled System for Tiltrotor Aircraft in Forward Flight.” Science China Technological Sciences 54 (10): 2708–15. https://doi.org/10.1007/s11431-011-4454-5
• Yang, Changpeng, Tangwen Yin, Weina Zhao, Dan Huang, and Shan Fu. 2014b. “Human Factors Quantification via Boundary Identification of Flight Performance Margin.” Chinese Journal of Aeronautics 27 (4): 977–85. https://doi.org/10.1016/j.cja.2014.03.016
• Yang, Tao, Liu Zhiyong, Xiong Neng, Sun Yan, and Lin Jun. 2018. “Optimization of Positional Parameters of Close-Formation Flight for Blended-Wing-Body Configuration.” Heliyon 4 (12): e01019. https://doi.org/10.1016/j.heliyon.2018.e01019
• Yang, Tihao, Hai Zhong, Yifu Chen, Yayun Shi, Junqiang Bai, and Feifei Qin. 2021. “Transition Prediction and Sensitivity Analysis for a Natural Laminar Flow Wing Glove Flight Experiment.” Chinese Journal of Aeronautics 34 (8): 34–47. https://doi.org/10.1016/j.cja.2020.12.042
• Yanguo, Song, and Wang Huanjin. 2009. “Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft.” Chinese Journal of Aeronautics 22 (3): 250–56. https://doi.org/10.1016/s1000-9361(08)60095-3
• Yao, Xiangjie, Rui Huang, Haiyan Hu, and Haojie Liu. 2024. “Transonic Aerodynamic–Structural Coupling Characteristics Predicted by Nonlinear Data-Driven Modeling Approach.” AIAA Journal 62 (3): 1159–78. https://doi.org/10.2514/1.j063360
• Yao, Zhuoer, Daochun Li, Zi Kan, and Jinwu Xiang. 2025. “Adaptive Terminal Sliding Combined Super Twisting Control Design and Flight Tests for Automatic Carrier Landing System.” Chinese Journal of Aeronautics 38 (4): 103202. https://doi.org/10.1016/j.cja.2024.08.033
• Yasue, Kanako. 2020. “Extraction of Monophasic Data from Flight Test Data via Cluster Analysis.” Journal of Aircraft 57 (3): 399–407. https://doi.org/10.2514/1.c035564
• Yates, Edward H. 1965. “Cost Analysis as an Aid to Aircraft Design.” Journal of Aircraft 2 (2): 100–107. https://doi.org/10.2514/3.43625
• Yechout, T. R. 1988a. “Flight-Test Determination of Aircraft Cruise Characteristics Using Acceleration and Deceleration Techniques.” Journal of Aircraft 25 (7): 577–82. https://doi.org/10.2514/3.45626
• Yingsong, Gu, Yang Zhichun, and He Shun. 2015. “Body Freedom Flutter of a Blended Wing Body Model Coupled with Flight Control System.” Procedia Engineering 99: 46–50. https://doi.org/10.1016/j.proeng.2014.12.506
• You, Hangil, Seongik Kim, and Gun Jin Yun. 2020. “Design Criteria for Variable Camber Compliant Wing Aircraft Morphing Wing Skin.” AIAA Journal 58 (2): 867–78. https://doi.org/10.2514/1.j058002
• Youmin, Z., Z. Hongcai, and D. Guanzhong. 1992. “A New Bias Partitioned Square-Root Information Filter and Smoother for Aircraft Flight State and Parameter Estimation.” In [1992] Proceedings of the 31st IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1992.371628
• Youmin Zhang, Guanzhong Dai, Hongcai Zhang, and Qingguo Li. 1994. “A SVD-Based Extended Kalman Filter and Applications to Aircraft Flight State and Parameter Estimation.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 2. IEEE. https://doi.org/10.1109/acc.1994.752384
• Yu, Junho, and Yoonsoo Kim. 2024. “Fault-Tolerant RS-LQR Based Yaw Control for Distributed Electric Propulsion Aircraft.” In 2024 24th International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.23919/iccas63016.2024.10773016
• Yu, Haitao, Baolin Tian, Zhen Yan, et al. 2023. “Watt Linkage–Based Legged Deployable Landing Mechanism for Reusable Launch Vehicle: Principle, Prototype Design, and Experimental Validation.” Engineering 20: 120–33. https://doi.org/10.1016/j.eng.2022.05.015
• Yu, Yang, Zhengjie Wang, and Shijun Guo. 2017. “Efficient Method for Aeroelastic Tailoring of Composite Wing to Minimize Gust Response.” International Journal of Aerospace Engineering 2017: 1–12. https://doi.org/10.1155/2017/1592527
• Yu, Xiang, and Youmin Zhang. 2015. “Design of Passive Fault-Tolerant Flight Controller against Actuator Failures.” Chinese Journal of Aeronautics 28 (1): 180–90. https://doi.org/10.1016/j.cja.2014.12.006
• Yue, Shuai, Qing Lin, Guang Zheng, and Zhonghua Du. 2022b. “Modeling and Experimental Validation of Vertical Landing Reusable Launch Vehicle under Symmetric Landing Conditions.” Chinese Journal of Aeronautics 35 (12): 156–72. https://doi.org/10.1016/j.cja.2022.06.022
• Yue, Shuai, Branislav Titurus, Zhiqian Li, Chunbo Wu, and Zhonghua Du. 2022a. “Analysis of Liquid Spring Damper for Vertical Landing Reusable Launch Vehicle with Network-Based Methodology.” Nonlinear Dynamics 111 (3): 2135–60. https://doi.org/10.1007/s11071-022-07944-z
• Yue, Shuai, Branislav Titurus, Hong Nie, and Ming Zhang. 2019. “Liquid Spring Damper for Vertical Landing Reusable Launch Vehicle under Impact Conditions.” Mechanical Systems and Signal Processing 121: 579–99. https://doi.org/10.1016/j.ymssp.2018.11.034
• Yue, Ting, Xiangyang Zhang, Lixin Wang, and Junqiang Ai. 2017a. “Flight Dynamic Modeling and Control for a Telescopic Wing Morphing Aircraft via Asymmetric Wing Morphing.” Aerospace Science and Technology 70: 328–38. https://doi.org/10.1016/j.ast.2017.08.013
• Yun, Donggyu, Hyunwoo Kim, Hong-Gye Sung, Hyoung-Sik Choi, and In-Young Yang. 2026. “Performance Modeling and Mode Transition of Dual-Mode Scramjet Engine Considering All Operating Conditions.” Aerospace Science and Technology 175: 111990. https://doi.org/10.1016/j.ast.2026.111990
• Zaw, Khaing Phyo, and Sergey Vladislavovich Baranovski. 2026. “Structural Parameter Selection for Lightweight Composite Aircraft Wings: A Scoping Review of MDO, Aeroelastic Tailoring, and Stacking Sequence Optimization.” Aerospace 13 (6): 563. https://doi.org/10.3390/aerospace13060563
• Zeitler, Andreas, Andreas Schwierz, and Sebastian Hiergeist. 2018. “Datalink System Maturation and Flight Testing of the Sagitta UAS Demonstrator.” In 2018 IEEE/AIAA 37th Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc.2018.8569693
• Zeng, Jie, and Sunil L. Kukreja. 2013. “Flutter Prediction for Flight/Wind-Tunnel Flutter Test under Atmospheric Turbulence Excitation.” Journal of Aircraft 50 (6): 1696–1709. https://doi.org/10.2514/1.c031710
• Zeng, Yu, Shijie Liu, Hongbo Wang, et al. 2026. “Combustion Mode Reorganization via Rotating Detonation: Enabling Efficient Deflagration in a Scramjet Combustor.” Proceedings of the Combustion Institute 42: 106436. https://doi.org/10.1016/j.proci.2026.106436
• Zhang, Bing, Kanglong Chen, and Lei Zu. 2020. “Aeroelastic Tailoring Method of Tow-Steered Composite Wing Using Matrix Perturbation Theory.” Composite Structures 234: 111696. https://doi.org/10.1016/j.compstruct.2019.111696
• Zhang, Liu, and Meng He. 2026. “Virtual Flight Test for Three-Axis Decoupling Fluidic Flight Control of Tailless Flying Wing.” Chinese Journal of Aeronautics 39 (4): 103811. https://doi.org/10.1016/j.cja.2025.103811
• Zhang, Wenjin, Nan Lan, and Ping Sun. 2011. “An Integrated Reliability Evaluation Model of Aircraft Flight Test.” In The Proceedings of 2011 9th International Conference on Reliability, Maintainability and Safety. IEEE. https://doi.org/10.1109/icrms.2011.5979264
• Zhang, Jingchao, Chunsheng Nie, Jinsheng Cai, and Shucheng Pan. 2024. “A Reduced-Order Model for Fast Predicting Ionized Flows of Hypersonic Vehicles along Flight Trajectory.” Chinese Journal of Aeronautics 37 (1): 89–105. https://doi.org/10.1016/j.cja.2023.09.007
• Zhang, YingXue, and GuangRun Sheng. 2019. “Design of Fuzzy Neural Network PID Controller for Hypersonic Vehicle.” In 2019 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac48633.2019.8996408
• Zhang, Cheng, Tao Song, Hong Tao, and Tao Jiang. 2025d. “Flight Envelope Constrained UAV Shipboard Landing Control within an Identified Quiescent Period.” Chinese Journal of Aeronautics 38 (8): 103463. https://doi.org/10.1016/j.cja.2025.103463
• Zhang, Shuo, and Zhengjie Wang. 2019. “Dynamic Distributed Morphing Control of an Aeroelastic Wing for a Small Drone.” Journal of Aircraft 56 (6): 2324–41. https://doi.org/10.2514/1.c035182
• Zhang, Yingxin, Qing Wang, Chaoyang Dong, and Yifan Jiang. 2013. “H∞ Output Tracking Control for Flight Control Systems with Time-Varying Delay.” Chinese Journal of Aeronautics 26 (5): 1251–58. https://doi.org/10.1016/j.cja.2013.07.024
• Zhang, Tian-tian, Zhen-guo Wang, Wei Huang, and Li Yan. 2016. “Parameterization and Optimization of Hypersonic-Gliding Vehicle Configurations during Conceptual Design.” Aerospace Science and Technology 58: 225–34. https://doi.org/10.1016/j.ast.2016.08.020
• Zhang, Chaoyue, Yongchao Wang, Yuxiang Luo, Yufei Jiang, Lintao Wei, and Yaoming Zhou. 2026. “Priority-Driven Multi-Objective Reinforcement Learning for Aggressive Flight Control of Fixed-Wing Aircraft.” Chinese Journal of Aeronautics: 104377. https://doi.org/10.1016/j.cja.2026.104377
• Zhang, Mengchuang, Shasha Xia, Yongsheng Huang, Jiawei Tian, and Zhiping Yin. 2023. “Research on Engine Thrust and Load Factor Prediction by Novel Flight Maneuver Recognition Based on Flight Test Data.” Aerospace 10 (11): 961. https://doi.org/10.3390/aerospace10110961
• Zhang, Shuyang, Hui Yang, Yingjie Guo, Yan Wang, and Zongquan Deng. 2025b. “Design and Aerodynamic Analysis of Leading Edge for Morphing Wing.” Journal of Aircraft 62 (4): 835–46. https://doi.org/10.2514/1.c038158
• Zhang, Xu, Lianjie Yue, Tinglong Huang, Qifan Zhang, and Xinyu Zhang. 2019. “Numerical Investigation of Mode Transition and Hysteresis in a Cavity-Based Dual-Mode Scramjet Combustor.” Aerospace Science and Technology 94: 105420. https://doi.org/10.1016/j.ast.2019.105420
• Zhang, Ping, Li Zhou, Wenjie Cheng, and Tao Qiu. 2015. “Conceptual Design and Experimental Demonstration of a Distributedly Actuated Morphing Wing.” Journal of Aircraft 52 (2): 452–61. https://doi.org/10.2514/1.c032739
• Zhang, Chaofan, Qun Zong, Qi Dong, Bailing Tian, Zhiyu Li, and Jing Zong. 2017a. “Approach and Landing Trajectory Optimization for Reusable Launch Vehicle Using Adaptive Gauss Pseudo-Spectral Method.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027798
• Zhao, Hong, Zhiwei Ding, Gen Leng, and Jianbo Li. 2023b. “Flight Dynamics Modeling and Analysis for a Mars Helicopter.” Chinese Journal of Aeronautics 36 (9): 221–30. https://doi.org/10.1016/j.cja.2023.05.007
• Zhao, Zhen-tao, Xi He, Hao Wang, et al. 2027. “Design and Multi-Objective Optimization Approach for the Waverider Based on Deep Neural Operators.” Aerospace Science and Technology 180: 113728. https://doi.org/10.1016/j.ast.2026.113728
• Zhao, Wei, and Rakesh K. Kapania. 2019. “Actuator Energy and Drag Minimization of a Blended-Wing-Body with Variable-Camber Continuous Trailing-Edge Flaps.” Engineering Optimization 52 (9): 1561–87. https://doi.org/10.1080/0305215x.2019.1660776
• Zhao, Jian, Haiyang Li, Xiangyue He, Yuechen Huang, and Jianghui Liu. 2020. “Uncertainty Analysis for Return Trajectory of Vertical Takeoff and Vertical Landing Reusable Launch Vehicle.” Mathematical Problems in Engineering 2020: 1–18. https://doi.org/10.1155/2020/4313758
• Zhao, Guojun, Zhaoyang Tian, Hongliang Pan, Lei Shi, and Guoqiang He. 2023a. “Combustion Mode and Heat Release Characteristics of a Kerosene-Fueled Rocket-Aided Ramjet Combustor in Ramjet-to-Scramjet Mode Transition.” Aerospace Science and Technology 141: 108529. https://doi.org/10.1016/j.ast.2023.108529
• Zhao, Yanqin, Ye Yuan, and Renliang Chen. 2023c. “Influence of Differential Longitudinal Cyclic Pitch on Flight Dynamics of Coaxial Compound Helicopter.” Chinese Journal of Aeronautics 36 (9): 207–20. https://doi.org/10.1016/j.cja.2023.06.002
• Zhao, Qingfeng, Zhou Zhou, and Zhilin Zhang. 2023d. “Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV.” Journal of Aircraft 60 (6): 1889–1900. https://doi.org/10.2514/1.c037208
• Zhdanov, Oleksander, Olha Sushchenko, and Victor Dehtiarov. 2025. “Research of Flight Lifting Control Surfaces in a Wind Tunnel.” In 2025 IEEE 8th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc61130.2025.11399693
• Zheng, Jiahong, Weizhen Cheng, Yan Li, Shuaike Jiao, and Xide Li. 2025a. “In-Flight Measurement Method and Application Research of Helicopter Rotor Blade Motion Parameters.” Chinese Journal of Aeronautics 38 (9): 103592. https://doi.org/10.1016/j.cja.2025.103592
• Zheng, Ziyang, Biao Wang, Chaoying Tang, and Wei Chen. 2025b. “Modeling and Analysis of Integrated Flight-Propulsion for Distributed Electric Propulsion Aircraft.” In 2025 International Conference on Automation, Electrical Control Systems and Equipment (AECSE). IEEE. https://doi.org/10.1109/aecse67874.2025.11383643
• Zhenxing, Gao, and Gu Hongbin. 2009. “Generation and Application of Spatial Atmospheric Turbulence Field in Flight Simulation.” Chinese Journal of Aeronautics 22 (1): 9–17. https://doi.org/10.1016/s1000-9361(08)60063-1
• Zhi Chaoyou, Li Zhenshui, and Li Xia. 2007. “LXI Addresses Aircraft Flight Control System Simulation Test.” In 2007 IEEE Autotestcon. IEEE. https://doi.org/10.1109/autest.2007.4374261
• Zhigulev, V. N., and Iu. L. Zhilin. 1959. “On Bodies of Minimum Wave Drag.” Journal of Applied Mathematics and Mechanics 23 (6): 1462–75. https://doi.org/10.1016/0021-8928(59)90004-8
• Zhiming, Chen, Yu Yimeng, and Meng Min. 2025. “Research on Decoupling Technology for Flight-Measured Aerodynamic Loads.” In 2025 3rd Asian Aerospace and Astronautics Conference (AAAC). IEEE. https://doi.org/10.1109/aaac66612.2025.11427524
• Zhixin, Guo. 2022a. “Flight Test Scheme Design of Flight Simulator Data Package Sound Acquisition for Civil Aircraft.” In 2022 8th International Conference on Mechanical Engineering and Automation Science (ICMEAS). IEEE. https://doi.org/10.1109/icmeas57305.2022.00057
• Zhixin, Guo. 2022b. “Planning of Flight Simulator Data Package Flight Test for Civil Aircraft.” In 2022 8th International Conference on Mechanical Engineering and Automation Science (ICMEAS). IEEE. https://doi.org/10.1109/icmeas57305.2022.00056
• Zhong, Lunlong, and Mora-Camino Félix. 2015. “A Two-Stage Approach for Managing Actuators Redundancy and Its Application to Fault Tolerant Flight Control.” Chinese Journal of Aeronautics 28 (2): 469–77. https://doi.org/10.1016/j.cja.2015.02.004
• Zhou, Yongquan, Zongfan Bao, Rui Wang, Shilei Qiao, and Yuxiang Zhou. 2015a. “Quantum Wind Driven Optimization for Unmanned Combat Air Vehicle Path Planning.” Applied Sciences 5 (4): 1457–83. https://doi.org/10.3390/app5041457
• Zhou, Jinlong, Linghua Dong, and Weidong Yang. 2022. “Experimental Study on Transfer Functions of an Active Rotor under Different Flight Conditions.” Chinese Journal of Aeronautics 35 (8): 107–20. https://doi.org/10.1016/j.cja.2021.10.026
• Zhou, Xi, Lin Liu, Zong-ji Chen, and Hai-bin Duan. 2007. “Validation of Flight Control Law Based on LFT and Structured Singular Value.” Chinese Journal of Aeronautics 20 (1): 60–65. https://doi.org/10.1016/s1000-9361(07)60008-9
• Zhou, Yunfan, Zhixun Xia, Feng Ding, and Wei Huang. 2023c. “Upgraded Design Methodology for Airframe/engine Integrated Full-Waverider Vehicle Considering Thrust Chamber Design.” Acta Astronautica 211: 1–14. https://doi.org/10.1016/j.actaastro.2023.05.036
• Zhou, Bingkang, Xiangyu Yi, Zhaowei Wang, and Zhufei Li. 2023b. “Aerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic Flow.” AIAA Journal 61 (3): 1435–39. https://doi.org/10.2514/1.j062455
• Zhou, Ling, Rui Zhao, and Renfu Li. 2018. “A Combined Criteria-Based Method for Hypersonic Three-Dimensional Boundary Layer Transition Prediction.” Aerospace Science and Technology 73: 105–17. https://doi.org/10.1016/j.ast.2017.12.002
• Zhu, Wenkai. 2022. “Notes on the Hypersonic Boundary Layer Transition.” Advances in Aerodynamics 4 (1): 23. https://doi.org/10.1186/s42774-022-00117-x
• Zhu, Maolin, and Ning Qin. 2021. “Balancing Laminar Extension and Wave Drag for Transonic Swept Wings.” AIAA Journal 59 (5): 1660–72. https://doi.org/10.2514/1.j059914
• Zimmerman, Norman H., and Jason T. Weissenburger. 1964. “Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds.” Journal of Aircraft 1 (4): 190–202. https://doi.org/10.2514/3.43581
• Zoby, Ernest V., Roop N. Gupta, and Kam-Pui Lee. 1993. “Hypervelocity Stagnation-Point Heating Rate Discrepancies.” Journal of Spacecraft and Rockets 30 (6): 773–74. https://doi.org/10.2514/3.26388
• Zonta, Daniele, Branko Glisic, and Sigrid Adriaenssens. 2013. “Value of Information: Impact of Monitoring on Decision-Making.” Structural Control and Health Monitoring 21 (7): 1043–56. https://doi.org/10.1002/stc.1631

Primary Sources, Non-Peer-Reviewed

• ”- Dimensional Analysis and Dynamic Similitude.” 2015. In Introduction to Fluid Mechanics. CRC Press. https://doi.org/10.1201/b18979-10
• “2 Optimal Experiment Design for Linear Regression Models – a Primer.” 2022. In Optimal Input Signals for Parameter Estimation. De Gruyter. https://doi.org/10.1515/9783110351040-002
• “3 Numerical Search for D-Optimal Designs – Basic Methods for a Linear Regression.” 2022. In Optimal Input Signals for Parameter Estimation. De Gruyter. https://doi.org/10.1515/9783110351040-003
• “5 Optimal Input Signals for Linear Systems Described by ODEs.” 2022. In Optimal Input Signals for Parameter Estimation. De Gruyter. https://doi.org/10.1515/9783110351040-005
• “7 Optimal Input Signals for DPS – Time Domain Synthesis.” 2022. In Optimal Input Signals for Parameter Estimation. De Gruyter. https://doi.org/10.1515/9783110351040-007
• A-21 Aircraft Noise Measurement Aviation Emission Modeling. n.d. Helicopter and V/STOL Aircraft Noise Measurement Problems. SAE International. https://doi.org/10.4271/air1286
• A-4 Aircraft Instruments Committee. n.d.-a. Flight Test Procedures for Static Pressure Systems Installed in Subsonic Transport Aircraft. SAE International. https://doi.org/10.4271/arp921a
• A-4 Aircraft Instruments Committee. n.d.-b. Integrated Flight Instruments and Flight Control Systems. SAE International. https://doi.org/10.4271/air722
• A-5C Aircraft Tires Committee. n.d.-a. Aircraft Tire History. SAE International. https://doi.org/10.4271/air5487
• A-5C Aircraft Tires Committee. n.d.-b. History of Commercial Aircraft New Tire Qualification Testing. SAE International. https://doi.org/10.4271/air5651
• A-6A3 Flight Control and Vehicle Management Systems Cmt. n.d.-a. Aircraft Flight Control Actuation System Failure-Detection Methods. SAE International. https://doi.org/10.4271/air5273a
• A-6A3 Flight Control and Vehicle Management Systems Cmt. n.d.-b. Aircraft Flight Control Systems Descriptions. SAE International. https://doi.org/10.4271/air4094
• Aagren, Tove S., Allen W. Ruan, Carlos Malpica, Shannah Withrow-Maser, and Larry Meyn. 2025. In-Flight System Identification of the Ingenuity Mars Helicopter. Analytical Mechanics Associates, Inc. https://ntrs.nasa.gov/citations/20250010356
• Abada, O., H. Kbab, and S. Haif. 2024. “Optimizing the Design of a Supersonic Planar Dual Bell Nozzle (PDBN).” Kosmìčna nauka ì tehnologìâ 30 (2): 15–27. https://doi.org/10.15407/knit2024.02.015
• Abbas, Ali, and Gordon Hazen. 2025. “On the Value of Information across Decision Problems.” Decision Analysis 22 (1): 1–13. https://doi.org/10.1287/deca.2024.0187
• Abbasi, A. A., and J. E. Cooper. 2009. “Statistical Evaluation of Flutter Boundaries from Flight Flutter Test Data.” Aeronautical Journal 113 (1139): 41–51. https://doi.org/10.1017/s0001924000002761
• Abbass, Amr. 2024. “A Numerical Model for Scramjet and Ramjet Efficiency Study during Dual and Individual Modes of Operation.” Journal of Management and Engineering Sciences: 36–48. https://doi.org/10.61552/jmes.2024.02.002
• Abbott, William Y., John O. Benson, Randall G. Oliver, and Robert A. Williams. 1982. Validation Flight Test of UH-60A for Rotorcraft Systems Integration Simulator (RSIS). Defense Technical Information Center. https://doi.org/10.21236/ada125428
• Abdallah, Ayman M. 2018. “A New Concept for Three-Dimensional Aerodynamic Attitude Flight Envelope.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3153
• Abdallah, Ayman M., Brett A. Newman, and Ashraf M. Omran. 2013. “Measuring Aircraft Nonlinearity across Aerodynamic Attitude Flight Envelope.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4985. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4985
• Abdallah, Ayman M., Brett A. Newman, and Ashraf M. Omran. 2014. “Measuring Aircraft Nonlinearity across Aerodynamic Attitude Flight Envelope-Revisited with Symmetrized Aerodynamics.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2193
• Abdel-Salam, Tarek, and Robert Carson. 2004. “Three-Dimensional Numerical Study of a Dual-Mode Scramjet Combustor.” In 37th AIAA Thermophysics Conference. AIAA 2004-2384. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2384
• Abdel-Salam, T., S. Tiwari, and T. Mohieldin. 2001a. “Analysis of a Dual-Mode Scramjet Combustor.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3194
• Abdel-Salam, T., S. Tiwari, and T. Mohieldin. 2001b. “Dual-Mode Flowfield in Scramjet Combustor.” In 35th AIAA Thermophysics Conference. AIAA 2001-2966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2966
• Abdelkader, Ahmed, M. Harmin, Jonathan Cooper, and F. Bron. 2011. “Aeroelastic Tailoring of Metallic Wing Structures.” In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2011-1712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1712
• Abdullah, Nur Azam, and Erwin Sulaeman. 2013. “Aeroelastic Tailoring of Oscillating Supersonic Wing with External Stores.” Applied Mechanics and Materials 464: 110–15. https://doi.org/10.4028/www.scientific.net/amm.464.110
• Abdulrahim, Mujahid. 2019. “Using Simulated, Unmanned, and Manned Aircraft in Undergraduate Flight Test Engineering Education.” In AIAA Scitech 2019 Forum. AIAA 2019-0065. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0065
• Abdulrahim, Mujahid, and Rick Lind. 2004. “Flight Testing and Response Characteristics of a Variable Gull-Wing Morphing Aircraft.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5113
• Abe, Takashi, Kazuhisa Fujita, Hirotaka Otsu, Kazumori Hama, Shozo Shingu, and Koichi Ichizono. 2001. “Reentry Environment Advanced Diagnostics (READ) Flight-Experiment on USERS Reentry Vehicle.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1905
• Abel, I., J. Newsom, and H. Dunn. 1979. “Application of Two Synthesis Methods for Active Flutter Suppression on an Aeroelastic Wind Tunnel Model.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1633. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1633
• Abel, I., B. Perry III, and H. Murrow. 1977. “Synthesis of Active Controls for Flutter Suppression on a Flight Research Wing.” In Guidance and Control Conference. AIAA 1977-1062. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1062
• Abell, Bruce. 1989. “Response: Costs of the National Aerospace Plane.” Science 246 (4936): 1375–1375. https://doi.org/10.1126/science.246.4936.1375.a
• Abercrombie, Gary E. 1979. Mini-RPV Engine Demonstrator Program. Defense Technical Information Center. https://doi.org/10.21236/ada073573
• Abernethy, Robert B., Gary R. Adams, John W. Steurer, et al. 1986. Uncertainty of in-Flight Thrust Determination. SAE AIR 1678. Pratt and Whitney. https://ntrs.nasa.gov/citations/19880028001
• Abou Khalil, Jacques. n.d. “Experimental and Numerical Study of an Electroactive “Live-Skin” Applied to the Morphing of Aircraft Wing Prototypes for the Greening of Air-Transport.” PhD diss., Université de Toulouse (2023-2025). https://doi.org/10.70675/66b39910zfac2z4bb0za3edz063330634814
• Abou-Kebeh LLano, Sami, Roberto Gil-Pita, and Manuel Rosa-Zurera. 2024. “Application of Deep Learning to Identify Flutter Flight Testing Signals Parameters and Analysis of Real F-18 Flutter Flight Test Data.” Preprint, . https://doi.org/10.20944/preprints202412.0648.v1
• Abramov, Nick, Mikhail Goman, Max Demenkov, and Alex Khrabrov. 2005. “Lateral-Directional Aircraft Dynamics at High Incidence Flight with Account of Unsteady Aerodynamic Effects.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6331. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6331
• Abramson, Jane. 1975. Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Control Airfoil. Defense Technical Information Center. https://doi.org/10.21236/ada027164
• Abrego, Anita I., Kurtis R. Long, and Michael Rutkowski. 2001. A Wind Tunnel Investigation of a Small Scale Tiltrotor Model in Descending Flight. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020052595
• Abrego, Anita I., Thomas H. Maier, and David L. Sharpe. 1999. “Aeroelastic Stability for Straight and Swept-Tip Rotor Blades in Hover and Forward Flight.” In Proceedings of the Vertical Flight Society Forum 55 - Montreal, Canada 1999. The Vertical Flight Society. https://doi.org/10.4050/vfs-f55-00009
• “Accelerated Flight Performance.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.009
• Acevedo Giraldo, Daniel. n.d. “Experimental and Analytical Investigation of the Aerodynamic Noise Emitted by Generic Distributed Electric Propulsion Wing-Propellers Configurations.” PhD diss., Ecully, Ecole centrale de Lyon. https://doi.org/10.70675/91a5e6d8z4c59z4909z9b0bzfadfeea5d797
• Acheson, Kurt, and Mark Rothnie. 2009. “Fast and Accurate Use of Unstructured CFD Methods to Assess Performance and Aerodynamic Heating of Reusable Launch Vehicles in Hypersonic Flight.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3632
• Ackeret, J. 1925. Air Forces on Airfoils Moving Faster than Sound. NACA-TM-317. NASA. https://ntrs.nasa.gov/citations/19930087085
• Acree, C. W., Jr., and Krishna Hoffman. 2004. “Whirl Flutter Studies for a SSTOL Transport Demonstrator.” In American Helicopter Society 4th Decennial Specialist’’s Conference on Aeromechanics. https://ntrs.nasa.gov/citations/20050009924
• Acree, C. W., Jr., C. Kitaplioglu, and M. McCluer. 1997. “Comparison of XV-15 Full-Scale Wind Tunnel and in-Flight Blade-Vortex Interaction Noise.” In Proceedings of the Vertical Flight Society Forum 53 - Virginia Beach, VA 1997. The Vertical Flight Society. https://doi.org/10.4050/vfs-f53-3017
• Active Flutter Suppression. 2016. Wiley. https://doi.org/10.1002/9781118823491.ch4
• “Active Wave Control of Boundary-Layer Transition.” 1990. In Viscous Drag Reduction in Boundary Layers. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865978.0179.0199
• Adams, K. 1983a. “The Air Force Flight Test Center Artificial Icing and Rain Testing Capability.” In 2nd Flight Testing Conference. AIAA 1983-2688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2688
• Adams, K. 1983b. “The Air Force Flight Test Center Palletized Airborne Water Spray System.” In 21st Aerospace Sciences Meeting. AIAA 1983-30. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-30
• Adams, D., and H. Graves. 1983. “Simulation Validation in Support of the Patriot Flight Test Program.” In 2nd Flight Testing Conference. AIAA 1983-2720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2720
• Adams, C., and U. Hinders. 1974. “Design-to-Cost for the a-10 Close Air Support Aircraft.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-963
• Adams, Richard H., and Eugene S. Rubin. 1958. A High Temperature Stream Tube for a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0200634
• Adegbindin, Moustaine, Nathan Love, Rakesh K. Kapania, and Joseph A. Schetz. 2016. “Control Power Optimization Using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2016-3361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3361
• Adelgren, Russell, John Minor, David Warner, and Jason Doster. 2004. The Development of a Hands-On Unmanned Aerial Vehicle/Remotely Piloted Vehicle Flight Test and Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada428090
• Adler, Eytan, and Joaquim R. Martins. 2023. “Blended Wing Body Configuration for Hydrogen-Powered Aviation.” In AIAA AVIATION 2023 Forum. AIAA 2023-4020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4020
• Adolph, C. 1978. “Integrated Test Mission Control: Present and Future at the Air Force Flight Test Center.” In Aircraft Systems and Technology Conference. AIAA 1978-1461. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1461
• Adolph, C. 1981. “The Air Force Flight Test Center: Utah Test and Training Range in the 1980’s.” In 1st Flight Test Conference. AIAA 1981-2487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2487
• Advisory Group for Aerospace Research and Development. 1984. Flight Test Techniques. AD-A147625. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19840026325
• Advisory Group for Aerospace Research and Development. 1997. Future Aerospace Technology in the Service of the Alliance: Sustained Hypersonic Flight: Volume 3. ISBN: 92-836-0049-5. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19980018672
• Advisory Group for Aerospace Research and Development. 1999. System Identification for Integrated Aircraft Development and Flight Testing [l’Identification Des Systemes Pour Le Developpement Integre Des Aeronefs Et Les Essais En Vol]. AC/323(SCI)TP/7. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19990032449
• “Aerodynamic Control Forces and Static Stability.” 2001. In Flight Vehicle Performance and Aerodynamic Control. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861857.0251.0317
• Aerodynamic Drag in Cruising Flight. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch7
• “Aerothermodynamic Assessment of Corrugated Panel Thermal Protection Systems.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0387.0403
• “Aerothermodynamic Base Heating.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0049.0065
• “Aerothermodynamic Design of a Hypersonic Lifting Body Including GPS Navigation Capability.” 1993. In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-4013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4013
• “Aerothermodynamic Entry Environment of the Space Shuttle Orbiter.” 1983. In Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865626.0003.0020
• “Aerothermodynamic Environment for Jovian Entry with Silica Heat Shield.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0108.0128
• “Aerothermodynamics of the Dual-Mode Combustion System.” 2001. In Scramjet Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866609.0569.0595
• Agar, J. R. 1982. DC-10-10 Winglet Flight Test Program Management. Douglas Aircraft Co. https://ntrs.nasa.gov/citations/19840061665
• “The AGARD Flight Test Panel.” 1959. In Stability and Control. Elsevier. https://doi.org/10.1016/b978-1-4831-9730-2.50003-x
• Agarwalla, Soumik. 2025. “Comparative Analysis of Landing-Leg Architectures for Reusable Launch Vehicles.” International Journal For Multidisciplinary Research 7 (5): 58723. https://doi.org/10.36948/ijfmr.2025.v07i05.58723
• Aggarwal, Shiv. 2003. System Identification of X-33 Neural Network. Embry-Riddle Aeronautical Univ. https://ntrs.nasa.gov/citations/20030093594
• Aguilera Munoz, Camilo, and Kenneth H. Yu. 2014. “Effect of Fin-Guided Fuel Injection on Dual Mode Scramjet Operation.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3945
• Ahlefeldt, Thomas, and Jürgen Quest. 2014. “Real-Flight Reynolds Number Microphone-Array Measurements on a Scaled Model in ETW.” In 52nd Aerospace Sciences Meeting. AIAA 2014-1483. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1483
• Ahmed, Raf, A. S. Johnston, J. C. Garrison, J. L. Gaines, and J. D. Waggoner. 2003. Design and Demonstration of Bolt Retractor Separation System for X-38 Deorbit Propulsion Stage. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20030106488
• Ahmed, Feroz, Burak Turhan, Djamel Rezgui, and Mahdi Azarpeyvand. 2024. “Aeroacoustics of Distributed Electric Propulsion Systems: Effect of Rotational Speed Mismatch.” Preprint, . https://doi.org/10.2139/ssrn.4875220
• Ahmed, Y., N. Zayed, and K. Said. 2011. “Calculation of Aerodynamic Heating of a Conical Forebody along Flight Trajectory.” International Conference on Aerospace Sciences and Aviation Technology 11 (ASAT CONFERENCE): 1–16. https://doi.org/10.21608/asat.2011.27136
• Ahn, Jongmin, Kijoon Kim, Seungkeun Kim, and Jinyoung Suk. 2017. “Reconfigurable Flight Control Design for the Complex Damaged Blended Wing Body Aircraft.” International Journal of Aeronautical and Space Sciences 18 (2): 290–99. https://doi.org/10.5139/ijass.2017.18.2.290
• Ahn, Jon, and Donghoon Lee. 2012. “Airfoil Designs and Free-Flight Tests of a Fixed Wing MAV Design.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2774
• Ahtye, W. F. 1980. “A Measurement of Forward-Flight Effects on the Noise from a JT15D-1 Turbofan Engine in the NASA-Ames 40- by 80-Foot Wind Tunnel.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800054471
• Ahuja, Vivek, and Roy Hartfield. 2009. “Optimization of Air-Breathing Hypersonic Aircraft Design for Maximum Cruise Speeds Using Genetic Algorithms.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7323. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7323
• Aiken, William S., and Donald A. Howard. 1949. A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods. NACA-TN-1967. NASA. https://ntrs.nasa.gov/citations/19930082623
• Aiken, William S., and Bernard Wiener. 1955. Analysis of the Horizontal-Tail Loads Measured in Flight on a Multiengine Jet Bomber. NACA-TN-3479. NASA. https://ntrs.nasa.gov/citations/19930084276
• Aiken, William S., Jr., and Raymond A. Fisher. 1956. Lift-Curve Slopes Determined in Flight on a Flexible Swept-Wing Jet Bomber. NACA-RM-L56E21a. NASA. https://ntrs.nasa.gov/citations/19930089410
• Aiken, William S., Jr., and Raymond A. Fisher. 1957. Horizontal-Tail Parameters as Determined from Flight-Test Tail Loads on a Flexible Swept-Wing Jet Bomber. NACA-RM-L56J02. NASA. https://ntrs.nasa.gov/citations/19930089464
• Aiken, William S., Jr., and John A. See. 1951. Strain-Gage Measurements of Buffeting Loads on a Jet-Powered Bomber Airplane. NACA-RM-L50I06. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050031169
• “Air Arc Simulation of Hypersonic Environments.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0663.0700
• Air Force Flight Test Center Edwards AFB CA. 1970. U.S. Air Force Aircraft in Southeast Asia Tested by the Air Force Flight Test Center. Defense Technical Information Center. https://doi.org/10.21236/ada529707
• Air Force Flight Test Center Edwards AFB CA. 1974a. Stability and Control. Volume 1. Stability and Control Flight Test Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada011561
• Air Force Flight Test Center Edwards AFB CA. 1974b. Stability and Control. Volume 2. Stability and Control Flight Test Theory. Defense Technical Information Center. https://doi.org/10.21236/ada011562
• Air Force Flight Test Center Edwards AFB CA. 2002. Flight Test Control Room Personnel Training and Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada402888
• Air Force Test Pilot School Edwards Afb Ca. 1962a. Volume 1. Performance Flight Testing. Appendix a. Symbols Terms and Abbreviations. Defense Technical Information Center. https://doi.org/10.21236/ada320207
• Air Force Test Pilot School Edwards Afb Ca. 1962b. Volume 1. Performance Flight Testing. Appendix B. U.S. Standard Atmosphere Altitude, Temperature, Pressure and Density. Defense Technical Information Center. https://doi.org/10.21236/ada320208
• Air Force Test Pilot School Edwards Afb Ca. 1962c. Volume 1. Performance Flight Testing. Appendix D. Charts of Interest for the USAF Test Pilot School. Defense Technical Information Center. https://doi.org/10.21236/ada320203
• Air Force Test Pilot School Edwards Afb Ca. 1967a. Volume 1. Performance Flight Testing. Appendix C-1. Pitot-Static Position Error Relations. Defense Technical Information Center. https://doi.org/10.21236/ada320209
• Air Force Test Pilot School Edwards Afb Ca. 1967b. Volume 1. Performance Flight Testing. Appendix C-2. Pitot-Static Charts. Defense Technical Information Center. https://doi.org/10.21236/ada320224
• Air Force Test Pilot School Edwards Afb Ca. 1969. Volume II. Flying Qualities Phase, Chapter 16. Chapter 16: Reprint of NASA TN D-5153, the Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities. Defense Technical Information Center. https://doi.org/10.21236/ada319985
• Air Force Test Pilot School Edwards Afb Ca. 1979. Volume 1. Performance Flight Testing. Appendix E. Distribution Tables. Defense Technical Information Center. https://doi.org/10.21236/ada320202
• Air Force Test Pilot School Edwards Afb Ca. 1987. Volume 1. Aircraft Performance. Chapter 10. Hypersonic Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ada320212
• Air Force Test Pilot School Edwards Afb Ca. 1988a. Volume II. Flying Qualities Phase. Chapter 14: Flight Control Systems. Defense Technical Information Center. https://doi.org/10.21236/ada319984
• Air Force Test Pilot School Edwards Afb Ca. 1988b. Volume II. Flying Qualities Phase. Chapter 3: Differential Equations. Defense Technical Information Center. https://doi.org/10.21236/ada319974
• Air Force Test Pilot School Edwards Afb Ca. 1988c. Volume II. Flying Qualities Phase. Chapter 8: Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada319979
• Air Force Test Pilot School Edwards Afb Ca. 1989. Volume II. Flying Qualities Phase. Chapter 9: Roll Coupling. Defense Technical Information Center. https://doi.org/10.21236/ada319980
• Air Force Test Pilot School Edwards Afb Ca. 1990a. Volume II. Flying Qualities Phase. Chapter 6: Maneuvering Flight. Defense Technical Information Center. https://doi.org/10.21236/ada319977
• Air Force Test Pilot School Edwards Afb Ca. 1990b. Volume IV. Flight Test Management. Chapter 1. Introduction to Flight Test Management. Defense Technical Information Center. https://doi.org/10.21236/ada320058
• Air Force Test Pilot School Edwards Afb Ca. 1990c. Volume IV. Flight Test Management. Chapter 5. Flight Test Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ada320062
• Air Force Test Pilot School Edwards Afb Ca. 1991a. Volume 1. Performance Flight Testing. Annex 6A. Programmed Text for Supersonic Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ada320218
• Air Force Test Pilot School Edwards Afb Ca. 1991b. Volume II. Flying Qualities Flight Testing Phase. Chapter 10: High Angle of Attack. Defense Technical Information Center. https://doi.org/10.21236/ada319981
• Air Force Test Pilot School Edwards Afb Ca. 1992a. Volume 1. Performance Flight Testing Phase. Chapter 3. Low L/D.. Defense Technical Information Center. https://doi.org/10.21236/ada320221
• Air Force Test Pilot School Edwards Afb Ca. 1992b. Volume II. Flying Qualities Flight Test. Chapter 11: Engine-Out Theory. Defense Technical Information Center. https://doi.org/10.21236/ada319982
• Air Force Test Pilot School Edwards Afb Ca. 1993. Volume IV. Flight Test Management. Chapter 5A. Instrumentation Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada320063
• Air Force Test Pilot School Edwards Afb Ca. 1994a. Performance Phase Planning Guide. Defense Technical Information Center. https://doi.org/10.21236/ada320219
• Air Force Test Pilot School Edwards Afb Ca. 1994b. Volume 4. Test Management Phase. Chapter 8. Design of Experiments Appendices. Defense Technical Information Center. https://doi.org/10.21236/ada320066
• Air Force Test Pilot School Edwards Afb Ca. 1995. Systems Phase Planning Guide. Defense Technical Information Center. https://doi.org/10.21236/ada320042
• Aircraft and Flight Test Instrumentation. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch3
• Aircraft as Research Tools. 1999. NASA/EW-1999-03-001-DFRC. NASA. https://ntrs.nasa.gov/citations/20000024991
• “Aircraft Cost Considerations.” 2010. In Aircraft Design. Cambridge University Press. https://doi.org/10.1017/cbo9780511844652.018
• “Aircraft Design at the Naval Postgraduate School: Tactical Waverider/long-Range Cargo Aircraft.” 1993. In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-4007. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4007
• “Aircraft Dynamic Stability.” 2003. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862069.0303.0388
• “Aircraft Dynamic Stability.” 2014. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102547.0331.0420
• “Aircraft Flight Control.” 2014. In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/b17346-12
• “Aircraft Flutter Control System Design.” 2011. In Eigenstructure Control Algorithms: Applications to aircraft/rotorcraft handling qualities design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e_ch12
• Aircraft Flutter Testing. 1997. ISBN: 0-16-049155-X. Langley Research Center. https://ntrs.nasa.gov/citations/20020076128
• “Aircraft Lateral-Directional Handling Qualities Design.” 2011. In Eigenstructure Control Algorithms: Applications to aircraft/rotorcraft handling qualities design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e_ch9
• “Aircraft Longitudinal Handling Qualities Design.” 2011. In Eigenstructure Control Algorithms: Applications to aircraft/rotorcraft handling qualities design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e_ch10
• “Aircraft Stability and Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.010
• “Aircraft Stability and Control Augmentation.” 2003. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862069.0433.0472
• “Aircraft Stability and Control Augmentation.” 2014. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102547.0465.0508
• “Aircraft Stability Derivatives.” 1998. In Introduction to Aircraft Flight Dynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862052.0333.0354
• “Aircraft Static Stability.” 2003. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862069.0173.0238
• “Aircraft Static Stability.” 2014. In Introduction to Aircraft Flight Mechanics. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102547.0195.0264
• “Airfoil Static-Pressure Thrust: Flight-Test Verification.” 1990. In Aircraft Design, Systems and Operations Conference. AIAA 1990-3286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3286
• “Airplane Spin Testing.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0383.0416
• Akaryildiz, Bora, Aziz Cihan Kaya, and Reşit Demirkıran. 2025. “Integrating Cross-Axis Decoupling into Conventional Flight Control Laws for Improved Maneuverability in Fighter Aircrafts.” Preprint, . https://doi.org/10.2139/ssrn.5733616
• Akens, D. S., A. R. Jarrell, and L. L. Jones. 1965. History of the George C. Marshall Space Flight Center from January 1: June 30, 1964, Volume 1. NASA-TM-X-57307. NASA. https://ntrs.nasa.gov/citations/19660010357
• Akin, David. 2010. “Applications of Ultra-Low Ballistic Coefficient Entry Vehicles to Existing and Future Space Missions.” In SpaceOps 2010 Conference. AIAA 2010-1928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1928
• Aksu, Arda. 2014. “Aerodynamic Parameter Estimation of a Missile without Wind Angle Measurements.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2557
• Aksu, Tekin, and Sitki Uslu. 2017. “Large-Eddy Simulation of a Dual-Mode Scramjet Combustor Using Non-Adiabatic Flamelet Modeling.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0559. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0559
• Al Bakri, Fawaz. n.d. “Semi-Analytical Terminal and Automatic Approach and Landing Trajectory Planners for Unpowered Reusable Launch Vehicle.” PhD diss., University of Missouri–Columbia. https://doi.org/10.32469/10355/70012
• AL-Bakri, Fawaz F., and Craig A. Kluever. 2017. “Automatic Approach and Landing Trajectory Planner for Unpowered Reusable Launch Vehicle.” Advances in Aerospace Science and Technology 02 (04): 31–47. https://doi.org/10.4236/aast.2017.24004
• Alag, G., J. Burken, and G. Gilyard. 1986. “Eigensystem Synthesis for Active Flutter Suppression on an Oblique-Wing Aircraft.” In Astrodynamics Conference. AIAA 1986-2243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2243
• Alag, G., and E. Duke. 1985. “Development of Control Laws for a Flight Test Maneuver Autopilot Foran F-15 Aircraft.” In Guidance, Navigation and Control Conference. AIAA 1985-1859. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1859
• Albertani, Roberto, Bret Stanford, James Hubner, and Peter Ifju. 2005. “Characterization of Flexible Wing MAVs: Aeroelastic and Propulsion Effects on Flying Qualities.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6324
• Albisser, Marie. n.d. “Identification of Aerodynamic Coefficients from Free Flight Data.” PhD diss., Université de Lorraine. https://doi.org/10.70675/ab94f713z868bz4379za278z50bc17451ea3
• Alex, Alvin, and V. Lijo. 2021. “Unstart Phenomena Induced by Forced Excitation in a Dual-Mode Scramjet.” In Volume 10: Fluids Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2021-69420
• Alexander, Sidney R. 1947. Drag Measurements of a Swept-Back Wing Having Inverse Taper as Determined by Flight Tests at Supersonic Speeds. NACA-RM-L6L30. NASA. https://ntrs.nasa.gov/citations/19930085820
• Alexander, William E. 1970. A Transducer for Controlling Simulated Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0875525
• Alexander, Grover L. 1979. AQUILA Remotely Piloted Vehicle System Technology Demonstrator (RPV-STD) Program. Volume I. System Description and Capabilities. Defense Technical Information Center. https://doi.org/10.21236/ada068345
• Alexander, Michael G. 1991. Subsonic Wind Tunnel Testing Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada240263
• Alexander, W., and J. Foughner Jr. 1973. “Drag and Stability Characteristics of High-Speed Parachutes in the Transonic Range.” In 4th Aerodynamic Deceleration Systems Conference. AIAA 1973-473. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-473
• Alexander, W., and S. Griffin. 1974. “Design Study of Basic Models for Use in the Proposed 8 by 10 Ft. High-Reynolds-Number Transonic Wind Tunnel /HIRT/ at Arnold Engineering Development Center.” In 12th Aerospace Sciences Meeting. AIAA 1974-82. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-82
• Alexander, Walter K., Stanley A. Griffin, and Robert L. Holt. 1973. Wind Tunnel Model Parametric Study for Use in the Proposed 8 Ft x 10 Ft High Reynolds Number Transonic Wind Tunnel (HIRT) at Arnold Engineering Development Center. Defense Technical Information Center. https://doi.org/10.21236/ad0763725
• Alexanderian, Alen. 2021. “Optimal Experimental Design for Infinite-Dimensional Bayesian Inverse Problems Governed by PDEs: A Review.” Inverse Problems 37 (4): 043001. https://doi.org/10.1088/1361-6420/abe10c
• Alexanderian, Alen, Philip J. Gloor, and Omar Ghattas. 2016. “On Bayesian a- and D-Optimal Experimental Designs in Infinite Dimensions.” Bayesian Analysis 11 (3): 671–95. https://doi.org/10.1214/15-ba969
• Alexanderian, Alen, and Steven Maio. 2026. “Submodularity of the Expected Information Gain in Infinite-Dimensional Linear Inverse Problems.” Evolution Equations and Control Theory 25 (0): 262–77. https://doi.org/10.3934/eect.2026090
• Aley, Kade, Tufan K. Guha, and Rajan Kumar. 2018. “Experimental Characterization of a High-Lift Supercritical Airfoil with Microjets.” In 2018 Flow Control Conference. AIAA 2018-3688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3688
• Alford, Lionel D. 2004. How Compensation in Test and Evaluation Affects Aircraft Acquisition. Defense Technical Information Center. https://doi.org/10.21236/ada423468
• Alford, Lionel D., and Robert C. Knarr. 1999. General Flight Test Theory Applied to Aircraft Modifications,. Defense Technical Information Center. https://doi.org/10.21236/ada371942
• Ali, O. A. S. 2026. “A5.3: Toward Virtualized Flight Test Telemetry Architectures in the Era of Digital IF.” In Lectures. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2026/a5.3
• Alich, James, and Benigno Castillo. 2007. “Incorporation of Measurement Science into Flight Test Instrumentation.” In 2007 U.S. Air Force T&E Days. AIAA 2007-1608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1608
• Allel, Moncef, David Bou Saba, and Jérôme Persiani. 2023. “Model-Based Actuator Fault Detection and Isolation of Fleasy’s Innovative VTOL Prototype with Flight Experimental Validation.” In AIAA AVIATION 2023 Forum. AIAA 2023-3453. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3453
• Allen, Julian H. 1957. Motion of a Ballistic Missile Angularly Misaligned with the Flight Path upon Entering the Atmosphere and Its Effect upon Aerodynamic Heating, Aerodynamic Loads, and Miss Distance. NACA-TN-4048. NASA. https://ntrs.nasa.gov/citations/19930084822
• Allen, J. 1964. “Analysis of Booster Systems with a Recoverable Hypersonic Airplane First Stage.” In Aerospace Propulsion Meeting. AIAA 1964-543. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-543
• Allen, Julian H., and A. J. Eggers Jr. 1957. A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth’s Atmosphere at High Supersonic Speeds. NACA-TN-4047. NASA. https://ntrs.nasa.gov/citations/19930084817
• Allen, H. Julian, and A. J. Eggers Jr. 1958. A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth’s Atmosphere at High Supersonic Speeds. NACA-TR-1381. NASA. https://ntrs.nasa.gov/citations/19930091020
• Allen, Christian, Clare Fenwick, Neil Taylor, and Lesmana Djayapertapa. 2003. “Investigation of Flutter Suppression by Active Control.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3510
• Allen, Richard, and Eric Hofbeck. 1986. “An in-Flow Microphone Probe for Airplane Flight Testing.” In 10th Aeroacoustics Conference. AIAA 1986-1890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1890
• Allen, Michael, Andrew Lizotte, Ryan Dibley, and Robert Clarke. 2005. “Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6313
• Allen, B., D. Sauvageau, and C. Joyner. 1994. “Reusable Launch Vehicle Design Flexibility.” In Space Programs and Technologies Conference and Exhibit. AIAA 1994-4499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-4499
• Allen, Timothy, Bradley Sexton, and Matthew J. Scott. 2015. “SUGAR Truss Braced Wing Full Scale Aeroelastic Analysis and Dynamically Scaled Wind Tunnel Model Development.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1171
• Allison, Dennis O., and J. Ray Dagenhart. 1987. Two Experimental Supercritical Laminar-Flow-Control Swept-Wing Airfoils. NASA-TM-89073. NASA. https://ntrs.nasa.gov/citations/19890009895
• Allongue, M., and T. Krysinski. 1990. “Validation of a New General Aerospatiale Aeroelastic Rotor Model through the Wind Tunnel and Flight Tests Data.” In Proceedings of the Vertical Flight Society Forum 46 - Washington, DC 1990. The Vertical Flight Society. https://doi.org/10.4050/vfs-f46-1027
• Alpert, Hannah. n.d. “Reconstructing Surface Heating from an Inflatable Atmospheric Re-Entry Vehicle.” In IEEE Spectrum Webinar. https://ntrs.nasa.gov/citations/20260000127
• Alshabu, A., H. Olivier, V. Herms, and I. Klioutchnikov. 2009. “Wave Processes on a Supercritical Airfoil.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_85
• Altitude Wind Tunnel at NASA Glenn Research Center: An Interactive History. 2008. NASA/SP-2008-4608. NASA. https://ntrs.nasa.gov/citations/20080040678
• Altman, J. 1965. “Some Considerations Associated with Flight Testing the Commercial Supersonic Transport.” In Flight Testing Conference. AIAA 1965-220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-220
• Altman, Aaron. 2015. “Closing the Loop on Aircraft Conceptual Sizing Using the Merlin Flight Simulator.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1012
• Altree, Lillian R., and William F. Baxter. 1968. Legal Aspects of Airport Noise and Sonic Boom. Part 2. Defense Technical Information Center. https://doi.org/10.21236/ad0682902
• Alunno, Emil, Justin D. Sprunger, Spencer Smith, Erik R. Fernandez, and Kareem A. Ahmed. 2026. “MXOD Flight 1: Modular Ground Test Article for Pre-Flight Validation.” In AIAA SCITECH 2026 Forum. AIAA 2026-0344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0344
• Alviani, Robert, Gregory A. Blaisdell, and Jonathan Poggie. 2022. “Computational Analysis of Planned High-Speed Swept Wing-Elevon Experiments.” In AIAA SCITECH 2022 Forum. AIAA 2022-2198. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2198
• Alyanak, Edward J., and Edmund Pendleton. 2014. “A Design Study Employing Aeroelastic Tailoring and an Active Aeroelastic Wing Design Approach on a Tailless Lambda Wing Configuration.” In 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2014-3158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3158
• American Institute of Aeronautics and Astronautics. 1992. 6th AIAA Biennial Flight Test Conference, Hilton Head Island, SC, Aug. 24-26, 1992, Selected Papers. NASA. https://ntrs.nasa.gov/citations/19930027254
• Ames Research Staff. 1953. Equations, Tables, and Charts for Compressible Flow. NACA-TR-1135. NASA. https://ntrs.nasa.gov/citations/19930091059
• Amouyal, G., and D. Weihs. 2015. “Energy-Saving Periodic Flight at Transonic Speeds.” GSTF Journal on Aviation Technology. https://doi.org/10.5176/2382-5758_2.1.12
• Amouyal, G., and D. Weihs. 2016. “Energy-Saving Periodic Flight at Transonic Speeds.” GSTF Journal on Aviation Technology 2 (1): 2. https://doi.org/10.7603/s40957-015-0002-1
• Amundsen, Ruth M., Charles P. Leonard, and Walter E. Bruce III. 2004. Hyper-X Hot Structures Comparison of Thermal Analysis and Flight Data. Paper 109-A0016. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040111308
• An, Chao, Guixi Huo, Yang Meng, and Changchuan Xie. 2024. “Study on Aerodynamic Characteristics and Flight Dynamics of Multi-Body Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-2315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2315
• “Analysis of Gust-Response Flight-Test Data.” 1988. In Gust Loads on Aircraft: Concepts and Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861888.0173.0186
• “Analysis of Jupiter Probe Heat-Shield Recession Uncertainties.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0293.0320
• Anand, A. Vivek, B. Nagaraj Goud, J. Sahana, V. Hariprasad, and K. Arun Kumar. 2019. “Implementing Micropatterned Surface for Drag Reduction in UAV.” International Journal of Recent Technology and Engineering (IJRTE) 8 (4): 4710–14. https://doi.org/10.35940/ijrte.d8548.118419
• Ananthasayanam, M. 1998. “Teaching of Airplane Flight Performance at the Indian Institute of Science, Bangalore.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4524
• Ananthkrishnan, N. 2004. “Small-Perturbation Analysis of Airplane Flight Dynamics: A Reappraisal. I: Longitudinal Modes.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4950. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4950
• Andersen, G., Ed Forster, R. Kolonay, and F. Eastep. 1996. “A Study of Control Surface Blending for Active Aeroelastic Wing Technology.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1443
• Anderson, F. W. 1976. Orders of Magnitude: A History of NACA and NASA, 1915-1976. NASA-SP-4403. NASA. https://ntrs.nasa.gov/citations/19760019059
• Anderson, Griffin. 1987. “An Outlook on Hypersonic Flight.” In 23rd Joint Propulsion Conference. AIAA 1987-2074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2074
• Anderson, Charles. 1993. “Future Technology Aim of the National Aerospace Plane Program.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1988. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1988
• Anderson, Seth B. 2000. Early Years of NASA Ames Flight Research. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20050156611
• Anderson, Erin K., Alana Cardona, and Brian H. Mason. 2023. “Structural Sizing of a Composite Transonic Truss-Braced Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-2083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2083
• Anderson, Logan S., Ryan Caverly, and Jared A. Grauer. 2026. “Active Flutter Suppression Control Design for Wind-Tunnel Testing Using μ -Synthesis.” In AIAA SCITECH 2026 Forum. AIAA 2026-1746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1746
• Anderson, L., W. Engelmann, and E. Scicchitano. 1973. “Emergency Air Start System for the F-14B Flight Test Aircraft.” In 9th Propulsion Conference. AIAA 1973-1252. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1252
• Anderson, S., and R. Innis. 1965. “Stability and Control Considerations for STOL AIRCRAFT.” In Low-Speed Flight Meeting. AIAA 1965-715. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-715
• Anderson, Caroline, and Michael P. Kinzel. 2023. “Numerical Evaluation of Entry System Trajectory Control via Active Porosity Control of Transpiration Cooled Thermal Protection System.” In AIAA SCITECH 2023 Forum. AIAA 2023-0391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0391
• Anderson, D., and W. Stephenson. 1965. “The Role of Ground Testing in Space Flight.” In Flight Testing Conference. AIAA 1965-207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-207
• Anderson, L., J. Vincent, and B. Hildreth. 1983. “AV-8B System Identification Results from Full Scale Development Flight Test Program.” In 2nd Flight Testing Conference. AIAA 1983-2746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2746
• Anderson, F. W., Jr. 1981. Orders of Magnitude: A History of NACA and NASA, 1915: 1980. NASA-SP-4403. NASA. https://ntrs.nasa.gov/citations/19820007082
• Anderton, D. A. 1978. Sixty Years of Aeronautical Research, 1917-1977. NASA-EP-145. NASA. https://ntrs.nasa.gov/citations/19790018918
• André, Thierry, Antoine Durant, and Ivan Fedioun. 2015. “Hypersonic Boundary-Layer Transition Tripped by Wall Injection: Global Mode Analysis.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3525. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3525
• Andrew, G. 1967. “Determination of Subsonic Drag Rise by Limit Line Analysis in the Hodograph Plane.” In 5th Aerospace Sciences Meeting. AIAA 1967-4. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-4
• Andrews, J. 1996. “Performance Analysis of a First Stage Rocket Powered Bounceback Trajectory for RLV Applications.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2772
• Andrews, J. 1998. “Status of the Kistler Reusable Launch Vehicle.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3955
• Andrews, W. H., and H. A. Rediess. 1959. Flight-Determined Stability and Control Derivatives of a Supersonic Airplane with a Low-Aspect-Ratio Unswept Wing and a Tee-Tail. NASA-MEMO-2-2-59H. NASA. https://ntrs.nasa.gov/citations/19630004010
• Andrews, William H., Thomas R. Sisk, and Robert W. Darville. 1956. Longitudinal Stability Characteristics of the Convair YF-102 Airplane Determined from Flight Tests. NACA-RM-H56I17. NASA. https://ntrs.nasa.gov/citations/19930089556
• Andrianatos, Andreas. n.d. “Ground Testing at Superorbital Flight Conditions in a Large Scale Expansion Tube.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2020.628
• Andrisani, Dominick, II, and Mark Jones. 1994. “A Feasibility Study of the Use of Axisymmetric Thrust Vectoring for Enhanced in-Flight Simulation.” In Flight Simualtion Technologies Conference. AIAA 1994-3421. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3421
• “The Anglo-French Supersonic Transport.” 1962. Aircraft Engineering and Aerospace Technology 34 (11): 313–313. https://doi.org/10.1108/eb033632
• Ankenbruck, Herman O. 1954. Determination of Longitudinal Stability in Supersonic Accelerated Maneuvers for the Douglas D-558-II Research Airplane. NACA-RM-L53J20. NASA. https://ntrs.nasa.gov/citations/19930087952
• Ankenbruck, Herman O., and Theodore E. Dahlen. 1953. Some Measurements of Flying Qualities of a Douglas D-558-II Research Airplane during Flights to Supersonic Speeds. NACA-RM-L53A06. NASA. https://ntrs.nasa.gov/citations/19930087460
• Anoosha, V. Yamini, Kushal D. Gowda, Saathvik Bhat, Manjunath Sagar, and Vijay Jaya Vignesh. 2020. “Computational Analysis and Optimization of Boxwing Aircraft for Reducing Induced Drag.” International Journal of Innovative Technology and Exploring Engineering 9 (6): 1966–72. https://doi.org/10.35940/ijitee.f4658.049620
• Antcliff, Richard R., and Anna-Marie R. McGowan. 2000. Active Control Technology at NASA Langley Research Center. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000072568
• Anton, Nicoleta, Ruxandra Botez, and Dumitru Popescu. 2009. “New Methodologies for Aircraft Stability Derivatives Determination from Its Geometrical Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-6046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6046
• Antonison, M., Leik Myrabo, S. Chen, et al. 1989. “Laser-Boosted Lightcraft Technology Demonstrator.” In USRA, NASA(USRA University Advanced Design Program Fifth Annual Summer Conference. https://ntrs.nasa.gov/citations/19940004552
• Anyoji, Masayuki, Kei Nose, Shingo Ida, Daiju Numata, Hiroki Nagai, and Keisuke Asai. 2010. “Low Reynolds Number Airfoil Testing in a Mars Wind Tunnel.” In 40th Fluid Dynamics Conference and Exhibit. AIAA 2010-4627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4627
• Ao, Shuhuai. 2026. “From Concorde to Future Supersonic Transport (SST): Designs for Reducing Sonic Boom in Future Supersonic Commercial Aircraft.” International Journal of Engineering and Technology. https://doi.org/10.7763/ijet.2026.v18.1366
• Ao, Ziqiao, and Jinglai Li. 2024. “On Estimating the Gradient of the Expected Information Gain in Bayesian Experimental Design.” Proceedings of the AAAI Conference on Artificial Intelligence 38 (18): 20311–19. https://doi.org/10.1609/aaai.v38i18.30012
• Aponso, Bimal. 2019. “Physics & History of Vertical Flight.” In Santa Clara High School - NASA Ames Speakers Event. https://ntrs.nasa.gov/citations/20190027589
• “Appendix B: Aircraft Models for Parameter Estimation.” n.d. In Modelling and Parameter Estimation of Dynamic Systems. Institution of Engineering and Technology. https://doi.org/10.1049/pbce065e_appendixb
• Appendix C Stability and Control Derivatives for a Notional GA Aircraft. 2021. Wiley. https://doi.org/10.1002/9781118949818.app3
• “Appendix F Flight Test for Drag Parameters.” 1999. In Performance of Light Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781624103704.0459.0464
• “Application of Dynamic Flight Control to Realization of Aircraft Spatial Flight Manoeuvre.” n.d. In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0043104
• “Application Status and Future Prospect of Aircraft Morphing Wing.” 2023. Journal of Mechanical Engineering 59 (19): 1. https://doi.org/10.3901/jme.2023.19.001
• “Approximate Expressions for the Dimensionless Aerodynamic Stability and Control Derivatives.” 1997. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-340-63200-0.50024-1
• “Approximate Expressions for the Dimensionless Aerodynamic Stability and Control Derivatives.” 2013. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-08-098242-7.00031-6
• “Approximate Expressions for the Dimensionless Aerodynamics Stability and Control Derivatives.” 2007. In Flight Dynamic Principles. Elsevier. https://doi.org/10.1016/b978-075066927-6/50025-8
• “Approximate Inviscid Radiating Flowfield Analysis for Outer Planet Entry Probes.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0042.0064
• Arad, Eran. 2026. “High Fidelity Simulation of Circular-Shape Advanced Hypersonic Vehicles Using Dual Mode Scramjet Propulsion.” In AIAA AVIATION 2026 Forum. AIAA 2026-4173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4173
• Ardema, M., and L. Williams. 1972. “Automated Synthesis of Transonic Transports.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-794
• Ardema, Mark, and Robert Windhorst. 1998. “Optimization of Supersonic Transport Trajectories.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4220
• Arent, Lauren, and Jay Falatko. 1992. “757 Fly-by-Wire Demonstrator Flight Test.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4099
• Aretskin-Hariton, Eliot, Jennifer Gratz, Jason Kirk, et al. 2024. “Multidisciplinary Optimization of a Transonic Truss-Braced Wing Aircraft Using the Aviary Framework.” In AIAA SCITECH 2024 Forum. AIAA 2024-1084. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1084
• Argyris, Costas, and Costas Papadimitriou. 2016. “A Bayesian Framework for Optimal Experimental Design in Structural Dynamics.” In Conference Proceedings of the Society for Experimental Mechanics Series. Springer International Publishing. https://doi.org/10.1007/978-3-319-29754-5_26
• Argyris, Costas, and Costas Papadimitriou. 2017. “Bayesian Optimal Experimental Design Using Asymptotic Approximations.” In Conference Proceedings of the Society for Experimental Mechanics Series. Springer International Publishing. https://doi.org/10.1007/978-3-319-54858-6_26
• Arieli, R., and M. Tauber. 1979. “Computation of Subsonic and Transonic Flow about Lifting Rotor Blades.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1667. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1667
• Armstrong, Johnny G. 1977. Flight Planning and Conduct of the X-24B Research Aircraft Flight Test Program. Defense Technical Information Center. https://doi.org/10.21236/adb029224
• Armstrong, William D., William R. Lindberg, John E. McInroy, and Jonathan W. Naughton. 2006. Active Flutter Suppression Using Cooperative, High Frequency, Dynamic-Resonant Aero-Effectors. Defense Technical Information Center. https://doi.org/10.21236/ada463491
• Army Aviation School Fort Rucker Al. 1961. Evaluation of Automatic Flight Control System AN/ASW-12(V) in an RL-23D Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0255507
• Arnaiz, H. H. 1977. Flight-Measured Lift and Drag Characteristics of a Large, Flexible, High Supersonic Cruise Airplane. NASA-TM-X-3532. NASA. https://ntrs.nasa.gov/citations/19770017156
• Arnaiz, H. H., J. B. Peterson Jr., and J. C. Daugherty. 1980. Wind-Tunnel/flight Correlation Study of Aerodynamic Characteristics of a Large Flexible Supersonic Cruise Airplane (XB-70-1). 3: A Comparison between Characteristics Predicted from Wind-Tunnel Measurements and Those Measured in Flight. NASA-TP-1516. NASA. https://ntrs.nasa.gov/citations/19800009724
• Arnold, Eugene. 1981. “Defending the Flight Test Budget.” In 1st Flight Test Conference. AIAA 1981-2444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2444
• Arnold, James O., and George S. Deiwert. 1997. “Survey of Aerothermodynamics Facilities Useful for the Design of Hypersonic Vehicles Using Air-Breathing Propulsion.” In Future Aerospace Technology in the Service of the Alliance. https://ntrs.nasa.gov/citations/19980018683
• Arnottt, A. D., and L. Bernstein. 2000. “The Aerodynamic Interaction at the Junction between a Forward-Swept Wing and a Plate.” Aeronautical Journal 104 (1032): 67–88. https://doi.org/10.1017/s0001924000017802
• Aronstein, David, and Kurt Schueler. 2004. “Conceptual Design of a Sonic Boom Constrained Supersonic Business Aircraft.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-697. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-697
• Arora, Rajesh, and M. Ananthasayanam. 2003. “Trajectory Design for a Reusable Launch Vehicle Demonstrator during Re-Entry Phase.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5547
• Arora, Rajesh, J. George, and X. Athnasius. 2003. “Trajectory Design for a Flyback Mission of a Reusable Launch Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5546
• Arrow, Bernard. n.d. “A General Approach to the Flutter Problem of Helicopter Blades in Hovering, Vertical, and Forward Flight.” PhD diss., Drexel University. https://doi.org/10.17918/00006625
• Arteaga, Ricardo A., Nickolas Demidovich, John Dinofrio, Chuck Greenlow, James G. Nelson, and Tim Williams. n.d.-a. “High-Altitude ADS-B Flight Tests on a NASA ER-2 Research Airplane.” In SciTech Forum. https://ntrs.nasa.gov/citations/20220014456
• Arteaga, Ricardo A., Nickolas Demidovich, John Dinofrio, Chuck Greenlow, James G. Nelson, and Tim Williams. n.d.-b. “High-Altitude ADS-B/GPS LPV Flight Tests on a NASA ER-2 Research Airplane.” In 2024 AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20230015051
• Arteaga, Ricardo A., Nickolas Demidovich, John Dinofrio, Chuck Greenlow, Timothy Williams, and James Nelson. 2023. “High-Altitude ADS-B Flight Tests on an ER-2 Research Airplane.” In AIAA SCITECH 2023 Forum. AIAA 2023-1589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1589
• Arteaga, Ricardo A., Nickolas Demidovich, John Dinofrio, Chuck Greenlow, Timothy Williams, and James Nelson. 2024. “Flight Testing ADS B and GPS LPV Approaches on a NASA ER-2 Research Airplane.” In AIAA SCITECH 2024 Forum. AIAA 2024-0307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0307
• Ascani, L., B. Burroughs, L. Lackman, and W. Obrien. 1980. “Advanced Structures: Meeting the Challenge of Low-Cost Future Aircraft Systems.” In Aircraft Systems Meeting. AIAA 1980-1868. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1868
• Ashenafi, Yonatan, Piyush Pandita, and Sayan Ghosh. 2022. “Reinforcement Learning-Based Sequential Batch-Sampling for Bayesian Optimal Experimental Design.” Journal of Mechanical Design 144 (9): 091705. https://doi.org/10.1115/1.4054631
• Ashenden, Russell. 1993. “The Air Force Flight Test Center Artificial Icing and Rain Testing Capability Upgrade Program.” In 31st Aerospace Sciences Meeting. AIAA 1993-295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-295
• Asher, Troy A., Timothy L. Willliams, and Brian K. Strovers. 2013. “Reverse Engineering Crosswind Limits: A New Flight Test Technique?” In Society of Experimental Test Pilots. https://ntrs.nasa.gov/citations/20140010193
• Ashokkumar, Chimpalthradi R. 2023. “Machine Actuating Commands for Autonomy of an Unmanned Combat Air Vehicle.” In AIAA SCITECH 2023 Forum. AIAA 2023-2537. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2537
• Ashworth, J., T. Mouch, and M. Luttges. 1988. “Application of Forced Unsteady Aerodynamics to a Forward Swept Wing X-29 Model.” In 26th Aerospace Sciences Meeting. AIAA 1988-563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-563
• Ashworth, J., M. Waltrip, and M. Luttges. 1986. “Three-Dimensional Unsteady Flow Fields Elicited by a Pitching Forward Swept Wing.” In 4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference. AIAA 1986-1104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1104
• Asim, Muhammad Farhat, Jehanzeb Masud, Suhail Akhtar, Bilal Malik, Taimur Ali Shams, and Ibrahim Sher. 2022. “On Improvement of Flight Dynamic Model of a Supersonic Aircraft Using Wind Tunnel to Flight Corrections.” In AIAA SCITECH 2022 Forum. AIAA 2022-0690. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0690
• Askren, W., and E. Vail. 1963. “An Interdisciplinary Effort- the X-20A /Dyna-Soar/ 1962 Centrifuge Flight Simulation Program.” In Heterogeneous Combustion Conference. AIAA 1963-1012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1012
• Aslan, Göktuğ Murat, Dilek F. Kurtulus, Serdar Kirimlioglu, and Zafer Kulunk. 2017. “Aeroelastic Modelling and Testing of a Thin Laminated Composite Missile Fin/Wing.” In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2017-4324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4324
• Asper, Garrett D., and Benjamin M. Simmons. 2022. Rapid Flight Control Law Deployment and Testing Framework for Subscale VTOL Aircraft. NASA/TM-20220011570. NASA. https://ntrs.nasa.gov/citations/20220011570
• Assadourian, Arthur, and John P. Reeder. 1948. Flight Measurements of the Longitudinal Stability and Control Characteristics of the Grumman F8F-1 Airplane, TED No. NACA 2379. NACA-RM-SL8H27. Langley Research Center. https://ntrs.nasa.gov/citations/20050029413
• “Assessment of Alternate Thermal Protection Systems for the Space Shuttle Orbiter.” 1983. In Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865626.0300.0324
• “Assessment of Key Aerothermal Issues for the Structural Design of High Speed Vehicles.” 1992. In Thermal Structures and Materials for High-Speed Flight. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866128.0059.0091
• Astakhov, S. A., V. I. Biryukov, and I. A. Kiselev. 2024. “Vibrational Dynamics of Rocket-Powered Vehicle in High-Speed Monorail Tests of Aircraft Components.” Russian Engineering Research 44 (8): 1196–1201. https://doi.org/10.3103/s1068798x24701776
• “Asymmetric Nose-Tip Shape Change during Atmospheric Entry.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0311.0327
• “Asymptotic Methods for the Prediction of Transonic Wind Tunnel Wall Interference.” 1991. In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1712
• Atencio, A., Jr. 1975. “Wind Tunnel Measurements of Forward Speed Effects on Jet Noise from Suppressor Nozzles and Comparison with Flight Test Data.” In 8th Fluid and PlasmaDynamics Conference. AIAA 1975-870. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-870
• Atencio, A., Jr., J. V. Kirk, P. T. Soderman, and L. P. Hall. 1972. Comparison of Flight and Wind Tunnel Measurements of Jet Noise for the XV-5B Aircraft. NASA-TM-X-62182. NASA. https://ntrs.nasa.gov/citations/19730001302
• Atencio, A., Jr., and P. Soderman. 1973. “Comparison of Aircraft Noise Measured in Flight Test and in the NASA Ames 40- by 80-Foot Wind Tunnel.” In Aeroacoustics Conference. AIAA 1973-1047. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1047
• Atesoglu, Özgür, and Kemal Özgören. 2006. “High-Alpha Flight Maneuverability Enhancement of a Twin Engine Fighter-Bomber Aircraft for Air Combat Superiority Using Thrust-Vectoring Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6056. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6056
• Atkin, Chris. 2004. “Performance Trade-off Studies for a Retrofit Hybrid Laminar Flow Control System.” In 2nd AIAA Flow Control Conference. AIAA 2004-2215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2215
• Atkin, Chris. 2008. “Laminar Flow Control: Leap or Creep?” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-3986. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-3986
• Atkin, Chris, Rob Sunderland, and Shahid Mughal. 2006. “Parametric PSE Studies on Distributed Roughness Laminar Flow Control.” In 3rd AIAA Flow Control Conference. AIAA 2006-3694. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3694
• Atkins, Tim, David M. Gillespie, Todd Honeycutt, et al. n.d. “Artemis I Flight Instrumentation Data Quality Assessment and Processing.” In 2024 AIAA Science and Technology Forum and Exposition (AIAA SciTech Forum). https://ntrs.nasa.gov/citations/20230017158
• Atkinson, R. J. 1964. “The Testing of Supersonic Transport Structures in Fatigue.” In International Council of the Aeronautical Sciences. AIAA 1964-570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-570
• “Atmospheric Entry Probes.” 2007. In Planetary Landers and Entry Probes. Cambridge University Press. https://doi.org/10.1017/cbo9780511536052.019
• “Atmospheric Model.” 1993. In Dynamics of Atmospheric Re-Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861741.0021.0045
• Attar, Shavit, Joel van der Lee, Rudy Kaner, and Dan Michaels. 2026. “Characterization of Dual-Mode Scramjet with Distributed Fuel Injection.” In AIAA SCITECH 2026 Forum. AIAA 2026-0596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0596
• Attia, Ahmed, Sven Leyffer, and Todd S. Munson. 2025. “Robust a-Optimal Experimental Design for Sensor Placement in Bayesian Linear Inverse Problems.” SIAM/ASA Journal on Uncertainty Quantification 13 (2): 744–74. https://doi.org/10.1137/24m1667543
• Aubeelack, Hema. n.d. “Multidisciplinary Design Optimization under Uncertainty of a Blended-Wing-Body Aircraft for Passenger Transport.” PhD diss., Toulouse 3. https://doi.org/10.70675/fa207839z078cz4de3za09fz53641267d140
• August, Colby R., Fotis Kopsaftopoulos, and Peiyuan Zhou. 2026. “Characterizing Morphing Wing States via Stochastic Functional Models for Fly-by-Feel Aircraft.” In AIAA SCITECH 2026 Forum. AIAA 2026-0040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0040
• Aujogue, Nicolas. n.d. “Acoustic Imaging of Aircraft Engine Sources from Flight Test Data.” PhD diss., Lyon, INSA. https://doi.org/10.70675/54571960z44b5z4098zbf77z390e787e10ff
• Aupoix, B. 1993. “Experimental Validation of Hypersonic Viscous Flow Models.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_4
• Austin, Kevin J. n.d. “Evolutionary Design of Robust Flight Control for a Hypersonic Aircraft.” PhD diss., The University of Queensland. https://doi.org/10.14264/105958
• Austin, F., R. Hadcock, D. Hutchings, D. Sharp, S. Tang, and C. Waters. 1976. “Aeroelastic Tailoring of Advanced Composite Lifting Surfaces in Preliminary Design.” In 17th Structures, Structural Dynamics, and Materials Conference. AIAA 1976-1506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1506
• Autenrieb, Johannes. 2023. “Data Fusion-Based Incremental Nonlinear Model Following Control Design for a Hypersonic Waverider Configuration.” In AIAA SCITECH 2023 Forum. AIAA 2023-1997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1997
• “Aviation History and UAS.” n.d. In On Integrating Unmanned Aircraft Systems into the National Airspace System. Springer Netherlands. https://doi.org/10.1007/978-1-4020-8672-4_2
• “Avionics—Part I Steep Landing Systems for VTOL Aircraft.” 1969. Journal of the American Helicopter Society 14 (3): 24–24. https://doi.org/10.4050/jahs.14.3.24
• Awadalla Ali Haj Ahmed, Abdalsalam. 2024. “Aeroelastic Structural Analysis to Calculate Symmetrical Divergence Modes of an Aircraft Wing Using Aerodynamic Lifting Line Theory.” Engineering and Technology Journal 09 (30). https://doi.org/10.47191/etj/v9i10.08
• Axten, Christopher, and Mark Maughmer. 2023. “Comparison of Tail Rotor Performance with a Slotted, Natural-Laminar-Flow Airfoil.” In Proceedings of the Vertical Flight Society 79th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0079-2023-18005
• Ayar, Murat, and K. Melih Guleren. 2019. “A Short Brief on the Aircraft History and Anatomy.” In Sustainable Aviation. Springer International Publishing. https://doi.org/10.1007/978-3-030-14195-0_6
• Ayers, T. G. 1981. “Report of the Wind Tunnel/flight Correlation Panel.” In NASA. Langley Research Center High Reynolds Number Res. - 1980. https://ntrs.nasa.gov/citations/19810022608
• Ayers, T. G. 1982. “Review of the 1980 Wind-Tunnel/Flight Correlation Panel.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017322
• Ayers, T. G. 1990. “The Need for a Hypersonic Demonstrator.” In European Symposium on the Future of High Speed Air Transport. https://ntrs.nasa.gov/citations/19910026354
• Azevedo, Joao. 1987. “Aeroelastic Analysis of Launch Vehicles in Transonic Flight.” In 28th Structures, Structural Dynamics and Materials Conference. AIAA 1987-708. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-708
• Babcock, Deric, and Andrew Arena. 2004. “Estimating Aircraft Stability Derivatives through Finite Element Analysis.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5174
• Babcock, Judson, and Rick Lind. 2012. “Aeroelastic Effects of Wing Stiffness on the Flight Dynamics of a MAV.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4400
• Babcock, Chris, and Joe Salamone. 2006. “Modifications to the Gulfstream Sonic Boom Simulator for the Enhancement of Low-Boom Simulations.” Journal of the Acoustical Society of America 120 (5_Supplement): 3121–3121. https://doi.org/10.1121/1.4787649
• Babineaux, T. 1966. “Experimental Assessment of the Effect of Large Amounts of Argon in Aplanetary Atmosphere on Stagnation-Point Convective Heating.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-29. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-29
• Babu, V. 2021. “Ramjet and Scramjet Engine.” In Fundamentals of Propulsion. Springer International Publishing. https://doi.org/10.1007/978-3-030-79945-8_8
• Babu, Sushanlal, Muhammed Anaz Khan, P. Rohith, V. R. Levi Reuben, and Ajith Raj Rajendran. 2026. “A Comprehensive Numerical Study on Trailing-Edge Camber Morphing of a NACA 4412 Airfoil for Aerodynamic Performance Enhancement and Longitudinal Stability of Fixed-Wing UAVs.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01260-1
• Bach, R., Jr. 1980. “A Variational Technique for Smoothing Flight-Test and Accident Data.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1601
• Bach, R., Jr., and R. Wingrove. 1983. “Applications of State Estimation in Aircraft Flight-Data Analysis.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2087
• Bachalo, W., D. Modarress, and D. Johnson. 1977. “Experiments on Transonic and Supersonic Turbulent Boundary-Layer Separation.” In 15th Aerospace Sciences Meeting. AIAA 1977-47. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-47
• Bachalo, W., J. Smith, and R. Rudoff. 1990. Advanced Instrumentation for Aircraft Icing Research. NASA-CR-185225. NASA. https://ntrs.nasa.gov/citations/19900011690
• Bachelder, Ed, and Bimal Aponso. 2020a. “Novel Techniques for Characterizing and Testing Aircraft Handling Qualities.” In Proceedings of the Vertical Flight Society Handling Qualities 2020 Technical Meeting - Huntsville, Alabama 2020. The Vertical Flight Society. https://doi.org/10.4050/sm_2020_hq-915
• Bachelder, Ed, and Bimal Aponso. 2020b. “Novel Techniques for Characterizing and Testing Aircraft Handling Qualities Part Two.” In Proceedings of the Vertical Flight Society Handling Qualities 2020 Technical Meeting - Huntsville, Alabama 2020. The Vertical Flight Society. https://doi.org/10.4050/sm_2020_hq-914
• Bachelder, Edward, Bimal Aponso, US Army CCDC AvMC, Jeffrey Lusardi, and Martine Godfroy-Cooper. 2020. “Estimating Handling Qualities Ratings from Slalom Flight Data: A Psychophysical Perspective.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16387
• Bachelder, Edward, David Klyde, Peter Thompson, and Chuck Harris. 2004. “System Identification Methods for Improving Flutter Flight Test Techniques.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5065. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5065
• Bachelder, Ed, Peter Thompson, David Klyde, and Daniel Alvarez. 2011. “A New System Identification Method Using Short Duration Flight Test Inputs.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6445. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6445
• Bade, W. L. 1975. “Stagnation-Point Heat Transfer Correlation for Ionized Gases.” Physics of Fluids 18 (8): 1073–74. https://doi.org/10.1063/1.861259
• Baer-Riedhart, J. 1981. “The Development and Flight Test Evaluation of an Integrated Propulsion Control System for the HiMAT Research Airplane.” In 1st Flight Test Conference. AIAA 1981-2467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2467
• Baer-Riedhart, Jennifer L., and Robert J. Landy. 1987. Highly Integrated Digital Electronic Control: Digital Flight Control, Aircraft Model Identification, and Adaptive Engine Control. NASA-TM-86793. NASA. https://ntrs.nasa.gov/citations/19870014186
• Baggett, Jennifer, Andrew Kreshock, and Jinwei Shen. 2021. “Comparison of Wind Tunnel Tiltrotor Loads of Two Hub Types under Different Pylon Angles with Multibody Dynamics Analyses.” In Proceedings of the Vertical Flight Society 77th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0077-2021-16759
• Bahm, Catherine, Ethan Baumann, John Martin, David Bose, Roger Beck, and Brian Strovers. 2005. “The X-43A Hyper-X Mach 7 Flight 2 Guidance, Navigation, and Control Overview and Flight Test Results.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3275
• Bahm, Catherine M., and Edward A. Haering Jr. 1995. Ground-Recorded Sonic Boom Signatures of F-18 Aircraft Formation Flight. NASA-TM-104312. NASA. https://ntrs.nasa.gov/citations/19960009267
• Bahm, Catherine M., and Edward A. Haering Jr. 1996. “Ground-Recorded Sonic Boom Signatures of F-18 Aircraft in Formation Flight.” In The 1995 NASA High-Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/19960055060
• Bai, Chen-Yuan, Juan Li, and Zi-Niu Wu. 2015. “Unsteady Lift for Impulsively Started Transonic/Supersonic Flow.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2015-53062
• Bai, Xue, Ning Tang, and Wei Li. 2019. “Design and Implementation of Flight Test Parameter Calibration Data Management System.” Journal of Physics: Conference Series 1419 (1): 012026. https://doi.org/10.1088/1742-6596/1419/1/012026
• Baier, Robert J. 1970. Flight Test Evaluation of a Supercritical-Speed Shaft. Defense Technical Information Center. https://doi.org/10.21236/ad0878050
• Bailey, Roger M., Robert W. Hostetler Jr., Kevin N. Barnes, Celeste M. Belcastro, and Christine M. Belcastro. 2005. Experimental Validation: Subscale Aircraft Ground Facilities and Integrated Test Capability. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050232740
• Bailey, William D., Andrew J. Knoedler, David A. Harris, and Bruce H. McClintock. 1996. Investigation of Using Global Positioning for Air Data System Calibration of General Aviation Aircraft (Have Pacer II). Defense Technical Information Center. https://doi.org/10.21236/ada303524
• Bailey, Randall, Louis Knotts, Scott Horowitz, and Hugh Malone III. 1987. “Effect of Time Delay on Manual Flight Control and Flying Qualities during in-Flight and Ground-Based Simulation.” In Flight Simulation Technologies Conference. AIAA 1987-2370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2370
• Bailey, Randall E., Steve Williams, Kemper Kibler, and Trey Arthur. 2020. “eXternal Vision System Development and Testing for X-59 Low Boom Flight Demonstrator.” In AIAA Aviation 2020 Forum. AIAA 2020-3087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3087
• Baird, Weldon R. 1964. Summary of the Aerothermoelastic Development Program for the X-20A (Dyna-Soar). Defense Technical Information Center. https://doi.org/10.21236/ad0450460
• Baird, E. F., N. S. Sinder, and R. B. Wittman. 1975. “Stabilizer Flutter Investigated by Flight Test.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003017
• Baize, Daniel G. 1996. The 1995 NASA High-Speed Research Program Sonic Boom Workshop. NASA-CP-3335-Vol-1. NASA. https://ntrs.nasa.gov/citations/19960055049
• Bajaj, Anhad Singh. 2019. “Development of Flight Envelope of a Twin Turboprop Aircraft (ATR-72).” Preprint, . https://doi.org/10.31224/osf.io/ecxpv
• Baker, Thomas F. 1953a. Results of Measurements of Maximum Lift and Buffeting Intensities Obtained during Flight Investigation of the Northrop X-4 Research Airplane. NACA-RM-L53G06. NASA. https://ntrs.nasa.gov/citations/19930087804
• Baker, Thomas F. 1953b. Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range from 0.5 to 0.95. NACA-RM-L53I17. NASA. https://ntrs.nasa.gov/citations/19930087898
• Baker, Thomas F. 1954. Measured Data Pertaining to Buffeting at Supersonic Speeds of the Douglas D-558-II Research Airplane. NACA-RM-L53L10. NASA. https://ntrs.nasa.gov/citations/19930088116
• Bakos, Robert J. n.d. “An Investigation of Test Flow Nonequilibrium Effects on Scramjet Combustion.” PhD diss., The University of Queensland. https://doi.org/10.14264/366376
• Bakos, R., A. Castrogiovanni, J. Calleja, L. Nucci, and J. Erdos. 1996. “Expansion of the Scramjet Ground Test Envelope of the Hypulse Facility.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4506
• Bakos, R. J., C.-Y. Tsai, R. C. Rogers, and A. T. Shih. 1999. The Mach 10 Component of NASA’s Hyper-X Ground Test Program. General Applied Science Labs., Inc. https://ntrs.nasa.gov/citations/20040086987
• Bakos, R. J., C.-Y. Tsai, R. C. Rogers, and A. T. Shih. 2001. Hyper-X Mach 10 Engine Flowpath Development: Fifth Entry Test Conditions and Methodology. AIAA Paper 2001-1814. General Applied Science Labs., Inc. https://ntrs.nasa.gov/citations/20010058924
• Balakrishnan, S., J. Shen, J. Grohs, S. Balakrishnan, J. Shen, and J. Grohs. 1997. “Hypersonic Vehicle Trajectory Optimization and Control.” In Guidance, Navigation, and Control Conference. AIAA 1997-3531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3531
• Balakumar, Ponnampalam, and Amanda Chou. 2016. “Transition Prediction in Hypersonic Boundary Layers Using Receptivity and Freestream Spectra.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0847
• Balaram, Bob, Timothy Canham, Courtney Duncan, et al. 2018. “Mars Helicopter Technology Demonstrator.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0023
• Balas, Gary, Peter Seiler, and Claudia Moreno. 2011. “Linear Parameter Varying Control for the X-53 Active Aeroelastic Wing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6290
• Balch, David T. 1978. “Full-Scale Wind Tunnel Tests of a Modern Helicopter Main Rotor Correlation with Model Rotor Test Data and with Theory.” In Proceedings of the Vertical Flight Society Forum 34 - Washington, D.C. 1978. The Vertical Flight Society. https://doi.org/10.4050/vfs-f34-003
• Baldwin, G. Douglas. 2007. “Utility of a Mono Tiltrotor (MTR) Scaled Demonstrator.” In Proceedings of the Vertical Flight Society Forum 63 - Virginia Beach, VA 2007. The Vertical Flight Society. https://doi.org/10.4050/vfs-f63-100
• Ball, Dale L. 2013. “An Early Demonstration of the Role That ICME Can Play in Airframe Design and Cost Analyses.” In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2013-1849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1849
• Ballano Martinez, Roman, Matej Andrejasic, and Julien Christophe. 2025. “Aerodynamic and Aeroacoustic Optimization of Distributed Electric Propulsion Systems.” In Measurement, Modelling and Simulations Techniques for Novel Aircraft Architectures. von Karman Institute for Fluid Dynamics. https://doi.org/10.35294/ls2025-01-ballano-martinez
• Ballouz, Elie Robert, and Bor-Chin Chang. n.d. “Aircraft Flight Control System Analysis and Design.” PhD diss., Drexel University. https://doi.org/10.17918/etd-7772
• Baltes, Edmund, and Wilfried Spitz. 2002. “Virtual Flight Test as Advanced Step in Aircraft Development.” In AIAA’s Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum. AIAA 2002-5823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5823
• Bamber, Millard J. 1961. Aircraft Store Trajectories Predicted from Wind-Tunnel Investigations Compared with Full-Scale Flight Results. Defense Technical Information Center. https://doi.org/10.21236/ad0267450
• Banerjee, Portia, and Matteo Corbetta. 2021. “Uncertainty Quantification of Expected Time-of-Arrival in UAV Flight Trajectory.” In AIAA Aviation 2021 Forum. AIAA 2021-2380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2380
• Bania, Piotr, and Anna Wójcik. 2025. “An Approximate Bayesian Approach to Optimal Input Signal Design for System Identification.” Preprint, . https://doi.org/10.20944/preprints202509.1390.v2
• Banks, Daniel W. 2008. “Detection and Characterization of Boundary-Layer Transition in Flight at Supersonic Conditions Using Infrared Thermography.” In 13th International Symposium on Flow Visualization. https://ntrs.nasa.gov/citations/20080030370
• Banks, Daniel. 2009. “Flight Research and Validation Formerly Experimental Capabilities Supersonic Project.” In NASA ARMD Fundamental Aeronautics Program 2009 Annual Review. https://ntrs.nasa.gov/citations/20090037047
• Banks, Daniel W. 2011. “Flight Research and Validation Overview.” In 2011 Technical Conference. https://ntrs.nasa.gov/citations/20120001675
• Banks, Daniel. 2012. “Flight Research and Validation Overview.” In 2012 NASA Fundamental Aeronautics Program Annual Technical Conference. https://ntrs.nasa.gov/citations/20120011979
• Banks, Daniel W., and David F. Fisher. 2006. Aft-End Flow of a Large-Scale Lifting Body during Free-Flight Tests. NASA/TM-2006-213681. NASA. https://ntrs.nasa.gov/citations/20060026026
• Banks, Daniel W., Michael A. Frederick, and Peter Sturdza. 2011. “Supersonic Boundary Layer Transition Flight Experiment.” In Fundamental Aeronautics Program 2011 Annual Meeting. https://ntrs.nasa.gov/citations/20120002661
• Banks, D. W., M. A. Frederick, R. R. Tracy, J. R. Matisheck, and N. D. Vanecek. 2012a. In-Flight Boundary-Layer Transition of a Large Flat Plate at Supersonic Speeds. NASA/TM-2012-216021. NASA. https://ntrs.nasa.gov/citations/20120015436
• Banks, Daniel W., Michael Alan Fredericks, Richard R. Tracy, Jason R. Matisheck, and Neal D. Vanecek. 2012b. “In-Flight Boundary-Layer Transition on a Large Flat Plate at Supersonic Speeds.” In 15th International Symposium on Flow Visualization. https://ntrs.nasa.gov/citations/20120014341
• Banks, H. T., and K. L. Rehm. 2014. “Parameter Estimation in Distributed Systems: Optimal Design.” Eurasian Journal of Mathematical and Computer Applications 2 (1): 70–80. https://doi.org/10.32523/2306-6172-2014-2-1-70-80
• Banner, R. D., and M. R. Kinsler. 1961. Status of X-15 Aerodynamic-Heating Studies. ARS PAPER-1629-61. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19630005436
• Banner, R. D., A. E. Kuhl, and R. D. Quinn. 1962. Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane. NASA-TM-X-638. NASA. https://ntrs.nasa.gov/citations/19660020178
• Banner, Richard D., John G. McTigue, and Gilbert Petty Jr. 1958. Boundary-Layer-Transition Measurements in Full-Scale Flight. NACA-RM-H58E28. National Advisory Committee for Aeronautics. High-Speed Flight Station. https://ntrs.nasa.gov/citations/19630008170
• Bansal, Sahil. 2019. “Bayesian Optimal Experimental Design Involving Multiple Setups for Dynamic Structural Testing.” International Journal for Uncertainty Quantification 9 (5): 439–52. https://doi.org/10.1615/int.j.uncertaintyquantification.2019025897
• Barbaux, Yann, and Jacques Cinquin. n.d. “Materials for Supersonic Civil Transport Aircraft.” In Aerospace Materials. IOP Publishing Ltd. https://doi.org/10.1887/0750307420/b873c4
• Barham, Robert. 1994. “Thrust Vector Aided Maneuvering of the YF-22 Advanced Tactical Fighter Prototype.” In Biennial Flight Test Conference. AIAA 1994-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2105
• Barker, W. 1966. “The Hoverbug VTOL Flying Simulator.” In Military Aircraft Systems Meeting. AIAA 1966-799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-799
• Barker, Jeffrey, and Gary Balas. 1999. “Flight Control of a Tailless Aircraft via Linear Parameter-Varying Techniques.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4133
• Barkmeyer, Daniel, Ryan Starkey, and Mark Lewis. 2005. “Inverse Waverider Design for Inward Turning Inlets.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-3915. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3915
• Barnes, David R., Frank A. Bill, Joseph B. Wilkerson, and David W. Taylor. 1979. “The Circulation Control Rotor Flight Demonstrator Test Program.” In Proceedings of the Vertical Flight Society Forum 35 - Washington, D.C. 1979. The Vertical Flight Society. https://doi.org/10.4050/vfs-f35-122
• Barnes, David, George McCoubrey, Douglas Kirkpatrick, and David Taylor. 1976. “Circulation Coontrol Rotor Flight Demonstrator.” In Proceedings of the Symposium on Rotor Technology, Essington, PA, August 1976. The Vertical Flight Society. https://doi.org/10.4050/sm_rotor_1976-2050
• Barnhart, David, Brian McKee, and Thomas Webber. 1988. “Flight Dynamics and Control Facility for Ground Based Flight Testingof Integrated KEW Technology.” In 4th Flight Test Conference. AIAA 1988-2148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2148
• Barnwell, R. 1974. “Transonic Flow about Lifting Wing-Body Combinations.” In 12th Aerospace Sciences Meeting. AIAA 1974-185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-185
• Barnwell, R. W. 1975. Analysis of Transonic Flow about Lifting Wing-Body Configurations. NASA-TR-R-440. NASA. https://ntrs.nasa.gov/citations/19750016609
• Barnwell, R. W. 1976. Approximate Method for Calculating Transonic Flow about Lifting Wing-Body Configurations. NASA-TR-R-452. NASA. https://ntrs.nasa.gov/citations/19760014063
• Baron, Judson R., and I. Efrat. 1979. An off Design Shock Capturing Finite Difference Approach for Caret Waverider Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada068819
• Barret, Chris. 1998. Lifting Body Flight Vehicles. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990103152
• Barret, Chris. 1999. “The Lifting Body Legacy: X-33.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-382. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-382
• Barret, Chris, and Chris Barret. 1997. “Design of Flight Control Augmentors and Resulting Flight Stability and Control Analysis.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-425. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-425
• Barry, Brian, Simon J. Parke, Nicholas W. Bown, Hansgeorg Riedel, and Martin Sitzmann. 1994. “The Flight Testing of Natural and Hybrid Laminar Flow Nacelles.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/94-gt-408
• Barsamian, V. 1965. “Application of Vector Plotting to Flight Flutter Testing.” In Flight Testing Conference. AIAA 1965-213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-213
• Bartasevicius, Julius, Pedro A. Fleig, Annina Metzner, and Mirko Hornung. 2022. “Design and Testing of an in-Flight Thrust Measurement System for a Pylon-Mounted Miniature Jet Engine.” In AIAA SCITECH 2022 Forum. AIAA 2022-1827. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1827
• Bartasevicius, Julius, and Mirko Hornung. 2023. “In-Flight Drag Measurement and Validation for a Medium-Sized UAV.” In AIAA SCITECH 2023 Forum. AIAA 2023-0372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0372
• Bartels, Robert. 2013. “Developing an Accurate CFD Based Gust Model for the Truss Braced Wing Aircraft.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3044. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3044
• Bartels, R., and R. Bartels. 1997. “Computation of Shock Buffet Onset for a Conventional and Supercritical Airfoil.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-833. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-833
• Bartels, Robert E., and Robert C. Scott. 2014. “Computed and Experimental Flutter/LCO Onset for the Boeing Truss-Braced Wing Wind Tunnel Model.” In 44th AIAA Fluid Dynamics Conference. AIAA 2014-2446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2446
• Bartels, Robert E., and Robert C. Scott. 2015. “Analysis of Limit Cycle Oscillation Data from the Aeroelastic Test of the SUGAR Truss-Braced Wing Model.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2720
• Bartels, Robert E., Bret Stanford, and Josiah M. Waite. 2019. “Performance Enhancement of the Flexible Transonic Truss-Braced Wing Aircraft Using Variable Camber Continuous Flaps.” In AIAA Scitech 2019 Forum. AIAA 2019-2035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2035
• Barth, James. n.d. “Mixing and Combustion Enhancement in a Mach 12 Shape-Transitioning Scramjet Engine.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2014.614
• Barthelemy, Robert. 1989a. “The National Aero-Space Plane Program.” In Maintainablity of Aerospace Systems Symposium. AIAA 1989-5053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5053
• Bartkowicz, Matt, Heath Johnson, Graham Candler, and Charles H. Campbell. 2009. Orbiter Boundary Layer Transition Stability Modeling at Flight Entry Conditions. JSC-CN-18484. Minnesota Univ. https://ntrs.nasa.gov/citations/20090026339
• Bartlett, D. W. 1975. Effects of Differential and Symmetrical Aileron Deflection on the Aerodynamic Characteristics of an NASA Supercritical-Wing Research Airplane Model. NASA-TM-X-3231. NASA. https://ntrs.nasa.gov/citations/19830002803
• Bartlett, D. W., and C. D. Harris. 1974. Effects of Wing Trailing-Edge Truncation on Aerodynamic Characteristics of a NASA Supercritical-Wing Research Airplane Model. NASA-TM-X-3024. NASA. https://ntrs.nasa.gov/citations/19830002751
• Bartlett, D. W., C. D. Harris, and T. C. Kelly. 1973. Wind-Tunnel Development of Underwing Leading-Edge Vortex Generators on a NASA Supercritical-Wing Research Airplane Configuration. NASA-TM-X-2808. NASA. https://ntrs.nasa.gov/citations/19830002762
• Bartlett, Dennis W., and Richard J. Re. 1972. Wind-Tunnel Investigation of Basic Aerodynamic Characteristics of a Supercritical-Wing Research Airplane Configuration. NASA-TM-X-2470. NASA. https://ntrs.nasa.gov/citations/19780016135
• Bartlett, D. W., and G. Sangiorgio. 1975. Effects of Landing Gear, Speed Brake and Protuberances on the Longitudinal Aerodynamic Characteristics of an NASA Supercritical-Wing Research Airplane Model. NASA-TM-X-72684. NASA. https://ntrs.nasa.gov/citations/19830002815
• Bartley, J. 1975. “Flight Flutter Testing of Multi-Jet Aircraft.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003021
• Bartolome Calvo, Javier, and Thino Eggers. 2011. “Application of a Coupling of Aerodynamics and Flight Dynamics to the SHEFEX I Flight Experiment.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2323. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2323
• Barz, Fynn. 2026. “Multifidelity Fluid-Structure Coupled Shape Optimization of a Hypersonic Glide Vehicle.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5022
• Basappa, K., and Ravindra Jategaonkar. 2004. “Evaluation of Recursive Methods for Aircraft Parameter Estimation.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5063
• Bassett, Zachary, Jing Pei, Adam Milne Slagle, and Bandu N. Pamadi. 2018. “Application of an Optimal Control Allocation Scheme with Structural Load and Aero Heating Feedback for a Morphing Inflatable Aerodynamic Decelerator.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0014
• Bathel, Brett, Paul Danehy, Craig Johansen, Stephen Jones, and Christopher Goyne. 2012. “Hypersonic Boundary Layer Measurements with Variable Blowing Rates Using Molecular Tagging Velocimetry.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-2886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2886
• Batill, S., R. Nelson, T. Mueller, and W. Wells. 1982. “Smoke Flow Visualization at Transonic and Supersonic Mach Numbers.” In 20th Aerospace Sciences Meeting. AIAA 1982-188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-188
• Batson, V., J. Hatfield, and N. Novack. 1981. “A Unique Integrated Flight Testing Facility for Advanced Control/display Research.” In 1st Flight Test Conference. AIAA 1981-2490. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2490
• Batterson, J., and V. Klein. 1983. “An Application of Parameter Identification to the Oscillatory Motionof an Airplane at High C(L).” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2067. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2067
• Batterson, J., and V. Klein. 1984. “A Preliminary Analysis of Flight Data from the AFTI/F-16 Airplane.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2085
• Batterson, James, and Vladislav Klein. 1987. “Partitioning of Flight Data for Aerodynamic Modeling of Aircraft at High Angles of Attack.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2621
• Battiston, Andrea, Rita Ponza, and Ernesto Benini. 2022. “Design of a Rear BLI Non-Axisymmetric Propulsor for a Transonic Flight Experiment.” In AIAA AVIATION 2022 Forum. AIAA 2022-3803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3803
• Baudoin, Michaël. 2006. “Absorption of Sonic Boom by Clouds.” In AIP Conference Proceedings, vol. 838. AIP. https://doi.org/10.1063/1.2210429
• Bauer, Jeff. 2007. “The NASA Dryden Flight Research Center Unmanned Aircraft System Service Capabilities.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20070024645
• Bauer, Jeffrey T. 2008. Small UAS Test Area at NASA’s Dryden Flight Research Center. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20080013589
• Bauer, Jeffrey E. 2009. UAS Related Activities at NASA’s Dryden Flight Research Center. DFRC-984. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090022802
• Bauer, F., P. Garabedian, and I. C. Chang. 2026. “Wave Drag and the Entropy Inequality in Transonic Flow.” In Computational Fluid Dynamics Techniques. CRC Press. https://doi.org/10.1201/9781003760528-2
• Baughman, Christopher, and Kevin Longeauay. 2015. Handling Qualities Evaluations of Unmanned Aircraft Systems. Defense Technical Information Center. https://doi.org/10.21236/ada616887
• Baumann, Ethan. 2006a. “Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-638
• Baumann, Ethan. 2006b. “X-43A Flight Controls.” In Graduate Aeronautic Labs. of Caltech (GALCIT) Aeronautic Seminar. https://ntrs.nasa.gov/citations/20060047627
• Baumann, Ethan, Joe Hernandez, and John Ruhf. 2013. “An Overview of NASA’s SubsoniC Research Aircraft Testbed (SCRAT).” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140008316
• Baumann, Ethan, Joseph Pahle, Mark Davis, and John White. 2008. “X-43A Flush Airdata Sensing System Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6570
• Baumgartner, Robert, and John Elvin. 1995. “Lifting Body: An Innovative RLV Concept.” In Space Programs and Technologies Conference. AIAA 1995-3531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3531
• Baurle, R., and D. Eklund. 2001. “Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4-6.5.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3299. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3299
• Bawa, Vidit, and Quentin Michalski. 2025. “An Experimental Framework for in-Flight Determination of Rocket Aerodynamic Drag.” In 2025 Regional Student Conferences. AIAA 2025-104785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-104785
• Bayard, D. S. 1992. “Statistical Plant Set Estimation Using Schroeder-Phased Multisinusoidal Input Design.” In In: 1992 American Control Conference, 11th, Chicago, IL, June 24-26, 1992, Proceedings. Vol. 4 (A93-22776 07-63). https://ntrs.nasa.gov/citations/19930038969
• Bayard, D. 1993. Statistical Plant Set Estimation Using Schroeder-Phased Multisinusoidal Input Design. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210004493
• “Bayesian Experimental Design.” 2014. In Bayesian Probability Theory. Cambridge University Press. https://doi.org/10.1017/cbo9781139565608.030
• Bazill, Dale G., and Gavin D. Jenney. 1970. Research on Flight Control Systems. Volume 3. Fly-By-Wire Techniques. Defense Technical Information Center. https://doi.org/10.21236/ad0879436
• Bazin, John, Travis Fields, and Andrew J. Smith. 2016. “Feasibility of in-Flight Quadrotor Individual Motor Thrust Measurements.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1760. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1760
• Beaird, H. 1967. “Flight Testing the Lear Model 23/24.” In Simulation and Support Conference. AIAA 1967-263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-263
• Bean, D., and B. Lee. 1994. “Correlation of Wind Tunnel and Flight Test Data for F/A-18 Vertical Tail Buffet.” In 12th Applied Aerodynamics Conference. AIAA 1994-1800. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1800
• Beasley, G. P. 1984. NASA Aircraft Controls Research, 1983. NASA-CP-2296. NASA. https://ntrs.nasa.gov/citations/19840012499
• Beaufrere, Henry. 1988. “Integrated Flight Control System Design for Fighter Aircraft Agility.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4503. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4503
• Becker, John V. 1940. Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel, Special Report. NACA-SR-137. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090014208
• Beeharry, Yogesh, and Raviduth Ramful. 2024. Applications of AI in UAVs Using in-Flight Parameters. Wiley. https://doi.org/10.1002/9781394230648.ch4
• Beeler, De E. 1961. Research-Airplane-Committee Report on Conference on the Progress of the X-15 Project. NASA-TM-X-57072. NASA. https://ntrs.nasa.gov/citations/19710070129
• Beeler, De E., Donald R. Bellman, and Edwin J. Saltzman. 1956. Flight Techniques for Determining Airplane Drag at High Mach Numbers. NACA-TN-3821. NASA. https://ntrs.nasa.gov/citations/19930084521
• Befus, Jack, E. Randel Nelson, David R. Ellis, and Joe Latas. 1987. “Flight Test Investigations of a Wing Designed for Natural Laminar Flow.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/871044
• Beh, H., G. Hofinger, and P. Huber. 2018. “Control Law Design and Flight Test Results of the Experimental Aircraft X-31A.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-15
• Beharie, M. M., J. O. Pedro, and L. Dala. 2015. “Design of a Quadrotor Flight Test Stand for System Identification.” Aeronautical Journal 119 (1214): 501–21. https://doi.org/10.1017/s0001924000010587
• Beheim, M. A. 1982. “NASA Research in Aircraft Propulsion.” In ASME. https://ntrs.nasa.gov/citations/19820005273
• Behzadpour, Forouzan. 2025. “Sustainable Flight National Partnership: The Transonic Truss-Braced Composite Wings of NASA/Boeing X-66A.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3106. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3106
• Beilman, John L. 1972. “An Integrated System of Airborne and Ground-Based Instrumentation for Flying Qualities Research with the X-22A Airplane.” In Proceedings of the Vertical Flight Society Forum 28 - Washington, D.C. 1972. The Vertical Flight Society. https://doi.org/10.4050/vfs-f28-031
• Beilman, J. 1983. “Indoctrination of Navy Test Pilots to Vectored Thrust Flight in the X-22A in-Flight Simulator.” In Flight Simulation Technologies Conference. AIAA 1983-1076. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1076
• Bekar, Ümit Can, Bilgehan Tanyeri, Ibrahim Enes Uslu, N. Arda Güngör, and Gökhan İnalhan. 2025. “Validation of an AI-Assisted Terrain Aided Navigation Algorithm Using Real-World Flight Test Instrumentation Data.” Preprint, . https://doi.org/10.20944/preprints202505.2427.v1
• Belák, Jan, and Martin Hromčík. 2023a. “Modular Propeller-Wing Interaction Modeling Method for Tilt-Rotor Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.4671509
• Belisle, Michael, Tyler Neale, Helen Reed, and William Saric. 2010. “Design of a Swept-Wing Laminar Flow Control Flight Experiment for Transonic Aircraft.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4381
• Belisle, Michael, Matthew Roberts, Thomas Williams, et al. 2012. “A Transonic Laminar-Flow Wing Glove Flight Experiment: Overview and Design Optimization.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2667. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2667
• Bell, James. 2007. “Transonic/Supersonic Wind Tunnel Testing of the NASA Orion Command Module.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1006
• “The Bell X-22A V/STOL, Variable Stability Research Airplane: Lessons Learned.” 1990. In Aircraft Design, Systems and Operations Conference. AIAA 1990-3207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3207
• Bellin, A. I., and A. Brooks. 1983. “Status Report: DARPA/NASA Convertible Turbofan/Turboshaft Engine Program.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/83-gt-196
• Bellman, Donald R. 1959. A Summary of Flight-Determined Transonic Lift and Drag Characteristics of Several Research Airplane Configurations. NASA-MEMO-3-3-59H. NASA. https://ntrs.nasa.gov/citations/19980228028
• Bellosta, Tommaso, Alberto Guardone, Giulio Gori, Pietro Congedo, and Olivier le Maitre. 2021. “Uncertainty Quantification for in-Flight Ice Accretion under Appendix-C and Appendix-O Conditions.” In AIAA Aviation 2021 Forum. AIAA 2021-2645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2645
• Belov, Vasilii, Viktor Bolotskiy, Vyacheslav Pisarev, Aleksandr Laznenko, Yulii Slepak, and Dmitrii Shinkarev. 2016. “Thermal Endurance Tests of the Cockpit Glass Canopy of Modern Supersonic Aircraft.” Science Bulletin of the Novosibirsk State Technical University, no. 3: 81–94. https://doi.org/10.17212/1814-1196-2016-3-81-94
• Belte, Daumants. 1987. “In-Flight Ice Accretion Characteristics of Rotor Blade Airfoil Sections.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-176
• Bement, L. J. 1978. Rotor Systems Research Aircraft (RSRA) Emergency Escape System. AHS 78-12. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19790034125
• Ben-Haim, Yakov. 2006. “Value of Information.” In Info-Gap Decision Theory. Elsevier. https://doi.org/10.1016/b978-012373552-2/50008-4
• Bender, R. 1969. “Saturn V/S-IC Stage Model and Flight Test Base Thermal Environment.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-318
• Bender, Anne, Russell Westphal, and Aaron Drake. 2010. “Application of the Boundary Layer Data System on a Laminar Flow Swept Wing Model in Flight.” In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2010-4360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4360
• Bender, Gary L., George M. Yamakawa, Michael K. Herbst, Patrick J. Sullivan, Robert D. Robbins, and Robert A. Williams. 1984. Airworthiness and Flight Characteristics Test (A&FC) of the CH-47D Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ada151380
• Benders, Sebastian, Simon Schopferer, and Arne Nawrath. 2020. “In-Flight Kinematic Model Parameter Estimation and Adaptive Path Planning for Unmanned Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-0135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0135
• Bendix Corp York Pa. 1963. Portable Aircraft Condition Evaluator Recorder. Defense Technical Information Center. https://doi.org/10.21236/ad0427770
• Benjamin, Leroy. 2023. “Aerodynamic Design of a Propeller-Heat Exchanger Setup for Distributed Electric Propulsion.” In AIAA AVIATION 2023 Forum. AIAA 2023-4432. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4432
• Bennett, Charles V. 1945. Stability and Control Characteristics of a Fighter Airplane in Inverted Flight Attitude as Determined by Model Tests. NACA-WR-L-15. NASA. https://ntrs.nasa.gov/citations/19930092555
• Bennett, George. 1991. “Automation of Prototype General Aviation Aircraft Development.” In CAD/CAM Robotics and Factories of the Future ’90. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-85838-3_47
• Bennett, R., and I. Abel. 1981. “Application of a Flight Test and Data Analysis Technique to Flutter of a Drone Aircraft.” In Dynamics Specialists Conference. AIAA 1981-652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-652
• Benoit, Tuur, Jon Verbeke, Rob De Roo, and Yves Lemmens. 2014. “Flight Dynamics Simulation with Integrated Electrical System Model for Pilot-in-the-Loop Testing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2056. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2056
• Bensassi, Khalil, Alejandro A. Laguna, Andrea Lani, and Nagi N. Mansour. 2016. “Modeling and Simulation of Radiative Compressible Flows in Aerodynamic Heating Arc-Jet Facility.” In International Conference on Computational Fluid Dynamics (ICCFD9). https://ntrs.nasa.gov/citations/20160003299
• Bensassi, Khalil, Andrea Lani, Olivier Chazot, and Patrick Rambaud. 2012. “Arbitrary Lagrangian Eulerian Simulation of a Moving Piston in Hypersonic Ground Test Facility.” In 42nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2012-3265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3265
• Benson, Geoffrey, Richard Bumstead, and A. J. Hutto. 1978. “Use of Helicopter Flight Simulation for Height-Velocity Test Predictions and Flight Test Risk Reduction.” In Proceedings of the Vertical Flight Society Forum 34 - Washington, D.C. 1978. The Vertical Flight Society. https://doi.org/10.4050/vfs-f34-037
• Benson, William W., Michael Fritzinger, Justin Costley, Brian Tibbetts, Brent Edwards, and Tim Kibbey. 2023. “Mars Ascent Vehicle Flight Test Mission Design, Analysis, and Instrumentation.” In 45th Rocky Mountain AAS Guidance, Navigation and Control Conference. https://ntrs.nasa.gov/citations/20230000476
• Benton, Mark. 1990. “Design Synthesis of Shuttle-Class Hypersonic SSTO Vehicle.” In 28th Aerospace Sciences Meeting. AIAA 1990-297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-297
• Beppu, G., and H. C. Curtiss Jr. 1966. An Analytical Study of Factors Influencing the Longitudinal Stability of Tilt-Wing VTOL Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0640945
• Beranek, R., M. F. Platzer, and L. Saunders. 1965. On Some Aerodynamic Aspects of the Panel Flutter Problem. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19660013044
• Berens, Thomas, and Norbert Bissinger. 1998. “Forebody Precompression Performance of Hypersonic Flight Test Vehicles.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1574
• Beresh, Steven. 2022. “Ground Testing of Unsteady Aerodynamic Environments in Hypersonic Flight.” In Proposed for presentation at the NASA / AFRL Workshop on High-Speed Test Techniques held November 30-December 1, 2022 in virtual,. US DOE. https://doi.org/10.2172/2006213
• Berg, John, Kuang-Ying Ting, Eli Livne, and Kristi A. Morgansen. 2025. “A Destabilize/Stabilize Approach to Experimental Active Flutter Suppression Technology Development.” In AIAA SCITECH 2025 Forum. AIAA 2025-1852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1852
• Berger, J. 1979. “A Comparison of Predictions Obtained from Wind Tunnel Tests and the Results from Cruising Flight: Airbus and Concorde.” In Flight Mechanics Panel Specialists Meeting on Performance Prediction Methods. https://ntrs.nasa.gov/citations/19790022965
• Berger, Karen T., Brian Paul Anderson, and Charles H. Campbell. 2014. “Space Shuttle Boundary Layer Transition Flight Experiment Ground Testing Overview.” In Thermal and Fluids Analysis Workshop (TFAWS). https://ntrs.nasa.gov/citations/20150013973
• Berger, Karen T., Brian P. Anderson, Charles H. Campbell, Michael T. Garske, Luis A. Saucedo, and Gerald R. Kinder. 2010. “Boundary Layer Transition Flight Experiment Overview and in-Situ Measurements.” In Thermal and Fluids Analysis Workshop 2010. https://ntrs.nasa.gov/citations/20100030598
• Berger, Karen T., Brian P. Anderson, Charles H. Campbell, et al. 2011. “Boundary Layer Transition Flight Experiment Overview.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110013660
• Berger, Karen T., Kevin E. Hollingsworth, Shelia A. Wright, and Shann J. Rufer. 2015. “NASA Langley Aerothermodynamics Laboratory: Hypersonic Testing Capabilities.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1337
• Berkowitz, A., C. Kyriss, and A. Martellucci. 1977. “Boundary Layer Transition Flight Test Observations.” In 15th Aerospace Sciences Meeting. AIAA 1977-125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-125
• Berman, Theodore. 1947. Spin and Recovery Characteristics of the Curtiss-Wright XP-87 Airplane. NACA-RM-L7F02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019623
• Berra, Lee, Christopher Campbell, and Taylor Wilson. 2017. “Developing a Flight Test Strategy for Adaptive Flight Control Laws.” In AIAA Flight Testing Conference. AIAA 2017-3649. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3649
• Berridge, Dennis C., Heather Kostak, Gregory McKiernan, Bradley M. Wheaton, Thomas D. Wolf, and Steven P. Schneider. 2019. “Hypersonic Ground Tests with High-Frequency Instrumentation in Support of the Boundary Layer Transition (BOLT) Flight Experiment.” In AIAA Scitech 2019 Forum. AIAA 2019-0090. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0090
• Berridge, Dennis C., Gregory McKiernan, Tim P. Wadhams, et al. 2018. “Hypersonic Ground Tests in Support of the Boundary Layer Transition (BOLT) Flight Experiment.” In 2018 Fluid Dynamics Conference. AIAA 2018-2893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2893
• Berry, Scott A. 1967. Re-Entry-F Turbulent Heating Experiment: Langley Research Center. 19690018169. Langley Research Center. https://ntrs.nasa.gov/citations/20250007312
• Berry, Scott A., Aaron H. Auslender, Authur D. Dilley, and John F. Calleja. 2000c. Hypersonic Boundary-Layer Trip Development for Hyper-X. AIAA Paper 2000-4012. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000080347
• Berry, Scott A., Karen T. Berger, Thomas J. Horvath, and William A. Wood. 2016. “Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160010109
• Berry, Scott, Kamran Daryabeigi, Kathryn Wurster, and Robert Bittner. 2008a. “Boundary Layer Transition on X-43A.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080023459
• Berry, Scott A., Michael DiFulvio, and Matthew K. Kowalkowski. 2000a. Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 20-Inch Mach 6 Air Tunnel. NASA/TM-2000-210316. NASA. https://ntrs.nasa.gov/citations/20000120037
• Berry, Scott A., Michael DiFulvio, and Matthew K. Kowalkowski. 2000b. Forced Boundary-Layer Transition on X-43 (Hyper-X) in NASA LaRC 31-Inch Mach 10 Air Tunnel. NASA/TM-2000-210315. NASA. https://ntrs.nasa.gov/citations/20000120047
• Berry, D., and G. Gilyard. 1973. “Airframe/propulsion System Interactions: An Important Factor in Supersonic Aircraft Flight Control.” In Guidance and Control Conference. AIAA 1973-831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-831
• Berry, Scott A., Thomas J. Horvath, Amy M. Cassady, Benjamin S. Kirk, K. C. Wang, and Andrew J. Hyatt. 2006a. “Boundary Layer Transition Results from STS-114.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20060022549
• Berry, Scott A., Thomas J. Horvath, Francis A. Greene, Gerald R. Kinder, and K. C. Wang. 2006b. “Overview of Boundary Layer Transition Research in Support of Orbiter Return to Flight.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20060022550
• Berry, Scott, Thomas Horvath, Brian Hollis, H. Hamilton II, and Richard Thompson. 1999. “X-33 Hypersonic Boundary Layer Transition.” In 33rd Thermophysics Conference. AIAA 1999-3560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3560
• Berry, Scott A., Thomas J. Horvath Jr., Richard Schwartz, Martin Ross, Brian Anderson, and Charles H. Campbell. 2008b. “Infrared Imaging of Boundary Layer Transition Flight Experiments.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080023461
• Berry, Scott, Roger Kimmel, and Eli Reshotko. 2011. “Recommendations for Hypersonic Boundary Layer Transition Flight Testing.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3415
• Berry, Scott A., Rudolph A. King, Michael A. Kegerise, et al. 2010. “Orbiter Boundary Layer Transition Prediction Tool Enhancements.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100003043
• Berry, Victor, David Lindsay, Tom Parham Jr., David Popelka, and Donald J. Baker. 1995. “Results of an Aeroelastic Tailoring Study for a Composite Tiltrotor Wing.” In Proceedings of the Vertical Flight Society Forum 51 - Ft. Worth, TX 1995. The Vertical Flight Society. https://doi.org/10.4050/vfs-f51-2020
• Berry, D. T., D. L. Mallick, and G. B. Gilyard. 1976. “Handling Qualities Aspects of NASA YF-12 Flight Experience.” In Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011063
• Berry, Scott, Norman Merski, and Robert Blanchard. 2002a. “Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparison to Flight.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4701
• Berry, Scott A., N. Ronald Merski, and Robert C. Blanchard. 2002b. “Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparisons to Flight.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030005486
• Bertelrud, A. 1980. “Local Skin Friction and Static Pressure on a Swept Wing in Flight.” In 11th Aerodynamic Testing Conference. AIAA 1980-423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-423
• Bertelrud, A. 1981a. “Static-Pressure and Skin-Friction Distributions on a Swept Wing in Flight at Mach Numbers from 0.27 to 0.9.” In 14th Fluid and Plasma Dynamics Conference. AIAA 1981-1216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1216
• Bertelrud, A. 1981b. “Steady and Unsteady Effects on the Aerodynamic Flow on a Swept Wing in Flight.” In 1st Flight Test Conference. AIAA 1981-2418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2418
• Bertelrud, Arild, Jerry Budd, David Sollberger, Rex Churchward, Larry Smilg, and Jim Stowers. 1999. “A Hypersonic Flight Test to Document Laminar/turbulent Transition.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4849
• Bertelrud, Arild, Geva delaTova, Philip J. Hamory, et al. 2000. Pegasus(Registered Trademark) Wing-Glove Experiment to Document Hypersonic Crossflow Transition: Measurement System and Selected Flight Results. NASA/TM-2000-209016. NASA. https://ntrs.nasa.gov/citations/20000011504
• Bertelrud, Arild, and Sharon Graves. 1994. “Analysis of Flight Flow Characteristics in the Leading Edge Region of Swept Wings at Subsonic and Transonic Speeds.” In Biennial Flight Test Conference. AIAA 1994-2152. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2152
• Bertelrud, Arild, Paul Kolodziej, Gregk. Noffz, and Afzal Godil. 1992. “Plans for in-Flight Measurement of Hypersonic Crossflow Transition on the Pegasus Launch Vehicle.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4104
• Berton, Benoit, Jean-Claude Courty, Mariana Kok, Edmond Tobin, and Trevor M. Young. 2014. “Evaluation of Functional Coatings for Laminar Flow Applications on Future Business Jets through Ground and Flight Testing.” In AIAA Flight Testing Conference. AIAA 2014-2578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2578
• “Betsy’s Legacies: Other Supersonic Planes to Lifting Bodies.” 2017. In America’s First Rocket Company: Reaction Motors, Inc.. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624104428.0117.0138
• Bevacqoa, Tim, Tony Adams, Zhu. J. Jim, and P. Prabhakara Rao. 2004. A Flight Control Approach for Small Reentry Vehicles. Ohio Univ. https://ntrs.nasa.gov/citations/20040112033
• Bever, Glenn A. 1981. “The Development and Use of a Computer-Interactive Data Acquisition and Display System in a Flight Environment.” In 1st Flight Test Conference. https://ntrs.nasa.gov/citations/19820030411
• Bever, Glenn A. 1984. The Development of an Airborne Instrumentation Computer System for Flight Test. NASA-TM-86036. NASA. https://ntrs.nasa.gov/citations/19840012453
• Bever, Glenn A. 1986. Airborne Instrumentation Computer System. ARC-11602. Ames Research Center. https://ntrs.nasa.gov/citations/19860000323
• Bever, Glenn A. 1991a. Digital Signal Conditioning for Flight Test Instrumentation. NASA-TM-101739. NASA. https://ntrs.nasa.gov/citations/19910011822
• Bever, Glenn A. 1991b. Digital Signal Conditioning for Flight Test, Volume 19 [Le Traitement Du Signal Numérique Pour Les Essais En Vol]. AGARD-AG-160-VOL-19. Ames Research Center. https://ntrs.nasa.gov/citations/19910017118
• Bever, Glenn. 1992. “The Development of an Airborne Information Management System for Flight Test.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4113
• Beyers, Martin, Lars Ericsson, Lars Ericsson, and Martin Beyers. 1997. “Extraction of Subscale Free-Flight Aerodynamics from Rotary Tests of Combat Aircraft.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-730
• Bezdek, W., and R. Galloway. 1982. “Digital Test Pilot Concept.” In 20th Aerospace Sciences Meeting. AIAA 1982-259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-259
• Bezerra, Italo Sabino Arrais, Sandi Itamar Schafer de Souza, and Paulo Gilberto de Paula Toro. 2024. “Influence of Flight Speed Fluctuations on the Mixed-Based Intake System Performance of a Scramjet Demonstrator.” Preprint, . https://doi.org/10.2139/ssrn.4919975
• Bhagwandin, Vishal, and Jubaraj Sahu. 2023. Toward High-Enthalpy Simulations for Hypersonic Applications: The Double Cone Test Case. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1216596
• Bhamidipati, Keerti, Natalie Spivey, Scott Stebbins, Samson Truong, and Benjamin Park. 2024. “X-57 Cruise Motor GVT Using Fixed-Base Correction Technique.” In International Modal Analysis Conference (IMAC) XLII. https://ntrs.nasa.gov/citations/20230014021
• Bhandari, Rajan, and Imon Chakraborty. 2026. “Optimization of a Hybrid-Electric Multi-Tilt-Rotor Aircraft with Conventional and Vertical Takeoff and Landing Capabilities.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0206
• Bhatia, Manav, Ohad Gur, Rakesh Kapania, William Mason, Joseph Schetz, and Raphael Haftka. 2010. “Progress towards Multidisciplinary Design Optimization of Truss Braced Wing Aircraft with Flutter Constraints.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9077
• Bhattarai, Mahesh, Nabin Bhandari, Roshani Sah, and Ashish Karki. 2026. “Aerodynamic and Stability Analysis of a VTOL Blended-Wing Body UAS with Experimental Flight Testing.” Unmanned Systems: 1–13. https://doi.org/10.1142/s2301385027500713
• Bi, Zhixian, Nanji Zhu, Qing Shen, and Zhanfeng Zhang. 2007. “Measurement on Transition of Hypersonic Boundary Layer over Circular Cone.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6728. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6728
• Biber, Kasim. 2016. “Flight Dynamics Modeling of a Propeller-Driven Cargo Airplane.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0806. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0806
• Biber, Kasim, and Carl Tilmann. 2003. “Supercritical Airfoil Design for Future HALE Concepts.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1095. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1095
• Biblarz, O., B. Pomerantz, and S. Lindsey. 1998. “Transonic Missile Drag Area-Rule and Afterbody-Role Verification with CFD.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-527
• Bielawa, R. L. 1976. Aeroelastic Analysis for Helicopter Rotor Blades with Time-Variable, Non-Linear Structural Twist and Multiple Structural Redundancy: Mathematical Derivation and Program User’s Manual. NASA-CR-2638. NASA. https://ntrs.nasa.gov/citations/19770003613
• Bier, Niko, Stefan Keye, David Rohlmann, and Silke von Deetzen. 2013. “Design of a Wind Tunnel Model for Maximum Lift Predictions Based on Flight Test Data.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2930
• Biggi, Massimo, Pierre Abdel Nour, and Giorgio Vicenzotti. 2024. “Next Generation Civil Tiltrotor Technology Demonstrator Program: Towards Flight Test.” In AIAA SCITECH 2024 Forum. AIAA 2024-1491. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1491
• Bigler, R. 1986. “AV-8B High Angle of Attack/departure Resistance System Flight Test Program.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9729. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9729
• Bihrle, W., Jr. 1970. “The Influence of the Static and Dynamic Aerodynamic Characteristics on the Spinning Motion of Aircraft.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-946
• Bilstein, Roger E. 1989b. Orders of Magnitude: A History of the NACA and NASA, 1915-1990. NASA-SP-4406. NASA. https://ntrs.nasa.gov/citations/19890017434
• Bilstein, Roger E., and Lane E. Wallace. 1998. “Flights of Discovery: Fifty Years at the NASA Dryden Flight Research Center.” Technology and Culture 39 (3): 588. https://doi.org/10.2307/1215936
• Bingaman, J. 2012. “Unmanned Aircraft and the Applicability of Military Flying Qualities Standards.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4415
• Binion, T., Jr. 1969. “A V/STOL Wind-Tunnel Wall Interference Study.” In 7th Aerospace Sciences Meeting. AIAA 1969-171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-171
• Binion, T. W., Jr. 1970. Description and Calibration of the AEDC Low Speed Wind Tunnel (V/STOL). Defense Technical Information Center. https://doi.org/10.21236/ad0877999
• Binion, T. W., Jr. 1974. An Investigation of Three-Dimensional Wall Interference in a Variable Porosity Transonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0787658
• Binion, T., Jr., and C. Lo. 1972. “Application of Wall Corrections to Transonic Wind Tunnel Data.” In 7th Aerodynamic Testing Conference. AIAA 1972-1009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1009
• Biot, M. A. 1949. “Transonic Drag of an Accelerated Body.” Quarterly of Applied Mathematics 7 (1): 101–5. https://doi.org/10.1090/qam/28157
• Birkeland, Paul, and Robert Meuser. 1999. “Thinking through Reusable Launch Vehicle Licensing.” In Space Technology Conference and Exposition. AIAA 1999-4463. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4463
• Birrer, M., and C. Stemmer. 2012. “Chemical Nonequilibrium Effects in the Wake of an Obstacle in Hypersonic Boundary-Layer Flows.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203267
• Biswell, Brian, and Jordi Puig-Suari. 1996. “Lifting Body Effects on Equilibrium Orientation of Tethers in the Atmosphere.” In Astrodynamics Conference. AIAA 1996-3598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3598
• Bjarke, Lisa J., and L. J. Ehernberger. 1989. “An in-Flight Technique for Wind Measurement in Support of the Space Shuttle Program.” In Society of Flight Test Engineers 20th Annual Symposium. https://ntrs.nasa.gov/citations/19900004908
• Black, R. 1968. “High-Speed Store Separation: Correlation between Wind-Tunnel and Flight-Test Data.” In 3rd Aerodynamics Testing Conference. AIAA 1968-361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-361
• Blackburn, W. E., and A. D. Rita. 1968. Flight Research Program to Evaluate Methods of Improving Compound Helicopter Maneuver Capability. Defense Technical Information Center. https://doi.org/10.21236/ad0670942
• Blackwell, R., and T. Millott. 2008. “Dynamics Design Characteristics of the Sikorsky X2 Technology™ Demonstrator Aircraft.” In Proceedings of the Vertical Flight Society AHS 64th Annual Forum, Montréal, Québec, April 29-May 1, 2008. The Vertical Flight Society. https://doi.org/10.4050/vfs-f64-000174
• Blackwell, J. A., Jr. 1969. Preliminary Study of Effects of Reynolds Number and Boundary-Layer Transition Location on Shock-Induced Separation. NASA-TN-D-5003. NASA. https://ntrs.nasa.gov/citations/19690006789
• Blackwell, J. A., Jr. 1978. Scale Effects on Supercritical Airfoils. Lockheed-Georgia Co. https://ntrs.nasa.gov/citations/19790036097
• Blackwell Jr. and R. H. K. C. Frederickson. 1981. Wind Tunnel Evaluation of Aeroelastically Conformable Rotors. Defense Technical Information Center. https://doi.org/10.21236/ada096129
• Blaha, B. 1969. “Flight and Wind Tunnel Investigation of Installation Effects on Supersonic Cruise Exhaust Nozzles at Transonic Speeds.” In 5th Propulsion Joint Specialist. AIAA 1969-427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-427
• Blake, William. 2002. Drag Reduction from Formation Flight. Flying Aircraft in Bird-Like Formations Could Significantly Increase Range. Defense Technical Information Center. https://doi.org/10.21236/ada401264
• Blake, B., and K. Lunn. 1980. “Helicopter Stability and Control Test Methodology.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1610
• Blanchard, Willard S. 1953. Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model. NACA-RM-SL53E11a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023638
• Blanchard, R. 1989. “Rarefied-Flow Aerodynamics Measurement Experiment on the Aeroassist Flight Experiment.” In 27th Aerospace Sciences Meeting. AIAA 1989-636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-636
• Blanchard, Robert C. 1990. “A Flight Experiment to Measure Rarefied-Flow Aerodynamics.” In ICAS Congress. https://ntrs.nasa.gov/citations/19910039780
• Blanchard, R., W. Phillips, G. Kelly, and J. Findlay. 1980. “Comparisons of Subsonic Drag Estimates Derived from Pioneer Venus Probes Flight Data with Wind-Tunnel Results.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1578
• Blanchard, Antoine, and Themistoklis Sapsis. 2021. “Output-Weighted Optimal Sampling for Bayesian Experimental Design and Uncertainty Quantification.” SIAM/ASA Journal on Uncertainty Quantification 9 (2): 564–92. https://doi.org/10.1137/20m1347486
• Blanchard, Robert C., Richard G. Wilmoth, Christopher E. Glass, et al. 2001a. Infrared Sensing Aeroheating Flight Experiement: STS-96 Flight Results. AIAA Paper 2001-0352. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010018568
• Blanchard, Robert C., Richard G. Wilmoth, Christopher E. Glass, et al. 2001b. Infrared Sensing Aeroheating Flight Experiment: STS-96 Flight Results. AIAA Paper 2001-0352. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010003921
• Blanchard, Robert, Richard Wilmoth, and Gerald LeBeau. 1996. “Orbiter Aerodynamic Acceleration Flight Measurements in the Rarefied Flow Transition Regime.” In 14th Applied Aerodynamics Conference. AIAA 1996-2467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2467
• Bland, William M., Jr., and Katherine A. Collie. 1961. Free-Flight Aerodynamic-Heating Data to Mach Number 10.4 for a Modified Von Karman Nose Shape. NASA-TN-D-889. NASA. https://ntrs.nasa.gov/citations/19980228066
• Bland, W. M., Jr., R. Kolenkiewicz, and A. G. Swanson. 1958. Free-Flight Aerodynamic-Heating Data at Mach Numbers up to 10.9 on a Flat-Faced Cylinder. NACA-RM-L57K29. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19630003999
• Blankson, Isaiah, and Jon Pyle. 1993. “NASA’s Hypersonic Flight Research Program.” In 31st Aerospace Sciences Meeting. AIAA 1993-308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-308
• Bleimeyer, M. 1981. “Fiber Optics in Flight Test Instrumentation Applications.” In 1st Flight Test Conference. AIAA 1981-2515. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2515
• Blevins, Aaron T., Aaron McKinnis, Jeffrey Xu, and Shawn S. Keshmiri. 2022. “Flight Test Validation of Real-Time UAS Mission Planning Autonomy and Optimal Path Planning for Flight Line Surveys.” In AIAA SCITECH 2022 Forum. AIAA 2022-2292. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2292
• Bliss, D. B. 1980. Wind Tunnel Wall Interference. Defense Technical Information Center. https://doi.org/10.21236/ada093301
• Blocker, Wayne, and David Ruebush. 2005. “X-43A Stage Separation System: A Flight Data Evaluation.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3335
• Blue, Paul, Gary Balas, Paul Blue, and Gary Balas. 1997. “Linear Parameter-Varying Control for Active Flutter Suppression.” In Guidance, Navigation, and Control Conference. AIAA 1997-3640. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3640
• Blue, Lisa, and Kevin Crawford. 1997. Development of the Flight Test Telemetry System for Clipper Graham: A New Way to Do Business. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990098445
• Bobbitt, P. 1980. “Modern Fluid Dynamics of Subsonic and Transonic Flight.” In International Meeting and Technical Display on Global Technology 2000. AIAA 1980-861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-861
• Bobbitt, Percy J., William D. Harvey, Charles D. Harris, and Cuyler W. Brooks. 1992. “The Langley 8-Ft Transonic Pressure Tunnel Laminar-Flow-Control Experiment: Background and Accomplishments.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_8
• Bock, H. G., S. Körkel, E. Kostina, and J. P. Schlöder. n.d. “Robustness Aspects in Parameter Estimation, Optimal Design of Experiments and Optimal Control.” In Reactive Flows, Diffusion and Transport. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-28396-6_6
• Bock, C., Jr. 1976. “B-1 Flight Test: Progress Report.” In Aircraft Systems and Technology Meeting. AIAA 1976-886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-886
• Boehm, Ben, Pete Flick, Brian Sanders, Chris Pettit, Eric Reichenbach, and Scott Zillmer. 2001. “Static Aeroelastic Response Predictions of the Active Aeroelastic Wing (AAW) Flight Research Vehicle.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1372
• Boeing Co Morton Pa Vertol Div. 1961. Flight Test Evaluation of an Improved External Cargo Sling System for h- 34 Helicopters. Defense Technical Information Center. https://doi.org/10.21236/ad0256426
• Boeing Co Renton Wa Airplane Div. 1964. Commercial Supersonic Transport Program. Phase 2-A. Comprehensive Report. Volume 7-A. Sonic Boom and Noise. Defense Technical Information Center. https://doi.org/10.21236/ad0804043
• Boeing Co Seattle Wa. 1963. Dyna Soar Testing for the Boeing Company. Defense Technical Information Center. https://doi.org/10.21236/ad0336996
• “Boeing Flies Blended Wing Body Research Aircraft.” 2008. Aircraft Engineering and Aerospace Technology 80 (1). https://doi.org/10.1108/aeat.2008.12780aaf.003
• “Boeing to Use X-43A Flight Test Results for Future Hypersonic Applications.” 2005. Aircraft Engineering and Aerospace Technology 77 (2). https://doi.org/10.1108/aeat.2005.12777baf.006
• Boeing Vertol Co Philadelphia Pa. 1974. CH-47 Helicopter: Submittal of Flight Test Results on Triple Cargo Hook System (SRD 84R2). Defense Technical Information Center. https://doi.org/10.21236/ada955522
• Bogar, Thomas, Michal Bangham, Robert Forward, and Mark Lewis. 1999. “Hypersonic Airplane Space Tether Orbital Launch (HASTOL) System: Interim Study Results.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4802
• Bogdonoff, Seymour M. 1999. Hypersonic Flight Vehicles: Perspective and Prognosis,. Defense Technical Information Center. https://doi.org/10.21236/ada370547
• Bogue, Rodney. 1992. “Recent Flight-Test Results of Optical Airdata Techniques.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4086
• Bogue, Rodney, and Peter Erbland. 1992. “Perspective on the National Aero-Space Plane Program Instrumentationdevelopment.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5086
• Bohlmann, Jonathan, Michael Love, Daniel Barker, William Rogers, and Beth Paul. 1992. “Application of Analytical and Design Tools for Fighter Wing Aeroelastic Tailoring.” In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2373
• Bohlmann, Jonathan, Terrence Weisshaar, and Clinton Eckstrom. 1988. “Aeroelastic Tailoring for Oblique Wing Lateral Trim.” In 29th Structures, Structural Dynamics and Materials Conference. AIAA 1988-2263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2263
• Bohn-Meyer, Marta, Stephen Kilp, Peggy Chun, and Masashi Mizukami. 2004. “Doing Systems Engineering without Thinking about It at NASA Dryden Flight Research Center.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20050170640
• Boissinot, Antoine, and Mojtaba Kheiri. 2023. “Aeroelastic Behaviour of Urban Air Mobility Aircraft with Distributed Electric Propulsion Subjected to Urban Wind Gusts.” In Progress in Canadian Mechanical Engineering. Volume 6. Université de Sherbrooke. Faculté de génie. https://doi.org/10.17118/11143/20948
• Bokser, V. D., and G. G. Sudakov. 2008. “Aerodynamic Drag of Bodies in Transonic Flow. Theory and Applications to Computational Aerodynamics.” Fluid Dynamics 43 (4): 613–24. https://doi.org/10.1134/s0015462808040145
• Bolender, Michael A., and David B. Doman. 2005. Flight Path Angle Dynamics of Air-Breathing Hypersonic Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada444974
• Boles, John, and Ryan Milligan. 2013. Technology for Sustained Supersonic Combustion Task Order 0006: Scramjet Research with Flight-Like Inflow Conditions. Defense Technical Information Center. https://doi.org/10.21236/ada586382
• Bolt, M. 1981. “Flight Test Data Processing for Fleet Ballistic Missile Programs.” In 1st Flight Test Conference. AIAA 1981-2394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2394
• Bond, Aleck C., Dorothy B. Lee, and Charles B. Rumsey. 1958. Heat Transfer Measured in Free Flight on a Slightly Blunted 25 Deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89. NACA-RM-L58G21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19630010649
• Bond, Aleck C., and Andrew G. Swanson. 1953. Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance Characteristics of the North American MX-770 (X-10) Missile at Mach Numbers from 0.80 to 1.70. NACA-RM-SL53D10A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029470
• Bonelli, Francesco, Luigi Cutrone, Raffaele Votta, Annarita Viggiano, and Vinicio Magi. 2011. “Preliminary Design of a Hypersonic Air-Breathing Vehicle.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2319
• Bonin, Jannis, Daniel Kliche, and Christian Mundt. 2017. “Simulations of Stagnation Point Radiative Heating Rates and Spectral Analysis of Entry Vehicles.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1611. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1611
• Bonnema, Kenneth L., and William A. Lokos. 1989. “AFTI/F-111 Mission Adaptive Wing Flight Test Instrumentation Overview.” In International Instrumentation Symposium. https://ntrs.nasa.gov/citations/19910035087
• Bonnema, Kenneth, and Stephen Smith. 1988. “AFTI/F-111 Mission Adaptive Wing Flight Research Program.” In 4th Flight Test Conference. AIAA 1988-2118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2118
• Boonjue, S., C. Roseberry, and D. Wilson. 1996. “Results from Initial Operation of a Continuous-Flow, Arc-Heated Hypersonic Propulsion Test Facility.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4505
• Bordogna, Marco Tito, Terence Macquart, Dimitri Bettebghor, and Roeland De Breuker. 2016. “Aeroelastic Optimization of Variable Stiffness Composite Wing with Blending Constraints.” In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2016-4122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4122
• Borek, R. W., and A. Pool. 1994. Basic Principles of Flight Test Instrumentation Engineering, Volume 1, Issue 2. ISBN: 92-835-0731-2. Dryden Flight Research Center. https://ntrs.nasa.gov/citations/19940029434
• Borek, R. W., and R. B. Richardson. 1969. Flight and Laboratory Tests of an ‘‘L-Band’’ Telemetry RF System. NASA. https://ntrs.nasa.gov/citations/19690058007
• Borer, Nicholas K., Trong Bui, and Andrew Smith. 2023. “Cruise Propulsion System Thermal Analysis for NASA’s X-57 “Maxwell” Mod II Configuration.” In AIAA AVIATION 2023 Forum. AIAA 2023-4273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4273
• Borer, Nicholas K., David E. Cox, and Ryan D. Wallace. 2019. “Flight Performance Maneuver Planning for NASA’s X-57 “Maxwell” Flight Demonstrator: Part 1: Power-Off Glides.” In AIAA Aviation 2019 Forum. AIAA 2019-2855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2855
• Borer, Nicholas K., Michael D. Patterson, Jeffrey K. Viken, et al. 2016. “Design and Performance of the NASA SCEPTOR Distributed Electric Propulsion Flight Demonstrator.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160010157
• Borer, Nicholas K., James R. Reynolds, and Ryan D. Wallace. 2024. “Flight Performance Maneuver Planning for NASA’s X-57 “Maxwell” Flight Demonstrator – Part 2: Power-On Effects.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4133
• Borg, Dave. 2001. “Flight Testing of the CF34-8C Engine on the GE B747 Flying Test Bed.” In 1st AIAA, Aircraft, Technology Integration, and Operations Forum. AIAA 2001-5271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-5271
• Borg, Matthew P., David W. Adamczak, Adam J. Culler, and Michael D. Kurtz. 2025b. “HIFLIER Hypersonic Flight Experiment: Design, Analysis, and Ground Test.” In AIAA SCITECH 2025 Forum. AIAA 2025-0733. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0733
• Borg, Matthew P., David W. Adamczak, and Matthew W. Tufts. 2025a. “HIFLIER Hypersonic Flight Experiment: Ascent Results.” In AIAA SCITECH 2025 Forum. AIAA 2025-0734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0734
• Bornemisza, Tibor. 1990. “Ceramic Small Gas Turbine Technology Demonstrator.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-306
• Borrok, Martin J., and David C. Rider. 1970. “Results of the ATA CAS Flight Test Program.” Navigation 17 (3): 278–89. https://doi.org/10.1002/j.2161-4296.1970.tb00050.x
• Borst, Henry. 1990. “The Curtiss-Wright X-19 Experimental Aircraft: Lessons Learned.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3206. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3206
• Boschetti, Pedro, Elsa Cárdenas, and Nelson Garcia. 2004. “Experimental Aerodynamic Study of UAV Wind Tunnel Model for Low Reynolds Number.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-4969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4969
• Bosmajian, Neil. 2000. “Development of a Hypersonic Test Facility: A National Asset Utilizing Magnetic Levitation.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-160
• Bosmajian, Neil. 2002. “Magnetic Levitation and Electromagnetic Propulsion Technology Development in Support of Hypersonic Ground Test Facilities (Invited).” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3036. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3036
• Boswinkle, R. W., Jr., and S. L. Smith III. 1958. Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane. NACA-RM-L58A15. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19660027826
• Bosworth, John T. 2006. “NASA Dryden Status.” In SAE Aerospace Control and Guidance Systems Conference. https://ntrs.nasa.gov/citations/20060052412
• Bosworth, John. 2008. “Flight Results of the NF-15B Intelligent Flight Control System (IFCS) Aircraft with Adaptation to a Longitudinally Destabilized Plant.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6985. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6985
• Bosworth, John T. 2010. “NASA Dryden Status.” In NASA Dryden Status: Aerospace Control and Guidance. https://ntrs.nasa.gov/citations/20110011495
• Bosworth, John T., and Timothy H. Cox. 1989. A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft. NASA-TM-4142. NASA. https://ntrs.nasa.gov/citations/19900002437
• Bosworth, John T., and P. C. Stoliker. 1996. The X-31A Quasi-Tailless Flight Test Results. NASA-TP-3624. NASA. https://ntrs.nasa.gov/citations/19960029101
• Bosworth, J. T., and J. C. West. 1986. Real-Time Open-Loop Frequency Response Analysis of Flight Test Data. AIAA PAPER 86-9738. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19860047346
• Bottasso, Carlo, and Pierluigi Montinari. 2013. “Rotorcraft Flight Envelope Protection by Model Predictive Control.” In Proceedings of the Vertical Flight Society 69th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/vfs-f69-0282
• Bouchez, Marc. 2001. “Dual-Mode Ramjet Thermo-Mechanical Design and Associated Performance.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1918. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1918
• Boudreau, J. 1976. “Integrated Flight Control System Design for CCV.” In Aircraft Systems and Technology Meeting. AIAA 1976-941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-941
• Boudreau, A. H. 1978. Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones Using Distributed Roughness and Spherical-Type Tripping Devices at Hypersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada052034
• Boudreau, A. H. 1979. A Correlation of Artificially Induced Boundary-Layer Transition Data from Blunt Slender Cones at Hypersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada070446
• Boudreau, A., V. Smith III, and D. Daniel. 1993. “Developmental Testing of Ramjet/scramjet Propulsion Systems.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5121
• Bouslog, S. A., M. Y. An, L. N. Hartmann, and S. M. Derry. 1991. Review of Boundary Layer Transition Flight Data on the Space Shuttle Orbiter. AIAA PAPER 91-0741. Lockheed Engineering and Sciences Co. https://ntrs.nasa.gov/citations/19910034820
• Bouslog, S., J. Mammano, and B. Strauss. 1998. Thermal Management Design for the X-33 Lifting Body. NASA/CR-1998-208247. NASA. https://ntrs.nasa.gov/citations/19980200836
• Bouwer, Scott, and Kevin Ignatuk. 2025a. “SB>1 DEFIANT JMR Technology Demonstrator Aircraft Main Rotor Gearbox Technology Insertions & Teardown Results.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-229
• Bouwer, Scott, and Kevin Ignatuk. 2025b. “SBb1 DEFIANT JMR Technology Demonstrator Aircraft Main Rotor Gearbox Technology Insertions & Teardown Results.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0229
• Bouwer, Scott, and Eric Kaiser. 2019. “Design and Development of the Main Rotor Gearbox for the Sikorsky Boeing SB>1 DEFIANT JMR Technology Demonstrator Aircraft.” In Proceedings of the Vertical Flight Society 75th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0075-2019-14675
• Bowcutt, Kevin. 1992. “Hypersonic Aircraft Optimization Including Aerodynamic, Propulsion, and Trim Effects.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5055. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5055
• Bowden, Thomas H., and Gerald A. Shockey. 1970. A Wind-Tunnel Investigation of the Aerodynamic Environment of a Full Scale Helicopter Rotor in Forward Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0875744
• Bowers, D. A. 1963. Leading Edges Development: Dyna Soar. Defense Technical Information Center. https://doi.org/10.21236/ad0409321
• Bowers, D. 1980. “Propulsive Aerodynamics of an Advanced Nozzle/forward Swept Wing Aircraft Configuration.” In 16th Joint Propulsion Conference. AIAA 1980-1158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1158
• Bowers, Al, Jennifer Hansen Cole, and Cam Martin. 2007. “Gliding Experiments of the Wright Brothers: The Wrights and Flight Research 1899-1908.” In Gliding Experiments of the Wright Brothers: The Wrights and Flight Research 1899-1908. https://ntrs.nasa.gov/citations/20080000869
• Bowers, Al, Jennifer Hansen Cole, and Cam Martin. 2008. Gliding Experiments of the Wright Brothers: The Wrights and Flight Research 1899-1908. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20080008875
• Bowers, Albion H., Jennifer Hansen Cole, and John Campbell Martin. 2011. “Gliding Experiments of the Wright Brothers: The Wrights and Flight Research 1899-1908.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110023705
• Bowers, A. H., and D. R. Sandlin. 1984. A Comparison of Computer-Generated Lift and Drag Polars for a Wortmann Airfoil to Flight and Wind Tunnel Results. NASA-CR-176963. NASA. https://ntrs.nasa.gov/citations/19860019447
• Bowers, A. H., and A. G. Sim. 1984. A Comparison of Wortmann Airfoil Computer-Generated Lift and Drag Polars with Flight and Wind Tunnel Results. NASA-TM-86035. NASA. https://ntrs.nasa.gov/citations/19850004560
• Bowles, Roland L. 1992. “Program Overview: 1991 Flight Test Objectives.” In Airborne Wind Shear Detection and Warning Systems: Fourth Combined Manufacturers’ and Technologists’ Conference, Part 1. https://ntrs.nasa.gov/citations/19930010402
• Bowman, James S. 1965. “Airplane Spinning.” In NASA Conference on Aircraft Operating Problems: A Compilation of the Papers Presented. https://ntrs.nasa.gov/citations/20000011996
• Bowman, James S., Jr. 1956. Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395. NACA-RM-SL56H02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028485
• Bowman, J., Jr., H. Stough, S. Burk Jr., and J. Patton Jr. 1978. “Correlation of Model and Airplane Spin Characteristics for a Low-Wing General Aviation Research Airplane.” In Aircraft Systems and Technology Conference. AIAA 1978-1477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1477
• Boyce, Russell, Sullivan Gerard, and Allan Paull. 2003. “The HyShot Scramjet Flight Experiment: Flight Data and CFD Calculations Compared.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7029
• Boyce, R., and A. Paull. 2001. “Scramjet Intake and Exhaust CFD Studies for the HyShot Scramjet Flight Experiment.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1891. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1891
• Boyd, D. Douglas, Jr., and Casey L. Burley. 2001. “Analysis of Measured and Predicted Acoustics from an XV-15 Flight Test.” In Proceedings of the Vertical Flight Society Forum 57 - Washington, D.C. 2001. The Vertical Flight Society. https://doi.org/10.4050/vfs-f57-00016
• Boyden, R. P. 1974. Dynamic Stability Characteristics in Pitch, Yaw, and Roll of a Supercritical-Wing Research Airplane Model. NASA-TM-X-2900. NASA. https://ntrs.nasa.gov/citations/19830002753
• Boyden, R. P. 1978. Subsonic Roll Damping of a Model with Swept-Back and Swept-Forward Wings. NASA-TM-78677. NASA. https://ntrs.nasa.gov/citations/19780012118
• Boyer, Kenneth. 1964. “Technique for Testing Dynamically Simulated Free Flight Ejection Models in a Polysonic Blowdown Wind Tunnel.” In Aerodynamic Testing Conference. AIAA 1964-1121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-1121
• Boztug, B. A., S. Soganci, S. Aydin, and O. Cicek. 2026. “B1.2: Flight Test Instrumentation Blade Clearance Optical Measurement Method and Optimization in Scope of T625 GOKBEY Helicopter.” In Lectures. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2026/b1.2
• Bradford, John, John Olds, Ryan Bechtel, Tim Cormier, and Donald Messitt. 2000. “Exploration of the Design Space for the ABLV-GT SSTO Reusable Launch Vehicle.” In Space 2000 Conference and Exposition. AIAA 2000-5136. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5136
• Bradley, Marty K., and Christopher K. Droney. 2011. Subsonic Ultra Green Aircraft Research. NASA/CR-2011-216847. NASA. https://ntrs.nasa.gov/citations/20110011321
• Bradley, Marty K., and Christopher K. Droney. 2012. Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development. NASA/CR-2012-217556. NASA. https://ntrs.nasa.gov/citations/20120009038
• Bradley, Marty K., and Christopher K. Droney. 2015. Subsonic Ultra Green Aircraft Research: Phase 2: Hybrid Electric Design Exploration: Volume 2. NASA/CR-2015-218704/VOL2. NASA. https://ntrs.nasa.gov/citations/20150017039
• Bradley, Marty K., Christopher K. Droney, and Timothy J. Allen. 2015. Subsonic Ultra Green Aircraft Research: Truss Braced Wing Design Exploration: Phase II: Volume I. NASA/CR-2015-218704/VOL1. NASA. https://ntrs.nasa.gov/citations/20150017036
• Bradley, P., P. Siemers III, and C. Pruett. 1981. “Comparison of Forward Fuselage to Space Shuttle Orbiter Flight Pressure Data to Wind Tunnel and Analytical Results in the Hypersonic Machnumber Range.” In 1st Flight Test Conference. AIAA 1981-2477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2477
• Bragg, M., and G. Gregorek. 1989. “Environmentally Induced Surface Roughness Effects on Laminar Flow Airfoils: Implications for Flight Safety.” In Aircraft Design and Operations Meeting. AIAA 1989-2049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2049
• Braman, K., W. Schweikhard, and T. Yechout. 1983. “Thrust Modeling: A Simplified in-Flight Thrust and Airflow Prediction Technique for Flight Test Performance Measurements.” In 2nd Flight Testing Conference. AIAA 1983-2751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2751
• Brand, A. G., and J. C. Narramore. 1992. “Navier-Stokes Correlations to Fuselage Wind Tunnel Test Data.” In Proceedings of the Vertical Flight Society Forum 48 - Washington, D.C. 1992. The Vertical Flight Society. https://doi.org/10.4050/vfs-f48-1038
• Brandeau, G. 1978. “Evolution of a Cost-Effective, Task-Oriented, Lateral-Directional SAS for the a-10 Aircraft.” In Aircraft Systems and Technology Conference. AIAA 1978-1460. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1460
• Brandis, Aaron M., and Brett A. Cruden. 2017. “Titan Atmospheric Entry Radiative Heating.” In 47th AIAA Thermophysics Conference. AIAA 2017-4534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4534
• Brandis, Aaron, Christopher Johnston, Brett Cruden, Dinesh Prabhu, and Deepak Bose. 2012. “Validation of High Speed Earth Atmospheric Entry Radiative Heating from 9.5 to 15.5 Km/s.” In 43rd AIAA Thermophysics Conference. AIAA 2012-2865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2865
• Brandon, Jay. 2024. “X-59: GNC Architecture for NASA’s Supersonic X-Plane.” In CEAS EuroGNC 2024. https://ntrs.nasa.gov/citations/20240006461
• Brandon, Jay, Philip Brown, Michael Phillips, and Louis Glaab. 1995. “Ground-to-Flight Handling Qualities Comparisons for a High Performance Airplane.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3457
• Brandon, Jay M., Philip W. Brown, and Alfred J. Wunschel. 1987. Piloted-Simulation Study of Effects of Vortex Flaps on Low-Speed Handling Qualities of a Delta-Wing Airplane. NASA-TP-2747. NASA. https://ntrs.nasa.gov/citations/19870017489
• Brandon, Jay M., Frank L. Jordan Jr., Robert A. Stuever, and Catherine W. Buttrill. 1997. Application of Wind Tunnel Free-Flight Technique for Wake Vortex Encounters. NASA-TP-3672. NASA. https://ntrs.nasa.gov/citations/19980001023
• Brandon, Jay, James Simon, D. Owens, and Jason Kiddy. 1996. “Free-Flight Investigation of Forebody Blowing for Stability and Control.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3444
• Braslow, A. L. 1966. Analysis of Boundary-Layer Transition on X-152-2 Research Airplane. NASA-TN-D-3487. NASA. https://ntrs.nasa.gov/citations/19660020887
• Braslow, A. L. 1999b. History of Suction-Type Laminar-Flow Control with Emphasis on Flight Resrearch: Monographs in Aerospace History Number 13. PB99-166142. NASA Headquarters. https://ntrs.nasa.gov/citations/19990078750
• Braun, Walter F. 1958. The Free Flight Aerodynamics Range. Defense Technical Information Center. https://doi.org/10.21236/ad0202249
• Bray, K. N. C. 1962. “Evaluation of the Hypersonic Gun Tunnel.” In Hypersonic Flow Research. Elsevier. https://doi.org/10.1016/b978-0-12-395595-1.50027-1
• Bray, R. 1963. “Piloted Simulator Studies Pertaining to the Low-Speed Longitudinal Handling Qualities of a Supersonic Transport Airplane.” In Heterogeneous Combustion Conference. AIAA 1963-1003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1003
• Brazel, J., R. Tanzilli, and A. Begany. 1965. “Determination of Thermal Performance of Char under Heating Conditions Simulating Atmospheric Entry.” In Thermophysics Specialist Conference. AIAA 1965-640. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-640
• Brennan, Sean, and Michael McDaniel. 1994. Airship Applications of Modern Flight Test Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada284253
• Brenner, Martin J. 2001. “Aeroservoelastic Uncertainty Model Identification from Flight Data.” In Confederation of European Aerospace Societies. https://ntrs.nasa.gov/citations/20010071675
• Brenner, Martin, Richard Lind, David Voracek, Martin Brenner, Richard Lind, and David Voracek. 1997. “Overview of Recent Flight Flutter Testing Research at NASA Dryden.” In 38th Structures, Structural Dynamics, and Materials Conference. AIAA 1997-1023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1023
• Brevault, Loïc, Mathieu Balesdent, Ali Hebbal, and Antoine Patureau De Mirand. 2019. “Surrogate Model-Based Multi-Objective MDO Approach for Partially Reusable Launch Vehicle Design.” In AIAA Scitech 2019 Forum. AIAA 2019-0704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0704
• Brewer, J. D. 1966. NASA Research on Promising V/STOL Aircraft Concepts. NASA-TM-X-59964. NASA. https://ntrs.nasa.gov/citations/19680018334
• Brewer, R., and D. Brant. 1980. “Thermal Protection System for the Galileo Mission Atmospheric Entry Probe.” In 18th Aerospace Sciences Meeting. AIAA 1980-358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-358
• “Brian Trubshaw: Test Pilot.” 2006. Aircraft Engineering and Aerospace Technology 78 (6). https://doi.org/10.1108/aeat.2006.12778fae.001
• Bridges, P. G., E. J. Cross Jr., and D. W. Boatwright. 1977. “Flight Test Evaluation of a Method to Determine the Level Flight Performance of a Propeller-Driven Aircraft.” In Business Aircraft Meeting, Century 2. https://ntrs.nasa.gov/citations/19770013132
• “A Brief History of General Electric (of the USA) Aircraft Engine Business.” 1978. Aircraft Engineering and Aerospace Technology 50 (10): 25–28. https://doi.org/10.1108/eb035490
• Briggs, Hugh C. 2017. “Design and Implementation of a Flutter Suppression Experiment.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4357
• Brignac, W. J., H. B. Ness, M. K. Johnson, and L. M. Smith. 1976. “YF-16 Flight Flutter Test Procedures.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014094
• Brilliant, H. M., and C. A. Bauer. 1977. “Comparison of Estimated with Measured Maximum Instantaneous Distortion Using Flight Data from an Axisymmetric Mixed Compression Inlet.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19770055718
• Brinda, V., S. Dasgupta, and Madan Lal. 2006. “Trajectory Optimization and Guidance of an Air Breathing Hypersonic Vehicle.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7997
• Brinker, Joseph. 2004. “Autonomous Steering of the Joint Unmanned Combat Air System (J-UCAS) X-45A.” In AIAA 3rd “Unmanned Unlimited” Technical Conference, Workshop and Exhibit. AIAA 2004-6575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6575
• Brinker, Joseph, and Kevin Wise. 2000. “Flight Testing of a Reconfigurable Flight Control Law on the X-36 Tailless Fighter Aircraft.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-3941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3941
• Brinza, Ionut O. 2024. “Hybride Laminar Flow Control Wing Demonstrator.” In AIAA SCITECH 2024 Forum. AIAA 2024-2351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2351
• Brion, Vincent, Motoyuki Aki, and Sergey Shkarayev. 2006. “Numerical Simulations of Low Reynolds Number Flows around Micro Air Vehicles and Comparison against Wind Tunnel Data.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3864
• “British Research Aircraft: Brief Details of Two Single-Seat Research Aircraft Produced by the British Aircraft Corporation.” 1962. Aircraft Engineering and Aerospace Technology 34 (10): 287–287. https://doi.org/10.1108/eb033620
• Broeren, Andy P., Sam Lee, Brian S. Woodard, Christopher W. Lum, and Timothy G. Smith. 2019. Independent Effects of Reynolds Number and Mach Number on the Aerodynamics of an Iced Swept Wing. NASA/TM-2019-220012. NASA. https://ntrs.nasa.gov/citations/20190027696
• Broeren, Andy, Brian Woodard, Jeff Diebold, and Frederic Moens. 2017. “Low-Reynolds Number Aerodynamics of an 8.9 Percent Scale Semispan Swept Wing for Assessment of Icing Effects.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170007300
• Bromberg, J., and G. Hansen. 1965. “Future Requirements for Lh Sub 2 Vehicle Flight Testing.” In Flight Testing Conference. AIAA 1965-217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-217
• Bronder, Timothy, Jason Lee, David Heinz, and Nicholas Helms. 2012. “Initial Testing and Development of an Organic Remote Pilot Aircraft Capability at the USAF Test Pilot School.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-3082. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3082
• Bronz, Murat, Hector Garcia de Marina, and Gautier Hattenberger. 2017. “In-Flight Thrust Measurement Using on-Board Force Sensor.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0698. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0698
• Bronz, Murat, and Gautier Hattenberger. 2016. “Aerodynamic Characterization of an off-the-Shelf Aircraft via Flight Test and Numerical Simulation.” In AIAA Flight Testing Conference. AIAA 2016-3979. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3979
• Brooks, R. 1986. “Advanced Instrumentation, Control, and Estimation Concepts for Flight Test and Evaluation.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9796
• Brooks, B., and K. Mackall. 1984. “Measurement and Analysis of Acoustic Flight Test Data for Two Advanced Design High Speed Propeller Models.” In 22nd Aerospace Sciences Meeting. AIAA 1984-250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-250
• Brotherhood, P. 1975. “Some Aerodynamic Measurements in Helicopter Flight Research.” Aeronautical Journal 79 (778): 450–65. https://doi.org/10.1017/s0001924000036009
• Broughton, R. 1978. “B-1 Flight Test Progress Report.” In Aircraft Systems and Technology Conference. AIAA 1978-1448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1448
• Brower, William B. 2024. “Dimensional Analysis, Dynamic Similitude, and Inspectional Analysis.” In A Primer in Fluid MechanicsDynamics of Flows in One Space Dimension. CRC Press. https://doi.org/10.1201/9781003575214-5
• Brower, W., Jr. 1989. “Theoretical Study of Passive Drag-Reduction on Transonic Airfoils.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3382. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3382
• Brown, Clinton E. 1944. NACA Investigation of a Jet-Propulsion System Applicable to Flight. NACA-WR-L-528. NASA. https://ntrs.nasa.gov/citations/19930093539
• Brown, E. 1965. “A Survey of Low-Disc-Loading VTOL Aircraft Designs.” In Aircraft Design and Technology Meeting. AIAA 1965-756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-756
• Brown, D. 1981. “Application of Pulse Code Modulation Technology to Aircraft Dynamics Data Acquisition.” In Aircraft Systems and Technology Conference. AIAA 1981-1736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1736
• Brown, David. 1989. “Supersonic STOVL Conceptual Design of a Fighter/attack Aircraft.” In Aircraft Design and Operations Meeting. AIAA 1989-2112. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2112
• Brown, Travis A. 1997. Electric Fuzing Instrumentation System Test Program on the F/A-18A Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada389429
• Brown, Anthony. 2004. “AIRS II Flight Determination of Turboprop Transport Aeroplane Lift, Drag, and Propulsive Effiency Effects in Freezing Drizzle Icing.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4949
• Brown, Nelson A. 2009a. F-15 Intelligent Flight Control System and Aeronautics Research at NASA Dryden. DFRC-992. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090021683
• Brown, Nelson A. 2009b. Intelligent Flight Control System and Aeronautics Research at NASA Dryden. DFRC-992. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090022141
• Brown, Laurie, and Russell Boyce. 2012. “3D Separations within the SCRAMSPACE I Hypersonic Flight Experiment Scramjet.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5890
• Brown, Laurie, Russell Boyce, and Sandy Tirtey. 2011. “Numerical Simulation of SCRAMSPACE I Flight Experiment.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2367
• Brown, S., and D. Bradley. 1981. “Uncertainty Analysis for Flight Test Performance Calculations.” In 1st Flight Test Conference. AIAA 1981-2390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2390
• Brown, E., and J. Duhon. 1965. “Helicopter Wind Tunnel Data and Theory Correlated to Full Scale Flight Performance.” In Flight Testing Conference. AIAA 1965-209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-209
• Brown, Jessica, and George Haglund. 1988. “Sonic Boom Loudness Study and Airplane Configuration Development.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4467
• Brown, Nelson, Allwyn Samuel, Richard Colgren, and Jim Lookadoo. 2007. “Mars Exploration Airplane: Design, Construction, and Flight Testing of a Stability, Control, and Performance Demonstrator.” In AIAA Infotech@Aerospace 2007 Conference and Exhibit. AIAA 2007-2723. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2723
• Brown, Richard N., and Kumar V. Singh. 2015. “Optimal Sizing and Configurations of the Control Surfaces for Active Aeroelastic Control.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2241
• Brown, Laurie, Sandy Tirtey, Paul van Staden, and Michael Creagh. 2012. “Static Stability of the SCRAMSPACE I Mach 8 Hypersonic Flight Experiment.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5936
• Brown, Charles, Ted Wierzbanowski, Helmut Reda, and Gregory T. Duecker. 1992. An Environmental Study of the National Aerospace Plane. Defense Technical Information Center. https://doi.org/10.21236/ada266071
• Browne, Oliver M., Daniel Maldonado, Jeffrey A. Housman, Jared Duensing, and William E. Milholen. 2024. “Simulating Transonic Buffet Aerodynamics for the Boeing Transonic Truss-Braced Wing Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-0065. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0065
• Brune, Andrew J., and Chelsey Morrow. 2023. “Uncertainty Analysis of Slug Calorimeters in the Hypersonic Material Environmental Test System Arc-Jet Facility.” In AIAA AVIATION 2023 Forum. AIAA 2023-4038. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4038
• Brunner, Michael. 1996. “High-Fidelity Simulation as a Low Cost Enhancement to Flight Test.” In Flight Simulation Technologies Conference. AIAA 1996-3520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3520
• Brunner, M. J., C. Dolan, R. Grasier, S. Kottock, and G. Merlo. 1966. Study of Thermal Protection Requirements for a Lifting Body Entry Vehicle Suitable for near-Earth Missions Final Report. NASA-CR-73043. NASA. https://ntrs.nasa.gov/citations/19670008947
• Bruno, Claudio. 2023. “Hypersonic Flight and Its Impact on Propulsion.” In Airbreathing Hypersonic Propulsion. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-7927-9_4
• Brunton, Steven L., Bernd R. Noack, and Petros Koumoutsakos. 2020. “Machine Learning for Fluid Mechanics.” Annual Review of Fluid Mechanics 52 (1): 477–508. https://doi.org/10.1146/annurev-fluid-010719-060214
• Bryant, Robert L. 1948. Longitudinal Trim and Tumble Characteristics of a 0.057-Scale Model of the Chance Vought XF7U-1 Airplane, TED NO. NACA DE311. NACA-RM-SL8F14. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028902
• Bryant, W. H., and W. F. Hodge. 1974. “Effects of Flight Instrumentation Errors on the Estimation of Aircraft Stability and Control Derivatives.” In Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017472
• Bryant, W., F. Morrell, and M. Bailey. 1984. “Flight Test Configuration for Verifying Inertial Sensor Redundancy Management Techniques.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2496
• Bryson, A. E., Jr., W. C. Hoffman, and J. Zvara. 1968. A Terminal Guidance Scheme for Lifting Body Entry Vehicles. NASA-CR-86126. NASA. https://ntrs.nasa.gov/citations/19690010344
• Buch Jr. and George M. 2010. AMC’s Future Strategic Airlifter: The Blended Wing Body?. Defense Technical Information Center. https://doi.org/10.21236/ada526601
• Buchanan, T. D., and W. A. Crosby. 1983. Captive Trajectory System Test Planning Information for AEDC Supersonic Wind Tunnel (a) and Hypersonic Wind Tunnels (B) and (C). Defense Technical Information Center. https://doi.org/10.21236/ada136439
• Buckingham, E. 1914. “On Physically Similar Systems; Illustrations of the Use of Dimensional Equations.” Physical Review 4 (4): 345–76. https://doi.org/10.1103/physrev.4.345
• Budd, Gerald D., Ronald L. Gilman, and David Eichstedt. 1993. “Operational and Research Aspects of a Radio-Controlled Model Flight Test Program.” In AIAA. https://ntrs.nasa.gov/citations/19930040745
• Bueche, J. 1966. “Effect of Spherical Roughness on Hypersonic Boundary-Layer Transition.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-26. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-26
• Buenz, D. A., S. Brooks, R. Mohr, and J. Kanow. 1975. Identification of T-2 Aerodynamic Derivatives from Flight Data. Defense Technical Information Center. https://doi.org/10.21236/ada021996
• Bufalino, Sam. 1995. “Managing the Introduction of CAIS to F/A-18E/F Flight Test Operations (Common Airborne Instrumentation System).” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3899
• Buffington, James M. 1997. Tailless Aircraft Control Allocation. Defense Technical Information Center. https://doi.org/10.21236/ada327799
• Bugg, F. M., and W. C. Sleeman Jr. 1967. Low-Speed Tests of an All-Flexible Parawing for Landing a Lifting-Body Spacecraft. NASA-TN-D-4010. NASA. https://ntrs.nasa.gov/citations/19670019428
• Bui, Trong T. 2013. “Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Laminar-Flow Glove.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3032
• Bui, Trong T. 2018. “Analysis of High-Speed Aerodynamics of a Swept Wing with Seamless Flaps (Invited).” In 2018 Applied Aerodynamics Conference. AIAA 2018-3808. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3808
• Bull, G., and P. Bridges. 1983. “A New Method for Flight Test Determination of Propulsive Efficiency and Drag Coefficient.” In 2nd Flight Testing Conference. AIAA 1983-2750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2750
• Bullard, C. 1967. “Attitude of a Spinning Rocket under Thrust with Statistically Variederror Sources.” In Control and Flight Dynamics Conference. AIAA 1967-536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-536
• Bulmer, B. 1974. “Study of Base Pressure in Laminar Hypersonic Flow: Reentry Flight Measurements.” In 7th Fluid and PlasmaDynamics Conference. AIAA 1974-537. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-537
• Bulyshev, Alexander, Farzin Amzajerdian, Eric Roback, and Reisse Robert. 2014. “A Super-Resolution Algorithm for Enhancement of FLASH LIDAR Data: Flight Test Results.” In International Society for Optical Engineering. https://ntrs.nasa.gov/citations/20140011915
• Bundick, W. Thomas. 1990. Development of an Adaptive Failure Detection and Identification System for Detecting Aircraft Control Element Failures. NASA-TP-3051. NASA. https://ntrs.nasa.gov/citations/19910015837
• Bunge, Roberto, Felipe Munera Savino, and Ilan Kroo. 2015. “Stall/Spin Flight Test Techniques with COTS Model Aircraft and Flight Data Systems.” In AIAA Flight Testing Conference. AIAA 2015-3225. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3225
• Buning, Pieter G., Tin-Chee Wong, Arthur D. Dilley, and Jenn L. Pao. 2000. Prediction of Hyper-X Stage Separation Aerodynamics Using CFD. AIAA Paper 2000-4009. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000091005
• Bunnell, Mort V., and Noel K. Delany. 1947. Comparison of Wind-Tunnel Predictions with Flight Measurements of the Longitudinal-Stability and -Control Characteristics of a Douglas BTD-1 Airplane. NACA-RM-A6L30. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20030063163
• Bur, R., R. Benay, B. Corbel, and J. Délery. 2002. “Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction.” In Drag Reduction by Shock and Boundary Layer Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45856-2_3
• Burcham, Frank W., Timothy R. Conners, and Michael D. Maxwell. 1995a. “Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/95-gt-119
• Burcham, F., Jr., and John Burken. 1994. “Flight Testing a Propulsion-Controlled Aircraft Emergency Flight Control System on an F-15 Airplane.” In Biennial Flight Test Conference. AIAA 1994-2123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2123
• Burcham, Frank W., Jr., John J. Burken, Trindel A. Maine, and C. Gordon Fullerton. 1997a. Development and Flight Test of an Emergency Flight Control System Using Only Engine Thrust on an MD-11 Transport Airplane. NASA/TP-1997-206217. NASA. https://ntrs.nasa.gov/citations/19980210483
• Burcham, Frank W., Jr., Timothy R. Conners, and Michael D. Maxwell. 1994. Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/19990064011
• Burcham, Frank W., Jr., C. Gordon Fullerton, and Trindel A. Maine. 2004. Manual Manipulation of Engine Throttles for Emergency Flight Control. NASA/TM-2004-212045. NASA. https://ntrs.nasa.gov/citations/20040021348
• Burcham, Frank W., Jr., Donald H. Gatlin, and James F. Stewart. 1995b. “An Overview of Integrated Flight-Propulsion Controls Flight Research on the NASA F-15 Research Airplane.” In An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program. https://ntrs.nasa.gov/citations/19950026589
• Burcham, Frank W., Jr., Trindel A. Maine, C. Gordon Fullerton, and Lannie Dean Webb. 1996. Development and Flight Evaluation of an Emergency Digital Flight Control System Using Only Engine Thrust on an F-15 Airplane. NASA-TP-3627. NASA. https://ntrs.nasa.gov/citations/19970001362
• Burcham, Frank, Jr., Trindel Maine, and Thomas Wolf. 1992. “Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4109
• Burcham, F., Jr., L. Myers, J. Nugent, P. Lasagna, and L. Webb. 1981. “Recent Propulsion System Flight Tests at the NASA Dryden Flight Research Center.” In 1st Flight Test Conference. AIAA 1981-2438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2438
• Burcham, F., Jr., L. Myers, and K. Walsh. 1983. “Flight Evaluation Results for a Digital Electronic Engine Control Inan F-15 Airplane.” In 2nd Flight Testing Conference. AIAA 1983-2703. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2703
• Burcham, Frank, Jr., and Drew Pappas. 1996. “Development and Flight Test of an Augmented Thrust-Only Flight Control System on an MD-11 Transport Airplane.” In Guidance, Navigation, and Control Conference. AIAA 1996-3742. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3742
• Burcham, Frank, Jr., and Ronald Ray. 1987. “The Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2877
• Burcham, Frank W., Jr., Ronald J. Ray, Timothy R. Conners, and Kevin R. Walsh. 1997b. Propulsion Flight Research at NASA Dryden from 1967 to 1997. NASA/TP-1998-206554. NASA. https://ntrs.nasa.gov/citations/19980218800
• Burcham, F., Jr., G. Trippensee, D. Fisher, and T. Putnam. 1986. “Summary of Results of NASA F-15 Flight Research Program.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9761. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9761
• Burdges, K. 1973. “A Synthesis of Transonic, 2-D Airfoil Technology.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-792
• Burdges, K. 1979. “Experimental Measurements of Shock/boundary-Layer Interaction of a Supercritical Airfoil.” In 12th Fluid and Plasma Dynamics Conference. AIAA 1979-1499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1499
• Burger, K. 1983. “In-Flight Short Field Landing Investigations on a Combat Aircraft with Thrust Reverser.” In 2nd Flight Testing Conference. AIAA 1983-2693. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2693
• Burkardt, Leo A., and Leo C. Franciscus. 1990. “RAMSCRAM: A Flexible RAMJET/SCRAMJET Engine Simulation Program.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-323
• Burke, P. K. 1983. “Validation of Gunsight Accuracy through Limited Flight Testing: The Night Tracer Flight.” In 2nd Flight Testing Conference. AIAA 1983-2692. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2692
• Burken, John. 1992. “Flight-Determined Stability Analysis of Multiple-Input-Multiple-Output Control Systems.” In Guidance, Navigation and Control Conference. AIAA 1992-4396. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4396
• Burkhardt, Johannes, Michael Graesslin, and Ulrich Schoettle. 1999. “Impact of Mission Constraints on Optimal Flight Trajectories for the Lifting Body X-38.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4167
• Burks, J. 1981. “Rotor Systems Research Aircraft /RSRA/ Rotor Force and Moment Measurement System.” In 1st Flight Test Conference. AIAA 1981-2516. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2516
• Burley, R. 1970. “Flight Performance of Auxiliary Inlet Ejector and Plug Nozzle at Transonic Speeds.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-701
• Burn, Melissa, and Kenneth J. Plotkin. 1989. PCBOOM2: Enhancement of PCBOOM Sonic Boom Analysis Program. Defense Technical Information Center. https://doi.org/10.21236/ada401725
• Burner, Alpheus W., William A. Lokos, and Danny A. Barrows. 2005. Aeroelastic Deformation: Adaptation of Wind Tunnel Measurement Concepts to Full-Scale Vehicle Flight Testing. NASA/TM-2005-213790. NASA. https://ntrs.nasa.gov/citations/20060002833
• Burnett, Edward. 2002. “Flight Test Rehearsal Using Computer Connectivity to Increase Flight Test Safety.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2002-4478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4478
• Burnett, David, and Mark Lewis. 1993. “A Re-Evaluation of the Waverider Design Process.” In 31st Aerospace Sciences Meeting. AIAA 1993-404. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-404
• Burns, W. 1970. “Free-Flight Wind Tunnel Test of Hypersonic Decelerators.” In Propulsion and ASW Meeting. AIAA 1970-587. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-587
• Burns, W. J. 1974. ABRES Flight Test Evaluation of RV Accuracy. Defense Technical Information Center. https://doi.org/10.21236/ada048471
• Burns, Kevin. 2004. “The History of Aerospace Research at Cornell Aeronautical Laboratory and Calspan: 1946 to 1996.” In Space 2004 Conference and Exhibit. AIAA 2004-5884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5884
• Burns, Kevin R. 2022. “The History of Hypersonic Research at Cornell Aeronautical Laboratory.” In AIAA SCITECH 2022 Forum. AIAA 2022-1604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1604
• Burns, Kevin R. 2026. “The History of Tire Testing at Cornell Aeronautical Laboratory.” In AIAA SCITECH 2026 Forum. AIAA 2026-2553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2553
• Burns, Kevin, and Adam Bruckner. 2006. “The History of Aerospace Research at Cornell Aeronautical Laboratory and Calspan.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-335
• Burns, Kevin, William Milliken, and Irving Statler. 2007. “The History of Aerospace Research at Cornell Aeronautical Laboratory and Calspan.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-359
• Burns, Willoughby, III. 1992. “Kinetic Kill Vehicle Flight Test Program.” In Aerospace Design Conference. AIAA 1992-1211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1211
• Burnside, Nathan. 2012. “DDS-Suite: A Dynamic Data Acquisition, Processing, and Analysis System for Wind Tunnel Testing.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-3169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3169
• Bursey, R., and R. Dickinson. 1990. “Flight Test Results of the F-15 SMTD Thrust Vectoring/thrust Reversing Exhaust Nozzle.” In 26th Joint Propulsion Conference. AIAA 1990-1906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1906
• Burton, R., and D. Bischoff. 1976. “More Effective Aircraft Stability and Control Flight Testing Throughuse of System Identification Technology.” In Aircraft Systems and Technology Meeting. AIAA 1976-894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-894
• Busetto, Alberto Giovanni, Cheng Soon Ong, and Joachim M. Buhmann. 2009. “Optimized Expected Information Gain for Nonlinear Dynamical Systems.” In Proceedings of the 26th Annual International Conference on Machine Learning. ACM. https://doi.org/10.1145/1553374.1553387
• Bush, Lee. 1965. “An Abstract of an Analysis: The Effect of the Airframe Manufacturer’s Cost on the Cost of Aircraft Ownership.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/650370
• Bushnell, D. M. 1992. “Supersonic Laminar Flow Control.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_7
• Bushnell, Dennis M. 2006. “SCALING: Wind Tunnel to Flight.” Annual Review of Fluid Mechanics 38 (1): 111–28. https://doi.org/10.1146/annurev.fluid.38.050304.092208
• Buss, Marvin W., and Brock M. Nicholson. 1971. Engineering Flight Test, AH-1G (HueyCobra) Helicopter Autorotational Entry Characteristics. Defense Technical Information Center. https://doi.org/10.21236/ad0887550
• Bussing, T., and E. Murman. 1983. “A One-Dimensional Unsteady Model of Dual Mode Scramjet Operation.” In 21st Aerospace Sciences Meeting. AIAA 1983-422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-422
• Butler, J. P., and D. A. Rees. 1974. Development of Statistical Fatigue Failure Characteristics of 0.125-Inch 2024-T3 Aluminum under Simulated Flight-by-Flight Loading. Defense Technical Information Center. https://doi.org/10.21236/ada002310
• Butter, Ulrich, Heinz-Jürgen Pausder, and Volker Gollnick. 1996. “ACT Demonstrator/ Flying Helicopter Simulator: A New Demonstrator Test Bed for Flight Control and Cockpit Technologies.” In Proceedings of the Vertical Flight Society Forum 52 - Washington, DC 1996. The Vertical Flight Society. https://doi.org/10.4050/vfs-f52-1152
• Butters, W. G., and K. S. Zeisel. 1982. Lightning Tests on the WC-130 Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada129141
• Buttrill, Carey S., and Jacob A. Houck. 1990. “Hot-Bench Simulation of the Active Flexible Wing Wind-Tunnel Model.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3121
• Bynum, Michael, and Robert Baurle. 2011. “A Design of Experiments Study for the HIFiRE Flight 2 Ground Test Computational Fluid Dynamics Results.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2203
• Bynum, D. S., R. L. Ledford, and W. E. Smotherman. 1970. Wind Tunnel Pressure Measuring Techniques. Defense Technical Information Center. https://doi.org/10.21236/ad0714565
• Byrne, W. 1971. “Sonic Boom Simulation with Detonable Gases.” In 9th Aerospace Sciences Meeting. AIAA 1971-186. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-186
• Byrnes, J., R. Murphy, R. Ball, et al. 1974. “V/STOL Demonstrator Vehicle for Ejector Thrust Augmentation Technology.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-995
• Caballero, N. 2001. “Drag Reduction in Airfoils Using Control Devices in the Shock Wave-Boundary Layer Interaction Region.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_40
• Cabarbaye, Aurélien. n.d. “Design, Model and Control of a New Type of VTOL Aircraft.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/142832fez8c1cz4237z83b9z89d813801148
• Cahill, J. F., and P. C. Connor. 1979. Correlation of Data Related to Shock-Induced Trailing-Edge Separation and Extrapolation to Flight Reynolds Number. NASA-CR-3178. NASA. https://ntrs.nasa.gov/citations/19790023024
• Cain, Maurice R. 1979. Facility Air Control Systems Design for a Pilot Transonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada379310
• Cain, Terrence, and Craig Walton. 2003. “The Sustained Hypersonic Flight Experiment.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7030. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7030
• Calarese, W., and R. Walterick. 1978. “Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1180
• Cale, David B. 1982. “800 Shaft Horsepower Advanced Technology Demonstrator Engine (ATDE) Status Update.” In Proceedings of the Vertical Flight Society Forum 38 - Anaheim, CA 1982. The Vertical Flight Society. https://doi.org/10.4050/vfs-f38-015
• Calhoun, Philip. 2000. “An Entry Flight Controls Analysis for a Reusable Launch Vehicle.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-1046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1046
• Calico, R., Jr., and S. Fuller. 1981. “Stability Characteristics of a Forward Swept Wing Aircraft at High Angles of Attack.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1884
• Calise, Anthony. 2000. “Development of a Reconfigurable Flight Control Law for the X-36 Tailless Fighter Aircraft.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-3940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3940
• Callaghan, J. 1968. “The Simulation of Sonic Boom by Ballistic Models.” In 3rd Aerodynamics Testing Conference. AIAA 1968-383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-383
• Callies, R., and G. Wimmer. 2000. “Optimal Hypersonic Flight Trajectories with Full Safety in Case of Mission Abort.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3996
• Calloway, R. S. 1986. “CID-720 Aircraft High-Environment Flight Instrumentation System.” In Full-Scale Transport Controlled Impact Demonstration. https://ntrs.nasa.gov/citations/19860012476
• Camacho, P. 1991. “VTOL/SP: A Vertical Takeoff and Landing Vehicle Synthesis Program.” In Aircraft Design and Operations Meeting. AIAA 1991-3098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3098
• Camacho, Peter P., Khanh H. Pham, Leo L. Chou, Neal A. Harrison, and Abdollah Khodadoust. 2020. “Progress on Aerodynamic Performance Analysis of SNLF Transonic Truss-Braced Wing.” In AIAA Scitech 2020 Forum. AIAA 2020-1025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1025
• Cambier, Jean-Luc, Susan Tokarcik, and Dinesh Prabhu. 1992. “Numerical Simulation of Unsteady Flow in a Hypersonic Shock Tunnel Facility.” In 17th Aerospace Ground Testing Conference. AIAA 1992-4029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4029
• Campbell, John P. 1959. “Research on VTOL and STOL Aircraft in the United States.” In Advances in Aeronautical Sciences. Elsevier. https://doi.org/10.1016/b978-1-4831-9833-0.50014-1
• Campbell, John P. 1964. Status of V/stol Research and Development in the United States. NASA-RP-286. NASA. https://ntrs.nasa.gov/citations/19640018315
• Campbell, Mark R. 2025. “History of the Assured Crew Return Vehicle and Spaceflight Medical Evacuation.” Aerospace Medicine and Human Performance 96 (10): 953–55. https://doi.org/10.3357/amhp.6737.2025
• Campbell, Charles H., Jose Caram, Scott Berry, Michael DiFulvio, and Tom Horvath. 1997. “Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical Results.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20040100807
• Campbell, Charles, Jose Caram, Chien Li, and Christopher Madden. 1996. “Aerothermodynamic Environment Definition for an X-23/X-24A Derived Assured Crew Return Vehicle.” In 31st Thermophysics Conference. AIAA 1996-1862. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1862
• Campbell, Charles, Rudolph King, Scott Berry, Michael Kegerise, and Thomas Horvath. 2010. “Roles of Engineering Correlations in Hypersonic Entry Boundary Layer Transition Prediction.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-247
• Campbell, Richard L., Sudheer Nayani, and Michelle Lynde. 2015. “Unstructured Grids for Sonic Boom Analysis and Design.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1250
• Campbell, Charles H., Ioannis Nompelis, Graham Candler, Michael Barnhart, and Seokkwan Yoon. 2009. Hypersonic Navier Stokes Comparisons to Orbiter Flight Data. JSC-CN-18483. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20090026318
• Campbell, John P., and Charles L. Seacord Jr. 1943. The Effect of Mass Distribution on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free-Flight Tunnel. NACA-TR-769. NASA. https://ntrs.nasa.gov/citations/19930091848
• “The Canadair CL-84 Experimental Aircraft: Lessons Learned.” 1990. In Aircraft Design, Systems and Operations Conference. AIAA 1990-3205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3205
• Canter, David, and Allen Groves. 1994. “X-31 Post-Stall Envelope Expansion and Tactical Utility Testing.” In Biennial Flight Test Conference. AIAA 1994-2171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2171
• Cao, D. Y., J. B. Zhang, and C. H. Lee. 2007. “Conceptual Design and Numerical Simulations of Hypersonic Waverider Vehicle.” In New Trends in Fluid Mechanics Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-75995-9_86
• Capellari, Giovanni, Eleni Chatzi, and Stefano Mariani. 2016. “An Optimal Sensor Placement Method for SHM Based on Bayesian Experimental Design and Polynomial Chaos Expansion.” In Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016). Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece. https://doi.org/10.7712/100016.2257.6762
• Capone, F. J. 1975. Wind Tunnel/flight Data Correlation for the Boeing 737-100 Transport Airplane. NASA-TM-X-72715. NASA. https://ntrs.nasa.gov/citations/19750022978
• Capone, F. J. 1981. Aeropropulsive Characteristics of Twin Nonaxisymmetric Vectoring Nozzles Installed with Forward-Swept and Aft-Swept Wings. NASA-TP-1778. NASA. https://ntrs.nasa.gov/citations/19810010493
• Capone, Francis, and Karen Deere. 2001. “Transonic Investigation of Two-Dimensional Nozzles Designed for Supersonic Cruise Aircraft.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3199
• Carbonaro, M. 1993. “Aerodynamic Force Measurements in the VKI Longshot Hypersonic Facility.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_29
• Carico, Dean. 1998. Flight Test Automation Options. Defense Technical Information Center. https://doi.org/10.21236/ada350677
• Carico, Dean, Chengjian He, and Peter Blemel. 2001. Web-Based Flight Test Training and Mishap Investigation Support. Defense Technical Information Center. https://doi.org/10.21236/ada389261
• Carlomagno, G. M., L. Luca, and G. Cardone. 1993. “Hypersonic Aerodynamics Research with an Infrared Imaging System.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_44
• Carlon, Andre G., Rafael H. Lopez, Leandro F. F. Miguel, and André J. Torii. 2022. “Bayesian Optimal Experimental Design.” In Uncertainty Modeling: Fundamental Concepts and Models. Biblioteca Central da Universidade de Brasilia. https://doi.org/10.4322/978-65-86503-88-3.c15
• Carlsen, Wayne. 1994. “Development of Transonic Area-Rule Methodology.” In 12th Applied Aerodynamics Conference. AIAA 1994-1841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1841
• Carlson, H. W. 1964a. Correlation of Sonic-Boom Theory with Wind-Tunnel and Flight Measurements. NASA-TR-R-213. NASA. https://ntrs.nasa.gov/citations/19650002272
• Carlson, H. W. 1964b. Influence of Airplane Configuration on Sonic- Boom Characteristics. NASA-RP-208. NASA. https://ntrs.nasa.gov/citations/19640015089
• Carlson, H. 1965. “The Influence of Airplane Configuration on the Shape and Magnitude of Sonic-Boom Pressure Signatures.” In Aircraft Design and Technology Meeting. AIAA 1965-803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-803
• Carlson, H. 1970. “On the Application of Heat and Force Fields to the Sonic Boom Minimization Problem.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-903. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-903
• Carlson, H. W., and C. M. Jackson Jr. 1966. Nomograms for Determining Sonic-Boom Overpressure. NASA. https://ntrs.nasa.gov/citations/19660041457
• Carlson, J., R. Mabli, and R. Sickeler. 1965. “Results of Handling Qualities Research for the C-5A.” In Aircraft Design and Technology Meeting. AIAA 1965-740. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-740
• Carlson, H. L., D. J. Maglieri, and N. J. McLeod. 1971. Status of Studies in Sonic Boom. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710021311
• Carlson, H., and O. Morris. 1966. “Wind-Tunnel Sonic-Boom Testing Techniques.” In 2nd Aerodynamic Testing Conference. AIAA 1966-765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-765
• Carlyle, L. 1976. Comparison of Military and Commercial Design-To-Cost Aircraft Procurement and Operational Support Practices. Defense Technical Information Center. https://doi.org/10.21236/ada956001
• Carman, J. 1970. “A Study of the Magnus Effects on a Sounding Rocket at Supersonic Speeds.” In 8th Aerospace Sciences Meeting. AIAA 1970-207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-207
• Carnahan, K. R., G. J. Hartman, and G. J. Neuner. 1975. Development of TPS Flight Test and Operational Instrumentation. NASA-CR-147845. NASA. https://ntrs.nasa.gov/citations/19760023195
• Carpenter, Paul J. 1951. “Effects of Compressibility on the Performance of Two Full-Scale Helicopter Rotors.” In Proceedings of the Vertical Flight Society Forum 7 - Washington, D.C. 1951. The Vertical Flight Society. https://doi.org/10.4050/vfs-f7-002
• Carpenter, Paul J. 1952. Effects of Compressibility on the Performance of Two Full-Scale Helicopter Rotors. NACA-TR-1078. NASA. https://ntrs.nasa.gov/citations/19930092123
• Carpenter, Forrest L., and Paul Cizmas. 2020. “UNS3D Simulations for the Third Sonic Boom Prediction Workshop Part II: C608 Low-Boom Flight Demonstrator.” In AIAA Aviation 2020 Forum. AIAA 2020-2733. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2733
• Carpenter, Forrest L., Lydia J. Hantsche, Larry J. Cliatt, and Edward A. Haering. 2025. “Supersonic Flight Testing to Assess Ground Recording Systems for NASA’s Low Boom Flight Demonstrator.” In AIAA SCITECH 2025 Forum. AIAA 2025-0194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0194
• Carpenter, Paul J., and James P. Shivers. 1956. “Experimental Investigation of Compressibility Effects on a Helicopter Rotor Having NACA 632-015 Airfoil Sections.” In Proceedings of the Vertical Flight Society Forum 12 - Washington, D.C. 1956. The Vertical Flight Society. https://doi.org/10.4050/vfs-f12-007
• Carpenter, Andrew, William Solomon, Anne Sullivan, Andrea J. Korntheuer, and Christopher Harris. 2018. “CFD Design and Flight Test of a Swept Laminar Flow Control Wing.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3809
• Carr, Alexander. 2021. “2aPA2: Probability Distributions of Sonic Boom Noise Metrics in Isotropic Turbulent Fields.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f2421
• Carr, Alexander N., Joel B. Lonzaga, and Steven A. E. Miller. n.d.-a. “Nonnormality of Sonic Boom Loudness Metrics in the Turbulent Atmospheric Boundary Layer at Large Lateral Distances from the Flight Path.” In 183rd Meeting of the Acoustical Society of America. https://ntrs.nasa.gov/citations/20220017634
• Carr, Alexander N., Joel B. Lonzaga, and Steven A. E. Miller. n.d.-b. “Split-Step Simulations of Sonic Boom Propagation beyond the Lateral Cutoff in a Turbulent Atmosphere.” In 183rd Meeting of the Acoustical Society of America. https://ntrs.nasa.gov/citations/20220017631
• Carrese, Robert, Pier Marzocca, Oleg Levinski, and Nishit Joseph. 2016. “Initial Investigations of Supercritical Airfoil Dynamic Response Due to Transonic Buffet.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1552
• Carrillo, Xavier, Roeland De Breuker, and Jurij Sodja. 2024. “Aeroelastic Tailoring of a Strut-Braced Wing for a Medium Range Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-2590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2590
• Carroll, Mikki. 2025. “NACA:: An Indigenous Model of Leadership and Core Values.” In Indigenous Educational Leadership Through Community-Based Knowledge and Research. University of New Mexico Press. https://doi.org/10.2307/jj.34055366.19
• Carroll, Alex T., and Aaron M. Brandis. 2023. “Stagnation Point Convective Heating Correlations for Entry into H2/He Atmospheres.” In AIAA SCITECH 2023 Forum. AIAA 2023-0208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0208
• Carroll, G., and H. Cox. 1983. “A Missile Flight Control System Using Boundary Layer Thrust Vector Control.” In 19th Joint Propulsion Conference. AIAA 1983-1149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1149
• Carten, Andrew S., Jr. 1978. Flight Tests of the Air-Launched Balloon System (ALBS) Prototype Model. Defense Technical Information Center. https://doi.org/10.21236/ada057610
• Carter, Dennis. 1988. “The Integration of Wind Tunnel and Water Tunnel Results for a New in-Flight Simulator Configuration.” In 15th Aerodynamic Testing Conference. AIAA 1988-2045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2045
• Carter, John F. 1997. Production Support Flight Control Computers: Research Capability for F/A-18 Aircraft at Dryden Flight Research Center. NASA/TM-97-206233. NASA. https://ntrs.nasa.gov/citations/19970041277
• Carter, John, John Kelly, Dan Jones, and James Lee. 2013. “Space Technology Demonstrations Using Low Cost, Short-Schedule Airborne and Range Facilities at the Dryden Flight Research Center.” In Next-Generation Suborbital Researchers Conference 2013. https://ntrs.nasa.gov/citations/20170011296
• Carter, John F., and Christopher J. Nagy. 1996. NASA Landing Systems Research Aircraft. DRC-95-31. NASA Hugh L. Dryden Flight Research Center, Edwards, CA. https://ntrs.nasa.gov/citations/19960021846
• Carter, A. L., and R. L. Sims. 1981. Comparison of Theoretical Predictions of Orbiter Airloads with Wind Tunnel and Flight Test Results for a Mach Number of 0.52. NASA-TM-81358. NASA. https://ntrs.nasa.gov/citations/19810014533
• Carter, John, and Mark Stephenson. 1999. “Initial Flight Test of the Production Support Flight Control Computers at NASA Dryden Flight Research Center.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4203
• Caruso, P. S., Jr., and C. R. Naegeli. 1976a. Low-Perigee Aerodynamic Heating during Orbital Flight of an Atmosphere Explorer. NASA-TN-D-8308. NASA. https://ntrs.nasa.gov/citations/19760025417
• Caruso, P. S., Jr., and C. R. Naegeli. 1976b. Theoretical and Empirical Low Perigee Aerodynamic Heating during Orbital Flight of an Atmosphere Explorer. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/19760052458
• Cassanto, J. 1971. “Flight Test Base Pressure Results at Hypersonic Mach Numbers and highReynolds Numbers in Turbulent Flow: Implications to Ground Test Simulation Requirements.” In 9th Aerospace Sciences Meeting. AIAA 1971-134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-134
• Cassanto, J., J. Coats, and N. Rasmussen. 1968. “Correlation of Measured Free Flight Base Pressure Data for M Equals 4 to M Equals 19 in Laminar and Turbulent Flow.” In Fluid and Plasma Dynamics Conference. AIAA 1968-699. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-699
• Castillo Zuñiga, David F., Alain Giacobini Souza, and Luiz Carlos S. Goes. 2019. “Development of an Aeroelastic in-Flight Testing System for a Flexible Wing Unmanned Aerial Vehicle Using Acceleration and Strain Sensors.” In AIAA Scitech 2019 Forum. AIAA 2019-2033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2033
• Castner, Raymond S. 2009. “Wind Tunnel Model Design for the Study of Plume Effects on Sonic Boom for Isolated Exhaust Nozzles.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090029905
• Castner, Raymond. 2010a. “Exhaust Nozzle Plume Effects on Sonic Boom Test Results for Isolated Nozzles.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4936
• Castner, Raynold S. 2010b. Wind Tunnel Model Design for the Study of Plume Effects on Sonic Boom for Isolated Exhaust Nozzles. NASA/TM-2010-216259. NASA. https://ntrs.nasa.gov/citations/20100019443
• Castner, Raymond. 2011. “Exhaust Nozzle Plume Effects on Sonic Boom Test Results for Vectored Nozzles.” In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2011-5974. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-5974
• Castner, Raymond. 2022a. “Quiet Supersonic Technology (QueSST) X-Plane Test.” In Local Experimental Aircraft Association (EAA) Chapter Presentation. https://ntrs.nasa.gov/citations/20220000038
• Castner, Ray. 2022b. “Quiet Supersonic Technology (X-59 QueSST) X-Plane Testing, Analysis, and Progress.” In NASA Engineering and Safety Center (NESC) Aerosciences Technology Discipline Team (TDT) Face to Face meeting. https://ntrs.nasa.gov/citations/20220005771
• Castner, Raymond S., Stephanie Simerly, and Michael Rankin. 2018. “Supersonic Inlet Test for a Quiet Supersonic Transport Technology Demonstrator in the NASA Glenn 8-Foot by 6-Foot Supersonic Wind Tunnel.” In 2018 Applied Aerodynamics Conference. AIAA 2018-2850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2850
• Catanach, Thomas. 2025. Robust Bayesian Optimal Experimental Design under Model Misspecification. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/3395483
• Catanach, Thomas, and Jacob Callahan. 2024. Robust Bayesian Optimal Experimental Design for Data Fusion with Model Discrepancy. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/3006534
• Catanach, Thomas, and Niladri Das. 2024. “Robust Bayesian Optimal Experimental Design for Misspecified Linear and Nonlinear Models.” In SIAM UQ 2024 - Trieste, , Italy - February - 2024. US DOE. https://doi.org/10.2172/2540411
• Cattolica, Robert J. 1993. “Electron Beam Fluorescence Imaging for Hypersonic Research.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_25
• Cavagna, Luca, Sergio Ricci, and Luca Riccobene. 2009b. “A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design.” In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2009-2571. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2571
• Cavagna, Luca, Sergio Ricci, and Lorenzo Travaglini. 2010. “Structural Sizing and Aeroelastic Optimization in Aircraft Conceptual Design Using NeoCASS Suite.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9076. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9076
• Cavolowsky, John, and Mark Newfield. 1992. “Laser Absorption Flow Diagnostics for Use in Hypersonic Ground-Basedand Flight Experiments.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5088
• Cazier, F., Jr., and M. Kehoe. 1986a. “Flight Test of a Decoupler Pylon for Wing/store Flutter Suppression.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9730
• Cazier, F. W., Jr., and M. W. Kehoe. 1986b. “Flight Test of Passive Wing/store Flutter Suppression.” In 1986 Aircraft/Stores Compatibility Symposium. https://ntrs.nasa.gov/citations/19860022096
• Čečrdle, Jiří. 2015. “Experimental Research on Whirl Flutter.” In Whirl Flutter of Turboprop Aircraft Structures. Elsevier. https://doi.org/10.1533/9781782421863.41
• Čečrdle, Jiří. 2018. “Aeroelastic Stability of Turboprop Aircraft: Whirl Flutter.” In Flight Physics - Models, Techniques and Technologies. InTech. https://doi.org/10.5772/intechopen.70171
• Čečrdle, Jiří. 2023. “Experimental Research into Whirl Flutter.” In Whirl Flutter of Turboprop Aircraft Structures. Elsevier. https://doi.org/10.1016/b978-0-323-95555-3.00012-3
• Cenkci, Martha J. 1991. ZEST Flight Test Experiments, Kauai Test Facility, Hawaii. Defense Technical Information Center. https://doi.org/10.21236/ada241143
• Cenko, A. 1992. “Integrating Test Results with Analysis to Improve Safe Separation Flight Tests.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4110
• Cenko, A. 1994. “Analytic Investigation of Wind Tunnel Test Anomalies to Determine Flight Test Envelopes for Safe Store Release.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2610
• Cenko, A. 1999. “F/A-18C/JDAM CFD Challenge Wind Tunnel and Flight Test Results.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-120
• Cenko, A., A. Piranian, and M. Talbot. 1995. “Utilizing Wind Tunnel Test Data and Analysis to Determine Flight Test Envelopes for Safe Store Release.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-328
• Centlivre, Francis A. 2023. “Optimization of Heat Release within a Dual-Mode Ramjet Using Ignition Delay Energy Source Terms.” In AIAA SCITECH 2023 Forum. AIAA 2023-0010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0010
• Cerreta, Peter A. 1957. Wind-Tunnel Investigation of the Drag of a Proposed Boundary-Layer-Controlled Airship. Defense Technical Information Center. https://doi.org/10.21236/ad0127331
• Cesnik, Carlos. 2002. Active Aeroelastic Tailoring of High-Aspect-Ratio Composite Wings. Defense Technical Information Center. https://doi.org/10.21236/ada401331
• Cesnik, Carlos E. 2005. Active Aeroelastic Tailoring of High-Aspect-Ratio Composite Wings. Defense Technical Information Center. https://doi.org/10.21236/ada439640
• Cesnik, Carlos, Miguel Ortega-Morales, and Mayuresh Patil. 2000. “Active Aeroelastic Tailoring of High Aspect Ratio Composite Wings.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1331. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1331
• “CFD Optimization and Test Validation of 2D Ramjet Nozzle for Hypersonic Vehicle.” 1994. In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-2951. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2951
• Chadsey, David, and Thomas Yechout. 2001. “AC-130H Drag Definition Flight Test Program.” In 1st AIAA, Aircraft, Technology Integration, and Operations Forum. AIAA 2001-5262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-5262
• Chakraborty, Imon. 2019. “Design Overview of the Hexa-Chakra Electric Vertical Takeoff and Landing Personal Air Vehicle.” In AIAA Scitech 2019 Forum. AIAA 2019-0554. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0554
• Chaloner, Kathryn. 1984. “Optimal Bayesian Experimental Design for Linear Models.” Annals of Statistics 12 (1): 283–300. https://doi.org/10.1214/aos/1176346407
• Chaloner, Kathryn, and Isabella Verdinelli. 1995. “Bayesian Experimental Design: A Review.” Statistical Science 10 (3): 273–304. https://doi.org/10.1214/ss/1177009939
• Chamberlin, R. 1974. Flight Reynolds Number Effects on a Contoured Boattail Nozzle at Subsonic Speeds. NASA-TM-X-3053. NASA. https://ntrs.nasa.gov/citations/19740013526
• Chamberlin, R., and B. Blaha. 1973. “Flight and Wind Tunnel Investigation of the Effects of Reynolds Number on Installed Boattail Drag at Subsonic Speeds.” In 11th Aerospace Sciences Meeting. AIAA 1973-139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-139
• Chambers, Joseph R. 2000b. Partners in Freedom: Contributions of the Langley Research Center to U.S. Military Aircraft of the 1990’s. NASA/SP-2000-4519. NASA. https://ntrs.nasa.gov/citations/20000115606
• Chambers, Joseph R. 2003. Concept to Reality: Contributions of the Langley Research Center to US Civil Aircraft of the 1990s. NASA/SP-2003-4529. NASA. https://ntrs.nasa.gov/citations/20030059513
• Chambers, Alan, and R. Dale Reed. 1993. Subsonic Airplane for High-Altitude Research. ARC-12822. NASA Ames Research Center, Moffett Field, CA. https://ntrs.nasa.gov/citations/19930000102
• Champagne, G. 1991. “Jet Noise Reduction Concepts for the Supersonic Transport.” In 9th Applied Aerodynamics Conference. AIAA 1991-3328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3328
• Champine, R. 1971. “Flight Investigation of a Tilt-Wing VTOL Aircraft in the Terminal Area under Simulated Instrument Conditions.” In 9th Aerospace Sciences Meeting. AIAA 1971-7. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-7
• Chan, Patrick. 2018. “Fiber Optics Sensing System (FOSS) at NASA Armstrong Flight Research Center (AFRC): Summary and Recent Deployments.” In Edwards Technical Symposium. https://ntrs.nasa.gov/citations/20180007391
• Chan, Wai Lee, and Matthias Ihme. 2014. “Large-Eddy Simulations of a Dual-Mode Scramjet Combustor: Operating Point ‘a’ of University of Virginia’s Scramjet Experiments.” In 52nd Aerospace Sciences Meeting. AIAA 2014-1161. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1161
• Chan, Wai Lee, and Matthias Ihme. 2016. “Analysis of Combustion Closure Assumptions in a Dual-Mode Scramjet Combustor.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1900
• Chan, David T., Gregory S. Jones, William E. Milholen, and Scott L. Goodliff. 2017. “Transonic Drag Reduction through Trailing-Edge Blowing on the FAST-MAC Circulation Control Model.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3246
• Chan, David, Patrick Shea, Scott Goodliff, et al. n.d.-b. “Overview of the High Reynolds Number Ascent Wind Tunnel Test of the Space Launch System at the National Transonic Facility.” In 2023 AIAA SCITECH Forum. https://ntrs.nasa.gov/citations/20220017796
• Chan, David, Anthony Washburn, Sarah Langston, Bryce Moran, Joe Coppin, and Peter Martin. n.d.-a. “High Reynolds Number Testing of the NATO AVT-298 SWiFT Configuration at the National Transonic Facility.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20240015936
• Chana, William F., and T. M. Sullivan. 1993. “The Tilt Wing Design for a Family of High Speed VSTOL Aircraft.” In Proceedings of the Vertical Flight Society Forum 49 - St. Louis, MO 1993. The Vertical Flight Society. https://doi.org/10.4050/vfs-f49-2018
• Chandler, T., and J. Chisholm. 1993. “F405 Engine in-Flight Thrust Methodology Development for the T-45A Flight Test Program.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2544
• Chandrasekhara, M., S. Ahmed, and L. Carr. 1990. “Schlieren Studies of Compressibility Effects on Dynamic Stall of Airfoils in Transient Pitching Motion.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3038. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3038
• Chang, M., P. Trivailo, and L. Plotnikova. 2002. “Active Control of an Aircraft Wing Flutter Suppression Using Piezoelectric Actuators: A Study of Matlab Simulation.” In Structural Stability and Dynamics. WORLD SCIENTIFIC. https://doi.org/10.1142/9789812776228_0125
• Chaowanapreecha, Puwit, and Pitaakphong Rattanagraikanakorn. 2023. “Simulation-Based Design Framework for Supersonic University Sounding Rocket Project.” In 2023 Regional Student Conferences. AIAA 2023-75759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-75759
• Chaplin, Ross. 2013. “RANS CFD Predictions of a Supersonic Jet in a Transonic Crossflow.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2911
• Chapman, Dean R. 1958. An Approximate Analytical Method for Studying Entry into Planetary Atmospheres. NACA-TN-4276. NASA. https://ntrs.nasa.gov/citations/19930085059
• Chapman, Keith B., Gregory T. Dell, Duane L. Rosenberg, and John Bristow. 1999a. Autonomous Formation Flying from Ground to Flight. AI Solutions, Inc. https://ntrs.nasa.gov/citations/19990071192
• Chapman, Keith B., Gregory T. Dell, Duane L. Rosenberg, and John Bristow. 1999b. “Autonomous Formation Flying from the Ground to Flight.” In 1999 Flight Mechanics Symposium. https://ntrs.nasa.gov/citations/19990064187
• Chapman, G., and D. Kirk. 1974. “Nonlinear Parameter Identification: Ballistic Range Experience Applicable to Flight Testing.” In Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017467
• “Chapter 2. Exploring the Flight Envelope.” 2005. In Flight Dynamics. Princeton University Press. https://doi.org/10.1515/9781400866816-003
• “Chapter 5 the Value of Information in Decision Models.” 2004. In Quantitative Techniques for Decision Making in Construction. Hong Kong University Press. https://doi.org/10.1515/9789882202603-006
• “CHAPTER NINE. the Minimum Drag of Thin Wings.” 1990. In Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400860777.159
• Chaput, Armand. 1987. “Preliminary Sizing Methodology for Hypersonic Vehicles.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2954. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2954
• Chaput, Armand. 1989. “International Competition: The NASP Challenge.” In National Aerospace Plane Conference. AIAA 1989-5018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5018
• “Characteristics of the HIEST and Its Applicability for Hypersonic Aerothermodynamic and Scramjet Research.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0239.0253
• Chase, Adam Thomas. n.d. “Flight Testing Small UAVs for Aerodynamic Parameter Estimation.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2014.38
• Chase, R. 1979. “A Comparative Assessment of Reusable Launch-Vehicle Candidates.” In Conference on Advanced Technology for Future Space Systems. AIAA 1979-894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-894
• Chase, Adam, and Robert A. McDonald. 2014. “Flight Testing Small UAVs for Aerodynamic Parameter Estimation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0033
• Chase, Ramon, and Leon McKinney. 2005. “A Least Cost Reusable Operationally Responsive Space Launch Vehicle Demonstrator.” In Space 2005. AIAA 2005-6745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6745
• Chattopadhyay, Aditi, Thomas R. McCarthy, and Sen Zhang. 1995a. “A Coupled Rotor/Wing Optimization Procedure for High Speed Tilt-Rotor Aircraft.” In Proceedings of the Vertical Flight Society Forum 51 - Ft. Worth, TX 1995. The Vertical Flight Society. https://doi.org/10.4050/vfs-f51-2003
• Chattopadhyay, A., J. Narayan, N. Pagaldipti, X. Wensheng, and S. Cheung. 1995b. “Optimization Procedure for Reduced Sonic Boom in High Speed Flight.” In Fluid Dynamics Conference. AIAA 1995-2156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2156
• Chau, Timothy, and Jared C. Duensing. n.d. “Aerodynamic Design Optimization of a Cruise-Slotted Transonic Truss-Braced Wing for Turbulent Flow.” In AIAA Aviation Forum. https://ntrs.nasa.gov/citations/20250006220
• Chaudhari, Bhargav N., and Timothy T. Takahashi. 2022. “Reassessing the B2707-100 Supersonic Transport Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-0776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0776
• Chaudhary, Anmol Krishna Mohan, C. Deepan, A. Latshathipathi, S. R. Arun, and Rakesh Kumar Shah. 2020. “Optimization of a3D Aircraft Morphing Wing with Highly Controllable Aerodynamic Performance.” International Journal of Recent Technology and Engineering (IJRTE) 8 (6): 4295–4300. https://doi.org/10.35940/ijrte.f9141.038620
• Chauffour, Marie-Laure, and Mark Lewis. 2003. “Corrected Shock-Based Design for Waverider Geometries.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7060. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7060
• Chauffour, Marie-Laure, and Mark Lewis. 2004. “Corrected Waverider Design for Inlet Applications.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3405. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3405
• Chaussee, D. 1978. “On the Transonic Flow Field Surrounding Tangent Ogive Bodies with Emphasis on Nose Drag Calculations.” In 16th Aerospace Sciences Meeting. AIAA 1978-212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-212
• Chauvin, L., R. Erb, D. Greenshields, and J. Pavlosky. 1968. “Apollo Thermal-Protection System Development.” In Entry Vehicle Systems and Technology Meeting. AIAA 1968-1142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1142
• Chauvin, Leo T., and Katherine C. Speegle. 1957. Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7. NACA-RM-L57D04. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19660024020
• “Chemical Effects in External Hypersonic Flows.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0205.0254
• “Chemical Kinetic Effects in Hypersonic Flow Introduction: Introduction.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0141.0142
• Chen, F. J., I. E. Beckwith, and T. R. Creel Jr. 1984. Correlations of Supersonic Boundary-Layer Transition on Cones Including Effects of Large Axial Variations in Wind-Tunnel Noise. NASA-TP-2229. NASA. https://ntrs.nasa.gov/citations/19840009466
• Chen, Fang-Jeng, and Scott A. Berry. 2010. HyBoLT Flight Experiment. NASA/TM-2010-216725. NASA. https://ntrs.nasa.gov/citations/20100027425
• Chen, Jianqiang, Siwei Dong, Xi Chen, Xianxu Yuan, and Guoliang Xu. 2021. “Stationary Cross-Flow Breakdown in a High-Speed Swept-Wing Boundary Layer.” Physics of Fluids 33 (2): 024108. https://doi.org/10.1063/5.0039901
• Chen, Xiaomao, and Jinglong Han. 2017. “Aeroelastic Tailoring of High-Aspect-Ratio Composite Joined-Wing UAV.” Mathematical Models in Engineering 3 (1): 41–48. https://doi.org/10.21595/mme.2017.18505
• Chen, Xiaoqing, Zhongxi Hou, He Lietang, and Jianxia Liu. 2008. “Multi-Object Optimization of Waverider Generated from Conical Flow and Osculating Cone.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-131. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-131
• Chen, P., D. Liu, K. Chang, et al. 2006. “Aerothermodynamic Optimization of Hypersonic Vehicle TPS Design by POD/RSM-Based Approach.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-777
• Chen, Xuyang, Xiaoyu Mao, Xinliang Li, and Changping Yu. 2026. “Large Eddy Simulation of Hypersonic Boundary Layer Transition on the Hypersonic Transition Research Vehicle Model Lifting Body at High Angles of Attack.” Physics of Fluids 38 (6): 065140. https://doi.org/10.1063/5.0335632
• Chen, Zhen, Zhiwei Shi, Sinuo Chen, Xueqi Liao, and Yang Mei. 2023b. “Active Flutter Suppression on a Flexible Wing via Leading-Edge Blowing and Circulation Control.” Physics of Fluids 35 (9): 094106. https://doi.org/10.1063/5.0162013
• Chen, Zhen, Zhiwei Shi, Sinuo Chen, Shengxiang Tong, and Yizhang Dong. 2023a. “Active Flutter Suppression for a Flexible Wing Model with Trailing-Edge Circulation Control via Reinforcement Learning.” AIP Advances 13 (1): 015317. https://doi.org/10.1063/5.0130370
• Chen, Wei, and John Valasek. 1999. “Observer/Kalman Filter Identification for on-Line System Identification of Aircraft.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4173
• Chen, Zhenli, and Bingian Zhang. 2006. “A CFD Method of Reducing the Supersonic Drag Basing on the Area Rule Concept.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3334. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3334
• Chen, Zhiqiang, and Yonghui Zhao. 2020. “Active Disturbance Rejection Control for Hypersonic Flutter Suppression Based on Parametric ROM.” Journal of Aerospace Engineering 33 (6): 04020083. https://doi.org/10.1061/(asce)as.1943-5525.0001201
• Chen, Ping-Chih, Zhiqiang Zhou, Satyajit S. Ghoman, and Nathan J. Falkiewicz. 2015. “Low-Weight Low-Drag Truss-Braced Wing Design Using Variable Camber Continuous Trailing Edge Flaps.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1176
• Chen, Xingliang, Shaohua Zhu, Bing Liu, Huamin Zhang, Zongyuan Guo, and Fei Qin. 2024. “Study on Heat Release Characteristics of the Dual Composite Flame Stabilizers for the Dual-Mode Scramjet.” Preprint, . https://doi.org/10.2139/ssrn.4871447
• Cheney, H. 1977. “Analysis Methods and Computer Programs Developed for the YC-15 STOL Flight Test Program.” In Aircraft Systems and Technology Meeting. AIAA 1977-1215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1215
• Cheney, Harold. 1988. “A Flexible Computer Program for Aircraft Flight Test Performance.” In 4th Flight Test Conference. AIAA 1988-2125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2125
• Cheng, Chen, and Xun Huan. 2026. “Optimal Stopping for Sequential Bayesian Experimental Design.” Preprint, . https://doi.org/10.2139/ssrn.6835508
• Cheng, H. K., S. Y. Meng, R. Chow, and R. C. Smith. 1980. “Transonic Swept-Wing Analysis Using Asymptotic and Other Numerical Methods.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800038581
• Chern, Jeng-Shing, Yen-Hsun Chen, and Zuu-Chang Hong. 1994. “Flight Envelopes for Hypersonic Aero-Rendezvous at Constant Altitude.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3472
• Chernyi, G. G., and A. L. Gonor. 1973. “Lifting Body Configurations for Sustained Hypersonic Flight.” In Astronautical Research 1971. Springer Netherlands. https://doi.org/10.1007/978-94-010-2559-1_11
• Cherry, F. 1975. “Composites Technology: Threshold to Low Cost Aircraft Structures.” In Aircraft Systems and Technology Meeting. AIAA 1975-1006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1006
• Chetty, Shyam, and J. Raol. 1992. “Computer Aided Evaluation of Aircraft Handling Qualities and Flight Control System Robustness.” In Guidance, Navigation and Control Conference. AIAA 1992-4423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4423
• Cheung, Samson. 1993. Supersonic Airplane Study and Design. NASA-CR-193219. NASA. https://ntrs.nasa.gov/citations/19940006678
• Chevalier, H., J. Brown, and R. Wilke. 1974. “A Method for Preventing Airplane Stall/spin.” In Mechanics and Control of Flight Conference. AIAA 1974-863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-863
• Chew, Weikang. n.d. “Stagnation Point Radiation Measurement for Re-Entry Heating.” PhD diss., The University of Queensland. https://doi.org/10.14264/369006
• Childs, Joan M. 1953. Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Deg Sweepback. NACA-RM-L52K13b. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930087404
• Chin, Alexander Wong. n.d. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2011.43
• Chin, J. 1970. The Application of MIL-F-8785B (ASG) to the Evaluation of Landing-Approach Flying Qualities of a Lifting-Body-Type Shuttle Vehicle. Grumman Aerospace Corp. https://ntrs.nasa.gov/citations/19700028517
• Chin, Alexander, Martin Brenner, and Marlin Pickett. 2011. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6206. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6206
• Chin, J., V. Chacon, and J. Gera. 1987. “X-29A Flight Control System Performance during Flight Test.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2878
• Chin, W. C., and D. P. Rizzetta. 1979. “Airfoil Design in Subcritical and Supercritical Flows.” Journal of Applied Mechanics 46 (4): 761–66. https://doi.org/10.1115/1.3424650
• Chinvorarat, Sinchai, Boonchai Watjatrakul, Pongsak Nimdum, Teerawat Sangpet, and Pumyos Vallikul. 2024. “Flight Test Stall Analysis of a Light Amphibious Airplane with NACA 2412 Wing Airfoil.” In AIP Conference Proceedings, vol. 3236. AIP Publishing. https://doi.org/10.1063/5.0237061
• Chipman, R., F. Rauch, M. Rimer, and B. Muniz. 1984. Body-Freedom Flutter of a 1/2-Scale Forward-Swept-Wing Model, an Experimental and Analytical Study. NASA-CR-172324. NASA. https://ntrs.nasa.gov/citations/19840013485
• Chipman, R., F. Rauch, M. Rimer, B. Muniz, and R. Ricketts. 1985. “Transonic Test of a Forward Swept Wing Configuration Exhibiting BodyFreedom Flutter.” In 26th Structures, Structural Dynamics, and Materials Conference. AIAA 1985-689. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-689
• Cho, Yongseung, M. Nagati, and Paul Jaramillo. 1995. “Parameter Estimation with a Multi-Point Model (for Analysis of Aircraft Aerodynamic Characteristics).” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3498
• Choi, JaeWon, ByeongUk Lim, SiHun Lee, and SangJoon Shin. 2020. “Aeroelastic Tailoring of a Forward-Swept Wing Using One-Dimensional Beam Analysis.” Journal of the Korean Society for Aeronautical & Space Sciences 48 (8): 555–63. https://doi.org/10.5139/jksas.2020.48.8.555
• Chokani, Ndaona. 2000. “Wave Modulation in the Transition of a Hypersonic Boundary Layer Flow.” In Fluids 2000 Conference and Exhibit. AIAA 2000-2653. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2653
• Choosak Ngaongam and Rapee Ujjin. 2024. “Aerodynamic Characteristics of Forward Swept Wing in Subsonic Speed.” CFD Letters 16 (5): 1–8. https://doi.org/10.37934/cfdl.16.5.18
• Chopra, Inderjit, and Ranjan Ganguli. 1993. “Aeroelastic Optimization of a Helicopter Rotor with Composite Tailoring.” In Proceedings of the Vertical Flight Society Forum 49 - St. Louis, MO 1993. The Vertical Flight Society. https://doi.org/10.4050/vfs-f49-2043
• Chou, D. C., J. H. Baek, R. W. Luiden, and N. O. Stockman. 1981. “Scale Effects on Turbulent Boundary Layer Development and Flow Separation around V/STOL Inlets at High Incidence.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19810036134
• Chou, Amanda, and Eric C. Marineau. 2024. A Summary of the 2023 Joint High-Speed Boundary Layer Transition Workshop. Langley Research Center. https://ntrs.nasa.gov/citations/20240005810
• Chou, Amanda, Eric C. Marineau, and Douglas R. Smith. n.d. “Joint AFOSR/ONR/NASA HTP Boundary Layer Transition Workshop Summary for RAeS.” In Royal Aeronautical Society Specialist Group Conference on High-Speed Aerodynamics - Towards Hypersonic Flight. https://ntrs.nasa.gov/citations/20230013048
• Chou, David C., and Theodore F. Smith. 1974. Aerodynamic Heating of Supersonic Blunt Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada001135
• Choubey, Gautam, and Manvendra Tiwari. 2022a. “Advances in Scramjet Fuel Injection Technology.” In Scramjet Combustion. Elsevier. https://doi.org/10.1016/b978-0-323-99565-8.00005-7
• Choubey, Gautam, and Manvendra Tiwari. 2022b. “Factors Affecting the Scramjet Performance.” In Scramjet Combustion. Elsevier. https://doi.org/10.1016/b978-0-323-99565-8.00002-1
• Choubey, Gautam, and Manvendra Tiwari. 2022c. “Scramjet Combustion Mechanism.” In Scramjet Combustion. Elsevier. https://doi.org/10.1016/b978-0-323-99565-8.00006-9
• Choudhury, Mushrif, Jie Cui, and Vahid Motevalli. 2020. “Effects of Supercritical Airfoil Upper Camber Modification on Overall Airfoil Performance.” In World Congress on Momentum, Heat and Mass Transfer. Avestia Publishing. https://doi.org/10.11159/enfht20.02
• Chow, W. L. 1979. Separated Flow Problems within the Transonic and Supersonic Flow Regimes. Defense Technical Information Center. https://doi.org/10.21236/ada071899
• Chow, L., and P. Goorjian. 1982. “Implicit Unsteady Transonic Airfoil Calculations at Supersonic Freestreams.” In 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference. AIAA 1982-934. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-934
• Chowdhary, Abhijit, Ahmed Attia, and Alen Alexanderian. 2026. “Robust Optimal Experimental Design of Infinite-Dimensional Bayesian Nonlinear Inverse Problems.” SIAM Journal on Scientific Computing 48 (2): B262-B288. https://doi.org/10.1137/24m1693921
• Chowdhary, Girish, and Ravindra Jategaonkar. 2006. “Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6146
• Christiansen, R. S. 1984. A Large-Scale Investigation of V/STOL Ground Effects. AIAA PAPER 84-0336. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19840035242
• Chudoba, Bernd, and Michael Cook. 2003. “Identification of Design-Constraining Flight Conditions for Conceptual Sizing of Aircraft Control Effectors.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5386. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5386
• Chun, Jaechul, Tobias Scheuermann, Jens von Wolfersdorf, and Bernhard Weigand. 2006. “Experimental Study on Combustion Mode Transition in a Scramjet with Parallel Injection.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8063
• Chun, K., and D. Swanson. 1964. “Dynamic Simulation of Supersonic Inlet and Engine.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-598
• Chung, P. M., and G. Goodwin. 1962. Effects of Nonequilibrium Flows on Aerodynamic Heating during Entry into the Earth’s Atmosphere from Parabolic Orbits. NASA. https://ntrs.nasa.gov/citations/19630026626
• Chung, Victoria I., and Brian K. Hutchinson. 2001. A Unique Software System for Simulation-to-Flight Research. AIAA Paper 2001-4057. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010098605
• Churchward, Rex, R. Piquette, D. Smith, M. Arnold, and Daniel J. Rasky. 1998. Ceramic Fairings for a Hypersonic Flight Experiment. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020053708
• Cicolani, Luigi S., Allen H. McCoy, Mark B. Tischler, George E. Tucker, Pinhas Gatenio, and Dani Marmar. 1999. “Flight-Time Identification of a UH-60A Helicopter and Slung Load.” In System Identification for Integrated Aircraft Development and Flight Testing. https://ntrs.nasa.gov/citations/19990032457
• Cipollini, Francesca, and Jean-Marie Muylaert. 2006. “European Activities on Advanced Flight Measurement Techniques for Hypersonic Space Vehicles.” In 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2006-3832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3832
• Clark, J. 1964. “Research on Vtol Aircraft Handling Qualities Criteria.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-618
• Clark, Frank B. 1980. “A Hybrid Composite Horizontal Stabilizer for the XH-2/CCR Flight Demonstrator Aircraft.” In Proceedings of the Vertical Flight Society Forum 36 - Washington, D.C. 1980. The Vertical Flight Society. https://doi.org/10.4050/vfs-f36-035
• Clark, James W., David P. Miller, and Robert A. Gallant. 1963. Investigation of Control and Stability Augmentation Requirements for Tandem Tilting Ducted Propeller VTOL Transports. Defense Technical Information Center. https://doi.org/10.21236/ad0419126
• Clark, E., Jr. 1970. “The Effects of Products of Inertia on the Roll Behavior of Ballisticre-Entry Vehicles.” In 8th Aerospace Sciences Meeting. AIAA 1970-204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-204
• Clarke, Robert, Michael Allen, Ryan Dibley, Joseph Gera, and John Hodgkinson. 2005. “Flight Test of the F/A-18 Active Aeroelastic Wing Airplane.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6316
• Clarke, Robert, John J. Burken, John T. Bosworth, and JEffrey E. Bauer. 2018. “X-29 Flight Control System: Lessons Learned.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-13
• Clarke, R., and J. Roskam. 1982. “A Simple, Low Cost Application of a Flight Test Parameter Identification System.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1312
• Clarke, R., D. Shane, J. Roskam, and D. I. Rummer. 1982. Development of a Simple, Self-Contained Flight Test Data Acquisition System. NASA-CR-168912. NASA. https://ntrs.nasa.gov/citations/19820015371
• Cleary, Joseph W., and Lyle J. Gray. 1947. High-Speed Wind-Tunnel Tests of a Model of the Lockheed YP-80A Airplane Including Correlation with Flight Tests and Tests of Dive-Recovery Flaps. NACA-RM-A7A29. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019287
• Clement, W. F., W. B. Cleveland, and D. L. Key. 1984. “Assessment of Simulation Fidelity Using Measurements of Piloting Technique in Flight.” In AGARD Helicopter Guidance and Control Systems for Battlefield Support. https://ntrs.nasa.gov/citations/19850008508
• Cliatt, Larry J., Edward A. Haering, Thomas P. Jones, Erin R. Waggoner, Ashley K. Flattery, and Scotty L. Wiley. 2014. “A Flight Research Overview of WSPR, a Pilot Project for Sonic Boom Community Response.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2268. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2268
• Cliett, Charles B. 1952. Structural Considerations of Perforated Materials Used in Boundary Layer Control: And Appendix: Low-Speed-Flight Research Program. Defense Technical Information Center. https://doi.org/10.21236/ad0006050
• Cliff, Susan E., Marie Denison, Shayan Moini-Yekta, Donald E. Morr, and Donald A. Durston. 2016a. “Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flows with Shock Interactions.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160004757
• Cliff, Susan E., Marie Denison, Emre Sozer, and Shayan Moini-Yekta. 2016b. “Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet with Shock Interactions.” In Scitech. https://ntrs.nasa.gov/citations/20160000294
• Cliff, Eugene, Klaus-H. Well, and Klaus Schnepper. 1992. “Flight-Test Guidance for Airbreathing Hypersonic Vehicles.” In Guidance, Navigation and Control Conference. AIAA 1992-4301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4301
• Clough, Bruce. 1990. “Short Take-off and Landing Maneuver Technology Demonstrator (STOL/MTD) Lessons Learned: Integrated Flight/propulsion Control (IFPC).” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3307
• Clousing, Lawrence A. 1946. Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-Type Airplane as Measured in Flight. NACA-WR-A-60. NASA. https://ntrs.nasa.gov/citations/19930092569
• Clousing, L. A. 1964. Some Comparisons of Aircraft Flight Characteristics with Those Shown by Ground Simulation. NASA-TM-X-51994. NASA. https://ntrs.nasa.gov/citations/19650019783
• Coakley, Janet M. n.d. “Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2011.26
• Cobham, Alan, and Marcus Langley. 1940. “The History and Progress of Refuelling in Flight.” Journal of the Royal Aeronautical Society 44 (355): 557–603. https://doi.org/10.1017/s0368393100103438
• Cobleigh, Brent R., and Mark A. Croom. 2001. Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack. NASA/TM-2001-210393. NASA. https://ntrs.nasa.gov/citations/20010055264
• Cobleigh, Brent, and Mark A. Croom. 2003. “Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack.” In Symposium on Advanced Flow Management. Part A: Vortex Flows and High Angle of Attack for Military Vehicles. Part B: Heat Transfer and Cooling in Propulsion and Power Systems. https://ntrs.nasa.gov/citations/20040040219
• Cobleigh, Brent R., Mark A. Croom, and B. F. Tamrat. 1994. “Comparison of X-31 Flight, Wind-Tunnel, and Water-Tunnel Yawing Moment Asymmetries at High Angles of Attack.” In Fourth High Alpha Conference: Volume 1. https://ntrs.nasa.gov/citations/19950007820
• Cobo-González, Álvaro, Rodney Rodríguez-Robles, and Cristina Cuerno-Rejado. 2026. “Recent Advances in Active Flutter Suppression: A Comprehensive Review.” Aeronautical Journal: 1–43. https://doi.org/10.1017/aer.2026.10212
• Cocco, Alessandro, and Mattia Meroli. 2026. “Multifidelity Aeroelastic Framework for Predicting Trim of Fixed and Rotary Wing Aircraft.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0187
• Cochrane, J. A., and A. G. Boissevain. 1978. “Quiet, Short-Haul Research Aircraft: Current Status and Future Plans.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780064007
• Cochrane, John, and Kenneth Graham. 1971. “Pilot Safety for the X-24A Lifting Body Vehicle.” In Proceedings of the NASA Government-Industry System Safety Conference. https://ntrs.nasa.gov/citations/19720018319
• Cochrane, J. A., D. W. Riddle, and V. C. Stevens. 1981. “Quiet Short-Haul Research Aircraft: The First 3 Years of Flight Research.” In V/STOL Conference. https://ntrs.nasa.gov/citations/19820035674
• Cocking, B., and W. Bryce. 1975. “Subsonic Jet Noise in Flight Based on Some Recent Wind-Tunnel Tests.” In 2nd Aeroacoustics Conference. AIAA 1975-462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-462
• Cockrell, Charles E., Jr., Walter C. Engelund, Robert D. Bittner, Arthur D. Dilley, Tom N. Jentink, and Abdelkader Frendi. 2000. Integrated Aero-Propulsion CFD Methodology for the Hyper-X Flight Experiment. AIAA Paper 2000-4010. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000091003
• Coder, James G., and Sven Schmitz. 2019. “Thermodynamic Decomposition of Compressible Wave Drag in the Euler Equations.” In AIAA Aviation 2019 Forum. AIAA 2019-2958. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2958
• Coe, Charles F. 1985. An Assessment of Wind Tunnel Test Data on Flexible Thermal Protection Materials and Results of New Fatigue Tests of Threads. NASA-CR-177466. NASA. https://ntrs.nasa.gov/citations/19910004659
• Coe, Paul, Jr., and John Perkins. 1990. “Exploratory Wind Tunnel Investigation of the Stability and Control Characteristics of a Three-Surface, Forward-Swept Wing Advanced Turboprop Model.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3074
• Cohan, S., and N. B. Hirsh. 1966. XV-9A Hot Cycle Research Aircraft Program. Defense Technical Information Center. https://doi.org/10.21236/ad0638366
• Cohen, M. 1970. “Comparison of Wind Tunnel and Flight Test Techniques for Determiningtransonic Buffet Characteristics on the McDonnell Douglas F-4 Airplane.” In Propulsion and ASW Meeting. AIAA 1970-584. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-584
• Cohen, Dorothea, and Jeanette H. Le. 1991. “The Role of the Remotely Augmented Vehicle (RAV) Laboratory in Flight Research.” In AIAA Flight Simulation Technologies Conference. https://ntrs.nasa.gov/citations/19910063181
• Coiro, D., P. De Matteis, and M. Amato. 1990. “Wake Effects on the Prediction of Transonic Viscous Flows around Airfoils with an Euler/boundary Layer Interaction Approach.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3061. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3061
• Coker, M. J., J. B. Hoffman, and J. H. Lawrence Jr. 1978. Windshield Technology Demonstrator Program-Canopy Detail Design Options Study. Defense Technical Information Center. https://doi.org/10.21236/ada070376
• Cole, S. 1986. “Divergence Study of a High-Aspect Ratio, Forward-Swept Wing.” In 24th Aerospace Sciences Meeting. AIAA 1986-9. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9
• Cole, Jennifer H., Frank Batteas, and Gordon Fullerton. 2006. “Aircraft Control Using Engine Thrust: A History of Learning TOC Real-Time.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20060048250
• Cole, Jennifer H., Bruce R. Cogan, C. Gordon Fullerton, John J. Burken, Michael W. Venti, and Frank W. Burcham. 2007. Emergency Flight Control of a Twin-Jet Commercial Aircraft Using Manual Throttle Manipulation. DFRC-650. NASA Dryden Flight Research Facility. https://ntrs.nasa.gov/citations/20090009358
• Cole, John N., and Robert T. England. 1967. Evaluation of Noise Problems Anticipated with Future VTOL Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0658448
• Coles, Darrell, and Michael Prange. 2012. “Toward Efficient Computation of the Expected Relative Entropy for Nonlinear Experimental Design.” Inverse Problems 28 (5): 055019. https://doi.org/10.1088/0266-5611/28/5/055019
• Colgren, Richard. 1996. “Results of the U-2 Autopilot and Air Data System (APADS) Development and Flight Test Program.” In Guidance, Navigation, and Control Conference. AIAA 1996-3743. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3743
• Collar, A. R. 1946. “The Expanding Domain of Aeroelasticity.” Journal of the Royal Aeronautical Society 50 (428): 613–36. https://doi.org/10.1017/s0368393100120358
• Collercandy, Ranjit. 1992. “An Improved Approach for the Computation of Transonic/supersonic Flows with Applications to Aerospace Configurations.” In 10th Applied Aerodynamics Conference. AIAA 1992-2613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2613
• Collier, F., Jr. 1993. “An Overview of Recent Subsonic Laminar Flow Control Flight Experiments.” In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. AIAA 1993-2987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2987
• Collier, F. S., Jr., D. W. Bartlett, R. D. Wagner, V. V. Tat, and B. T. Anderson. 1990. “Correlation of Boundary Layer Stability Analysis with Flight Transition Data.” In IUTAM Symposium on Laminar-Turbulent Transition. https://ntrs.nasa.gov/citations/19910055306
• Collins, I. K., R. L. Stallings Jr., and R. L. Wright. 1970. Experimental Heat-Transfer Distributions on a Blunt Lifting Body at Mach 3.71. NASA-TN-D-5616. NASA. https://ntrs.nasa.gov/citations/19700009652
• Colonno, Michael, and Juan Alonso. 2010. “Sonic Boom Minimization Revisited: The Robustness of Optimal Low-Boom Designs.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9364
• “Combined Flight Control/utility System.” 1974. Aircraft Engineering and Aerospace Technology 46 (3): 12–17. https://doi.org/10.1108/eb035139
• Combs, H. G. 1976. Configuration Development Study of the X-24C Hypersonic Research Airplane, Phase 1. NASA-CR-145032. NASA. https://ntrs.nasa.gov/citations/19790007768
• Combs, H. G. 1977. Configuration Development Study of the X-24C Hypersonic Research Airplane, Phase 3. NASA-CR-145103. NASA. https://ntrs.nasa.gov/citations/19790008669
• Comer, Anthony M., Zach Atkinson, Pratibha Bhandari, Zachary Miller, and Elijah Harp. 2026a. “Development of a Simulation to Flight Workflow for Subscale Flight Testing of Experimental Control Laws.” In AIAA SCITECH 2026 Forum. AIAA 2026-2063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2063
• Comer, Anthony M., Rajan Bhandari, Stefanus H. Putra, and Imon Chakraborty. 2024. “Design, Control Law Development, and Flight Testing of a Subscale Lift-Plus-Cruise Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-2644. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2644
• Comer, Anthony M., Benjamin M. Simmons, and Garrett D. Asper. 2025. Design, Simulation, and Flight Testing of a Multi-Purpose VTOL Flight Control System. OSTEM Internship Program, Langley Research Center. https://ntrs.nasa.gov/citations/20250000954
• Comey, D. H., D. G. Culy, and J. E. Cassidy. 1978. “Trade-Off Studies with an Interactive Engine/Airframe Life-Cycle-Cost Model.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/781033
• “Communications Flight Test.” 2010. In Test and Evaluation of Aircraft Avionics and Weapons Systems. Institution of Engineering and Technology. https://doi.org/10.1049/sbra033e_ch4
• “Comparison of Aircraft Noise Measured in Flight Test and in a NASA Ames Wind Tunnel.” 1975. In Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865121.0493.0506
• “Comparison of Static Aerodynamic Data Obtained in Dynamic Wind Tunnel Tests and Numerical Simulation Research.” 2018. Tehnicki vjesnik - Technical Gazette 25 (2). https://doi.org/10.17559/tv-20161221140914
• Compton, H., W. Scallion, J. Schiess, and W. Suit. 1982. “Shuttle Entry Performance and Stability and Control Derivatives Extraction from Flight Measurement Data.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1317. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1317
• Compton, William, III, and Khaled Abdol-Hamid. 1990. “Navier-Stokes Simulation of Transonic Afterbody Flows with Jet Exhaust.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3057
• “Computational Analysis of Combustion in Recirculating Flow for Rocket Exhausts in Supersonic Streams.” 1981. In 17th Joint Propulsion Conference. AIAA 1981-1386. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1386
• “Computational and Experimental Study of Kinetic Heating at Hypersonic Speeds.” 1993. In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5022
• Comunian, Paolo, Jacopo Serpieri, and Gioacchino Cafiero. 2025. “Optimizing Distributed Electric Propulsion Throughgenetic Algorithms.” Preprint, . https://doi.org/10.2139/ssrn.5304787
• Condon, G. W. 1975. “Rotor Systems Research Aircraft (RSRA) Requirements for, and Contributions to, Rotorcraft State Estimation and Parameter Identification.” In AGARD Methods for Aircraft State and Parameter Identification. https://ntrs.nasa.gov/citations/19750021949
• Condon, G. W., and R. Letchworth. 1976. “Rotor Systems Research Aircraft (RSRA).” In AGARD Flight(Ground Testing Fac. Correlation. https://ntrs.nasa.gov/citations/19760018198
• Conners, Timothy. 1989. “Measurement Effects on the Calculation of in-Flight Thrust for an F404 Turbofan Engine.” In 25th Joint Propulsion Conference. AIAA 1989-2364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2364
• Conners, Timothy, and Robert Sims. 1998. “Full Flight Envelope Direct Thrust Measurement on a Supersonic Aircraft.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3872. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3872
• Conners, Timothy, and Thomas Wayman. 2011. “The Feasibility of High-Flow Nacelle Bypass for Low Sonic Boom Propulsion System Design.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3797. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3797
• Connolly, Brian J., Charles R. Krouse, and Grant O. Musgrove. 2021. “Implementing a Dual-Mode Scramjet Combustor Model in NPSS.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3538. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3538
• “Continuing to Push the State-of-the-Art: The Gathering Consensus on Hypersonic Flight, May 1955–October 1957.” 2006. In US Hypersonic Research and Development. Routledge. https://doi.org/10.4324/9780203012994-10
• Control Allocation and Flight Control System Design. 2016. Wiley. https://doi.org/10.1002/9781118827789.ch8
• Cook, Stephen. 1995a. “The Reusable Launch Vehicle Technology Program.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6153
• Cook, Stephen A. 1995b. The Reusable Launch Vehicle Technology Program and the X-33 Advanced Technology Demonstrator. NASA-TM-111868. NASA. https://ntrs.nasa.gov/citations/19960045833
• Cook, Stephen. 1996. “X-33 Reusable Launch Vehicle Structural Technologies.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4563
• Cook, M. V. 1997. “Aerodynamic Stability and Control Derivatives.” In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-340-63200-0.50018-6
• Cook, M. V. 2007. “Aerodynamic Stability and Control Derivatives.” In Flight Dynamic Principles. Elsevier. https://doi.org/10.1016/b978-075066927-6/50016-7
• Cook, Michael V. 2013. “Aerodynamic Stability and Control Derivatives.” In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-08-098242-7.00013-4
• Cook, S., J. Cross, and M. Hoffbauer. 1994. “Hypersonic Gas-Surface Energy Accommodation Test Facility.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2637
• Cook, W. L., and D. H. Hickey. 1965. Correlation of Wind-Tunnel and Flight-Test Aerodynamic Data for Five V/STOL Aircraft. AGARD-520. NASA AMES RES. CENTER. https://ntrs.nasa.gov/citations/19670020207
• Cook, W. L., and D. H. Hickey. 1975. Correlation of Low Speed Wind Tunnel and Flight Test Data for V/STOL Aircraft. NASA-TM-X-62423. NASA. https://ntrs.nasa.gov/citations/19750015485
• Cook, W. L., and D. H. Hickey. 1976. “Correlation of Low Speed Wind Tunnel and Flight Test Data for V/STOL Aircraft.” In AGARD Flight(Ground Testing Fac. Correlation. https://ntrs.nasa.gov/citations/19760018205
• Cook, A. M., R. C. Innis, and L. S. Rolls. 1969. Flight-Determined Aerodynamic Properties of a Jet-Augmented, Auxiliary-Flap, Direct-Lift- Control System Including Correlation with Wind-Tunnel Results. NASA-TN-D-5128-REV. NASA. https://ntrs.nasa.gov/citations/19690022584
• Cook, W. L., and D. C. Whittley. 1975. Comparison of Model and Flight Test Data for an Augmented Jet Flap STOL Research Aircraft. NASA-TM-X-62491. NASA. https://ntrs.nasa.gov/citations/19760003005
• Cook, W. L., and D. C. Whittley. 1976. “Comparison of Model and Flight Test Data for an Augmentor-Wing STOL Research Aircraft.” In AGARD Flight(Ground Testing Fac. Correlation. https://ntrs.nasa.gov/citations/19760018204
• Cooke, D. 1980a. “Space Shuttle Stability and Control Flight Test Techniques.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1608
• Cooke, D. 1980b. “Subsonic Stability and Control Flight Test Results of the Space Shuttle /Tail Cone Off/.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1604
• Cooke, D. 1982. “Space Shuttle Stability and Control Test Plan.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1315
• Cooke, Douglas R., and Joe H. Engle. 2016. “Entry Flight Testing the Space Shuttle, 1977 to 1984.” In AIAA Flight Testing Conference. AIAA 2016-3357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3357
• Cooksey, J. M., P. G. Dillenschneider, and R. D. Meyer. 1964. “Wind Tunnel-Flight Dynamics Simulator.” In Aerodynamic Testing Conference. AIAA 1964-1108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-1108
• Coombe, A. J. 1970. “Flight Testing the Islander: A Description of the Early Flight Test Development of the Aircraft.” Aircraft Engineering and Aerospace Technology 42 (8): 15–27. https://doi.org/10.1108/eb034670
• Cooney, T. V. 1952. The Vertical-Tail Loads Measured during a Flight Investigation on a Jet-Powered Bomber Airplane. NACA-RM-L52G21. NASA. https://ntrs.nasa.gov/citations/19930087215
• Coons, L. 1986. “Propulsion Challenges for Hypersonic Flight.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2620
• Coons, Thomas E., and Xun Huan. 2025. “A Multifidelity Estimator of the Expected Information Gain for Bayesian Optimal Experimental Design.” SIAM/ASA Journal on Uncertainty Quantification 13 (4): 1990–2021. https://doi.org/10.1137/25m1731812
• Corcau, Jenica-Ileana, Liviu Dinca, and Ciprian-Marius Larco and Cristian Vidan. 2026. “Hybrid-Electric Distributed Propulsion with Fuel Cell Integration: Architecture and System-Level Analysis for Commuter Aircraft.” In Distributed Generation - Technologies, Control and Applications [Working Title]. IntechOpen. https://doi.org/10.5772/intechopen.1016437
• Cord, T. 1989. “A Standard Evaluation Maneuver Set for Agility and the Extended Flight Envelope: An Extension to HQDT.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3357
• Corda, Stephen. 1995. “Dynamic Ground Effects Flight Test of the NASA F-15 Aircraft.” In NASA. Dryden Flight Research Center, An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program. https://ntrs.nasa.gov/citations/19950026603
• Corda, Stephen, Timothy R. Moes, Masashi Mizukami, et al. 2000. The SR-71 Test Bed Aircraft: A Facility for High-Speed Flight Research. NASA/TP-2000-209023. NASA. https://ntrs.nasa.gov/citations/20000064011
• Corda, Stephen, M. Jake Vachon, Nathan Palumbo, et al. 2001. The F-15B Propulsion Flight Test Fixture: A New Flight Facility for Propulsion Research. NASA/TM-2001-210395. NASA. https://ntrs.nasa.gov/citations/20030093544
• Corke, Thomas C., and Rodney D. Bowersox. 2018. “Hypersonic Boundary Layer Cross Flow Transition: Characteristics and Control.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0352
• Cornelison, Charles J., and James O. Arnold. 1997. Status Report for the Hypervelocity Free-Flight Aerodynamic Facility. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020048460
• Corsiglia, Victor R., Douglas A. Wardwell, and Richard E. Kuhn. 1990. Small-Scale Experiments in STOVL Ground Effects. SAE PAPER 901060. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19910036633
• Corsiglia, Victor R., Douglas A. Wardwell, and Richard E. Kuhn. 1991. “Small-Scale Experiments in STOVL Ground Effects.” In RAS International Powered Life Conference. https://ntrs.nasa.gov/citations/19910012778
• Cosenito, Gary B. 2010. “Flight Testing the X-48B at the Dryden Flight Research Center.” In University of Arizona Aerospace and Mechanical Engineering. https://ntrs.nasa.gov/citations/20100040481
• Cosentino, Gary. 2006. “NASA Dryden UAS Perspective.” In Unmanned Aerial Vehicles Platforms, Payloads and Opportunities. https://ntrs.nasa.gov/citations/20060047626
• Cosentino, Gary B. 2007. “CFD to Flight: Some Recent Success Stories of X-Plane Design to Flight Test at the NASA Dryden Flight Research Center.” In 2007 ITEA Symposium. https://ntrs.nasa.gov/citations/20080007530
• Cosentino, Gary B. 2008. Computational Fluid Dynamics Analysis Success Stories of X-Plane Design to Flight Test. NASA/TM-2008-214636. NASA. https://ntrs.nasa.gov/citations/20080022273
• Cosentino, Gary B. 2009. “UAV Research, Operations, and Flight Test at the NASA Dryden Flight Research Center.” In UCSD Seminar. https://ntrs.nasa.gov/citations/20090033637
• Cosgrove, W. J., and P. E. Ryan. 1969. Empirically Determined Wind and Scale Effects on Hot Gas Recirculation Characteristics of Jet V/STOL Aircraft. NASA-CR-1445. NASA. https://ntrs.nasa.gov/citations/19690031387
• “Cost of Aircraft.” 2016. In Why Can’t We Make Money in Aviation?. Routledge. https://doi.org/10.4324/9781315547244-7
• Costa, Guillermo J., and Ricardo A. Arteaga. 2011. Asset Analysis and Operational Concepts for Separation Assurance Flight Testing at Dryden Flight Research Center. DFRC-E-DAA-TN2188. California State Polytechnic Univ. https://ntrs.nasa.gov/citations/20110008317
• Costa, R., J. Silva, S. Wu, Q. Chu, and J. Mulder. 2000. “Atmospheric Re-Entry Modeling and Simulation: Application to the Crew Return Vehicle.” In Modeling and Simulation Technologies Conference. AIAA 2000-4086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4086
• Cotton, L. S. 1974. Three-Axis Fluidic/Electronic Automatic Flight Control System Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ada000894
• Couch, L. M., and W. D. Morris. 1968. Experimental Pressure Distributions on a Blunt Lifting-Entry Body at Mach 3.71. NASA-TN-D-4494. NASA. https://ntrs.nasa.gov/citations/19680012212
• Coulouvrat, Francois. 1998. “Sonic Boom beyond the Carpet Edge.” In 4th AIAA/CEAS Aeroacoustics Conference. AIAA 1998-2247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2247
• Coulouvrat, F. 2022. “Sonic Boom More than Two Centuries of Investigation.” In Inter-Noise 2022. Institute of Acoustics. https://doi.org/10.25144/14336
• Courtin, Christopher, R. John Hansman, and Mark Drela. 2020. “Flight Test Results of a Subscale Super-STOL Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-0977. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0977
• Covington, M. 1966. “A Technique for Measuring Mesospheric Densities with the X-15 Research Airplane.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-441
• Cox, Brian. 2009. “Intelligent Combat Maneuvers for Unmanned Combat Air Vehicles.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2009-01-3098
• Cox, Franklin D., and George A. Bobula. 2015. Test Record of Flight Tests Using Alcohol-to-Jet/JP-8 Blended Fuel. Defense Technical Information Center. https://doi.org/10.21236/ada622291
• Cox, David, Kevin Cunningham, and Geoff Brian. n.d. “AirSTAR: Simulation and Reduced-Scale Flight Test Facility.” In Flight Test Society of Australia Symposium 2011. https://ntrs.nasa.gov/citations/20200004807
• Cox, David, Kevin Cunningham, and Thomas Jordan. 2012. “Subscale Flight Testing for Aircraft Loss of Control: Accomplishments and Future Directions.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-5029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5029
• Cox, C., C. Lewis, R. Pap, et al. 1995. “Prediction of Unstart Phenomena in Hypersonic Aircraft.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6018
• Cox, Timothy H., and Alisa Marshall. 2000. Longitudinal Handling Qualities of the Tu-144LL Airplane and Comparisons with Other Large, Supersonic Aircraft. NASA/TM-2000-209020. NASA. https://ntrs.nasa.gov/citations/20000052206
• Cox, Brian, and Jan Roskam. 1990. “Preliminary Design of a Supersonic Short Takeoff and Vertical Landing (STOVL) Fighter Aircraft.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3231. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3231
• Craig, R., and R. Reich. 1981. “Flight Test Aerodynamic Drag Characteristics Development and Assessment of in-Flight Propulsion Analysis Methods for the AGM-109 Cruise Missile.” In 1st Flight Test Conference. AIAA 1981-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2423
• Crain, W. K., C. L. Frost, and C. D. Engel. 1989. SRB Ascent Aerodynamic Heating Design Criteria Reduction Study, Volume 1. NASA-CR-183580. NASA. https://ntrs.nasa.gov/citations/19890014144
• Crane, H. L., M. D. McLaughlin, and J. A. White. 1959. Comparison of Control-Fixed Stability Derivatives for Two Supersonic Fighter Airplanes as Determined from Flight and Wind-Tunnel Tests. NASA-MEMO-2-3-59L. NASA. https://ntrs.nasa.gov/citations/19660022438
• Crassidis, Agamemnon. 2005. “Nonlinear Identification Update of an Air-Data System Using Experimental Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-5919. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5919
• Crawford, Kevin, and John Thomas. 2006. “Developmental Flight Instrumentation System for the Crew Launch Vehicle.” In International Telemetering Conference. https://ntrs.nasa.gov/citations/20070002018
• Creagh, Michael, Peter Beasley, Igor Dimitrijevic, Melrose Brown, and Sandy Tirtey. 2012. “A Kalman-Filter Based Inertial Navigation System Processor for the SCRAMSPACE 1 Hypersonic Flight Experiment.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5894
• Creating Hypersonic Flow in Flight. 2019. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105142.0829.0836
• Crippa, Simone, and Arthur Rizzi. 2008. “Steady, Subsonic CFD Analysis of the VFE-2 Configuration and Comparison to Wind Tunnel Data.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-397
• Crites, R., M. Rueger, D. Evans, and S. Lehman. 1992. “Comparison of Transonic Wind Tunnel and Flight Data for a High Performance Fighter Aircraft.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3983. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3983
• Crogan, Leonard E. 1961. Drag and Stability Data for Several SAMOS Configurations Obtained from Free-Flight Model Firings. Defense Technical Information Center. https://doi.org/10.21236/ad0323887
• Croom, D. 1977. “Wind-Tunnel and Flight Evaluation of Spoilers as Trailing-Vortex Hazard Alleviation Devices.” In 15th Aerospace Sciences Meeting. AIAA 1977-10. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-10
• Croom, C. C., and B. J. Holmes. 1985. “Flight Evaluation of an Insect Contamination Protection System for Laminar Flow Wings.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/850860
• Croom, Cynthia C., Gregory S. Manuel, and John P. Stack. 1987. “Tollmien-Schlschfing Instabilities in Laminar Flow in-Flight Detection Of.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/871016
• Cross, J. L. 1984. YO-3A Acoustics Research Aircraft Systems Manual. NASA-TM-85968. NASA. https://ntrs.nasa.gov/citations/19850001767
• Cross, J., and M. Watts. 1983. “In-Flight Acoustic Testing Techniques Using the YO-3A Acoustic Research Aircraft.” In 2nd Flight Testing Conference. AIAA 1983-2754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2754
• Crouch, Jeffrey. 2008. “Modeling Transition Physics for Laminar Flow Control.” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-3832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-3832
• Crounse, David R. 2005. Chapter 6: Flight Test Instrumentation. RTO-AG-300-V14. US Air Force Flight Test Center. https://ntrs.nasa.gov/citations/20050209972
• Crow, Steven C., and Gene G. Bergmeier. 1996. “Active Sonic Boom Control.” In The 1995 NASA High-Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/19960055054
• Crowder, James P. 2018. “Infrared Cameras for Boundary Layer Transition Visualization in Industrial Wind Tunnel and Flight Testing.” In Handbook of Flow Visualization. Routledge. https://doi.org/10.1201/9780203752876-27
• Crowther, W. J., and P. J. Lamont. 2001. “A Neural Network Approach to the Calibration of a Flush Air Data System.” Aeronautical Journal 105 (1044): 85–95. https://doi.org/10.1017/s0001924000011532
• “Cruise and Climb of an Ideal Subsonic Airplane.” n.d. In Fundamentals of Airplane Flight Mechanics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-46573-7_5
• Cruz, Christopher I., and Walter C. Engelund. 1991. Enhancements to the High Speed Convective Heating and Viscous Drag Prediction Techniques of the Aerodynamic Preliminary Analysis System (APAS). AIAA PAPER 91-1435. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910058871
• Cruz, E. S., N. B. Gorenberg, and A. W. Kerr. 1969. A Flight Envelope Expansion Study for the XH-51A Compound Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ad0864282
• Cruz, Juan R., and Justin S. Green. 2019. “Subsonic Dynamic Testing of a Subscale ADEPT Entry Vehicle.” In AIAA Aviation 2019 Forum. AIAA 2019-2898. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2898
• Cruz, Christopher, and George Ware. 1992. “Predicted Aerodynamic Characteristics for HL-20 Lifting-Body Using the Aerodynamic Preliminary Analysis System (APAS).” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3941
• Cruz, Christopher I., George M. Ware, Sue B. Grafton, William C. Woods, and James C. Young. 1989. Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting-Body Configuration at Mach Numbers from 0.05 to 20.3. NASA-TM-101641. NASA. https://ntrs.nasa.gov/citations/19930015333
• Cuda, Vincent, Jr. 2022. Instrumentation and Testing of Ground and Flight Hardware. Analytical Mechanics Associates (United States). https://ntrs.nasa.gov/citations/20220018908
• Culp, M., and D. Cooke. 1982. “Stability and Control Flight Test Results of the Space Transportation System’s Orbiter.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1316
• Culpepper, Grace G., Jielong Cai, and Sidaard Gunasekaran. 2022. “Effect of Forward Propeller Tilt and Inlet Shape in Propeller-in-Wing Thrust Vectoring.” In AIAA SCITECH 2022 Forum. AIAA 2022-1539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1539
• Culy, Douglas G. 1995. “Forecasting Engine and Airframe Development Cost.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/952031
• Cumelles Céspedes, Joel. n.d. “System Identification of High-Performance Paraglider-Harness/pilot Dynamics: From Modelling to Flight Test Data.” PhD diss., Universitat Politècnica de Catalunya. https://doi.org/10.5821/dissertation-2117-471720
• Cumming, Stephen B., Trong Bui, Mark S. Smith, Mike Frederick, and Daniel Banks. 2017. “Aerodynamics and Performance X-Plane Airworthiness Guidelines and Best Practices.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170005548
• Cumming, Stephen, and Corey Diebler. 2005. “Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6312
• Cumming, Stephen, and Hyun Dae Kim. 2018. Propulsion-Airframe Integration Flight Test Instrumentation. AFRC-E-DAA-TN57587. NASA Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20180004244
• Cumming, D., and W. Lowe. 1971. “Experimental Wall Interference Studies in a Transonic Wind Tunnel.” In 6th Aerodynamics Testing Conference. AIAA 1971-292. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-292
• Cummings, Russell, Scott Morton, and Stefan Siegel. 2003. “Numerical Predictions and Wind Tunnel Experiment for a Pitching Unmanned Combat Air Vehicle.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-417
• Cunningham, T. B. 1984. “Opportunities for Aircraft Controls Research.” In NASA. Langley Research Center NASA Aircraft Controls Research, 1983. https://ntrs.nasa.gov/citations/19840012531
• Cunningham, Kevin, John Foster, Austin Murch, and Eugene Morelli. 2008. “Practical Application of a Subscale Transport Aircraft for Flight Research in Control Upset and Failure Conditions.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6200
• Cunningham, J. A., and J. W. Haney Jr. 1983. “Space Shuttle Wing Leading Edge Heating Environment Prediction Derived from Development Flight Data.” In NASA. Langley Research Center Shuttle Performance: Lessons Learned, Pt. 2. https://ntrs.nasa.gov/citations/19840002095
• Cunningham, Michael, Nikhil Nigam, Sricharan K. Ayyalasomayajula, et al. 2022. “Integrated Vehicle-Propulsion-Control Design Architecture for Distributed Electric Propulsion-Enabled Aircraft.” In AIAA AVIATION 2022 Forum. AIAA 2022-3484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3484
• Cunningham, Kevin, Gautam H. Shah, Melissa A. Hill, Brent P. Pickering, Jonathan S. Litt, and Scott B. Norin. 2018. “A Generic T-Tail Transport Airplane Simulation for High-Angle-Of-Attack Dynamics Modeling Investigations.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20190000436
• Curran, Damian R., Vincent Wheatley, and Michael K. Smart. 2018. “Investigation of Combustion Mode Control in a Mach 8 Shape-Transitioning Scramjet.” In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2018-5380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-5380
• Curry, Timothy J., and James G. Batterson. 2000. Estimation of Handling Qualities Parameters of the Tu-144 Supersonic Transport Aircraft from Flight Test Data. NASA/CR-2000-210290. NASA. https://ntrs.nasa.gov/citations/20000103558
• Curry, Robert E., Michael R. Mendenhall, and Bryan Moulton. 1992a. “In-Flight Evaluation of Aerodynamic Predictions of an Air-Launched Space Booster.” In AGARD Symposium on Theoretical and Experimental Methods in Hypersonic Flows. https://ntrs.nasa.gov/citations/19920022564
• Curry, Robert E., Robert R. Meyer Jr., and Gerald D. Budd. 1992b. “Pegasus Hypersonic Flight Research.” In SAE. https://ntrs.nasa.gov/citations/19940035352
• Curry, Robert E., Bryan J. Moulton, and John Kresse. 1989. “An in-Flight Investigation of Ground Effect on a Forward-Swept Wing Airplane.” In AGARD Symposium on Aerodynamics of Combat Aircraft, Controls, and of Ground Effect. https://ntrs.nasa.gov/citations/19900004886
• Curry, Robert E., Bryan J. Moulton, and John Kresse. 1990. “An in-Flight Investigation of Ground Effect on a Forward-Swept Wing Airplane.” In AGARD, Aerodynamics of Combat Aircraft Controls and of Ground Effects. https://ntrs.nasa.gov/citations/19900019217
• Curry, R., and A. Sim. 1982. “Unique Flight Characteristics of the AD-1 Oblique-Wing Research Airplane.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1329
• Curry, R. E., and A. G. Sim. 1984. In-Flight Total Forces, Moments and Static Aeroelastic Characteristics of an Oblique-Wing Research Airplane. NASA-TP-2224. NASA. https://ntrs.nasa.gov/citations/19870000670
• Curtin, M. M., D. R. Bogue, D. Om, S. M. B. Rivers, O. C. Pendergraft Jr., and R. A. Wahls. 2002. Investigation of Transonic Reynolds Number Scaling on a Twin-Engine Transport. AIAA Paper 2002-0420. Boeing Commercial Airplane Co. https://ntrs.nasa.gov/citations/20030003815
• Curtiss, H. C., Jr. 1965. Downwash Tests of the Dual Tandem Ducted Propeller VTOL Research Aircraft Configurations to Evaluate Engine Inlets, Protection Devices and Study Aerodynamic Interference. Defense Technical Information Center. https://doi.org/10.21236/ad0628669
• Curtiss, H., Jr. 1969. “Dynamic Stability of V/STOL Aircraft at Low Speeds.” In VTOL Research, Design, and Operations Meeting. AIAA 1969-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-194
• Curtiss Jr., H. C. Putman, and W. F. J. V. Lebacqz. 1967. An Experimental Investigation of the Longitudinal Dynamic Stability Characteristics of a Four-Propeller Tilt-Wing VTOL Model. Defense Technical Information Center. https://doi.org/10.21236/ad0663848
• Cusick, Andrew, and Konstantinos Kontis. 2019. “Creation of Design and Analysis Tools for Large Design Space Reusable Launch Vehicle Shape Optimization.” In AIAA Aviation 2019 Forum. AIAA 2019-2929. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2929
• Cusimano, George, and Norman Johnson. 1994. “JOINT Stars: A Flight Test Retrospective.” In Biennial Flight Test Conference. AIAA 1994-2120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2120
• Czechowicz, Bogusław, Mirosław Nowakowski, and Grzegorz Kowaleczko. 2015. “Modelling of Flight Dynamics of an Airplane Encountering Trailing Vortices Generated by Another Airplane.” Journal of KONES. Powertrain and Transport 19 (1): 41–50. https://doi.org/10.5604/12314005.1137305
• Czysz, Paul A. 1963. Correlation of Wind Tunnel Blockage Data. Defense Technical Information Center. https://doi.org/10.21236/ad0407689
• Czysz, Paul, and S. Murthy. 1996. “SSTO Launcher Demonstrator for Flight Test.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4574
• D’Amico, William, Daniel Simon, and Bruce Land. 2004. “A Perspective for Hypersonic Vehicle Flight Instrumentation.” In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2004-2294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2294
• D’Angelo, Salvatore, Edmondo Minisci, D. Daniele, and Luciano Guerra. 1999. “Optimization Methodology for the Climb Trajectory of a SSTO Lifting-Body Reusable Launcher.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4165
• “D-Optimal Designs for Exponential Models.” n.d. In Lecture Notes in Statistics. Springer-Verlag. https://doi.org/10.1007/0-387-31610-8_7
• “D-Optimal Designs for Rational Models.” n.d. In Lecture Notes in Statistics. Springer-Verlag. https://doi.org/10.1007/0-387-31610-8_6
• “D. Propellers for High Speed Flight.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-012
• “D. Supersonic and Transonic Small Perturbation Theory.” 1954. In General Theory of High Speed Aerodynamics. Princeton University Press. https://doi.org/10.1515/9781400877553-006
• Dadd, Graham, Rachel Owen, J. Hodges, and K. Atkinson. 2006. “Sustained Hypersonic Flight Experiment (SHyFE).” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7926
• Dahlen, Theodore E. 1953. Maximum Altitude and Maximum Mach Number Obtained with the Modified Douglas D-558-II Research Airplane during Demonstration Flights. NACA-RM-L53B24. NASA. https://ntrs.nasa.gov/citations/19930089125
• Dallery, Francois. 1987. “Failure Detection and Identification for a Reconfigurable Flight Control System.” In NASA Langley Research Center Joint University Program for Air Transportation Research, 1983. https://ntrs.nasa.gov/citations/19870009096
• Damman, L. 1976. “Flight Test Development and Evaluation of a Multimode Digital Flightcontrol System in an A-7D.” In Aircraft Systems and Technology Meeting. AIAA 1976-927. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-927
• Damstrom, E., and J. Mayes. 1970. “Transonic Flight and Wind Tunnel Buffet Onset Investigation of the F-8D Aircraft: Analysis of Data and Test Techniques.” In Earth Sources Observations and Information Systems Metting. AIAA 1970-341. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-341
• Damveld, Herman. 2004. “Determination of Instationary Aeroelastic Stability Derivatives for Real-Time Simulation.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5365
• Dana, W. 1968. “Flight Simulation of Night Landings of Lifting Entry Vehicles.” In 2nd Simulation and Support Conference. AIAA 1968-259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-259
• Dana, William. 1993. “The X-15 Airplane: Lessons Learned.” In 31st Aerospace Sciences Meeting. AIAA 1993-309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-309
• Dana, W. H., H. G. Gaidsick, and R. C. McCracken. 1969. Evaluation of an Indirect Viewing System for Lifting-Body Terminal-Area Navigation and Landing Tasks. NASA-TN-D-5299. NASA. https://ntrs.nasa.gov/citations/19690020352
• Dana, William H., and J. R. Gentry. 1970. “Pilot Impressions of Lifting Body Vehicles.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000633
• Dancik, Paul J., Frederick R. Mazzitelli, and William B. Peck. 1958. “Test Experience on the Vertol 76 Tilt Wing VTOL Research Aircraft.” In Proceedings of the Vertical Flight Society Forum 14 - Washington, D.C. 1958. The Vertical Flight Society. https://doi.org/10.4050/vfs-f14-002
• Danehy, Paul M., Christoper B. Ivey, Brett F. Barthel, et al. 2010. “Orbiter BLT Flight Experiment Wind Tunnel Simulations: Nearfield Flowfield Imaging and Surface Thermography.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100002209
• Daniel, Castroviejo, and Patrick Hendrick. 2023. “Test Bench for Electric Propellers and Distributed Propulsion.” In Sustainable Aviation. Springer International Publishing. https://doi.org/10.1007/978-3-031-32639-4_12
• Daniel, Leo, and Guy Ramusat. 2005. “Prospective and Economic Impact of Composites in Reusable Launch Vehicle.” In Space 2005. AIAA 2005-6618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6618
• Daniel, Leo, Giorgio Tumino, Torben Henriksen, and Christian Dujarric. 2004. “Advanced Composite Technology in Reusable Launch Vehicle (RLV).” In Space 2004 Conference and Exhibit. AIAA 2004-5825. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5825
• Danis, Reed. n.d. “Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-Foot Wind Tunnel.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2018.63
• Danowsky, Brian P. 2017. “Flutter Suppression of a Small Flexible Aircraft Using MIDAAS.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4353
• Danowsky, Brian P., Aditya Kotikalpudi, David Schmidt, Chris Regan, and Peter Seiler. 2018. “Flight Testing Flutter Suppression on a Small Flexible Flying-Wing Aircraft.” In 2018 Multidisciplinary Analysis and Optimization Conference. AIAA 2018-3427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3427
• Danowsky, Brian, P. Schulze, and Marty Brenner. 2012. “Structured-Singular-Value-Based Optimal Aeroelastic Uncertainty Quantification Using Surrogate Models and Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4950. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4950
• Dantsker, Or D. 2024a. “Development, Integration, and Initial Ground & Flight Testing of an Unmanned Aircraft for Dynamically-Scaled Flight Testing Research: Great Planes Avistar 30cc.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4395
• Dantsker, Or D. 2024b. “Methodology for Designing Dynamically-Scaled Flight Testing Research with the Avistar Series of UAVs.” In AIAA SCITECH 2024 Forum. AIAA 2024-2842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2842
• Dantsker, Or D., Marco Caccamo, and Renato Mancuso. 2023a. “Expanded Flight & Ground Testing Data Set for an Unmanned Aircraft: Great Planes Avistar Elite.” In AIAA SCITECH 2023 Forum. AIAA 2023-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2105
• Dantsker, Or D., Marco Caccamo, Moiz Vahora, and Renato Mancuso. 2020. “Flight & Ground Testing Data Set for an Unmanned Aircraft: Great Planes Avistar Elite.” In AIAA Scitech 2020 Forum. AIAA 2020-0780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0780
• Dantsker, Or D., Stephen T. Haviland, Ryan Allford, et al. 2023b. “Flight Testing of Tailless Subscale HAPS Aircraft.” In AIAA AVIATION 2023 Forum. AIAA 2023-3780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3780
• Dantsker, Or D., Stephen T. Haviland, Jason Mukherjee, et al. 2022. “Flight Testing of Subscale HAPS Models to Evaluate Aircraft Configurations.” In AIAA AVIATION 2022 Forum. AIAA 2022-3638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3638
• Dantsker, Or D., and Renato Mancuso. 2019. “Flight Testing Data Set for Subscale GA Aircraft: 26%-Scale Cub Crafters CC11-100 Sport Cub S2.” In AIAA Scitech 2019 Forum. AIAA 2019-1616. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1616
• Dantsker, Or D., Renato Mancuso, Byron Ward, Christian Miller, Donovan F. Shea, and Kyle Collins. 2025. “Flight Testing Instrumentation Development and Integration for a Subscale Integrated High Lift Propulsor Testbed.” In AIAA SCITECH 2025 Forum. AIAA 2025-2416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2416
• Dantsker, Or D., and Michael S. Selig. 2015. “High Angle of Attack Flight of a Subscale Aerobatic Aircraft.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2568
• Dantsker, Or D., Simon Yu, Moiz Vahora, and Marco Caccamo. 2019. “Flight Testing Automation to Parameterize Unmanned Aircraft Dynamics.” In AIAA Aviation 2019 Forum. AIAA 2019-3230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3230
• Darden, C. 1976. “Sonic Boom Theory: Its Status in Prediction and Minimization.” In 14th Aerospace Sciences Meeting. AIAA 1976-1. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1
• Darden, Christine M. 1999. “Progress in Sonic-Boom Understanding: Lessons Learned and Next Steps.” In High-Speed Research: 1994 Sonic Boom Workshop. Configuration, Design, Analysis and Testing. https://ntrs.nasa.gov/citations/20000027455
• Das, Sudipto, Kartik Venkatraman, and Madhusudan A. Padmanabhan. 2021. “A Study of the Active Aeroelastic Wing Concept for a Delta Wing Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-0730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0730
• Dasgupta, Arnab, Rishabh Choudhury, Andrew Neely, Sean O’Bryne, and Joe Kurtz. 2012. “Thermal-Structural Modelling of TDLAS System for SCRAMSPACE Hypersonic Flight Test.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5900
• Daud Filho, Antonio Carlos. n.d. “A Tilt-Wing VTOL UAV Configuration Study: Flight Dynamics Modeling, Simulation, States Estimation, Control, Systems Integration and Flight Testing.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/t.18.2023.tde-27032023-153150
• Davidson, Ron, John T. Bosworth, Steven R. Jacobson, Michael Pl Thomson, and Charles C. Jorgensen. 2003. Flight Test of an Intelligent Flight-Control System. DRC-01-35. Boeing Phantom Works. https://ntrs.nasa.gov/citations/20110023963
• Davidson, John R., and James F. Dalby. 1961. Optimum Design of Insulated Compression Plates Subjected to Aerodynamic Heating. NASA-TN-D-520. NASA. https://ntrs.nasa.gov/citations/20040020120
• Davidson, J., F. Lallman, J. D. McMinn, et al. 1999. Flight Control Laws for NASA’s Hyper-X Research Vehicle. AIAA Paper 99-4124. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040086945
• Davies, Rose G. 2020a. “Introduction of Supersonic Flight.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9780429261152-11
• Davies, Rose G. 2020b. “Transonic Flight and Aerofoils.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9780429261152-9
• Davies, Rose G. 2025a. “Introduction of Supersonic Flight.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9781032692883-12
• Davies, Rose G. 2025b. “Transonic Flight and Aerofoils.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9781032692883-10
• Davis, J. 1968b. “A Shock Tube Technique for Producing Subsonic, Transonic, and Supersonic Flows with Extremely High Reynolds Numbers.” In 6th Aerospace Sciences Meeting. AIAA 1968-18. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-18
• Davis, S. 1972. “Calculation of Sonic Boom Signatures by Bicharacteristic Methods.” In 10th Aerospace Sciences Meeting. AIAA 1972-195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-195
• Davis, S. S. 1980. Experimental Studies of Scale Effects on Oscillating Airfoils at Transonic Speeds. NASA-TM-81216. NASA. https://ntrs.nasa.gov/citations/19800018788
• Davis, S. S. 1981. “Experimental Studies of Scale Effects on Oscillating Airfoils at Transonic Speeds.” In AGARD Boundary Layer Effects on Unsteady Airfoils. https://ntrs.nasa.gov/citations/19810014521
• Davis, Hubert P. 1989. A Technology Demonstrator Vehicle for Advanced Launch Systems. AIAA PAPER 89-2949. Davis Aerospace Co. https://ntrs.nasa.gov/citations/19890059821
• Davis, R., and M. Fischer. 1983. “Cloud Particle Effects on Laminar Flow and Instrumentation for Theirmeasurement aboard a NASA LFC Aircraft.” In 2nd Flight Testing Conference. AIAA 1983-2734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2734
• Davis, R., M. Fischer, D. Fisher, and R. Young. 1986. “Cloud Particle Effects on Laminar Flow in the NASA LEFT Program: Preliminary Results.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9811
• Davis, J., T. Garnett, and J. Gaul. 1977. Heavy Lift Helicopter Flight Control System. Volume III. Automatic Flight Control System Development and Feasibility Demonstration. Defense Technical Information Center. https://doi.org/10.21236/ada050059
• Davis, Charles E., and John R. Mertens. 1958. “Wind Tunnel and Flight Testing the XV-3 Fixed-Wing VTOL.” In Proceedings of the Vertical Flight Society Forum 14 - Washington, D.C. 1958. The Vertical Flight Society. https://doi.org/10.4050/vfs-f14-004
• Davis, Mark C., Alexander G. Sim, Matthew Rhode, and Kevin D. Johnson. 2006. “Wind Tunnel Results of the B-52B with the X-43A Stack.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20060022150
• Davis, Mark C., Alexander G. Sim, Matthew Rhode, and Kevin D. Johnson Sr. 2007. “Wind-Tunnel Results of the B-52B with the X-43A Stack.” Journal of Spacecraft and Rockets 2007 44 (4). https://ntrs.nasa.gov/citations/20070034701
• Davis, Mark C., and J. Terry White. 2006a. Flight Test Determined Aerodynamics Force and Moment Characteristics of the X-43A Research Vehicle at Mach 7.0. DFRC-459. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20090009773
• Davis, Mark, and John White. 2006b. “Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8028
• Davison, T. 1963. “Measurement of Net Thrust in Flight.” In Testing of Manned Flight Systems Conference. AIAA 1963-1802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1802
• Dawicke, David S. n.d. “Digital Image Correlation Applications at NASA Langley Research Center (1990 to 2025).” In ASTM Workshop on Novel and Emerging Uses of Sensor Technology in Mechanical, Fatigue, and Fracture Testing. https://ntrs.nasa.gov/citations/20250003935
• Day, Richard E. 1953. Measurements Obtained during the Glide-Flight Program of the Bell X-2 Research Airplane. NACA-RM-L53G03a. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930087801
• Day, Richard E. 1997. Coupling Dynamics in Aircraft: A Historical Perspective. NASA-SP-532. NASA. https://ntrs.nasa.gov/citations/19970019603
• Day, R. E., and R. G. Hoey. 1961. X-15 Mission Planning and Operational Procedures. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19710070140
• Day, Richard E., and Donald Reisert. 1959. Flight Behavior of the X-2 Research Airplane to a Mach Number of 3.20 and a Geometric Altitude of 126,200 Feet. NASA-TM-X-137. NASA. https://ntrs.nasa.gov/citations/19980227870
• Day, Richard E., and Wendell H. Stillwell. 1952. First Landing of Bell X-2 Research Airplane. NACA-RM-L52I11. NASA. https://ntrs.nasa.gov/citations/19930087318
• Dayton, K. 1993. “National Aerospace Plane Integrated Fuselage/Cryotank Risk Reductionprogram.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2564
• De Angelis, V. M., and M. H. Tang. 1969. Fin Loads and Control-Surface Hinge Moments Measured in Full-Scale Wind-Tunnel Tests on the X-24A Flight Vehicle. NASA-TM-X-1922. NASA. https://ntrs.nasa.gov/citations/19710005026
• De Crombrugghe, Guerric. n.d. “On Binary Scaling and Ground-to-Flight Extrapolation in High-Enthalpy Facilities.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2017.456
• De Filippis, Federico, Raffaele Savino, and Adolfo Martucci. 2005. “Numerical-Experimental Correlation of Stagnation Point Heat Flux in High Enthalpy Hypersonic Wind Tunnel.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3277
• de Paula, Camila, Guilherme Fernandes, and Victor Maldonado. 2025. “Aerodynamic Simulations of a Blended Fan-in-Wing Body VTOL Configuration for Optimal and Efficient Flight Transition.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3764
• de Visser, J. 1999. “Aeroelastic and Strength Optimisation of a Composite Aircraft Wing Using a Multilevel Approach.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1258
• de Vries, Reynard, Maurice Hoogreef, and Roelof Vos. 2019b. “Preliminary Sizing of a Hybrid-Electric Passenger Aircraft Featuring over-the-Wing Distributed-Propulsion.” In AIAA Scitech 2019 Forum. AIAA 2019-1811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1811
• de Vries, Reynard, and Roelof Vos. 2022. “Aerodynamic Performance Benefits of over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-0128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0128
• De Wagter, Christophe, and Joost Meulenbeld. 2019. “Modeling the Unstable DelftaCopter Vertical Take-off and Landing Tailsitter Unmanned Air Vehicle in Hover and Forward Flight from Flight Test Data.” International Journal of Micro Air Vehicles 11: 1756829319880302. https://doi.org/10.1177/1756829319880302
• Deal, P., G. Keyser, B. Fisher, and N. Crabill. 1981. “Thunderstorm Hazards Flight Research: Program Overview.” In 1st Flight Test Conference. AIAA 1981-2412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2412
• Deam, D. 1984. “An Electromagnetic Vibrator for Use in Flutter Testing.” In 22nd Aerospace Sciences Meeting. AIAA 1984-86. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-86
• Deandrea, Jay, James Roache, and Michael Robinson. 1991. “Three-Dimensional Unsteady Flow Fields Elicited by Pitching a Canardand Forward Swept Wing Configuration.” In 29th Aerospace Sciences Meeting. AIAA 1991-5. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-5
• Deangelis, V. 1981. “In-Flight Deflection Measurement of the HiMAT Aeroelastically Tailored Wing.” In 1st Flight Test Conference. AIAA 1981-2450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2450
• “The Debate over Manned Military Spaceflight: The Spaceflight Revolution and Dyna-Soar, October 1957–May 1959.” 2006. In US Hypersonic Research and Development. Routledge. https://doi.org/10.4324/9780203012994-11
• Debiasi, Marco, Zeng Yan, and Tat Loon Chng. 2010. “Swept-Back Grid Fins for Transonic Drag Reduction.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4244
• Dec, John, and Robert Braun. 2006. “An Approximate Ablative Thermal Protection System Sizing Tool for Entry System Design.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-780
• Dec, J., and R. Mitcheltree. 2002. “Probabilistic Design of a Mars Sample Return Earth Entry Vehicle Thermal Protection System.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-910. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-910
• Deck, Sebastien. 2004. “Detached-Eddy Simulation of Transonic Buffet over a Supercritical Airfoil.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5378
• Deck, Ulrich, and Werner Würz. 2023. “In-Flight Measurements on the Influence of Freestream Turbulence on a NLF Airfoil.” In AIAA AVIATION 2023 Forum. AIAA 2023-3675. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3675
• Decker, William A., Rickey C. Simmons, George E. Tucker, and Edwin W. Aiken. 1994. Handling Qualities Influences on Civil Tiltrotor Terminal Operating Procedure Development. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020002849
• Deckert, J. C. 1981. Flight Test Results for the F-8 Digital Fly-by-Wire Aircraft Control Sensor Analytic Redundancy Management Technique. AIAA PAPER 81-1796. Charles Stark Draper Laboratory, Inc. https://ntrs.nasa.gov/citations/19810059731
• Deckert, J. C., M. N. Desai, J. J. Deyst Jr., and A. S. Willsky. 1978. Reliable Dual-Redundant Sensor Failure Detection and Identification for the NASA F-8 DFBW Aircraft. NASA-CR-2944. NASA. https://ntrs.nasa.gov/citations/19780012198
• Deckert, W. H., and C. A. Holzhauser. 1973. “Evaluation of V/STOL Research Aircraft Design.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19740028807
• Deckman, R. W., and H. E. Arnold. 1960. Summary of XM-70 Flutter Model Tests from 1 March 1958 to 20 May 1960 Naa Designation NA-267 Af Designation XB-70. Defense Technical Information Center. https://doi.org/10.21236/ad0331888
• Deel, Arlin, William R. Horton, Alton G. Steinmetz, and Charles J. Bowers. 1972. Engineering Flight Test, Boeing-Vertol Model 347 Advanced Technology Helicopter, Phase 2. Defense Technical Information Center. https://doi.org/10.21236/ad0909933
• Deem, R., and J. Murphy. 1965. “Flat Plate Boundary Layer Transition at Hypersonic Speeds.” In 2nd Aerospace Sciences Meeting. AIAA 1965-128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-128
• Deepa, M. S., and S. C. Gupta. 2023. “Flight Envelope Expansion during Prototype Development.” Journal of Aerospace Sciences and Technologies: 220–32. https://doi.org/10.61653/joast.v65i2.2013.727
• Deepak, N. R., Taprabata Ray, and Russell Boyce. 2006. “Nose Cone Design Optimization for a Hypersonic Flight Experiment Trajectory.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7998
• Deere, Karen A., James M. Luckring, S. Naomi McMillin, Jeffrey D. Flamm, and Dino Roman. 2016. “CFD Predictions for Transonic Performance of the ERA Hybrid Wing-Body Configuration.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160007649
• Deere, Karen A., Sally Viken, Melissa B. Carter, et al. 2018. “Computational Component Build-up for the X-57 Maxwell Distributed Electric Propulsion Aircraft.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1275
• Deere, Karen A., Jeffrey K. Viken, Sally Viken, Melissa B. Carter, Michael Wiese, and Norma Farr. 2017. “Computational Analysis of a Wing Designed for the X-57 Distributed Electric Propulsion Aircraft.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3923. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3923
• Deere, Karen A., Jeffrey K. Viken, Sally A. Viken, Melissa B. Carter, Michael R. Wiese, and Norma L. Farr. 2022. Computational Analysis of the X-57 Maxwell Airplane at Unpowered Conditions (Preliminary Fuselage). Langley Research Center. https://ntrs.nasa.gov/citations/20210011034
• Dees, Ray A., and Cheng M. Moua. 2010. “Challenges and Lessons Learned from Resurrecting a Legacy Research Flight Controller.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100001731
• Deets, D., and L. Brown. 1986. “Wright Brothers Lectureship in Aeronautics: Experience with HiMAT Remotely Piloted Research Vehicle: An Alternate Flight Test Approach.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2754
• Deets, Dwain A., V. Michael Deangelis, and David P. Lux. 1986. HiMAT Flight Program: Test Results and Program Assessment Overview. NASA-TM-86725. NASA. https://ntrs.nasa.gov/citations/19880000644
• Defense Science Board Washington Dc. 1988. Report of the Defense Science Board Task Force on the National Aerospace Plane (NASP). Defense Technical Information Center. https://doi.org/10.21236/ada201124
• Defense Science Board Washington Dc. 1993. Report of the Defense Science Board Task Force on Simulation, Readiness and Prototyping. Defense Technical Information Center. https://doi.org/10.21236/ada266125
• “Definitions of Aerodynamic Stability and Control Derivatives.” 1997. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-340-63200-0.50019-8
• “Definitions of Aerodynamic Stability and Control Derivatives.” 2007. In Flight Dynamic Principles. Elsevier. https://doi.org/10.1016/b978-075066927-6/50019-2
• “Definitions of Aerodynamic Stability and Control Derivatives.” 2013. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-08-098242-7.00025-0
• Defoort, Sebastien, Marc Ferrier, and Laurent Serre. 2014. “Design and Full 3D Nose-to-Tail Computation of a Turbofan+ Scramjet Mach 8 Civil Aircraft.” In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2014-2532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2532
• Dehaan, Mark. 1990. “Induced Drag of Wings with Highly Swept and Tapered Wing Tips.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3062. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3062
• Dehennis, Timothy. 2025. “Evaluation and Implementation of Low Core Hardness Gears in the SB>1 DEFIANT JMR Technology Demonstrator Aircraft.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0228
• Dehideniya, Dissanayake Mudiyanselage Mahasen B. n.d. “Optimal Bayesian Experimental Designs for Complex Models.” PhD diss., Queensland University of Technology. https://doi.org/10.5204/thesis.eprints.131625
• Deiler, Christoph. 2016. “Aerodynamic Modeling, System Identification and Analysis of Iced Aircraft Configurations.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3852
• Dejarnette, F. R., H. H. Hamilton, K. J. Weilmuenster, and F. M. Cheatwood. 1985. A Review of Some Approximate Methods Used in Aerodynamic Heating Analyses. AIAA PAPER 85-0906. North Carolina State University. https://ntrs.nasa.gov/citations/19850055429
• Dekkala, Vinay, Shivansh Rana, Yash Raj, et al. 2024. “Design Optimization of a Waverider to Enhance the Aerodynamic Efficiency.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4137
• Del Frate, John H. 1992. “In-Flight Flow Visualization Results from High Angle of Attack Tests on a Forward Swept Wing Aircraft with Comparisons to Water Tunnel Results.” In Flow Visualization VI. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-84824-7_44
• Del Frate, John H., and John A. Saltzman. 1992. “In-Flight Flow Visualization Results from the X-29A Aircraft at High Angles of Attack.” In 6th AIAA Biennial Flight Test Conference. https://ntrs.nasa.gov/citations/19930027275
• del Val, Anabel, and Madhurima Das. 2026. “Model Error Effects on Hypersonic Ground-To-Flight Extrapolation.” In AIAA SCITECH 2026 Forum. AIAA 2026-0659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0659
• Dela Peña, Arthur. 2026. “Fuel-Efficiency Potential and Engineering Readiness of the Transonic Truss-Braced Wing: Common-Baseline Assessment and Integration-Penalty Analysis.” Preprint, . https://doi.org/10.2139/ssrn.7511406
• Delany, Noel K., and William M. Kauffman. 1945. Correlation of Wind-Tunnel Predictions with Flight Tests of a Twin-Engine Patrol Airplane II: Lateral- and Directional-Stability and Control Characteristics. NACA-WR-A-71. NASA. https://ntrs.nasa.gov/citations/19930092585
• DelFrate, John H. 2007. “Update on Piloted and Un-Piloted Aircraft at NASA Dryden.” In W-HALES 2007: NASA-NICT Joint Workshop on HALE UAV and Wireless Systems. https://ntrs.nasa.gov/citations/20070017915
• DelFrate, John. 2008. “Suborbital Science Program: Dryden Flight Research Center.” In W-HALES 2008: NASA-NICT Joint Workshop on HALE UAV and Wireless System. https://ntrs.nasa.gov/citations/20080021724
• Delgado, Frank J., Michael F. Abernathy, and Janis White. 2001. “Hybrid Synthetic-Vision System for the X-38 Crew Return Vehicle.” In SPIE Proceedings, vol. 4363, edited by Jacques G. Verly. SPIE. https://doi.org/10.1117/12.438020
• Delgado, Frank J., Scott Altman, Michael F. Abernathy, and Janis White. 2000. “Virtual Cockpit Window for the X-38 Crew Return Vehicle.” In SPIE Proceedings, vol. 4023, edited by Jacques G. Verly. SPIE. https://doi.org/10.1117/12.389361
• Delgado, Xavier, and Anubhav Datta. 2026. “Parametric Whirl Flutter Testing of Swept-Tip Proprotor Blades.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0269
• Demarchi, Joseph N., and Robert K. Haning. 1978. Flight Verification of the Advanced Flight Control Actuation System (AFCAS) in the T-2C Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada060326
• Demetriades, Anthony. 1975. Hydrodynamic Stability and Transition to Turbulence in the Hypersonic Boundary Layer over a Sharp Cone. Defense Technical Information Center. https://doi.org/10.21236/ada016536
• Demiroglu, Yusuf, and Melike Nikbay. 2023. “Development of a Sonic Boom Propagation Code for Low-Boom Supersonic Aircraft Design and Optimization.” In AIAA SCITECH 2023 Forum. AIAA 2023-1513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1513
• Demiroglu, Yusuf, Sihmehmet Yildiz, and Melike Nikbay. 2021. “Multi-Fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design.” In AIAA Scitech 2021 Forum. AIAA 2021-1009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1009
• Demo, B. 1986. “The NDS 2000 Flight Test Instrumentation System in the F-20 Tigershark.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9797. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9797
• Denardo, Billy Pat, and Thomas N. Canning. 1952. Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes a-3B Missile at a Mach Number of 5.0. NACA-RM-SA52C10. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20090023659
• Deng, Guang Chen, Satoshi Baba, Stéphane Moreau, and Philippe Lavoie. 2023. “Wall-Resolved Large-Eddy Simulation of Supercritical Airfoil Side-Edge Noise.” In Progress in Canadian Mechanical Engineering. Volume 6. Université de Sherbrooke. Faculté de génie. https://doi.org/10.17118/11143/20871
• Deng, Bo, Li Luo, and WenChang Wang. 2022. “Theory of Engineering Knowledge in the Revolutionary Change of Epistemology.” Journal of Engineering Studies 14 (4): 311–25. https://doi.org/10.3724/j.issn.1674-4969.22090101
• Denham, Casey L., and D. Bruce Owens. 2016. “Rotary Balance Wind Tunnel Testing for the FASER Flight Research Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3105
• Denieul, Yann, Daniel Alazard, Joel Bordeneuve, Clement Toussaint, and Gilles Taquin. 2015. “Interactions of Aircraft Design and Control: Actuators Sizing and Optimization for an Unstable Blended Wing-Body.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2553
• Denison, Marie F., Jenna L. Eppink, and Joshua K. Smith. 2023. “Computational Study of Low-Speed Boundary-Layer Laminar-Turbulent Transition over a 30º Swept Plate in a Channel.” In AIAA AVIATION 2023 Forum. https://ntrs.nasa.gov/citations/20230008266
• Department of the Air Force Justification of Estimates for Fiscal Year 1981, Submitted to Congress January 1980, Aircraft Procurement, Air Force, Missile Procurement, Air Force, Other Procurement, Air Force. 1980. Defense Technical Information Center. https://doi.org/10.21236/ada097782
• Department of the Air Force Justification of Estimates for Fiscal Year 1987 Submitted to Congress February 1986: Aircraft Procurement, Air Force. 1986. Defense Technical Information Center. https://doi.org/10.21236/ada169365
• Department of the Air Force Justification of Estimates for Fiscal Years 1992/1993 Biennial Budget Estimates Submitted to Congress February 1991: Aircraft Procurement, Air Force. 1991. Defense Technical Information Center. https://doi.org/10.21236/ada236184
• Department of the Air Force Justification of Fiscal Year 1991 Budget Estimates Submitted to Congress January 1990. Aircraft Procurement, Air Force. 1990. Defense Technical Information Center. https://doi.org/10.21236/ada218310
• Department of the Air Force. Committee Staff Procurement Backup Book, FY 1995 Budget Estimates, February 1994. Aircraft Procurement, Air Force. Volume 1. 1994. Defense Technical Information Center. https://doi.org/10.21236/ada277389
• Depiro, Maxwell. n.d. “Strut Fuel Injector Penetration and Mixing Enhancement for a Dual-Mode Scramjet.” PhD diss., University of Virginia. https://doi.org/10.18130/v3h292
• Deprés, D., and P. Brenner. 2012. “Simulation of Afterbody Transonic Flows Using Partially-Averaged Navier Stokes Model for Turbulence.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203025
• Derby, Michael R., Alan J. Wadcock, and Gloria K. Yamauchi. 2003. “Measured Aerodynamic Interaction of Two Tiltrotors.” In Proceedings of the Vertical Flight Society Forum 59 - Phoenix, AZ 2003. The Vertical Flight Society. https://doi.org/10.4050/vfs-f59-000239
• “Design and CFD Analysis of Supercritical Airfoil 0714 under Ground-Level Atmospheric Conditions.” 2024. Journal of Information Systems Engineering and Management. https://doi.org/10.52783/jisem.v9i4.74
• “Design Considerations for a Re-Entry Vehicle Thermal Protection System.” 1963. In Technology of Lunar Exploration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864834.0761.0782
• “Design of a Hypersonic Waverider-Derived Airplane.” 1993. In 31st Aerospace Sciences Meeting. AIAA 1993-401. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-401
• “Design of Experiments for Model Development and Validation.” 2016. In Nonlinear Regression Modeling for Engineering Applications: Modeling, Model Validation, and Enabling Design of Experiments. ASME-Wiley. https://doi.org/10.1115/1.861nonq_ch18
• “Design of the Circulation Control Wing STOL Demonstrator Aircraft.” 1979. In Aircraft Systems and Technology Meeting. AIAA 1979-1842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1842
• “Design Validation and Verification for Non-Intrusive Flight Test Instrumentation (NIFTI) Using Model-Based Systems Engineering (MBSE).” 2026. In MODSIM2025, 26th International Congress on Modelling and Simulation.. Modelling and Simulation Society of Australia and New Zealand. https://doi.org/10.36334/modsim2025.c01.pattarakunnan
• Dessornes, O., D. Scherrer, and P. Novelli. 2001. “Tests of the JAPHAR Dual Mode Ramjet Engine.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1886
• “Determination of Thermal Performance of Char under Heating Conditions Simulating Atmospheric Entry.” 1966. In Thermophysics and Temperature Control of Spacecraft and Entry Vehicles. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864926.0549.0568
• Detore, J., and T. Gaffey. 1969. “The Stopped-Rotor Variant of the Proprotor VTOL Aircraft.” In VTOL Research, Design, and Operations Meeting. AIAA 1969-220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-220
• Deveaux, G. D. 1965. Component Testing XV-9A Hot Cycle Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0627361
• “Development of a Continuous Full Flight-Envelope Simulation from System Identification Models.” 2012. In Aircraft and Rotorcraft System Identification. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600868207.0645.0718
• “Development of the Shock Tunnel and Its Application to Hypersonic Flight.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0701.0758
• Devriendt, Christof, Tim De Troyer, Gert De Sitter, and Patrick Guillaume. 2012. “Transmissibilty-Based Operational Modal Analysis for Flight Flutter Testing Using Exogenous Inputs.” Shock and Vibration 19 (5): 1071–83. https://doi.org/10.1155/2012/938039
• Dey, Subhasish. 2014. “Dimensional Analysis and Similitude.” In GeoPlanet: Earth and Planetary Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-19062-9_11
• Dhayalan, R., Subrahmanyam Saderla, and Ajoy Kanti Ghosh. 2018. “Parameter Estimation of UAV from Flight Data Using Neural Network.” Aircraft Engineering and Aerospace Technology 90 (2): 302–11. https://doi.org/10.1108/aeat-03-2016-0050
• Di Clemente, Marco, Giuseppe Rufolo, and Francesco Battista. 2007. “An Extrapolation from Flight Methodology for a Re-Entry Vehicle Wing Leading Edge Test in a Plasma Wind Tunnel Facility.” In 39th AIAA Thermophysics Conference. AIAA 2007-3895. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3895
• Diamond, John K. 1988. “Miniature PCM Compatible Wideband Spectral Analyzer for Hypersonic Flight Research.” In International Instrumentation Symposium. https://ntrs.nasa.gov/citations/19890040293
• Dias, Joaquim N. 2022. “Flight Test Determination of Power Effects on Longitudinal Stability Using System Identification.” In AIAA AVIATION 2022 Forum. AIAA 2022-3637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3637
• Dias, Joaquim N., and Roberto D. Girardi. 2016. “Two-Point Aerodynamic Model Identification from Dynamic Wind Tunnel Tests.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-2012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2012
• Dibley, Ryan, Michael Allen, Robert Clarke, Joe Gera, and John Hodgkinson. 2005. “Development and Testing of Control Laws for the Active Aeroelastic Wing Program.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6314. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6314
• Dicarlo, Daniel, Philip Brown, and James Hallissy. 1992. “Flight Test Operations Using an F-106B Research Airplane Modified with a Wing Leading-Edge Vortex Flap.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4094. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4094
• Dickes, Edward G., David R. Gingras, Randy S. Hultbertg, and Stefan J. Kloc. 2002. Unmanned Combat Air Vehicle (UCAV) Automated Refueling Simulation Development. Delivery Order 0009: Volume 2: KC-135. Defense Technical Information Center. https://doi.org/10.21236/ada459237
• Dickey, Robert R. 1959. The Effect of Moment of Area Rule Modifications on the Drag, Lift and Pitching Moment Characteristics of an Unswept Aspect Ratio 6 Wing and Body Combination. NASA-MEMO-2-24-59A. NASA. https://ntrs.nasa.gov/citations/19980231999
• Dickhudt, J. 1983. “Scientific Data Processor: Telemetry Preprocessing in the Real-Timeflight Test Environment.” In 2nd Flight Testing Conference. AIAA 1983-2755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2755
• Dicristina, V. 1979. Hypersonic Heat Transfer Test Program in the VKI Longshot Facility. Defense Technical Information Center. https://doi.org/10.21236/ada065645
• Diederich, Franklin W., and Bernard Budiansky. 1948. Divergence of Swept Wings. NACA-TN-1680. NASA. https://ntrs.nasa.gov/citations/19930082318
• Diesperov, V. N., Yu. B. Lifshitz, and O. S. Ryzhov. 1976. “Stabilization Law and Drag in Transonic Range of Velocities.” In Symposium Transsonicum II. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_15
• Dietrick, Robert A. 2013. Hypersonic Flight: Time to Go Operational. Defense Technical Information Center. https://doi.org/10.21236/ad1018856
• DiFranco, Dante A. 1971. The Development of Flying Qualities for Lifting Re-Entry Vehicles during Terminal Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0742246
• Diggins, J. L. 1951. Diffuser Investigations in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0895227
• Dikshit, Abhijnan, Tom Stokkermans, Shawn Lim, and James Wang. 2022. “Effect of Lifting Surface and Tail Configuration on the Aerodynamics and Flight Mechanics of VTOL Aircraft.” In Proceedings of the Vertical Flight Society 78th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0078-2022-17483
• Dillman, Robert, John DiNonno, Richard Bodkin, et al. 2013. “Flight Performance of the Inflatable Reentry Vehicle Experiment 3.” In International Planetary Probe Workshop (IPPW-10). https://ntrs.nasa.gov/citations/20140000147
• Dillon, J. L., and T. R. Creel Jr. 1978. Aerodynamic Characteristics at Mach Number 0.2 of a Wing-Body Concept for a Hypersonic Research Airplane. NASA-TP-1189. NASA. https://ntrs.nasa.gov/citations/19780017116
• Dillon, J. L., and J. L. Pittman. 1978. Aerodynamic Characteristics at Mach 6 of a Wing-Body Concept for a Hypersonic Research Airplane. NASA-TP-1249. NASA. https://ntrs.nasa.gov/citations/19780022112
• Dilmi, Smain. 2022. “Enhancing Flight Envelope for a Nonlinear Aeroelastic Wing-Section Using Adaptive Fuzzy Sliding Mode Control Law.” Journal of Aerospace Engineering 35 (3): 04022009. https://doi.org/10.1061/(asce)as.1943-5525.0001401
• “Dimensional Analysis and Dynamic Similitude.” 2009. In Introduction to Fluid Mechanics. CRC Press. https://doi.org/10.1201/9781420085259-9
• “Dimensional Analysis and Physical Similitude.” 2014. In Flow, Deformation and Fracture. Cambridge University Press. https://doi.org/10.1017/cbo9781139030014.005
• Dimensional Analysis and Similitude. 2024. Wiley. https://doi.org/10.1002/9781394266173.ch5
• Dimopoulos, Thomas, Pericles Panagiotou, and Kyros Yakinthos. 2019. “Stability Study and Flight Simulation of a Blended-Wing-Body UAV.” MATEC Web of Conferences 304: 02013. https://doi.org/10.1051/matecconf/201930402013
• Ding, Feng, Jun Liu, Chi-bing Shen, and Wei Huang. 2015. “Simplified Osculating Cone Method for Design of a Waverider.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-43934
• Ding, Feihao, Yan Ren, and Gecheng Zha. 2026. “Numerical Study of High Lift Performance of a Drooped CoFlow Jet Supercritical Airfoil with Flap.” In AIAA AVIATION 2026 Forum. AIAA 2026-4143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4143
• Ding, Pengchong, and Li Zhou. 2022. “Distributed Flexible Drive of Trailing Edge Variable Camber Wing.” In Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2022, edited by Daniele Zonta, Zhongqing Su, Branko Glisic. SPIE. https://doi.org/10.1117/12.2611738
• Dingell, Charles W., Clemente Quintana, David Scott Hafermalz, and John F. Keener. 1999. “Updated Environmental Control System for the X-38 Crew Return Vehicle.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/1999-01-1935
• Dinonno, J. M., F. M. Cheatwood, S. J. Hughes, et al. 2016. “HIAD on ULA (HULA) Orbital Reentry Flight Experiment Concept.” In International Planetary Probe Workshop. https://ntrs.nasa.gov/citations/20160010175
• DiOttavio, James, Joseph Andrews, Russ Altieri, and William Welsh. 2014. “Ground and Flight Testing of a Hub Mounted Vibration Suppression System.” In Proceedings of the Vertical Flight Society 70th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0070-2014-9489
• Dippold, Vance F., III. 2022. High Speed Inlet Distortion Test for the X 59 Low Boom Flight Demonstrator in the NASA Glenn 8-by 6-Foot Supersonic Wind Tunnel. E-20056. Glenn Research Center. https://ntrs.nasa.gov/citations/20220010443
• “Direct Numerical Simulations of Hypersonic Boundary Layer Transition over a Hypersonic Transition Research Vehicle Model Lifting Body at Different Angles of Attack.” 2023. Physics of Fluids 35 (4): 044111. https://doi.org/10.1063/5.0146651
• Dirling, R., Jr., C. Swain, and T. Stokes. 1975. “The Effect of Transition and Boundary Layer Development on Hypersonic Reentry Shape Change.” In 10th Thermophysics Conference. AIAA 1975-673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-673
• Diskin, Glenn S., and G. Burton Northam. 1987. Effects of Scale on Supersonic Combustor Performance. AIAA PAPER 87-2164. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19870058170
• Disotell, Kevin J., Carson J. Nietert, Julia A. Taylor, et al. 2026. “Subscale Flight and Wind Tunnel Testing of STUART: Transportable, Autonomous Aerial Rescue Vehicle.” In AIAA AVIATION 2026 Forum. AIAA 2026-4270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4270
• “Distributed Electric Propulsion.” 2018. Aerospace Testing International 2018 (4): 14–14. https://doi.org/10.12968/s1478-2774(23)50178-2
• Dittmar, James. 1989. “Comparison of Propeller Cruise Noise Data Taken in the NASA Lewis 8-by 6-Foot Wind Tunnel with Other Tunnel and Flight Data.” In 12th Aeroacoustic Conference. AIAA 1989-1059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1059
• Dittmar, James H., and Paul L. Lasagna. 1982. “A Preliminary Comparison between the SR-3 Propeller Noise in Flight and in a Wind Tunnel.” Journal of the Acoustical Society of America 71 (S1): S29-S29. https://doi.org/10.1121/1.2019314
• Dittmar, J. H., P. L. Lasagna, and K. G. Mackall. 1983. A Preliminary Comparison between the SR-6 Propeller Noise in Flight and in a Wind Tunnel. NASA-TM-83341. NASA. https://ntrs.nasa.gov/citations/19830016016
• DiviaHarshaVardini, R. C., Arul K. Prakash, and G. Rajesh. 2023. “Assessment of Modified 𝛾-Model for Hypersonic Boundary Layer Transition Prediction Considering Leading Edge Bluntness.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3017
• Dix, R. W. 1964. Engineering Simulation of Powered Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0604865
• Dix, R. E., and G. R. Mattasits. 1980. Comparison of Wind Tunnel and Flight Test Measurements of Static Aerodynamic Loading of a Captive Store. Defense Technical Information Center. https://doi.org/10.21236/ada087237
• Dixon, Nolan L., and Douglas F. Hunsaker. 2023. “A Theoretical Trade-Off between Wave Drag and Sonic Boom Loudness Due to Equivalent Area Changes on a Supersonic Body.” In AIAA SCITECH 2023 Forum. AIAA 2023-1512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1512
• Djayapertapa, Lesmana, and Christian Allen. 2002. “Numerical Simulation of Transonic Flutter Suppression by Active Control.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2713
• Djojodihardjo, Harijono. 2023. “Aeroelastic Experiments-Ground Vibration and Flight Flutter Test Case Studies.” In Introduction to Aeroelasticity. Springer Nature Singapore. https://doi.org/10.1007/978-981-16-8078-6_14
• Doan, Andrew, Adam Johnson, Tony Loogman, Paul Bremner, Joel Sills, and Erica Bruno. 2020. “End-to-End Assessment of Artemis-1 Development Flight Instrumentation.” In 38th Annual Conference on Experimental and Applied Mechanics (IMAC XXXVIII). https://ntrs.nasa.gov/citations/20200003089
• Dods, J. B., Jr., and R. D. Hanly. 1972. “In-Flight Aeroacoustic Environments on Prospective Space Shuttle Vehicles.” In NASA Space Shuttle Technol. Conf.. https://ntrs.nasa.gov/citations/19720023219
• Dodson, Michael G. 2005. An Historical and Applied Aerodynamic Study of the Wright Brothers’ Wind Tunnel Test Program and Application to Successful Manned Flight. Defense Technical Information Center. https://doi.org/10.21236/ada437187
• Dodson, R. O., Jr. 1982. “Comparison of Flight Measured, Predicted and Wind Tunnel Measured Winglet Characteristics on a KC-135 Aircraft.” In NASA. Dryden Flight Research Facility KC-135 Winglet Program Rev.. https://ntrs.nasa.gov/citations/19840019623
• Doebler, William. 2021. “2pPA7: Simulated X-59 on- and off-Design Sonic Boom Levels in Realistic Atmospheres for Noise Dose Range Estimation.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f248e
• Doebler, William, Alexandra Loubeau, and Victor Sparrow. 2018. “Sonic Boom Carpet Widths for NASA’s Low Boom Flight Demonstrator Using Realistic Atmospheric Profiles in the Western Hemisphere.” Journal of the Acoustical Society of America 143 (3_Supplement): 1913–1913. https://doi.org/10.1121/1.5036232
• Doebler, William Jeffrey, and Jonathan Rathsam. 2020. “How Loud Is X-59’s Shaped Sonic Boom?” Proceedings on Meetings in Acoustics (POMA) 36 (1). https://ntrs.nasa.gov/citations/20205002229
• Doengi, F., D. Dinkler, and B. Kroeplin. 1995. “Active Panel Flutter Suppression Using Self-Sensing Piezoactuators.” In 36th Structures, Structural Dynamics and Materials Conference. AIAA 1995-1078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1078
• Doggett, R. V., Jr., and R. H. Ricketts. 1980. Dynamic Response of a Forward-Swept-Wing Model at Angles of Attack up to 15 Deg at a Mach Number of 0.8. NASA-TM-81863. NASA. https://ntrs.nasa.gov/citations/19810003937
• Doggett, Robert V., Jr., Jose A. Rivera Jr., and Eric C. Stewart. 1995. Flutter Clearance Flight Tests of an OV-10A Airplane Modified for Wake Vortex Flight Experiments. NASA-TM-109168. NASA. https://ntrs.nasa.gov/citations/19950019961
• Doherty, David. n.d.-a. “Electropermanent Free-Flight Model Release System for the Hypersonic X3/R Impulse Facility.” PhD diss., The University of Queensland. https://doi.org/10.14264/30640a6
• Doherty, Luke. n.d.-b. “Flowpath Design for a Dual Mode Mach 5 Scramjet.” PhD diss., The University of Queensland. https://doi.org/10.14264/346509
• Doherty, J. 1978. “Ramjet Ground and Flight Test Performance Correlations.” In 14th Joint Propulsion Conference. AIAA 1978-936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-936
• Doherty, John J., Handing Wang, and Yaochu Jin. 2018. “Use of Global Drag Rise Boundaries to Investigate Ill-Posed Transonic Airfoil Optimization.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3953
• Doig, G. 2014. “Transonic and Supersonic Ground Effect Aerodynamics.” Progress in Aerospace Sciences 69: 1–28. https://doi.org/10.1016/j.paerosci.2014.02.002
• Doko, Sayogyo, and Rianto Sasongko. 2026. “Parameter Estimation of Short-Period Low Order Equivalent System for Fighter Aircraft under Extreme Flight Conditions.” American Journal of Aerospace Engineering 12 (1): 1–11. https://doi.org/10.11648/j.ajae.20261201.11
• Dolan, C. 1970. “Refurbishable Ablative Thermal Protection System Concepts for a Multi-Mission Lifting Entry Vehicle.” In Advanced Space Transportation Meeting. AIAA 1970-277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-277
• Doll, Carsten, Maurice Hoogreef, Pierluigi Iannelli, Henk Jentink, and Daniel Kierbel. 2024. “Final Design, Manufacturing and Testing of the Clean Sky 2 Distributed Electric Propulsion Scaled Flight Demonstrator D08 DEP-SFD.” In AIAA SCITECH 2024 Forum. AIAA 2024-1304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1304
• Dolnik, Alexander, and Dan Michaels. 2025. “Experimental Study of Mode Transition in a Cavity-Based Dual-Mode Scramjet Combustor.” In AIAA SCITECH 2025 Forum. AIAA 2025-0956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0956
• Dolvin, Douglas. 2008. “Hypersonic International Flight Research and Experimentation (HIFiRE) Fundamental Science and Technology Development Strategy.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2581
• Dolvin, Douglas. 2009. “Hypersonic International Flight Research and Experimentation Technology Development and Flight Certification Strategy.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7228
• Dominick, Floyd L., and Joseph C. Watts. 1967. Continued Engineering Flight Test of the YOH-6A Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ada951581
• Don, Michael, and Mitchell Grabner. 2022. A Field-Programmable Gate Array (FPGA)-Based Instrumentation System for an Embedded Flight Controller. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1156875
• Donegan, James J. 1954. Matrix Methods for Determining the Longitudinal-Stability Derivatives of an Airplane from Transient Flight Data. NACA-TR-1169. NASA. https://ntrs.nasa.gov/citations/19930090974
• Donegan, James J., and Henry A. Pearson. 1952. Matrix Method of Determining the Longitudinal-Stability Coefficients and Frequency Response of an Aircraft from Transient Flight Data. NACA-TR-1070. NASA. https://ntrs.nasa.gov/citations/19930092115
• Donelli, Raffaele, D. de Rosa, M. Di Clemente, et al. 2009. “Laminar-Turbulent Transition Flight Experiment on the EXPERT Capsule.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7214
• Donelli, Raffaele, Antonio Schettino, Jean Perraud, Douglas Fletcher, and Sebastien Paris. 2005. “Design of a Laminar-Turbulent Transition Flight Experiment.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3410
• Donelson, John, William Lewerenz, and Roger Durbin. 1989. “UHB Demonstrator Flight Test Program: Phase 2.” In 25th Joint Propulsion Conference. AIAA 1989-2582. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2582
• Dong, C., F. Wu, Y. Liu, Z. Huang, and Y. Cai. 2023b. “Fast Trajectory Planning and Guidance for Vertical Landing Reusable Launch Vehicle.” IET Conference Proceedings 2023 (21): 129–34. https://doi.org/10.1049/icp.2023.3008
• Dong, Haibo, and Xiaolin Zhong. 1998. “High-Order Semi-Implicit Simulation of Hypersonic Boundary Layer Stability and Transition.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-127
• Donohue, James. 2013. “Dual-Mode Scramjet Flameholding Operability Measurements.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-698. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-698
• Donovan, J. F., and M. S. Selig. 1989. “Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University.” In Lecture Notes in Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-84010-4_4
• Doo, Johnny T., Marilena D. Pavel, Arnaud Didey, et al. 2021. NASA Electric Vertical Takeoff and Landing (eVTOL) Aircraft Technology for Public Services – a White Paper. International Vehicle Research, Inc. https://ntrs.nasa.gov/citations/20205000636
• Dooley, L. W., and R. D. Yeary. 1979. Flight Test Evaluation of the High Inertia Rotor System. Defense Technical Information Center. https://doi.org/10.21236/ada071648
• Dorobantu, Andrei, Peter J. Seiler, and Gary J. Balas. 2013. “Validating Uncertain Aircraft Simulation Models Using Flight Test Data.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4984. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4984
• Dorsey, John, David Myers, and Carl Martin. 2000. “Reusable Launch Vehicle Tank/intertank Sizing Trade Study.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-1043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1043
• Dougherty, Edward R. n.d. “Optimal Experimental Design.” In Optimal Signal Processing Under Uncertainty. SPIE. https://doi.org/10.1117/3.2317891.ch5
• Dougherty, George. 2018. “Promoting Disruptive Military Innovation: Best Practices for DoD Experimentation and Prototyping Programs.” Defense Acquisition Research Journal 25 (1): 2–29. https://doi.org/10.22594/dau.17-782.25.01
• Dougherty, Nathan S. 2021a. “The AEDC 10-Deg Cone Wind Tunnel-Flight Laminar-Turbulent Correlation Program.” In AIAA Scitech 2021 Forum. AIAA 2021-1875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1875
• Dougherty, N. Sam. 2021b. “The AEDC 10-Deg Cone Wind Tunnel/Flight Laminar-Turbulent Correlation Program (Invited Historical).” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20205009427
• Dougherty, N., Jr., and D. Fisher. 1980. “Boundary-Layer Transition on a 10-Deg Cone: Wind Tunnel/flight Correlation.” In 18th Aerospace Sciences Meeting. AIAA 1980-154. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-154
• Douglas Aircraft CO INC Santa Monica CA. 1963. Army-Navy Instrumentation Program. Fixed Wing Research Phase. Defense Technical Information Center. https://doi.org/10.21236/ad0407056
• Dowell, Earl H. 1996. Limit Cycle Oscillations (LCO) and Nonlinear Aeroelastic Wing Response. Defense Technical Information Center. https://doi.org/10.21236/ada325524
• Dowell, E. H., and D. B. Bliss. 1978. Wind Tunnel Wall Interference. Defense Technical Information Center. https://doi.org/10.21236/ada055735
• Dowell, Earl H., and Kenneth C. Hall. 2003. Theoretical Prediction of Limit Cycle Oscillations in Support of Flight Flutter Testing. Defense Technical Information Center. https://doi.org/10.21236/ada426408
• Downing, J. Micah. 1992. “Lateral Spread of Sonic Boom Measurements from US Air Force Boomfile Flight Tests.” In NASA. Langley Research Center, High-Speed Research: Sonic Boom, Volume 1. https://ntrs.nasa.gov/citations/19920024639
• Downing, Micah, and Noel Zamot. 1995. “USAF Flight Test Investigation of Focused Sonic Booms.” Journal of the Acoustical Society of America 97 (5_Supplement): 3257–3257. https://doi.org/10.1121/1.411682
• Downs, Robert. 2021. “2pPA10: Investigation of Sonic Boom Waveforms and Metrics at Elevated Receiver Locations.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f2486
• “Drag and Propulsive Efficiency of a Light Aircraft Based on a New Flight Test Technique.” 1990. In 28th Aerospace Sciences Meeting. AIAA 1990-233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-233
• “Drag Coefficient Variations of an Oscillating NACA 0012 Airfoil.” 2008. Journal of the Korean Society for Aeronautical & Space Sciences 36 (2): 137–45. https://doi.org/10.5139/jksas.2008.36.2.137
• Drag Polar Measurement in Level Flight. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch7
• Dragna, Didier. 2021. “2aPA7: Sonic Boom Reflection over Irregular Terrain.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f2426
• Dragone, Thomas. 2000. “Structural Innovations in Design, Manufacturing, and Testing on the X-34 Reusable Launch Vehicle.” In Space 2000 Conference and Exposition. AIAA 2000-5309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5309
• Dragos Daniel, Ion Guta, Gheorma Cristian-Tudor, Pascale Catalin, Berceanu Radu, and Neagu Mihai. 2026. “Flight Control System for Ultra-Light Aircraft Conversion to VTOL Unmanned Aircraft Vehicle.” Preprint, . https://doi.org/10.20944/preprints202601.0351.v1
• Drain, Bethany A., Laura K. Kushner, Edward T. Schairer, and James T. Heineck. 2017. “Model Deformation Measurements of the Truss-Braced Wing Aircraft in the NASA Ames 11-By 11-Ft Transonic Wind Tunnel.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1054
• Drake, Hubert M. 1949a. Measured Characteristics of the Douglas D-558-1 Airplane (BuAero No. 37971) in Two Landings. NACA-RM-L9D20a. NASA. https://ntrs.nasa.gov/citations/19930085907
• Drake, Hubert M. 1949b. Measurement of the Dynamic Lateral Stability of the Douglas D-558-1 Airplane (BuAero No. 37971) in Rudder Kicks at a Mach Number of 0.72. NACA-RM-L9D06a. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930085857
• Drake, H. M. 1964. Aerodynamic Testing Using Special Aircraft. NASA-TM-X-51605. NASA. https://ntrs.nasa.gov/citations/19650025624
• Drake, David, and S. N. Balakrishnan. 2004. “Theta-D Controller-Filter for Aeroelastic Flutter Suppression.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4816. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4816
• Drake, Hubert M., and John B. McKay. 1953. Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight. NACA-RM-L53E04. NASA. https://ntrs.nasa.gov/citations/19930087560
• Drake, Aaron, and William Solomon. 2010. “Flight Testing of a 30-Degree Sweep Laminar Flow Wing for a High-Altitude Long-Endurance Aircraft.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4571. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4571
• Drake, H. M., and W. C. Williams. 1958. The Research Airplane- past, Present, and Future. NASA. https://ntrs.nasa.gov/citations/19650070849
• Drakin, I. I. 1963. Aerodynamic and Radiation Heating during Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0295828
• Draper, A., M. Buck, and D. Selegan. 1983. “Aerospace Technology Demonstrators/research and Operational Options.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1054
• Draper, James S., and James P. Moran. 1973. A Study of Wind Tunnel Simulation of High Altitude Rocket Plumes. Defense Technical Information Center. https://doi.org/10.21236/ad0755840
• Drees, J. M. 1976. The Art and Science of Rotary Wing Data Correlation. Bell Helicopter Textron. https://ntrs.nasa.gov/citations/19760057068
• Dresser, H., C. Newberry, T. Surber, K. Szema, and S. R. Chakravarthy. 1990. “A Comparison of CFD, Wind Tunnel, and Flight Pressures on the Space Shuttle Orbiter Payload Bay Doors.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3213
• Dreyer, Nathan, Erik R. Fernandez, Andrew La Sorsa, Justin D. Sprunger, and Kareem A. Ahmed. 2026. “Design and Characterization of a High-Enthalpy Hypersonic Wind Tunnel: The HyperReact Facility.” In AIAA SCITECH 2026 Forum. AIAA 2026-2861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2861
• Dreyer, C., and D. Shoch. 1986. “F-16 Flutter Testing at Eglin Air Force Base.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9819
• Drinkwater, F. J., III, H. C. Quigley, L. S. Rolls, and H. L. Turner. 1964. V/stol Handling Qualities as Determined by Flight Test and Simulation Techniques. NASA. https://ntrs.nasa.gov/citations/19650032844
• Drinkwater, F. J., III, B. A. Schlaff, and M. D. White. 1958. A Comparison of Flight-Measured Carrier- Approach Speeds with Values Predicted by Several Different Criteria for 41 Fighter-Type Airplane Configurations. NACA-RM-A57L11. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19670022400
• Driscoll, T., R. Stockdale, and F. Schelke. 1975. “Determination of Aerodynamic Coupling Derivatives through Flight Test.” In Guidance and Control Conference. AIAA 1975-1119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1119
• Driver, C. 1974. “Advanced Supersonic Transport Design Developments.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-987
• Droney, Christopher K., Anthony J. Sclafani, Neal A. Harrison, Adam D. Grasch, and Michael D. Beyar. 2020. Subsonic Ultra Green Aircraft Research: Phase III – Mach 0.75 Transonic Truss-Braced Wing Design. NASA/CR-20205005698. NASA. https://ntrs.nasa.gov/citations/20205005698
• Drovandi, Christopher C., and Minh-Ngoc Tran. 2018. “Improving the Efficiency of Fully Bayesian Optimal Design of Experiments Using Randomised Quasi-Monte Carlo.” Bayesian Analysis 13 (1): 139–62. https://doi.org/10.1214/16-ba1045
• Du, Wei. n.d. “Dynamic Modeling and Ascent Flight Control of Ares-I Crew Launch Vehicle.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/etd-180810-1029
• Du, Ziliang, Zhiqiang Wan, Yuting Dai, Siyan Zhu, and Chao Yang. 2017. “Robust Aeroelastic Design Optimization of Hypersonic Vehicle with Uncertainties in Aerodynamic Loads, Heat Flux, and Structure.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-1938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1938
• Du, Huan, Xu Zhang, and Yumin Ma. 2025. “Study on Control Method of Angle of Attack in Subscale Flight Testing.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-9771-4_47
• Dual-Mode Combustion Scramjet. 2022. Wiley. https://doi.org/10.1002/9781119640646.ch7
• Duan, Zhiwei, Zhixiang Xiao, and Song Fu. 2012. “Simulation of Transition Triggered by Isolated Roughness in Hypersonic Boundary Layer.” In 42nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2012-3076. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3076
• Dubben, James, and Charles Denegri. 2007. “Underwing Missile Aerodynamic Effects on Flight-Measured Limit Cycle Oscillations.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-1801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1801
• Duberg, J. E. 1957. “Some NACA Research on Effect of Transient Heating on Aircraft Structures.” Journal of Fluids Engineering 79 (5): 1014–18. https://doi.org/10.1115/1.4013207
• Dubin, A. 1978. “Supersonic Transport Market Penetration Model.” In Conference on Air Transportation: Technical Perspectives and Forecasts. AIAA 1978-1557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1557
• Dublin, M., and R. Peller. 1975. “Flight Flutter Testing of Supersonic Interceptors.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003022
• Dudley, Jonathan, and Jason Torres. 2007. “Viscous GBU38 Store Separation from Parent F15E Aircraft during Transonic Flight with Flight Test Comparison.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-72. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-72
• Dugan, D. C., R. G. Erhart, and L. G. Schroers. 1980. The XV-15 Tilt Rotor Research Aircraft. NASA-TM-81244. NASA. https://ntrs.nasa.gov/citations/19810001546
• Duggirala, Ravi, Christopher Roy, and Joseph Schetz. 2009. “Analysis of Interference Drag for Strut-Strut Interaction in Transonic Flow.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-51. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-51
• Duke, E. L. 1982. Automated Flight Test Maneuvers: The Development of a New Technique. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19840061677
• Duke, E. 1983. “Development of a Flight Test Maneuver Autopilot for a Highly Maneuverable Aircraft.” In 21st Aerospace Sciences Meeting. AIAA 1983-61. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-61
• Duke, Eugene L., Marle D. Hewett, Randal W. Brumbaugh, David M. Tartt, Robert F. Antoniewicz, and Arvind K. Agarwal. 1988. The Use of an Automated Flight Test Management System in the Development of a Rapid-Prototyping Flight Research Facility. NASA-TM-100435. NASA. https://ntrs.nasa.gov/citations/19880011512
• Duke, Eugene L., Frank P. Jones, and Ralph B. Roncoli. 1986. Development and Flight Test of an Experimental Maneuver Autopilot for a Highly Maneuverable Aircraft. NASA-TP-2618. NASA. https://ntrs.nasa.gov/citations/19880011769
• Duke, E. L., and D. P. Lux. 1983. The Application and Results of a New Flight Test Technique. AIAA PAPER 83-2137. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19830060741
• Dukeman, Gregory A., and Michael W. Gallaher. 1998. Guidance and Control Concepts for the X-33 Technology Demonstrator. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990102412
• Dukes, Theodor A. 1970. Feedback Control of VTOL Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0871424
• Dumbacher, Dan, and Paul Klevatt. 1994. “DC-XA: First Step Top a Reusable Launch Vehicle.” In Space Programs and Technologies Conference and Exhibit. AIAA 1994-4682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-4682
• Dungan, G., and C. Clark. 1994. “Flight Testing Large Lateral Asymmetries on Highly Augmented Fighter/attack Aircraft.” In Biennial Flight Test Conference. AIAA 1994-2138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2138
• Dungan, Sean D., Vincenzo Russo, and Christoph Brehm. 2026. “Solid Particulate Transition Investigation of the HIFLIER Hypersonic Flight Experiment.” In AIAA SCITECH 2026 Forum. AIAA 2026-1146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1146
• Dunlap, Roger, and A. M. Kuethe. 1961. Effects of Cooling on Transition in the Boundary Layer on a Hemisphere in Simulated Hypersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0256234
• Dunning, Peter D., Bret K. Stanford, Hyunsun A. Kim, and Christine Jutte. 2014. “Aeroelastic Tailoring of a Plate Wing with Functionally Graded Materials.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0344
• Duong, Duc-Lam, Tapio Helin, and Jose Rodrigo Rojo-Garcia. 2023. “Stability Estimates for the Expected Utility in Bayesian Optimal Experimental Design.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3025075/v1
• Duran, Daryl. 2026. “Development and Flight Testing of the Stability Augmentation System for the XB-1 Supersonic Demonstrator.” In AIAA SCITECH 2026 Forum. AIAA 2026-2637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2637
• Duran, Sebastian, and Jingyi Zeng. 2026. “An Automated Design-to-CFD Workflow for Hypersonic Waverider Analysis.” In 2026 Regional Student Conferences. AIAA 2026-109216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-109216
• Durand, W. F., and E. P. Lesley. 1926. Comparison of Tests on Air Propellers in Flight with Wind Tunnel Model Tests on Similar Forms. NACA-TR-220. NASA. https://ntrs.nasa.gov/citations/19930091287
• “The Duration and Properties of the Flow in a Hypersonic Shock Tunnel.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0513.0546
• Durbin, Enoch J. 1959. “The Systems Concept in Planning Flight Test Instrumentation.” In Instrumentation Systems. Elsevier. https://doi.org/10.1016/b978-1-4831-9728-9.50011-4
• Durmaz, Seher, and Metin O. Kaya. 2013. “Aeroelastic Response of an Aircraft Wing Modeled as a Thin-Walled Composite Beam.” In Volume 1: Advances in Aerodynamics. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2013-64261
• Durston, Don. n.d. “NASA Supersonics Research — Leading toward Quiet Supersonic Flight!!” In EAA AirVenture 2022. https://ntrs.nasa.gov/citations/20220009235
• Durston, Don. 2023a. “NASA Supersonics Research and the X-59 — How They Will Benefit You!!” In Discover NASA With NASA CT Space Grant. https://ntrs.nasa.gov/citations/20230002822
• Durston, Don. 2023b. “Nasa Supersonics Research and the X-59 —to Enable Future Supersonic Travel!” In NASA Connecticut Space Grant Consortium. https://ntrs.nasa.gov/citations/20230011538
• Durston, Donald, Susan Cliff, Thomas Wayman, Jason Merret, Alaa Elmiligui, and Linda Bangert. 2011. “Near Field Sonic Boom Test on Two Low-Boom Configurations Using Multiple Measurement Techniques at NASA Ames (Invited).” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3333
• Durston, Donald A., Alaa A. Elmiligui, Susan E. Cliff, Courtney Winski, Melissa B. Carter, and Eric Walker. 2014. “Experimental and Computational Sonic Boom Assessment of Boeing N+2 Low Boom Models.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2140
• Dusterberry, J. C. 1964. Manned Flight Simulation Facilities. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19660003380
• Dutton, J. C., and A. L. Addy. 1980. A Theoretical and Experimental Investigation of Transonic Flow in the Throat Region of Annular Axisymmetric, Supersonic Nozzles. Defense Technical Information Center. https://doi.org/10.21236/ada084787
• Duval, R. 1981. “The Use of Frequency Methods in Rotorcraft System Identification.” In 1st Flight Test Conference. AIAA 1981-2386. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2386
• Dwivedi, Anubhav, and G. S. Sidharth. 2026. “Nonlinear Analysis of Reattaching Hypersonic Boundary Layer Transition to Turbulence.” In AIAA AVIATION 2026 Forum. AIAA 2026-4298. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4298
• Dwyer, Jim. 1994. “Learjet Model 60 Flight Test Program.” In Biennial Flight Test Conference. AIAA 1994-2158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2158
• Dykes, John W., and Dimitri N. Mavris. 2016. “A Methodology for the Robust Design Optimization of Flight Dynamic System Identification Experiments.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-2008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2008
• “The Dyna-Soar Cancellation.” 2006. In US Hypersonic Research and Development. Routledge. https://doi.org/10.4324/9780203012994-14
• “Dynamic Lateral-Directional Stability Theory and Flight Test Methods.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0311.0322
• “Dynamic Longitudinal Stability Flight Test Methods and Data Reduction.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0247.0254
• “Dynamic Stability and Control.” n.d. In Fundamentals of Airplane Flight Mechanics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-46573-7_11
• Dziuba, Dylan, Byung-Young Min, Shawn Sandor, et al. 2024. “Wind Tunnel Testing of X2 Technology Spinning Coaxial Hubs with Aspirated Inlets – Comparison between Two Wind Tunnel Models and with CFD.” In Proceedings of the Vertical Flight Society 80th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0080-2024-1176
• “E- and c-Optimal Designs.” n.d. In Lecture Notes in Statistics. Springer-Verlag. https://doi.org/10.1007/0-387-31610-8_8
• E-33 In Flight Propulsion Measurement Committee. n.d.-a. Advanced Ducted Propulsor in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air5450
• E-33 In Flight Propulsion Measurement Committee. n.d.-b. In-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air1703a
• E-33 In Flight Propulsion Measurement Committee. n.d.-c. In-Flight Thrust Determination for Aircraft with Thrust Vectoring. SAE International. https://doi.org/10.4271/air6007
• E-33 In Flight Propulsion Measurement Committee. n.d.-d. Propeller/Propfan in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air4065
• E-33 In Flight Propulsion Measurement Committee. n.d.-e. Time-Dependent in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air5020
• E-33 In Flight Propulsion Measurement Committee. n.d.-f. Uncertainty of in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air1678a
• E21 Committee. n.d. Test Method for Calculation of Stagnation Enthalpy from Heat Transfer Theory and Experimental Measurements of Stagnation-Point Heat Transfer and Pressure. ASTM International. https://doi.org/10.1520/e0637-98
• Eckert, E. R. G. 1956. “Engineering Relations for Heat Transfer and Friction in High-Velocity Laminar and Turbulent Boundary-Layer Flow over Surfaces with Constant Pressure and Temperature.” Journal of Fluids Engineering 78 (6): 1273–83. https://doi.org/10.1115/1.4014011
• Eckhardt, Brad. 2001. “International Space Station’s X-38 Crew Return Vehicle Cabin Condensation Study.” In 15th AIAA Computational Fluid Dynamics Conference. AIAA 2001-2654. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2654
• Eckstrom, C., and C. Spain. 1982. “Design Considerations and Experiences in the Use of Composite Material for an Aeroelastic Research Wing.” In 23rd Structures, Structural Dynamics and Materials Conference. AIAA 1982-678. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-678
• “ECO Demonstrator Begins Flight Testing.” 2018. Aerospace Testing International 2018 (1): 12–12. https://doi.org/10.12968/s1478-2774(23)50032-6
• “Ecodemonstrator Flight Test Program Takes Off.” 2020. Aerospace Testing International 2020 (3): 12–12. https://doi.org/10.12968/s1478-2774(22)50336-1
• Edelman, Louis M. n.d. “Pathway to a 21st Century NASA X-Plane through Hampton Roads.” In Williamsburg Comic Con. https://ntrs.nasa.gov/citations/20240011663
• Edenborough, H. 1967. “Investigation of Tilt-Rotor VTOL Aircraft Rotor-Pylon Stability.” In 5th Aerospace Sciences Meeting. AIAA 1967-17. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-17
• Edge, D., and John Perkins. 1995. “Three-Dimensional Aerodynamic Analysis of a Subsonic Transport High-Lift Configuration and Comparisons with Wind-Tunnel Test Results.” In 13th Applied Aerodynamics Conference. AIAA 1995-1846. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1846
• Edquist, Karl. 2006. “Computations of Viking Lander Capsule Hypersonic Aerodynamics with Comparisons to Ground and Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6137
• Edwards, J. B. 1961. “Fundamental Aspects of Propulsion for Laminar Flow Aircraft.” In Boundary Layer and Flow Control. Elsevier. https://doi.org/10.1016/b978-1-4832-1323-1.50019-1
• Edwards, C. L. W. 1974. A Forebody Design Technique for Highly Integrated Bottom-Mounted Scramjets with Application to a Hypersonic Research Airplane. NASA-TM-X-71971. NASA. https://ntrs.nasa.gov/citations/19750003901
• Edwards, C. L. W. 1976. A Forebody Design Technique for Highly Integrated Bottom-Mounted Scramjets with Application to a Hypersonic Research Airplane. NASA-TN-D-8369. NASA. https://ntrs.nasa.gov/citations/19770009076
• Edwards, J. 1981. “Flight Test Results of an Active Flutter Suppression System Installed on a Remotely Piloted Research Vehicle.” In Dynamics Specialists Conference. AIAA 1981-655. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-655
• Edwards, T. 1992. “CFD Applications in Hypersonic Flight.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5025
• Edwards, John W. 1998. Calculated Viscous and Scale Effects on Transonic Aeroelasticity. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19980202470
• Edwards, C. L. W., and S. R. Cole. 1983. Predictions of Entry Heating for Lower Surface of Shuttle Orbiter. NASA-TM-84624. NASA. https://ntrs.nasa.gov/citations/19830021360
• Edwards, Sophia, Rachel U. Constantin, Cary D. Smith, and Mark Gragston. 2024. “Development and Initial Characterization of Adhesive Temperature Sensitive Paint Films for Aerodynamic Heating Measurements.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4275
• Edwards, Stephen, Dimitri Mavris, and Barry Hellman. 2010. “Rocketback Trajectory Figures of Merit for a Reusable Booster Technology Flight Demonstrator.” In AIAA SPACE 2010 Conference & Exposition. AIAA 2010-8667. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8667
• Edwards, F. G., and R. C. Wingrove. 1969. A Technique for Identifying Pilot Describing Functions from Routine Flight-Test Records. NASA-TN-D-5127. NASA. https://ntrs.nasa.gov/citations/19690014464
• “The Effect of Surface Roughness Character on Turbulent Re-Entry Heating.” 1981. In Aerothermodynamics and Planetary Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865510.0083.0108
• “Effects of Aerodynamic Heating and TPS Thermal Performance Uncertainties on the Shuttle Orbiter.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0247.0268
• “Effects of Atmospheric Structure on Radiative Heating for Jupiter Entry Probe.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0003.0021
• “Effects of Wind-Tunnel Disturbances on Hypersonic Boundary-Layer Transition. I, II.” 1972. In 10th Aerospace Sciences Meeting. AIAA 1972-181. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-181
• Efimtsov, B. M., A. Yu. Golubev, V. B. Kuznetsov, et al. 2004. Effect of Transducer Flushness on Measured Surface Pressure Fluctuations in Flight. AIAA Paper 2005-0800. Tsentralni Aerogidrodinamicheskii Inst. https://ntrs.nasa.gov/citations/20050041756
• Egerton, Harry S., and James E. Fitzpatrick. 1967. The Model K-I6B V/STOL Research Amphibious Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0674529
• Eggers, Thino. 2002. “Aerodynamic Analysis of the Dual-Mode Ramjet Vehicle JAPHAR.” In New Results in Numerical and Experimental Fluid Mechanics III. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45466-3_17
• Eggers, Thino. 2003. “Aerodynamic Behaviour of a Liquid Fly-Back Booster in Transonic Cruise Flight.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3422
• Eggers, Thino, and Tarik Barth. 2006. “Aerodynamic Analysis of the DLR Flight Experiment SHEFEX.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8027
• Eggers, Thino, Jose Longo, Marcus Hoerschgen, and Andreas Stamminger. 2005. “The Hypersonic Flight Experiment SHEFEX.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3294
• Eggers, Thino, Jose Longo, John Turner, et al. 2006. “The SHEFEX Flight Experiment: Pathfinder Experiment for a Sky Based Test Facility.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7921
• Eggers, Th., and Ph. Novelli. 1999. “Design Studies for a Mach 8 Dual Mode Ramjet Flight Test Vehicle.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4877
• Eggers, Alfred J., Jr., H. Julian Allen, and Stanford E. Neice. 1958. A Comparative Analysis of the Performance of Long-Range Hypervelocity Vehicles. NACA-TR-1382. NASA. https://ntrs.nasa.gov/citations/19930092363
• Eggers, A. J., Jr., and B. L. Swenson. 1966. Lifting Entry Vehicles for Future Space Missions. AIAA PAPER 66-956. NASA. https://ntrs.nasa.gov/citations/19670035411
• Eggers, A. J., Jr., and B. L. Swenson. 1967. Lifting Entry Vehicles for Future Space Missions. NASA. https://ntrs.nasa.gov/citations/19670043942
• Eggert, Christopher A., Laura White, Joanna N. Schmidt, Ben D. Phillips, and Zachary D. Windous. 2024. “Method for System-Level Multidisciplinary Uncertainty Analysis of Low-Boom Flight Vehicles.” In AIAA SCITECH 2024 Forum. AIAA 2024-1876. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1876
• Eglin, Paul, Martin Embacher, Damien Desvigne, and Enric Roca-Leon. 2025. “Airbus RACER High Speed Demonstrator Flight Tests.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0182
• Ehernberger, L. J., Edward A. Haering Jr., Mary G. Lockhart, and Edward H. Teets. 1992. Atmospheric Analysis for Airdata Calibration on Research Aircraft. AIAA PAPER 92-0293. NASA Hugh L. Dryden Flight Research Facility. https://ntrs.nasa.gov/citations/19920043122
• Ehernberger, L. J., Morton G. Wurtele, and Robert D. Sharman. 1994. “Simple Atmospheric Perturbation Models for Sonic-Boom-Signature Distortion Studies.” In NASA. Langley Research Center, High-Speed Research: 1994 Sonic Boom Workshop: Atmospheric Propagation and Acceptability Studies. https://ntrs.nasa.gov/citations/19950008474
• Ehresman, C. 1981. “The Technological Development History of the Aircraft of World War I.” In Aircraft Systems and Technology Conference. AIAA 1981-1612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1612
• Eichelsdörfer, Jonas. 2026a. “Modal Blending for Active Flutter Suppression.” In AIAA SCITECH 2026 Forum. AIAA 2026-1556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1556
• Eichelsdörfer, Jonas. 2026b. “Open-Source Benchmark Model for Active Flutter Suppression.” In AIAA SCITECH 2026 Forum. AIAA 2026-1555. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1555
• Eisenberg, Joseph D., and Jeffrey V. Bowles. 1986. “Folding Tilt Rotor Demonstrator Feasibility Study.” In Proceedings of the Vertical Flight Society Forum 42 - Washington D.C. 1986. The Vertical Flight Society. https://doi.org/10.4050/vfs-f42-2001
• Eklund, D., R. Baurle, and M. Gruber. 2001. “Numerical Study of a Scramjet Combustor Fueled by an Aerodynamic Ramp Injector in Dual-Mode Combustion.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-379
• El-Kebir, Hamza, and Melkior Ornik. 2020. “In-Flight Air Density Estimation and Prediction for Hypersonic Flight Vehicles.” In 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2020-2412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2412
• El-Sayed, Ahmed F. 2016. “Pulsejet, Ramjet, and Scramjet Engines.” In Fundamentals of Aircraft and Rocket Propulsion. Springer London. https://doi.org/10.1007/978-1-4471-6796-9_5
• El-Sayed, Ahmed F. 2024a. “History and Classification of Aircraft Engines.” In History and Evolution of Aircraft. CRC Press. https://doi.org/10.1201/9781003450115-9
• El-Sayed, Ahmed F. 2024b. “History and Classification of Civil Aircraft.” In History and Evolution of Aircraft. CRC Press. https://doi.org/10.1201/9781003450115-4
• El-Sayed, Ahmed F. 2024c. “History and Classification of Military Aircraft.” In History and Evolution of Aircraft. CRC Press. https://doi.org/10.1201/9781003450115-5
• Elbanna, Hesham, and Leland Carlson. 1989. “Determination of Aerodynamic Sensitivity Coefficients in the Transonic and Supersonic Regimes.” In 27th Aerospace Sciences Meeting. AIAA 1989-532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-532
• Eldredge, R. C., V. W. Horton, and R. E. Klein. 1965. Flight-Determined Low-Speed Lift and Drag Characteristics of the Lightweight m2-f1 Lift- Ing Body. NASA-TN-D-3021. NASA. https://ntrs.nasa.gov/citations/19650023756
• Eldridge-Allegra, Ian K., Tsz Yeung Xu, Kai M. Kruger Bastos, and Earl H. Dowell. 2023. “Computational Study of Transonic Buffet’s Sensitivity to Reynolds Number and Wind Tunnel Wall Effects.” In AIAA SCITECH 2023 Forum. AIAA 2023-1426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1426
• Elhashani, Atahir, Adel Kurban, and Marwa L. Agela. 2014. “Aircraft Free Flight Simulation in a Wind Tunnel.” Applied Mechanics and Materials 541-542: 1390–93. https://doi.org/10.4028/www.scientific.net/amm.541-542.1390
• Elias, Antonio L., and Martin A. Knutson. 1995. “Pegasus Air-Launched Space Booster Flight Test Program.” In AGARD, Space Systems Design and Development Testing. https://ntrs.nasa.gov/citations/19960003894
• Eliassen, O. M. 1965. “Oscillographic Recording or Magnetic Tape Recording for Airborne Data Acquisition.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50008-7
• Elkowitz, Laurie, Andrew Wanchek, Robert Rockwell, Christopher Goyne, and Chloe Dedic. 2023. “Dual-Mode Scramjet Control Using Optical Emission Sensors.” Preprint, Optica Open. https://doi.org/10.1364/opticaopen.24317149.v1
• Elliott, G. 1968. “Hypersonic Lifting Body Optimization.” In Entry Vehicle Systems and Technology Meeting. AIAA 1968-1157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1157
• Elliott, Graydon A., and Roger G. Furgurson. 1978. “800 Shaft Horsepower Advanced Technology Demonstrator Engine.” In Proceedings of the Vertical Flight Society Forum 34 - Washington, D.C. 1978. The Vertical Flight Society. https://doi.org/10.4050/vfs-f34-043
• Ellis, David. 1989. “Overview: Design of an Efficient Lightweight Airframe Structure Forthe National Aerospace Plane.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1406
• Ellis, Macon C., and Clinton E. Brown. 1943. NACA Investigation of a Jet-Propulsion System Applicable to Flight. NACA/TR-802. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050241734
• Ellison, William, and John Latz. 2003. “Design and Flight Testing of the X-35 Air Data System.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5319
• Ellsworth, Joel. 2010. “An Analytical Explanation for the X-43A Flush Air Data Sensing System Pressure Mismatch between Flight and Theory.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4964. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4964
• Ellsworth, J. A., W. R. Fox, D. E. Lovendahl, and J. E. Moore. 1977. Guided Drogue Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ada049164
• Elmer, K. R., and M. C. Joshi. 1994. “Variability of Measured Sonic Boom Signatures.” In NASA. Ames Research Center, High-Speed Research: Sonic Boom, Volume 1. https://ntrs.nasa.gov/citations/19940023694
• Elmer, Kevin, H. Welge, Joseph Salamone, and Robert Cowart. 2013. “SCAMP: Supersonic Passenger Transport Transonic Acceleration Flight Profiles with Considerations of Focused Sonic Boom.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-1065. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1065
• Elmiligui, Alaa, Susan Cliff, Michael Aftosmis, et al. 2011. “Sonic Boom Computations for a Mach 1.6 Cruise Low Boom Configuration and Comparisons with Wind Tunnel Data (Invited).” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3496
• Elmiligui, Alaa, Mohagna Pandya, Melissa Carter, Boris Diskin, and Sudheer Nayani. n.d.-a. “USM3D Simulations for the Third Sonic Boom Prediction Workshop (SBPW-3).” In 2021 AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20205011142
• Elmiligui, Alaa, Mohagna J. Pandya, Melissa B. Carter, Boris Diskin, and Sudheer N. Nayani. n.d.-b. “USM3D Simulations for Third Sonic Boom Workshop.” In SciTech Forum 2021. https://ntrs.nasa.gov/citations/20205002836
• ElSharkawy, Ezzeldin, Vitor T. Valente, Joel S. Rachaprolu, and Eric Greenwood. 2024. “Calibration of an Air Data System for Small Multirotor Aircraft.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4393
• Elshazly, E., Mohammed Kassem, and M. A. Elshafei. 2025. “Aeroelastic Coupled Mode Behavior of Swept Composite Wing.” Journal of Physics: Conference Series 3070 (1): 012001. https://doi.org/10.1088/1742-6596/3070/1/012001
• Elvin, John D. 1996. “Lockheed Martin Approach to a Reusable Launch Vehicle (RLV).” In AIP Conference Proceedings, vol. 361. AIP. https://doi.org/10.1063/1.49950
• Elzey, Michael B., Lewis R. Owens Jr., Richard A. Wahls, and Douglas L. Wilson. 1999. “High Reynolds Number Effects on HSCT Stability and Control Characteristics.” In First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop. https://ntrs.nasa.gov/citations/20000044876
• Emadian, Ata, and Mohammad Sajjadi. 2026. “Data-Driven Estimation of Aerodynamic Coefficients of an Embraer-190 Aircraft Using Dependent Gaussian Processes and Real Flight Data.” Preprint, . https://doi.org/10.2139/ssrn.6982178
• Eminton, E., and W. T. Lord. 1956. “Note on the Numerical Evaluation of the Wave Drag of Smooth Slender Bodies Using Optimum Area Distributions for Minimum Wave Drag.” Journal of the Royal Aeronautical Society 60 (541): 61–63. https://doi.org/10.1017/s0368393100132407
• Emme, E. M. 1976. “With a View to Their Practical Solution: Sixty Years with NACA and NASA, 1915: 1976.” In Winter Colloq. Series. https://ntrs.nasa.gov/citations/19840011209
• Enciu, Daniela. 2019. “Flight Envelope Expansion via Piezoelectric Actuation Receptance Method and Time-Delayed Feedback Control.” International Journal of Modeling and Optimization: 317–21. https://doi.org/10.7763/ijmo.2019.v9.729
• “Energy Analysis of High-Speed Flight Systems.” 1991. In High-Speed Flight Propulsion Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866104.0143.0235
• “Energy Approach to Performance Flight Testing.” 2003. In Flight Testing Of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861840.0143.0151
• Eney, J. 1967. “Navy Variable Stability Studies of Longitudinal Handling Qualities.” In Control and Flight Dynamics Conference. AIAA 1967-576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-576
• Eney, J. 1969. “Flight Evaluation of Power Approach Short Period Dynamics in the Variable-Stability NF-8D.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-896
• Engblom, William, Franco Frate, and Chris Nelson. 2005. “Progress in Validation of Wind-US for Ramjet/Scramjet Combustion.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-1000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1000
• Engelien, Timothy. 1994. “Flight Testing a Ground Collision Warning System on the F-15E.” In Biennial Flight Test Conference. AIAA 1994-2121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2121
• Engelund, Walter C., Scott D. Holland, Charles E. Cockrell Jr., and Robert D. Bittner. 1999. “Propulsion System Airframe Integration Issues and Aerodynamic Database Development for the Hyper-X Flight Research Vehicle.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20040086964
• Engelund, Walter C., Scott D. Holland, Charles E. Cockrell Jr., and Robert D. Bittner. 2000. Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments. AIAA Paper 2000-4006. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000092515
• Engelund, Walt, and Brad Neal. 2013. “X-43A Lessons Learned.” In Hypersonic Lesson Learned Workshop. https://ntrs.nasa.gov/citations/20140008538
• Englar, Robert J. 1970. Two-Dimensional Transonic Wind Tunnel Tests of Three 15-Percent Thick Circulation Control Airfoils. Defense Technical Information Center. https://doi.org/10.21236/ad0882075
• Enkenhus, K. 1969. “Hypersonic Testing in the V.K.I. Longshot Free-Piston Tunnel.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-333
• Ennix, Kimberly A., Frank W. Burcham Jr., and Lannie D. Webb. 1993. “Flight-Determined Engine Exhaust Characteristics of an F404 Engine in an F-18 Airplane.” In AIAA/SAE/ASME/ASEE Joint Propulsion Conference and Exhibit. https://ntrs.nasa.gov/citations/19940010668
• Ennix-Sandhu, Kimberly. 2006. “NASA Dryden Flight Research Center: We Fly What Others Only Imagine.” In 17th Annual Girs’’ Math/Science Conference. https://ntrs.nasa.gov/citations/20070025006
• Enns, Dale. 2003. Robust Flight Control. Defense Technical Information Center. https://doi.org/10.21236/ada411755
• Eppel, Joseph C., Dennis W. Riddle, and Victor C. Stevens. 1988a. “Flight Measured Downwash of QSRA.” In Aircraft Symposium. https://ntrs.nasa.gov/citations/19890063932
• Eppel, Joseph C., Dennis W. Riddle, and Victor C. Stevens. 1988b. Flight Measured Downwash of the QSRA. NASA-TM-101050. NASA. https://ntrs.nasa.gov/citations/19890008222
• Eppink, Jenna, and Richard Wlezien. 2011. “Data Analysis for the NASA/Boeing Hybrid Laminar Flow Control Crossflow Experiment.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3879
• Epple, R., and R. Altenbach. 1982. “Dynamic Stability Testing of the Orbiter Flight Control System/flexible Body Interaction.” In Guidance and Control Conference. AIAA 1982-1531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1531
• Eppley, Charles V. 1963. History of the USAF Experimental Flight Test Pilot School 4 February 1951-12 October 1961. Defense Technical Information Center. https://doi.org/10.21236/ad0400112
• Eqbal, Mithun, Matthew Marino, and Patrick Farley. 2023. “Leading and Trailing Edge Configuration for Distributed Electric Propulsion Systems.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2752820/v1
• Eqbal, Mithun, Matthew Marino, Nuwantha Fernando, and Graham Wild. 2022. “Design Factors of High- Speed Turbo-Electric Distributed Propulsion System.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-1986257/v1
• Erdman, Peter. 2005. Analysis of the DEBI Flight Data. Defense Technical Information Center. https://doi.org/10.21236/ada435347
• Erdos, John. 1998. “On the Bridge from Hypersonic Aeropropulsion Ground Test Data to Flight Performance.” In 20th AIAA Advanced Measurement and Ground Testing Technology Conference. AIAA 1998-2494. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2494
• Erdos, John, John Calleja, and Jose Tamagno. 1994. “Increase in the Hypervelocity Test Envelope of the HYPULSE Shock-Expansion Tube.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2524
• Erhard, Racheal M., and Juan J. Alonso. 2022. “A Comparison of Propeller Wake Models for Distributed Electric Propulsion and eVTOL Aircraft in Complex Flow Conditions.” In AIAA SCITECH 2022 Forum. AIAA 2022-1676. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1676
• Erhard, Racheal M., Matthew A. Clarke, and Juan J. Alonso. 2021. “A Low-Cost Aero-Propulsive Analysis of Distributed Electric Propulsion Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-1200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1200
• Erickson, R. E., R. M. Kufeld, J. L. Cross, and C. W. Acree. 1985. “RSRA Flight Development Test in the Airplane Configuration.” In Proceedings of the Vertical Flight Society Forum 41 - Ft. Worth, TX 1985. The Vertical Flight Society. https://doi.org/10.4050/vfs-f41-1255
• Erickson, R. E., R. M. Kufeld, J. L. Cross, R. W. Hodge, W. F. Ericson, and R. D. G. Carter. 1984. NASA Rotor System Research Aircraft Flight-Test Data Report: Helicopter and Compound Configuration. NASA-TM-85843. NASA. https://ntrs.nasa.gov/citations/19840024311
• Erickson, Gary, John Schreiner, and Lawrence Rogers. 1990. “Multiple Vortex and Shock Interactions at Subsonic, Transonic, and Supersonic Speeds.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3023
• Erickson Jr., Ladden John C., Borst Richard M., Ordway Henry V., and Donald E. 1965. A Theory for VTOL Propeller Operation in a Static Condition. Defense Technical Information Center. https://doi.org/10.21236/ad0623527
• Ericson, W., and M. Falco. 1965. “Magnetoaerodynamic Drag and Flight Control.” In 6th Biennial Gas Dynamics Symposium. AIAA 1965-630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-630
• Ericsson, L. 1969. “A New Treatment of Roll-Pitch Coupling for Ballistic Re-Entry Vehicles.” In 7th Aerospace Sciences Meeting. AIAA 1969-101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-101
• Ericsson, L. 1985. “Is the Free Flight/wind Tunnel Equivalence Concept Valid for Unsteady Viscous Flow?” In 23rd Aerospace Sciences Meeting. AIAA 1985-378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-378
• Erol, Demspm., Lisa M. Valencia, James C. Simpson, et al. 2004. “Space-Based Telemetry and Range Safety Flight Demonstration #1.” In 41st Space Congress. https://ntrs.nasa.gov/citations/20130011313
• Ertugrul, Eren, and Emre Koyuncu. 2023. “Neural Network-Based UAV System Identification from Sparse Flight Test Data.” In AIAA SCITECH 2023 Forum. AIAA 2023-1344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1344
• Escalera Mendoza, Alejandra S., and Richard Hale. 2020. “Effects of Radome Design on Antenna Performance in Transonic Flight Conditions.” In AIAA Scitech 2020 Forum. AIAA 2020-2187. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2187
• Esch, Donald. n.d. “Stagnation Region Heating of a Phenolic-Nylon Ablator during Return from Planetary Missions.” PhD diss., Louisiana State University and Agricultural & Mechanical College. https://doi.org/10.31390/gradschool_disstheses.2119
• Escher, W., and G. Brewer. 1974. “Hydrogen: Make-Sense Fuel for an American Supersonic Transport.” In 12th Aerospace Sciences Meeting. AIAA 1974-163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-163
• Esposito, S. 2023a. “Analysis of Plasma Formation during Hypersonic Flight in the Earth Atmosphere.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-39
• Esposito, A. 2023b. “A Combustion-Driven Facility to Study Phenomenologies Related to Hypersonic Sustained Flight.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-47
• Estes, C. L., and E. F. McClain. 1948. Flight Tests of a Ground Speed Indicator over Measured Runs,. Defense Technical Information Center. https://doi.org/10.21236/ada305029
• “Estimation and Sensitivity in Flight Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.017
• Etesse, Andre. 1979. “Design-to-Cost and Aerospatiale’s Aircraft Division.” Aircraft Engineering and Aerospace Technology 51 (3): 23–25. https://doi.org/10.1108/eb035522
• Eulrich, B., K. Govindaraj, and W. Harrington. 1978. “Estimation of the Aerodynamic Stability and Control Parameters for the F-106A Aircraft from Flight Data: Maneuver Design and Flight Dataanalysis.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1326
• Eulrich, B., and E. Rynaski. 1980. “Identification of Flexible Aircraft from Flight Data.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1633. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1633
• “Evaluation of Equipment Performance for Altitude Test Facility Flight Environment Simulation System.” 2022. In Proceedings of 2022 the 12th International Workshop on Computer Science and Engineering. WCSE. https://doi.org/10.18178/wcse.2022.06.002
• “An Evaluation of Sailplane Drag Coefficient Parameters from Flight Test Results.” 1974. In 2nd International Symposium on the Technology and Science of Low Speed and Motorless Flight. AIAA 1974-1020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1020
• “An Evaluation of the Hypersonic Gun Tunnel.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0547.0579
• Evangelista, Raquel, Robert J. McGhee, and Betty S. Walker. 1989. “Correlation of Theory to Wind-Tunnel Data at Reynolds Numbers below 500,000.” In Lecture Notes in Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-84010-4_12
• Evangelista, Marco, and Massimiliano Mori. 2025. “Static System Error Compensation in Air Data Calibration for Tiltrotor System Certification.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0128
• Evangelista, R., W. Pfenninger, S. Mangalam, and A. Bar-Sever. 1987. “Design and Wind Tunnel Test of a High Performance Low Reynolds Number Airfoil.” In 5th Applied Aerodynamics Conference. AIAA 1987-2349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2349
• Evans, Albert J. 1954. The Zero-Lift Drag of a Slender Body of Revolution (NACA RM-10 Research Model) as Determined from Tests in Several Wind Tunnels and in Flight at Supersonic Speeds. NACA-TR-1160. NASA. https://ntrs.nasa.gov/citations/19930092188
• Evans, J. S., P. W. Huber, and C. J. Schexnayder. 1970. “Comparison of Theoretical and Flight-Measured Ionization in a Blunt Body Reentry Flow Field.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19700058379
• Evans, M., and L. Schilling. 1983. “Simulations Used in the Development and Flight Test of the HiMAT Vehicle.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2505
• Evans, Robert A., and Joseph C. Sonntag. 1963. “Economics and Operating Results Prototype Aircraft Jet Engine-Electric Power Plant.” In ASME 1963 Aviation and Space, Hydraulic, and Gas Turbine Conference and Products Show. American Society of Mechanical Engineers. https://doi.org/10.1115/63-ahgt-36
• Evans, A. G., F. W. Zok, C. G. Levi, et al. 2011. Revolutionary Materials for Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada552599
• Eversman, Walter, and Indranil Danda Roy. 1996. “Active Flutter Suppression Using MIMO Adaptive LMS Control.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1345
• “Exact Optimal Designs and Sample Sizes in Model I of Regression Analysis.” 2011. In Optimal Experimental Design with R. Chapman and Hall/CRC. https://doi.org/10.1201/b10934-15
• The Expected Fisher Information Matrix. 2022. Wiley. https://doi.org/10.1002/9781119237754.app3
• “Experimental Studies of Radiative Base Heating of a Jovian Entry Model.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0148.0171
• “Experimental Transonic Flutter Characteristics of Supersonic Cruise Configurations.” 1990. In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-979. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-979
• Exploring Flight Research with Experimental Gliders. 1999. NASA-EB-1999-03-002-DFRC. NASA. https://ntrs.nasa.gov/citations/20000032161
• “Exploring the Flight Envelope.” 2015. In Flight Dynamics. Princeton University Press. https://doi.org/10.2307/j.ctt1287kgx.5
• “External Tank Laminar and Rarefied Aeroheating.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0312.0331
• Exton, R. J. 1993. “Absorption, Scattering, and Fluorescence Techniques for Hypersonic Flow Measurements.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_18
• Eyi, Sinan, Kyle M. Hanquist, and Iain D. Boyd. 2018. “Aerothermodynamic Design Optimization of Hypersonic Vehicles.” In 2018 Multidisciplinary Analysis and Optimization Conference. AIAA 2018-3108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3108
• Eyi, S., and M. Yumusak. 2012. “Design Optimization in Hypersonic Flows.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5827. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5827
• F37 Committee. n.d.-a. Specification for Aeroelasticity Requirements for a Light Sport Airplane. ASTM International. https://doi.org/10.1520/f3619-26
• F37 Committee. n.d.-b. Standard Specification for Aeroelasticity Requirements for a Light Sport Airplane. ASTM International. https://doi.org/10.1520/f3619
• F38 Committee. n.d.-a. Practice for Methods to Safely Bound Flight Behavior of Unmanned Aircraft Systems Containing Complex Functions. ASTM International. https://doi.org/10.1520/f3269-21
• F38 Committee. n.d.-b. Standard Practice for Methods to Safely Bound Flight Behavior of Unmanned Aircraft Systems Containing Complex Functions. ASTM International. https://doi.org/10.1520/f3269-17
• “Facility Opportunities and Associated Stream Chemistry Considerations for Hypersonic Air-Breathing Propulsion.” 1992. In 17th Aerospace Ground Testing Conference. AIAA 1992-3991. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3991
• “Facility Requirements for Hypersonic Propulsion System Testing.” 1991. In High-Speed Flight Propulsion Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866104.0481.0526
• Fahy, William P., Andrew Chang, Hao Wu, and Joseph H. Koo. 2021. “Recent Developments of Ablative Thermal Protection Systems for Atmospheric Entry.” In AIAA Scitech 2021 Forum. AIAA 2021-1474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1474
• Fairbairn, G. 1964. “Structural Materials for Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-628. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-628
• Faïsse, Emmeline. n.d. “Integrated Structural and Control Design (Co-Design) for Active Flutter Suppression.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/c7bfd6f3z9deez44edz8b34zc551fda30c97
• Faïsse, Emmeline, Robin Vernay, Fabio Vetrano, Daniel Alazard, and Joseph Morlier. 2021. “Adding Control in Multidisciplinary Design Optimization of a Wing for Active Flutter Suppression.” In AIAA Scitech 2021 Forum. AIAA 2021-0892. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0892
• Fakhraei, Samin, and Julien Weiss. 2016. “Uncertainty Analysis of Test Data at the NRC 1.5-Meter Trisonic Wind Tunnel.” In 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2016-3498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3498
• Falarski, M. D., and K. W. Mort. 1969. Large-Scale Wind-Tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody. NASA-TN-D-5468. NASA. https://ntrs.nasa.gov/citations/19690029390
• Falempin, Francois. 1999. “Ramjet/scramjet Technology: French Capabilities.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2377. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2377
• Falempin, Francois, and Laurent Serre. 2004. “LEA Flight Test Program: Status in 2004.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3344
• Falempin, Francois, and Laurent Serre. 2006. “LEA Flight Test Program: Status in 2006.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7925
• Falempin, F., R. Thevenot, and PhGirard Vancamberg, ard, PhRol. 1995. “Hypersonic Airbreathing Propulsion: Flight Test Needs.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6013
• Falkiewicz, Nathan, Scott Frendreis, and Carlos Cesnik. 2011. “Effect of Control Surface-Fuselage Inertial Coupling on Hypersonic Vehicle Flight Dynamics.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6378
• Fallon, Edward, II, Anthony Taylor, and Robert Meyerson. 1999. “Landing System Design Summary of the K-1 Reusable Launch Vehicle.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1720
• Fan, Frank, and Steven Hall. 2014. “Gain-Scheduled Higher Harmonic Control for Full Flight Envelope Vibration Reduction.” In Proceedings of the Vertical Flight Society 70th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0070-2014-9498
• Fang, Chung. 2018. “Dimensional Analysis and Model Similitude.” In Springer Textbooks in Earth Sciences, Geography and Environment. Springer International Publishing. https://doi.org/10.1007/978-3-319-91821-1_6
• Fanning, A., and E. Lucas. 1979. “Recommendations for Obtaining Nozzle/afterbody Drag Data Based on a Comparison of Wind Tunnel and Flight Data.” In 15th Joint Propulsion Conference. AIAA 1979-1169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1169
• Fantini, Jay A. 1998. Conversion from Engineering Units to Telemetry Counts on Dryden Flight Simulators. NASA/CR-1998-206563. NASA. https://ntrs.nasa.gov/citations/19990004344
• Farbridge, J. E., and R. C. Smith. 1977. “The Transonic Multi-Foil Augmentor-Wing.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19770052117
• Farhat, Charles. 1998. Real Time Predictive Flutter Analysis and Continuous Parameter Identification of Accelerating Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada361695
• Farhat, Charbel. 2000. Real-Time Predictive Flutter Analysis and Continuous Parameter Identification of Acclerating Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada389378
• Farhat, Charbel. 2001. Real-Time Predictive Flutter Analysis and Continuous Parameter Identification of Accelerating Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada387498
• Farmer, N. B. 1974. Apollo Experience Report: Development Flight Instrumentation. NASA-TN-D-7598. NASA. https://ntrs.nasa.gov/citations/19740010398
• Farrow, Malcolm. 2013. “Optimal Experiment Design, Bayesian.” In Encyclopedia of Systems Biology. Springer New York. https://doi.org/10.1007/978-1-4419-9863-7_1234
• Fay, John F., Ganesh N. Kumar, and C. M. Seaford. 1991. “Aerothermodynamic Environment Predictions in Support of the Aeroassist Flight Experiment.” In AIAA Atmospheric Flight Mechanics Conference. https://ntrs.nasa.gov/citations/19910062575
• Faymon, Karl A. 1990. “Microwave Beam Powered Mars Airplane.” In Intersociety Energy Conversion Engineering Conference. https://ntrs.nasa.gov/citations/19910053308
• Fechter, Judie, and Charlene Mills. 1988. “Keys to a Successful Flight Test.” In 4th Flight Test Conference. AIAA 1988-2174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2174
• Fedioun, I., and E. Orlik. 2012. “Boundary Layer Transition on the LEA Hypersonic Vehicle Forebody.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5864
• “Feedback Flight Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.013
• Fegely, Cody, Mark Tischler, Ondrej Juhasz, and Hong Xin. 2016. “Flight Dynamics and Control Modeling with System Identification Validation of the Sikorsky X2 Technology Demonstrator.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11500
• Fehrs, Michael, and Sebastian Helm. 2025. “Transonic High Reynolds Number Transition Model Validation Based on ETW Cryogenic Wind Tunnel Data.” In AIAA SCITECH 2025 Forum. AIAA 2025-1714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1714
• Feller, William V., and Paige B. Burbank. 1958. Wind-Tunnel Investigation of the Heat Transfer to the X-15 Airplane. NASA. https://ntrs.nasa.gov/citations/19930092394
• Felt, L. R., and M. W. Kehoe. 1985. Flight Flutter Testing at Ames-Dryden. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19860063064
• Feng, Chen, Xiao Tang, Bing Xiong, and Xiaoqiang Fan. 2026. “Design Method and Optimization of Hypersonic Blended Wing-Body Vehicle Based on Parametric Subdivision Surfaces.” Preprint, . https://doi.org/10.2139/ssrn.7359960
• Feng, Deborah, and Jerry Chi Yiu Yan. 2017. “Center Overview and UAV Highlights at NASA Ames Research Center.” In National Oceanic and Atmospheric Administration. https://ntrs.nasa.gov/citations/20170006536
• Fenno, Charles C., Jr., H. A. Hassan, and Perry A. Newman. 1988. “Unsteady Viscous-Inviscid Interaction Procedures for Transonic Airfoils Using Cartesian Grids.” In AIAA Applied Aerodynamics Conference. https://ntrs.nasa.gov/citations/19880053530
• Ferguson, Frederick, and John Anderson Jr. 1993. “Expanding the Waverider Design Space Using General Supersonic and Hypersonic Generating Flows.” In 31st Aerospace Sciences Meeting. AIAA 1993-505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-505
• Ferguson, Frederick, Nastassja Dasque, and Mookesh Dhanasar. 2015a. “The Design, Analysis and Performance Evaluation of Waverider Configurations for Hypersonic Vehicle Applications.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1008
• Ferguson, Frederick, Nastassja Dasque, Mookesh Dhanasar, and Isaiah M. Blankson. 2016. “Waverider Design, Analysis and Performance Evaluation.” In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2016-1663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1663
• Ferguson, Frederick, Mookesh Dhanasar, and Isaiah M. Blankson. 2015b. “Waverider Design and Analysis.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3508. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3508
• Ferguson, Brian G., and Kam W. Lo. 2000. “Turboprop and Rotary-Wing Aircraft Flight Parameter Estimation Using Both Narrow-Band and Broadband Passive Acoustic Signal-Processing Methods.” Journal of the Acoustical Society of America 108 (4): 1763–71. https://doi.org/10.1121/1.1286150
• Ferlemann, Shelly M., Charles R. McClinton, Ken E. Rock, and Randy T. Voland. 2005. Hyper-X Mach 7 Scramjet Design, Ground Test and Flight Results. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050215122
• Ferrandon, Olivier. 1998. “International Market for a Reusable Launch Vehicle.” In Space Studies. Springer Netherlands. https://doi.org/10.1007/978-94-011-5030-9_31
• Ferreira de Moura, Ermerson, and Guilherme Borges Ribeiro. 2025. “Hypersonic Waverider Vehicle Flight Control Autopilot System Design and Implementation.” In Proceedings of the 28th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2025.cob2025-1507
• Ferrell, Kenneth R., Alan C. Frederickson, and James S. Kishi. 1974. Flight Evaluation Compliance Test Techniques for Army Hot Day Hover Criteria. Defense Technical Information Center. https://doi.org/10.21236/ada109440
• Ferretto¹, Davide, Simone Camboni¹, and Roberta Fusaro². 2024. “Preliminary Evaluation of Performance, Cost and Environmental Sustainability of a LH2-Powered Narrow Body Aircraft.” Preprint, . https://doi.org/10.20944/preprints202407.1506.v1
• Ferri, Antonio. 1971a. “Airplane Configurations for Low Sonic Boom.” In Third Conference on Sonic Boom Research. https://ntrs.nasa.gov/citations/19710018906
• Ferri, A. 1971b. Practical Aspects of Sonic Boom Problems. NASA. https://ntrs.nasa.gov/citations/19710050123
• Ferri, A., and I. Schwartz. 1972. “Sonic Boom Generation Propagation and Minimization.” In 10th Aerospace Sciences Meeting. AIAA 1972-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-194
• Ferri, A., M. Siclari, and L. Ting. 1973. “Sonic Boom Analysis for High Altitude Flight at High Mach Number.” In Aeroacoustics Conference. AIAA 1973-1034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1034
• Ferrier, Marc, Ivan Fedioun, and Dmitry Davidenko. 2006. “Boundary Layer Transition Prediction on a Hypersonic Vehicle Forebody.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8092
• Ferrier, Marc, Evgeniy Orlik, Ivan Fedioun, and Dmitry Davidenko. 2008. “Transition Prediction of the 3D Boundary Layer under an Hypersonic Vehicle Forebody.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2599
• Ferris, Ryan, and Mehdi R. Khorrami. 2024. “Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 1 – Aerodynamic and Airframe Noise Simulations.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3058
• Fetterman, D. E., Jr., E. J. Hopkins, and E. J. Saltzman. 1962. Comparison of Full-Scale Lift and Drag Characteristics of the X-15 Airplane with Wind-Tunnel Results and Theory. NASA-TM-X-713. NASA. https://ntrs.nasa.gov/citations/19650014320
• Fey, Uwe, Yasuhiro Egami, Robert Konrath, Tania Kirmse, Thomas Ahlefeldt, and Jürgen Kompenhans. 2010. “Advanced Measurement Techniques for High Reynolds Number Testing in Cryogenic Wind Tunnels.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1301
• Fidell, Sanford, Nicolaas Reddingius, Michael Harris, and Andrew B. Kugler. 1989. Noise and Sonic Boom Impact Technology. Initial Development of an Assessment System for Aircraft Noise (ASAN). Volume 1. Executive Summary. Defense Technical Information Center. https://doi.org/10.21236/ada214164
• Field, Edmund, James Armor, Kenneth Rossitto, Jeffery Schroeder, and Norman Weingarten. 2002. “Comparison of in-Flight and Ground Based Simulations of Large Aircraft Flying Qualities.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4800. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4800
• Fields, R. A. 1978. “Dryden Flight Research Center Hot Structures Research.” In NASA. Langley Res. Center Recent Advan. in Structures for Hypersonic Flight, Pt. 2. https://ntrs.nasa.gov/citations/19790013270
• Fields, R. A., F. V. Olinger, and R. C. Momaghan. 1972. Experimental Investigation of Mach 3 Cruise Heating Simulations on a Representative Wing Structure for Flight Loads Measurement. NASA-TN-D-6749. NASA. https://ntrs.nasa.gov/citations/19720012272
• Filipovic, Z., and G. Dikic. 2011. “Design and Implementation of PCM/FM Telemetry Systems for Aircraft and Missile Testing during Flight Test Procedure.” International Conference on Aerospace Sciences and Aviation Technology 14 (AEROSPACE SCIENCES): 1–15. https://doi.org/10.21608/asat.2011.23257
• Filippoli, Giorgio, Beniamino M. Perri, Stefano Cacciola, Carlo E. D. Riboldi, and Lorenzo Trainelli. 2026a. “Flight-Test-Based Analysis of Blowing Effects on Trimmed Aerodynamic Polars of a Distributed Electric Propulsion Aircraft Demonstrator.” In IOCAE 2026. MDPI. https://doi.org/10.3390/engproc2026142013
• Filippoli, Giorgio, Beniamino M. Perri, Niko Terzaroli, Stefano Cacciola, Carlo E. D. Riboldi, and Lorenzo Trainelli. 2026b. “Safety Considerations for a Distributed Electric Propulsion Aircraft: Lessons Learnt from an Automated Flight Test Accident Involving a Research Demonstrator.” Preprint, . https://doi.org/10.20944/preprints202605.1028.v1
• Filippou, Evangelos, Spyridon Kilimtzidis, Athanasios Kotzakolios, and Vassilis Kostopoulos. 2024. “Towards Structural and Aeroelastic Similarity in Scaled Wing Models: Development of an Aeroelastic Optimization Framework.” Preprint, . https://doi.org/10.20944/preprints202401.0348.v1
• Finch, Thomas W., and Donald W. Briggs. 1953. Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane. NACA-RM-L52K18b. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930087476
• Finch, Thomas W., and Gene J. Matranga. 1959. Launch, Low-Speed, and Landing Characteristics Determined from the First Flight of the North American X-15 Research Airplane. NASA-TM-X-195. NASA. https://ntrs.nasa.gov/citations/19980236840
• Finchum, John A. 1974. “Précis—Assessment of Airframe Production Cost Risk.” Management Science 21 (2): 237–237. https://doi.org/10.1287/mnsc.21.2.237
• Findlay, J., G. Kelly, J. McConnell, and H. Compton. 1984. “Shuttle ‘Challenger’ Aerodynamic Performance from Flight Data: Comparisons with Predicted Values and ‘Columbia’ Experience.” In 22nd Aerospace Sciences Meeting. AIAA 1984-485. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-485
• Finnestead, Rodger L., and William J. Connor. 1969. Engineering Flight Test. AH-1G Helicopter, Hueycobra, Phase B, Part 6. Defense Technical Information Center. https://doi.org/10.21236/ad0862700
• Finnestead, Rodger L., William J. Connor, Emmett Laing, and Marvin W. Buss. 1970. Engineering Flight Test AH-1G Helicopter (Hueycobra). Phase D (Airworthiness and Flight Characteristics). Part 2. Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0874210
• First Glide Flight of Heavy Lifting Body Planned Soon. 1966. NASA NEWS RELEASE-66-89. NASA. https://ntrs.nasa.gov/citations/19660014496
• “First Laminar Flow Flight Tests Prove Drag Reduction Potential: ELFIN Project Leads the Way for European Laminar Aircraft.” 1992. Aircraft Engineering and Aerospace Technology 64 (1): 5–7. https://doi.org/10.1108/eb037198
• Fischel, Jack. 1960. V. the X-15 Flight Research Program in Relation to the Development of Advanced Military Aircraft. Flight Research Center. https://ntrs.nasa.gov/citations/19670023746
• Fischel, Jack, Robert W. Darville, and Donald Reisert. 1957. Effects of Wing-Mounted External Stores on the Longitudinal and Lateral Handling Qualities of the Douglas D-558-II Research Airplane. NACA-RM-H57H12. NASA. https://ntrs.nasa.gov/citations/19930090143
• Fischel, Jack, and Jack Nugent. 1953. Flight Determination of the Longitudinal Stability in Accelerated Maneuvers at Transonic Speeds for the Douglas D-558-II Research Airplane Including the Effects of an Outboard Wing Fence. NACA-RM-L53A16. NASA. https://ntrs.nasa.gov/citations/19930087532
• Fischel, Jack, and Donald Reisert. 1955. Effect of Several Wing Modifications on the Low-Speed Stalling Characteristics of the Douglas D-558-II Research Airplane. NACA-RM-H55E31a. NASA. https://ntrs.nasa.gov/citations/19930088809
• Fischel, Jack, and Donald Reisert. 1956. Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane. NACA-RM-H56C30. NASA. https://ntrs.nasa.gov/citations/19930090225
• Fischel, J., and T. A. Toll. 1964. The x-15 Project- Results and New Research. NASA-RP-186. NASA. https://ntrs.nasa.gov/citations/19640012152
• Fischenberg, D. 1995. “Identification of an Unsteady Aerodynamic Stall Model from Flight Test Data.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3438
• Fischer, R. 2005. “Integrated Bayesian Experimental Design.” In AIP Conference Proceedings, vol. 803. AIP. https://doi.org/10.1063/1.2149824
• Fischer, Wolfgang P. P. 2008. “Beta-Titanium Alloy Thermal Protection System for Re-Entry Vehicles.” SAE International Journal of Aerospace 01 (1): 461–72. https://doi.org/10.4271/2008-01-2149
• Fischer, Michael C., and Chandra S. Vemuru. 1991. “Application of Laminar Flow Control to the High Speed Civil Transport: The NASA Supersonic Laminar Flow Control Program.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/912115
• Fischer, M., A. Wright Jr., and R. Wagner. 1983. “A Flight Test of Laminar Flow Control Leading-Edge Systems.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2508. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2508
• Fisher, Lloyd J. 1948. Ditching Tests of a 1/20-Scale Model of the Northrop B-35 Airplane. NACA-RM-SL8A29. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028614
• Fisher, H. 1970. “Re-Entry Vehicle Crew Visibility Considerations.” In Advanced Space Transportation Meeting. AIAA 1970-262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-262
• Fisher, David F. 1999. Fifty Years of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-1996. NASA/TP-1999-206568. NASA. https://ntrs.nasa.gov/citations/19990047114
• Fisher, David F. 2007. Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. NASA/TP-2007-213684. NASA. https://ntrs.nasa.gov/citations/20070023367
• Fisher, David, Daniel Banks, and David Richwine. 1990. “F-18 High Alpha Research Vehicle Surface Pressures: Initial in-Flight Results and Correlation with Flow Visualization and Wind-Tunnel Data.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3018
• Fisher, David, and Brent Cobleigh. 1994. “Controlling Forebody Asymmetries in Flight: Experience with Boundary Layer Transition Strips.” In 12th Applied Aerodynamics Conference. AIAA 1994-1826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1826
• Fisher, D. L., and N. S. Dougherty Jr. 1982. “Flight and Wind-Tunnel Correlation of Boundary-Layer Transition on the AEDC Transition Cone.” In AGARD Flight Mech. Panel Symp.. https://ntrs.nasa.gov/citations/19830006162
• Fisher, D. F., and N. S. Dougherty Jr. 1983. “Flight and Wind-Tunnel Correlation of Boundary-Layer Transition on the AEDC Transition Cone.” In AGARD Ground(Flight Test Tech. and Correlation. https://ntrs.nasa.gov/citations/19830022092
• Fisher, David F., and Wendy R. Lanser. 1994. “Flight and Full-Scale Wind-Tunnel Comparison of Pressure Distributions from an F-18 Aircraft at High Angles of Attack.” In Fourth High Alpha Conference: Volume 1. https://ntrs.nasa.gov/citations/19950007817
• Fisher, Lloyd J., and Ellis E. McBride. 1948. Ditching Tests of a 1/10-Scale Model of the North American XFJ-1 Airplane Ted No. NACA 314. NACA-RM-SL8K15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026359
• Fisher, Lloyd J., and Ellis E. McBride. 1955. Ditching Investigation of a 1/10-Scale Model of the Grumman F9F-2 Airplane, TED No. NACA DE 335. NACA-RM-SL50I29B. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029429
• Fisher, David F., and Robert R. Meyer Jr. 1988. Flow Visualization Techniques for Flight Research. NASA-TM-100455. NASA. https://ntrs.nasa.gov/citations/19890002348
• Fisher, David F., and Robert R. Meyer Jr. 1989. “Flow Visualization Techniques for Flight Research.” In AGARD, Flight Test Techniques. https://ntrs.nasa.gov/citations/19900001562
• Fisher, Lloyd J., and Garland J. Morris. 1948. Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane. NACA-RM-SL8K18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029398
• Fisher, David F., and Steve Parcel. 2007. Six Decades of Flight Research: Dryden Flight Research Center, 1946: 2006 [DVD]. NASA/TM-2007-214617. NASA. https://ntrs.nasa.gov/citations/20070031215
• Fisher, D., and J. Peterson Jr. 1978. “Flight Experience on the Need and Use of Inflight Leading Edge Washing for a Laminar Flow Airfoil.” In Aircraft Systems and Technology Conference. AIAA 1978-1512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1512
• Fisher, Tom, Mark K. Quinn, and Katharine Smith. 2018. “Free-Flight Testing of Hypersonic Edney Shock Interactions.” In 2018 Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2018-4283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4283
• Fisher, Lloyd J., and William C. Thompson. 1949. Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane with Speedpak Attached. NACA-RM-SL9H05a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050071552
• Fisher, Lloyd J., and William C. Thompson. 1950. Ditching Investigation of a 1/15-Scale Model of the Convair-Liner Airplane. NACA-RM-SL50K02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019446
• Fisher, Lloyd J., and William C. Thompson. 1955. Ditching Investigation of a 1/12-Scale Model of the Douglas F3D-2 Airplane, TED No. NACA DE 381. NACA-RM-SL52J30. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029469
• Fisher, Lloyd J., and John O. Windham. 1950a. Ditching Investigation of a 1/14-Scale Model of the Northrop C-125 Airplane. NACA-RM-SL51C28. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030016
• Fisher, Lloyd J., and John O. Windham. 1950b. Ditching Investigation of a 1/24-Scale Model of the Boeing B-47 Airplane. NACA-RM-SL50E03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029374
• Fisher, Lloyd J., and John O. Windham. 1951. Ditching Investigation of a 1/24-Scale Model of the Douglas C-124 Airplane. NACA-RM-SL51F20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029442
• Fisher, Lloyd J., and John O. Windham. 1955a. Ditching Investigation of a 1/11-Scale Model of the Chance Vought F7U-3 Airplane, TED NO. NACA DE 360. NACA-RM-SL52K07A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029459
• Fisher, Lloyd J., and John O. Windham. 1955b. Ditching Investigation of a 1/20-Scale Model of the Boeing Stratocruiser Airplane (C-97). NACA-RM-SL9I16. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030043
• Fitz, J. S., and R. J. Stattel. 1965. Airborne Telemetry Calibrator Type 4x4, Mod i. NASA-TM-X-55256. NASA. https://ntrs.nasa.gov/citations/19650020358
• Fitzgerald, James. 1992. “ES-3A Flight Test Program.” In Aerospace Design Conference. AIAA 1992-1230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1230
• Fitzgerald, Timothy, John Ralston, and Bruce Hildreth. 1994. “Improvements to the Naval Air Warfare Center Aircraft Division’s F/A-18 Subsonic Aerodynamic Model.” In Flight Simualtion Technologies Conference. AIAA 1994-3400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3400
• Fitzsimmons, Jeff. 1996. “Cost Analysis of a DC-X Reusable Launch Vehicle: Is It Affordable?” In Space Programs and Technologies Conference. AIAA 1996-4414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4414
• Fitzsimmons, R., R. McKinnon, E. Johnson, and J. Brooks. 1980. “Flight and Wind Tunnel Test Results of the Mechanical Jet Noise Suppressor Nozzle.” In 18th Aerospace Sciences Meeting. AIAA 1980-165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-165
• Fivel, H. J., R. V. Masek, and L. J. Mockapetris. 1975. Analytical Comparison of Hypersonic Flight and Wind Tunnel Viscous/inviscid Flow Fields. NASA-CR-2489. NASA. https://ntrs.nasa.gov/citations/19750011514
• Flanagan, M. J., Jr. 1993. “Aerodynamic Heating in the Vicinity of Hypersonic, Axisymmetric, Shock-Wave Boundary-Layer Interactions.” In AIAA. https://ntrs.nasa.gov/citations/19930062515
• Fleck, T. 1983. “Flight Testing of the Autopilot and Terrain Following Radar System in the Tornado Aircraft.” In 2nd Flight Testing Conference. AIAA 1983-2770. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2770
• Flemming, Robert J., Randall K. Britton, and Thomas H. Bond. 1994. “Role of Wind Tunnels and Computer Codes in the Certification and Qualification of Rotorcraft for Flight in Forecast Icing.” In European Rotorcraft Forum. https://ntrs.nasa.gov/citations/19950006784
• Fletcher, D. 1994. “An Investigation of Taguchi Methods for Flight Test Optimization.” In Biennial Flight Test Conference. AIAA 1994-2146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2146
• “Flight Characteristics of Quad Ducted Fan Helicopter with Thrust Vectoring Nozzles.” 2014. Journal of Unmanned System Technology. https://doi.org/10.21535/tht7nm82
• “Flight Control.” 2015. In Smart Autonomous Aircraft. CRC Press. https://doi.org/10.1201/b19350-7
• “Flight Control System Design Guidelines.” 2011. In Eigenstructure Control Algorithms: Applications to aircraft/rotorcraft handling qualities design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e_ch8
• “Flight Control System for an Airplane.” 1999. Aircraft Engineering and Aerospace Technology 71 (1). https://doi.org/10.1108/aeat.1999.12771aad.001
• “Flight Control System of an Advanced Air Superiority Fighter.” 1977. In Guidance and Control Conference. AIAA 1977-1079. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1079
• Flight Control Systems. 2022. Wiley. https://doi.org/10.1002/9781119738251.ch4
• “Flight Dynamics of Elastic Aircraft.” 2014. In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/b17346-14
• “Flight Envelope.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0355.0410
• The Flight Environment: Standard Atmosphere. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch2
• Flight Flutter Testing Symposium. 1975. NASA-SP-385. NASA. https://ntrs.nasa.gov/citations/19760003007
• “Flight Measurements of Tile Gap Heating on the Space Shuttle.” 1983. In Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865626.0255.0270
• “Flight Performance.” 2012. In Designing Unmanned Aircraft Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868443.0353.0379
• “Flight Performance.” 2014. In Designing Unmanned Aircraft Systems. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102615.0349.0376
• Flight Performance of Civil Small and Light Fixed-Wing Unmanned Aircraft Systems (UAS) � Test Methods. n.d. BSI British Standards. https://doi.org/10.3403/30426801u
• Flight Sciences Lab INC Buffalo NY. 1964. A General Investigation of Hypersonic Stability and Control under Trimmed Flight Conditions. Defense Technical Information Center. https://doi.org/10.21236/ad0442900
• “Flight Test Data Analysis of Hybrid Vertical Take-off and Landing Unmanned Aerial Vehicle.” 2016. Journal of Instrumentation, Automation, and Systems. https://doi.org/10.21535/dnk59q51
• “Flight Test Manual.” 1959. In Stability and Control. Elsevier. https://doi.org/10.1016/b978-1-4831-9730-2.50001-6
• Flight Test Planning. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch6
• “Flight Test Programme.” 1970. Aircraft Engineering and Aerospace Technology 42 (4): 25–32. https://doi.org/10.1108/eb034622
• “Flight Test Results for an Advanced Technology Light Airplane.” 1977. In Aircraft Systems and Technology Meeting. AIAA 1977-1217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1217
• Flight Testing. 1992. ISBN: 92-835-0688-X. NASA. https://ntrs.nasa.gov/citations/19930010712
• “Flight Tests on Way for Boeing Fuel Cell Airplane.” 2007. Fuel Cells Bulletin 2007 (5): 2–3. https://doi.org/10.1016/s1464-2859(07)70156-6
• “Flight Vehicle Lift-Drag Characteristics.” 2001. In Flight Vehicle Performance and Aerodynamic Control. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861857.0075.0101
• “Flight-Surface Seal Is Designed to Prevent “Seal Flutter”.” 2010. Sealing Technology 2010 (6): 15. https://doi.org/10.1016/s1350-4789(10)70317-2
• “Flight: Drag and Thrust.” 2026. In Birds Up Close. The MIT Press. https://doi.org/10.7551/mitpress/10839.003.0009
• Flittie, Kirk, and Bob Curtin. 1998. “Pathfinder Solar-Powered Aircraft Flight Performance.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4446
• Florence, D., and A. Hiltz. 1968. “Thermal Protection Systems for a Mars-Entry Vehicle.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-304
• Florence, D., H. Thibault, and A. Hiltz. 1978. “Selection, Development, Characterization and Flight Test of a Thermal Protection System for an Earth Entry Satellite Vehicle.” In 2nd Thermophysics and Heat Transfer Conference. AIAA 1978-861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-861
• Florio, Brendan James, Robert McKibbin, Calum Braham, John Ockendon, and Colin Please. 2019. “Estimating Transonic Drag.” ANZIAM Journal 59: 1. https://doi.org/10.21914/anziamj.v59i0.13408
• “Flow Control and High-Lift Performance for Flying-Wing Unmanned Combat Air Vehicle Configurations by Inserting Slots.” 2016. International Journal of Multiphysics 10 (2). https://doi.org/10.21152/1750-9548.10.2.117
• Fluid Dynamics Research on Supersonic Aircraft. 1998. AC/323(AVT)TP/6. NASA. https://ntrs.nasa.gov/citations/19990018232
• Flutter Testing Techniques. 1976. NASA-SP-415. NASA. https://ntrs.nasa.gov/citations/19770014078
• Flynn, Darin C., Nalin A. Ratnayake, and Michael Frederick. 2009. “Design and Calibration of a Flowfield Survey Rake for Inlet Flight Research.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090005944
• Foch, Richard. 1992. “Test Pilot’s Notes on Flying the Low Altitude/Airspeed Unmanned Research Aircraft (LAURA).” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4078
• Foch, Richard J., and Peggy L. Toot. 1989. “Flight Testing Navy Low Reynolds Number (LRN) Unmanned Aircraft.” In Lecture Notes in Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-84010-4_30
• Ford, Terry. 1989. “Helicopter Handling Qualities.” Aircraft Engineering and Aerospace Technology 61 (1): 2–4. https://doi.org/10.1108/eb036732
• Förder, D., and G. Steiner. 2020. “2.1 Robust and Flexible Flight Test Instrumentation for Wireless and Wired Measurements.” In Proceedings - ettc2020. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2020/2.1
• Foreman, K. 1963. “Terrestrial Hypersonic Flight Propulsion.” In Hypersonic Ramjet Conference. AIAA 1963-110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-110
• Forster, E., R. Kolonay, V. Venkayya, and F. Eastep. 1996. “Optimization of a Generic Fighter Wing Incorporating Active Aeroelastic Wing Technology.” In 6th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1996-4010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4010
• Fosdick, George W. 1970. Flight Test Evaluation of the Three-Axis Mechanical Stability Augmentation System. Defense Technical Information Center. https://doi.org/10.21236/ad0880677
• Foss, W. E., Jr., and J. M. Swihart. 1956. Transonic Aerodynamic and Trim Characteristics of a Multi-Engine Delta-Wing Airplane Model. NACA-RM-L55I27B. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19660010447
• Foster, Richard. 1989. “Optimization of the Rocket Mode Trajectory in a Rocket Based Combined Cycle (RBCC) Engine Powered SSTO Vehicle.” In 25th Joint Propulsion Conference. AIAA 1989-2295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2295
• Foster, L. D., T. F. Greenwood, and D. B. Lee. 1985. “Shuttle System Ascent Aerodynamic and Plume Heating.” In NASA. Johnson Space Center Space Shuttle Tech. Conf., Pt. 2. https://ntrs.nasa.gov/citations/19850008666
• Fotia, M. L., J. Hoke, and F. Schauer. 2019. “Advancements in Laboratory-Scale Detonation Experiments at Air Force Research Laboratory.” In Advances in Pulsed and Continuous Detonation. TORUS PRESS. https://doi.org/10.30826/icpcd201823
• Fouladi, Kamran. 1993. “Unstructured Grids for Sonic-Boom Analysis.” In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. AIAA 1993-2929. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2929
• Fouladi, Kamran. 1999. “CFD Predictions of Sonic-Boom Characteristics for Unmodified and Modified SR-71 Configurations.” In High-Speed Research: 1994 Sonic Boom Workshop. Configuration, Design, Analysis and Testing. https://ntrs.nasa.gov/citations/20000027452
• Foulke, William K. 1965. Exploration of High-Speed Flight with the XH-51A Rigid Rotor Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ad0617966
• Fournier, Hugo, Robin Vernay, Paolo Massioni, Minh Tu Pham, and Laurent Bako. 2023. “Active Flutter Suppression H∞ Synthesis Using Multiple Models with Imposed Aeroelastic Poles.” In AIAA SCITECH 2023 Forum. AIAA 2023-0686. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0686
• Fournis, Camille. 2022. “Wave Drag Prediction Using the Lamb Vector in Two-Dimensional Steady Transonic Flows.” In AIAA AVIATION 2022 Forum. AIAA 2022-3886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3886
• Fox, Francis T. 1964. “Operations of the Supersonic Transport in the Terminal Area.” Journal of the Aero-Space Transport Division 90 (2): 59–67. https://doi.org/10.1061/jatdaz.0000037
• Fox, R., H. Miura, and S. Rao. 1972. “Automated Design Optimization of Supersonic Airplane Wing Structures under Dynamic Constraints.” In 13th Structures, Structural Dynamics, and Materials Conference. AIAA 1972-333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-333
• Foxworth, T. 1968. “The Air Line Pilot Views Supersonic Transport Operations.” In 5th Annual Meeting and Technical Display. AIAA 1968-1001. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1001
• Franciscus, L. 1983. “Supersonic Fan Engines for Military Aircraft.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2541. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2541
• Freakley, Craig. n.d. “Design, Construction and Flight Test of the Inlet and Electronic Ignition System for a Mach 2 Ramjet.” PhD diss., The University of Queensland. https://doi.org/10.14264/299462
• Frederick, Michael A., and Nalin A. Ratnayake. 2010. “Flight Test Results from the Rake Airflow Gage Experiment on the F-15B Airplane.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100024394
• Frederick, Michael A., and Nalin A. Ratnayake. 2011. Flight Test Results from the Rake Airflow Gage Experiment on the F-15B Airplane. NASA/TM-2011-215977. NASA. https://ntrs.nasa.gov/citations/20120011162
• Fredericks, Bill. 2015. “Flight Test of NASA GL-10 Distributed Electric Propulsion UAV.” In Proceedings of the Vertical Flight Society Second Annual Transformative Vertical Flight Workshop, NASA Ames, August 2015. The Vertical Flight Society. https://doi.org/10.4050/sm_2015_tvf-2799
• “The Free Flight Range: A Tool for Research in the Physics of High Speed Flight.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0627.0650
• Freeman, Jeffrey L., and Garrett T. Klunk. 2018. “Dynamic Flight Simulation of Spanwise Distributed Electric Propulsion for Directional Control Authority.” In 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. AIAA 2018-4997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4997
• Freeman, D. C., Jr. 1980. Dynamics Stability Derivatives of Space Shuttle Orbiter Obtained from Wind-Tunnel and Approach and Landing Flight Tests. NASA-TP-1634. NASA. https://ntrs.nasa.gov/citations/19800012851
• Freeman, Delman C., Jr., Daivd E. Reubush, Charles R. McClinton, Vincent L. Rausch, and J. Larry Crawford. 1997a. The NASA Hyper-X Program. NASA/TM-1997-207243. NASA. https://ntrs.nasa.gov/citations/19980018480
• Freeman, D. C., Jr., and B. Spencer Jr. 1980. Comparison of Space Shuttle Orbiter Low-Speed Static Stability and Control Derivatives Obtained from Wind-Tunnel and Approach and Landing Flight Tests. NASA-TP-1779. NASA. https://ntrs.nasa.gov/citations/19810004555
• Frei, D. R. 1982. “X-29A Forward-Swept-Wing Demonstrator Airplane.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017333
• French, Mark. 1988a. “Evaluation of a New Supersonic Flutter Prediction Tool.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4376
• French, K. 1988b. “Flight Test Experience with an RPV Emergency (Parachute) Recovery System.” In 4th Flight Test Conference. AIAA 1988-2139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2139
• Fresconi, Frank, Benjamin Greunwald, and Tansel Yucelen. 2017. “Adaptive Missile Flight Control for Complex Aerodynamic Phenomena.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4207
• Freudinger, Lawrence C., and Michael W. Kehoe. 1990. Flutter Clearance of the F-14A Variable-Sweep Transition Flight Experiment Airplane, Phase 2. NASA-TM-101717. NASA. https://ntrs.nasa.gov/citations/19900015819
• Freuler, R., and M. Hoffmann. 1977. “A Digital Data Acquisition and Reduction System for Flight Testing General Aviation Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1977-1216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1216
• Freund, Donald, Donald Howe, Frank Simmons, and Lawrence Schuester. 2008. “Quiet Spike Prototype Aerodynamic Characteristics from Flight Test.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-125
• Friedmann, P., C. Venkatesan, and K. Yuan. 1992. “Development of a Structural Optimization Capability for the Aeroelastic Tailoring of Composite Rotor Blades with Straight and Swept Tips.” In 4th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1992-4779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4779
• Friehmelt, Holger. 1996. “Thrust Vectoring and Tailless Aircraft Design: Review and Outlook.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3412
• Friehmelt, Holger, and Michael Jost. 2000. “Flush Air Data System: An Advanced Air Data System for Aerospace Applications.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4191
• Friend, C. 1964. “A Fundamental Study of Reaction Control Criteria for Jet Vtol Aircraft.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-787
• Friend, E. L., and G. M. Sakamoto. 1978. Flight Comparison of the Transonic Agility of the F-111A Airplane and the F-111 Supercritical Wing Airplane. NASA-TP-1368. NASA. https://ntrs.nasa.gov/citations/19790004885
• Frinell, R. 1983. “Closing the Loop with a Flight Test Customer: Management and Follow-up Techniques for Vendor or Customer Flight Testing.” In 2nd Flight Testing Conference. AIAA 1983-2743. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2743
• Frostig, Y., and G. Simitses. 2001. “Structural Similitude and Scaling Laws for Sandwich Beams.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1280. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1280
• Fry, Bernard L. 1965. “Low-Speed Aerodynamic Flight Boundaries and Control Aspects OF TILT-WING AIRCRAFT.” In Proceedings of the Vertical Flight Society Forum 21 - Washington, D.C. 1965. The Vertical Flight Society. https://doi.org/10.4050/vfs-f21-002
• Fry, B. 1967. “Assessment of Commercial VTOL Aircraft with Rotor or Propeller Lift Systems.” In Commercial Aircraft Design and Operation Meeting. AIAA 1967-411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-411
• Fry, C. M., and A. P. Sage. 1974. “Identification of Aircraft Stability and Control Parameters Using Multilevel, Hierarchical Estimation.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017468
• Frye, Mark W., Roger M. Bailey, and Artie D. Jessup. 2004. NASA-Langley Research Center’s Aircraft Condition Analysis and Management System Implementation. NASA/TM-2004-213276. NASA. https://ntrs.nasa.gov/citations/20040170449
• Fu, S., and L. Wang. 2007. “Modeling Flow Transition in Hypersonic Boundary Layer.” In New Trends in Fluid Mechanics Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-75995-9_9
• “Fuel Cell Demonstrator Aeroplane for Ground and Flight Testing.” 2007. Aircraft Engineering and Aerospace Technology 79 (4). https://doi.org/10.1108/aeat.2007.12779daf.013
• Fugate, Jason, Nhan T. Nguyen, and Juntao Xiong. 2019. “Aero-Structural Modeling of the Truss-Braced Wing Aircraft Using Potential Method with Correction Methods for Transonic Viscous Flow and Wing-Strut Interference Aerodynamics.” In AIAA Aviation 2019 Forum. AIAA 2019-3028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3028
• Fuhrmann, Henri. 1993. “Application of Natural Laminar Flow to a Supersonic Transport Concept.” In 11th Applied Aerodynamics Conference. AIAA 1993-3467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3467
• Fujii, Keisuke. 2005. “An Experiment of Two Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-891. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-891
• Fujii, Keisuke, and Yasutoshi Inoue. 1998b. “Aerodynamic Heating Measurement on Ceramic Tile Region of Hypersonic Flight Experiment (HYFLEX).” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-605
• Fujii, Kenji, Toshiya Nakamura, Hiroshi Kawato, and Shigeya Watanabe. 2003. “Concepts and Studies of Flight Experiment Vehicles for Reusable Space Transportation System.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-6984. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6984
• Fujii, Keisuke, Shigeya Watanabe, Takuji Kurotaki, and Masao Shirouzu. 2000. “Aerodynamic Heating Measurements on Nose and Elevon of Hypersonic Flight Experiment Vehicle.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-267
• Fujita, Takeshi, Yasushi Ito, Kazuhiro Nakahashi, and Toshiyuki Iwamiya. 2001. “Aerodynamics Evaluation of NAL Experimental Supersonic Airplane in Ascent Using CFD.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-564
• Fukami, Koji, Shin-ichiro Higashino, and Akira Sakurai. 2004. “Dynamic Wind-Tunnel Testing Using Captive Flight Method.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5176
• Fukushima, Yuma, and Soshi Kawai. 2017. “Wall-Modeled Large-Eddy Simulation of Transonic Buffet over a Supercritical Airfoil at High Reynolds Number.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0495. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0495
• Fullerton, C. Gordon. 1993. Propulsion Controlled Aircraft Research. ISSN: 0742-3705. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/19950059270
• “Fundamentals of the Optimal Experimental Design.” n.d. In Lecture Notes in Statistics. Springer-Verlag. https://doi.org/10.1007/0-387-31610-8_2
• Funk, Jack, and Harry C. Mickleboro. 1953. A Comparison of Gust Loads Measured in Flight on a Swept-Wing Airplane and an Unswept-Wing Airplane. NACA-RM-L52L02. NASA. https://ntrs.nasa.gov/citations/19930087449
• Funk, Jack, and Richard H. Rhyne. 1956. An Investigation of the Loads on the Vertical Tail of a Jet-Bomber Airplane Resulting from Flight through Rough Air. NACA-TN-3741. NASA. https://ntrs.nasa.gov/citations/19930084537
• Furbish, David Jon. 1997. “Dimensional Analysis and Similitude.” In Fluid Physics in Geology. Oxford University Press. https://doi.org/10.1093/oso/9780195077018.003.0009
• Furlong, G. Chester, and James E. Fitzpatrick. 1947. Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-Series Airfoil Sections. NACA-TN-1299. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930081927
• “Further Development and Flight Test of an Autonomous Precision Landing System Using a Parafoil.” 1994. In Biennial Flight Test Conference. AIAA 1994-2141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2141
• Fusi, Francesca, Giuseppe Quaranta, Alberto Guardone, and Pietro M. Congedo. 2015. “Drag Minimization of an Isolated Airfoil in Transonic Inviscid Flow by Means of Genetic Algorithms.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1722
• “G. the Experimental Aerodynamics of Wings at Transonic and Supersonic Speeds.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-016
• Gade, Prasad V. N., and Daniel J. Inman. 1996. “ℋ∞ Controller Design for Wing/Store Flutter Suppression.” In Active Control of Vibration and Noise. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1996-0909
• Gadeberg, Burnett L., and Howard L. Ziff. 1951. Flight Determined Buffet Boundaries of Ten Airplanes and Comparisons with Five Buffeting Criteria. NACA-RM-A50I27. NASA. https://ntrs.nasa.gov/citations/19930086444
• Gage, Peter, and Jeremy Vander Kam. 2003. “A Data Model for Evaluating Reusable Launch Vehicle Concepts.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1330
• Gai, S., N. Mudford, and C. Hackett. 1992. “Heat Flux and Shock Shape Measurements on an Aeroassist Flight Experiment Model in a High Enthalpy Free Piston Shock Tunnel.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3907. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3907
• Gainer, C. A. 1963. Air Force Flight Control and Flight Display Integration Program. Defense Technical Information Center. https://doi.org/10.21236/ad0404850
• Gainer, T. G., M. J. Mann, and J. K. Huffman. 1984. Low-Speed Investigation of Effects of Wing Leading- and Trailing-Edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward-Swept Wing. NASA-TM-85795. NASA. https://ntrs.nasa.gov/citations/19840018599
• Gajoni, Paolo, Guillaume Grossir, Dániel G. Kovács, and Alberto Guardone. 2026. “Time-Resolved Schlieren Analysis of Boundary-Layer Transition on a Blunt Cone in Hypersonic Flow.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5066
• Gal-Or, Benjamin. 2001. “Thrust Vectoring Flight Control to Maximize Future Jet Transport Flight Safety.” International Journal of Turbo and Jet Engines 18 (1). https://doi.org/10.1515/tjj.2001.18.1.41
• Gale, Lawrence J., and Stanley H. Scher. 1949. An Investigation of the Spin and Recovery Characteristics of a 1/25-Scale Model of the Douglas D-558-II Airplane. NACA-RM-L8K19a. NASA. https://ntrs.nasa.gov/citations/19930085614
• “Galileo Probe Forebody Thermal Protection.” 1982. In Thermophysics of Atmospheric Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865565.0328.0353
• Gallagher, J. 1968. “Capabilities of in-Flight Thrust Reversing.” In Control and Flight Dynamics Conference. AIAA 1968-880. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-880
• Gallagher, J., and W. Fellers. 1983. “The F-5 Story: Prototype and Technology Demonstrator.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1062. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1062
• Gallagher, Frank, and Fu-Shang (John) Wei. 2008. “k-Max Rotor Blade Flight Loads Survey for out of Envelope Flight Test.” In Proceedings of the Vertical Flight Society AHS 64th Annual Forum, Montréal, Québec, April 29-May 1, 2008. The Vertical Flight Society. https://doi.org/10.4050/vfs-f64-000306
• Gallani, Murilo A., Luiz Carlos Sandoval Góes, and Luiz Augusto Rodrigues Nerosky. 2020. “Effects of Distributed Electric Propulsion on the Performance of a General Aviation Aircraft.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3594. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3594
• Gallington, R., and M. Miller. 1970. “The Ram-Wing: A Comparison of Simple One- Dimensional Theory with Wind Tunnel and Free Flight Results.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-971. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-971
• Gally, Thomas, and Leland Carlson. 1993. “Survey of Nonequilibrium Re-Entry Heating for Entry Flight Conditions.” In 24th Plasma Dynamics, and Lasers Conference. AIAA 1993-3230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3230
• Ganguli, Ranjan, and Inderjit Chopra. 1997. “Aeroelastic Tailoring of Composite Couplings and Blade Geometry of a Helicopter Rotor Using Optimization Methods.” Journal of the American Helicopter Society 42 (3): 218–28. https://doi.org/10.4050/jahs.42.218
• Ganzer, V. M., R. G. Joppa, and G. Vanderwees. 1977. Analysis of Low Altitude Atmospheric Turbulence Data Measured in Flight. NASA-CR-2886. NASA. https://ntrs.nasa.gov/citations/19770025195
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021a. “Airworthiness Verification Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00009-7
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021b. “Combined Test of the Flight Control Subsystem.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00005-x
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021c. “Development and Expectations on Test Techniques of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00010-3
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021d. “Flight Control System Control Law and the Flying Quality Evaluation Test.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00004-8
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021e. “Flight Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00008-5
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021f. “Onboard Ground Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00007-3
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021g. “Unit Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00002-4
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021h. “Verification and Validation of Flight Control System Airborne Software.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00003-6
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021i. ““Iron Bird” Integration Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00006-1
• Garcia, Joseph A., Jeffrey V. Bowles, David J. Kinney, John E. Melton, and Xun J. Jiang. 2019. VIPER Integrated MDAO Analysis for Conceptual Design of Supersonic X-Plane Vehicles. NASA/TM—2019–220239. NASA. https://ntrs.nasa.gov/citations/20190027157
• Garcia, F., Jr., R. M. Hicks, and J. P. Mendoza. 1973. A Wind Tunnel Flight Correlation of Apollo 16 Sonic Boom. NASA-TM-X-62073. NASA. https://ntrs.nasa.gov/citations/19730012346
• Garcia, F., Jr., J. H. Jones, and H. R. Henderson. 1985. Correlation of Predicted and Measured Sonic Boom Characteristics from the Reentry of STS-1 Orbiter. NASA-TP-2475. NASA. https://ntrs.nasa.gov/citations/19850021382
• Garcia, F., Jr., K. M. Morrison, J. H. Jones, and H. R. Henderson. 1982. Preliminary Sonic Boom Correlation of Predicted and Measured Levels for STS-1 Entry. NASA-TM-58242. NASA. https://ntrs.nasa.gov/citations/19820013160
• Garcia-Llama, Eduardo. 2007. “Analytic Guidance for the First Entry in a Skip Atmospheric Entry.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6897. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6897
• Garcia-Velo, Juan, and Bruce Walker. 1995. “Aerodynamic Parameter Estimation for High-Performance Aircraft Using Extended Kalman Filtering.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3500. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3500
• Gardinier, Debra, and Anthony Taylor. 1999. “Design and Testing of the K-1 Reusable Launch Vehicle Landing System Airbags.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1757
• Gardner, Anthony, Armin Weiss, James T. Heineck, et al. n.d. “Boundary Layer Transition Measured by DIT on the PSP Rotor in Forward Flight.” In Vertical Flight Society Annual Forum. https://ntrs.nasa.gov/citations/20205009333
• Garland, Benjamine J., Andrew G. Swanson, and Katherine C. Speegle. 1957. Aerodynamic Heating and Boundary-Layer Transition on a 1/10-Power Nose Shape in Free Flight at Mach Numbers up to 6.7 and Free-Stream Reynolds Numbers up to 16 x 10(exp 6). NACA-RM-L57E14a. NASA. https://ntrs.nasa.gov/citations/19930089758
• Garman, Karl, and Dominick Andrisani. 2003. “A Portable Data Acquisition System for Flight Testing Light Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5618
• Garoutte, S., and J. Bryan. 1983. “New Radar Calibration and Performance Monitoring Techniques for Enhanced Flight Test Data.” In 2nd Flight Testing Conference. AIAA 1983-2780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2780
• Garrard, W., and B. Liebst. 1983. “Active Flutter Suppression Using Eigenspace and Linear Quadratic Design Techniques.” In Guidance and Control Conference. AIAA 1983-2222. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2222
• Garretson, Mervin. 2012. “The Sonic Boom of 1994.” In Deaf American Prose, 1980–2010. Gallaudet University Press. https://doi.org/10.2307/j.ctv2rcngb8.5
• Garrett, Mike, David Avanesian, Matthew Granger, et al. 2019. “Development of an 11 kW Lightweight, High Efficiency Motor Controller for NASA X-57 Distributed Electric Propulsion Using SiC MOSFET Switches.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4400
• Garrick, I. E. 1968. Atmospheric Effects on the Sonic Boom. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19680025436
• Garringer, D. J., and E. J. Saltzman. 1966. Summary of Full-Scale Lift and Drag Characteristics of the X-15 Airplane. NASA-TN-D-3343. NASA. https://ntrs.nasa.gov/citations/19660010056
• Gates, Russell, Albion Bowers, and Richard Howard. 1996. “A Comparison of Flight Input Techniques for Parameter Estimation of Highly-Augmented Aircraft.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3363. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3363
• Gates, Ordway B., Jr., and Leonard Sternfield. 1950. Effect of an Autopilot Sensitive to Yawing Velocity on the Lateral Stability of the Douglas D-558-II Airplane. NACA-RM-L50F22. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019392
• Gebert, Glenn, Joy Kelly, Juan Lopez, and Johnny Evers. 2000a. “Virtual Flight Testing in a Ground Test Facility.” In 18th Applied Aerodynamics Conference. AIAA 2000-4019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4019
• Gebert, Glenn, Joy Kelly, Juan Lopez, and Johnny Evers. 2000b. “Wind Tunnel Based Virtual Flight Testing.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-829. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-829
• Gee, Kent L., Daniel J. Novakovich, Logan T. Mathews, Mark C. Anderson, and Reese D. Rasband. 2020. Development of a Weather-Robust Ground-Based System for Sonic Boom Measurements. NASA/CR-20205001870. NASA. https://ntrs.nasa.gov/citations/20205001870
• Geiger, Clarence J. 1963. History of the X-20A Dyna-Soar. Volume I.. Defense Technical Information Center. https://doi.org/10.21236/ada951933
• Gelzer, Christian, and Curtis Peebles. 2015. “The NACA’s High Speed Flight Research Station and the Development of Reaction Control Systems.” In The NACA Centenary: A Symposium on 100 Years of Aerospace Research and Development. https://ntrs.nasa.gov/citations/20160000534
• Genaro, Gino, and José Bezerra Pessoa Filho. 2006. “Simulation of a Multilayer Thermal Protection System Submitted to Conditions Representative of Atmospheric Reentry.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-c2.7.08
• General Dynamics/Astronautics San Diego Ca. 1961. WS 107A-1 Flight Test Working Group, Flight Test Report, Atlas Missile 32E. Defense Technical Information Center. https://doi.org/10.21236/ad0843200
• General Dynamics/Astronautics San Diego Ca. 1962. (WS 107A-1) Flight Test Working Group Flight Test Report Atlas Missile 11F. AMR Range Test Number 71. Defense Technical Information Center. https://doi.org/10.21236/ad0852659
• General Dynamics/Astronautics San Diegoca. 1961. WS 107-1 Flight Test Working Group, Flight Test Report, Atlas Missile 26E.. Defense Technical Information Center. https://doi.org/10.21236/ad0843112
• General Electric Co Cincinnati Oh. 1964. XV-5A Lift Fan Flight Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0447839
• “Generally on Automatic Flight Control.” n.d. In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0043100
• Gennaretti, M., U. Iemma, and L. Morino. 1996. “BEM for Aerodynamics and Aeroacoustics of Rotors in Subsonic/transonic Forward Flight.” In Aeroacoustics Conference. AIAA 1996-1699. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1699
• Gentry, J. 1968. “Lifting Body Flight Test.” In 2nd Simulation and Support Conference. AIAA 1968-243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-243
• Gentry, Jerauld R. 1972. “Lifting Body Flight Test.” Aeronautical Journal 76 (736): 268–70. https://doi.org/10.1017/s0001924000043013
• Gentry, J. R., B. A. Peterson, and M. O. Thompson. 1966. Lifting-Body Flight Test Program. NASA. https://ntrs.nasa.gov/citations/19670039468
• George, Sara Mohan, S. S. Selvi, and J. R. Raol. 2022. “Aircraft Parameter Estimation Using Gaussian Sum Information Filter with Lyapunov Stability Analysis.” Webology 19 (1): 3275–90. https://doi.org/10.14704/web/v19i1/web19216
• Gera, J. 1986. “Dynamics and Controls Flight Testing of the X-29A Airplane.” In 24th Aerospace Sciences Meeting. AIAA 1986-167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-167
• Gera, Joseph, Dominick Andrisani II, Jeffrey E. Bauer, and David B. Crawford. 1987. Real-Time Comparison of X-29A Flight Data and Simulation Data. AIAA PAPER 87-0344. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19870035296
• Gera, Joseph, and John T. Bosworth. 1987. Dynamic Stability and Handling Qualities Tests on a Highly Augmented, Statically Unstable Airplane. NASA-TM-88297. NASA. https://ntrs.nasa.gov/citations/19870017487
• Gera, J., R. Wilson, E. Enevoldson, and L. Nguyen. 1981. “Flight Test Experience with High-Alpha Control System Techniques on the F-14 Airplane.” In 1st Flight Test Conference. AIAA 1981-2505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2505
• Gerdes, R. M., and C. S. Hynes. 1975. Factors Affecting Handling Qualities of a Lift-Fan Aircraft during Steep Terminal Area Approaches. NASA-TM-X-62424. NASA. https://ntrs.nasa.gov/citations/19750014241
• Gerlach, O. H. 1965. “High-Accuracy Instrumentation Techniques for Non-Steady Flight Measurements.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50009-9
• Gerlach, O. H. 1967. “Measurements of Performance, Stability and Control Characteristics in Non-Steady Flight with a High-Accuracy Instrumentation System.” In Aerospace Instrumentation. Elsevier. https://doi.org/10.1016/b978-1-4831-9836-1.50013-7
• German, Brian J., Ayush Jha, Siena K. S. Whiteside, and Jason R. Welstead. n.d. “Overview of the Research Aircraft for eVTOL Enabling techNologies (RAVEN) Activity.” In AIAA Aviation 2023 Forum. https://ntrs.nasa.gov/citations/20230006253
• Gertsen, W., and H. Shomber. 1965. “Longitudinal Handling Qualities Criteria: An Evaluation.” In Aircraft Design and Technology Meeting. AIAA 1965-780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-780
• Geuther, Steven, Kasey Ackerman, and Benjamin Simmons. 2024. “Overview of the Subscale RAVEN Flight Controls and Modeling Testbed.” In Proceedings of the Vertical Flight Society 80th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0080-2024-1185
• Geuther, Steven C., Benjamin M. Simmons, and Kasey A. Ackerman. n.d. “Overview of the Subscale RAVEN Flight Controls and Modeling Testbed.” In Vertical Flight Society’s 80th Annual Forum & Technology Display. https://ntrs.nasa.gov/citations/20240004190
• Ghaffari, Farhad. 1994. Navier-Stokes, Flight, and Wind Tunnel Flow Analysis for the F/A-18 Aircraft. NASA-TP-3478. NASA. https://ntrs.nasa.gov/citations/19950012699
• Ghanchi, Mohammadshadab A., and Srikanth Gururajan. 2026. “Lessons Learned from the Design, Development, and Subscale Flight Testing of a Hybrid-VTOL UAS.” In AIAA SCITECH 2026 Forum. AIAA 2026-1866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1866
• Ghate, Aditya S., Jordan B. Angel, Gaetan Kenway, Man Long Wong, and Cetin C. Kiris. 2026. “Large Eddy Simulations of High-Lift Common Research Model in the NTF Wind Tunnel at Flight Scale Reynolds Numbers.” In AIAA SCITECH 2026 Forum. AIAA 2026-0020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0020
• Ghate, Aditya S., Gaetan K. Kenway, Gerrit-Daniel Stich, Oliver M. Browne, Jeffrey A. Housman, and Cetin C. Kiris. 2021. “Transonic Lift and Drag Predictions Using Wall-Modelled Large Eddy Simulations.” In AIAA Scitech 2021 Forum. AIAA 2021-1439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1439
• Ghazi, Mohammad. 1993. “Wind Tunnel Investigation of Wind Shear Effect on Turning Flight.” In Flight Simulation and Technologies. AIAA 1993-3641. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3641
• Ghoreyshi, Mehdi, Keith Bergeron, Andrew J. Lofthouse, and Russell M. Cummings. 2016. “CFD Calculation of Stability and Control Derivatives for Ram-Air Parachutes.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1536
• Ghoreyshi, Mehdi, R. K. Nangia, and Michel van Rooij. 2022. “NATO AVT–316, Multi-Swept Combat Wing Design – Aerodynamic Ways towards a Robust Flight Envelope.” In AIAA SCITECH 2022 Forum. AIAA 2022-0296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0296
• Ghosh, Debdoot, and Hideaki Ogawa. 2022. “Design and Numerical Investigation of a Hypersonic Waverider Based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion.” In 26th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2022-2734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2734
• Ghosh, Mriganka S., and Mayuresh Patil. 2022. “Incorporation of Nonlinearities into Actuator Selection for Active Flutter Suppression.” In AIAA SCITECH 2022 Forum. AIAA 2022-1126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1126
• Ghosh, Mriganka S., and Mayuresh Patil. 2026. “Nonlinear Actuator Modeling and Describing Function Analysis for Active Flutter Suppression.” In AIAA SCITECH 2026 Forum. AIAA 2026-1061. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1061
• Ghosh, A., and S. Raisinghani. 1993. “Parameter Estimates of an Aeroelastic Aircraft as Affected by Model Simplifications.” In Flight Simulation and Technologies. AIAA 1993-3640. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3640
• Ghosh, A., and S. Raisinghani. 2000. “Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4102
• Ghosh, A., S. Raisinghani, and L. Patnaik. 2000. “Parameter Estimation from Flight Data with Process and Measurement Noise Using Neural Networks.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4101
• Ghosh Roy, Abhishek, and Naba Kumar Peyada. 2016. “Stable and Unstable Aircraft Parameter Estimation in Presence of Noise Using Intelligent Estimation Technique.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3708. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3708
• Ghosh Roy, Abhishek, and N. K. Peyada. 2017. “Longitudinal Aircraft Parameter Estimation Using Neuro-Fuzzy and Genetic Algorithm Based Method.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-3896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3896
• Gibbings, J. C. 1982. “The Use of Dimensional Analysis in Aerodynamics: An Historical Note.” Aeronautical Journal 86 (855): 176–78. https://doi.org/10.1017/s000192400001873x
• Gibbons, Michael, and Johnt. Batina. 1989. “Supersonic Far-Field Boundary Conditions for Transonic Small-Disturbance Theory.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1283
• Gibson, W. 1981. “Flight Testing De Havilland Aircraft Limited DASH-8 Utilizing Onboard Data Analysis by Microprocessor.” In 1st Flight Test Conference. AIAA 1981-2507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2507
• Gibson, T. 2002. “Investigation of Wind Tunnel Model Deformation under High Reynolds Number Aerodynamic Loading.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-424. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-424
• Gibson, F. W., and R. C. Goetz. 1971. Investigation of Control-Surface Instabilities on Lifting-Body Reentry Vehicles at a Mach Number of 15.4. NASA-TN-D-6301. NASA. https://ntrs.nasa.gov/citations/19710021765
• Gibson, Chris, James Neidhoefer, Stephen Cooper, Lindley Carlton, Chadwick Cox, and Charles Jorgensen. 2002. “Development and Flight Test of the X-43A-LS Hypersonic Configuration UAV.” In 1st UAV Conference. AIAA 2002-3462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3462
• Giessler, F. J., and John F. Nash. 1971. O-2A Aircraft Sea Flight Loads Recording Program. Defense Technical Information Center. https://doi.org/10.21236/ada030351
• Gilbert, Leon M. n.d. “Thermal Degradation of a Char Forming Plastic during Hypersonic Flight.” PhD diss., Drexel University. https://doi.org/10.17918/00006518
• Gilbert, M. G., D. K. Schmidt, and T. A. Weisshaar. 1982. Quadratic Synthesis of Integrated Active Controls for an Aeroelastic Forward-Swept-Wing-Aircraft. AIAA PAPER 82-1544. Purdue Univ. https://ntrs.nasa.gov/citations/19830031240
• Gilbert, Michael, and Walter Silva. 1987. “The Effects of Aeroelastic Deformation on the Unaugmented Stopped-Rotor Dynamics of an X-Wing Aircraft.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2563
• Gilbrook, Aaron J., Yiyuan Ma, and Ali Elham. 2023. “Conceptual Design and Optimization of a Strut-Braced Wing Full Electric Regional Aircraft with Distributed Propulsion.” In AIAA AVIATION 2023 Forum. AIAA 2023-4428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4428
• Gillan, Mark. 1993. “Computational Analysis of Drag Reduction and Buffet Alleviation in Viscous Transonic Flow over Porous Airfoils.” In 11th Applied Aerodynamics Conference. AIAA 1993-3419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3419
• Gillespie, Warren, Jr., and Richard G. Arbic. 1951. Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.87 to 1.39 of 1/10-Scale Models of the Northrop MX-775A Missile. NACA-RM-SL51K07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030052
• Gillis, Clarence L. 1957. A Brief Analog Investigation of Inertia Coupling in Rolling Maneuvers of an Airplane Configuration Using a Variable-Incidence Wing as the Longitudinal Control. NACA-RM-L57F18. NASA. https://ntrs.nasa.gov/citations/19930089776
• Gillis, Clarence L., and Rowe Chapman Jr. 1953. Summary of Pitch-Damping Derivatives of Complete Airplane and Missile Configurations as Measured in Flight at Transonic and Supersonic Speeds. NACA-RM-L52K20. NASA. https://ntrs.nasa.gov/citations/19930087384
• Gilruth, Robert R. 1962. “Section l. Objectives of Free Flight Research.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-014
• Gilyard, G. B. 1972. Flight-Determined Derivatives and Dynamic Characteristics of the CV-990 Airplane. NASA-TN-D-6777. NASA. https://ntrs.nasa.gov/citations/19720015377
• Gilyard, G. B., and D. Belte. 1974. Flight-Determined Lag of Angle-of-Attack and Angle-of-Sideslip Sensors in the YF-12A Airplane from Analysis of Dynamic Maneuvers. NASA-TN-D-7819. NASA. https://ntrs.nasa.gov/citations/19740026347
• Gilyard, G. B., and J. W. Edwards. 1983. “Real-Time Flutter Analysis of an Active Flutter-Suppression System on a Remotely Piloted Research Aircraft.” In AGARD Ground(Flight Test Tech. and Correlation. https://ntrs.nasa.gov/citations/19830022109
• Gilyard, Glenn B., and Donald K. Hill. 1978. Flight Determined Longitudinal and Lateral-Directional Derivatives of the YF-12A Airplane (U). AFRC-E-DAA-TN72852. NASA Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20200000229
• Gimmestad, D. 1981. “Aeroelastic Tailoring of a Composite Winglet for KC-135.” In Dynamics Specialists Conference. AIAA 1981-607. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-607
• Gindin, Yosef, and Eliezer Darom. 1996. “Simulation Tools within an Aircraft Upgrade Program: A Cost-Effective Approach.” In Flight Simulation Technologies Conference. AIAA 1996-3522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3522
• Ginn, Starr. 2014. “Enabling Electric Propulsion for Flight.” In IMECH Disruptive Green Propulsion Technologies. https://ntrs.nasa.gov/citations/20140017743
• Ginn, Starr Renee. 2015. “Enabling Electric Propulsion for Flight.” In Aerospace Electrical Systems Expo. https://ntrs.nasa.gov/citations/20150009298
• Gion, E. J. 1976. Plane Shock: Thermal Layer Interactions. Defense Technical Information Center. https://doi.org/10.21236/adb013138
• Girgis, I., G. Brown, and R. Miles. 2002. “Heat Transfer and Boundary Layer Growth for Ultra High Reynolds Number Compressible Turbulent Boundary Layers for a Radiatively Driven Hypersonic Wind Tunnel.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-575
• Glaser, Scott T., and Brian K. Strovers. 2011. “Handling Qualities Flight Testing of the Stratospheric Observatory for Infrared Astronomy (SOFIA).” In Society of Flight Test Engineers. https://ntrs.nasa.gov/citations/20110023827
• Glass, David, and Christopher Glass. 2002. “Airframe Research and Technology for Hypersonic Airbreathing Vehicles.” In AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2002-5137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5137
• Glauert, H. 1928. “The Effect of Compressibility on the Lift of an Aerofoil.” Proceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character 118 (779): 113–19. https://doi.org/10.1098/rspa.1928.0039
• Glazkov, S. A., A. R. Gorbushin, S. L. Osipova, and A. V. Semenov. 2016. “Influence of Movable Test Section Elements Configuration on Its Drag and Flow Field Uniformity at Transonic Speeds.” In AIP Conference Proceedings, vol. 1770. Author(s). https://doi.org/10.1063/1.4963950
• Glazkov, S. A., and A. V. Semenov. 2024. “Wind-Tunnel Wall Interference and Experimental Data Corrections in Subsonic Flows.” In 22-st INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2022). Crossref. https://doi.org/10.53954/9785604990148_62
• Gleason, Daniel, David Walker, and Norman Howell. 1996. “USAF Test Pilot School Test Management Program.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-159. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-159
• Glezer, Ari. 2009. Diagnostics for Wind Tunnel Dynamic Flight Maneuvering Using Controlled, Trapped Vorticity. Defense Technical Information Center. https://doi.org/10.21236/ada584974
• Glezer, Ari. 2012. Diagnostics for Wind Tunnel Dynamic Flight Maneuvering Using Controlled, Trapped Vorticity. Defense Technical Information Center. https://doi.org/10.21236/ada564711
• Glowacki, Walter J. 1971. NOL Hypervelocity Wind Tunnel. Report No. 2: Nozzle Design. Defense Technical Information Center. https://doi.org/10.21236/ad0727591
• Gnemmi, P., J. Haertig, and M. Schaffar. 1991. “Computation of the BVI Noise for the BO105 Model Rotor in Forward Flight and Comparison with Wind Tunnel Tests.” In Proceedings of the Vertical Flight Society Forum 47 - Phoenix, AZ 1991. The Vertical Flight Society. https://doi.org/10.4050/vfs-f47-2003
• Gnoffo, Peter A. 1989a. “Conservation Equations and Physical Models for Hypersonic Air Flows over the Aeroassist Flight Experiment Vehicle.” In NASA, Ames Research Center, NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12. https://ntrs.nasa.gov/citations/19910001584
• Gnoffo, Peter A. 1989b. “Upwind-Biased, Point-Implicit Relaxation Strategies for Viscous, Hypersonic Flows.” In AIAA Computational Fluid Dynamics Conference. https://ntrs.nasa.gov/citations/19890054445
• Gnoffo, Peter A., and Francis A. Greene. 1987. A Computational Study of the Flowfield Surrounding the Aeroassist Flight Experiment Vehicle. AIAA PAPER 87-1575. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19870055810
• Godil, A., and A. Bertelrud. 1992. “Design of a Wing Shape for Study of Hypersonic Crossflow Transition in Flight.” Computing Systems in Engineering 3 (4-Jan). https://ntrs.nasa.gov/citations/19930036716
• Godwin, O. D., F. D. Frazier, and R. E. Durnin. 1964. Performance Flight Test Techniques. Defense Technical Information Center. https://doi.org/10.21236/ad0613504
• Goecke, S. A. 1971. Comparison of Wind Tunnel and Flight-Measured Base Pressures from the Sharp-Leading-Edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0. NASA-TN-D-6348. NASA. https://ntrs.nasa.gov/citations/19710014446
• Goecke, S. A. 1973. Flight-Measured Base Pressure Coefficients for Thick Boundary-Layer Flow over an Aft-Facing Step for Mach Numbers from 0.4 to 2.5. NASA-TN-D-7202. NASA. https://ntrs.nasa.gov/citations/19730015590
• Goett, Harry J., and Joseph Bicknell. 1939. Comparison of Profile-Drag and Boundary-Layer Measurements Obtained in Flight and in the Full-Scale Wind Tunnel. NACA-TN-693. NASA. https://ntrs.nasa.gov/citations/19930081546
• Goetz, R. C. 1972. “Flutter Technology for Space Shuttle.” In NASA Space Shuttle Technol. Conf.. https://ntrs.nasa.gov/citations/19720023216
• Gohardani, Amir S., Georgios Doulgeris, and Riti Singh. 2011. “Challenges of Future Aircraft Propulsion: A Review of Distributed Propulsion Technology and Its Potential Application for the All Electric Commercial Aircraft.” Progress in Aerospace Sciences 47 (5): 369–91. https://doi.org/10.1016/j.paerosci.2010.09.001
• Gölcük, Ali İhsan, and Dilek Funda Kurtulus. 2026. “Numerical Investigation of NACA 64A-204 Airfoil Performance at Subsonic and Supersonic Regimes.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-5907-7_8
• Goldfeld, Marat. 2003. “Compressible Boundary Layer Investigation for Ramjet/Scramjet Inlets and Nozzles.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-4247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4247
• Goldthorpe, Steven, Kenneth Rossitto, David Hyde, and Krish Krothapalli. 2010. “X-48B Blended Wing Body Flight Test Performance of Maximum Sideslip and High to Post Stall Angle-of-Attack Command Tracking.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7514
• Gomes, Sergio, and David Speirits. 1991. “Airship Response to Turbulence: Results from a Flight Dynamics Simulation Combined with a Wind Tunnel Investigation.” In 9th Lighter-Than-Air Systems Technology Conference. AIAA 1991-1276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1276
• Gong, Les. 2005. Real-Time Simulation of Aeroheating of the Hyper-X Airplane. DRC-98-76. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110014692
• Gong, Chunlin, Bin Chen, and Liangxian Gu. 2014. “Design and Optimization of RBCC Powered Suborbital Reusable Launch Vehicle.” In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2014-2361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2361
• Gong, Leslie, William L. Ko, Robert D. Quinn, and W. Lance Richards. 1987. Comparison of Flight-Measured and Calculated Temperatures on the Space Shuttle Orbiter. NASA-TM-88278. NASA. https://ntrs.nasa.gov/citations/19880002647
• Gong, Andrew, Hugh Maunder, and Dries Verstraete. 2017. “Development of an in-Flight Thrust Measurement System for UAVs.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-5092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-5092
• Gong, Chester, and Minghong G. Wu. 2015. SSI-ARC Flight Test 3 Data Review. ARC-E-DAA-TN27374. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20160000575
• Gonzalez, Marcello, Marcel Ilie, and Cameron Perry. 2026. “Impact of a Supercritical Airfoil on the Transonic Aerodynamic Performance of an M-Wing.” In AIAA SCITECH 2026 Forum. AIAA 2026-0866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0866
• González Mendoza, Manuel A. 2026a. “Geometry-Dependent Aerodynamic Variability and Cross-Environment Consistency of UAV Payloads across CFD, Wind Tunnel, and Flight Testing.” Preprint, . https://doi.org/10.2139/ssrn.6501899
• González Mendoza, Manuel A. 2026b. “Quantifying Geometry-Dependent Cross-Environment Aerodynamic Variability of UAV Payloads in CFD, Wind Tunnel, and Flight Testing.” Preprint, . https://doi.org/10.2139/ssrn.7315084
• Goodman, R., and P. Conigliaro. 1986. “F-14A Low Altitude High Angle of Attack Simulation and Flight Test Program.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9774
• Goodman, Jenny, and Peter Ireland. 2006. “Thermal Modelling for the Sustained Hypersonic Flight Experiment.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8071
• Goodrich, W. D., S. M. Derry, and J. J. Bertin. 1983a. “Shuttle Orbiter Boundary Layer Transition at Flight and Wind Tunnel Conditions.” In NASA. Langley Research Center Shuttle Performance: Lessons Learned, Pt. 2. https://ntrs.nasa.gov/citations/19840002082
• Goodrich, W., S. Derry, and J. Bertin. 1983b. “Shuttle Orbiter Boundary-Layer Transition: A Comparison of Flight and Wind Tunnel Data.” In 21st Aerospace Sciences Meeting. AIAA 1983-485. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-485
• Goodson, Kenneth W. 1966. “Comparison of Wind-Tunnel and Flight Results on a Four-Propeller Tilt-Wing Configuration.” In Conference on V/STOL and STOL aircraft. https://ntrs.nasa.gov/citations/19660015322
• Goodwin, Gabriel B., Ryan F. Johnson, David Kessler, and Harsha K. Chelliah. 2019. “Premixed Ethylene-Air Combustion in a Dual-Mode Scramjet Cavity Combustor with a Turbulent Inflow.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4270
• Goodyer, M. 1990. “An Aerofoil Testing Technique for Low Supersonic Speeds in an Adaptive Flexible-Walled Wind Tunnel.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3086
• Goodyer, M., and R. Kilgore. 1972. “The High Reynolds Number Cryogenic Wind Tunnel.” In 7th Aerodynamic Testing Conference. AIAA 1972-995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-995
• Gopal, Vijay, Gowtham Sai Somaroutu, Aswin Suresh, and Harshwardhan Prasad. 2026. “Development of High Unit-Reynolds Number Supersonic Wind Tunnel Facility at the University of Texas at Arlington.” In AIAA SCITECH 2026 Forum. AIAA 2026-2544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2544
• Gopal, Vijay, and Donald Wilson. 2016. “Reduced-Order Analysis of Dual Mode Scramjet Isolator Operation.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1167
• Goraj, Zdobyslaw, Jonas Stankunas, Martinsh Kleinhofs, Villu Mikita, and Antonin Pištek. 2007. “A Short History of Seminars on “Recent Research and Design Progress in Aeronautical Engineering and Its Influence on Education”.” Aviation 11 (1): 3–5. https://doi.org/10.3846/16487788.2007.9635948
• Gorn, Michael H. 2003. An Indispensable Ingredient: Flight Research and Aircraft Design. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20050201678
• Gorton, Susan. 2015a. “NASA Overview: Vertical Flight Research.” In Proceedings of the Rotorcraft Propulsion Specialists Meeting - Williamsburg, Virginia 2015. The Vertical Flight Society. https://doi.org/10.4050/sm_prop_2015-3564
• Gorton, Susan A. 2015b. “NASA Vertical Flight Research.” In Annual AHS International Forum and Technology Display. https://ntrs.nasa.gov/citations/20150008412
• Gotlieb, P. 1977. “The Preliminary Design of a Lift-Cruise Fan Airplane Flight Control System.” In V/STOL Conference. AIAA 1977-602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-602
• Gotlieb, P., G. E. Lewis, and L. J. Little. 1976. Preliminary Design-Lift/cruise Fan Research and Technology Airplane Flight Control System. NASA-CR-137971. NASA. https://ntrs.nasa.gov/citations/19770004121
• Göttlicher, Christoph, Marcus Gnoth, Matthias Bittner, and Florian Holzapfel. 2016. “Aircraft Parameter Estimation Using Optimal Control Methods.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1534
• Gottlieb, Jonah R., John M. Mines, Daniel C. Garmendia, Jerold W. Emhoff, and Daniel E. Clemens. 2024. “Coupled Vehicle and Trajectory Design Optimization for Boost-Glide Hypersonic Systems.” In AIAA SCITECH 2024 Forum. AIAA 2024-0373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0373
• Goupil, Marc Y. n.d. “Dynamic Pressure Sensing for the Flight Test Data System.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2020.10
• Gove, W. D. 1929. The Variation in Engine Power with Altitude Determined from Measurements in Flight with a Hub Dynamometer. NACA-TR-295. NASA. https://ntrs.nasa.gov/citations/19930091364
• Gowtham, M., N. Sreenivasaraja, and Kasmir Anthireyan. 2022. “Mathematical Derivation of Different Nose Angles to Reduce Drag Force on Rocket.” International Journal of Innovative Research in Advanced Engineering 9 (12): 471–82. https://doi.org/10.26562/ijirae.2022.v0912.03
• Goyne, Christopher, Christopher Hall, Walter O’Brien, and Joseph Schetz. 2006. “The Hy-V Scramjet Flight Experiment.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7901
• Graber, B., E. Softley, and R. Zempel. 1968. “Experimental Observation of Transition of the Hypersonic Boundary Layer.” In 6th Aerospace Sciences Meeting. AIAA 1968-39. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-39
• Grabowsky, W., H. Eldridge, and R. Wheaton. 1981. “Reentry Vehicle Instrumentation Survey.” In 1st Flight Test Conference. AIAA 1981-2372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2372
• Gracey, W. 1967. Operational Aspects of Steep VTOL Approaches as Determined from Helicopter Tests under Simulated IFR Conditions. NASA-TM-X-60457. NASA. https://ntrs.nasa.gov/citations/19680018078
• Graf, E., Th. Leveugle, Ph. Berthe, Ralf Klaedtke, and Luciano Basile. 1998. “International Cooperation on X-38 and Crew Return Vehicles (X-38/CRV) for the International Space Station.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1635
• Grafe, M., D. Yemelyanau, and S. Ginka. 2026. “B2.1: Deterministic Time-Synchronized Wireless Sensors for Lightweight Flight Test Instrumentation.” In Lectures. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2026/b2.1
• Grafton, S., W. Gilber, M. Croom, and D. Murri. 1982. “High Angle-of-Attack Characteristics of a Forward-Swept Wing Fighterconfiguration.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1322. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1322
• Graham, David, John Dahlin, Keith Meredith, and Jay Vadnais. 2005. “Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-8. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-8
• Graham, Gary, and Kim Yeow. 1990. “Two Dimensional Post Stall Maneuver of a NACA 0015 Airfoil at High Pitching Rates.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2810. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2810
• Grant, Daniel, Mujahid Abdulrahim, and Rick Lind. 2006. “Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing Sweep.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6505
• Grant, Peter R., Zhanhong Luo, Stacey F. Liu, and Gregory J. Moszczynski. 2017. “Development of Post-Stall Flight Models from Certification Flight Test and Wind-Tunnel Data.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2017-1549. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1549
• Grant, Frederick C., and John R. Sevier Jr. 1960. Transonic and Supersonic Wind-Tunnel Tests of Wing-Body Combinations Designed for High Efficiency at a Mach Number of 1.41. NASA-TN-D-435. NASA. https://ntrs.nasa.gov/citations/19980230620
• Grant, John, Harvey Willenberg, Brian Tillotson, Joseph Stemler, Michal Bangham, and Robert Forward. 2000. “Hypersonic Airplane Space Tether Orbital Launch: HASTOL: A Two-Stage Commercial Launch System.” In Space 2000 Conference and Exposition. AIAA 2000-5353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5353
• Grantham, William D., Lee H. Person Jr., Philip W. Brown, et al. 1985b. Handling Qualities of a Wide-Body Transport Airplane Utilizing Pitch Active Control Systems (PACS) for Relaxed Static Stability Application. NASA-TP-2482. NASA. https://ntrs.nasa.gov/citations/19880005605
• Grantham, W. D., P. M. Smith, W. R. Neely Jr., P. L. Deal, and K. R. Yenni. 1985a. Ground-Based and in-Flight Simulator Studies of Flight Characteristics of a Twin-Fuselage Passenger Transport Airplane during Approach and Landing. NASA-TP-2451. NASA. https://ntrs.nasa.gov/citations/19850025831
• Grantham, William, and Robert Williams. 1987. “Comparison of in-Flight and Ground-Based Simulator Derived Flying Qualities and Pilot Performance for Approach and Landing Tasks.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2290
• Grantz, Arthur. 1994. “Calibration of Aerodynamic Engineering Methods for Waverider Design.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-382. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-382
• Grantz, Arthur. 2011. “X-37B Orbital Test Vehicle and Derivatives.” In AIAA SPACE 2011 Conference & Exposition. AIAA 2011-7315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-7315
• Grasmeyer, Joel. 1999. “Multidisciplinary Design Optimization of a Transonic Strut-Braced Wing Aircraft.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-10. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-10
• Gratton, Guy. 2018. “The Flight Envelope.” In Initial Airworthiness. Springer International Publishing. https://doi.org/10.1007/978-3-319-75617-2_4
• Grauer, Jared. n.d.-a. “Advances in Aircraft System Identification at NASA Langley Research Center.” In Princeton University Seminar Series. https://ntrs.nasa.gov/citations/20240004342
• Grauer, Jared A. n.d.-b. “Flight Dynamics and Control Research at NASA Langley Research Center (LaRC).” In Aerospace Control and Guidance Systems Committee (ACGSC) Meeting #136. https://ntrs.nasa.gov/citations/20260002745
• Grauer, Jared A. n.d.-c. “Recent System Identification Research at NASA Langley Research Center.” In 20th Mechanics in Aviation Conference. https://ntrs.nasa.gov/citations/20220016828
• Grauer, Jared A. 2018. Dynamic Modeling Using Output-Error Parameter Estimation Based on Frequency Responses Estimated with Multisine Inputs. NASA/TM-2018-220108. NASA. https://ntrs.nasa.gov/citations/20180008442
• Grauer, Jared A. 2020a. Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements. NF1676L-35569. Langley Research Center. https://ntrs.nasa.gov/citations/20200003206
• Grauer, Jared A. 2020b. “Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements.” In AIAA SciTech 2020. https://ntrs.nasa.gov/citations/20200002779
• Grauer, Jared A., and Matthew J. Boucher. n.d. “System Identification of Flexible Aircraft: Lessons Learned from the X-56A Phase 1 Flight Tests.” In AIAA SciTech 2020. https://ntrs.nasa.gov/citations/20200002775
• Grauer, Jared A., and Matthew Boucher. 2017. “Aeroelastic Modeling of X-56A Stiff-Wing Configuration Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0699. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0699
• Grauer, Jared A., and Matthew J. Boucher. 2018. “Real-Time Parameter Estimation for Flexible Aircraft.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3155
• Grauer, Jared, Jennifer Heeg, and Eugene Morelli. 2012. “Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4641. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4641
• Grauer, Jared A., and Eugene A. Morelli. 2024. Aircraft Parameter Estimation Considering Process and Measurement Noise. Langley Research Center. https://ntrs.nasa.gov/citations/20240006797
• Grauer, Jared, and Josiah Waite. 1986. “Design of a Collocation-Based Active Flutter Suppression Control Law for the IAWTM Wind Tunnel Model.” In Guidance, Navigation and Control Conference. AIAA 1986-2242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2242
• Grauer, Jared A., and Josiah Waite. 2024. “Design of a Collocation-Based Active Flutter Suppression Control Law for the IAWTM Wind Tunnel Model.” In AIAA SCITECH 2024 Forum. AIAA 2024-2201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2201
• Graves, Rick. 2013. “Continuum-Limit Design and Optimization of an Osculating-Cones Waverider at Mach 20.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-1096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1096
• Gray, W., Jr. 1964. “Nasa Flight Research Center Handling-Qualities Program on General-Aviation Aircraft.” In General Aviation Aircraft Design and Operations Meeting. AIAA 1964-192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-192
• Graziani, Samuele, Leonardo Ialongo, Roberta Fusaro, and Nicole Viola. 2025. “Towards Early-Stage Sonic Boom Prediction: From Hypersonic Vehicles to Low-Boom Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.5583632
• Graziani, Samuele, Nicole Viola, Roberta Fusaro, Sebastien Hengy, Marie Albisser, and Bastien Martinez. 2024. “Sonic Boom Numerical Validation of a Mach 4.7 Experimental Test.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3184
• Greatrex, F. B. 1963. “Take-Off and Landing of the Supersonic Transport: A Paper Presented at the Symposium Held at Southampton University on Noise Problems of the Supersonic Transport.” Aircraft Engineering and Aerospace Technology 35 (8): 221–25. https://doi.org/10.1108/eb033765
• Green, William. 1980. High Performance Auxiliary Power Unit Technology Demonstrator. Defense Technical Information Center. https://doi.org/10.21236/ada098618
• Green, J. 1986. “Aeroelastic Tailoring of Composite Wings with External Stores.” In 27th Structures, Structural Dynamics and Materials Conference. AIAA 1986-1021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1021
• Green, Bradford. 2008. “Computational Prediction of Roll Damping for the F/A-18E at Transonic Speeds.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6379
• Green, M., M. Budnick, and L. Yang. 1983. “Supporting Flight Data Analysis for Space Shuttle Orbiter Experiments at NASA Ames Research Center.” In 18th Thermophysics Conference. AIAA 1983-1532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1532
• Green, Steven, and Dennis Fernandez. 1994. “F117A Composite Rudder Aeroelastic Stability Flight Test Program.” In Biennial Flight Test Conference. AIAA 1994-2107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2107
• Greene, L. P. 1958. X-15 Research Airplane Development Status. NASA. https://ntrs.nasa.gov/citations/19930092381
• Greene, Joel. 1964. “A Daylight Astro Tracker for Supersonic Transport Navigation.” Navigation 11 (3): 228–36. https://doi.org/10.1002/j.2161-4296.1964.tb02097.x
• Greene, Francis, Gregory Buck, and William Wood. 2001. “Measured and Computed Hypersonic Aerodynamic/aeroheating Characteristics for an Elliptically Blunted Flared Cylinder.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-562
• Greene, G. C., T. C. Kelly, and R. J. Keynton. 1966. Effects of Model Geometric Accuracy on Comparison of Wind-Tunnel and Flight Pressure Measurements on a Launch Vehicle. NASA-TN-D-3274. NASA. https://ntrs.nasa.gov/citations/19660009170
• Greene, R. L., and M. L. Nacht. 1967. Panel Flutter Studies of Boost-Vehicle Full-Scale Flight Insulation Panels. NASA-TM-X-1417. NASA. https://ntrs.nasa.gov/citations/19670023223
• Greenwell, Douglas. 2004. “A Review of Unsteady Aerodynamic Modelling for Flight Dynamics of Manoeuvrable Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5276
• Greer, W. L. 2010. An Application of Cost-Effectiveness Analysis in a Major Defense Acquisition Program: The Decision by the U.S. Department of Defense to Retain the C-17 Transport Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada537484
• Gregorek, G. M., M. J. Hoffmann, G. S. Weislogel, and G. M. Vogel. 1977. “In-Flight Measurements of the GA(W)-2 Aerodynamic Characteristics.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/770461
• Gregory, B. R. 1970. Post Flight Dynamic Analysis Simulation. MFS-15067. BOEING CO. https://ntrs.nasa.gov/citations/19700000585
• Gregory, Irene M., Enric Xargay, Chengyu Cao, and Naira Hovakimyan. 2010. “Flight Test of an L(sub 1) Adaptive Controller on the NASA AirSTAR Flight Test Vehicle.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100033219
• Gregory, Irene, Enric Xargay, Chengyu Cao, and Naira Hovakimyan. 2011. “Flight Test of L1 Adaptive Control Law: Offset Landings and Large Flight Envelope Modeling Work.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6608
• Griffin, Kenneth. 2006. “Highly Aeroelastic Control Derivative Linear Modeling for Active Aeroelastic Wing.” In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th. AIAA 2006-2163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-2163
• Griffin, K., and F. Eastep. 1981. “Active Control of Forward Swept Wings with Divergence and Flutter Aeroelastic Instabilities.” In Dynamics Specialists Conference. AIAA 1981-637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-637
• Griffin, K., and F. Jonas. 1983. “Wake Characteristics and Interactions of the Canard/wing Lifting Surface Configuration of the X-29 Forward-Swept Wing Flight Demonstrator.” In Applied Aerodynamics Conference. AIAA 1983-1835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1835
• Grimm, Sabine, Alan Brennan, and Anna Heath. 2023. “Value of Information and Implementation.” In Value of Information for Healthcare Decision-Making. Chapman and Hall/CRC. https://doi.org/10.1201/9781003156109-12
• Grindle, Laurie. 2011. “X-43A Final Flight Observations.” In 2011 Flight Test Safety Workshop. https://ntrs.nasa.gov/citations/20110014424
• Grindle, Laurie. 2012. “Hyper-X/X-43A: Dryden’s Role.” In Lockheed Martin Interchange. https://ntrs.nasa.gov/citations/20120016867
• Grindle, Laurie, and Catherine Bahm. 2006. The X-43A (Hyper-X) Flies into the Record Books. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20060056098
• Grindle, Laurie, Robert Sakahara, Davis Hackenberg, and William Johnson. 2017. Unmanned Aircraft Systems (UAS) Integration in the National Airspace System (NAS) Project KDP-C Review. AFRC-E-DAA-TN43956. NASA Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20170006091
• Groot, Koen J., Ethan S. Beyak, Daniel T. Heston, and Helen L. Reed. 2020. “Boundary-Layer Stability of a Natural-Laminar-Flow Airfoil at Flight Conditions.” In AIAA Aviation 2020 Forum. AIAA 2020-3052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3052
• Grose, D. L. 1979. “The Development of the DAST I Remotely Piloted Research Vehicle for Flight Testing an Active Flutter Suppression Control System.” PhD diss., Kansas Univ.. https://ntrs.nasa.gov/citations/19790009678
• Grossir, Guillaume, Davide Masutti, and Olivier Chazot. 2015. “Flow Characterization and Boundary Layer Transition Studies in VKI Hypersonic Facilities (Invited).” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0578
• Grossman, Ben T. 2025. “Supersonic Rocket Sled Testing at Hurricane Mesa Test Facility.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3730
• “Ground and Flight Testing of Digital Flight Control Systems.” 2000. In Flight Control Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866555.0197.0224
• “Ground Testing Facility for Hypersonic Materials.” 2023. Aerospace Testing International 2023 (1): 91–91. https://doi.org/10.12968/s1478-2774(23)50337-9
• “Ground Testing of X-48B Blended Wing Body Concept.” 2007. Aircraft Engineering and Aerospace Technology 79 (2). https://doi.org/10.1108/aeat.2007.12779bab.029
• Gruber, Mark, Todd Barhorst, Kevin Jackson, et al. 2009. “Instrumentation and Performance Analysis Plans for the HIFiRE Flight 2 Experiment.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090041353
• Guan, X. 2014a. “Supersonic Wing-Body Wave Drag Co-Ordinated Optimisation Based on FCE Methodology.” Aeronautical Journal 118 (1209): 1359–72. https://doi.org/10.1017/s0001924000010010
• Gubbels, Arthur, Stephan Carignan, and D. Ellis. 2000. “The NRC Bell 412 Advanced Systems Research Aircraft: Facility Description and Results of Safety System Flight Tests.” In Modeling and Simulation Technologies Conference. AIAA 2000-4577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4577
• Gudmundsson, Snorri. 2014a. “Aircraft Cost Analysis.” In General Aviation Aircraft Design. Elsevier. https://doi.org/10.1016/b978-0-12-397308-5.00002-7
• Gudmundsson, Snorri. 2014b. “Aircraft Drag Analysis.” In General Aviation Aircraft Design. Elsevier. https://doi.org/10.1016/b978-0-12-397308-5.00015-5
• Gudmundsson, Snorri. 2022a. “Aircraft Cost Analysis.” In General Aviation Aircraft Design. Elsevier. https://doi.org/10.1016/b978-0-12-818465-3.00003-3
• Gudmundsson, Snorri. 2022b. “Aircraft Drag Analysis.” In General Aviation Aircraft Design. Elsevier. https://doi.org/10.1016/b978-0-12-818465-3.00016-1
• Guelhan, Ali, Florian Klingenberg, Sebastian Willems, et al. 2026. “Long Duration Hypersonic Flight Experiment ATHEAt.” In AIAA SCITECH 2026 Forum. AIAA 2026-0528. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0528
• Guelhan, Ali, Frank Siebe, Thomas Thiele, Dominik Neeb, John Turner, and Josef Ettl. 2012. “Instrumentation of the SHEFEX-II Flight Experiment and Selected Flight Data.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5819
• Guerreiro, Nelson, and James Hubbard. 2008. “Flight Testing of a Model Aircraft with Trailing-Edge Flaps Optimized for Lift Distribution Control.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6709. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6709
• Guiot, R., and H. Wunnenberg. 1980. “Comparison of Aerodynamic Coefficients Obtained from Theoretical Calculations Wind Tunnel Tests and Flight Tests Data Reduction for the Alpha Jet Aircraft.” In Meeting of the Flight Mech. Panel. https://ntrs.nasa.gov/citations/19800009729
• Gülhan, Ali, Florian Klingenberg, Sebastian Willems, et al. 2024. “Long Duration Hypersonic Flight Experiment ATHEAt.” In IAF Space Transportation Solutions and Innovations Symposium. International Astronautical Federation (IAF). https://doi.org/10.52202/078373-0051
• Guo, Yaobin, Xuejian Wang, and Binjiang Zhang. 1988. Experiment Investigation on Longitudinal Characteristics of the Forward Swept Wing. Defense Technical Information Center. https://doi.org/10.21236/ada191553
• Guoling, Sun, and Zhou Ji. 2014. Application Status of C/C Composites for Thermal Protection System in Re-Entry Spacecraft. Wiley. https://doi.org/10.1002/9781118932995.ch50
• Gupta, Manhar. n.d. “Energy Deposition for Hypersonic Flight Control.” PhD diss., The University of Queensland. https://doi.org/10.14264/923d57d
• Gupta, S. 1990. “Aerodynamic Characteristics of Forward Sweep.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3041. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3041
• Gupta, Kajal, T. Doyle, and E. Hahn. 2005. “AE/Flutter Simulation and Flight Test Correlation of the F/A-18 Active Aeroelastic Wing (AAW).” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-233
• Gupta, N. K., and W. E. Hall Jr. 1975. Input Design for Identification of Aircraft Stability and Control Derivatives. NASA-CR-2493. NASA. https://ntrs.nasa.gov/citations/19750009298
• Gupta, N., and K. Iliff. 1982. “Identification of Aerodynamic Indicial Functions Using Flight Data.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1375
• Gupta, K. K., S. F. Lung, and A. H. Ibrahim. 2015. “Numerical CFD Simulation and Test Correlation in a Flight Project Environment.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20160000559
• Gupta, N. K., R. K. Mehra, and W. E. Hall. 1976. “Application of Optimal Input Synthesis to Aircraft Parameter Identification.” Journal of Dynamic Systems, Measurement, and Control 98 (2): 139–45. https://doi.org/10.1115/1.3427000
• Gupta, Roop, and Ann Simmonds. 1988. “Stagnation Flow Field Analysis for an Aeroassist Flight Experiment Vehicle.” In 23rd Thermophysics, Plasmadynamics and Lasers Conference. AIAA 1988-2613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2613
• Gur, Ohad, Manav Bhatia, Joseph Schetz, William Mason, Rakesh Kapania, and Dimitri Mavris. 2009. “Multidisciplinary Design Optimization of a Truss Braced Wing Aircraft.” In 9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO). AIAA 2009-7114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7114
• Gur, Ohad, Joseph Schetz, and William Mason. 2010a. “Aerodynamic Considerations in the Design of Truss-Braced Wing Aircraft.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4813
• Gusarov, A. A., and V. A. Levin. 1981. “Three-Dimensional Shape of a Body of Minimum Drag in a Hypersonic Gas Stream.” Fluid Dynamics 16 (6): 881–85. https://doi.org/10.1007/bf01089717
• Gustafson, F. B. 1956. “A History of NACA Research on Rotating-Wing Aircraft.” Journal of the American Helicopter Society 1 (1): 16–26. https://doi.org/10.4050/jahs.1.1.16
• Gustafson, F. B. 1970a. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. I. NASA. https://ntrs.nasa.gov/citations/19700068735
• Gustafson, F. B. 1970b. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. II. NASA. https://ntrs.nasa.gov/citations/19700068736
• Gustafson, F. B. 1970c. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. III. NASA. https://ntrs.nasa.gov/citations/19700068737
• Gustafson, F. B. 1970d. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. III Cont’d. NASA. https://ntrs.nasa.gov/citations/19700068740
• Gustafson, F. B. 1970e. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. IV. NASA. https://ntrs.nasa.gov/citations/19710030680
• Gustafson, F. B. 1970f. History of NACA/NASA Rotating-Wing Aircraft Research, 1915-1970. IV Cont’d. NASA. https://ntrs.nasa.gov/citations/19710034474
• Gustafson, F. B., and Alfred Gessow. 1947. Effect of Blade Stalling on the Efficiency of a Helicopter Rotor as Measured in Flight. NACA-TN-1250. NASA. https://ntrs.nasa.gov/citations/19930082030
• Guy, Joshua Earl. n.d. “Design of a Re-Entry Experiment to Measure Aeroshell Heating Rates.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2018.302
• Guy, Yair, Thomas McLaughlin, and Julie Morrow. 2001. “Blunt Body Wave Drag Reduction by Means of a Standoff Spike.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-888. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-888
• Ha, C. 1990. “Reconfigurable Aircraft Flight Control System via Robust Direct Adaptive Control.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3226. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3226
• Ha, Tae H., Keunseok Lee, and John T. Hwang. 2020. “Large-Scale Multidisciplinary Optimization under Uncertainty for Electric Vertical Takeoff and Landing Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-0904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0904
• Ha, Jae-Seok, Chan-Yik Park, and Sang-Yong Kim. 2017. “Structural Health Monitoring of a Military Aircraft Using an Analog and Fiber Optic Sensor-Based Data Acquisition System for Structural Life Management.” In Structural Health Monitoring 2017. DEStech Publications, Inc. https://doi.org/10.12783/shm2017/13859
• Haans, Wouter, Hester Bijl, Marc Gerritsma, and Bas Oudheusden. 2004. “Small Scale Flow Phenomena of Hole-Suction Type Laminar Flow Control Sailplanes.” In 2nd AIAA Flow Control Conference. AIAA 2004-2312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2312
• Haase, W., H. Åslund, M. Kuntz, and F. Menter. n.d. “The TUM Forward-Swept Wing Generic Aircraft.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-39507-2_34
• Haber, J. 1993. “Cumulative Sonic Boom Damage to Plaster.” In 15th Aeroacoustics Conference. AIAA 1993-4446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4446
• Haberland, Wolfgang. 1980. “An Experimental Aircraft to Test New Technologies.” Aircraft Engineering and Aerospace Technology 52 (9): 25–27. https://doi.org/10.1108/eb035665
• Hackenberg, Davis L., and Wayne Hicks. 2011. “Orion Pad Abort 1 Flight Test: Ground and Flight Operations.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110010950
• Hadaller, O. J., J. E. Schmidt, A. M. Momenthy, and P. E. Johnson. 1980. “Impact of Changing Fuel Characteristics on Supersonic Cruise Airplane.” In NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2. https://ntrs.nasa.gov/citations/19810009495
• Hader, Christoph, and Hermann F. Fasel. 2021. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Straight Cone at Mach 7.” In AIAA Aviation 2021 Forum. AIAA 2021-2865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2865
• Hader, Christoph, and Hermann F. Fasel. 2024. “Numerical Investigation of Hypersonic Boundary-Layer Transition for an Ogive Geometry.” In AIAA SCITECH 2024 Forum. AIAA 2024-1569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1569
• Hader, Christoph, Madlen Leinemann, and Hermann F. Fasel. 2020. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Slender Cone.” In AIAA Aviation 2020 Forum. AIAA 2020-2993. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2993
• Haderlie, Jacob, and William Crossley. 2009. “A Parametric Approach to Supercritical Airfoil Design Optimization.” In 9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO). AIAA 2009-6950. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6950
• Haefeli, R. 1969. “Sonic Boom Propagation from Maneuvering Aircraft.” In 6th Annual Meeting and Technical Display. AIAA 1969-1134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-1134
• Haering, Edward, Larry Cliatt, Kenneth Plotkin, Domenic Maglieri, Michael Delaney, and Jacob Brown. 2013. “SCAMP: Rapid Focused Sonic Boom Waypoint Flight Planning Methods, Execution, and Results.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-932
• Haering, Ed, and Ken Plotkin. 2013. Display Provides Pilots with Real-Time Sonic-Boom Information. DRC-008-001. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20130011240
• Haering, Edward A., Jr. 1993. Calibrating Airplane Instrumentation to Measure Winds. ARC-12846. Dryden Flight Research Facility. https://ntrs.nasa.gov/citations/19930000084
• Haering, Edward A., Jr., L. J. Ehernberger, and Stephen A. Whitmore. 1995. “Preliminary Airborne Measurements for the SR-71 Sonic Boom Propagation Experiment.” In NASA High Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/19960002619
• Haering, Edward A., Jr., and James E. Murray. 2004. Shaped Sonic Boom Demonstration/Experiment Airborne Data. No Number:. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070023459
• Hafez, M., E. Murman, and J. South. 1978. “Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential Equation.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1148
• Haftka, Raphael T., Bernard Grossman, Pi-Jen Kao, David M. Polen, and Jaroslaw Sobieszczanski-Sobieski. 1989. “Integrated Aerodynamic-Structural Design of a Forward-Swept Transport Wing.” In Recent Advances in Multidisciplinary Analysis and Optimization, Part 1. https://ntrs.nasa.gov/citations/19890015797
• Hagenmaier, Mark A., John Boles, and Ryan T. Milligan. 2013. Scramjet Research with Flight-Like Inflow Conditions. Defense Technical Information Center. https://doi.org/10.21236/ada589252
• Haglund, George. 1991. “HSCT Designs for Reduced Sonic Boom.” In Aircraft Design and Operations Meeting. AIAA 1991-3103. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3103
• Haglund, G. T., and E. J. Kane. 1973. Flight Test Measurements and Analysis of Sonic Boom Phenomena near the Shock Wave Extremity. NASA-CR-2167. NASA. https://ntrs.nasa.gov/citations/19730009295
• Haglund, G., and E. Kane. 1974b. “Flight Test Measurements and Analysis of Sonic Boom Phenomena near the Shock Wave Extremity.” In 12th Aerospace Sciences Meeting. AIAA 1974-62. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-62
• Hagopian, Jeff. 2002. “2nd Generation Reusable Launch Vehicle-Concepts for Flight Operations.” In SpaceOps 2002 Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-t3-55
• Hall, J. L. 2002. “An Overview of the Aerocapture Flight Test Experiment (AFTE).” In AIAA Atmosphere Flight Mechanics Conference and Exhibit. https://ntrs.nasa.gov/citations/20060029898
• Hall, R. M., D. W. Banks, David F. Fisher, et al. 1994. “High Alpha Technology Program (HATP) Ground Test to Flight Comparisons.” In Fourth High Alpha Conference: Volume 1. https://ntrs.nasa.gov/citations/19950007816
• Hall, J. R., R. N. Hopko, and R. O. Piland. 1953. Drag Measurements at Low Lift of a Four- Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conductive to Low Transonic Drag Rise. NACA-RM-L53E29. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19650003113
• Hall, G. W., and R. K. Merrill. 1983. Flight Testing the Rotor Systems Research Aircraft (RSRA). NASA-TM-85852. NASA. https://ntrs.nasa.gov/citations/19840005109
• Hall, D., and D. Nowlan. 1977. “Aerodynamics of Ballistic Re-Entry Vehicles with Asymmetric Nosetips.” In 10th Fluid and Plasmadynamics Conference. AIAA 1977-701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-701
• Hall, Ian A., and Jonathan Poggie. 2019. “Simulation of Unstart in Hypersonic Flow with a Dual-Mode Scramjet Model.” In AIAA Scitech 2019 Forum. AIAA 2019-0946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0946
• Hall, W. E., Jr., N. K. Gupta, and R. S. Hansen. 1978. Rotorcraft System Identification Techniques for Handling Qualities and Stability and Control Evaluation. AHS 78-30. Systems Control, Inc. https://ntrs.nasa.gov/citations/19790034143
• Hallion, R. P. 1984. On the Frontier: Flight Research at Dryden 1946-1981. NASA-SP-4303. NASA. https://ntrs.nasa.gov/citations/19850009625
• Hallion, Richard P. 1991. “X-15: The Perspective of History.” In Proceedings of the X-15 First Flight 30th Anniversary Celebration. https://ntrs.nasa.gov/citations/19910010761
• Ham, Johnnie A., Charles K. Gardner, and Mark B. Tischler. 1993. “Flight Testing and Frequency Domain Analysis for Rotorcraft Handling Qualities Characteristics.” In Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors. https://ntrs.nasa.gov/citations/19940008851
• Ham, Changho, Wiedae Kim, and Seungmin Oh. 1994. “Active Flutter Suppression of Composite Plate with Piezoelectric Actuators.” In Adaptive Structures Forum. AIAA 1994-1745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1745
• Hamada, Said, and Claudia P. Moreno. 2018. “Development of an Unmanned Aerial Vehicle (UAV) Research Platform for Flutter Analysis.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0021
• Hamer, Harold A., and Alton P. Mayo. 1953. Time-History Data of Maneuvers Performed by a Republic F84G Airplane during Squadron Operational Training. NACA-RM-L53C27. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019469
• Hamilton, H. H., II, and K. J. Weilmuenster. 1986. Calculation of Convective Heating on Proposed Aeroassist Flight Experiment Vehicle. AIAA PAPER 86-1308. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19860055175
• Hamory, Philip, and James Murray. 1992. “Flight Experience with Lightweight, Low-Power Miniaturized Instrumentation Systems.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4111
• Hamory, Philip J., and James E. Murray. 1993. “Flight Experience with Lightweight, Low-Power Miniaturized Instrumentation Systems.” In AIAA 6th Biennial Flight Test Conference. https://ntrs.nasa.gov/citations/19930013913
• Hang, Richard. 2015. “Armstrong Flight Research Center Flight Test Capabilities and Opportunities for the Applications of Wireless Data Acquisition Systems.” In Future of Instrumentation and Internet Workshop 2015 (FIIW): Passive Wireless Sensor Technologies (PWST). https://ntrs.nasa.gov/citations/20150008345
• Hang, Richard. 2017. “Wireless Instrumentation Systems for Flight Testing at NASA AFRC.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20170009876
• Hank, Joseph, James Murphy, and Richard Mutzman. 2008. “The X-51A Scramjet Engine Flight Demonstration Program.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2540
• Hanke, Dietrich. 2003. “Flight Test Evaluation and Data Analysis of Rate Limiting Induced PIO’s.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5317. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5317
• Hannum, Ned, and Frank Berkopec. 1989. “Fueling the National Aero-Space Plane with Slush Hydrogen.” In National Aerospace Plane Conference. AIAA 1989-5014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5014
• Hansen, Jennifer L., James E. Murray, and Norma V. Campos. 2004. The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20040085352
• Hansen, Jennifer L., James E. Murray, and Norma V. Campos. 2005. The NASA Dryden Flight Test Approach to an Aerial Refueling System. NASA/TM-2005-212859. NASA. https://ntrs.nasa.gov/citations/20050071533
• Hansman, R., Jr., and Anthony Craig. 1987. “Comparative Low Reynolds Number Tests of NACA 64-210, NACA 0012, andWortmann FX67-K170 Airfoils in Heavy Rain.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-259
• Hansmann, Philipp, and Eike Stumpf. 2025. “Blended Wing Body Design in UNICADO.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-7011252/v1
• Hanson, P. W. 1973. Evaluation of an Aeroelastic Model Technique for Predicting Airplane Buffet Loads. NASA-TN-D-7066. NASA. https://ntrs.nasa.gov/citations/19730008178
• Hanson, D. 1989. “Sound Power Spectrum and Wave Drag of a Propeller in Flight.” In 12th Aeroacoustic Conference. AIAA 1989-1081. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1081
• Hanson, R. K. 1993. “Laser-Based Diagnostics for Hypersonic Flows.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_16
• Hanson, Curt. 2012. “Multi-Vehicle Cooperative Control Research NASA Dryden Flight Research Center 1998: 2012.” In University of Southern California Multi-Vehicle Cooperative Control Lecture. https://ntrs.nasa.gov/citations/20120011977
• Hanson, Curt. 2014. “Multi-Vehicle Cooperative Control Research at the NASA Armstrong Flight Research Center, 2000-2014.” In NATO AVT - 212 Cooperative Technology Demonstration (CDT). https://ntrs.nasa.gov/citations/20140017044
• Hanson, Curtis E., Jack Ryan, Michael J. Allen, and Steven R. Jacobson. 2002. An Overview of Flight Test Results for a Formation Flight Autopilot. NASA/TM-2002-210729. NASA. https://ntrs.nasa.gov/citations/20030005820
• Hao, Qiao, Sun Peng, and Li Xinguo. 2017. “United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2108
• Hao, Xuan, Cheng Su, and Jiajian Zhou. 2016b. “The Research of Supersonic Aircraft Low Sonic Boom Configuration Design and Optimizations.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-4049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4049
• Hargraves, Charles R. 1961. An Analytical Study of the Longitudinal Dynamics of a Tilt-Wing VTOL. Defense Technical Information Center. https://doi.org/10.21236/ad0268350
• Harle, Vilho. 1979. “Convergent vs. Conflicting Interests in Processes of Armaments Acquisition: A Case Study of Two Finnish Decisions on the Procurement of Military Aircraft.” Cooperation and Conflict 14 (1): 21–33. https://doi.org/10.1177/001083677901400103
• Harney, Donald J. 1963. Chemical Kinetic Regimes of Hypersonic Flight Simulation. Defense Technical Information Center. https://doi.org/10.21236/ad0295147
• Harney, Ronald J. 2005. Chapter 8: Preparation of the Flight Test Plan. RTO-AG-300-V14. Naval Air Warfare Center Aircraft Division. https://ntrs.nasa.gov/citations/20050209993
• Harney, P., W. Clifton, and D. A. Johnson. 1983. Instrumentation and Data Processing for AFTI/F-16 Flight Testing. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19840033903
• Harney, P. F., and R. B. Richardson. 1968. “Flight and Laboratory Testing of a Double Sideband FM Telemetry System.” In INTERNATIONAL TELEMETERING CONFERENCE. https://ntrs.nasa.gov/citations/19690041143
• Harper, Paul W. 1953. Wing and Fuselage Loads Measured in Flight on the North American B-45 and F-82 Airplanes. NACA-RM-L52L09. NASA. https://ntrs.nasa.gov/citations/19930087408
• Harpold, D. N., and C. A. Reber. 1966. Flight Instrumentation Research. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/19660026639
• Harris, C. D. 1972. Wind-Tunnel Measurements of Aerodynamic Load Distribution on an NASA Supercritical-Wing Research Airplane Configuration. NASA-TM-X-2469. NASA. https://ntrs.nasa.gov/citations/19780016136
• Harris, Elwyn. 1993. “The National Aerospace Plane: Cost Considerations for the Follow-on Vehicle.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5012
• Harris, Chuck. 2004. “Accelerated Flutter Testing: A Possible Technique to Expedite Flutter Testing for New Aircraft.” In USAF Developmental Test and Evaluation Summit. AIAA 2004-6822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6822
• Harris, Robert, and R. Cuthbertson. 1987. “UDF/727 Flight Test Program.” In 23rd Joint Propulsion Conference. AIAA 1987-1733. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1733
• Harris, D., J. Gautrey, K. Payne, and R. Bailey. 2000. “The Cranfield Aircraft Handling Qualities Rating Scale: A Multidimensional Approach to the Assessment of Aircraft Handling Qualities.” Aeronautical Journal 104 (1034): 191–98. https://doi.org/10.1017/s0001924000028098
• Harris, Willard, and Willard Harris. 1997. “X-36 Tailless Agility Aircraft Subsystems Integration.” In 1997 World Aviation Congress. AIAA 1997-5505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-5505
• Harris, James, Dennis Hines, and Donald Rhea. 1994. “Migrating Traditional Post Test Data Analysis into Real Time Flight Data Analysis.” In Biennial Flight Test Conference. AIAA 1994-2149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2149
• Harrison, Glenn W. 2021. “Experimental Design and Bayesian Interpretation.” In A Modern Guide to Philosophy of Economics. Edward Elgar Publishing. https://doi.org/10.4337/9781788974462.00009
• Harrison, Sean, Ryan A. Darragh, Peter E. Hamlington, Mehdi Ghoreyshi, and Andrew J. Lofthouse. 2016. “Canard-Wing Interference Effects on the Flight Characteristics of a Transonic Passenger Aircraft.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-4179. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4179
• Harrison, Neal A., Gregory M. Gatlin, Sally A. Viken, et al. 2020. “Development of an Efficient M=0.80 Transonic Truss-Braced Wing Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-0011. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0011
• Harrison, D. R., and W. K. Lockman. 1968. “Heat-Transfer Telemetry from Free-Flight Models in Wind Tunnels. II.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19680044408
• Harrison, R. G., and W. J. Marko. 1968. “Heat-Transfer Telemetry from Free-Flight Models in Wind Tunnels. I.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19680044407
• Harsha, Philip, and Barry Waldman. 1989. “The NASP Challenge: Testing for Validation.” In National Aerospace Plane Conference. AIAA 1989-5005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5005
• Hart, J. 1984. “MAGNA Analysis of the T-38 Aircraft Student Canopy: Response to in-Flight Aerodynamic Pressure Loads.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2390
• Hart, Ronald. 1992. “B-2 Flight Test Program: An Update.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4118
• Hart, Pierce, and Sven Schmitz. 2022. “A Partial Pressure Field for Airfoil Wave Drag.” In AIAA SCITECH 2022 Forum. AIAA 2022-2482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2482
• Hartley, K. 1965. “The Learning Curve and Its Application to the Aircraft Industry.” Journal of Industrial Economics 13 (2): 122. https://doi.org/10.2307/2097667
• Hartman, Edwin P. 1970. Adventures in Research: A History of Ames Research Center, 1940-1965. NASA-SP-4302. NASA. https://ntrs.nasa.gov/citations/19700032163
• Hartman, David. 2019. “Identification of Hazardous Flight Conditions to Establish a Safe Flight Envelope for Autonomous Multirotor Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-1292. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1292
• Hartmann, G., G. Stein, and B. Powers. 1979. Flight Test Experience with an Adaptive Control System Using a Maximum Likelihood Parameter Estimation Technique. AIAA PAPER 79-1702. Honeywell, Inc. https://ntrs.nasa.gov/citations/19790061344
• Hartwich, Peter, Billy Burroughs, James Herzberg, and Curt Wiler. 2003. “Design Development Strategies and Technology Integration for Supersonic Aircraft of Low Perceived Sonic Boom.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-556
• Hartwig, Louis W., and Walter G. O. Sonneborn. 1971. “Results of High-Speed Flight Research with the High Performance UH-1 Compound Helicopter.” In Proceedings of the Vertical Flight Society Forum 27 - Washington, D.C. 1971. The Vertical Flight Society. https://doi.org/10.4050/vfs-f27-034
• Harvey, W., and P. Bobbitt. 1981. “Some Anomalies between Wind Tunnel and Flight Transition Results.” In 14th Fluid and Plasma Dynamics Conference. AIAA 1981-1225. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1225
• Harvey, W., and J. Pride. 1982. “The NASA Langley Laminar Flow Control Airfoil Experiment.” In 12th Aerodynamic Testing Conference. AIAA 1982-567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-567
• Harvey, Walter B., and Charles M. Ryan. 2012. A Quantitative Analysis of the Benefits of Prototyping Fixed-Wing Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada563152
• Hasan, Inamul, R. Mukesh, P. Radha Krishnan, R. Srinath, and R. B. Dhanya Prakash. 2022. “Forward Flight Performance Analysis of Supercritical Airfoil in Helicopter Main Rotor.” Intelligent Automation & Soft Computing 33 (1): 567–84. https://doi.org/10.32604/iasc.2022.023252
• Hasbrook, A. Howard. 1957. “Designing for Survival in VTOL Aircraft.” In Proceedings of the Vertical Flight Society Forum 13 - Washington, D.C. 1957. The Vertical Flight Society. https://doi.org/10.4050/vfs-f13-006
• Hasegawa, Susumu. 2025. “Comparison of Numerical Results with Wind Tunnel Aerodynamic Data of Flight Vehicle for Hypersonic Flight.” In AIAA SCITECH 2025 Forum. AIAA 2025-1335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1335
• Hasegawa, Yasumichi, Kenjiro Inagaki, Noboru Kobiki, et al. 1999. “Correlation between Analyses and Wind Tunnel Test Results:: What ATIC Has Done So Far.-.” In Proceedings of the Vertical Flight Society Forum 55 - Montreal, Canada 1999. The Vertical Flight Society. https://doi.org/10.4050/vfs-f55-00036
• Hashii, Wendy N., and Randolph C. Thompson. 2018. “Best Practices for Training the Structures Flight Test Engineer.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20180004483
• Hashimoto, Atsushi, Masataka Kohzai, Takashi Aoyama, and Mitsuhiro Murayama. 2011. “Wall Interference Analysis of Transonic Wind Tunnel with Porous Wall Model.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3017
• Hassan, Ahmed M., and Haitham E. Taha. 2016. “Geometric Nonlinear Controllability Analysis for Airplane Flight Dynamics.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0079. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0079
• Hassell, J. L., Jr. 1960. Investigation of the Low-Subsonic Stability and Control Characteristics of a 1 3-SCALE Free-Flying Model of a Lifting-Body Reentry Configuration. NASA-TM-X-297. NASA. https://ntrs.nasa.gov/citations/19630004024
• Hastings, E., Jr., J. Schoenster, C. Obara, and S. Dodbele. 1986. “Flight Research on Natural Laminar Flow Nacelles: A Progress Report.” In 22nd Joint Propulsion Conference. AIAA 1986-1629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1629
• Haus, Patrick J. 2023. “Ground and Flight Testing the New VISTA Simulation System (VSS).” In AIAA SCITECH 2023 Forum. AIAA 2023-1927. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1927
• Havey, C., and Margaret Kline. 1989. “Propulsion Optimization for Conceptual STOVL Aircraft.” In Aircraft Design and Operations Meeting. AIAA 1989-2020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2020
• Hawkins, Richard, and Arthur Dilley. 1992. “CFD Comparisons with Wind Tunnel and Flight Data for the X-15.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5047. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5047
• Hayes, Wallace D. 1969. “Review of Sonic Boom Theory.” In Aerodynamic Noise. University of Toronto Press. https://doi.org/10.3138/9781487582869-019
• Hayes, Julie, W. Horne, Stephen Jaeger, and Paul Soderman. 1999. “Measurement of Reynolds Number Effect on Airframe Noise in the 12-Foot Pressure Wind Tunnel.” In 5th AIAA/CEAS Aeroacoustics Conference and Exhibit. AIAA 1999-1959. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1959
• Haynes, Robert, Harry Luzetsky, and Ellen Phifer. 2025. “Lightweight Low-Cost Multifunctional Thermoplastic Composite Airframe.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0162
• He, Xuzhao, and Jialing Le. 2017. “Design and Performances Analysis of the Integrated Curved Cone Waverider-Inlet.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2145
• He, Xuzhao, Jialing Le, and Si Qin. 2017. “Design and Analysis Osculating General Curved Cone Waverider.” Aircraft Engineering and Aerospace Technology 89 (6): 797–803. https://doi.org/10.1108/aeat-12-2014-0214
• He, Xuzhao, Jialing Le, and Yingchuan Wu. 2009. “Design of a Curved Cone Derived Waverider Forebody.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7423
• He, Jia, Pei Zuo, Hua Li, and Min Xu. 1992. “The Research of Reducing 3-D Low Supersonic Shock Wave Reflection Ina 2-D Transonic Flexible Walls Adaptive Wind Tunnel.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3924. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3924
• Head, Robert E. 1962. “A Comparison of Rotor Blade Loads Measured in Flight and on a Quarter-Scale Wind Tunnel Model.” Journal of the American Helicopter Society 7 (3): 28–35. https://doi.org/10.4050/jahs.7.28
• Head, C. 1981. “Air-to-Air Missiles: Flight Test in the 80’S.” In 1st Flight Test Conference. AIAA 1981-2506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2506
• Heaney, Patrick S., David J. Piatak, Oleg Goushcha, James M. Ramey, Francesco Soranna, and Martin K. Sekula. n.d. “Comparison of Wind-Tunnel and Flight Unsteady Pressure Stochastic Characteristics for the Space Launch System Artemis I Flight.” In 2024 AIAA Science and Technology Forum and Exposition (AIAA SciTech Forum). https://ntrs.nasa.gov/citations/20230017162
• Heaney, Patrick S., David J. Piatak, Oleg Goushcha, James M. Ramey, Francesco Soranna, and Martin K. Sekula. 2024. “Comparison of Wind-Tunnel and Flight Unsteady Pressure Stochastic Characteristics for the Space Launch System Artemis I Flight.” In AIAA SCITECH 2024 Forum. AIAA 2024-0019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0019
• Heaney, Patrick S., David J. Piatak, Martin K. Sekula, and Francesco Soranna. 2022. “Comparison of Wind-Tunnel and Flight Unsteady Pressure Environments for the Ares I-X Flight Test Vehicle.” In AIAA SCITECH 2022 Forum. AIAA 2022-2413. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2413
• “Heat-Shield Material Tests in a Simulated Jovian Entry Heating Environment.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0222.0244
• Heath, Christopher, John W. Slater, and Sriram K. Rallabhandi. 2016. “Inlet Trade Study for a Low Boom Aircraft Demonstrator.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-4050. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4050
• Hebbar, Sheshagiri, and John Sommers. 1990. “Wind Tunnel Studies of Support Strut Interference on a 3 Percent YF-17 Fighter Aircraft Model at High Angles of Attack.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3083
• Heberling, Brian. 2020. “Inlet Vortex Generator Design for the X-59 Low Boom Flight Demonstrator.” In AIAA Aviation 2020 Forum. AIAA 2020-2757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2757
• Heck, M., J. Findlay, and H. Compton. 1983. “Calibration of the Aerodynamic Coefficient Identification Package Measurements from the Shuttle Entry Flights Using Inertial Measurement Unit Data.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2100
• Hedlund, Eric, Craig Higgins, Charles Rozanski, Nancy Fehring, and Dave Krueger. 1990. “The New High Reynolds Number Mach 8 Capability in the NSWC Hypervelocity Wind Tunnel 9.” In 16th Aerodynamic Ground Testing Conference. AIAA 1990-1379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1379
• Hedlund, E., and W. Ragsdale. 1985. “Improvements in Low Reynolds Number Testing in the NSWC Hypervelocity Wind Tunnel No. 9.” In 23rd Aerospace Sciences Meeting. AIAA 1985-226. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-226
• Heeg, Jennifer, Charles V. Spain, James R. Florance, et al. 2005. “Experimental Results from the Active Aeroelastic Wing Wind Tunnel Test Program.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20050203672
• Hefner, Jerry N. 1992. “Laminar Flow Control: Introduction and Overview.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_1
• Heidersbach, Ross, Dhuree Seth, Matthew McCrink, Guy Gordon Biberstein, and Moti Karpel. 2024. “Flight-Test Flutter Margin Identification Using the Parametric Flutter Margin.” In AIAA SCITECH 2024 Forum. AIAA 2024-2439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2439
• Heidersbach, Ross, Dhuree Seth, Matthew McCrink, and Moti Karpel. 2023. “Safe Flutter Flight Testing of an Unmanned Aerial Vehicle Utilizing Parametric Flutter Margin.” In AIAA SCITECH 2023 Forum. AIAA 2023-2071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2071
• Heiss, S., A. Eberle, L. Fornasier, and W. Paul. 1992. “Application of the Euler Method EUFLEX to a Fighter-Type Airplane Configuration at Transonic Speed.” In 10th Applied Aerodynamics Conference. AIAA 1992-2620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2620
• Helffer, Emmanuel, Olivier Deille, Jocelyn Briand, and Osmin Delverdier. 2014. “Fast and Light Acoustic Flight Test Measurements in Aircraft.” In AIAA Flight Testing Conference. AIAA 2014-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2581
• “Helicopter Flight Parameter Identification Studies at the University of York.” 1987. Aircraft Engineering and Aerospace Technology 59 (4): 16–17. https://doi.org/10.1108/eb036427
• Hellbaum, R. F., and H. Douglas Garner. 1988. A Discussion of Some Proposed Measurement Techniques for Hypersonic Flight and Instrumentation Research Experiments. AIAA PAPER 88-4651A. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880064681
• Heller, M., G. Sachs, K. Gunnarsson, H. Frank, and D. Rylander. 1998. “Flight Dynamics and Robust Control of a Hypersonic Test Vehicle with Ramjet Propulsion.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1521. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1521
• Hellman, Barry, Anhtuan Ngo, and Jon Wallace. 2010. “Technical Challenges for an Integrated Reusable Booster System Flight Demonstrator.” In AIAA SPACE 2010 Conference & Exposition. AIAA 2010-8668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8668
• Hemmig, F., V. Venkayya, and F. Eastep. 1979. “Flutter Speed Degradation of Damaged, Optimized Flight Vehicles.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-795
• Hemsch, Michael J., and Eric L. Walker. 2011. “The Crucial Role of Error Correlation for Uncertainty Modeling of CFD-Based Aerodynamics Increments.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110002871
• Hendershot, K. 1969. “Applications of a Tube Wind Tunnel in Supersonic Testing.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-335
• Henderson, C. 1964. “X-22a V/stol Aircraft Research Capabilities.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-786
• Henderson, H. R., D. A. Hilton, V. Huckel, D. J. Maglieri, and N. J. McLeod. 1971. Measurements of Sonic Boom Signatures from Flights at Cutoff Mach Number. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710018905
• Henderson, Brenda S., and Dennis L. Huff. 2021. “A History of Jet Noise Research at the National Aeronautics and Space Administration.” Journal of the Acoustical Society of America 150 (2). https://ntrs.nasa.gov/citations/20210021068
• Henderson, Brenda, Lennart Hultgren, Devin Boyle, et al. 2022. “Learjet Flight Test Update.” In Spring 2022 NASA Acoustics Technical Working Group and UAM Noise Working Group Meetings. https://ntrs.nasa.gov/citations/20220005137
• Henderson, Campbell, James Thornton, and Alton Mayo. 1952. Time-History Data of Maneuvers Performed by an F-86A Airplane during Squadron Operational Training. NACA-RM-L52C19. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019265
• Henderson, A., Jr. 1967. “Boundary-Layer Transition on Sharp Cones at Hypersonic Mach Numbers.” In 5th Aerospace Sciences Meeting. AIAA 1967-130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-130
• Henke, R. 2001. “Airbus a 320 HLF Fin Flight Tests.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_4
• Henne, P. A., and R. M. Hicks. 1978. “Transonic Wing Analysis Using Advanced Computational Methods.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780036777
• Henry, M., H. Wolf, and Paul Siemers III. 1988. “An Evaluation of Shuttle Entry Air Data System (SEADS) Flight Pressures: Comparisons with Wind Tunnel and Theoretical Predictions.” In 15th Aerodynamic Testing Conference. AIAA 1988-2052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2052
• Hensel, R. W. 1964. “A Survey of Recent Developments in Wind-Tunnel Testing Techniques at Transonic and Supersonic Speeds.” In Aerodynamic Testing Conference. AIAA 1964-1109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-1109
• Hensley, Douglas. 1994. “Flight Test Data Modelling and Compression by Fuzzy Extracted Topology Technique.” In Flight Simualtion Technologies Conference. AIAA 1994-3422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3422
• Henwood, Bart, and Rod Huete. 2007. “Flight Test Hazard Planning near the Speed of Light.” In Society of Experimental Test Pilots. https://ntrs.nasa.gov/citations/20070021634
• Hepler, Leslie J., Gary L. Skinner, Gary A. Smith, and Paul R. Bonin. 1973. Engineering Flight Test: AH-1G Helicopter with Model 212 Tail Rotor. Part I. Load Survey. Defense Technical Information Center. https://doi.org/10.21236/ad0776359
• Heppe, R., and J. Hong. 1964. “The Double-Delta Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-602
• Herdy, Joseph R. 2025. “Hypersonic Synthetic Environment Test Tunnels (HySETT) Program for Propulsion Testing Initiatives Yielding Flight Similitude.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3680. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3680
• Herencia, J., Paul Weaver, and Mike Friswell. 2007. “Morphing Wing Design via Aeroelastic Tailoring.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-2214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2214
• Herkes, W., R. Olsen, and S. Uellenberg. 2006. “The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction Concepts.” In 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference). AIAA 2006-2720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-2720
• Hermann, Tobias. 2024. “Correlation for Wall-Temperature Oscillations in Unsteady Stagnation Point Convective Heating.” Preprint, . https://doi.org/10.2139/ssrn.5036799
• Hernandez, Francisco J., and Frank W. Burcham Jr. 1988. Flight Measured and Calculated Exhaust Jet Conditions for an F100 Engine in an F-15 Airplane. NASA-TM-100419. NASA. https://ntrs.nasa.gov/citations/19890004064
• Hernandez, Francisco J., David B. Signor, Michael E. Watts, Gloria K. Yamauchi, and Philip LeMasurier. 1993. “Flight Measurements of Blade-Vortex Interaction Noise Including Comparisons with Full-Scale Wind Tunnel Data.” In Proceedings of the Vertical Flight Society Forum 49 - St. Louis, MO 1993. The Vertical Flight Society. https://doi.org/10.4050/vfs-f49-1002
• Herrington, Russel M., Paul E. Shoemacher, Eugene P. Bartlett, and Everett W. Dunlap. 1966. Flight Test Engineering Handbook. Defense Technical Information Center. https://doi.org/10.21236/ad0636392
• Herrlinger, S. 1991. “Operational Flight Test of E-9A Aircraft Systems.” In Aircraft Design and Operations Meeting. AIAA 1991-3172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3172
• Herrmann, G., and S. Nemat-Nasser. 1966. “Bending-Torsional Flutter of a Swept Wing in a Highdensity, Low-Speed Flow.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-475
• Herron, Marissa. 2007. “Sonic Boom Assessment for the Crew Exploration Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6635
• Hertz, T. J., M. H. Shirk, R. H. Ricketts, and T. A. Weisshaar. 1982. “On the Track of Practical Forward-Swept Wings.” Astronautics and Aeronautics 20. https://ntrs.nasa.gov/citations/19820035536
• Hertzfeld, Henry. 2000. “Policy and Legal Considerations for a Commercial Reusable Launch Vehicle.” In Space 2000 Conference and Exposition. AIAA 2000-5113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5113
• Hertzler, E. K., and P. W. Phillips. 1983. “Flight Test Derived Heating Math Models for Critical Locations on the Orbiter during Reentry.” In NASA. Langley Research Center Shuttle Performance: Lessons Learned, Pt. 2. https://ntrs.nasa.gov/citations/19840002080
• Herzog, Nikolai, Andreas Reeh, Andreas Kümmel, and Christian Breitsamter. 2021. “Analysis of Distributed Electric Propulsion on Commuter Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-1199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1199
• Hess, R. 1981. “Analysis of Aircraft Longitudinal Handling Qualities.” In Guidance and Control Conference. AIAA 1981-1771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1771
• Hess, R. 1984. “Toward a Unifying Theory for Aircraft Handling Qualities.” In 22nd Aerospace Sciences Meeting. AIAA 1984-236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-236
• Hess, R. A. 1986a. Effects of Wing Modification on an Aircraft’s Aerodynamic Parameters as Determined from Flight Data. NASA-TM-87591. NASA. https://ntrs.nasa.gov/citations/19860012079
• Hess, R. 1986b. “Validation of a Fighter Aircraft Simulation Using High Angle-of-Attack Flight Test Data.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2681. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2681
• Hess, Ronald K., and Peter M. Flick. 2004. “Autonomous Flight Control Development on the Active Aeroelastic Wing Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2004-01-3116
• Hess, R., and R. Hess. 1997. “A Unified Theory for Aircraft Handling Qualities and Adverse Aircraft-Pilot Coupling.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-454
• Hessman, F. 1982. “High Angle of Attack Aerodynamic Characteristics for a Finless TVC Missile Configuration.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1337
• Heston, Daniel T., Ethan S. Beyak, Koen J. Groot, and Helen L. Reed. 2021. “Boundary-Layer Stability of a Slotted, Natural-Laminar-Flow Airfoil at Flight Conditions.” In AIAA Scitech 2021 Forum. AIAA 2021-0845. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0845
• Heyong, Xu, and Zhengyin Ye. 2011. “Investigation of a Flutter Exciter for Aircraft Flight Testing Using Unstructured Overset Grids.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6670
• Hickman, R., and J. Kyser. 1972. “Refinements in High-Reynolds-Number Shock-Tunnel Technology.” In 7th Aerodynamic Testing Conference. AIAA 1972-996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-996
• Hicks, John W. 1992. “Development of a Hydrogen External Burning Flight Test Experiment on the NASA Dryden SR-71A Aircraft.” In SAE. https://ntrs.nasa.gov/citations/19930030641
• Hicks, John W. 1993. “Flight Testing of Airbreathing Hypersonic Vehicles.” In Space Course 1993. https://ntrs.nasa.gov/citations/19940011280
• Hicks, John, James Cooper Jr., and Walter Sefic. 1987b. “Flight Test Techniques for the X-29A Aircraft.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-82. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-82
• Hicks, John W., and Thomas Huckabine. 1989. Preliminary Flight-Determined Subsonic Lift and Drag Characteristics of the X-29A Forward-Swept-Wing Airplane. NASA-TM-100409. NASA. https://ntrs.nasa.gov/citations/19910019863
• Hicks, John W., Jan Kania, Robert Pearce, and Glen Mills. 1987a. Challenges in Modeling the X-29A Flight Test Performance. AIAA PAPER 87-0081. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19870035128
• Hicks, John, and Neil Matheny. 1987. “Preliminary Flight Assessment of the X-29A Advanced Technology Demonstrator.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2949
• Hicks, R. M., J. P. Mendoza, and F. Garcia Jr. 1972. A Wind Tunnel Flight Correlation of Apollo 15 Sonic Boom. NASA-TM-X-62111. NASA. https://ntrs.nasa.gov/citations/19730004289
• Hicks, John, and Bryan Moulton. 1988. “Effects of Maneuver Dynamics on Drag Polars of the X-29A Forward-Swept-Wing Aircraft with Automatic Wing Camber Control.” In 4th Flight Test Conference. AIAA 1988-2144. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2144
• Hicks, John W., and Kevin L. Petersen. 1988. Real-Time Flight Test Analysis and Display Techniques for the X-29A Aircraft. NASA-TM-101692. NASA. https://ntrs.nasa.gov/citations/19890004053
• Hicks, John W., and Kevin L. Petersen. 1989. “Real-Time Flight Test Analysis and Display Techniques for the X-29A Aircraft.” In AGARD, Flight Test Techniques. https://ntrs.nasa.gov/citations/19900001550
• Hicks, John W., and Gary Trippensee. 1997. “NASA Hypersonic X-Plane Flight Development of Technologies and Capabilities for the 21st Century Access to Space.” In Future Aerospace Technology in the Service of the Alliance. https://ntrs.nasa.gov/citations/19980018696
• Hicks, Raymond M., Garret N. Vanderplaats, Earll M. Murman, and Rosa R. King. 1976. “Airfoil Section Drag Reduction at Transonic Speeds by Numerical Optimization.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/760477
• Hieser, Gerald, Louis Kudlacik, and W. H. Gray. 1956. A Transonic Wind-Tunnel Investigation of a Seaplane Configuration Having a 40 Deg Sweptback Wing, TED No. NACA DE 387. Rept-4960. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029376
• Hieser, Gerald, and Charles F. Reid. 1954. A Transonic Wind-Tunnel Investigation of the Longitudinal Aerodynamic Characteristics of a Model of the Lockheed XF-104 Airplane. NACA-RM-SL54K19a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023314
• Higashino, Shin-Ichiro, and Akira Sakurai. 2003. “A UAV Flight-Experiment System for the Estimation of Aerodynamic Characteristics.” In 2nd AIAA “Unmanned Unlimited” Conf. and Workshop & Exhibit. AIAA 2003-6584. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6584
• Higgins, Allyn E., Samuel R. Schwartz, Harold C. Catey, and Robert F. Forsyth. 1968. Engineering Flight Test of the CH-47 (Chinook) Helicopter Integral Weight and Balance Systems (Ensure). Defense Technical Information Center. https://doi.org/10.21236/ad0832821
• Higgins, H., and H. Shomber. 1964. “The Effect of Variable Sweep on Supersonic Transport Handling Qualities.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-603. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-603
• “High-Altitude Long-Endurance (HALE) Sensor Aircraft.” 2026. In The Conceptual Design Process Illustrated. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624107719.0007.0050
• “High-Speed Flight.” 1996. In Thermal Structures for Aerospace Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862540.0001.0026
• “High-Speed Flight.” 2009. In Flight Physics. Springer Netherlands. https://doi.org/10.1007/978-1-4020-8664-9_9
• High-Speed Flight. 2010. Wiley. https://doi.org/10.1002/9780470710944.ch15
• “High-Speed Flight and Its Aerodynamic and Gasdynamic Challenges.” 2010. In German Development of the Swept Wing 1935–1945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867552.0069.0278
• “High-Speed Flight Thermal Management.” 1996. In Developments In High-Speed Vehicle Propulsion Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866401.0517.0579
• “High-Supersonic/Hypersonic Flows.” 2012. In Aerodynamic Principles of Flight Vehicles. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600869174.0221.0278
• Higham, Robin. 1963. “Aeronautical History — Some Offbeat British Archives.” American Archivist 26 (1): 63–65. https://doi.org/10.17723/aarc.26.1.k3451v612562x874
• Hilbert, K., J. Lebacqz, and W. Hindson. 1986. “Flight Investigation of a Multivariable Model-Following Control System for Rotorcraft.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9779
• Hildebrand, R. 1979. “The Air Launched Cruise Missile Flight Test Status.” In Aircraft Systems and Technology Meeting. AIAA 1979-1787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1787
• Hildreth, Bruce, and Roger Burton. 1983. “Coupling Simulation. System Identification and Flight Testing in an Aft Center of Gravity Flying Qualities Investigation.” In 2nd Flight Testing Conference. AIAA 1983-2718. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2718
• Hill, Jonathan L., and Matthew P. Borg. 2024. “Hypersonic Boundary Layer Transition Visualized via CO2-Enhanced Rayleigh Scattering.” In AIAA SCITECH 2024 Forum. AIAA 2024-0940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0940
• Hill, Michael A., and Edward A. Haering. 2017. “Flow Visualization of Aircraft in Flight by Means of Background Oriented Schlieren Using Celestial Objects.” In 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2017-3553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3553
• Hill, E., and Mike Huhlein. 1993. “Endo LEAP Flight Test Planning.” In Annual Interceptor Technology Conference. AIAA 1993-2701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2701
• Hill, Eugene, and Thomas Zierten. 1991. “Flight and Wind Tunnel Tests of the Aerodynamic Effects of Aircraft Ground Deicing/anti-Icing Fluids.” In 29th Aerospace Sciences Meeting. AIAA 1991-762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-762
• Hillaker, H. 1983a. “The F-16: A Technology Demonstrator, a Prototype, and a Flight Demonstrator.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1063
• Hillaker, H. 1983b. “F-16XL Flight Test Program Overview.” In 2nd Flight Testing Conference. AIAA 1983-2730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2730
• Hiller, Brett R., Richard L. Campbell, and Michelle N. Banchy. n.d.-a. “Cruise Slotted Wing Design with Natural Laminar Flow for Transonic Commercial Transport Aircraft.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20240014322
• Hiller, Brett R., Richard L. Campbell, and Michelle N. Banchy. n.d.-c. “Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft Using CDISC.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20230016544
• Hiller, Brett R., Richard L. Campbell, Michelle N. Lynde, and Taylor Kate Boyett. n.d.-b. “Design Exploration of a Transonic Cruise Slotted Airfoil.” In AIAA Aviation 2021. https://ntrs.nasa.gov/citations/20210016792
• Hillje, E., and R. Nelson. 1981. “Postflight Analysis of the Space Shuttle Ascent Air Data System.” In 1st Flight Test Conference. AIAA 1981-2457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2457
• Hillje, E., and D. Tymms. 1978. “Wind Tunnel and Flight Calibration of the Shuttle Orbiter Air Data System.” In 10th Aerodynamic Testing Conference. AIAA 1978-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-792
• Hilton, Harry. 2012. “Designer Materials for Controlling Thermally and Aerodynamically Excited Viscoelastic Lifting Surface Flutter and Structural Failures.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4952. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4952
• Hilton, D. A., and D. J. Maglieri. 1965. Significance of the Atmosphere and Aircraft Operations on Sonic-Boom Exposures. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19650021525
• Hinada, Motoki, Yoshifumi Inatani, Takashi Nakajima, and Masahisa Honda. 1991. “Parachute Deployment Experiment in Transonic and Supersonic Wind Tunnels.” In 11th Aerodynamic Decelerator Systems Technology Conference. AIAA 1991-859. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-859
• Hinchliffe, Benjamin L., and Ning Qin. 2016. “Using Surface Sensitivity from Mesh Adjoint Solution for Transonic Wing Drag Reduction.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0560
• Hinds, J., and O. Shames. 1975. Flight Test Evaluation of AVOID I (Avionic Observation of Intruder Danger) Collision Avoidance System. Defense Technical Information Center. https://doi.org/10.21236/ada011449
• Hines, R. 1977. “Advanced Supersonic Transport Propulsion Requirements.” In 13th Propulsion Conference. AIAA 1977-831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-831
• Hines, R., and J. Sabatella. 1973. “Influence of Noise Constraints on Supersonic Transport Engine Design.” In 9th Propulsion Conference. AIAA 1973-1295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1295
• Hinton, Michael J., and Charles N. Eastlake. 1999. “The Construction and Flight Testing of a Scaled, Remotely Piloted, Flight Test Vehicle.” In 1999 Annual Conference Proceedings. ASEE Conferences. https://doi.org/10.18260/1-2–8119
• Hirschel, Ernst Heinrich, and Claus Weiland. 2009a. “Short Introduction to Flight Trajectories for Aerothermodynamicists.” In Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-89974-7_2
• Hirschel, Ernst Heinrich, and Claus Weiland. 2009b. “The Thermal State of a Hypersonic Vehicle Surface.” In Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-89974-7_9
• Hirsh, Norman B. 1965. Aircraft Design XV-9A Hot Cycle Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0621684
• Hirshorn, Steven, and Guy Kemmerly. 2018. An Investigation of Risk Management Approaches for NASA Piloted X-Plane Projects. HQ-E-DAA-TN60124. NASA Headquarters. https://ntrs.nasa.gov/citations/20190001253
• Hirshorn, Steven R., Tiffany L. Smith, Ian Boyd, Giovanni La Fontaine, Nam H. Nguyen, and Campbell Knobloch. 2024. X-Plane Knowledge Capture Workshop Summary Report. NASA/CP-20230008230. NASA. https://ntrs.nasa.gov/citations/20230008230
• Hiruma, Masaharu, Ryoichi Takase, Hideyuki Taguchi, and Takeshi Tsuchiya. 2020. “Integrated Design of Trajectory and Robust Control for Hypersonic Experimental Aircraft.” In 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2020-2413. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2413
• “History of Aircraft & Aviation.” 2022. In Introduction to Aerospace Flight Vehicles. Embry-Riddle Aeronautical University. https://doi.org/10.15394/eaglepub.2022.1066.n2
• History of Supersonic Transport Aircraft Development. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch1
• Hite, Walter A. 1940. “Engineering Experimental Aeroplanes: Designing Prototype Machines for Manufacturing Economy.” Aircraft Engineering and Aerospace Technology 12 (5): 153–56. https://doi.org/10.1108/eb030645
• Hitzel, Stephan M. 2015. “Free-Flight High AoA Flows Simulation at Sub- and Transonic Speeds: F-16XL (CAWAPI-3).” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2871. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2871
• Hoadley, Arthur. 1988. “Development of a University Engineering Flight Test Aircraft FAA Licensed under Normal Category.” In 4th Flight Test Conference. AIAA 1988-2205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2205
• Hobbs, Christopher, and Juliet Page. 2011. “PCBoom Model Prediction Comparisons with Flight Test Measurement Data.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-1277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1277
• Hodgdon, Kathleen, and Juliet Page. 2013. “Low Amplitude Sonic Boom Noise Exposure and Social Survey Design.” In Proceedings of Meetings on Acoustics. ASA. https://doi.org/10.1121/1.4799817
• Hodge, J., and D. Audley. 1983. “Aerothermodynamic Parameter Estimation from Space Shuttle Thermocouple Data during Transient Flight Test Maneuvers.” In 21st Aerospace Sciences Meeting. AIAA 1983-482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-482
• Hodge, Mark W., and John W. Kelley. 2006. The Hyper-X Antenna Radiation Pattern Tests and Radio Frequency System Redesign. DFRC-422. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090008546
• Hodge, K., and D. Meyer. 1963. “Inertial Navigator Flight-Testing Experience with the Lockheed F-104.” In Testing of Manned Flight Systems Conference. AIAA 1963-1805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1805
• Hodge, J., P. Phillips, and D. Audley. 1981. “Flight Testing a Manned Lifting Reentry Vehicle /Space Shuttle/ for Aerothermodynamic Performance.” In 1st Flight Test Conference. AIAA 1981-2421. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2421
• Hodges, G. 1973. “Active Flutter Suppression: B-52 Controls Configured Vehicle.” In Dynamics Specialists Conference. AIAA 1973-322. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-322
• Hodges, Todd, Susan Gorton, and Karen Jackson. 2016. “Historical Contributions to Vertical Flight at the NASA Langley Research Center.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11334
• Hodges, G., and J. McKenzie. 1975. “B-52 Control Configured Vehicles Maneuver Load Control System Analysis and Flight Test Results.” In 13th Aerospace Sciences Meeting. AIAA 1975-72. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-72
• Hoe, Garrison, D. Bruce Owens, and Casey Denham. 2012. “Forced Oscillation Wind Tunnel Testing for FASER Flight Research Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4645
• Hoehne, Vernon O. 1967. The Subsonic Wind Tunnel of Battelle Columbus Laboratories. Defense Technical Information Center. https://doi.org/10.21236/ad0656486
• Hoerter, G. J., S. A. Powers, and M. R. Robinson. 1991. “The Development and Progress of Enhanced Fighter Maneuverability on the X-31.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/911171
• Hoey, R. 1983. “AFFTC Overview of Orbiter Reentry Flight Test Results.” In 2nd Flight Testing Conference. AIAA 1983-2682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2682
• Hoffman, M. 1971. “VTOL Aircraft Control Power Costs.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-768
• Hoffmann, M. J., G. M. Gregorek, and G. S. Weislogel. 1978. “Flight Test Techniques for Low Speed Airfoil Evaluation.” In NASA. Langley Res. Center Advanced Technol. Airfoil Res., Vol. 1, Pt. 2. https://ntrs.nasa.gov/citations/19790011830
• Hoffstedt, Donald J., Harold E. Bishop, and Herbert H. Steinmann. 1973. Flight Test of Advanced-Geometry Boron Blades. Defense Technical Information Center. https://doi.org/10.21236/ad0762199
• Hofmann, Rodolfo, Seyedbarzin Hosseini, and Florian Holzapfel. 2025. “Parameter Estimation of a Multi-Point Aerodynamic Model Based on Flight Data.” In AIAA SCITECH 2025 Forum. AIAA 2025-2175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2175
• Hoh, Roger H., and David G. Mitchell. 2018. “Handling-Qualities Specification – a Functional Requirement for the Flight Control System.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-1
• Hohenemser, K. H., and S.-K. Yin. 1973. “On the Question of Adequate Hingeless Rotor Modeling in Flight Dynamics.” In American Helicopter Society. https://ntrs.nasa.gov/citations/19730050266
• Holberg, D., and J. Grabowsky. 1981. “Pave Mover Flight Test Program.” In 1st Flight Test Conference. AIAA 1981-2492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2492
• Holdaway, George H. 1954. An Experimental Investigation of Reduction in Transonic Drag Rise at Zero Lift by the Addition of Volume to the Fuselage of a Wing-Body-Tail Configuration and a Comparison with Theory. NACA-RM-A54F22. NASA. https://ntrs.nasa.gov/citations/19930093744
• Holdaway, George H. 1955. Additional Comparisons between Computed and Measured Transonic Drag-Rise Coefficients at Zero Lift for Wing-Body-Tail Configurations. NACA-RM-A55F06. NASA. https://ntrs.nasa.gov/citations/19930088768
• Holden, M. S. 1993a. “Ground Test Facilities and Instrumentation for Aerothermal and Aero-Optical Studies of Hypersonic Interceptors.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_6
• Holden, Michael. 1993b. “Recent Advances in Hypersonic Test Facilities and Experimental Research.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5005
• Holden, Michael S. 2015. “Experimental Research and Analysis in Supersonic and Hypervelocity Flows in the LENS Shock Tunnels and Expansion Tunnel.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3660
• Holguin, Andrew, Larry Hudson, Chris Kostyk, Anthony “Nino” Piazza, Tim Risch, and Craig Stephens. 2018. “The Importance of Thermostructural Testing Hypersonic Structures.” In Hypersonic Technology and Systems Conference. https://ntrs.nasa.gov/citations/20180006671
• Holguin, Andrew, and Christopher B. Kostyk. 2010a. “Dryden Flight Research Center (DFRC) Thermal Capabilities and Status.” In NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20110006931
• Holguin, Andrew, and Christopher B. Kostyk. 2010b. “Thermal Testing Facilities and Efforts at Dryden Flight Research Center.” In NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20110000692
• Holland, Scott D., William C. Woods, and Walter C. Engelund. 2000. Hyper-X Research Vehicle (HXRV) Experimental Aerodynamics Test Program Overview. AIAA Paper 2000-4011. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000085906
• Hollis, Brian. 2008. “Heating Augmentation in Laminar Flow Due to Heat-Shield Cavities on the Project Orion CEV.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6558
• Hollis, Brian R., Scott A. Berry, Kevin E. Hollingsworth, and Sheila A. Wright. 2017. Experimental Study of Convective Heating on the Back Face and Payload of a Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Aeroshell. NASA-TP-2017-219581. NASA. https://ntrs.nasa.gov/citations/20170002597
• Hollis, Brian, Robert Nowak, Richard Thompson, et al. 1999. “X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel and Flight Conditions.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4163
• Hollmann, Martin. 1993. “The History of Composite Aircraft.” In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-3938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3938
• Holmes, P. K. 1966. “Sonic Boom.” Science 152 (3724): 865–865. https://doi.org/10.1126/science.152.3724.865.b
• Holmes, W. T. 1970. Lifting Body Patent Application. Patent Application Number: US-PATENT-APPL-SN-21263. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19710002742
• Holmes, B., C. Croom, P. Gail, G. Manuel, and D. Carraway. 1986. “Advanced Boundary Layer Transition Measurement Methods for Flight Applications.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9786
• Holmes, Bruce J., and Peter D. Gall. 1988. Method for Laminar Boundary Layer Transition Visualization in Flight. Patent Application Number: US-PATENT-APPL-SN-929862. Langley Research Center. https://ntrs.nasa.gov/citations/19890003180
• Holmes, Bruce J., and Clifford J. Obara. 1992. “Flight Research on Natural Laminar Flow Applications.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_3
• Holmes, B. J., C. P. Vandam, P. W. Brown, and P. L. Deal. 1980. Flight Evaluation of the Effect of Winglets on Performance and Handling Qualities of a Single-Engine General Aviation Airplane. NASA-TM-81892. NASA. https://ntrs.nasa.gov/citations/19810003504
• Holmes, J., and F. Woehr. 1971. “Wind-Tunnel Free-Flight Testing of Configurations with High-Finenessratio Bodies.” In 6th Aerodynamics Testing Conference. AIAA 1971-278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-278
• Holt, Maurice. 1976. “A Review of Numerical Techniques for Calculating Supercritical Airfoil Flows.” In Symposium Transsonicum II. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_40
• Holubik, Thomas E. 1988. History of the KC-10A Aircraft Acquisition. Defense Technical Information Center. https://doi.org/10.21236/ada194398
• Holway, H. 1966. “A Wind Tunnel Free Flight Testing Technique for Nonplanar Motion of Spinning Models.” In 2nd Aerodynamic Testing Conference. AIAA 1966-774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-774
• Holzhauser, Curt A., and Richard S. Bray. 1956. Wind-Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Degree Swept-Wing Airplane. NACA-TR-1276. NASA. https://ntrs.nasa.gov/citations/19930092274
• Holzhauser, C. A., R. C. Innis, and H. C. Quigley. 1964. A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers. NASA-TN-D-2231. NASA. https://ntrs.nasa.gov/citations/19640007812
• Hong, J. B., and Y. S. Jung. 2024. “Boundary Layer Transition Model with Compressibility Correction for Transonic Flow Simulations.” Journal of computational fluids engineering 29 (2): 13–33. https://doi.org/10.6112/kscfe.2024.29.2.013
• Hoogreef, Maurice, Roelof Vos, Reynard de Vries, and Leo L. Veldhuis. 2019. “Conceptual Assessment of Hybrid Electric Aircraft with Distributed Propulsion and Boosted Turbofans.” In AIAA Scitech 2019 Forum. AIAA 2019-1807. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1807
• Hook, W. Ray, and Delma C. Freeman Jr. 1989. Lifting-Body Option for a Space Station Rescue Vehicle. IAF PAPER 89-246. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19900026347
• Hooker, John R. 2014. “Design of a Hybrid Wing Body for Fuel Efficient Air Mobility Operations at Transonic Flight Conditions.” In 52nd Aerospace Sciences Meeting. AIAA 2014-1285. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1285
• Hooper, William. 1989. “Mach 5 and Mach 8 Hypersonic Test Facility.” In 25th Joint Propulsion Conference. AIAA 1989-2297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2297
• Hooser, Clinton. 2002. “Proposed Hypersonic Air Breathing Test Capability at the Holloman High Speed Test Track (Invited).” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3037. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3037
• Hopkins, E. J., and E. R. Keener. 1968. Unit Reynolds Number Effects on Boundary-Layer Transition at Mach 6. NASA. https://ntrs.nasa.gov/citations/19680046142
• Hopping, C., R. Counts, and T. Scanlan. 1986. “Long Range Planning for Flight Test Support.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9744. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9744
• Horak, Dan T., and Kevin Renze. 2016. “Dynamics and Aerodynamics of a Landing Airplane during a High-Speed Lateral Runway Departure.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1035
• Horing, Jennifer, Kurt Maute, and Iain D. Boyd. 2025. “Aerothermodynamic Sensitivity Analysis and Optimization of a Hypersonic Re-Entry Vehicle.” In AIAA SCITECH 2025 Forum. AIAA 2025-1560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1560
• Horn, Tom. 2008. NASA Dryden Flight Loads Laboratory. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20080017327
• Horn, Joe, Anthony Calise, and J. Prasad. 1998. “Flight Envelope Limiting Systems Using Neural Networks.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4459. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4459
• Horonjeff, Robert. 1962. “Runways and Taxiways for Supersonic Transports.” Journal of the Air Transport Division 88 (1): 43–62. https://doi.org/10.1061/jaceal.0000122
• Horowitz, Isaac, B. Golubev, T. Kopelman, and S. Britman. 1980. Research in Advanced Flight Control Design. Defense Technical Information Center. https://doi.org/10.21236/ada082424
• Horowitz, Stanley A., Bruce R. Harmon, and Daniel B. Levine. 2014. Using Cost Estimating Relationships to Develop a Price Index for Tactical Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada612975
• Horstman, C. 1987. “Prediction of Hypersonic Shock-Wave/turbulent-Boundary-Layer Interaction Flows.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1367
• Horstman, C., and M. Kussoy. 1967. “Free-Flight Measurements of Aerodynamic Viscous Effects on Lifting Re-Entry Bodies.” In 5th Aerospace Sciences Meeting. AIAA 1967-165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-165
• Horstmann, K., G. Redeker, A. Quast, U. Dressler, and H. Bieler. 1990. “Flight Tests with a Natural Laminar Flow Glove on a Transport Aircraft.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3044. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3044
• Horton, J. A., H. N. Massey, and G. J. Whyte. 1966. The First Experimental Flight Package of an Advanced Telemetry System with Adaptive Capability Technical Summary Report, 1 Jul. 1963: 15 Feb. 1965. NASA-CR-76515. NASA. https://ntrs.nasa.gov/citations/19660022608
• Horvath, Thomas, Matthew Rhode, and Gregory Buck. 1990. “Aerothermodynamic Measurements on a Proposed Assured Crew Return Vehicle (ACRV) Lifting-Body Configuration at Mach 6 and 10 in Air.” In 5th Joint Thermophysics and Heat Transfer Conference. AIAA 1990-1744. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1744
• Horvath, Thomas J., Deborah M. Tomek, Karen T. Berger, et al. 2010. “The HYTHIRM Project: Flight Thermography of the Space Shuttle during the Hypersonic Re-Entry.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100000137
• Hoskin, Dominique, Cuong Nguyen, and Wesley Harris. 2024. “Leading Edge Effects on Hypersonic Boundary Layer Receptivity and Transition.” In AIAA SCITECH 2024 Forum. AIAA 2024-2857. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2857
• Hosseini, Barzin, Jared A. Grauer, Florian Holzapfel, and Juergen Rauleder. 2025a. Higher-Order System Identification and Control Design for a Coaxial Rotorcraft. Georgia Institute of Technology. https://ntrs.nasa.gov/citations/20240008307
• Hosseini, Seyedbarzin, Rodolfo Hofmann, Florian Holzapfel, and Juergen Rauleder. 2025b. “Optimal Input Design for Aircraft Parameter Estimation: Flight Test Results.” In AIAA SCITECH 2025 Forum. AIAA 2025-2173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2173
• Hosseini, Seyedbarzin, and Florian Holzapfel. 2022. “Optimal Input Design for Flight Vehicle System Identification in Frequency Domain.” In AIAA SCITECH 2022 Forum. AIAA 2022-2297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2297
• Hou, Y., and H. Song. 2024. “Research on Credibility Analysis Model of Test Aircraft Based on Flight Test Mission.” IET Conference Proceedings 2023 (43): 19–24. https://doi.org/10.1049/icp.2024.0623
• Houbolt, J. C. 1974. Subcritical Flutter Testing and System Identification. NASA-CR-132480. NASA. https://ntrs.nasa.gov/citations/19740026358
• Houbolt, J. C., and A. G. Rainey. 1975. “On the Prediction of Critical Flutter Conditions from Subcritical Response Data and Some Related Wind-Tunnel Experience.” In Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003011
• Houck, J. A., F. L. Moore, J. J. Howlett, K. S. Pollock, and M. M. Browne. 1977. Rotor Systems Research Aircraft Simulation Mathematical Model. NASA-TM-78629. NASA. https://ntrs.nasa.gov/citations/19780005098
• Hough, M. 1981. “Maximum Reentry Drag Deceleration Revisited.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1861
• Howard, Richard, and Robert Bray. 1992. “Flight Test and Wind-Tunnel Study of a Scaled Unmanned Air Vehicle.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4075
• Howard, W., D. Jensen, and S. Batill. 1989. “Design of Unmanned Flight Vehicle Systems for Aerodynamic Data Acquisition.” In Aircraft Design and Operations Meeting. AIAA 1989-2110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2110
• Howe, D. 2002. “Engine Placement for Sonic Boom Mitigation.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-148
• Howell, Jan. 1988. “Reliability and Maintainability Evaluation during Flight Test.” In 4th Flight Test Conference. AIAA 1988-2185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2185
• Howell, Robert R., and Albert L. Braslow. 1955. Comparison of the Drag of a Fin-Stabilized Body of Revolution and of a Complete Airplane Configuration as Obtained at Transonic Speeds in a Slotted Wind Tunnel and in Free Flight. NACA-RM-L55H09. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019382
• Howell, R., and H. Korst. 1971. “Separation Controlled Transonic Drag-Rise Modification for V-Shaped Notches.” In 4th Fluid and Plasma Dynamics Conference. AIAA 1971-568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-568
• Howell, Charles T., and Kevin J. Shelton. 2019. “The NASA Urban Air Mobility Testbed Flight Research Aircraft.” In AUVSI Xponential 2019. https://ntrs.nasa.gov/citations/20200002700
• Howell, Charles T., III. 2011. “The Proposed Use of Unmanned Aerial System Surrogate Research Aircraft for National Airspace System Integration Research.” In AUVSI’’s Unmanned Systems North America 2011. https://ntrs.nasa.gov/citations/20110015029
• Howland, W. Lavern. 1953. “Flight Test Instrumentation Status.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/530162
• Hoyt, Robert. 2000. “Design and Simulation of Tether Facilities for the Hypersonic-Airplane Space-Tether Orbital Launch (HASTOL) Architecture.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3615
• Hozumi, Koichi, Yukimitsu Yamamoto, Alain Masson, Jacques Soutade, Patric Wagner, and Joelle Fontaine. 2001. “A Study for Prediction of Flight Aerodynamic Heating Using HYFLEX Flight and Wind Tunnel Data.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1826
• Hruby, R. J., and J. B. McDevitt. 1964. Fm Telemetry and Free-Flight Techniques for Aerodynamic Measurements in Conventional Wind Tunnels. NASA-TM-X-51648. NASA. https://ntrs.nasa.gov/citations/19650025659
• Hsia, Y.-C., Ben Gross, and J. Ortwerth. 1989. “Inviscid Analysis of a Dual Mode Scramjet Inlet.” In 25th Joint Propulsion Conference. AIAA 1989-2681. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2681
• Hsu, MoWei, and Hugh H. Liu. 2021. “Design of a Nonlinear Hierarchical Adaptive Controller for a Novel Tilt-Rotor VTOL AquaUAV.” In AIAA Scitech 2021 Forum. AIAA 2021-1283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1283
• Hu, Hui, and Paul A. Durbin. 2012. On the Simulation of Free Flight Vortices in Ground Test Facilities. Defense Technical Information Center. https://doi.org/10.21236/ada567602
• Hu, Shuyao, Chongwen Jiang, Zhenxun Gao, Chunhian Lee, and Guang Zuo. 2015. “Design of Periodic Cruise Vehicle Based on the Passive Waverider Method.” In AIAA SPACE 2015 Conference and Exposition. AIAA 2015-4546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4546
• Hu, Patrick, Kun Qu, Liping Xue, Kan Ni, and Earl Dowell. 2009. “Efficient Aeroelastic Model Updating in Support of Aircraft Flight Testing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5713
• Hu, Stephane, Victor Traisnel, Denis Walch, and Ilyass Tabiai. 2026. “In-Flight Wing Deflection Measurement on a Small-Scale Aircraft Using 2D-DIC.” Preprint, . https://doi.org/10.2139/ssrn.6790318
• Huan, Xun, and Nikola Banovic. 2024. Practical and Optimal Sequential Bayesian Experimental Design for Complex Systems Incorporating Human Experimenter Preferences (Final Scientific/Technical Report). Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/2483855
• Huang, Haoyang, Yitong Fan, Zhiqiang Ke, Ding Tang, Weiming Wang, and Dayong Li. 2024. “Designing a Variable Camber Wing Trailing Edge with Initially Curved Beams.” Preprint, . https://doi.org/10.2139/ssrn.4750675
• Huang, Guoping, Zuo Fengyuan, Wenyou Qiao, and Chen Xia. 2017a. “Design Method of Internal Waverider Inlet with Bump Compression Surface.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-4654. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4654
• Huang, Tianqiang, Bara’ah I. Fraihat, and Rafic Ajaj. 2025a. “Aeroelastic Tailoring of Strut-Braced Wing Using Tow-Steered Composites.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3471
• Huang, Ganglei, Ao Wang, Xi Chen, Guohua Tu, and Jianqiang Chen. 2025b. “Control of Stationary Görtler Vortices-Induced Hypersonic Boundary Layer Transition: Localized Steady Uniform Blowing.” Preprint, . https://doi.org/10.2139/ssrn.5171119
• Huang, Jiangtao, Zhu Zhou, Hongyang Liu, Zhenghong Gao, and Gang Liu. 2017b. “Numeric Simulation of Aircraft Gust Response Considering Aeroelastic Deformation.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2310
• Hubbard, Harvey H. 1969. “Recent Results of Sonic Boom Research.” In Aerodynamic Noise. University of Toronto Press. https://doi.org/10.3138/9781487582869-020
• Huber, F. 1966. “Probes for Measuring Mass Flux, Stagnation Point Heating, and Total Enthalpy of High Temperature Hypersonic Gas Flows.” In 2nd Aerodynamic Testing Conference. AIAA 1966-750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-750
• Hudson, Gary. 1998. “Roton Development and Flight Test Program.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5258
• Hudson, Mary L., Michael Glass, Tucker Hamilton, Eric Somers, and Rob Caldwell. 2018. “F-35 System Development and Demonstration Flight Testing at Edwards Air Force Base and Naval Air Station Patuxent River.” In 2018 Aviation Technology, Integration, and Operations Conference. AIAA 2018-3371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3371
• Hue, David, and Pascal Molton. 2020. “Turbulent Drag Induced by Low Surface Roughness at Transonic Speeds: Experimental/numerical Comparisons.” Physics of Fluids 32 (4): 045108. https://doi.org/10.1063/1.5143068
• Huebner, Lawrence D., James S. Richards, Joseph A. Brunty, R. Marshall Smith, and Dominic R. Trombetta. 2009. “A Perspective on Development Flight Instrumentation and Flight Test Analysis Plans for Ares I-X.” In 60th International Astronautical Congress. https://ntrs.nasa.gov/citations/20090037049
• Huebner, Lawrence, Kenneth Rock, Edward Ruf, David Witte, and Earl Andrews. 2001. “Hyper-X Flight Engine Ground Testing for X-43 Flight Risk Reduction.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1809
• Huebner, Lawrence D., Kenneth E. Rock, David W. Witte, Edward G. Ruf, and Earl H. Andrews Jr. 2000. Hyper-X Engine Testing in the NASA Langley 8-Foot High Temperature Tunnel. AIAA Paper 2000-3605. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000068996
• Huffman, J. K., and C. H. Fox Jr. 1978. Subsonic Longitudinal and Lateral-Directional Static Aerodynamic Characteristics for a Model with Swept Back and Swept Forward Wings. NASA-TM-74093. NASA. https://ntrs.nasa.gov/citations/19780012130
• Huffman, J. K., and C. H. Fox Jr. 1979. The Effect of Canard Relative Size and Vertical Location on the Subsonic Longitudinal and Lateral-Directional Static Aerodynamic Characteristics for a Model with a Swept Forward Wing. NASA-TM-78739. NASA. https://ntrs.nasa.gov/citations/19790019967
• Hughes, D. L. 1981. Comparison of Three Thrust Calculation Methods Using in-Flight Thrust Data. NASA-TM-81360. NASA. https://ntrs.nasa.gov/citations/19810021573
• Hughes, Stephen J., F. McNeil Cheatwood, Anthony M. Calomino, Henry S. Wright, Mary E. Wusk, and Monica F. Hughes. 2013. Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview. NF1676L-16795. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20130014935
• Hughes, D. L., and H. J. Johnson. 1972. Flight-Determined Characteristics of an Air Intake System on an F-111A Airplane. NASA-TN-D-6679. NASA. https://ntrs.nasa.gov/citations/19720011346
• Hughes, Charles W., and Rodney K. Wernicke. 1974. Flight Test of a Hingeless Flexbeam Rotor System. Defense Technical Information Center. https://doi.org/10.21236/ad0783393
• Hughes Tool Co Culver City Ca. 1963. Preliminary Design Study Hot Cycle Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0408650
• Hui, Kenneth, and David Collins. 2001. “In-Flight Calibration of Air Data Systems Using an Innovative Nose-Mask Sensor.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-410
• Hull, Peter. 2026. Optimal Experimental Design and Estimation When Potential Outcomes Are Bounded. National Bureau of Economic Research. https://doi.org/10.3386/w35629
• Hull, Donald L., and Kenneth L. Roger. 1975. B-52E CCV Flight Test Data Applicable to Parameter Estimation. Defense Technical Information Center. https://doi.org/10.21236/adb011143
• Hulshoff, S., J. Mulder, and H. Hoejmakers. 1996. “Estimation of Aircraft Dynamic Parameters Using Euler Computations and Comparison with Flight-Test Data.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3416
• Hunley, J. D. 1999. Toward Mach 2: The Douglas D-558 Program. NASA-SP-4222. NASA. https://ntrs.nasa.gov/citations/19990054836
• Hunt, Dillon. n.d. “Supersonic Combustion in Inlet-Fuelled Busemann-like Axisymmetric Scramjet Flow Paths.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2014.194
• Hunt, James L. 1989. “Hypersonic Airbreathing Vehicle Design (Focus on Aero-Space Plane).” In Hypersonics. Birkhäuser Boston. https://doi.org/10.1007/978-1-4684-9187-6_5
• Hur, Gi-Bong, and John Valasek. 2003. “System Identification of Powered Parafoil-Vehicle from Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5539
• Hurley, S. R. 1976. “The Application of Digital Computers to near-Real-Time Processing of Flutter Test Data.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014091
• Hurley, F., F. Spaid, F. Roos, L. Stivers Jr., and A. Bandettini. 1975. “Supercritical Airfoil Flowfield Measurements.” In 8th Fluid and PlasmaDynamics Conference. AIAA 1975-880. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-880
• Husmeier, Frank, and Hermann Fasel. 2007. “Numerical Investigations of Hypersonic Boundary Layer Transition over Circular Cones.” In 18th AIAA Computational Fluid Dynamics Conference. AIAA 2007-3843. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3843
• Hussein, Sarah M., and Bernd Chudoba. 2016. “Sizing Study for Assessing First-Order Feasibility of the Bell X-1A Supersonic Rocket-Powered Aircraft.” In 16th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2016-3464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3464
• Huston, Wilber B., A. Gerald Rainey, and Thomas F. Baker. 1955. A Study of the Correlation between Flight and Wind-Tunnel Buffeting Loads. NACA-RM-L55E16b. NASA. https://ntrs.nasa.gov/citations/19930088735
• Hutchinson, Herbert. 1963. “Further Definition of the Sonic Boom Problem and Its Influence on Supersonic Transport Design, Propulsion and Performance Requirements.” In Summer Meeting. AIAA 1963-230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-230
• Huttsell, L., and F. Eastep. 1989. “Aeroelastic Characteristics of NACA 0012 Airfoil at Angle of Attack.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3375
• Huttsell, L. J., T. E. Noll, and D. E. Holsapple. 1976. “Wind Tunnel Investigation of Supersonic Wing-Tail Flutter.” In NASA. Langley Res. Center Flutter Testing Tech.,. https://ntrs.nasa.gov/citations/19770014086
• Hwang, C., E. Johnson, and W. Pi. 1980. “Recent Development of the YF-17 Active Flutter Suppression System.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-769
• “Hybrid Laminar Flow Flight Tests Underway.” 1999. Aircraft Engineering and Aerospace Technology 71 (1). https://doi.org/10.1108/aeat.1999.12771aaf.007
• Hyde, David C., Frank R. Brown, Kamal M. Shweyk, and Gautam H. Shah. 2014. “Advanced Modeling and Uncertainty Quantification for Flight Dynamics (VSST1-7) Interim Results and Challenges.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0035
• Hyde, Charles R., and Jeffrey J. Massie. 1993. “Instrumentation and Telemetry Systems for Free-Flight Drop Model Testing.” In International Foundation for Telemetering, Annual International Telemetering Conference. https://ntrs.nasa.gov/citations/19930068757
• Hylton, Todd, Christopher Martin, Richmon Tun, and Vincent Castelli. 2012. “The DARPA Nano Air Vehicle Program.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-583
• Hyper-X Model Testing with Animation. 1996. NONP-NASA-VT-2000043976. Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20000033438
• Hypersonic Flight. 2025. Wiley. https://doi.org/10.1002/9781394309290.ch9
• “Hypersonic Flow at Low Reynolds Number Introduction: Introduction.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0011.0012
• “Hypersonic Ground Test Requirements.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0001.0015
• “A Hypersonic Ground-Test Facility Using Magnetic Levitation and Electromagnetic Propulsion.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0479.0497
• Iannuzzo, Generoso, Salvatore Russo, Alfonso Apicella, Lorenzo Rossi, and Sergio Esposito. 2018. “Morphing Wing Integration.” In Morphing Wing Technologies. Elsevier. https://doi.org/10.1016/b978-0-08-100964-2.00020-4
• Ide, H., J. Armstrong, J. Haney, and K. Szema. 1989. “Hypersonic Vehicle Forebody Design Studies and Aerodynamic Trends.” In 7th Applied Aerodynamics Conference. AIAA 1989-2182. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2182
• “Identification of Speed Brake, Ramp Door, Air-Drop, and Landing Gear Effects from ‘Transall’ Flight Data.” 1994. In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3473. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3473
• Idsardi, R. 1983. “A Distributed, Real Time, Flight Test System.” In 2nd Flight Testing Conference. AIAA 1983-2732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2732
• Ifju, Peter, Martin Waszak, and Luther Jenkins. 2001. “Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4005
• Ikawa, Hideo. 1989. “Rapid Methodology for Design and Performance Prediction of Integrated Scramjet/hypersonic Vehicle.” In 25th Joint Propulsion Conference. AIAA 1989-2682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2682
• Ilie, Marcel, and John Havenar. 2022. “A Fully-Coupled Computational Aeroelasticity Model for Transonic and Supersonic Flows.” In AIAA AVIATION 2022 Forum. AIAA 2022-3600. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3600
• Iliff, Kenneth. 1987. “Aircraft Parameter Estimation.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-623
• Iliff, K., and R. Maine. 1982. “NASA Dryden’s Experience in Parameter Estimation and Its Uses in Flight Test.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1373
• Iliff, K. W., and R. E. Maine. 1985. “Maximum Likelihood Estimation with Emphasis on Aircraft Flight Data.” In JPL Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 3. https://ntrs.nasa.gov/citations/19850022895
• Iliff, K., R. Maine, and D. Cooke. 1981. “Selected Stability and Control Derivatives from the First Space Shuttle Entry.” In 1st Flight Test Conference. AIAA 1981-2451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2451
• Iliff, K. W., R. E. Maine, and T. D. Montgomery. 1978a. Considerations in the Analysis of Flight Test Maneuvers. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19790066420
• Iliff, K. W., R. E. Maine, and M. F. Shafer. 1976. Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8-Scale F-15 Airplane Model Obtained from Flight Test. NASA-TN-D-8136. NASA. https://ntrs.nasa.gov/citations/19760008088
• Iliff, K. W., R. E. Maine, and S. T. Steers. 1978b. Flight-Determined Stability and Control Coefficients of the F-111A Airplane. NASA-TM-72851. NASA. https://ntrs.nasa.gov/citations/19780010132
• Iliff, K., and B. Powers. 1969. “A Comparison of Newton-Raphson and Other Methods for Determining Stability Derivatives from Flight Data.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-315
• Iliff, Kenneth, and Mary Shafer. 1992. “Space Shuttle Hypersonic Flight Research and the Comparison to Ground Test Results.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3988. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3988
• Iliff, Kenneth W., and Mary F. Shafer. 1993a. “A Comparison of Hypersonic Flight and Prediction Results.” In AIAA. https://ntrs.nasa.gov/citations/19930039009
• Iliff, Kenneth W., and Mary F. Shafer. 1993b. “Space Shuttle Hypersonic Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results.” In Aerospace Ground Testing Conference. https://ntrs.nasa.gov/citations/19940006365
• Iliff, Kenneth W., and Mary F. Shafer. 1995. “A Comparison of Hypersonic Vehicle Flight and Prediction Results.” In Aerospace Sciences Meeting and Exhibit. https://ntrs.nasa.gov/citations/19960003513
• Iliff, K. W., and L. W. Taylor Jr. 1969. “A Modified Newton-Raphson Method for Determining Stability Derivatives from Flight Data.” In COMPUTING METHODS IN OPTIMIZATION PROBLEMS-2, SECOND INTERNATIONAL CONFERENCE. https://ntrs.nasa.gov/citations/19700043156
• Iliff, Kenneth W., and Kon-Sheng Charles Wang. 1997. Flight-Determined Subsonic Longitudinal Stability and Control Derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with Thrust Vectoring. NASA/TP-97-206539. NASA. https://ntrs.nasa.gov/citations/19980007172
• Immenschuh, William. 1990. “Ryan X-13 Experimental Aircraft: Lessons Learned.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3236
• “In-Flight Demo of Multiple Unmanned Aircraft Autonomy System.” 2007. Aircraft Engineering and Aerospace Technology 79 (2). https://doi.org/10.1108/aeat.2007.12779baf.009
• Inagaki, Kenjiro, Ayano Yamamoto, Hirokage Ogoshi, Kenji Hayama, and Kenji Sakai. 1998. “Research on a Sonic Boom Evaluation and Low-Boom and Low-Drag Design.” Journal of the Acoustical Society of America 104 (3_Supplement): 1848–1848. https://doi.org/10.1121/1.424452
• Ince, D. B. 1967. “Application Experience with the B-70 Flight Test Data System.” In Aerospace Instrumentation. Elsevier. https://doi.org/10.1016/b978-1-4831-9836-1.50014-9
• “Incorporating Agility Flight Test Metrics Concurrently into the Aircraft Preliminary Design Process.” 1994. In Biennial Flight Test Conference. AIAA 1994-2135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2135
• INDES User’s Guide Multistep Input Design with Nonlinear Rotorcraft Modeling. 1979. NASA-CR-159085. NASA. https://ntrs.nasa.gov/citations/19810014193
• “Induced Drag Effect on Airframe Noise.” 1976. In Aeroacoustics: STOL Noise: Airframe and Airfoil Noise. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865190.0221.0235
• Inger, G. 1991. “Application of Oswaititsch’s Theorem to Supercritical Airfoil Drag Calculation.” In 9th Applied Aerodynamics Conference. AIAA 1991-3210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3210
• “Initial Flight Test of a Ground Deployed System for Flying Qualitiesassessment.” 1989. In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3359
• Integrated Propulsion Technology Demonstrator. Program Plan. 1994. NASA-CR-196870. NASA. https://ntrs.nasa.gov/citations/19950005410
• “Integration and Simulated Flight Testing of a Geared Fan V/STOL Airplane.” 1977. In V/STOL Conference. AIAA 1977-612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-612
• International Standard Atmosphere (ISA) Table. 2017. Wiley. https://doi.org/10.1002/9781118534786.app1
• “Introduction to Stability and Control Flight Testing.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0199.0208
• “Inviscid Hypersonic Flow Introduction: Introduction.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0319.0320
• Iollo, Jacopo. n.d. “Inference Driven Bayesian Experimental Design.” PhD diss., Université Grenoble Alpes. https://doi.org/10.70675/a36a13b4zb29fz4733zbd45z90d31edd1371
• Ippolito, Corey A., Nhan T. Nguyen, Joseph Totah, Khanh Trinh, and Eric B. Ting. 2013. “Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition.” In AIAA Infotech@Aerospace (I@A) Conference. AIAA 2013-5143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5143
• Iscold, Paulo. 2008. “Low-Cost Flight Test System for Light Aircrafts.” Aircraft Engineering and Aerospace Technology 80 (3): 243–52. https://doi.org/10.1108/00022660810873674
• Ishida, Takashi, Keiichi Ishiko, Atsushi Hashimoto, Takashi Aoyama, and Kuniyuki Takekawa. 2016. “Transonic Buffet Simulation over Supercritical Airfoil by Unsteady-FaSTAR Code.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1310
• Ishikawa, Hiroaki, Dongyoun Kwak, and Kenji Yoshida. 2007. “CFD Analysis on Flight Test Results of Supersonic Experimental Airplane NEXST-1.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-3925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3925
• Ishikawa, Hiroaki, Y. Makino, and K. Ohira. 2011. “Sonic-Boom Prediction of a Scaled Low-Boom Demonstration Aircraft Considering Viscosity Effects.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3662. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3662
• Ishikawa, Hiroaki, Yoshikazu Makino, Atsushi Ueno, and Masashi Kanamori. 2019. “Sonic Boom Assessment in Primary Boom Carpet of Low-Boom Supersonic Airplane (NASA C25D).” In AIAA Scitech 2019 Forum. AIAA 2019-0298. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0298
• Ishikawa, Yuhei, and Wataru Yamazaki. 2021. “Aerodynamic Shape Optimization of Waverider Fuselage by Response Surface Methodology.” Proceedings of The Computational Mechanics Conference 2021.34 (0): 113. https://doi.org/10.1299/jsmecmd.2021.34.113
• Ishimoto, Shinji. 1995. “Guidance Algorithm for Suborbital Flight Experiment of Unmanned Lifting Entry Vehicle.” In Guidance, Navigation, and Control Conference. AIAA 1995-3286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3286
• Ishimoto, Shinji, and Shinji Ishimoto. 1997. “New Algorithm of Maximum Likelihood Parameter Estimation for Flight Vehicles.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3784
• Ishimoto, Shinji, Minoru Takizawa, Hirokazu Suzuki, and Toshiki Morito. 1996. “Flight Control System of Hypersonic Flight Experiment Vehicle.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3403
• Ishmael, S. D., and D. R. McMonagle. 1983. AFTI/F-16 Flight Test Results and Lessons. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19840033380
• Islam, Md Azizul, Azizur Rahman, Achintya Saha, and Bruce Jo. 2025. “Design, Implementation, and Test Flight of a Lightweight Camber Morphing Wing Aircraft.” Preprint, . https://doi.org/10.31224/4605
• Isogai, Koji. 1988. “Aeroelastic tailoring.” Journal of the Japan Society for Composite Materials 14 (3): 96–101. https://doi.org/10.6089/jscm.14.96
• Ispir, Ali C., and Bayindir H. Saracoglu. 2019. “Development of a 1D Dual Mode Scramjet Model for a Hypersonic Civil Aircraft.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-3842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3842
• Ivaldi, Davide, Ney R. Secco, Song Chen, John T. Hwang, and Joaquim R. R. A. Martins. 2015. “Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft.” In 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2015-3436. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3436
• Ivanteeva, Lyudmila G., Victor V. Kovalenko, Evgeny V. Pavlyukov, and Leonid L. Teperin. 1998. “Validation of Sonic Boom Propagation Codes Using SR-71 Flight Test Data.” Journal of the Acoustical Society of America 104 (3_Supplement): 1849–1849. https://doi.org/10.1121/1.424456
• Ivanteyeva, Lyudmila G., Victor V. Kovalenko, Evgeny V. Pavlyukov, Leonid L. Teperin, and Robert G. Rackl. 2002. “Validation of Sonic Boom Propagation Codes Using SR-71 Flight Test Data.” Journal of the Acoustical Society of America 111 (1): 554–61. https://doi.org/10.1121/1.1404377
• Ivler, Christina, Mark Tischler, Elizabeth Rowe, James Martin, and Mark Lopez. 2019. “System Identification Guidance for Multirotor Aircraft: Dynamic Scaling and Test Techniques.” In Proceedings of the Vertical Flight Society 75th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0075-2019-14754
• Iwamiya, Toshiyuki. 2002. “A Computational Study on Unmanned Scaled Supersonic Experimental Airplane.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2841
• Jackel, Larry. 2020. “11. Program Management at DARPA: A Personal Perspective.” In The DARPA Model for Transformative Technologies. Open Book Publishers. https://doi.org/10.11647/obp.0184.11
• Jacklin, S. A. 1986. System Identification Techniques for Helicopter Higher Harmonic Control. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19870031967
• Jackman, Charles, Anne Douglas, and Kurt Brueske. 1992. “A Simulation of the Effects of the National Aerospace Plane Testing on the Stratosphere Using a Two-Dimensional Model.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5073
• Jackson, Eugene B. 1953. “The NACA Classification System—a Case History.” Aslib Proceedings 5 (3): 215–34. https://doi.org/10.1108/eb049481
• Jackson, Alexander Gordon. 2023a. “Aerodynamic Performance of the Inboard Elevon on a Blended-Wing-Body Aircraft.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14660895.v1
• Jackson, Christopher. 2023b. “Value of Information for Estimation Instead of Decision-Making.” In Value of Information for Healthcare Decision-Making. Chapman and Hall/CRC. https://doi.org/10.1201/9781003156109-7
• Jackson, Karen E., Richard L. Boitnott, Edwin L. Fasanella, Lisa E. Jones, and Karen H. Lyle. 2004. A History of Full-Scale Aircraft and Rotorcraft Crash Testing and Simulation at NASA Langley Research Center. Army Research Lab. https://ntrs.nasa.gov/citations/20040191337
• Jackson, E., and T. Coyle. 1983. “Assurance of the X-29 Advanced Technology Demonstrator Flight Control Software.” In 2nd Flight Testing Conference. AIAA 1983-2724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2724
• Jackson, E. Bruce, Christopher I. Cruz, and W. A. Ragsdale. 1992. Real-Time Simulation Model of the HL-20 Lifting Body. NASA-TM-107580. NASA. https://ntrs.nasa.gov/citations/19920021916
• Jackson, L. R., F. S. Kirkham, and J. P. Weidner. 1978. Structural Concepts and Experimental Considerations for a Versatile High-Speed Research Airplane. NASA-TM-78743. NASA. https://ntrs.nasa.gov/citations/19790005909
• Jackson, V., and D. Patch. 1968. “Design and Development of the Primary Fly-by- Wire Flight Control System for the XV-4B V/STOL Research Aircraft.” In Control and Flight Dynamics Conference. AIAA 1968-818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-818
• Jackson, E., and Robert Rivers. 1998. “Flight-Simulated Launch-Pad-Abort-to-Landing Maneuvers for a Lifting Body.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4254
• Jackson, E., Robert Rivers, Rajiv Chowdhry, W. Ragsdale, and David Geyer. 1993. “Investigation of the Launch Pad Abort Capabilities of the HL-20 Lifting Body.” In Flight Simulation and Technologies. AIAA 1993-3690. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3690
• Jackson, E. Bruce, Robert A. Rivers, Rajiv S. Chowdhry, W. A. Ragsdale, and David W. Geyer. 1994. Launch-Pad Abort Capabilities of the HL-20 Lifting Body. NASA-TM-4550. NASA. https://ntrs.nasa.gov/citations/19940030181
• Jacob, Neal, and Michael Amitay. 2022. “Three-Dimensional Flowfield Measurements of a Swept-Back Cantilevered Wing at High Angles of Attack.” In AIAA SCITECH 2022 Forum. AIAA 2022-0466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0466
• Jacob da Motta, L. A. 2020. “2.6 How Conventional Flight Test Instrumentation Concepts Can Contribute to the Innovative eVTOL Aerospace Development.” In Proceedings - ettc2020. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2020/2.6
• Jacobsen, R. A. 1974. Hot-Wire Anemometry for in-Flight Measurement of Aircraft Wake Vortices. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19740060871
• Jacobsen, R. A., and M. R. Barber. 1977. “Flight Test Techniques for Wake-Vortex Minimization Studies.” In Wake Vortex Minimization. https://ntrs.nasa.gov/citations/19780004079
• Jacobsen, R. A., and R. K. Greif. 1972. Simulation Study of the Lift Roll Coupling Problem for Hovering VTOL Aircraft. NASA-TN-D-6906. NASA. https://ntrs.nasa.gov/citations/19720020370
• Jacobson, Orlin M. 1952. Terrier Booster Flight Test Number 5. Defense Technical Information Center. https://doi.org/10.21236/ad0029208
• Jacobson, D. 1964. “An Evaluation of Lift Engines in Tactical Vtol Aircraft.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-767. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-767
• Jacobson, David. 2004. X-37 Flight Demonstrator: A Building Block in NASA’s Future Access to Space; X-37 Flight Demonstrator: Orbital Vehicle Technology Development Approach. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20040041357
• Jacobson, G. 2005. Thermal Testing of Dallas/Maxim iButton Temperature Logger, Model DS1922L, for Flight Qualification on Captive Flight Test Unit?1B (CFTU-1B). Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/877779
• Jacobson, Steve. 2015. “NASA Armstrong Flight Research Center Dynamics and Controls Branch.” In Aerospace Control and Guidance Systems Committee Meeting. https://ntrs.nasa.gov/citations/20150002848
• Jacobson, G., and A. Lavietes. 2005. Vibration Testing of Dallas/Maxim iButton Temperature Logger, Model DS1999L, for Flight Qualification on Captive Flight Test Unit?B (CFTU-B). Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/877879
• Jacques, Dave, Meir Pachter, Geno Wagner, and Bill Blake. 2001. “An Analytical Study of Drag Reduction in Tight Formation Flight.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4075
• Jaeger, Sam, and Maziar Hemati. 2025. “Hypersonic Glide Vehicle Trajectory Design Using Constrained Energy Maneuverability.” In 2025 Regional Student Conferences. AIAA 2025-97945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-97945
• Jaffal, Hayder M., A. S. Darwish, and Ibtisam A. Hassan. 2010. “Theoretical and Experimental Study of a Forward Swept Wing.” Anbar Journal of Engineering Sciences 3 (2): 15–30. https://doi.org/10.37649/aengs.2010.14202
• Jaffe, P. 1972. “Non-Planar Tests Using the Wind Tunnel Free-Flight Technique.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-983. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-983
• Jaffe, P. 1975. A Free Flight Investigation of Transonic Sting Interference. NASA-CR-142084. NASA. https://ntrs.nasa.gov/citations/19750008472
• Jaffe, P., and R. H. Prislin. 1966. Effect of Boundary-Layer Transition on Dynamic Stability. AIAA PAPER 64-427. NASA. https://ntrs.nasa.gov/citations/19660039520
• Jagtap, Swapnil Sarjerao. 2025. “Conceptual Aircraft Sizing Using Systems Engineering for N+3 Subsonic Hybrid-Electric Propulsion Concepts.” Preprint, . https://doi.org/10.31224/4316
• Jahn, Ingo H. 2023. “Conceptual Study into Wave Ingesting Propulsion for Hypersonic Flight.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3034
• Jakeman, John. 2024. “PyApprox: A Software Package for Sensitivity Analysis, Bayesian Inference, Optimal Experimental Design, and Multi-Fidelity Uncertainty Quantification and Surrogate Modeling.” In SIAM Conference on Uncertainty Quantification - Trieste, , Italy - February - 2024. US DOE. https://doi.org/10.2172/2540434
• Jakowluk, Wiktor. 2019. “Design of an Optimal Input Signal for Parameter Estimation of Linear Fractional-Order Systems.” In Lecture Notes in Electrical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-030-17344-9_10
• James, Chris. 2022. “The BOLT II Hypersonic Flight Test Could Bring Superfast Global Travel a Step Closer.” Preprint, . https://doi.org/10.64628/aa.36gmcnkfy
• James, C., Jr. 1981. “Aerodynamics of Rocket Plume Interactions at Supersonic Speeds.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1905
• James McGree. n.d. “Optimal Experimental Design for Nonlinear and Generalized Linear Models.” PhD diss., The University of Queensland. https://doi.org/10.14264/152747
• Jameson, A. 1979. Acceleration of Transonic Potential Flow Calculations on Arbitrary Meshes by the Multiple Grid Method. AD-A072301. New York, University. https://ntrs.nasa.gov/citations/19790061249
• Janardanan, Jyothi, and M. Jayakumar. 2006. “Robust Longitudinal Flight Controller Design for a Hypersonic Re-Entry Vehicle.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8076. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8076
• Jang, Jo-Won. 2003a. “Reynolds Number Effects on the near-Wake of an Oscillating Airfoil, Part 2: Turbulent Intensity.” Journal of the Korean Society for Aeronautical & Space Sciences 31 (8): 8–18. https://doi.org/10.5139/jksas.2003.31.8.008
• Jang, Jo-Won. 2003b. “Reynolds Number Effects on the near-Wake of an Oscillating Naca 4412 Airfoil, Part 1: Mean Velocity Field.” Journal of the Korean Society for Aeronautical & Space Sciences 31 (7): 15–25. https://doi.org/10.5139/jksas.2003.31.7.015
• Janić, Milan. 2025. “Supersonic Commercial Air Transport System.” In Automated, Faster and Greener Transport Systems. CRC Press. https://doi.org/10.1201/9781003504337-8
• Jankiewicz, Jakub Antoni. 2026. “The Impact of Staggered Fins on Aerodynamic Drag of a Transonic Sounding Rocket.” In Materials Research Proceedings, vol. 69. Materials Research Forum LLC. https://doi.org/10.21741/9781644904251-46
• Jann, Thomas, and Christian Greiner-Perth. 2009. “Flight Test Instrumentation for Evaluation of the FASTWing CL System.” In 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2009-2932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2932
• Jann, Thomas, and Oleg Yakimenko. 2015. “Flight-Test Instrumentation.” In Precision Aerial Delivery Systems: Modeling, Dynamics, and Control. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624101960.0685.0740
• Janna, William S. 2020. “Dimensional Analysis and Dynamic Similitude.” In Introduction to Fluid Mechanics, Sixth Edition. CRC Press. https://doi.org/10.1201/9780429324536-4
• Jansen, Ralph H., Cheryl Bowman, Amy Jankovsky, Rodger Dyson, and James L. Felder. 2017. “Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports.” In NASA Ames Research Center. https://ntrs.nasa.gov/citations/20170012222
• Jarvinen, P., and C. Bruce. 1976. “Mini-RPV Flight Dynamics Measurements.” In Guidance and Control Conference. AIAA 1976-1940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1940
• Jarvis, C. R. 1966. Operational Experience with the Electronic Flight Control Systems of a Lunar-Landing Research Vehicle. NASA-TN-D-3689. NASA. https://ntrs.nasa.gov/citations/19660030246
• Jarvis, C. R. 1967. Fly-by-Wire Flight Control System Experience with a Free-Flight Lunar-Landing Research Vehicle. AIAA PAPER 67-273. NASA. https://ntrs.nasa.gov/citations/19670041319
• Jarvis, George A., and Lloyd J. Fisher. 1946. Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16-Size Model. NACA-MR-L6A03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930093655
• Jäschke, Jacob. 2021. “2aPA6: Sonic Boom Simulation for Boom Carpet Determination.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f2425
• Jäschke, Jacob J., and Bernd Liebhardt. 2021. “Sonic Boom Simulation for Boom Carpet Determination.” Journal of the Acoustical Society of America 149 (4_Supplement): A74-A75. https://doi.org/10.1121/10.0004561
• Jategaonkar, Ravindra, Roland Behr, Wilhelm Gockel, and Christoph Zorn. 2005. “Data Analysis of Phoenix RLV Demonstrator Flight Test.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6129
• Javaid, Kashif, and Varnavas Serghides. 2003. “Thrust Matching Requirements for the Conceptual Design of Hypersonic Waverider Vehicles.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-6953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6953
• Javaid, Kashif, and Varnavas Serghides. 2004. “Airframe-Propulsion Integration Methodology for Waverider-Derived Hypersonic Cruise Aircraft Design Concepts.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1201
• Javorsek, Daniel, II, Immanuel Barshi, and David Iverson. 2016. “Enhancing Flight Test Safety with Real-Time Early Warning Techniques.” In International Test and Evaluation Association. https://ntrs.nasa.gov/citations/20190000256
• Jayaraman, Balaji, Kumar Gaurav, Dipak K. Giri, and Ajoy K. Ghosh. 2022a. “Nonsingular Fast Terminal Sliding Mode Flight Control of a Subscale Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-0751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0751
• Jayaraman, Buvana, and Mark Potsdam. 2014. “UH-60A Rotor Tip Vortex Prediction and Comparison to Full-Scale Wind Tunnel Measurements.” In Proceedings of the Vertical Flight Society 70th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0070-2014-9445
• Jayaraman, Buvana, Andrew Wissink, Rohit Jain, and Manas Khurana. 2022b. “Uncertainty Quantification Approach for Rotorcraft Simulations.” In Proceedings of the Vertical Flight Society 78th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0078-2022-1239
• Jee, Craig. n.d. “Supersonic Multi-Objective Optimization of a Rocket Based Combined Cycle Inlet by Differential Evolution.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2018-13341
• Jeffrie, H., and D. Rolston. 1972. “Survivable Flight Control System Compatibility Test Program.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-761. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-761
• Jenkins, Jerry. 1989. “Relationships among Nonlinear Aerodynamic Indicial Response Models, Oscillatory Motion Data, and Stability Derivatives.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3351
• Jenkins, B. Z., and A. S. Marks. 1975. Rotor Downwash Velocities about the UH-1M Helicopter: Flight Test Measurements and Theoretical Calculations. Defense Technical Information Center. https://doi.org/10.21236/ada008965
• Jenkins, J. M., G. P. E. Pearson, and M. H. Tang. 1968. Vertical-Tail Loads and Control-Surface Hinge-Moment Measurements on the M2-F2 Lifting Body during Initial Subsonic Flight Tests. NASA-TM-X-1712. NASA. https://ntrs.nasa.gov/citations/19710005528
• Jenney, Gavin D., Harry W. Schreadley, and Carl N. Allbright. 1982. Flight Test of a G. E. and DCI Direct Drive Fly-By-Wire Flight Control System. Defense Technical Information Center. https://doi.org/10.21236/ada117244
• Jensen, Robert. 2016. “Dale Reed Subscale Flight Research Lab (Ballin’ on a Budget).” In Outreach at Scaled. https://ntrs.nasa.gov/citations/20160003379
• Jensen, Jeff, and Bob Braendlein. 1996. “Review of the Marquardt Dual Mode Mach 8 Scramjet Development.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3037. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3037
• Jensen, S., and R. Pera. 1977. “Airplane/engine Optimization for an Operational Lift/cruise V/STOL Airplane.” In V/STOL Conference. AIAA 1977-572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-572
• Jentink, Henk W., and Rodney K. Bogue. 2005. “Optical Air Flow Measurements for Flight Tests and Flight Testing Optical Air Flow Meters.” In Flight Test: Sharing Knowledge and Experience. https://ntrs.nasa.gov/citations/20060011604
• Jeong, Minjae, Suhun Cho, and Solkeun Jee. 2026. “Control of Laminar-to-Turbulent Transition in Hypersonic Boundary Layer with Porous Surface.” In AIAA SCITECH 2026 Forum. AIAA 2026-0729. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0729
• Jeong, Tae Woong, and Sung Min Jo. 2026. “Stochastic Uncertainty Quantification of Radiative Heating in Hypersonic Atmospheric Entry.” In AIAA SCITECH 2026 Forum. AIAA 2026-0658. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0658
• Jernell, L. S. 1969. Antenna Effects on the Aerodynamic Characteristics of a 0.410-Scale Model of the Cajun Rocket at Mach Numbers from 2.30 to 4.63. NASA-TM-X-1771. NASA. https://ntrs.nasa.gov/citations/19690011744
• Jernell, L. S. 1971. Aerodynamic Characteristics of Wing-Body and Lifting-Body Configurations of Hypersonic Cruise Aircraft at Mach 2.30 to 4.63. NASA-TM-X-2287. NASA. https://ntrs.nasa.gov/citations/19710019385
• “Jet Thrust Measurement in Flight.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0069.0074
• Jeun, Buddy H., and Allan Whittaker. 2002. Multi-Sensor Information Fusion Technology Applied to the Development of Smart Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada467469
• Jewell, W. F. 1981. “Identification of Multiloop Pilot Describing Functions Obtained from Simulated Approaches to an Aircraft Carrier.” In JPL Proc. of the 17th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19820005813
• Jex, Henry R., Raymond E. Magdaleno, Paul Gelhausen, and Mark B. Tischler. 1987. Pre- and Post-Flight-Test Models versus Measured Skyship-500 Control Responses. AIAA PAPER 87-2508. Systems Technology, Inc. https://ntrs.nasa.gov/citations/19870061376
• Jha, Ratneshwar, and Aditi Chattopadhyay. 1999. “Smart Composite Wing Design for Optimal Aeroelastic Control.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1514
• Jiang, Wu. 2024. “Research of Climb Performance Calculation Method and Program Implementation for Civil Aircraft Flight Test.” In Mechanisms and Machine Science. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-62664-7_49
• Jiang, Genrui, Ming Dong, and Lei Zhao. 2026. “Influence of Morphing Sweep Angle on Hypersonic Boundary-Layer Transition.” Preprint, . https://doi.org/10.2139/ssrn.6809099
• Jiang, Xiuqiang, and Shuang Li. 2018. “Robust Flight Envelope Generation Approach for Mars Entry Using Uncertainty Quantification and Reachable Controllable Sets.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3160
• Jiang, Zhenhua, and Mehrdad Pakmehr. 2022. “Model Predictive Control for Distributed Electric Propulsion of eVTOL Vehicles: A Preliminary Design.” In AIAA SCITECH 2022 Forum. AIAA 2022-0878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0878
• Jiang, Zenghui, Wei Song, and Wei Lu. 2017. “Development of Hypersonic Wind Tunnel Free-Flight Test in CAAA.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2262
• Jiang, Zonglin, and Hongru Yu. 2017. “Theories and Technologies for Duplicating Hypersonic Flight Conditions for Ground Testing.” National Science Review 4 (3): 290–96. https://doi.org/10.1093/nsr/nwx007
• Jiang, Hongyan, and Yichuan Zhao. 2021. “A Review of Bayesian Optimal Experimental Design on Different Models.” In Emerging Topics in Statistics and Biostatistics. Springer International Publishing. https://doi.org/10.1007/978-3-030-72437-5_10
• Jianshuang Song, H. H. T. Liu, and Zhang Ren. 2012. “Self-Regulation Controller Design Based on Disturbance Estimation for Reusable Launch Vehicle.” In International Conference on Automatic Control and Artificial Intelligence (ACAI 2012). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2012.1344
• Jin, Sangwook, Hojin Choi, Jong-Ryul Byun, and Gisu Park. 2023. “Combustion Characteristics of a Dual-Mode Ramjet Engine with a Supersonic Aerodynamic Ramp Injector.” Preprint, . https://doi.org/10.2139/ssrn.4459211
• Jin, Peng, Bi Feng Song, and Xiao Ping Zhong. 2013. “Aeroelastic Tailoring of Blended Composite Panels with Lamination Parameters.” Applied Mechanics and Materials 401-403: 571–77. https://doi.org/10.4028/www.scientific.net/amm.401-403.571
• Jing, Cheng, and Tang Shuo. 2008. “Integrated Optimization Design of Hypersonic Cruise Vehicle.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-142
• Jing, Che, and Shao Yuan-pei. 2015. “Concurrent Subspace Optimization Design of Hypersonic Cruise Vehicle.” In 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2015-3242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3242
• Jo, Min-Seon, Bu-Kyeng Sung, Seung-Min Jeong, and JeongYeol Choi. 2024. “Operation Mode Analysis of Dual Combustion Ramjet Engine from 3D Turbulent Combustion Simulation.” In AIAA SCITECH 2024 Forum. AIAA 2024-1249. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1249
• Joels, Tsoof, and Daniella E. Raveh. 2022. “Wing Dynamic Shape-Sensing from Fiber-Optic Strain Data Using the Kalman State Estimator.” In AIAA SCITECH 2022 Forum. AIAA 2022-2420. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2420
• John, Arthur W. n.d. “Traffic Forecast for the Supersonic Transport.” PhD diss., Drexel University. https://doi.org/10.17918/00005601
• Johnsen, Lars, Christopher L. Martin, Mark F. Reeder, and Darrell S. Crowe. 2016. “Numerical Simulation of Supersonic Jets in Transonic and Supersonic Crossflows Using Kestrel.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-3576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3576
• Johnson, Clarence L. 1954. “Airplane Configurations for High-Speed Flight.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/540231
• Johnson, Clinton T. 1958. Flight Investigation of the Aerodynamic Forces on a Wing-Mounted External-Store Installation on the Douglas D-558-II Research Airplane. NACA-RM-H58B24. NASA. https://ntrs.nasa.gov/citations/19930090009
• Johnson, R. 1975. “The United States Naval Test Pilot School.” In Aircraft Systems and Technology Meeting. AIAA 1975-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1048
• Johnson, E. 1980. “Active Flutter Suppression Control Law Definition via Least Squares Synthesis.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-765
• Johnson, V. 1985. “A Computer-Assisted Process for Supersonic Aircraft Conceptual Design.” In Aircraft Design Systems and Operations Meeting. AIAA 1985-4027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4027
• Johnson, Jeff. 1989. “Flutter Testing of Modern Aircraft.” AIAA Student Journal 27. https://ntrs.nasa.gov/citations/19890063850
• Johnson, James R. 1994. Flight Dynamics Directorate (FDD) Research and Development for Aging Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada361159
• Johnson, Wayne. 2003. Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel. Army Aviation Systems Command. https://ntrs.nasa.gov/citations/20030063077
• Johnson, Wayne. 2004. Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics. AD-A526709. Army Aviation and Missile Command. https://ntrs.nasa.gov/citations/20100033458
• Johnson, Heath, and Graham Candler. 1999. “PSE Analysis of Reacting Hypersonic Boundary Layer Transition.” In 30th Fluid Dynamics Conference. AIAA 1999-3793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3793
• Johnson, Adam, Andrew Doan, Paul Bremner, Joel Sills, and Erica Bruno. n.d. “Assessment of Artemis-1 Pogo Flight Instrumentation System.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20205010358
• Johnson, E. H., C. Hwang, D. S. Joshi, C. A. Harvey, L. T. Huttsell, and M. G. Farmer. 1983. “Adaptive Flutter Suppression, Analysis and Test.” In AGARD Recent Transonic Flutter Invest. for Wings and External Stores. https://ntrs.nasa.gov/citations/19830013948
• Johnson, C. B., W. G. Johnson Jr., and P. G. Stainback. 1986. A Summary of Reynolds Number Effects on Some Recent Tests in the Langley 0.3-Meter Transonic Cryogenic Tunnel. SAE PAPER 861765. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19870045352
• Johnson, H. J., and W. D. Painter. 1976. The Development and Flight Test of an Electronic Integrated Propulsion Control System. Boeing Commercial Airplane Co. https://ntrs.nasa.gov/citations/19770055161
• Johnson, J. B., and D. R. Sandlin. 1984. Comparison of Theoretical and Flight-Measured Local Flow Aerodynamics for a Low-Aspect-Ratio Fin. NASA-CR-176995. NASA. https://ntrs.nasa.gov/citations/19860019448
• Johnson, J. Blair, and Doral R. Sandlin. 1986. Comparison of Theoretical and Flight-Measured Local Flow Aerodynamics for a Low-Aspect-Ratio Fin. NASA-TM-86806. NASA. https://ntrs.nasa.gov/citations/19870006508
• Johnson, Heath, Trevor Seipp, Graham Candler, Heath Johnson, Trevor Seipp, and Graham Candler. 1997. “Numerical Study of Hypersonic Reacting Boundary Layer Transition on Cones.” In 32nd Thermophysics Conference. AIAA 1997-2567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2567
• Johnson, Alan, and Joseph Servidio. 2008. “Ground Support Process Time Refinement for Reusable Launch Vehicle Regeneration Modeling.” In AIAA SPACE 2008 Conference & Exposition. AIAA 2008-7647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7647
• Johnson, Donald, and James Sorenson. 2006. “Flight Experiment Booster Sizing Study.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8117
• Johnson, D., and F. Spaid. 1981. “Measurements of the Boundary Layer and near Wake of a Supercritical Airfoil at Cruise Conditions.” In 14th Fluid and Plasma Dynamics Conference. AIAA 1981-1242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1242
• Johnson, David, Jareth Tosses, and Rylie Anderson. 2025. “Deriving Aircraft Characteristics from Arbitrary Flight Test Data.” In 2025 Regional Student Conferences. AIAA 2025-98509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-98509
• Johnson III, Cagliostro Joseph A., and Dominic. 1970. Experiments with a Supersonic Tube Wind-Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0702806
• Johnson, J. L., Jr., W. A. Newsom, and D. R. Satran. 1980. “Full-Scale Wind-Tunnel Investigation of the Effects of Wing Leading-Edge Modifications on the High Angle-of-Attack Aerodynamic Characteristics of a Low-Wing General Aviation Airplane.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800059132
• Johnston, I. A. (Ian Alexander). n.d. “Simulation of Flow around Hypersonic Blunt-Nosed Vehicles for the Calibration of Air Data Systems.” PhD diss., The University of Queensland. https://doi.org/10.14264/157834
• Johnston, Richard P. 2016. “Flight and Range Characteristics for a Subsonic Advanced Propeller-Driven Blended Wing Body Composite Air Frame Capable of Transporting a 150-Ton Military Cargo.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2016-01-2019
• Johnston, Zachary M., Neal Bitter, Gregory McKiernan, and Bradley M. Wheaton. 2026. “Hypersonic Boundary Layer Transition of BOLT-1B at Flight Conditions.” In AIAA SCITECH 2026 Forum. AIAA 2026-0737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0737
• Johnston, Zachary M., and Graham V. Candler. 2023. “Hypersonic Boundary Layer Transition of the BoLT-2 Flowfield at Flight Conditions, BOLT II Flight Test.” In AIAA SCITECH 2023 Forum. AIAA 2023-0084. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0084
• Johnston, Ian, Peter Jacobs, and Takayuki Shimoda. 1998. “A Study of Flush Air Data System Calibration Using Numerical Simulation.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1606. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1606
• Johnston, Patrick J., and Wallace C. Sawyer. 1988. An Historical Perspective on Hypersonic Aerodynamic Research at the Langley Research Center. AIAA PAPER 88-0230. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880034945
• Jones, Robert T. 1946. Properties of Low-Aspect-Ratio Pointed Wings at Speeds below and above the Speed of Sound. NACA-TN-1032. NASA. https://ntrs.nasa.gov/citations/19930084600
• Jones, Robert J. 1947. Wing Plan Forms for High-Speed Flight. NACA-TR-863. NASA. https://ntrs.nasa.gov/citations/19930091936
• Jones, R. A. 1964. Measured Heat-Transfer and Pressure Distribution on the Apollo Face at a Mach Number of 8 and Estimates for Flight Conditions. NASA-TM-X-919. NASA. https://ntrs.nasa.gov/citations/19690067294
• Jones, Robert. 1970. Flight Test Results of a DAVI Isolated Platform. Defense Technical Information Center. https://doi.org/10.21236/ad0880948
• Jones, Kevin. 2002. “Waverider Design Methods for Non-Conical Shock Geometries.” In 3rd Theoretical Fluid Mechanics Meeting. AIAA 2002-3204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3204
• Jones, Thomas. 2006. Flight Test of the Engine Fuel Schedules of the X-43A Hyper-X Research Vehicles. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20060056094
• Jones, Tom. 2017. “NASAs Quiet Supersonic Aircraft.” In EAA Airventure 2017. https://ntrs.nasa.gov/citations/20170007758
• Jones, C., M. Battersby, and R. Curtis. 1983. “Helicopter Flight Testing in Natural Snow and Ice.” In 2nd Flight Testing Conference. AIAA 1983-2786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2786
• Jones, Daniel S., and Trong T. Bui. 2012. 2011-2012 Dryden Center Innovation Fund End of the Year Report: Altitude-Compensating Rocket Nozzles. DFRC-E-DAA-TN5973. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20130009901
• Jones, Daniel S., Trong T. Bui, and Joseph H. Ruf. 2013. “Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3954. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3954
• Jones, K., F. Dougherty, A. Seebass, and H. Sobieczky. 1993. “Waverider Design for Generalized Shock Geometries.” In 31st Aerospace Sciences Meeting. AIAA 1993-774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-774
• Jones, Ryan, and Stuart Laurence. 2025. “Free-Flight Testing of Ogive Flare Geometry in Hypersonic Wind Tunnel.” In 2025 Regional Student Conferences. AIAA 2025-99832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-99832
• Jones, R. T., and J. W. Nisbet. 1974. “Transonic Transport Wings: Oblique or Swept.” Exxon Air World 27 (1, 19). https://ntrs.nasa.gov/citations/19750034895
• Jones, R. T., and J. W. Nisbet. 1976. “Aeroelastic Stability and Control of an Oblique Wing.” Aeronautical Journal 80. https://ntrs.nasa.gov/citations/19760064883
• Jones, Daniel S., Joseph H. Ruf, Trong T. Bui, Martel Martinez, and Clinton W. St. John. 2014. “Conceptual Design for a Dual-Bell Rocket Nozzle System Using a NASA F-15 Airplane as the Flight Testbed.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20140011268
• Jones, Daniel S., David Tow, and Jason L. Holland. 2024. “Introduction of an Agile Systems Engineering Process to the NASA Armstrong Flight Research Center.” In AIAA SCITECH 2024 Forum. AIAA 2024-2050. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2050
• Jones, Eugene, Sean Townsend, Yair Guy, and Thomas McLaughlin. 2000. “Reduction of the Wave Drag of a Blunt Body by Means of a Standoff Spike.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-268. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-268
• Jones, C., and A. Wilson. 1983. “Flight Testing of Military Ram Air Parachutes.” In 2nd Flight Testing Conference. AIAA 1983-2787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2787
• Jones, Gregory, Chung-Sheng Yao, and Brian Allan. 2006. “Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image Velocimetry.” In 3rd AIAA Flow Control Conference. AIAA 2006-3009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3009
• Jones, Ira P., Jr. 1952. Measurements of Aerodynamic Heating Obtained during Demonstration Flight Tests of the Douglas D-558-II Airplane. NACA-RM-L52I26a. NASA. https://ntrs.nasa.gov/citations/19930087316
• Jordan, J. 1974. “Development and Flight Test Progress of the YF-17.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-941
• Jordan, Thomas, and Roger Bailey. 2008. “NASA Langley’s AirSTAR Testbed: A Subscale Flight Test Capability for Flight Dynamics and Control System Experiments.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6660
• Jordan, Gareth H., and Kenneth Hutchins Jr. 1955. Preliminary Flight-Determined Pressure Distributions over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers. NACA-RM-H55A10. NASA. https://ntrs.nasa.gov/citations/19930088623
• Jordan, Thomas L., William M. Langford, and Jeffrey S. Hill. 2005. Airborne Subscale Transport Aircraft Research Testbed: Aircraft Model Development. AIAA Paper 2005-6432. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050232785
• Jorgensen, L. H., L. L. Levy Jr., and W. P. Nelms Jr. 1971. Preliminary Study of Advanced Hypersonic Research Aircraft. NASA-TM-X-2222. NASA. https://ntrs.nasa.gov/citations/19710008892
• Jorris, Timothy R. 2014. “Recent and Ongoing Hypersonic, Space Transit, and Space Launch Flight Tests.” In AIAA Flight Testing Conference. AIAA 2014-2579. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2579
• Jorris, Timothy, Nathan Lehman, William Gray, and Jay Kemper. 2011. “Unmanned Air Vehicle Flight Test Using a Manned Surrogate Aircraft.” In Infotech@Aerospace 2011. AIAA 2011-1529. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1529
• Jouannet, Christopher, Patrick Berry, Tomas Melin, Kristian Amadori, David Lundström, and Ingo Staack. 2012. “Subscale Flight Testing Used in Conceptual Design.” Aircraft Engineering and Aerospace Technology 84 (3): 192–99. https://doi.org/10.1108/00022661211222058
• Juhasz, Ondrej, Hong Xin, US Army CCDC AvMC, and Mark Tischler. 2020. “Inflow Based Flight Dynamics Modeling Improvements for the Sikorsky X2 Technology Demonstrator.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16291
• Jun, Tan Kai, Mohammad Yazdi Harmin, and Fairuz I. Romli. 2014. “Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation.” Applied Mechanics and Materials 629: 182–88. https://doi.org/10.4028/www.scientific.net/amm.629.182
• Junaid R, Mohammed, and Laila Beebi M. 2015. “Non-Linear Adaptive Control on Reusable Launch Vehicle Due to Actuator Stuck.” International Journal of Scientific Engineering and Research 3 (8): 45–48. https://doi.org/10.70729/ijser15399
• June, Jason, Alexandra M. Hickey, and Yueping Guo. 2025. “Local Flow Effects on Noise Prediction of Transonic Truss-Braced Wing Landing Gear.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3884
• June, Jason, Eric Nesbitt, Douglas M. Nark, and Michael G. Jones. 2024. “Comparison of Inlet Broadband Acoustic Liner Predictions to Quiet Technology Demonstrator 3 Flight Data.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3371
• June, Jason, Russell H. Thomas, and Yueping Guo. 2022. “System Noise Technology Roadmaps for a Transonic Truss-Braced Wing and Peer Conventional Configuration.” In 28th AIAA/CEAS Aeroacoustics 2022 Conference. AIAA 2022-3049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3049
• Jung, Yong, and James Baeder. 2019. “Uncertainty Quantification for Laminar-Turbulent Transition on Airfoil and Fuselage.” In Proceedings of the Vertical Flight Society 75th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0075-2019-14523
• Jung, Ki-Wook, Hyeonjae Kim, Min-Jea Tahk, and Chang-Hun Lee. 2025. “Feedback Landing Guidance for Reusable Launch Vehicle in Atmosphere Based on Homing Guidance.” In IAF Astrodynamics Symposium. International Astronautical Federation (IAF). https://doi.org/10.52202/083087-0113
• Jung, Dongwoo, and Mark Lowenberg. 2005. “Stability and Control Assessment of a Blended-Wing-Body Airliner Configuration.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6123
• Jung, W., and H.-G. Reimerdes. 2003. “Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-44866-2_10
• “Jupiter Probe Heat-Shield Configuration Optimization.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0321.0344
• Justin James Matt, Haiyang Chao, Mosarruf H. Shawon, Benjamin C. Svoboda, and Steven G. Hagerott. 2025. “System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data.” Preprint, . https://doi.org/10.31224/4308
• Jutte, Christine V., Brian Mason, and Robert E. Bartels. 2024. “Simplified Applied Loads of a Transonic Truss-Braced Wing Derived from Computational Fluid Dynamics.” In AIAA SCITECH 2024 Forum. AIAA 2024-2811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2811
• Kachadourian, G., R. L. Goldman, and D. M. Roha. 1975. “Flight Flutter Testing of the P6M.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003019
• Kacik, Dominika, and Tomasz Goetzendorf-Grabowski. 2025. “Review of the Advantages and Challenges of Strut-Braced and Truss-Braced Aircraft.” Aircraft Engineering and Aerospace Technology 97 (9): 1020–28. https://doi.org/10.1108/aeat-02-2025-0045
• Kahre, Karl T. 1987. “The National Aerospace Plane: A Political Overview.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/872529
• Kakojima, Hideaki, and Kiyoshi Akinaga. 2005. Programmable Flight Control Type Model Airplane for Survey. SAE International. https://doi.org/10.4271/2005-08-0284
• Kalaji, Ahmad T. 2023. “Design and Experimental Studies of Flexible Trailing Edge for Variable Camber Morphing Wing.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14653803.v1
• Kalemaris, Stanley G. 1980. “Feasibility of Forward: Swept Wing Technology for V/STOL Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/801176
• Kaletka, Juergen, and Kuang-Hua Fu. 1993. “Frequency-Domain Identification of Unstable Systems Using X-31A Aircraft Flight Test Data.” In Flight Simulation and Technologies. AIAA 1993-3635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3635
• Kalkhoran, Iraj M., and M. V. Otugen. 1994. Research Instrumentation for Polytechnic University’s Supersonic Wind Tunnel Facility. Defense Technical Information Center. https://doi.org/10.21236/ada299229
• Kamal, Ashraf, Amgad M. Aly, and Ahmed Elshabka. 2015. “Tuning of Airplane Flight Dynamic Model Using Flight Testing.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-1595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1595
• Kamali, Give, and Allan D. Pierce. 1972. “Examination of the Variances in Sonic Boom Waveforms Recorded during Flight Tests.” Journal of the Acoustical Society of America 51 (1A_Supplement): 94–94. https://doi.org/10.1121/1.1981712
• Kamalov, Firuz. 2017. “Expected Information Gain.” Applied Mathematical Sciences 11: 2377–82. https://doi.org/10.12988/ams.2017.7260
• Kambampati, Sandilya, Edward Smith, Mark Maughmer, and Taylor Hoover. 2016. “Multidisciplinary Design and Optimization for High Speed, High Efficiency Tiltrotors with Wing Extensions and Winglets.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11440
• Kamerman, C., L. Sutherland, and K. Plotkin. 1986. Exploratory Study of the Potential Effects of Exposure to Sonic Boom on Human Health. Volume 1. Sonic Boom Environment. Defense Technical Information Center. https://doi.org/10.21236/ada170986
• Kamiya, N., T. Nishi, and T. Itoh. 1978. “Design and Test of Transonic Airfoils under Consideration of Drag Divergence Mach Number.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1221
• Kanamori, Masashi, Shinya Koganezawa, Hiroaki Ishikawa, Atsushi Ueno, Yusuke Naka, and Yoshikazu Makino. 2025. “Numerical Analyses of Sonic Boom Waveforms in Flight Test of JAXA’s Robust En-Route Sonic-Boom Mitigation Technology Demonstration (Re-BooT) Project.” Journal of the Acoustical Society of America 158 (4_Supplement): A118-A118. https://doi.org/10.1121/10.0040315
• Kanamori, Masashi, Takashi Takahashi, Yusuke Naka, Yoshikazu Makino, Hidemi Takahashi, and Hiroaki Ishikawa. 2017. “Numerical Evauation of Effect of Atmospheric Turbulence on Sonic Boom Observed in D-SEND#2 Flight Test.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0278
• Kandil, Hamdy, Osama Kandil, and C. Liu. 1993. “Supersonic Vortex Breakdown over a Delta Wing in Transonic Flow.” In 11th Applied Aerodynamics Conference. AIAA 1993-3472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3472
• Kandil, Osama, Nitin Khasdeo, and Isik Ozcer. 2006. “Sonic Boom Mitigation through Thickness , Camber and Nose Angle Optimizations for a Delta Wing.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6636
• Kandil, O., and R. You. 2002. “Transonic and Supersonic, High Alpha Flow Prediction for SC-X Space Vehicle.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-849
• Kane, E. 1973. “A Study to Determine the Feasibility of a Low Sonic Boom Supersonic Transport.” In Aeroacoustics Conference. AIAA 1973-1035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1035
• Kaneko, Kento, Akira Oyama, and Aiko Yakeno. 2024. “Viscous Drag Reduction Effect of Riblet at Cruising Speed of Transonic Aircraft.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3588
• Kang, Namuk, James Whidborne, Linghai Lu, and Julien Enconniere. 2023b. “Scheduled Flight Control System of Tilt-Rotor VTOL PAV.” In AIAA SCITECH 2023 Forum. AIAA 2023-1530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1530
• Kang, Hao, Hyeonsoo Yeo, Jinwei Shen, Andrew Kreshock, Robert Thornburgh, and Matthew Floros. 2023a. “Correlation of Tiltrotor Aeroelastic Stability Wind Tunnel Test.” In Proceedings of the Vertical Flight Society 79th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0079-2023-18047
• Kannan, Keerthana, Anjan Chakrabarty, Joshua Baculi, Evan Kawamura, Wendy Holforty, and Corey Ippolito. n.d. “Comparison of Visual and LiDAR SLAM Algorithms Using NASA Flight Test Data.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20220017949
• Kannan, Keerthana, Corey Ippolito, and Wendy Holforty. 2024. “Flight Test Configuration of the Sensor Payload and the Ground Nodes in Distributed Sensing Frameworks.” In AIAA SciTech Conference. https://ntrs.nasa.gov/citations/20230017576
• Kannemans, H. 1995. “Flight Testing of a Wing Deflection Measurement Method.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3434
• Kantor, Samuel R., and Larry J. Cliatt II. 2017. A Study of Reflected Sonic Booms Using Airborne Measurements. DFRC-E-DAA-TN38565. NASA Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20170000397
• Kantrowitz, Arthur, and Coleman Dup Donaldson. 1945. Preliminary Investigation of Supersonic Diffusers. NACA-WR-L-713. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930093667
• Kao, P., and W. Anderson. 1981. “Flight Test Diagnostics Using Radar Cross-Section Measurements.” In 1st Flight Test Conference. AIAA 1981-2419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2419
• Kapania, Rakesh K., Joseph A. Schetz, and Wei Zhao. 2022. “Novel Airplane Design Configurations Using Truss-Braced Wing and Nature Stiffening Members.” In AIAA AVIATION 2022 Forum. AIAA 2022-3785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3785
• Kaplan, Marshall H. 2002. “Reusable Launch Vehicle Facts and Fantasies.” In AIP Conference Proceedings, vol. 608. AIP. https://doi.org/10.1063/1.1449851
• Karabacak, Mustafa, and Onder Turan. 2023. “Inverted Brayton Cycle Engine Optimization for Hypersonic Flight.” Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering 24 (4): 257–74. https://doi.org/10.18038/estubtda.1270986
• Karanian, A., and C. Kepler. 1965. “Experimental Hypersonic Inlet Investigation with Application to Dual-Mode Scramjet.” In Propulsion Joint Specialist Conference. AIAA 1965-588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-588
• Karel, G. 1967. “Near Term Reusable Rocket Launch Vehicle Concepts.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/670378
• Karimi Kelayeh, Ruhollah, and Mohammad Hasan Djavareshkian. 2024. “Aerodynamic Assessment of a Control Strategy Based on Twist Morphing Wing in a Flying Wing Aircraft.” Journal of Aerospace Engineering 37 (1): 04023087. https://doi.org/10.1061/jaeeez.aseng-5073
• Karl, Sebastian, Klaus Hannemann, Johan Steelant, and Andreas Mack. 2006. “CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8041. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8041
• Karlgaard, Christopher D., John G. Martin, Paul V. Tartabini, and Mark N. Thornblom. 2005. “Hyper-X Mach 10 Trajectory Reconstruction.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20050232845
• Karlgaard, Christopher D., Clara O’Farrell, Jason M. Ginn, and John W. Van Norman. 2016. “Supersonic Flight Dynamics Test 2: Trajectory, Atmosphere, and Aerodynamics Reconstruction.” In American Astronautical Society. https://ntrs.nasa.gov/citations/20160007703
• Karlgaard, Chris D., and Mark Schoenenberger. 2017. “Planetary Probe Entry Atmosphere Estimation Using Synthetic Air Data System.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0470. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0470
• Karlgaard, Chris D., Tyler D. Stoffel, Todd White, and Thomas K. West. 2022. “Data Fusion of in-Flight Aerothermodynamic Heating Measurements Using Kalman Filtering.” In AIAA AVIATION 2022 Forum. AIAA 2022-3794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3794
• Karlgaard, Christopher D., Tyler D. Stoffel, Todd R. White, and Thomas K. West IV. n.d. “Data Fusion of in-Flight Aerothermodynamic Heating Measurements Using Kalman Filtering.” In AIAA Aviation Forum. https://ntrs.nasa.gov/citations/20220006196
• Karlgaard, Christopher, Paul Tartabini, Robert Blanchard, Michael Kirsch, and Matthew Toniolo. 2004. “Hyper-X Post-Flight Trajectory Reconstruction.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4829. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4829
• Karlgaard, Chris D., Jake Tynis, and Clara O’Farrell. 2018. “Reconstruction of the Advanced Supersonic Parachute Inflation Research Experiment Sounding Rocket Flight Test.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3624. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3624
• Karns, Alex M., John A. Strike, Rajan Kumar, and Benjamin Dickinson. 2017. “Air Data System Calibration Methodology over Cylindrical Bodies.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0333
• Karpel, M. 1980. “Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-766
• Kass, G. 1970. “Improved Airplane Performance through Advanced Flight Control Systemdesign.” In Meeting on the Prospects for Improvement in Efficiency of Flight. AIAA 1970-875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-875
• Katz, H., G. F. Foppe, and D. T. Grossman. 1976. “F-15 Flight Flutter Test Program.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014093
• Kauffman, William M. 1945. Correlation of Wind-Tunnel Predictions with Flight Tests of a Twin-Engine Airplane I: Longitudinal-Stability and -Control Characteristics. NACA-MR-A5D04. NASA. https://ntrs.nasa.gov/citations/19930092584
• Kaul, Upender K., and Nhan T. Nguyen. 2014. “Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2444
• Kaul, Upender K., and Nhan T. Nguyen. 2015. “A 3-D Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2422
• Kaul, Upender K., and Nhan T. Nguyen. 2018. “Drag Characterization Study of Variable Camber Continuous Trailing Edge Flap.” Journal of Fluids Engineering 140 (10): 101108. https://doi.org/10.1115/1.4040070
• Kaul, Upender K., and Nhan T. Nguyen. 2019. “Extending a Correction Method for Unsteady Transonic Aerodynamics to Variable Camber Continuous Trailing Edge Flap.” In AIAA Aviation 2019 Forum. AIAA 2019-3157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3157
• Kawai, Soshi, and Kozo Fujii. 2005. “Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows.” In 35th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2005-5156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5156
• Kawakami, Hiroki, Takeshi Takatoya, and Hiroaki Ishikawa. 2007. “Static Aeroelastic Analysis of Supersonic Experimental Airplane NEXST-1 Flight Test.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4174
• Kawakami, Hiroki, Takeshi Takatoya, and Hiroaki Ishikawa. 2008. “Static Aeroelastic Analysis of Experimental SST NEXST-1 Flight Test Using Wing-Body Configuration Model.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6419
• Kaygan, Erdoğan, and Ceren Ulusoy. 2018. “Effectiveness of Twist Morphing Wing on Aerodynamic Performance and Control of an Aircraft.” Journal of Aviation 2 (2): 77–86. https://doi.org/10.30518/jav.482507
• Kayran, Altan. 2004. “Aeroelastic Stability of a Transport Aircraft with Wing Mounted Store Suspension: Part II — Flight Test.” In Volume 2. ASMEDC. https://doi.org/10.1115/esda2004-58468
• Kayran, Altan. 2007. “Flight Flutter Testing and Aeroelastic Stability of Aircraft.” Aircraft Engineering and Aerospace Technology 79 (2): 150–62. https://doi.org/10.1108/00022660710732707
• Kayten, Gerald G., and William Koven. 1945. Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas a-26 Airplane. NACA-TR-816. NASA. https://ntrs.nasa.gov/citations/19930092456
• Keener, E. 1984. “Computational-Experimental Pressure Distributions on a Transonic, Low-Aspect-Ratio Wing.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2092
• Kehlet, Alan B. 1954. Flight Results from a 1/10-Scale Rocket Model of the Lockheed XF-104 Airplane at Transonic Mach Numbers. NACA-RM-SL54E14. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023148
• Kehlet, Alan B., and Herbert G. Patterson. 1959. Free-Flight Test of a Technique for Inflating an NASA 12-Foot-Diameter Sphere at High Altitudes. NASA-MEMO-2-5-59L. NASA. https://ntrs.nasa.gov/citations/19980232004
• Kehoe, M. W. 1982. “KC-135A Winglet Flight Flutter Program.” In NASA. Dryden Flight Research Facility KC-135 Winglet Program Rev.. https://ntrs.nasa.gov/citations/19840019624
• Kehoe, M. W. 1984. Highly Maneuverable Aircraft Technology (HiMAT) Flight-Flutter Test Program. NASA-TM-84907. NASA. https://ntrs.nasa.gov/citations/19860017818
• Kehoe, Michael W. 1987a. “Aircraft Ground Vibration Testing at NASA Ames-Dryden Flight Research Facility.” In International Modal Analysis Conference. https://ntrs.nasa.gov/citations/19880063604
• Kehoe, Michael W. 1987b. Flutter Clearance of the F-14 Variable-Sweep Transition Flight Experiment Airplane, Phase 1. NASA-TM-88287. NASA. https://ntrs.nasa.gov/citations/19870018230
• Kehoe, Michael. 1988. “Aircraft Flight Flutter Testing at the NASA Ames-Dryden Flight Research Facility.” In 4th Flight Test Conference. AIAA 1988-2075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2075
• Kehoe, Michael W. 1995. “A Historical Overview of Flight Flutter Testing.” In AGARD Structures and Materials Panel Meeting. https://ntrs.nasa.gov/citations/19960004074
• Keidel, Dominic, Urban Fasel, Giulio Molinari, and Paolo Ermanni. 2019. “Flight Control Optimization and Wind Tunnel Validation of a Morphing Flying Wing.” In AIAA Scitech 2019 Forum. AIAA 2019-0854. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0854
• Keisler, Jeffrey. 2004. “Value of Information in Portfolio Decision Analysis.” Decision Analysis 1 (3): 177–89. https://doi.org/10.1287/deca.1040.0023
• Keller, Jeffrey D., Robert M. McKillip Jr., Joseph Horn, and Soohyeon Lee. 2026. “Development and Testing of a Subscale eVTOL Flight Vehicle for Stability, Control and Disturbance Response Characteristics.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0225
• Kelley, H. L., and J. Scheiman. 1963. Comparison of Flight Measured Helicopter Rotor Blade Chordwise Pressure Distributions and Two-Dimensional Airfoil Characteristics. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630011950
• Kelley, H. L., and J. Scheiman. 1967. Cmparison of Flight-Measured Helicopter Rotor-Blade Chordwise Pressure Distributions with Static Two-Dimensional Airfoil Characteristics. NASA-TN-D-3936. NASA. https://ntrs.nasa.gov/citations/19670014489
• Kelly, Ray D. 1964. “Supersonic Transport Development Program.” Journal of the Aero-Space Transport Division 90 (2): 1–8. https://doi.org/10.1061/jatdaz.0000024
• Kelly, R. 1974. “System Design and Flight Test Results of the Bendix/Bell MLS Category II/III Elevation Approach Guidance Function.” In Mechanics and Control of Flight Conference. AIAA 1974-909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-909
• Kelly, James. 1988. “Stability Flight Test Verification by Modal Separation.” In 4th Flight Test Conference. AIAA 1988-2129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2129
• Kelly, Seth, Tausif Jamal, William Millholen, and Craig Hunter. 2025. “Surface Flow Visualization via Tuft-Tracking on Transonic Truss-Braced Wing Configuration.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3092
• Kelly, Thomas C., and Robert S. Osborne. 1954. Effects of Fuselage Modifications on the Drag Characteristics of a 1/20-Scale Model of the Convair F-102 Airplane at Transonic Speeds. NACA-RM-SL54K18a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028506
• Kelly, J. R., and M. M. Winston. 1965. Stability Characteristics of a Tandem-Rotor Transport Helicopter as Determined by Flight Test. NASA-TN-D-2847. NASA. https://ntrs.nasa.gov/citations/19650015947
• Kelso, J. 1993. “Boresight Error Slope Predictions versus Flight Test Results in a Hypersonic Flow Field.” In Annual Interceptor Technology Conference. AIAA 1993-2688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2688
• Kemmerly, Guy T. 1990. Dynamic Ground-Effect Measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) Configuration. NASA-TP-3000. NASA. https://ntrs.nasa.gov/citations/19900013215
• Kemp, William B., Jr., and Thomas J. King Jr. 1956. Wind-Tunnel Measurements of Wing Buffeting on 1/16-Scale Model of Douglas D-558-II Research Airplane. NACA-RM-L56G31. NASA. https://ntrs.nasa.gov/citations/19930089459
• Kempel, R. W. 1971a. Analysis of a Coupled Roll Spiral Mode, Pilot Induced Oscillation Experienced with the M-2F2 Lifting Body. NASA-TN-D-6496. NASA. https://ntrs.nasa.gov/citations/19710023831
• Kempel, R. 1971b. “Assessment of Lifting Body Vehicle Handling Qualities.” In Space Shuttle Development Testing and Operations Conference. AIAA 1971-310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-310
• Kempel, Robert W., Walter E. McNeill, and Trindel A. Maine. 1988. Oblique-Wing Research Airplane Motion Simulation with Decoupling Control Laws. AIAA PAPER 88-0402. PRC Kentron, Inc. https://ntrs.nasa.gov/citations/19880035069
• Kempel, Robert W., and Weneth D. Painter. 1993. Development and Flight Testing of the HL-10 Lifting Body. ISSN: 0742-3705. PRC Inc. https://ntrs.nasa.gov/citations/19950059273
• Kempel, Robert, and Weneth Painter. 1994. “Development and Flight Testing of the HL-10 Lifting Body.” In Biennial Flight Test Conference. AIAA 1994-2180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2180
• Kempel, Robert W., Weneth D. Painter, and Milton O. Thompson. 1994. Developing and Flight Testing the HL-10 Lifting Body: A Precursor to the Space Shuttle. NASA-RP-1332. NASA. https://ntrs.nasa.gov/citations/19940030197
• Kempel, Robert W., Paul W. Phillips, C. Gordon Fullerton, and John J. Bresina. 1989. AFTI/F-111 Airplane Mission Adaptive Wing Operational Flight Evaluation Technique Using Uplinked Pilot Command Cues. PRC Systems Services, Aerospace Technologies Div., Edwards. https://ntrs.nasa.gov/citations/19910036370
• Kempel, R. W., and R. C. Thompson. 1971. Flight-Determined Aerodynamic Stability and Control Derivatives of the M2-F2 Lifting Body Vehicle at Subsonic Speeds. NASA-TM-X-2413. NASA. https://ntrs.nasa.gov/citations/19720004251
• Kemper, E. H., and D. J. Renselaer. 1969. CV-7A Transport Aircraft Modification to Provide an Augmentor-Wing Jet STOL Research Aircraft. Volume 1: Design Study. NASA-CR-73321. NASA. https://ntrs.nasa.gov/citations/19690015913
• Kendall, J. 1974. “Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary Layer Transition.” In 12th Aerospace Sciences Meeting. AIAA 1974-133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-133
• Kennamer, Noble, Steven Walton, and Alexander Ihler. 2023. “Design Amortization for Bayesian Optimal Experimental Design.” Proceedings of the AAAI Conference on Artificial Intelligence 37 (7): 8220–27. https://doi.org/10.1609/aaai.v37i7.25992
• Kennedy, P. 1986. “Combined Test Force Operations at the Air Force Flight Test Center.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9739
• Kenyon, R. E. 1974. Weapon System Costing Methodology for Aircraft Airframes and Basic Structures. Volume 3. Cost Data Base. Defense Technical Information Center. https://doi.org/10.21236/ada000399
• Kepler. 1980. “The Similitude Method.” In Fundamental Studies in Engineering. Elsevier. https://doi.org/10.1016/b978-0-444-99780-7.50008-2
• Kerr, Ryan. 2025. “Blended-Wing Body Airplane Tradeoffs: H2 vs. Jet Fuel.” In Proceedings of the Vertical Flight Society Fourth Annual H2-Aero Symposium - Long Beach, California, April 2025. The Vertical Flight Society. https://doi.org/10.4050/sm_h2_2025-5413
• Kertesz, T. 1965. “Correlation between Polaris Ground and Flight Test Shock and Vibration Data.” In Flight Testing Conference. AIAA 1965-206. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-206
• Keshmiri, Shahriar, Richard Colgren, and Maj Mirmirani. 2006. “Trajectory Optimization for a Generic Hypersonic Vehicle.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8157
• “Key Ideas in Experimental Design.” 2016. In Experimental Design for Laboratory Biologists. Cambridge University Press. https://doi.org/10.1017/9781139696647.003
• Khalid, Mahmood. 2023. “Performance of a Refurbished Unmanned Combat Air Vehicle Model with Trailing Edge Blowing.” Journal of King Abdulaziz University: Engineering Sciences 33 (1): 65–82. https://doi.org/10.4197/eng.33-1.5
• Khalid, S., and M. Faherty. 1990. “Propulsion System Flight Test Analysis Using Modeling Techniques.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3288
• Khambaswadkar, Ishaan. 2024. “Exploring the Challenges Faced in Developing Hypersonic Flight.” Preprint, . https://doi.org/10.58445/rars.2094
• Khamlak, Maryna. 2026. “Methodology for Ensuring Safety and Operational Reliability of Reusable Launch Vehicle Composite Structures under High-Intensity Vibroacoustic Loads.” American Journal of Engineering and Technology 08 (06): 01–61. https://doi.org/10.37547/tajet/book-26-01
• Khan, Kamrul Hasan, Rakesh K. Kapania, and Joseph A. Schetz. 2023. “Deep Learning Based Transonic Flutter Prediction Model for Multidisciplinary Design Optimization of Medium Range Truss Braced Wing Aircraft.” In AIAA AVIATION 2023 Forum. AIAA 2023-3944. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3944
• Khlebnikov, V. S. 1990. “Aerodynamic Drag of a Pair of Bodies in Transonic and Supersonic Flow.” Fluid Dynamics 25 (3): 458–62. https://doi.org/10.1007/bf01049830
• Khodja, M. R., M. D. Prange, and H. A. Djikpesse. 2010. “Guided Bayesian Optimal Experimental Design.” Inverse Problems 26 (5): 055008. https://doi.org/10.1088/0266-5611/26/5/055008
• Khoshlahjeh, Maryam, Farhan Gandhi, and Steven Webster. 2011. “Extendable Chord Rotors for Helicopter Envelope Expansion and Performance Improvement.” In Proceedings of the Vertical Flight Society 67th Annual Forum and Technology Display - Forum 67 - Virginia Beach, Virginia 2011. The Vertical Flight Society. https://doi.org/10.4050/vfs-f67-000362
• Kianvashrad, N., and D. Knight. 2017. “Simulation of Hypersonic Shock Wave: Laminar Boundary Layer Interactions.” In Progress in Flight Physics, edited by D. Knight, Y. Bondar, I. Lipatov, P. Reijasse. EDP Sciences. https://doi.org/10.1051/eucass/2016090409
• Kidd, R. 1965. “Application of Statistical Experimental Design Techniques to Flight-Test Programs.” In Flight Testing Conference. AIAA 1965-221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-221
• Kidd, James. 1988. “Investigation of the Effect of Variable Tail Dihedral on Airplane Stability and Control.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4335
• Kiefer, Dennis, and Jeffrey Calvert. 1992. “Developmental Evaluation of a Centrifuge Flight Simulator as an Enhanced Maneuverability Flying Qualities Tool.” In Flight Simulation Technologies Conference. AIAA 1992-4157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4157
• Kiel, Georg. 1939. Measurement of the True Dynamic and Static Pressures in Flight. NACA-TM-913. NASA. https://ntrs.nasa.gov/citations/19930094503
• Kilgore, Robert A. 1982. “The Cryogenic Wind Tunnel for High Reynolds Number Testing.” In Proceedings of the Ninth International Cryogenic Engineering Conference, Kobe, Japan, 11–14 May 1982. Elsevier. https://doi.org/10.1016/b978-0-408-01252-2.50096-0
• Kilgore, R., J. Adcock, and E. Ray. 1974. “Flight Simulation Characteristics of the Langley High Reynolds Number Cryogenic Transonic Tunnel.” In 12th Aerospace Sciences Meeting. AIAA 1974-80. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-80
• Kilmer, Frank G., and Joel R. Sklaroff. 1973. “Redundant System Design and Flight Test Evaluation for the Tags Digital Control System.” In Proceedings of the Vertical Flight Society Forum 29 - Washington, D.C. 1973. The Vertical Flight Society. https://doi.org/10.4050/vfs-f29-012
• Kim, Sungwook. n.d. “Optimal Experimental Design under a New Multivariate Weibull Regression Function.” PhD diss., University of Missouri–Columbia. https://doi.org/10.32469/10355/44178
• Kim, Sungwan. 1995. “MINIMAL TIME CHANGE DETECTION ALGORITHM FOR RECONFIGURABLE CONTROL SYSTEM AND APPLICATION TO AEROSPACE**This Work Was Supported by NASA Ames Research Center, DFRF through UCLA Flight Systems Research Center(FSRC), Grant Number NCC 2-374.” In Automatic Control in Aerospace 1994 (Aerospace Control ‘94). Elsevier. https://doi.org/10.1016/b978-0-08-042238-1.50045-8
• Kim, Ki C. 2004. Analytical Calculation of Helicopter Main Rotor Blade Flight Loads in Hover and Forward Flight. Defense Technical Information Center. https://doi.org/10.21236/ada423149
• Kim, Taehyoun. 2024. “Progressive Flutter Prediction Using Flight Data with Limited Sensors and Actuators.” In AIAA SCITECH 2024 Forum. AIAA 2024-0194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0194
• Kim, Sun-Kyoung, Chang-Soo Jeon, Hong-Gye Sung, Jong-Ryul Byen, and Hyun-Gull Yoon. 2010. “Performance Load Balancing and Sensitivity Analysis of Ramjet/Scramjet for Dual-Combustion/Dual-Mode Ramjet Engine Part II. Performance Sensitivity.” Journal of the Korean Society for Aeronautical & Space Sciences 38 (6): 596–604. https://doi.org/10.5139/jksas.2010.38.6.596
• Kim, Dong Hyun, Hyun Jung Kim, Il Kwon Oh, and Seok Soon Lee. 2007. “Nonlinear Aeroelastic Characteristics of a Laminated Composite Wing Considering Compressible Shock Wave Effects.” In Key Engineering Materials. Trans Tech Publications Ltd. https://doi.org/10.4028/0-87849-427-8.481
• Kim, Eung-tai, Yeong-cheol Kim, Kie-jeong Seong, Myoung-shin Hwang, and Hee-bong Eun. 2003. “A Study on the Parameter Estimation for General Aviation Canard Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5540
• Kim, WonGi, JaeYoul Ko, and Jaemyung Ahn. 2026. “Design Space Exploration of a Reusable Launch Vehicle through Integrated Stage-Mission Optimization.” In AIAA SCITECH 2026 Forum. AIAA 2026-1707. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1707
• Kim, Joshua P., and Donald L. Kunz. 2016. “Flying Qualities Evaluation of an Unmanned Aircraft Using JSBSim.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3542
• Kim, Duk-Min, and Hyoung Jin Lee. 2025. “Experimental Visualization of Hypersonic Boundary Layer Transition.” In AIAA SCITECH 2025 Forum. AIAA 2025-0558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0558
• Kim, Hyun D., Aaron T. Perry, and Phillip J. Ansell. 2018b. “A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology.” In 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. AIAA 2018-4998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4998
• Kim, B., M. Rasmussen, and M. Jischke. 1982. “Optimization of Waverider Configurations Generated from Axisymmetricconical Flows.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1299. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1299
• Kim, Y., and G. Winchenbach. 1985. “The Roll Motion of a Wraparound Fin Configuration at Subsonic and Transonic Mach Numbers.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1777
• Kim, Chong-sup, Inseok Yang, Gi-oak Koh, and Byung-soo Kim. 2018a. “Development of the Model-/Sensor-Based Nonlinear Dynamic Inversion Control Technique for Highly Maneuverability Fighter.” Journal of Institute of Control, Robotics and Systems 24 (7): 639–54. https://doi.org/10.5302/j.icros.2018.18.0049
• Kimathi, Stephan, and Bela Lantos. 2024. “An Extended Approach to UAV Parameter Estimation Using Simulated Flight Data.” Acta Polytechnica Hungarica 21 (2): 291–307. https://doi.org/10.12700/aph.21.2.2024.2.16
• Kimberlin, Ralph, and U. Solies. 1992. “Graduate Education in Flight Testing.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4069
• Kimmel, Roger L. 1999. “Trends in Hypersonic Boundary Layer Stability and Transition Research.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57514
• Kimmel, Roger. 2003. “Aspects of Hypersonic Boundary Layer Transition Control.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-772
• Kimmel, Roger, David Adamczak, Ryan Gosse, Karen Berger, and Shann Rufer. 2011. Ground Test and Computation of Boundary Layer Transition on the Hypersonic International Flight Research and Experimentation (HIFiRE)-5 Vehicle. Defense Technical Information Center. https://doi.org/10.21236/ada548272
• Kimmel, Roger, Sivaram Gogineni, Igor Adamovich, J. William Rich, and Xiaolin Zhong. 2003. “Update on MHD Control of Supersonic / Hypersonic Boundary-Layer Transition.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-6924. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6924
• Kimmel, Roger L., and J. Poggie. 1997. Three-Dimensional Hypersonic Boundary Layer Stability and Transition. Defense Technical Information Center. https://doi.org/10.21236/ada417303
• Kimmel, Roger, Stephen Schwoerke, and Mark Klein. 1996. “Three-Dimensional Hypersonic Laminar Boundary Layer Computations for Transition Experiment Design.” In Fluid Dynamics Conference. AIAA 1996-2080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2080
• Kimmerly, Eddie. n.d. “Scramjet Modeling Employing Boundary Layer Combustion of Hydrogen to Reduce Drag.” PhD diss., The University of Queensland. https://doi.org/10.14264/345542
• Kimura, Hiroyuki, Kazuhide Mizobata, and Hiromu Sugiyama. 2003. “Flight Performance Analysis of the Flight Demonstrator for the ATREX Engine.” Proceedings of Conference of Hokkaido Branch 2003.43 (0): 152–53. https://doi.org/10.1299/jsmehokkaido.2003.43.152
• King, L., and D. Johnson. 1983. “Comparison of Supercritical Airfoil Flow Calculations with Wind-Tunnel Results.” In 16th Fluid and Plasmadynamics Conference. AIAA 1983-1688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1688
• Kinsey, D., and F. Eastep. 1988. “Navier-Stokes Solution for a Thick Supercritical Airfoil with Strongshocks and Massively Separated Flow.” In 26th Aerospace Sciences Meeting. AIAA 1988-706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-706
• Kirby, Robert H. 1957. “Stability and Control of Propeller-Driven Transport VTOL Airplanes.” In Proceedings of the Vertical Flight Society Forum 13 - Washington, D.C. 1957. The Vertical Flight Society. https://doi.org/10.4050/vfs-f13-007
• Kirby, Robert H. 1960. “Compilation of Papers Summarizing Some Recent NASA Research on Manned Military Aircraft. I. VTOL Aircraft: State of the Art.” In Compilation of Papers Summarizing Some Recent NASA Research on Manned Military Aircraft. https://ntrs.nasa.gov/citations/19670023742
• Kirk, Lindsay C. 2016. Boundary Layer Transition during the Orion Exploration Flight Test 1 (EFT-1). JSC-CN-34666. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20150020957
• Kirk, Lindsay, Randolph P. Lillard, Joseph Olejniczak, and Hideyuki Tanno. 2015. “Boundary Layer Transition and Trip Effectiveness on an Apollo Capsule in the JAXA High Enthalpy Shock Tunnel (HIEST) Facility.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0209
• Kirk, Donn B., and Robert J. Miller. 1962. Free-Flight Tests of Fifth-Stage Scout Entry Vehicle at Mach Numbers of 5 and 17. NASA-TN-D-1425. NASA. https://ntrs.nasa.gov/citations/19620006855
• Kirkham, F., L. Jackson, and J. Weidner. 1974. “The Case for a High-Speed Research Airplane: Results from an in-House Study.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-988. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-988
• Kirkham, F. S., R. A. Jones, M. L. Buck, and W. P. Zima. 1975a. “Joint USAF/NASA Hypersonic Research Aircraft Study.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750055459
• Kirsten, P. 1985. “Development of a Fuel-Saving Flight Control System for the Space Shuttle Based on Flight Experience.” In Aircraft Design Systems and Operations Meeting. AIAA 1985-4040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4040
• Kirsten, P. W., and L. G. Ash. 1974. “A Comparison of Two Methods of Extracting Stability Derivatives from Flight Test Data.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017460
• Kitaplioglu, Cahit, M. McCluer, C. W. Acree Jr., and William Warmbrodt. 1997. Comparison of Full-Scale XV-15 Wind Tunnel and in-Flight Blade-Vortex Interaction Noise. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020040964
• Klausmeyer, Steven. 2004. “Drag, Lift, and Moment Estimates of Transonic Aircraft Using the Navier-Stokes Equations.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-553
• Klausmeyer, Steve M. 2026. “Estimation of Static and Dynamic Stability Derivatives Using FUN3D with Wind Tunnel Correlation.” In AIAA SCITECH 2026 Forum. AIAA 2026-1329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1329
• Klein, V. 1978. “Aircraft Parameter Estimation in Frequency Domain.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1344
• Klein, V. 1983a. A Review of System Identification Methods Applied to Aircraft. Joint Inst. for Acoustics and Flight Sciences. https://ntrs.nasa.gov/citations/19830025630
• Klein, A. F. 1983b. “The Synthesis of an Active Flutter Suppression Law Based on an Energy Criterion.” Aeronautical Quarterly 34 (4): 260–81. https://doi.org/10.1017/s000192590000977x
• Klein, Vladislav. 1989a. “Estimation of Aircraft Aerodynamic Parameters from Flight Data.” Progress in Aerospace Sciences 26 (1): 1–77. https://doi.org/10.1016/0376-0421(89)90002-x
• Klein, Vladislav. 1989b. “On Parameter Estimation of Highly Augmented Aircraft.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3356
• Klein, Vladislav. 1990. “Optimal Input Design for Aircraft Parameter Estimation Using Dynamicprogramming Principles.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2801
• Klein, Vladislav. 2002. Program of Research in Flight Dynamics in the JIAFS, George Washington University at NASA Langley Research Center. George Washington Univ. https://ntrs.nasa.gov/citations/20030015759
• Klein, V., and J. Batterson. 1983. “Determination of Aerodynamic Parameters of a Fighter Airplane from Flight Data at High Angles of Attack.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2066
• Klein, V., J. Batterson, and P. Murphy. 1981. “Determination of Model Structure and Parameters of an Airplane from Pre- and Post-Stall Flight.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1866
• Klein, Gary, Bryan Kashawlic, and Russell Enns. 2016. “Design and Flight Test of an Adaptive Vehicle Management System on an AH-64 Helicopter Demonstrator.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11554
• Klein, Vladislav, and Patrick C. Murphy. 1999. “Aerodynamic Parameters of High Performance Aircraft Estimated from Wind Tunnel and Flight Test Data.” In System Identification for Integrated Aircraft Development and Flight Testing. https://ntrs.nasa.gov/citations/19990032465
• Klein, Samuel, Willie Neiswanger, Daniel Ratner, Michael Kagan, and Sean Gasiorowski. 2026. “Supercharging Simulation-Based Inference for Bayesian Optimal Experimental Design.” Machine Learning: Science and Technology 7 (4): 045069. https://doi.org/10.1088/2632-2153/ae98e5
• Klein, Vladislav, and Keith D. Noderer. 1996. Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3: Parameters Estimated from Flight Data: Parameters Estimated from Flight Data: Part 3. NASA-TM-110259. NASA. https://ntrs.nasa.gov/citations/19960048458
• Kleinegesse, Steven, Christopher Drovandi, and Michael U. Gutmann. 2021. “Sequential Bayesian Experimental Design for Implicit Models via Mutual Information.” Bayesian Analysis 16 (3): 773–802. https://doi.org/10.1214/20-ba1225
• Klepl, M. 1992. “A Flutter Suppression System Using Strain Gages Applied to Active Flexible Wing Technology: Design and Test.” In Dynamics Specialists Conference. AIAA 1992-2098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2098
• Klimczyk, Witold Artur, and Zdobyslaw Jan Goraj. 2019. “Analysis and Optimization of Morphing Wing Aerodynamics.” Aircraft Engineering and Aerospace Technology 91 (3): 538–46. https://doi.org/10.1108/aeat-12-2017-0289
• Kline, Stephen J. 1986. “Method of Similitude and Introduction to Fractional Analysis of Overall Equations.” In Similitude and Approximation Theory. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-61638-9_3
• Klingenberg, Florian, Sebastian Willems, and Ali Gülhan. 2026. “Instrumentation and Data Acquisition of the Hypersonic Flight Experiment ATHEAt.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5043
• Klopfenstein, H. 1965. “Obtaining Airplane Drag Data from Nonsteady Flight.” In Flight Testing Conference. AIAA 1965-211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-211
• Klun, Johan, Bruce Lipe, and Henk Jentink. 2020. “Application of IRIG 106 Digital Data Recorder Standards for Flight Test.” In AGARDograph SCI-266. https://ntrs.nasa.gov/citations/20205001335
• Klunk, Garrett T., and Jeffrey L. Freeman. 2018. “Vertical Tail Area Reduction for Aircraft with Spanwise Distributed Electric Propulsion.” In 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. AIAA 2018-5022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-5022
• Klutchnikov, Igor, and Josef Ballmann. 2004. “DNS of Transonic Flow about a Supercritical Airfoil.” In ERCOFTAC Series. Springer Netherlands. https://doi.org/10.1007/978-1-4020-2313-2_24
• Klyde, David, James Reinsberg, Erica Sanders, and Alexander Kokolios. 2003. “Flight Test Evaluation of a Stability Augmentation Steering System for Aircraft Ground Handling.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5318
• Kmak, Frank, Mark Hudgins, and Dennis Hergert. 2001. “Revalidation of the NASA Ames 11-by 11-Foot Transonic Wind Tunnel with a Commercial Airplane Model.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-454
• Knackstedt, Wilhelm F. 1952. Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0008717
• Knapp, Matt. 1999. “Mission Optimization for a Reusable Launch Vehicle System.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4932
• Knapp, Ronald J., and Gareth H. Jordan. 1953. Flight-Determined Pressure Distributions over the Wing of the Bell X-1 Research Airplane (10-Percent-Thick Wing) at Subsonic and Transonic Speeds. NACA-RM-L53D20. NASA. https://ntrs.nasa.gov/citations/19930087577
• Knapp, Ronald J., Gareth H. Jordan, and Wallace E. Johnson. 1953. Fuselage Pressures Measured on the Bell X-1 Research Airplane in Transonic Flight. NACA-RM-L53I15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930089110
• Knauber, R. N., and S. Yanowitch. 1968. Scout First Stage Flight Characteristics. NASA-CR-111945. NASA. https://ntrs.nasa.gov/citations/19710023527
• Knaus, A. 1981. “A Technique to Determine Lift and Drag Polars in Flight and Their Application.” In 1st Flight Test Conference. AIAA 1981-2420. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2420
• Knight, Ross A. 1961. “Discussion of “Summary of Symposium on Supersonic Air Transport””.” Journal of the Air Transport Division 87 (2): 97–97. https://doi.org/10.1061/jaceal.0000115
• Knight, D. 2002. “RTO WG 10: Test Cases for CFD Validation of Hypersonic Flight.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-433
• Knight, Doyle D. 2022. “Reduction of Sonic Boom Signature Using Energy Deposition.” In AIAA SCITECH 2022 Forum. AIAA 2022-0096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0096
• Knight, Kyle, Eric Braun, Christopher Roy, Frank Lu, and Joseph Schetz. 2011. “Interference Drag Modeling and Experiments for a High Reynolds Number Transonic Wing.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3963
• Knighton, Donna. 1992. “Design and Utilization of a Flight Test Engineering Database Management System at the NASA Dryden Flight Research Facility.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4072. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4072
• Knittel, Jeremy, and Mark Lewis. 2012. “Multidisciplinary Optimization of StarBody Waverider Shapes for Lifting Aerocapture with Orbital Plane Change.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5809
• Knoblach, J. 1974. Terminal Homing Engineering Flight Test T7 and MT7 Missile Launch Transients Data Reduction and Summary. Defense Technical Information Center. https://doi.org/10.21236/ada003241
• Knoedler, Andre, William Bailey, Bruce McClintock, and David Harris. 1996. “Investigation of Global Positioning System Use for Air Data System Calibration of General Aviation Aircraft.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3417
• Knotts, Louis, and Randall Bailey. 1988. “Ground Simulator Requirements Based on in-Flight Simulation.” In Flight Simualtion Technologies Conference. AIAA 1988-4609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4609
• Knotts, L., and M. Parrag. 1983. “In-Flight Simulation at the U.S. Air Force and Naval Test Pilot Schools.” In Flight Simulation Technologies Conference. AIAA 1983-1078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1078
• Ko, William L. 1997. Thermostructural Behavior of a Hypersonic Aircraft Sandwich Panel Subjected to Heating on One Side. NASA-TM-4769. NASA. https://ntrs.nasa.gov/citations/19970017836
• Ko, William L., and Roger A. Fields. 1987. Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating. NASA-TM-88286. NASA. https://ntrs.nasa.gov/citations/19880001007
• Ko, William L., and Leslie Gong. 2000. Thermoelastic Analysis of Hyper-X Camera Windows Suddenly Exposed to Mach 7 Stagnation Aerothermal Shock. NASA/TP-2000-209030. NASA. https://ntrs.nasa.gov/citations/20000095550
• Ko, William L., and Leslie Gong. 2001. Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission. NASA/TP-2001-210398. NASA. https://ntrs.nasa.gov/citations/20010098879
• Kock, B. M., and W. D. Painter. 1968. Investigation of the Controllability of the M2-F2 Lifting-Body Launch from the B-52 Carrier Airplane. NASA-TM-X-1713. NASA. https://ntrs.nasa.gov/citations/19710005529
• Kock, B. M., and W. D. Painter. 1969. Operational Experiences and Characteristics of the M2-F2 Lifting Body Flight Control System. NASA-TM-X-1809. NASA. https://ntrs.nasa.gov/citations/19710005051
• Kock, Berwin M., William Schweikhard, David H. Campbell, et al. 1978. YF-12 Experiments Symposium, Volume 1. NASA-CP-2054-VOL-1. NASA. https://ntrs.nasa.gov/citations/19780024112
• Koegler, R. 1966. “Sonic Boom Analysis.” In 3rd Annual Meeting. AIAA 1966-941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-941
• Koehler, R., and E. Buchacker. 1986. “A Flight Test Method for Pilot/aircraft Analysis.” In NASA. Ames Research Center, 21st Annual Conference on Manual Control. https://ntrs.nasa.gov/citations/19860023539
• Koenig, David G., Kiyoshi Aoyagi, Michael R. Dudley, and Susan B. Schmidt. 1988. High Performance Forward Swept Wing Aircraft. Patent Number: US-PATENT-4,767,083. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19880019530
• Koenig, D. G., and L. S. Rolls. 1966. Flight-Measured Ground Effect on a Low-Aspect- Ratio Ogee Wing Including a Comparison with Wind-Tunnel Results. NASA-TN-D-3431. NASA. https://ntrs.nasa.gov/citations/19660018215
• Koeniguer, Donald, and Derek Spear. 2018. “Improved Altitude Hold and Hover Stabilization System Flight Testing on the United States Air Force HH-60G Helicopter.” In 2018 Flight Testing Conference. AIAA 2018-4169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4169
• Kogler, R., and D. Quam. 1983. “Estimating Roll Coupling Instability for Highly Augmented Aircraft.” In 21st Aerospace Sciences Meeting. AIAA 1983-366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-366
• Koh, J. 1971. “A New Wind Tunnel Technique for Providing Simulation of Flight Base Flow.” In 6th Aerodynamics Testing Conference. AIAA 1971-268. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-268
• Kohara, Makoto, Hiroyuki Tomoeda, and Hiromistu Kawazoe. 2016. “1408 a Study on Aerodynamic Characteristics of a Forward Swept Wing at Low Speed Flight.” Proceedings of Conference of Chugoku-Shikoku Branch 2016.54 (0): _1408-1_-_1408-2_. https://doi.org/10.1299/jsmecs.2016.54._1408-1_
• Kohlman, David L., William G. Schweikhard, and Ronald R. L. Renz. 1987. “Advances in Flight Test Instrumentation and Analysis.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/871802
• Kohn, Jerome, and Julius Pangilinan. 1986. “Database Application to Aircraft Engineering Functions Related to Flight Testing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9823
• Kohnhorst, Lloyd L., and Domenic A. Magnacca. 1980. Design and Test of a Hydra-Optic Flight Control Actuation System (HOFCAS) Concept. Defense Technical Information Center. https://doi.org/10.21236/ada094688
• Kohrs, R. 1982. “Space Shuttle Program Orbital Flight Test Program Results and Implications.” In Space Systems Conference. AIAA 1982-1776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1776
• Koike, Taiki, Yusuke Takahashi, Nobuyuki Oshima, and Kazuhiko Yamada. 2018. “Aerodynamic Heating Prediction of Flare-Type Membrane Inflatable Reentry Vehicle from Low Earth Orbit.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0289. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0289
• Kokolios, Alex. 1993. “X-31 Aerodynamic Characteristics Determined from Flight Data.” In NASA. Langley Research Center, NASA LaRC Workshop on Guidance, Navigation, Controls, and Dynamics for Atmospheric Flight, 1993. https://ntrs.nasa.gov/citations/19940020627
• Kokolios, Alexander. 1994. “Use of a Kalman Filter for the Determination of Aircraft Aerodynamic Characteristics from Flight Test Data.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-10. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-10
• Kolli, Ritvik. 2024. “High-Speed Flight.” Preprint, . https://doi.org/10.58445/rars.2008
• Komar, D., and R. Christenson. 1996. “Reusable Launch Vehicle Engine Systems Operations Analysis.” In Space Programs and Technologies Conference. AIAA 1996-4246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4246
• Komendat, Andy, and Agamemnon Crassidis. 2012. “Center of Gravity Estimation of an Aircraft Solely Using Standard Aircraft Measurement Sensors.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4411
• Konar, A. F., J. K. Mahesh, and B. Kizilos. 1974. Digital Flight Control System for Tactical Fighter. Volume 1. Digital Flight Control System Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada002320
• Kong, Jeffrey. 1994. “The Accuracy of Parameter Estimation in System Identification of Noisy Aircraft Load Measurement.” PhD diss., California Univ.. https://ntrs.nasa.gov/citations/19950012715
• Kong, Chuihuan, Lijun Pan, Dawei Wu, Rubing Ma, Changfu Cheng, and Yunwen Lou. 2023. “Research on Key Technologies of Scaled Model Flight Testing.” Journal of Physics: Conference Series 2658 (1): 012047. https://doi.org/10.1088/1742-6596/2658/1/012047
• Koning, Witold J. F. 2015. “Wind Tunnel Interference Effects on Tilt Rotor Testing Using Computational Fluid Dynamics.” PhD diss., Science and Technology Corp.. https://ntrs.nasa.gov/citations/20160004199
• Koning, Witold J. F. 2016. Wind Tunnel Interference Effects on Tilt Rotor Testing Using Computational Fluid Dynamics. NASA/CR-2015-219086. NASA. https://ntrs.nasa.gov/citations/20170000663
• Kontogiannis, Konstantinos, Adriano Cerminara, Nigel J. Taylor, Andras Sobester, and Neil Sandham. 2015b. “Parametric Geometry Models for Hypersonic Aircraft Components: Blunt Leading Edges.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3580
• Kontogiannis, Konstantinos, Andras Sobester, and Nigel J. Taylor. 2015a. “On the Conceptual Design of Waverider Forebody Geometries.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1009
• Konuk, Ege, and Drew Landman. 2023. “Computer Based Modeling for Tilt-Wing e-VTOL Propeller Performance.” In AIAA SCITECH 2023 Forum. AIAA 2023-0339. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0339
• Kopecki, Grzegorz. 2016. “Control Computers Diagnostics for UAV Flight Control System.” Aircraft Engineering and Aerospace Technology 88 (3): 420–26. https://doi.org/10.1108/aeat-10-2012-0187
• Koppes, Clayton R. 1989. “Engineer in Charge: A History of the Langley Aeronautical Laboratory 1917–1958 by James R. Hansen.” Technology and Culture 30 (2): 488–90. https://doi.org/10.1353/tech.1989.0133
• Koppes, Clayton R., and Frank W. Anderson. 1977. “Orders of Magnitude: A History of NACA and NASA, 1915-1976.” Technology and Culture 18 (3): 558. https://doi.org/10.2307/3103934
• Koppes, Clayton R., and James R. Hansen. 1989. “Engineer in Charge: A History of the Langley Aeronautical Laboratory 1917-1958.” Technology and Culture 30 (2): 488. https://doi.org/10.2307/3105131
• Kopsaftopoulos, Fotis, Raphael Nardari, Yu-Hung Li, Pengchuan Wang, Bo Ye, and Fu-Luo Chang. 2015. “Experimental Identification of Structural Dynamics and Aeroelastic Properties of a Self-Sensing Smart Composite Wing.” In Structural Health Monitoring 2015. Destech Publications. https://doi.org/10.12783/shm2015/163
• Korejwo, H., and M. Holden. 1992. “Ground Test Facilities for Aerothermal and Aero-Optical Evaluation of Hypersonic Interceptors.” In Aerospace Design Conference. AIAA 1992-1074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1074
• Kornev, A. V., M. B. Ambrozhevich, V. A. Sereda, and K. V. Migalin. 2021. “Aerodynamic Compensation Methods for Aeroelastic Divergence of Forward-Swept Wing.” Russian Aeronautics 64 (1): 28–36. https://doi.org/10.3103/s1068799821010049
• Korst, H., R. White, and R. Page. 1994. “Interference-Free Wind Tunnel Testing of Jet Propelled Missiles under Simulated Altitude and Full-Scale Reynolds Numbers.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2567
• Korsun, O. N., B. K. Poplavsky, A. V. Stulovskii, and Moung Htang Om. 2024. “Identification of Engine Thrust and Aerodynamic Drag Force According to Flight Test Data with Smoothing of Random Measurement Errors.” Teoriâ i sistemy upravleniâ, no. 3: 69–84. https://doi.org/10.31857/s0002338824030066
• Korunov, A. O. 2025. “Sonic Boom Characteristics under Strong Atmospheric Turbulence Using a Supersonic Civil Aircraft Demonstrator as an Example.” Акустический журнал / Acoustical Physics 71 (6): 835. https://doi.org/10.7868/s3034500625060085
• Korunov, A. O. 2026. “Rapid Estimation of the Sonic Boom Characteristics from Supersonic Passenger Aircraft in a Standard Atmosphere Based on Analytical Solutions: Caustics in Nonsteady Flight Modes.” Acoustical Physics 72 (2): 210–30. https://doi.org/10.1134/s1063771026600129
• Korunov, A. O., V. A. Gusev, and V. S. Gorbovskoy. 2024. “Rapid Estimation of Supersonic Civil Aircraft Sonic Boom Characteristics in Standard Atmosphere Based on Analytical Solutions. Cruise Flight.” Akustičeskij žurnal 70 (5): 725–39. https://doi.org/10.31857/s0320791924050075
• Korzun, Ashley M., and Louis A. Cassel. 2020. “Scaling and Similitude in Single Nozzle Supersonic Retropropulsion Aerodynamics Interference.” In AIAA Scitech 2020 Forum. AIAA 2020-0039. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0039
• Kosmos, G., and R. A. Greenwell. 1980. Airborne-Fiber Optics Manufacturing Technology, Aircraft Installation Processes. Defense Technical Information Center. https://doi.org/10.21236/ada093304
• Kossira, H., A. Bardenhagen, and W. Heinze. 1993. “Investigations on the Potential of Hypersonic Waveriders with the Integrated Aircraft Design Program PrADO-Hy.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5098
• Kostic, I., C. Mitrovic, D. Cvetkovic, and A. Bengin. 2002. “An Algorithm of Computation of Airfoil Drag in Lower Transonic Domain.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-545
• Kostyk, Christopher Barry. 2007. “Dryden Flight Research Center.” In Thermal and Fluids Analysis Workshop (TFAWS 2007). https://ntrs.nasa.gov/citations/20080008828
• Kostyk, christopher. 2008. “Thermal and Fluids Engineering at Dryden Flight Research Center in 2008.” In Thermal and Fluids Analysis Workshop 2008 (TFAWS 2008). https://ntrs.nasa.gov/citations/20080034696
• Kostyk, Chris. 2011. “Dryden Flight Research Center.” In Thennal and Fluids Analysis Workshop 2011 (TFAWS2011). https://ntrs.nasa.gov/citations/20110023921
• Kotfilia, R., and W. Painter. 1969. “Design, Development, and Flight Test Experience with Lifting Body Stability Augmentation Systems.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-887
• Kotob, S., and H. Kaufman. 1974. Digital System Identification and Its Application to Digital Flight Control. Rensselaer Polytechnic. https://ntrs.nasa.gov/citations/19740051018
• Kotob, S., and H. Kaufman. 1975. Minimum Variance System Identification with Application to Digital Adaptive Flight Control. Rensselaer Polytechnic Inst. https://ntrs.nasa.gov/citations/19760060695
• Kouznetsov, V. M. 1994. “Noise Problems of the Supersonic Civil Airplane.” Journal of the Acoustical Society of America 95 (5_Supplement): 2837–2837. https://doi.org/10.1121/1.409596
• Koven, William, and Gerald G. Kayten. 1946. Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas a-26 Airplane. NACA-ARR-L5H11a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092590
• Kowal, T. John. 2011. “Orion Flight Test-1 Thermal Protection System Instrumentation.” In NASA Langley Research Center. https://ntrs.nasa.gov/citations/20110012175
• Kraft, Edward. 1994. “Combining Ground Test, Computations, and Flight Test to Improve Aircraft/weapon Integration.” In Joint Test and Evaluation. AIAA 1994-2660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2660
• Kraft, Edward M. 2018. “Integrating Model-Based Systems Engineering and Uncertainty Quantification to Design Optimum Aircraft Test Campaigns.” In 2018 Applied Aerodynamics Conference. AIAA 2018-2853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2853
• Kraft, Edward M. 2020. “Transforming Ground and Flight Testing through Digital Engineering.” In AIAA Scitech 2020 Forum. AIAA 2020-1840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1840
• Kraft, Edward, and Gary Chapman. 1993. “A Critical Review of the Integration of Computations, Ground Tests, and Flight Test for the Development of Hypersonic Vehicles.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5101
• Kraiko, A. N., and D. E. Pudovikov. 1998. “Thin Airfoils of Minimum Wave Drag with Given Chord, Longitudinal Section Area, and Lift.” Fluid Dynamics 33 (4): 594–97. https://doi.org/10.1007/bf02698225
• Kraiko, A. N., N. I. Tillyaeva, and I. A. Brailko. 2025. “Construction of the Three-Dimensional Minimum-Wave-Drag Forebody of Given Length and with a Circular Base (Review).” Fluid Dynamics 60 (1): 7. https://doi.org/10.1134/s0015462824604716
• Kraiko, A. N., and R. A. Tkalenko. 1967. “Thin Flat Bodies of Minimum Wave Drag in Nonequilibrium Supersonic Flow.” Fluid Dynamics 2 (4): 37–41. https://doi.org/10.1007/bf01019533
• Kramer, Lynda J., Steven Williams, Trey Arthur, et al. 2018. “Initial Flight Testing of an eXternal Vision System (XVS) for the Low Boom Flight Demonstrator (LBFD).” In 2018 Flight Testing Conference. AIAA 2018-3411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3411
• Krause, E. 1992. “Hypersonic Research at German Universities — First Results of the Aachen Program.” In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-77922-0_13
• Krengel, Markus D., Martin Hepperle, and Andreas Huebner. 2019. “Aeroservoelastic Wing Sizing Using a Physics-Based Approach in Conceptual Aircraft Design.” In AIAA Aviation 2019 Forum. AIAA 2019-3368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3368
• Kreshock, Andrew, Hao Kang, Hyeonsoo Yeo, and Robert Thornburgh. 2016. “Validation of Comprehensive Modeling of the Wing and Rotor Aeroelastic Test System.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11432
• Kreshock, Andrew, Hyeonsoo Yeo, and Robert Thornburgh. 2018. “Comparison of Comprehensive Analyses Predicting Aeroelastic Stability of the Wing and Rotor Aeroelastic Test System.” In Proceedings of the Vertical Flight Society 74th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0074-2018-12761
• Kress, R. 1980. “Surface Combatant Fleet Offensive/defensive Enhancement by High Performance Turbofan VTOL Aircraft.” In Aircraft Systems Meeting. AIAA 1980-1811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1811
• Kress, R. 1983. “Variable Sweep Wing Design.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1051
• Kreutz, Frank. 1970. “Airborne Flight Test Data Acquisition and Automatic Data Processing System for Helicopter Test and Development Programs.” In Proceedings of the Vertical Flight Society Forum 26 - Washington, D.C. 1970. The Vertical Flight Society. https://doi.org/10.4050/vfs-f26-036
• Kriechbaum, G., and R. Stineman. 1971. “Design of Desirable Airplane Handling Qualities via Optimal Control.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-956
• Krieger, R., R. Hood, and D. Gillies. 1980. “Correlation of Oil Flow and Aerodynamic Characteristics of Arbitrarily Shaped Advanced Missile Concepts.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1560
• Krishnan, G. L. Yadhu, and K. S. Sajikumar. 2023. “Modelling and Analysis of Vertical Landing Reusable Launch Vehicle with Spring Damper.” In AIP Conference Proceedings, vol. 2949. AIP Publishing. https://doi.org/10.1063/5.0157175
• Krivec, D. K., R. T. Ling, and J. Vadyak. 1984. “Investigation of Transonic Inlet Drag Characteristics.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/841539
• Krizo, Matthew J., Salvatore J. Cusumano, Steven T. Fiorino, et al. 2013. “Design, Development, and in-Flight Testing of a Pointer/tracker for in-Flight Experiments to Measure Aero-Optical Effects over a Scaled Turret.” Optical Engineering 52 (07): 1–9. https://doi.org/10.1117/1.oe.52.7.071415
• Kroeger, R., and W. Martin. 1967. “The Streamline Matching Technique for V/STOL WIND Tunnel Wall Corrections.” In 5th Aerospace Sciences Meeting. AIAA 1967-183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-183
• Krone, N., Jr. 1980a. “Forward Swept Wing Design.” In The evolution of aircraft wing design; Proceedings of the Symposium. AIAA 1980-3047. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-3047
• Krone, N., Jr. 1980b. “Forward Swept Wing Flight Demonstrator.” In Aircraft Systems Meeting. AIAA 1980-1882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1882
• Kroo, Ilan. 1990. “The Sonic Boom of an Oblique Flying Wing.” In 13th Aeroacoustics Conference. AIAA 1990-4002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-4002
• Kroos, K. 1995. “A Comparison of Supersonic Aerodynamic Flight Characteristics between the Earth and Mars Atmospheres.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2642
• Krumenacker, Joseph, and Paul Pellicano. 1992. “Flight Simulation and Data Analysis during a High Angle of Attack Vortex Flow Control Flight Test Program.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4108
• Kryter, Karl D. 1969. “Sonic Booms from Supersonic Transport: The Operation of Supersonic Transport Is Considered in the Light of the Effects of Sonic Booms on People.” Science 163 (3865): 359–67. https://doi.org/10.1126/science.163.3865.359
• Kryvokhatko, Illia S., and Oleksandr M. Masko. 2018. “Aerodynamic Characteristics and Longitudinal Stability of Tube Launched Tandem-Scheme UAV.” In Flight Physics - Models, Techniques and Technologies. InTech. https://doi.org/10.5772/intechopen.70228
• Kryvokon, O. 2018. “From the History of Domestic Aircraft Engineering: Little-Known Figures.” History of science and technology 7 (11): 25–35. https://doi.org/10.32703/2415-7422-2017-7-11-25-35
• Kubo, Daisuke. 2018. “Gust Response Evaluation of Small UAS via Free-Flight in Gust Wind Tunnel.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0297
• Kubota, Hirotoshi. 2003. “Sonic Boom Research in Japan (Invited).” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3578
• Kucera, V., and M. Hromčík. 2013. “Delay-Based Signal Shapers and Acfa 2020 Blended Wing Body Flight Control System.” In Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics, edited by C. Vallet, D. Choukroun, C. Philippe, G. Balas, A. Nebylov, O. Yanova. EDP Sciences. https://doi.org/10.1051/eucass/201306767
• Küchemann, D. 1957. “Methods of Reducing the Transonic Drag of Swept: Back Wings at Zero Lift.” Journal of the Royal Aeronautical Society 61 (553): 37–42. https://doi.org/10.1017/s0368393100130536
• Kuehme, Daniel, Nicholas R. Alley, Caleb Phillips, and Bruce R. Cogan. 2014. “Flight Test Evaluation and System Identification of the Area-I Prototype-Technology-Evaluation Research Aircraft (PTERA).” In AIAA Flight Testing Conference. AIAA 2014-2577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2577
• Kufeld, Robert M., Ethan A. Romander, Michelle Dominguez, and Hannah Dromiack. 2019a. UH-60A Airloads Flight Test Program: Data Counter 8513. NASA/TM-2019–220317. NASA. https://ntrs.nasa.gov/citations/20200002094
• Kufeld, Robert M., Ethan A. Romander, Michelle Dominguez, and Hannah Dromiack. 2019b. UH-60A Airloads Flight Test Program: Data Counter 9505. NASA/TM-2019–220309. NASA. https://ntrs.nasa.gov/citations/20200003148
• Kuhl, A. E., M. V. Little, and J. T. Rogers. 1958. Analysis of Flight-Determined and Predicted Effects of Flexibility on the Steady-State Wing Loads of the B-52 Airplane. NACA-RM-H57C25. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19660030327
• Kuhn, Donald L. 1975. Analysis of Flight Data for Deepwell System Installed in EP-3E Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada955473
• Kuhn, Richard E. 1979. Height of Spray Produced by Vertical Takeoff and Landing (VTOL) Aircraft,. Defense Technical Information Center. https://doi.org/10.21236/ada073099
• Kukreja, Sunil L. 2007. “F-15B QuietSpike(TradeMark) Aeroservoelastic Flight Test Data Analysis.” In International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2007. https://ntrs.nasa.gov/citations/20070028827
• Kukreja, Sunil L. 2008a. Nonlinear System Identification for Aeroelastic Systems with Application to Experimental Data. NASA/TM-2008-214641. NASA. https://ntrs.nasa.gov/citations/20080045505
• Kukreja, Sunil L., and Dennis S. Bernstein. 2012. Sensor-Only System Identification for Structural Health Monitoring of Advanced Aircraft. NASA/TM-2012-216045. NASA. https://ntrs.nasa.gov/citations/20120016606
• Kulfan, Robert M. 1990. “Application of Favorable Aerodynamic Interference to Supersonic Airplane Design.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/901988
• Kulfan, R., and A. Sigalla. 1978. “Real Flow Limitations in Supersonic Airplane Design.” In 16th Aerospace Sciences Meeting. AIAA 1978-147. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-147
• Kulkarni, Tapan, and Steve Suh. 2005. “Optimal Design Solutions for Crew Exploration Vehicle.” In Space 2005. AIAA 2005-6623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6623
• Kullback, S., and R. A. Leibler. 1951. “On Information and Sufficiency.” Annals of Mathematical Statistics 22 (1): 79–86. https://doi.org/10.1214/aoms/1177729694
• Kumar, A. Sai, M. Ganesh, and Nirmith Kumar Mishra. 2023b. “Modelling and CFD Analysis of Supercritical Airfoil with Slotted Flap at Various Flight Segments.” In AIP Conference Proceedings, vol. 2808. AIP Publishing. https://doi.org/10.1063/5.0113316
• Kumar, R., and A. K. Ghosh. 2011. “Parameter Estimation Using Unsteady Downwash Model from Real Flight Data of Hansa-3 Aircraft.” Aeronautical Journal 115 (1171): 577–88. https://doi.org/10.1017/s0001924000006217
• Kumar, Ajit, and Ajoy Kanti Ghosh. 2017. “A Comparison of Model-Based and Data-Driven Methods for Aerodynamic Parameter Estimation from Flight Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0936
• Kumar, Ajit, and Ajoy K. Ghosh. 2018a. “Data-Driven Method Based Aerodynamic Parameter Estimation from Flight Data.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0768
• Kumar, Ajit, and Ajoy Kanti Ghosh. 2018b. “A GPR Based Novel Approach for Aerodynamic Parameter Estimation from Flight Data.” International Review of Aerospace Engineering (IREASE) 11 (6): 252. https://doi.org/10.15866/irease.v11i6.14521
• Kumar, Ravi, and Santanu Ghosh. 2023a. “Numerical Investigation of the Trailing Edge Morphing Using Corrugated Skin at a High Reynolds Number for NACA 0012 & NACA 64(1)-612 Airfoils.” In AIAA AVIATION 2023 Forum. AIAA 2023-4088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4088
• Kumar, Ajit, and A. K. Ghosh. 2023b. “Regularization Regression Methods for Aerodynamic Parameter Estimation from Flight Data.” Aircraft Engineering and Aerospace Technology 95 (5): 820–30. https://doi.org/10.1108/aeat-09-2019-0179
• Kumar, Rakesh, A. K. Ghosh, and Ajay Misra. 2013. “Parameter Estimation from Flight Data of Hansa-3 Aircraft Using Quasi-Steady Stall Modeling.” Journal of Aerospace Engineering 26 (3): 544–54. https://doi.org/10.1061/(asce)as.1943-5525.0000155
• Kumar, Rajesh, Saisanthosh G. Iyer, Narne Prudhvi, and Amardip Ghosh. 2022. “Mode Transition in a Strut Based Dual-Mode Scramjet Combustor.” In AIAA AVIATION 2022 Forum. AIAA 2022-3863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3863
• Kumar, Rajesh, Singeetham Pranaykumar, and Amardip Ghosh. 2023a. “Mode Transition in Cavity Based Dual Mode Scramjet Combustor.” In AIAA AVIATION 2023 Forum. AIAA 2023-4138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4138
• Kumar, N. Shantha, and N. Janardhana Rao. 2004. “Estimation of Stability and Control Derivatives of Light Canard Research Aircraft from Flight Data.” Defence Science Journal 54 (3): 277–92. https://doi.org/10.14429/dsj.54.2041
• Kumar Sulur Loganathan, Pradeep. 2023. “Design and CFD Analysis on the Reduction of Thermal Effect in Re-Entry Vehicle by Using Retractable Aerospike.” In Hypersonic and Supersonic Flight - Advances in Aerodynamics, Materials, and Vehicle Design. IntechOpen. https://doi.org/10.5772/intechopen.107841
• Kuntavanish, M., and R. Cancel. 1983. “Low Level Delivery Test Program: Correlation of Wind Tunnel/sled Track Test Separation Results.” In 2nd Flight Testing Conference. AIAA 1983-2761. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2761
• Kuntz, David, and Donald Potter. 2007. “Boundary Layer Transition and Hypersonic Flight Testing.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-308
• Kunwar, Bikash, and Imon Chakraborty. 2025. “Developing Flight Simulation Model for a Lift-Plus-Cruise Subscale Vehicle: Mass Properties, Propulsion, and System Identification.” In AIAA SCITECH 2025 Forum. AIAA 2025-0739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0739
• Kunwar, Bikash, Stefanus H. Putra, Henry C. McCormick, Rajan Bhandari, Imon Chakraborty, and Nadine Auda. 2026. “Control Law Development, Flight Testing, and System Identification of a Distributed Electric Propulsion Subscale Aircraft.” In AIAA SCITECH 2026 Forum. AIAA 2026-2288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2288
• Kuppuswamy, K., and N. Kiran. 1981. “Planning a Helicopter Flight Test Program.” In 1st Flight Test Conference. AIAA 1981-2381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2381
• Kuranov, Alexander, and Alexey Korabelnikov. 2008. “Hypersonic Technologies of Atmospheric Cruise Flight under AJAX Concept.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2524
• Kurdi, Mohammad, Ned Lindsley, and Philip Beran. 2007. “Uncertainty Quantification of the Goland+ Wing’s Flutter Boundary.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6309
• Kurkjian, Haig. 1947. “Some Test Instrumentation Problems of the Helicopter.” In Proceedings of the Vertical Flight Society Forum 3 - Philadelphia, PA 1947. The Vertical Flight Society. https://doi.org/10.4050/vfs-f3-009
• Kurnaz, Sefer, Omer Cetin, and Okyay Kaynak. n.d. “Fuzzy Logic Based Approach to Design of Flight Control and Navigation Tasks for Autonomous Unmanned Aerial Vehicles.” In Unmanned Aircraft Systems. Springer Netherlands. https://doi.org/10.1007/978-1-4020-9137-7_13
• Kurth, Guido, Christoph Bauer, and Norman Hopfe. 2015. “Performance Assessment for a Throttleable Ducted Rocket Powered Lower Tier Interceptor.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-4234. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4234
• Kusunose, Kazuhiro, James Crowder, and Robert Watzlavick. 1999. “Wave Drag Extraction from Profile Drag Based on a Wake-Integral Method.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-275
• Kusunose, K., D. Marcum, H. Chen, and N. Yu. 1987. “Transonic Analysis for Complex Airplane Configurations.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1196. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1196
• Kutney, John, and Stanley Piszkin. 1963. “Reduction of Drag Rise on the Convair 990 Airplane.” In Summer Meeting. AIAA 1963-276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-276
• Kutschinski, C. R. 1975. “Flight Testing Air-to-Air Missiles for Flutter.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003027
• Kutty, Prasad, Christopher D. Karlgaard, Eric M. Blood, et al. 2015. “Supersonic Flight Dynamics Test: Trajectory, Atmosphere, and Aerodynamics Reconstruction.” In American Astronomical Society. https://ntrs.nasa.gov/citations/20150006855
• Kuz’min, A. G. 2010. “Aerodynamic Surfaces Admitting Jumps of the Lift Coefficient in Transonic Flight.” In Computational Fluid Dynamics Review 2010. WORLD SCIENTIFIC. https://doi.org/10.1142/9789814313377_0022
• Kwak, Dong-Youn, Kenji Yoshida, Hiroaki Ishikawa, and Masayoshi Noguchi. 2006. “Flight Test Measurements of Surface Pressure on Unmanned Scaled Supersonic Experimental Airplane.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3483. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3483
• Kyeremeh, Ebenezer Adu, Emmanuel Y. Osei, Albert Sunnu, Richard Opoku, and Muyiwa Samuel Adaramola. 2023. “Wind Tunnel Studies of the Lift and Drag Characteristics of EYO-Series Airfoils under Ultra-Low Reynolds Number Conditions between 30,000 and 90,000.” Preprint, . https://doi.org/10.2139/ssrn.4545243
• La, Sara, W. Yeol Joe, Muhammad Akbar, and Bashir Alsaidi. 2018. “Surveys on Skin Design for Morphing Wing Aircraft: Status and Challenges.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0315
• La, A. T., T. P. Shivananda, T. Holtz, and R. S. Marx. 1993. “CFD Predictions of Flowfields about a Hypersonic Lifting Body.” In Flight Simulation and Technologies. AIAA 1993-3692. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3692
• La Sorsa, Andrew, Adam R. Kotler, Spencer D. Smith, and Kareem A. Ahmed. 2025. “Aerothermal Considerations on Ramjet and Scramjet Thermodynamic Cycles.” In AIAA SCITECH 2025 Forum. AIAA 2025-1528. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1528
• Lacerda Montes, Pedro, Vinicius Alves, and Guilherme Luis Takahashi de Carvalho. 2025. “Parametric Study of an Experimental Rocket’s Drag in Transonic Flow.” In Proceedings of the 27th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2023.cob2023-1895
• Lackey, J., and C. Hadfield. 1992. “Pitch Control Margin at High Angle of Attack: Quantitative Requirements (Flight Test Correlation with Simulation Predictions).” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4107
• Lacoste, Marc, Frédéric Fenot, Alain Lacombe, and Michel Cataldi. 1995. “Using C/SiC Composite Materials for Thermal Protection System for Planetary Entry System, Behaviour in Relevant Environment.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/951617
• Lada, C., and K. Kontis. 2009. “Fluidic Control of Cavity Configurations at Transonic and Supersonic Speeds.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_76
• Ladeinde, Foluso, Zhipeng Lou, D.-H. Kim, and Rajarshi Das. 2017. “Studies on Leading Edge Detection in Mechanically- and Combustion-Generated Shock Trains in Dual-Mode Scramjet Engines.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0556
• Ladyzhenskij, M. D. 1963. The Hypersonic Area Rule. Defense Technical Information Center. https://doi.org/10.21236/ad0295787
• Laflamme, H. 1970. “Ground Simulation: A Tool to Aid in Hypersonic Vehicle Design.” In Test Effectiveness in the 70’s Conference. AIAA 1970-385. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-385
• LaGraff, John E. 2007. Minnowbrook I: 1993 Workshop on End-Stage Boundary Layer Transition. NASA/CP-2007-214667. NASA. https://ntrs.nasa.gov/citations/20070038942
• Lam, L., and E. Stollenwerk. 1966. “Aerodynamic Force Measurement of Free-Flight Models in a Hypervelocity Shock Tunnel.” In 2nd Aerodynamic Testing Conference. AIAA 1966-771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-771
• Lamar, J. E., R. A. Bruce, J. D. Pride Jr., R. H. Smith, and P. W. Brown. 1986. In-Flight Flow Visualization of F-106B Leading-Edge Vortex Using the Vapor-Screen Technique. AIAA PAPER 86-9785. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19860047380
• Lamar, John E., Clifford J. Obara, Bruce D. Fisher, and David F. Fisher. 2001. Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds. NASA/TP-2001-210629. NASA. https://ntrs.nasa.gov/citations/20010047400
• Lamar, John E., Clifford J. Obara, Bruce D. Fisher, and David F. Fisher. 2008. Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds. NASA/TP-2001-210629/SUPPL. NASA. https://ntrs.nasa.gov/citations/20090004590
• “Laminar Flow Control Wing.” 1999. Aircraft Engineering and Aerospace Technology 71 (3). https://doi.org/10.1108/aeat.1999.12771cab.004
• Lamy, M. 1983. “Air Force Flight Test Instrumentation System.” In 2nd Flight Testing Conference. AIAA 1983-2736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2736
• Lan, C., Silvia Bianchi, and Jay Brandon. 2006. “Effects of Bearing Friction of a Free-to-Roll Test Rig on Transonic Roll Damping and Dihedral Effect.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6490. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6490
• Lan, Chuan-Tau, and Jay Brandon. 2003. “Development of Nonlinear Aerodynamic Models from Flight Data and Evaluation of Tabulated Aerodynamic Models.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5696
• Lan, C., Chialu Hsu, and Tai-Hsing Sun. 1995. “Calculation of Transonic Dynamic Stability Parameters by an Unsteady TSD Theory (Transonic Small-Disturbance Flow).” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3442. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3442
• Landberg, Magnus, Christopher Jouannet, Magnus Sethson, David Lundström, and Petter Krus. 2025. “An Actuator for Multiple Variable Camber Trailing Edge Flaps.” In AIAA SCITECH 2025 Forum. AIAA 2025-1647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1647
• Landis, Geoffrey A. 2001. Exploring Venus by Solar Airplane. NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20020022923
• Landman, Drew, Cole Burnette, Ege Konuk, and Engin Baris. 2022. “Wind Tunnel Test Techniques for Low-Reynolds Number Propeller Performance Enhancement.” In AIAA AVIATION 2022 Forum. AIAA 2022-3641. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3641
• Lang, J. 1981. “Organizing and Training for Innovative Flight Test Management.” In 1st Flight Test Conference. AIAA 1981-2416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2416
• Lang, J., and R. Pitzer. 1980. “Control and Data Acquisition Aircraft for ALCM Flight Tests.” In 11th Aerodynamic Testing Conference. AIAA 1980-446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-446
• Lange, Fabian. 2018. “Aerodynamic Optimization of an UHBR Engine Position on a Representative Short Range Aircraft Configuration at Cruise Flight Conditions.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3811
• Langford, G., D. Price, and M. Gallaher. 1990. “Aeroassist Flight Experiment Reaction Control System Preliminary Design.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2763
• Langham, T. 1979. “Aircraft Motion Sensitivity to Dynamic Stability Derivatives.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1621
• Langill, A., Jr. 1965. “Solid Rocket Motor Specific Impulse Correlation: Captive Test Data to Flight Test Results.” In Flight Testing Conference. AIAA 1965-205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-205
• Langley, Marcus. 1971. “The History of Metal Aircraft Construction.” Aeronautical Journal 75 (721): 19–30. https://doi.org/10.1017/s0001924000044560
• Langley Research Center. 1966. Summary of NACA/NASA Variable-Sweep Research and Development Leading to the F-111 (TFX). NASA-LWP-285. NASA. https://ntrs.nasa.gov/citations/20080013519
• Lantz, Edward. 1998. “A Reusable Launcher for Flight Testing Ramjet Powered Aircraft.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1583
• Lappos, Nicholas. 2020. “MATRIX Technology & DARPA ALIAS Program.” In Proceedings of the Vertical Flight Society Handling Qualities 2020 Technical Meeting - Huntsville, Alabama 2020. The Vertical Flight Society. https://doi.org/10.4050/sm_2020_hq-913
• Lappos, Nicholas D., and Kevin D. Phelps. 1991. “Results of Flight Tests of the Boeing Sikorsky Fantail™ Demonstrator.” In Proceedings of the Vertical Flight Society Forum 47 - Phoenix, AZ 1991. The Vertical Flight Society. https://doi.org/10.4050/vfs-f47-1051
• Lapshina, T. V., and N. A. Ostapenko. 2009. “A Criterion for Minimum Wave Drag of a Body.” Doklady Physics 54 (1): 37–42. https://doi.org/10.1134/s1028335809010108
• Large, R., W. May, and D. Okeefe. 1981. “Status and Tracking System for Flight Test Data Products.” In 1st Flight Test Conference. AIAA 1981-2395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2395
• Largent, J. 1986. “Principles of Flight Test.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9742. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9742
• Larrabee, Trenton Jameson. n.d. “Wind and Wake Sensing with UAV Formation Flight: System Development and Flight Testing.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.678
• Larsen, Charles. 2000. “Commercial Space Transportation Reusable Launch Vehicle Operations and Maintenance Considerations.” In Space 2000 Conference and Exposition. AIAA 2000-5114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5114
• Larsen, Charles. 2003. “Commercial Space Transportation Reusable Launch Vehicle Operations and Maintenance Developments.” In AIAA Space 2003 Conference & Exposition. AIAA 2003-6407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6407
• Larsen, Charles. 2005. “Development of Guide to Commercial Space Transportation Reusable Launch Vehicle Operations and Mainenance.” In Space 2005. AIAA 2005-6795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6795
• Larson, H. 1968. “Unusual Boundary-Layer Transition Results on Cones in Hypersonic Flow.” In 6th Aerospace Sciences Meeting. AIAA 1968-40. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-40
• Larson, R. R. 1972. Statistical Analysis of Landing Contact Conditions for Three Lifting Body Research Vehicles. NASA-TN-D-6708. NASA. https://ntrs.nasa.gov/citations/19720011245
• Larson, R. 1986. “Flight Control System Development and Flight Test Experience with the F-111 Mission Adaptive Wing Aircraft.” In Astrodynamics Conference. AIAA 1986-2237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2237
• Larson, R. R., R. E. Smith, and K. D. Krambeer. 1983. “Flight-Test Results Using Nonlinear Control with the F-8C Digital Fly-by-Wire Aircraft.” In Guidance and Control Conference. https://ntrs.nasa.gov/citations/19830060451
• Larsson, Roger. 2025. “Flight Control Investigation Using a 3D-Printed Radio-Controlled Demonstrator.” In Linköping Electronic Conference Proceedings, vol. 215. Linköping University Electronic Press. https://doi.org/10.3384/ecp215.1202
• Larsson, Roger, and Martin Enqvist. 2016. “An Easy to Use Engineering Method for Identification of Complex Flight Dynamics from Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3853
• “Lateral-Directional Stability Theory and Flight Test Methods.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0297.0310
• Lau, Kei. 2007. “Hypersonic Boundary Layer Transition: Application to High Speed Vehicle Design.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-310
• Lau, Wayne. 2025. “Magnetic Plasma Deflection for Hypersonic Flight.” Preprint, . https://doi.org/10.2139/ssrn.5683462
• Lau, Benton H., Nicole Obriecht, Tanner Gasow, Brandon Hagerty, Kelly C. Cheng, and Ben W. Sim. 2009. Boeing-SMART Test Report for DARPA Helicopter Quieting Program. Defense Technical Information Center. https://doi.org/10.21236/ada529306
• Laurence, Stuart. 2023. “Free-Flight Experiments in High-Speed Wind Tunnels.” Preprint, . https://doi.org/10.52843/cassyni.yyf0c4
• Laurence, Stuart J., Alexander Wagner, Hiroshi Ozawa, and Klaus Hannemann. 2014. “Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited).” In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2014-3110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3110
• Lauten, W. T., Jr., R. R. Lundstrom, and B. R. Okelly. 1954. Free-Flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds. NACA-RM-L54C22. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630003991
• Lawing, P. L. 1975. Analysis of Various Descent Trajectories for a Hypersonic-Cruise, Cold-Wall Research Airplane. NASA-TN-D-7860. NASA. https://ntrs.nasa.gov/citations/19750016601
• Lawing, P. L. 1978. Configuration Heating for a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-Delta Wing. NASA-TP-1143. NASA. https://ntrs.nasa.gov/citations/19780015446
• Lawing, Pierce, Julio Chu, William Milholen II, and Ndaona Chokani. 1991. “Comparison of Cryogenic Wind Tunnel, Flight, and Computational Results for a Thin, Low-Aspect-Ratio Wing.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1626
• Lawrence, David B. n.d. “The Quantification of the Value of Information in Decision Making.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180817-5660
• Lawrence, F., and B. Mills. 2002. “Status Update of the AEDC Wind Tunnel Virtual Flight Testing Development Program.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-168. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-168
• Layton, G. P. 1974. NASA Flight Research Center Scale F-15 Remotely Piloted Research Vehicle Program. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19740060853
• Layton, G. P. 1984. “A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility.” In Canadian Aeronautics and Space Inst. (CASI) Flight Test Symp.. https://ntrs.nasa.gov/citations/19840012447
• Layton, D. 1986. “Constant Altitude Helicopter Flight Testing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9787
• Layton, Jeffrey. 1996. “Aeroelastic and Aeroservoelastic Tailoring with Geometry Variables for Minimizing the Gust Response of a Cantilevered Finite Span Wing.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1442. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1442
• Layton, Garrison P., Jr. 1970. “Summary of Primary Results of the Lifting Body Program.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000634
• Lazzara, David S., Todd Magee, Hao Shen, and James H. Mabe. 2019. “Off-Design Sonic Boom Performance for Low-Boom Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-0606. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0606
• Lazzara, David S., Todd Magee, Hao Shen, and James H. Mabe. 2020. “Sonic Boom Performance of Low-Boom Aircraft in Non-Standard Atmospheres.” In AIAA Scitech 2020 Forum. AIAA 2020-0792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0792
• Lazzara, David S., Todd Magee, Hao Shen, James H. Mabe, Pedro B. Leal, and Darren J. Hartl. 2021. “A Decoupled Method for Estimating Non-Ideal Sonic Boom Performance of Low-Boom Aircraft Due to off-Design Flight Conditions and Non-Standard Atmospheres.” In AIAA Scitech 2021 Forum. AIAA 2021-1271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1271
• Lcls Life Cycle Logistics Supportability. n.d. Aircraft Engine Life Cycle Cost Guide. SAE International. https://doi.org/10.4271/air1939a
• Le, Daniel, Christopher Goyne, Roland Krauss, and James McDaniel. 2005. “Experimental Study of a Dual-Mode Scramjet Isolator.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-23. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-23
• Leach, Barrie, and Kenneth Hui. 2001. “In-Flight Technique for Calibrating Air Data Systems Using Kalman Filtering and Smoothing.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4260
• Leader, Mark K., Eliot Aretskin-Hariton, and Kenneth Moore. 2024. “Multidisciplinary Optimization of a Transonic Truss Braced Wing Aircraft with Hybrid-Electric Propulsion.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4294
• Lebacqz, J. V. 1974. “Application of a Kalman Filter Identification Technique to Flight Data from the X-22A Variable Stability V/STOL Aircraft.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017465
• Lebacqz, J., and B. Scott. 1984. “Ground-Simulation Investigation of VTOL Instrument Flight Rules Airworthiness Criteria.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2105
• Lebofsky, Sonia, Eric Ting, and Nhan T. Nguyen. 2015a. “Multidisciplinary Drag Optimization of Reduced Stiffness Flexible Wing Aircraft with Variable Camber Continuous Trailing Edge Flap.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1408
• Lebofsky, Sonia, Eric Ting, Nhan T. Nguyen, and Khanh V. Trinh. 2014. “Aeroelastic Modeling and Drag Optimization of Flexible Wing Aircraft with Variable Camber Continuous Trailing Edge Flap.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2443
• Lebofsky, Sonia, Eric Ting, Khanh V. Trinh, and Nhan T. Nguyen. 2015b. “Optimization for Load Alleviation of Truss-Braced Wing Aircraft with Variable Camber Continuous Trailing Edge Flap.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2723. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2723
• Lechniak, Jason A. 2017. “Manned versus Unmanned Risk and Complexity Considerations for Future Midsized X-Planes.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170005544
• Lederer, Melissa A. 1994. Hypervelocity WInd Tunnel Number 9, High Mach Number Development Program. Defense Technical Information Center. https://doi.org/10.21236/ada289934
• Lederer, R. 1996. “Testing the Actively Cooled, Fully Variable Hypersonic Demonstrator Nozzle: Results from the Test Campaign 1995/96.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4550. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4550
• Lee, Alexander David. n.d. “Parametric Modeling for Simulation Based Hypersonic Vehicle Design.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/etd-180810-3950
• Lee, E. B. 1977. The Study of Distributive Parameter Systems for Flight Control. Defense Technical Information Center. https://doi.org/10.21236/ada038281
• Lee, Cunbiao. 2024. “Transition in the Hypersonic Boundary Layer.” Preprint, . https://doi.org/10.52843/cassyni.2yztcr
• Lee, H., M. Chang, and M. Kaiser. 1998. “Flight Dynamics and Stability and Control Characteristics of the X-33 Technology Demonstrator Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4410
• Lee, Robert, and J. Downing. 1993. “Boom Event Analyzer Recorder: The USAF Unmanned Sonic Boom Monitor.” In 15th Aeroacoustics Conference. AIAA 1993-4431. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4431
• Lee, Robert A., and J. Micah Downing. 1996b. “Comparison of Measured and Predicted Lateral Distribution of Sonic Boom Overpressures from the United States Air Force Sonic Boom Database.” Journal of the Acoustical Society of America 99 (2): 768–76. https://doi.org/10.1121/1.414654
• Lee, D. B., and W. D. Goodrich. 1972. The Aerothermodynamic Environment of the Apollo Command Module during Superorbital Entry. NASA-TN-D-6792. NASA. https://ntrs.nasa.gov/citations/19720016296
• Lee, Yang-Ji, Sang-Hun Kang, and Soo-Seok Yang. 2015. “A Study on the Hypersonic Air-Breathing Engine Ground Test Facility Composition and Characteristics.” Journal of the Korean Society of Propulsion Engineers 19 (6): 81–90. https://doi.org/10.6108/kspe.2015.19.6.081
• Lee, Sanghoon, and Jae Gang Kim. 2021b. “Stagnation-Point Heating and Ablation Analysis of Orbital Re-Entry Experiment.” Physics of Fluids 33 (8): 086102. https://doi.org/10.1063/5.0057473
• Lee, Kyungjae, Boyeon Kim, Jaeseung Kim, and Inyoung Yang. 2026. “Experimental Investigation of Subsonic-Mode Combustion Performance in a Dual-Mode Scramjet Combustor under Variation in Fuel Temperature.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5088
• Lee, Jin-Ho, and Thomas M. Krivanek. 2005. Design and Fabrication of the ISTAR Direct-Connect Combustor Experiment at the NASA Hypersonic Tunnel Facility. NASA/TM-2005-213432. NASA. https://ntrs.nasa.gov/citations/20050080753
• Lee, Dong-Chan, and M. Nagati. 1999. “Improved Coupled Force and Moment Parameter Estimation for Aircraft.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4174
• Lee, Kyunghoon, Taewoo Nam, and Shinseong Kang. 2017b. “Propulsion System Modeling and Reduction for Conceptual Truss-Braced Wing Aircraft Design.” International Journal of Aeronautical and Space Sciences 18 (4): 651–61. https://doi.org/10.5139/ijass.2017.18.4.651
• Lee, Cynthia, Clifford Obara, Paul Vijgen, and Michael Wusk. 1991. “Flight Experiments Measuring Boundary-Layer Disturbances in Laminar Flow and Correlation with Stability Analysis.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1635
• Lee, Cynthia C., Clifford J. Obara, and Michael S. Wusk. 1990. “Flight-Measured Streamwise Disturbance Instabilities in Laminar Flow.” In AIAA/SFTE/DGLR/SETP Biannual Flight Test Conference. https://ntrs.nasa.gov/citations/19900046849
• Lee, Chang-Ho, Young-Min Park, Byeong-Hee Chang, and Yung-Gyo Lee. 2017a. “Calibration and Flight Test Results of Air Data Sensing System Using Flush Pressure Ports.” Journal of the Korean Society for Aeronautical & Space Sciences 45 (7): 531–38. https://doi.org/10.5139/jksas.2017.45.7.531
• Lee, Dorothy B., and Andrew G. Swanson. 1958. Heat Transfer Measured on a Flat-Face Cylinder-Flare Configuration in Free Flight at Mach Numbers from 1.6 to 2.7. NACA-RM-L58A06. NASA. https://ntrs.nasa.gov/citations/19930089838
• Lee-Rausch, Elizabeth M., and Robert T. Biedron. 2013. “FUN3D Airload Predictions for the Full-Scale UH-60A Airloads Rotor in a Wind Tunnel.” In 69th Annual American Helicopter Society Forum and Technology Display. https://ntrs.nasa.gov/citations/20130014010
• Lee-Rausch, Elizabeth, Neal Frink, Dimitri Mavriplis, Russ Rausch, and William Milholen. 2004. “Transonic Drag Prediction on a DLR-F6 Transport Configuration Using Unstructured Grid Solvers.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-554. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-554
• Lees, Lester, and Toshi Kubota. 1972. Hypersonic Research Project. Defense Technical Information Center. https://doi.org/10.21236/ad0755276
• Lei, Jia, and Xiaolin Zhong. 2011. “Non-Linear Breakdown in Hypersonic Boundary Layer Transition Induced by Freestream Disturbances.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3563
• Lei, Jia, and Xiaolin Zhong. 2012. “Numerical Study of Freestream Waves Induced Breakdown in Hypersonic Boundary Layer Transition.” In 42nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2012-2692. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2692
• Leitch, Harry, Olivia Stodieck, and Jie Yuan. 2024. “Effects of Coupled Thickness Variation on the Aeroelastic Performance of Continuous Tow Sheared Composite Wing.” Preprint, . https://doi.org/10.2139/ssrn.4786120
• Lemley, C., and R. Mullans. 1973. “Buffeting Pressures on a Swept Wing in Transonic Flight: Comparisonof Model and Full Scale Measurements.” In Dynamics Specialists Conference. AIAA 1973-311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-311
• Lennon, John F., and J. L. Poirter. 1974. Interpretation of Microwave Antenna Results from a Reentry Flight Test: A Comparison of Methods. Defense Technical Information Center. https://doi.org/10.21236/ada004046
• “LENS Hypervelocity Tunnels and Application to Vehicle Testing at Duplicated Flight Conditions.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0073.0110
• Lensi, Michael. 2000. “Estimating Open-Loop Stability and Control Derivatives for the Tu-144LL Supersonic Transport from Flight Data.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3901
• Lenz, R. W., and B. McKeever. 1976. “Time Series Analysis in Flight Flutter Testing at the Air Force Flight Test Center: Concepts and Results.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014089
• Leon, Olivier, Eric Hayden, and Farhan Gandhi. 2009. “Rotorcraft Operating Envelope Expansion Using Extendable Chord Sections.” In Proceedings of the Vertical Flight Society 65th Annual Forum, Grapevine, Texas, May 27-29, 2009. The Vertical Flight Society. https://doi.org/10.4050/vfs-f65-000318
• Leshikar, Christopher, and John Valasek. 2022. “System Identification Flight Testing of Inverted V-Tail Small Unmanned Air System.” In AIAA SCITECH 2022 Forum. AIAA 2022-2408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2408
• Letchworth, Gary. 2011. “X-33 Reusable Launch Vehicle Demonstrator, Spaceport and Range.” In AIAA SPACE 2011 Conference & Exposition. AIAA 2011-7314. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-7314
• Letchworth, Janet, and Gary Letchworth. 2000. “Second Generation Reusable Launch Vehicle Servicing of the International Space Station.” In Space 2000 Conference and Exposition. AIAA 2000-5141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5141
• Leuckert, Janin, Jan Domhardt, Wolfgang Nitsche, and Jürgen Quest. 2008. “On Application of Surface Measurement Techniques for Cryogenic High Reynolds Number Investigations on Wind Tunnel Models.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-842
• Leung, Jordan M., Gregory J. Moszczynski, and Peter R. Grant. 2019. “A State Estimation Approach for High Angle-of-Attack Parameter Estimation from Certification Flight Data.” In AIAA Scitech 2019 Forum. AIAA 2019-0013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0013
• “Level Flight Performance Flight Test and Data Reduction Methods for Propeller-Driven Aircraft.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0083.0096
• “Level Flight Performance Theory.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0075.0082
• Levin, D. 1981. “A Vortex-Lattice Method for Calculating Longitudinal Dynamic Stability Derivatives of Oscillating Delta Wings.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1876. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1876
• Levinson, Mark. 1987. “Gleanings from Oft-Neglected Sources: Institutional History from Technical Documents-The Case of the NACA.” Technology and Culture 28 (2): 314. https://doi.org/10.2307/3105569
• Lewerenz, William. 1987. “UHB Demonstrator Flight Test Program.” In 23rd Joint Propulsion Conference. AIAA 1987-1732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1732
• Lewis, Mark. 1991a. “Application of Waverider-Based Configurations to Hypersonic Vehicle Design.” In 9th Applied Aerodynamics Conference. AIAA 1991-3304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3304
• Lewis, Mike. 1991b. “NASA Langley Flight Test Program.” In Airborne Wind Shear Detection and Warning Systems: Third Combined Manufacturers’ and Technologists’ Conference, Part 1. https://ntrs.nasa.gov/citations/19910014862
• Lewis, Mark, and Allan Paull. 1998. “A Joint American-Australian University Hypersonic Research Program.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1551
• Leylek, Emily, and Mark Costello. 2013. “Flight Stability and Control of Articulated Wing Aircraft.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4982. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4982
• Li, Wu. 2015. “Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2581
• Li, Jinxian. 2023. “Aerodynamics-Based Forward-Swept Wing Structure Optimization.” Applied and Computational Engineering 10 (1): 297–306. https://doi.org/10.54254/2755-2721/10/20230134
• Li, Jinglun. 2024. “Research and Analysis of the Small Disturbance Equation in Subsonic, Transonic, and Supersonic Regimes.” Science and Technology of Engineering, Chemistry and Environmental Protection 2 (5): 3812. https://doi.org/10.61173/02vmsx61
• Li, Fengyi, Ricardo Baptista, and Youssef Marzouk. 2026b. “Expected Information Gain Estimation via Density Approximations: Sample Allocation and Dimension Reduction.” SIAM/ASA Journal on Uncertainty Quantification 14 (3): 974–1007. https://doi.org/10.1137/25m1740164
• Li, Shaoyan, and Zongji Chen. 2003. “Research of Autonomous Landing Control of Unmanned Combat Air Vehicle.” In SPIE Proceedings, vol. 5253, edited by Guangjun Zhang, Huijie Zhao, Zhongyu Wang. SPIE. https://doi.org/10.1117/12.522111
• Li, Fei, Meelan M. Choudhari, Chau-Lyan Chang, Roger Kimmel, David Adamczak, and Mark S. Smith. 2011. “Transition Analysis for the HIFiRE-1 Flight Experiment.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110013356
• Li, Fei, Meelan Choudhari, Chau-Lyan Chang, Roger Kimmel, David Adamczak, and Mark Smith. 2012. Hypersonic Transition Analysis for HIFiRE Experiments. NF1676L-13443. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20120007115
• Li, Fei, Meelan Choudhari, and Pedro Paredes. 2021. “Transition Analysis for Isolated Trips on BOLT-II Wind-Tunnel and Flight Configurations.” In AIAA Aviation 2021 Forum. AIAA 2021-2905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2905
• Li, Xiaoguang, and Sanford Fleeter. 1996. “Active Suppression of Nonlinear Stall Flutter Using Piezoelectric Actuators.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3177
• Li, Xiaoguang, and Sanford Fleeter. 2004. “Active Suppression of Nonlinear Stall Flutter Using Piezoelectic Actuators.” International Journal of Turbo and Jet Engines 21 (2). https://doi.org/10.1515/tjj.2004.21.2.69
• Li, Wu, and Karl Geiselhart. 2023. “Redesign of a Low-Boom Supersonic Transport Using Powered Engine Simulation for Sonic Boom Analysis.” In AIAA SCITECH 2023 Forum. AIAA 2023-1511. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1511
• Li, Wu, and Karl Geiselhart. 2024. “Assessment of off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport.” In AIAA SCITECH 2024 Forum. AIAA 2024-1875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1875
• Li, Xuefei, Zhansen Qian, Chunpeng Li, Xianhong Xiang, and Pengbo Xu. 2019c. “Research on Morphing Scheme and Forward-Swept Wing Parameters Based on a Forward-Swept Wing Morphing Aircraft.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-13-3305-7_108
• Li, Li, Lei Qiao, Jiakuan Xu, and Junqiang Bai. 2025b. “Improved Aerodynamic-Propulsion Integration Model for Distributed-Electric-Propulsion System and Its Integration in Sizing for Hybrid-Electric Distributed-Propulsion Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.5280480
• Li, Jianping, Di Shen, Wenyan Song, and Qiang Fu. 2017b. “Mode Transition Analysis of a Dual-Mode Ramjet Combustor.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2117
• Li, Pei, Helmut Sobieczky, and Richard Seebass. 1995. “A Design Method for Supersonic Transport Wings.” In 13th Applied Aerodynamics Conference. AIAA 1995-1819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1819
• Li, Qing, and Zhenguo Wang. 2017. “Dynamic Mode Decomposition of Turbulent Combustion Process in DLR Scramjet Combustor.” Journal of Aerospace Engineering 30 (5): 04017034. https://doi.org/10.1061/(asce)as.1943-5525.0000747
• Li, C., and T. Wey. 1988. “Numerical Simulation of Hypersonic Flow over an Aeroassist Flight Experiment Vehicle.” In 23rd Thermophysics, Plasmadynamics and Lasers Conference. AIAA 1988-2675. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2675
• Li, Yi, Jun Yang, and Nan Chang. 2013. “Stochastic Nonlinear Aeroelastic Analysis of a Swept Wing Based on Nastran.” Applied Mechanics and Materials 0: 738–42. https://doi.org/10.4028/www.scientific.net/amm.0.738
• Li, Shangkun, Yonghao Zhang, and Zhangming Wu. 2019a. “Advanced Aerodynamic Modelling for the Optimization of Aircraft Wing Performance via Aeroelastic Tailoring.” In AIAA Scitech 2019 Forum. AIAA 2019-1214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1214
• Li, Yang, and Li Zhou. 2016. “A Flutter Boundary Prediction Technique Based on Atmospheric Turbulence Excitation Responses.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3858. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3858
• Librescu, L., and S. Thangjitham. 1989. “The Warping Restraint Effect in the Critical and Subcritical Static Aeroelastic Behavior of Swept Forward Composite Wing Structures.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/891056
• Lichota, Piotr. 2016. “Inclusion of the D-Optimality in Multisine Manoeuvre Design for Aircraft Parameter Estimation.” Journal of Theoretical and Applied Mechanics: 87. https://doi.org/10.15632/jtam-pl.54.1.87
• Lichota, Piotr. 2023. “Unstable Tilt-Rotor Maximum Likelihood Wavelet-Based Identification from Flight Test Data.” Aircraft Engineering and Aerospace Technology 95 (8): 1275–85. https://doi.org/10.1108/aeat-01-2023-0013
• Lichota, Piotr, Per Ohme, and Krzysztof Sibilski. 2016. “Simultaneous Multi-Step Excitations for Aircraft System Identification.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3704
• Lichtenwalner, Peter F., Gerald R. Little, Lawrence E. Pado, and Robert C. Scott. 1996. “Adaptive Neural Control for Active Flutter Suppression.” In Fluids Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1996-0947
• Liebeck, R. 2002. “Design of the Blended-Wing-Body Subsonic Transport.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-2. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2
• Liebeck, Robert. 2008. “Flight Test of the Blended Wing Body X-48B.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6414
• Lieberman, W. 1963. “Contributions of an Automatic Data System to Accomplishment of the Model 727 Certification Flight Test Program.” In Testing of Manned Flight Systems Conference. AIAA 1963-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1813
• Liebhardt, Bernd. 2019. “Sonic Boom Carpet Computation as a Basis for Supersonic Flight Routing.” In AIAA Aviation 2019 Forum. AIAA 2019-3387. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3387
• Liebhardt, Bernd. 2021. “Supersonic Overland without a Sonic Boom – Quantifying the Speed Advantage of Mach-Cutoff Flight.” In AIAA Aviation 2021 Forum. AIAA 2021-3188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3188
• Liebhardt, Bernd, Florian Linke, and Katrin Dahlmann. 2013. “Supersonic Diversions: Assessment of Great-Circle versus Sonic Boom-Restricted Flight Routing.” In 2013 Aviation Technology, Integration, and Operations Conference. AIAA 2013-4309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4309
• Liebhardt, Bernd, Klaus Lütjens, Atsushi Ueno, and Hiroaki Ishikawa. 2020. “JAXA’s S4 Supersonic Low-Boom Airliner – a Collaborative Study on Aircraft Design, Sonic Boom Simulation, and Market Prospects.” In AIAA Aviation 2020 Forum. AIAA 2020-2731. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2731
• Liebst, B., W. Garrard, and W. Adams. 1984. “Eigenspace Design of an Active Flutter Suppression System.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1867
• Liechty, Derek S., Scott A. Berry, and Thomas J. Horvath. 2006b. Shuttle Return to Flight Experimental Results: Protuberance Effects on Boundary Layer Transition. NASA/TM-2006-214306. NASA. https://ntrs.nasa.gov/citations/20060020179
• Liechty, Derek S., Thomas J. Horvath, and Scott A. Berry. 2006a. Shuttle Return to Flight Experimental Results: Cavity Effects on Boundary Layer Transition. NASA/TM-2006-214305. NASA. https://ntrs.nasa.gov/citations/20060022161
• Lien, John, David Bose, and John Martin. 2004. “Automated Sensitivity Analysis of Hyper-X (X-43A) Separation Simulation.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2004-4930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4930
• Liff, K. W. 1978. “Estimation of Aerodynamic Characteristics from Dynamic Flight Test Data.” In AGARD Dyn. Stability Parameters. https://ntrs.nasa.gov/citations/19790006904
• “Lightweight Low-Cost Flight Test Instrumentation.” 2007. Aircraft Engineering and Aerospace Technology 79 (1). https://doi.org/10.1108/aeat.2007.12779aad.010
• Lillis, Brian J. 1987. Evaluation of Naphthene Rich Turbine Fuels as Heat Sinks for Hypersonic Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada182118
• Lilly, Howard C., and William H. Barlow. 1949. Stability Results Obtained with Douglas D-558-1 Airplane (Buaero No. 37971) in Flight up to a Mach Number of 0.89. NACA-RM-L8K03. NASA. https://ntrs.nasa.gov/citations/19930085488
• Lim, K., A. Sreenatha, and M. Harrap. 2000. “Some Experiences with Preliminary Parameter Estimation of a Model Aircraft.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3904
• Lima Filho, Geraldo Mulato de, Felipe Leonardo Lôbo Medeiros, and Angelo Passaro. 2021. “Decision Support System for Unmanned Combat Air Vehicle in beyond Visual Range Air Combat Based on Artificial Neural Networks.” Journal of Aerospace Technology and Management 13: e3721. https://doi.org/10.1590/jatm.v13.1228
• Limache, A., and E. Cliff. 1999. “Aerodynamic Sensitivity Theory for Rotary Stability Derivatives.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4313
• Limage, C. 1996. “Solid Fuel Ducted Rockets for Ramjet/scramjet Missile Applications.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2916. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2916
• Limitations and Flight Envelope. 2017. Wiley. https://doi.org/10.1002/9781118534786.ch20
• Lin, C.-F. 1983. “Direct Optimization Methods in Real-Time Parameter Identification Ofmissile Aerodynamic Characteristics.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2102
• Lin, Kuo-Chi. 2002. Simulation of a Swarm of Unmanned Combat Air Vehicles (UCAVS). Defense Technical Information Center. https://doi.org/10.21236/ada403633
• Lin, W., A. Chen, and E. Tinoco. 1990. “3D Transonic Nacelle and Winglet Design.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3064. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3064
• Lin, Charissa, Edward Crawley, and Jennifer Heeg. 1995. “Open Loop and Preliminary Closed Loop Results of a Strain Actuated Active Aeroelastic Wing.” In 36th Structures, Structural Dynamics and Materials Conference. AIAA 1995-1386. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1386
• Lin, Sheam-Chyun, and Yu-Shan Luo. 1995a. “Optimization of Waverider Configurations Generated from Inclined Circular and Elliptic Cones.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6089
• Lin, Sheam-Chyun, and Yu-Shan Luo. 1995b. “Optimization of Waverider Generated from Conical Flow with Combined Transverse and Longitudinal Curvature.” In 13th Applied Aerodynamics Conference. AIAA 1995-1849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1849
• Lin, Albert, and Steven A. Miller. 2025. “Predictive Modeling of Hypersonic Boundary Layer Transition with Stochastic Distributed Surface Roughness.” In AIAA SCITECH 2025 Forum. AIAA 2025-0519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0519
• Lin, V., B. Strovers, J. Lee, and R. Beck. 2008. “Platform Precision Autopilot Overview and Flight Test Results.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080033977
• Lincoln, John W., and William R. Elliott. 1994. “The USAF Aging Aircraft Program a Short History and Status.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/941231
• Lind, Rick C. 1997. A Presentation on Robust Flutter Margin Analysis and a Flutterometer. NASA/TM-97-206220. NASA. https://ntrs.nasa.gov/citations/19970037547
• Lind, Rick. 1999. “Gain-Scheduled Approximations to H-Infinity Controllers for the F/A-18 Active Aeroelastic Wing.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4205
• Lind, Rick, and Marty Brenner. 1997a. Utilizing Flight Data to Update Aeroelastic Stability Estimates. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/19970040574
• Lind, Rick, and Marty Brenner. 1997b. Worst-Case Flutter Margins from F/A-18 Aircraft Aeroelastic Data. NASA/TM-97-207564. NASA. https://ntrs.nasa.gov/citations/19980036976
• Lind, Rick, and Martin J. Brenner. 1998a. Robust Flutter Margin Analysis That Incorporates Flight Data. NASA/TP-1998-206543. NASA. https://ntrs.nasa.gov/citations/19980041295
• Lind, Rick C., and Martin J. Brenner. 1998b. A Worst-Case Approach for on-Line Flutter Prediction. NASA/TM-1997-207056. NASA. https://ntrs.nasa.gov/citations/19980017615
• Lind, Richard C., and Martin J. Brenner. 2001. On-Line Mu Method for Robust Flutter Prediction in Expanding a Safe Flight Envelope for an Aircraft Model under Flight Test. Patent Number: NASA-Case-DRC-09800-1. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20010054946
• Lind, RIck, and Marty Brenner. 2003. Flight-Test Evaluation of Flutter-Prediction Methods. DRC-01-57. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110023999
• Lind, Rick C., Martin J. Brenner, and Lawrence C. Freudinger. 1997. Improved Flight Test Procedures for Flutter Clearance. NASA/CR-97-207068. NASA. https://ntrs.nasa.gov/citations/19980018481
• Lind, Rick, Marty Brenner, and Lawrence C. Freudinger. 1999. Wavelet Applications for Flight Flutter Testing. H-2364. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/19990061885
• Linden, A. W. 1972. Rotor Systems Research Aircraft of Predesign Study. Volume 1: Summary and Conclusions. NASA-CR-112152. NASA. https://ntrs.nasa.gov/citations/19720025364
• Linden, A. W., and M. W. Hellyar. 1974. “The Rotor Systems Research Aircraft: A Flying Wind Tunnel.” In Canadian Aeronautics and Space Institute and American Institute of Aeronautics and Astronautics, Joint Meeting, Toronto. https://ntrs.nasa.gov/citations/19750027042
• Linderman, D., C. Hoelzer, and P. Howard. 1974. “Test and Evaluation of a Fighter Aircraft in-Flight Thrust Reverser.” In 10th Propulsion Conference. AIAA 1974-1170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1170
• Lindley, D. V. 1956. “On a Measure of the Information Provided by an Experiment.” Annals of Mathematical Statistics 27 (4): 986–1005. https://doi.org/10.1214/aoms/1177728069
• Lindsley, Ned. 2009. “Active Aeroelastic Technology Applied to a Joined Wing Concept with Model Complexity.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5710. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5710
• “Line-by-Line Transport Calculations for Jupiter Entry Probes.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0052.0082
• “Linear Quadratic Flight Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.016
• Ling, Lisa. 2017. “Mid-L/D Lifting Body Entry Demise Analysis.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4210
• Linse, Dennis J. 1991. “Neural Networks for Aircraft System Identification.” In NASA. Langley Research Center, Joint University Program for Air Transportation Research, 1990-1991. https://ntrs.nasa.gov/citations/19920008756
• Lipkens, Bart. 1995. “Application of Model Experiment Data to Test Sonic-Boom Propagation Models.” Journal of the Acoustical Society of America 97 (5_Supplement): 3258–3258. https://doi.org/10.1121/1.411623
• Lipkens, Bart. 2002. “Model Experiment to Study Sonic Boom Propagation through Turbulence. Part III: Validation of Sonic Boom Propagation Models.” Journal of the Acoustical Society of America 111 (1): 509–19. https://doi.org/10.1121/1.1371974
• Litt, Jonathan S. 2026. Power Optimal Control Allocation for Distributed Electric Propulsion in a Series/Parallel Hybrid Powertrain. National Aeronautics and Space Administration. https://doi.org/10.64631/gzky5262
• Littlefield, Alan C., and Gregory S. Melton. 1999. Design, Development,and Testing of Umbillical System Mechanisms for the X-33 Advanced Technology Demonstrator. NASA/TM-1999-208562. NASA. https://ntrs.nasa.gov/citations/20000024930
• Littlefield, Alan C., and Gregory S. Melton. 2000. “Design, Development, and Testing of Umbilical System Mechanisms for the X-33 Advanced Technology Demonstrator.” In 34th Aerospace Mechanisms Symposium. https://ntrs.nasa.gov/citations/20000048412
• Liu, Luoqin. 2022. “A New Similarity Law for Transonic–supersonic Flow.” Physics of Fluids 34 (8): 081705. https://doi.org/10.1063/5.0104406
• Liu, Chuanzhen, Peng Bai, Yanxia Chen, and Bingyan Chen. 2017b. “Research on the Design of Double Swept Waverider.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2140
• Liu, Yan, Junqiang Bai, and Eli Livne. 2015b. “Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap System Action Using Stochastic Kriging.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2421. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2421
• Liu, D. D., P. C. Chen, Lei Tang, K. T. Chang, and Adel Chemaly. 2002. Integrated Hypersonic Aerothermoelastic Methodology for Transatmospheric Vehicle (TAV)/Thermal Protection System (TPS) Structural Design and Optimization. Defense Technical Information Center. https://doi.org/10.21236/ada403577
• Liu, Chuanzhen, Yanhui Duan, Jinsheng Cai, and Guangda Yang. 2014. “Applications of Multi-Block CST Method for Quasi-Waverider Design.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0189. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0189
• Liu, D., and K. Fung. 1987. “Unsteady Transonic Aerodynamics of Oscillating Airfoils in Supersonic Freestream.” In 28th Structures, Structural Dynamics and Materials Conference. AIAA 1987-852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-852
• Liu, Yan, Jun Li, Honggang Zeng, Bo Liu, Nan Liu, and Junqiang Bai. 2017d. “Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap System under Multi-Task Profiles.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-4224. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4224
• Liu, Yi, Shaoxiu Ouyang, and Xiaoxia Zhao. 2019. “Drag Reduction Effect of a Variable Camber Wing of a Transport Aircraft Based on Trailing Edge Flap Deflection of Small Angles.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-13-3305-7_120
• Liu, Chuanzhen, Bai Peng, Bingyan Chen, and Chuqun Ji. 2016b. “Rapid Design and Optimization of Waverider from 3D Flow.” In 16th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2016-3288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3288
• Liu, Yan Chun, Zhen Dong Xu, and Ming Li. 2012a. “Numerical Simulation Study on Longitudinal Aerodynamic Characteristics of a Forward-Swept Wing Air Vehicle.” Applied Mechanics and Materials 263-266: 1880–83. https://doi.org/10.4028/www.scientific.net/amm.263-266.1880
• Liu, Da Wei, Xin Xu, Zhi Wei, and De Hua Chen. 2013. “Engineering Extrapolation to Flight Reynolds Number for Supercritical Airfoil Pressure Distribution Based on CFD Results.” Applied Mechanics and Materials 0: 517–23. https://doi.org/10.4028/www.scientific.net/amm.0.517
• Liu, Zhiyong, Wubing Yang, and Qing Shen. 2016a. “Investigation on Correlation between Wind Tunnel and Flight Test Data for Boundary Layer Transition.” In AIAA Flight Testing Conference. AIAA 2016-3980. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3980
• Liu, Wen, ChenAn Zhang, FaMin Wang, and ZhengYin Ye. 2018. “Design Method of a New Hypersonic Waverider Configuration.” SCIENTIA SINICA Technologica 49 (3): 255–67. https://doi.org/10.1360/n092017-00373
• Liverko A, V., and S. Sboev D. 2024. “Acoustic Noise in Three Tsagi’s Transonic and Supersonic Wind Tunnels.” In 22-St International Conference on the Methods of Aerophysical Research. Crossref. https://doi.org/10.53954/9785605099659_14
• Livingston, C. L. 1965. Wind Tunnel Tests of a Full-Scale Rotor at High Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0619157
• Livingston, F., and J. Williard. 1969. “Planetary Entry Body Heating Rate Measurements in Air and Venus Atmospheric Gas up to T Equal 15,000 Deg K.” In 4th Thermophysics Conference. AIAA 1969-635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-635
• Livne, Eli. 2017. “Active Flutter Suppression: State of the Art and Technology Maturation Needs.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-1119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1119
• Livne, Eli, Nathan Precup, and Marat Mor. 2014. “Design, Construction, and Tests of an Aeroelastic Wind Tunnel Model of a Variable Camber Continuous Trailing Edge Flap (VCCTEF) Concept Wing.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2442. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2442
• Lo, K. W., S. W. Perry, and B. G. Ferguson. n.d. “An Image Processing Approach for Aircraft Flight Parameter Estimation Using the Acoustical Lloyd’s Mirror Effect.” In ISSPA ‘99. Proceedings of the Fifth International Symposium on Signal Processing and its Applications (IEEE Cat. No.99EX359), vol. 2. Queensland Univ. Technol. https://doi.org/10.1109/isspa.1999.815720
• Lobbia, Marcus. 2015. “Optimization of Waverider-Derived Crew Reentry Vehicles Using a Rapid Aerodynamics Analysis Approach.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0757
• Lobbia, Marcus, and Kojiro Suzuki. 2014. “Multidisciplinary Design Optimization of Hypersonic Transport Configurations Using Waveriders.” In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2014-2359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2359
• Lock, R. C. 1957. “A Note on the Application of the Supersonic Area Rule to the Determination of the Wave Drag of Rectangular Wings.” Journal of Fluid Mechanics 2 (6): 575–82. https://doi.org/10.1017/s0022112057000385
• Lock, Andrew, Gerard Armstrong, Flynn Hack, Byrenn Birch, David Buttsworth, and Ingo H. Jahn. 2023. “Optical Aerodynamic Measurements of Hypersonic Free-Flight Using Bayesian State Estimation.” In AIAA AVIATION 2023 Forum. AIAA 2023-3713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3713
• Lockheed-Georgia Co Marietta. 1969. The Hummingbird XV-4B VTOL Research Aircraft Program. Defense Technical Information Center. https://doi.org/10.21236/ad0700436
• Lockman, W. K. 1967. Free-Flight Base Pressure and Heating Measurements on Sharp and Blunt Cones in a Shock Tunnel. NASA. https://ntrs.nasa.gov/citations/19670060153
• Loftin, L. K., Jr. 1967. Research Relating to Long-Range Supersonic Cruising Aircraft. AIAA PAPER 67-748. NASA. https://ntrs.nasa.gov/citations/19670062253
• Loftin, L. K., Jr. 1968. Research Relating to Long-Range Supersonic Cruising Aircraft. AIAA PAPER 67-748. NASA. https://ntrs.nasa.gov/citations/19680053730
• Logan, T. 1974. “Costs and Benefits of Composite Material Applications to a Civil STOL Aircraft.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-964. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-964
• Lohr, Sharon L. 1995. “Optimal Bayesian Design of Experiments for the One-Way Random Effects Model.” Biometrika 82 (1): 175. https://doi.org/10.2307/2337637
• Lokos, William A. 1990. “Predicted and Measured in-Flight Wing Deformations of a Forward-Swept-Wing Aircraft.” In Society of Flight Test Engineers. https://ntrs.nasa.gov/citations/19920053312
• Lokos, William A., Andrew Lizotte, Ned J. Lindsley, and Rick Stauf. 2005. Shock Location Dominated Transonic Flight Loads on the Active Aeroelastic Wing. NASA/ TM-2005-213667. NASA. https://ntrs.nasa.gov/citations/20060002813
• Lokos, William, Eric Miller, Larry Hudson, Andrew Holguin, David Neufeld, and Ronnie Haraguchi. 2015. “Strain Gage Loads Calibration Testing with Airbag Support for the Gulfstream III SubsoniC Research Aircraft Testbed (SCRAT).” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160000200
• Lokos, William, Candida Olney, Natalie Crawford, Rick Stauf, and Eric Reichenbach. 2002. “Wing Torsional Stiffness Tests of the Active Aeroelastic Wing F/A-18 Airplane.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1333
• Lombardi, G., M. Salvetti, A. Talamelli, M. Salvetti, A. Talamelli, and G. Lombardi. 1997. “Shock-Wave/boundary-Layer Interaction in Transonic Flow around a Forward-Swept Wing.” In 28th Fluid Dynamics Conference. AIAA 1997-1838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1838
• Londenberg, W. 1993. “Turbulence Model Evaluation for the Prediction of Flows over a Supercritical Airfoil with Deflected Aileron at High Reynolds Number.” In 31st Aerospace Sciences Meeting. AIAA 1993-191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-191
• London, John, III, and Phil Sumrall. 1999. Future X Pathfinder: Quick, Low Cost Flight Testing for Tomorrow’s Launch Vehicles. IAF-99-V.4.02. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990116207
• Londono, Monica, and Bret Leonhardt. 2012. “Parameter Identification of an Executive Transport Aircraft: Simulation Update and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4734
• Long, P. 1968. “Derivative Aircraft Model Testing Challenges Flight Test Ingenuity.” In 2nd Simulation and Support Conference. AIAA 1968-264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-264
• Long, Wei, Yan Liu, and Jia Ming Cao. 2014. “Wing Flutter Analysis Parameters during Flight.” Applied Mechanics and Materials 722: 93–96. https://doi.org/10.4028/www.scientific.net/amm.722.93
• “Longitudinal and Lateral Linear Stability and Control.” 2014. In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/b17346-10
• “Longitudinal Control and Trim Theory and Flight Test Methods.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0275.0284
• Longo, Jose. 2008. “Aerothermodynamics Issues of the DLR Hypersonic Flight Experiment SHEFEX-I (Invited).” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-4038. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4038
• Longstaff, R. 1995. “The Challenge of an International Aerospace Plane Project.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6074
• Lonkar, Sumit, and Pratikash Panda. 2025. “Mode Transition and Combustion-Induced Shock Train Dynamics in a Cavity-Based Dual-Mode Scramjet.” Preprint, . https://doi.org/10.2139/ssrn.5902346
• Lonzaga, Joel B. 2021. “Validation of a Sonic Boom Model through Atmospheric Turbulence with Flight Test Data.” Journal of the Acoustical Society of America 150 (4_Supplement): A91-A91. https://doi.org/10.1121/10.0007730
• López-Fidalgo, Jesús. 2023. “Bayesian Optimal Designs.” In Lecture Notes in Statistics. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-35918-7_4
• Lopez-Toledo, A. A., and M. Athans. 1974. On the Design of Optimal Input Signals in System Identification. NASA-CR-137383. NASA. https://ntrs.nasa.gov/citations/19740012058
• Lorang, Tony, and John Carr. 2017. “C-17A Globemaster III Aft Fuselage Drag Reduction Flight Demonstrations.” In AIAA Flight Testing Conference. AIAA 2017-3653. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3653
• Loschke, P. C., M. R. Barber, E. K. Enevoldson, and T. C. McMurtry. 1974. Flight Evaluation of Advanced Control Systems and Displays on a General Aviation Airplane. NASA-TN-D-7703. NASA. https://ntrs.nasa.gov/citations/19740019386
• Loschke, P. C., M. R. Barber, C. R. Jarvis, and E. K. Enevoldson. 1972. “Flight Evaluations of the Effect of Advanced Control Systems and Displays on the Handling Qualities of a General Aviation Airplane.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19720041914
• Loth, J., J. Fanucci, and S. Roberts. 1974. “Flight Performance of a Circulation Controlled STOL.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-994. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-994
• Loubeau, Alexandra, Jonathan Rathsam, and Jacob Klos. 2013. “Evaluation of an Indoor Sonic Boom Subjective Test Facility at NASA Langley Research Center.” In Proceedings of Meetings on Acoustics. Acoustical Society of America. https://doi.org/10.1121/1.4810766
• Love, J. E. 1964. X-15: Past and Future. SAE PAPER 650657. NASA. https://ntrs.nasa.gov/citations/19660032948
• Love, Robert D. 2022. “Enabling Local Aerial Mobility (LAM): Design of an Ultralight Solar Distributed-Electric-Propulsion Short-Takeoff-and-Landing (STOL) Aircraft Recumbent-Electric-Bike Hybrid.” In AIAA AVIATION 2022 Forum. AIAA 2022-3208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3208
• Love, J. E., and W. R. Young. 1966. Component Performance and Flight Operations of the X-15 Research Airplane Program. NASA. https://ntrs.nasa.gov/citations/19670032612
• Lovejoy, Andrew E. 2026. “Metal Laser Marking for Wind Tunnel Model Displacement Measurements Using Digital Image Correlation.” In AIAA SCITECH 2026 Forum. AIAA 2026-2356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2356
• Lovell, D. 1999. “European Research to Reduce Drag for Supersonic Transport Aircraft.” In 17th Applied Aerodynamics Conference. AIAA 1999-3100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3100
• Lovholt, Finn. 2021. “2pPA1: Building Vibration Due to Sonic Boom – Results from Simulations and Field Measurements.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f2484
• Loving, Donald L. 1961. A Wind-Tunnel Investigation of a Transonic-Transport Configuration Utilizing Drag-Reducing Devices at Mach Numbers from 0.20 to 1.03. NASA-TN-D-636. NASA. https://ntrs.nasa.gov/citations/20040008071
• Loving, D. L. 1966. Wind-Tunnel-Flight Correlation of Shock-Induced Separated Flow. NASA-TN-D-3580. NASA. https://ntrs.nasa.gov/citations/19660028007
• “Low Drag Airfoil Design Utilizing Passive Laminar Flow and Coupled Diffusion Control.” 1980. In Viscous Flow Drag Reduction. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865466.0212.0232
• Lowry, John. 1995. “The Bootstrap Approach to Predicting Airplane Flight Performance.” Journal of Aviation/Aerospace Education & Research. https://doi.org/10.15394/jaaer.1995.1167
• Lozino-Lozinsky, G., E. Dudar, V. Chvanov, and B. Katorgin. 1996. “MAKS-D Experimental Rocket Powered Plane: Demonstrator of Technologies.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4573. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4573
• Lu, Ping. 1991. “Trajectory Optimization and Guidance for a Hypersonic Vehicle.” In 3rd International Aerospace Planes Conference. AIAA 1991-5068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-5068
• Lu, Ping. 2005. “Asymptotic Analysis of Quasi-Equilibrium Glide in Lifting Entry Flight.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6128
• Lu, H., and S. Lanter. 1980. “Simulation of High Bypass Ratio Engine Jet Noise Flight Effects by Model Jet Wind Tunnel Test.” In 6th Aeroacoustics Conference. AIAA 1980-1030. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1030
• Lu, Chen, Rong-Bing Li, Jian-Ye Liu, and Ting-Wan Lei. 2018. “Air Data Estimation by Fusing Navigation System and Flight Control System.” Journal of Navigation 71 (5): 1231–46. https://doi.org/10.1017/s037346331800022x
• Lu, Yifei, Zhigang Wang, Qi Wu, Yu Yang, and Gang Liu. 2025. “Design and Verification of Multi-Mode Variable Camber Wing Trailing Edge.” In 2nd International Conference on Green Aviation (ICGA 2024). MDPI. https://doi.org/10.3390/engproc2024080045
• Lu, Pong-Jeu, and Dun-Yann Yeh. 1993. “Transonic Flutter Suppression Using Active Acoustic Excitations.” In 3rd Shear Flow Conference. AIAA 1993-3285. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3285
• Lucas, E., A. Fanning, and L. Steers. 1978. “Comparison of Nozzle and Afterbody Surface Pressures from Wind Tunnel and Flight Test of the YF-17 Aircraft.” In 14th Joint Propulsion Conference. AIAA 1978-992. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-992
• Luckert, H. 1973. “Static Stability and Drag Studies for Bodies of Revolution in Supersonic Flow.” In 3rd Sounding Rocket Technology Conference. AIAA 1973-295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-295
• Luckring, J. M. 2002. “Reynolds Number and Leading-Edge Bluntness Effects on a 65 Deg Delta Wing.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20020016863
• Luckring, J. M. 2003. “Transonic Reynolds Number and Leading-Edge Bluntness Effects on a 65 Deg Delta Wing.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030013954
• Luckring, James M. 2004. “Reynolds Number, Compressibility, and Leading-Edge Bluntness Effects on Delta-Wing Aerodynamics.” In 24th International Congress of the Aeronautical Sciences. https://ntrs.nasa.gov/citations/20040110336
• Luckring, James M., Charles H. Fox Jr., and Jeffrey S. Cundiff. 1989. “Reynolds Number Effects on the Transonic Aerodynamics of a Slender Wing-Body Configuration.” In Transonic Symposium: Theory, Application and Experiment, Volume 2. https://ntrs.nasa.gov/citations/19910014821
• Luckring, J. M., and T. A. Ghee. 2001. Subsonic Reynolds Number Effects on a Diamond Wing Configuration. AIAA Paper 2001-0907. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010011041
• Luers, James K., and Ira B. Fiscus. 1984. Nozzle Tests for Simulating Heavy Rain in a Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada139566
• Lugo, Rafael A., Robert Tolson, and Robert Blanchard. 2014. “Statistical Entry, Descent, and Landing Flight Reconstruction with Flush Air Data System Observations Using Inertial Navigation and Monte Carlo Techniques.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0388. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0388
• Lundstrom, Reginald R., and Hal T. Baber Jr. 1956. Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined from Flight Test for a Mach Number Range of 1.1. to 1.8. NACA-RM-L55L16. NASA. https://ntrs.nasa.gov/citations/19930089027
• Lundstrom, Reginald R., William T. Lauten Jr., and Ellwyn E. Angle. 1948. Transonic-Flutter Investigation of Wings Attached to Two Low-Acceleration Rocket-Propelled Vehicles. NACA-RM-L8I30. NASA. https://ntrs.nasa.gov/citations/19930085467
• Luo, Shibin, Wencai Luo, Zhiyong Lin, and Zhengguo Wang. 2003. “Application of Taguchi Design Methods and Uniform Design Methods to Scramjet Propulsion System Optimization for Hypersonic Cruise Vehicle.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5193
• Luoma, Arvo A. 1954. Longitudinal Stability and Control Characteristics at Transonic Speeds of a 1/30-Scale Model of the Republic XF-103 Airplane. NACA-RM-SL54H24. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023318
• Luquet, David. n.d. “3D Simulation of Acoustical Shock Waves Propagation through a Turbulent Atmosphere. Application to Sonic Boom.” PhD diss., Paris 6. https://doi.org/10.70675/97718b5bz3a9cz4170z9f07z1f209f6220d1
• Luria, Capt F., and R. Guyton. 1992. “Flight Testing of Pneumatic Forebody Vortex Control on the X-29 Technology Demonstrator.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/922008
• Lusty, A. H., Jr. 1966. Lifting Bodies of Minimum Drag in Hypersonic Flow. NASA-CR-77177. NASA. https://ntrs.nasa.gov/citations/19660025387
• Luu, Anh Quan. 2025. “Design Optimization of a Blended-Wing-Body Aircraft with Integrated Fan-in-Wing.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/29170238
• Lux, Jessica, and Darryl A. Burkes. 2008. Hyper-X (X-43A) Flight Test Range Operations Overview. NASA/TM-2008-214626. NASA. https://ntrs.nasa.gov/citations/20080007525
• Lux, Jessica, Bob Downing, and Jack Sheldon. 2007. “Design of a Mission Data Storage and Retrieval System for NASA Dryden Flight Research Center.” In International Telemetry Conference (ITC) 2007. https://ntrs.nasa.gov/citations/20070034159
• Lux-Baumann, Jessica, and Darryl A. Burkes. 2005. “Hyper-X (X-43A) Flight Test Range Operations.” In International Telemetering Conference. https://ntrs.nasa.gov/citations/20050237906
• Lux-Baumann, Jessica, and Darryl Burkes. 2006. Hyper-X (X-43A) Flight Test Range Operations Overview. DFRC-580. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090007796
• Lux-Baumann, Jessica R., Ray A. Dees, and David J. Fratello. 2006a. “Control Room Training for the Hyper-X Program Utilizing Aircraft Simulation.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20060027798
• Lux-Baumann, Jesica, Ray Dees, and David Fratello. 2006b. Control Room Training for the Hyper-X Project Utilizing Aircraft Simulation. NASA/TM-2006-213685. NASA. https://ntrs.nasa.gov/citations/20060053371
• Lykins, Ryan, and Shahriar Keshmiri. 2010. “System Identification of a COTS Autopilot System Using Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7648
• Lympany, Shane V., and Juliet A. Page. n.d. “Influence of Atmospheric Variability on Predicted Sonic Boom Metrics.” In 186th Meeting of the Acoustical Society of America. https://ntrs.nasa.gov/citations/20240005397
• Lympany, Shane V., and Juliet A. Page. 2024. “Acoustic Measurements of Full-Scale Electric Vertical Takeoff and Landing Aircraft.” Journal of the Acoustical Society of America 155 (3_Supplement): A152-A152. https://doi.org/10.1121/10.0027133
• Lynch, R., and W. Rogers. 1976. “Aeroelastic Tailoring of Composite Materials to Improve Performance.” In 17th Structures, Structural Dynamics, and Materials Conference. AIAA 1976-1505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1505
• Lynch, G., Jr. 1972. “A-X Air Force Flight Evaluation.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-770. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-770
• Lynde, Michelle N., Richard L. Campbell, Brett R. Hiller, and Lewis R. Owens. 2021. “Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article.” In AIAA Scitech 2021 Forum. AIAA 2021-0173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0173
• Lyons, M., R. Vepa, S. McIntosh Jr., and D. Debra. 1973. “Control Law Synthesis and Sensor Design for Active Flutter Suppression.” In Guidance and Control Conference. AIAA 1973-832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-832
• Lyu, Yuchao, Chongwen Jiang, Shuyao Hu, and Zhenxun Gao. 2018. “Improved Design of Waverider Based on Mach Line Cutting of Compression Surfaces.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0279
• M2-F2 Lifting Body Accident Summary. 1967. NASA NEWS RELEASE-67-205. NASA. https://ntrs.nasa.gov/citations/19670022976
• Ma, Edward. 1992. “A Transonic/supersonic/hypersonic CFD Analysis of the Entry Space Shuttle Orbiter.” In 10th Applied Aerodynamics Conference. AIAA 1992-2614. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2614
• Ma, Binlin, Xinbing Su, Taorui Li, and Ning Wang. 2017b. “Numerical Study on Influence of Canard on Static Aeroelastic Characteristics of Forward-Swept Wing.” In Proceedings of the 2017 International Conference on Mechanical, Electronic, Control and Automation Engineering (MECAE 2017). Atlantis Press. https://doi.org/10.2991/mecae-17.2017.72
• Ma, Xiaoyong, Shidong Zhong, Yu Xiao, Wei Li, Zhigang Zhang, and Yi Zhang. 2017a. “Aerodynamic Performance Analysis of a New Conception Hypersonic Aircraft.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2171
• Mabe, James, Darren Hartl, Dimitris Lagoudas, Benjamin McAdams, and Ryan Trout. 2023. “Sma Based Adaptive Structure Demonstrator for an Overland Low Boom Supersonic Vehicle.” In 10th ECCOMAS Thematic Conference on Smart Structures and Materials. Dept. of Mechanical Engineering & Aeronautics University of Patras. https://doi.org/10.7712/150123.9791.444611
• Mabius, L., and H. Kaufman. 1976. An Adaptive Flight Controller for the F-8 without Explicit Parameter Identification. Analytic Sciences Corporation. https://ntrs.nasa.gov/citations/19770045952
• MacDonald, Adam, and Michael Shepherd. 2008. “Development and Flight Test of a Reconfigurable Avionics Research Pod for the USAF Test Pilot School and Air Force Institute of Technology.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1604
• Macgregor, R. K. 1971. Limitations in Thermal Scale Modeling. NASA. https://ntrs.nasa.gov/citations/19710047291
• Mach, Number, and Reynolds. 2022. “Mach Number & Reynolds Number.” In Introduction to Aerospace Flight Vehicles. Embry-Riddle Aeronautical University. https://doi.org/10.15394/eaglepub.2022.1066.n13
• Machida, Shigeru, Kenji Yoshida, and Takeshi Ohnuki. 2007. “Supersonic Flight Testing of Unmanned Experimental Airplane for Next-Generation SST.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-854. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-854
• Machin, Ricardo, Jenny Stein, and John Muratore. 1999. “An Overview of the X-38 Prototype Crew Return Vehicle Development and Test Program.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1703. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1703
• Machnik, A., T. Decker, and R. Ashworth. 2022. “4.2 Tailoring Flight Test Instrumentation with Additive Manufacturing.” In Proceedings - ettc2022. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2022/4.2
• Mack, Pamela E. 1998. From Engineering Science to Big Science: The NACA and NASA Collier Trophy Research Project Winners. NASA/SP-1998-4219. NASA. https://ntrs.nasa.gov/citations/20000012419
• Mack, R., and C. Darden. 1979. “Some Effects of Applying Sonic Boom Minimization to Supersonic Cruise Aircraft Design.” In 5th Aeroacoustics Conference. AIAA 1979-652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-652
• Mackall, D., M. Pickett, L. Schilling, and C. Wagner. 1988. “The NASA Integrated Test Facility and Its Impact on Flight Research.” In 4th Flight Test Conference. AIAA 1988-2095. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2095
• Mackall, Dale A., Robert Sakahara, and Steven E. Kremer. 1998. The X-33 Extended Flight Test Range. NASA/TM-1998-206557. NASA. https://ntrs.nasa.gov/citations/19980236873
• Mackle, Kieran. n.d. “Co-Design of Hypersonic Vehicle Shape and Trajectory.” PhD diss., University of Queensland Library. https://doi.org/10.14264/f113470
• Mackle, Kieran, and Ingo Jahn. 2024. “Efficient and Flexible Methodology for the Aerodynamic Shape Optimization of Hypersonic Vehicle Concepts in a High-Dimensional Design Space.” In AIAA SCITECH 2024 Forum. AIAA 2024-2838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2838
• Macmillan, A. 1981. “Navstar Global Positioning System Flight Test Program Overview.” In 1st Flight Test Conference. AIAA 1981-2350. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2350
• Macpherson, Duncan. 1962. An Explicit Solution to the Powered Flight Dynamics of a Rocket Vehicle. Defense Technical Information Center. https://doi.org/10.21236/ad0293892
• Macquart, Terence, Noud Werter, and Roeland De Breuker. 2016. “Aeroelastic Tailoring of Blended Composite Structures Using Lamination Parameters.” In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2016-1966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1966
• Macwilkinson, D. G., W. T. Blackerby, and J. H. Paterson. 1974a. Correaltion of Full-Scale Drag Predictions with Flight Measurements on the C-141A Aircraft. Phase 2: Wind Tunnel Test, Analysis, and Prediction Techniques. Volume 1: Drag Predictions, Wind Tunnel Data Analysis and Correlation. NASA-CR-2333. NASA. https://ntrs.nasa.gov/citations/19740010566
• Macwilkinson, D. G., W. T. Blackerby, and J. H. Paterson. 1974b. Correlation of Full-Scale Drag Predictions with Flight Measurements on the C-141A Aircraft: Phase 2: Wind Tunnel Tests, Analysis, and Prediction Techniques. Volume 2: Wind Tunnel Test and Basic Data. NASA-CR-2334. NASA. https://ntrs.nasa.gov/citations/19740010567
• Madagan, A. 1969. “Free-Flight Investigation of the Aerodynamic Characteristics of a 10-Deg Semiangle Cone at Mach Numbers from 6 to 16.” In 7th Aerospace Sciences Meeting. AIAA 1969-133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-133
• Maddalon, D. V. 1966. Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects. NASA-TN-D-3320. NASA. https://ntrs.nasa.gov/citations/19660010304
• Maddalon, D., C. Land, F. Collier, and L. Montoya. 1989. “Transition Flight Experiments on a Swept Wing with Suction.” In 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1989-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1893
• Maddalon, D., and R. Wagner Jr. 1969. “Influence of Measured Freestream Disturbances on Hypersonic Boundary-Layer Transition.” In 2nd Fluid and Plasma Dynamics Conference. AIAA 1969-704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-704
• Madhusudana Rao, V., K. Singh Chowhan, V. Patel, N. Prasad, and P. Subramanyam. 2014. “7.4: Challenges in Design and Development of Indigenous Flight Test Instrumentation System for a High Performance Fighter Aircraft.” In Proceeding - etc2014. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/etc2014/7.4
• Madsen, A. P. 1982. “F-16E Program Overview and Wind Tunnel/flight Correlation.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017331
• Madsen, C., and C. Cerimele. 2000. “Updated Flight Performance and Aerodynamics from a Large Scale Parafoil Test Program.” In Modeling and Simulation Technologies Conference. AIAA 2000-4311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4311
• Madzsar, George C., Randall L. Bickford, and David B. Duncan. 1994. “Instrumentation for in-Flight SSME Rocket Engine Plume Spectroscopy.” In AIAA, ASME, SAE, and ASEE. https://ntrs.nasa.gov/citations/19940030762
• Maestrello, L., A. Bayliss, S. M. Mangalam, and M. R. Malik. 1986. Boundary Layer Transition. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880005560
• Magee, John, and Robert Taylor. 1971. Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model. Volume 4. Part 2. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details. Defense Technical Information Center. https://doi.org/10.21236/ad0735733
• Magee, J., and K. Wernicke. 1979a. “XV-15 Flight Test Results Compared with Design Goals.” In Aircraft Systems and Technology Meeting. AIAA 1979-1839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1839
• Magee, J., and K. Wernicke. 1979b. “XV-15 Tilt Rotor Research Aircraft: Program Report.” In Atlantic Aeronautical Conference. AIAA 1979-704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-704
• Maglieri, D. J. 1967. Sonic Boom Flight Research: Some Effects of Airplane Operations and the Atmosphere on Sonic Boom Signatures. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19680011947
• Maglieri, Domenic J., Herbert R. Henderson, Steven J. Massey, and Eugene G. Stansbery. 2011a. A Compilation of Space Shuttle Sonic Boom Measurements. NASA/CR-2011-217080. NASA. https://ntrs.nasa.gov/citations/20110011322
• Maglieri, Domenic J., Herbert R. Henderson, Steven J. Massey, and Eugene G. Stansbery. 2011b. A Compilation of Space Shuttle Sonic Boom Measurements: Supplemental STS Sonic Boom Files. NASA/CR-2011-217080/Suppl. NASA. https://ntrs.nasa.gov/citations/20110012383
• Maglieri, Domenic J., and Kenneth J. Plotkin. 1991. Sonic Boom. No Number:. Eagle Engineering, Inc. https://ntrs.nasa.gov/citations/19920001390
• Maglieri, Domenic J., Victor E. Sothcott, and John Hicks. 1990. Influence of Vehicle Configuration and Flight Profile on X-30 Sonic Booms. AIAA PAPER 90-5224. Eagle Engineering, Inc. https://ntrs.nasa.gov/citations/19910029827
• Magruder, William. 1964. “Operation of Supersonic Transport at Airports.” Journal of the Aero-Space Transport Division 90 (2): 31–51. https://doi.org/10.1061/jatdaz.0000035
• Mahaffey, P. T. 1975. “Flight Flutter Testing the B-58 Airplane.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003023
• Mahale, Amrita, and Narayan Ananthkrishnan. 2006. “Analytical Criterion for Onset of Departure in Inertia-Coupled Roll Maneuvers of Airplanes.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6267
• Mahesh, J., C. Stone, W. Garrard, and H. Dunn. 1980. “Active Flutter Suppression Using Linear Quadratic Gaussian Theory.” In Guidance and Control Conference. AIAA 1980-1758. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1758
• Mahzari, Milad, Todd R. White, Robert Braun, and Deepak Bose. 2013. “Inverse Estimation of the Mars Science Laboratory Entry Aerothermal Environment and Thermal Protection System Response.” In 44th AIAA Thermophysics Conference. AIAA 2013-2780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2780
• Maine, R. 1977. “Maximum Likelihood Estimation of Aerodynamic Derivatives for an Oblique Wing Aircraft from Flight Data.” In Guidance and Control Conference. AIAA 1977-1135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1135
• Maine, Trindel, Glenn Gilyard, and Heather Lambert. 1990. “A Preliminary Evaluation of an F100 Engine Parameter Estimation Process Using Flight Data.” In 26th Joint Propulsion Conference. AIAA 1990-1921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1921
• Maine, R. E., and K. W. Iliff. 1980. “Estimation of the Accuracy of Dynamic Flight-Determined Coefficients.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800033530
• Maine, R. E., and K. W. Iliff. 1981. The Theory and Practice of Estimating the Accuracy of Dynamic Flight-Determined Coefficients. NASA-RP-1077. NASA. https://ntrs.nasa.gov/citations/19810019327
• Maine, R., and K. Iliff. 1982. “Selected Stability and Control Derivatives from the First Three Space Shuttle Entries.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1318
• Maine, Richard E., and Kenneth W. Iliff. 1986. Application of Parameter Estimation to Aircraft Stability and Control: The Output-Error Approach. NASA-RP-1168. NASA. https://ntrs.nasa.gov/citations/19870020066
• Maine, R., and J. Murray. 1986. “Application of Parameter Estimation to Highly Unstable Aircraft.” In Astrodynamics Conference. AIAA 1986-2020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2020
• Maine, Trindel, Peter Schaefer, John Burken, and Frank Burcham. 1994. “Design Challenges Encountered in a Propulsion-Controlled Aircraft Flight Test Program.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-3359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3359
• Maisel, M., and D. Harris. 1981. “Hover Tests of the XV-15 Tilt Rotor Research Aircraft.” In 1st Flight Test Conference. AIAA 1981-2501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2501
• Makarewicz, Rufin. 2024. “Double Sonic Boom of an Aerial Bomb and a Ballistic Missile.” Preprint, . https://doi.org/10.2139/ssrn.4835330
• Makino, Y., Z. Lei, and T. Iwamiya. 2002. “Nacelle Design Study of a Supersonic Experimental Airplane Using Aerodynamic Shape Optimization.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-105
• Makino, Yoshikazu, and Masayoshi Noguchi. 2003. “Sonic-Boom Research Activities on Unmanned Scaled Supersonic Experimental Airplane (Invited).” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3574
• Makino, Yoshikazu, Takaaki Sugiura, Tadaharu Watanuki, et al. 1997. “The Effect of Nose Bluntness of a Low-Boom Configuration on Sonic-Boom.” In 15th Applied Aerodynamics Conference. AIAA 1997-2213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2213
• Malcolm, Gerald, and Robert Nelson. 1987. “Comparison of Water and Wind Tunnel Flow Visualization Results on a Generic Fighter Configuration at High Angles of Attack.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2423
• Malcolm, G., and A. Skow. 1986. “Enhanced Controllability through Vortex Manipulation on Fighter Aircraft at High Angles of Attack.” In 13th Atmospheric Flight Mechanics Conference. AIAA 1986-2277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2277
• Malcom, L., and J. Husband. 1976. “Digital Flight Control for the NASA 737 Airplane.” In Guidance and Control Conference. AIAA 1976-1912. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1912
• Malik, Mujeeb. 1987. “Prediction and Control of Transition in Hypersonic Boundary Layers.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1414
• Malik, M. R. 2000. “Hypersonic Boundary-Layer Receptivity and Stability.” In Laminar-Turbulent Transition. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-03997-7_61
• Malik, M., T. Zang, and D. Bushnell. 1990. “Boundary Layer Transition in Hypersonic Flows.” In 2nd International Aerospace Planes Conference. AIAA 1990-5232. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-5232
• Mallen, Joseph, and Paul Dancik. 1959. “The Tilt-Wing Propeller VTOL Aircraft Present Status and Future Role.” Journal of the American Helicopter Society 4 (1): 15–19. https://doi.org/10.4050/jahs.4.15
• Mallik, Wrik, Rakesh K. Kapania, and Joseph A. Schetz. 2013. “Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Aircraft with Flutter Constraint.” In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2013-1454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1454
• Malloy, Donald, Andrew Hughes, and David Kidman. 2010. “Techniques for Integrating Ground and Flight Test and Modeling and Simulation to Improve Aircraft Propulsion Acquisition.” In U.S. Air Force T&E Days 2010. AIAA 2010-1718. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1718
• Mallozzi, Lina, Pierluigi De Paolis, Gabriele Di Francesco, and Alessandro d’Argenio. 2014. “Computational Results for Flight Test Points Distribution in the Flight Envelope.” In Computational Methods in Applied Sciences. Springer International Publishing. https://doi.org/10.1007/978-3-319-11541-2_26
• Malmuth, N. 1984. “An Asymptotic Theory of Wind Tunnel Wall Interference on Subsonic Slender Bodies.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1625. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1625
• Malmuth, N. D., and J. D. Cole. 1984. Study of Asymptotic Theory of Transonic Wind Tunnel Wall Interference. Defense Technical Information Center. https://doi.org/10.21236/ada141431
• Malmuth, N., C. Wu, and J. Cole. 1986. “Transonic Wave Drag Estimation and Optimization Using the Nonlinear Area Rule.” In 4th Applied Aerodynamics Conference. AIAA 1986-1798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1798
• Malyuta, Danylo, Taylor Reynolds, Michael Szmuk, Mehran Mesbahi, Behcet Acikmese, and John M. Carson. 2019. “Discretization Performance and Accuracy Analysis for the Rocket Powered Descent Guidance Problem.” In AIAA Scitech 2019 Forum. AIAA 2019-0925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0925
• Man, Jun, Jiangjiang Zhang, Weixuan Li, Lingzao Zeng, and Laosheng Wu. 2016. “Sequential Ensemble-Based Optimal Design for Parameter Estimation.” Water Resources Research 52 (10): 7577–92. https://doi.org/10.1002/2016wr018736
• Manan, Abdul, and Jonathan Cooper. 2008. “Uncertainty of Composite Wing Aeroelastic Behaviour.” In 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2008-5868. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-5868
• Mandal, Tanmay, and Yu Gu. 2016. “Online Pilot Model Parameter Estimation Using Sub-Scale Aircraft Flight Data.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0636
• Manela, J. 1983. “Interaction of Multiple Supersonic Jets with a Transonic Flow Field.” In 16th Fluid and Plasmadynamics Conference. AIAA 1983-1680. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1680
• “Maneuvering Re-Entry Vehicles: Particle Motion.” 1993. In Dynamics of Atmospheric Re-Entry. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861741.0239.0280
• Mangalam, Arun, and Mark Davis. 2009. “Ground/Flight Correlation of Aerodynamic Loads with Structural Response.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-881. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-881
• Mangalam, Siva, Peter Flick, and Martin Brenner. 2007. “Higher Level Aerodynamic Input for Aeroservoelastic Control of Flexible Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6380
• Mangalam, Arun, Christine Jutte, and Marty Brenner. 2010. “Aerodynamic and Structural Measurement of the Aerostructures Test Wing for Flutter Testing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8113
• Mangalam, S., and W. Pfenninger. 1984. “Wind-Tunnel Tests on a High Performance Low-Reynolds Number Airfoil.” In 13th Aerodynamic Testing Conference. AIAA 1984-628. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-628
• Mani, Mori, Ben Rider, Anthony Sclafani, et al. 2010. “RANS Technology for Transonic Drag Prediction; a Boeing Perspective of the 4th Drag Prediction Workshop.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4221
• Manke, J. A., and M. V. Love. 1975. X-24B Flight Test Program. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19760035693
• Manke, John A., John P. Retelle, and Robert W. Kempel. 1970. “Assessment of Lifting Body Vehicle Handling Qualities.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000630
• Mann, Michael J., Jarrett K. Huffman, and Charles H. Fox Jr. 1987. Subsonic Longitudinal and Lateral-Directional Characteristics of a Forward-Swept-Wing Fighter Configuration at Angles of Attack up to 47 Deg. NASA-TP-2727. NASA. https://ntrs.nasa.gov/citations/19870017441
• Mann, M., and C. Mercer. 1985. “A Forward-Swept Wing Configuration Designed for High Maneuverabilityby Use of Three-Dimensional Transonic Theory.” In 3rd Applied Aerodynamics Conference. AIAA 1985-4069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4069
• Mann, M. J., and C. E. Mercer. 1986. Forward-Swept Wing Configuration Designed for High Maneuverability by Use of a Transonic Computational Method. NASA-TP-2628. NASA. https://ntrs.nasa.gov/citations/19870002269
• Manning, Clarke, Kurt Baum, Christopher Greek, and Jeffrey Braun. 1992. “The Enhanced Flight Screener Operational Demonstration Flight Test Program.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4115
• Manning, E, Thomas, II, Clifford Ratliff, and Edward Marquart. 1995. “Bridging the Gap between Ground and Flight Tests: Virtual Flight Testing (VFT).” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3875
• Maples, Dupree. 1979. Aerodynamic Heating of Conventional Weapons. Defense Technical Information Center. https://doi.org/10.21236/ada069807
• Marchinski, L. 1974. “Aircraft Structures Designed to Cost.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-962. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-962
• Marcum, David L. 2001. Computational Simulation of Unsteady, Viscous, Hypersonic Flow about Flight Vehicles with Store Separation. Defense Technical Information Center. https://doi.org/10.21236/ada387492
• Marcy, William L., Harriet J. Stephenson, and Thomas V. Cooney. 1956. Analysis of the Vertical-Tail Loads Measured during a Flight Investigation at Transonic Speeds of the Douglas X-3 Research Airplane. NACA-RM-H56H08. NASA. https://ntrs.nasa.gov/citations/19930090115
• Maria-Agneta, Balint, and Balint Stef. 2011. “Oscillation Susceptibility of an Unmanned Aircraft Whose Automatic Flight Control System Fails.” In Advances in Flight Control Systems. InTech. https://doi.org/10.5772/14936
• Marineau, Eric C. 2016. “Prediction Methodology for 2nd Mode Dominated Boundary Layer Transition in Hypersonic Wind Tunnels.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0597. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0597
• Markhotok, Anna. 2021. “Wave Drag Modification in the Presence of Discharges.” In Aerodynamics. IntechOpen. https://doi.org/10.5772/intechopen.86858
• Markman, S. 1984. “Considerations in the Use of in-Flight and Ground Based Simulation.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2102
• Markman, Steven. 1989. “In-Flight and Ground Based Simulation: Capabilities and Limitations.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1989-3328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3328
• Markopoulos, Nikos, and Kenneth Mease. 1990. “Thrust Law Effects on the Longitudinal Stability of Hypersonic Cruise.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2820
• Marlow, Michael. 2003. “Highly Operable Propulsion for Reusable Launch Vehicle Applications.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5281
• Marmel, Frédéric. 2021. “2pPA3: Impact of Low Sonic Boom Exposure on Psychophysical and Cognitive Performance.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f248a
• Marmie, John, Andres Martinez, and Andrew Petro. 2015. Propulsion Technology Demonstrator. NASA FS-2015-03-23-ARC. NASA. https://ntrs.nasa.gov/citations/20150016065
• Marques, Pascual. 2013. “Flight Stability and Control of Tailless Lambda Unmanned Aircraft.” International Journal of Unmanned Systems Engineering 1 (2): 1–4. https://doi.org/10.14323/ijuseng.2013.5
• Marschalk, Sven, Peter C. Luteijn, Dirk van Os, Daan M. Pool, and Coen C. de Visser. 2021. “Stall Buffet Modeling Using Swept Wing Flight Test Data.” In AIAA Scitech 2021 Forum. AIAA 2021-0286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0286
• Marschall, Jochen. 2011. Testing and Modeling Ultra-High Temperature Ceramic (UHTC) Materials for Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada553782
• Marshall, R. T. 1971. Flight Determined Acceleration and Climb Performance of an F-104G Airplane for Use in an Optimum Flight Path Computer Program. NASA-TN-D-6398. NASA. https://ntrs.nasa.gov/citations/19710017526
• Marshall, Laurie. 2000. “Summary of Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment.” In 18th Applied Aerodynamics Conference. AIAA 2000-4418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4418
• Marshall, Laurie A., Catherine Bahm, Griffin P. Corpening, and Robert Sherrill. 2005b. Overview with Results and Lessons Learned of the X-43A Mach 10 Flight. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20050175679
• Marshall, Laurie, Griffin Corpening, and Robert Sherrill. 2005a. “A Chief Engineer’s View of the NASA X-43A Scramjet Flight Test.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3332
• Marshall, R. T., and W. G. Schweikhard. 1973. Modeling of Airplane Performance from Flight-Test Results and Validation with an F-104G Airplane. NASA-TN-D-7137. NASA. https://ntrs.nasa.gov/citations/19730007281
• Martellucci, A., B. L. Maguire, and R. S. Neff. 1972. Analysis of Flight Test Transition and Turbulent Heating Data. Part 1: Boundary Layer Transition Results. NASA-CR-129045. NASA. https://ntrs.nasa.gov/citations/19730003560
• Martin, Dennis J. 1958. Summary of Flutter Experiences as a Guide to the Preliminary Design of Lifting Surfaces on Missiles. NACA-TN-4197. NASA. https://ntrs.nasa.gov/citations/19930085030
• Martin, W. G. 1978. High Altitude Altimeter Flight Test. Defense Technical Information Center. https://doi.org/10.21236/ada066904
• Martin, J. L. 1979. The Quiet Short-Haul Research Aircraft (QSRA). NASA Ames Research Center. https://ntrs.nasa.gov/citations/19800043214
• Martin, J. L. 1980. “The Quiet Short-Haul Research Aircraft (QSRA).” In Society of Experimental Test Pilots Soc. of Exptl. Test Pilots Tech. Rev., Vol. 14, No. 4. https://ntrs.nasa.gov/citations/19800022808
• Martin, James. 2006. “The Triplet Reusable Launch Vehicle Concept.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4960
• Martin, Ainsley, Gavin Stay, Abigail Lingel, and Douglas Fontes. 2024. “Image Analysis of the Dynamics of Reusable Launch Vehicle.” In Volume 7: Engineering Education. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2024-142760
• Martin Co Denver Co. 1966. SSLV-5 No. 9 Post Firing Flight Test Report (Final Evaluation Report) and Mol-Eft Final Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ad0378020
• Martin, Fred, Jr. 1999. “Parafoil Aerodynamic Characteristics Derived from Flight Measured Suspension System Loads.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1734
• Martin, F., Jr., W. Sickles, and S. Stanley. 1993. “Transonic Wind Tunnel Wall Interference Analysis for the Space Shuttle Launch Vehicle.” In 31st Aerospace Sciences Meeting. AIAA 1993-420. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-420
• Martinez, Martel. 2012. “Dryden Flight Research Center: Presentation to Portland State Aerospace Society.” In Portland State Aerospace Society Meeting. https://ntrs.nasa.gov/citations/20120013432
• Martinez, Bastien, Myriam Bastide, and Pierre Wey. 2014. “Free Flight Measurement Technique in Shock Tunnel.” In 30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2014-2523. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2523
• Martinez, Debbie, Paul Davidson, P. Kenney, and B. Hutchinson. 2004. “NASA Langley Research Center’s Simulation-to-Flight Concept Accomplished through the Integration Laboratories of the Transport Research Facility.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2004-4934. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4934
• Martínez Morán, G. 2018. “11.1: Intelligent Networked Flight Test Instrumentation for a New Fighter Prototype.” In Proceeding - ettc2018. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2018/11.1
• Martinez Schramm, Jan, Klaus Hannemann, Sebastian Karl, Sebastien Defoort, Paul Viguier, and Johan Steelant. 2015. “Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3627
• Martos, Borja, Paul Kiszely, and John Foster. 2011. “Flight Test Results of a GPS-Based Pitot-Static Calibration Method Using Output-Error Optimization for a Light Twin-Engine Airplane.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6669. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6669
• Marwaha, Monika, John Valasek, and Puneet Singla. 2008. “GLOMAP Approach for Nonlinear System Identification of Aircraft Dynamics Using Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6895. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6895
• Marx, A. J. 1959. “A Survey of Flight Flutter Testing Techniques.” In Stability and Control. Elsevier. https://doi.org/10.1016/b978-1-4831-9730-2.50023-5
• Marx, H. 1983. “Comparative Cost of Military Aircraft: Fiction versus Fact.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2565. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2565
• Marx, William, Dimitri Mavris, and Daniel Schrage. 1995. “A Hierarchical Aircraft Life Cycle Cost Analysis Model.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3861
• Marzocca, Piergiovanni, Gianfranco Chiocchia, and Liviu Librescu. 2000. “Unsteady Aerodynamics in Various Flight Speed Regimes for Flutter/dynamic Response Analyses.” In 18th Applied Aerodynamics Conference. AIAA 2000-4229. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4229
• Marzouk, Osama. 2025. “Algorithm for Numerically Solving Airplane Inverse Simulation Problems in Flight Dynamics.” Preprint, . https://doi.org/10.20944/preprints202506.1467.v1
• Mas Colomer, Joan. n.d. “Aeroelastic Similarity of a Flight Demonstrator via Multidisciplinary Optimization.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/641c36e3z1c8ez400fzb0e4z97b4192e068b
• Masek, R. V., D. Hender, and J. A. Forney. 1973. “Evaluation of Aerodynamic Heating Uncertainties for Space Shuttle.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730051552
• Maslov, Anatoly A. 2001. Experimental Study of Stability and Transition of Hypersonic Boundary Layer around Blunted Cone. Defense Technical Information Center. https://doi.org/10.21236/ada408241
• Maslov, A. A., and S. G. Mironov. 2000. “Experimental Investigations of the Hypersonic Boundary Layer Stability.” In Laminar-Turbulent Transition. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-03997-7_63
• Mason, W. 1982. “Wing-Canard Aerodynamics at Transonic Speeds: Fundamental Considerations on Minimum Drag Spanloads.” In 20th Aerospace Sciences Meeting. AIAA 1982-97. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-97
• Mason, Justin R. 2013. “F-35B Aircraft Performance Model Validation of Short Take-off Flight Test Data.” In 2013 International Powered Lift Conference. AIAA 2013-4245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4245
• Mason, M. L., and F. J. Capone. 1983. Aeropropulsive Characteristics of Twin Single-Expansion-Ramp Vectoring Nozzles Installed with Forward-Swept Wings and Canards. NASA-TP-2133. NASA. https://ntrs.nasa.gov/citations/19830013890
• Mason, Michelle L., Shann J. Rufer, Brian R. Hollis, et al. 2024. “NASA Langley Hypersonic Experimental Aerothermodynamic Capabilities and Recent Contributions.” In AIAA Aviation Forum. https://ntrs.nasa.gov/citations/20240008907
• Masson, Christian, Charles Veilleux, Eric Laurendeau, and Ion Paraschivoiu. 1999a. “Accurate Induced Drag Predictions over Wing Mounted on a Fuselage Operating in the Transonic Regime.” In 17th Applied Aerodynamics Conference. AIAA 1999-3187. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3187
• Masson, Christian, Charles Veilleux, and Ion Paraschivoiu. 1999b. “Drag Predictions Using Euler Solutions of 2D and 3D Transonic Flows.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-527
• Mastropietro, A. J., Jason Kempenaar, Matthew Redmond, Michael Pauken, and Walt Ancarrow. 2015. “First Test Flight Thermal Performance of the Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Vehicle.” In International Conference on Environmental Systems 2015. https://ntrs.nasa.gov/citations/20170007025
• “Materials for Supersonic Civil Transport Aircraft.” 2015. In Aerospace Materials. CRC Press. https://doi.org/10.1201/9781420034721-5
• Mathavaraj, S., Omkar Halbe, and Radhakant Padhi. 2010. “Robust Control of a Reusable Launch Vehicle in Reentry Phase Using Model Following Neuro-Adaptive Design.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8312
• Mathavaraj, S., and Radhakant Padhi. 2020. “Optimally Allocated Nonlinear Robust Control of a Reusable Launch Vehicle during Re-Entry.” Unmanned Systems 08 (01): 33–48. https://doi.org/10.1142/s230138502050003x
• Matheny, Cloyce E. 1950. Maximum Pitching Angular Accelerations of Airplanes Measured in Flight. NACA-TN-2103. NASA. https://ntrs.nasa.gov/citations/19930082808
• Matheny, N., and G. Panageas. 1981. “HiMAT Aerodynamic Design and Flight Test Experience.” In 1st Flight Test Conference. AIAA 1981-2433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2433
• Mathews, Charles W., Donald B. Talmage, and James B. Whitten. 1948. Longitudinal Stability and Control Characteristics of a B-29 Airplane with a Booster Incorporated in the Elevator Control System to Provide Various Stick-Force and Control-Rate Characteristics. NACA-RM-L50D11. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019337
• Mathews, Charles W., and Jim Rogers Thompson. 1947. Drag Measurements at Transonic Speeds of NACA 65-009 Airfoils Mounted on a Freely Falling Body to Determine the Effects of Sweepback and Aspect Ratio. NACA-RM-L6K08c. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20030063971
• Matranga, Gene J. 1961a. Analysis of X-15 Landing Approach and Flare Characteristics Determined from the First 30 Flights. NASA-TN-D-1057. NASA. https://ntrs.nasa.gov/citations/19980227282
• Matranga, Gene J. 1961b. Launch Characteristics of the X-15 Research Airplane as Determined in Flight. NASA-TN-D-723. NASA. https://ntrs.nasa.gov/citations/20040047146
• Matranga, Gene J., and James R. Peele. 1957. Flight-Determined Static Lateral Stability and Control Characteristics of a Swept-Wing Fighter Airplane to a Mach Number of 1.39. NACA-RM-H57A16. NASA. https://ntrs.nasa.gov/citations/19930089538
• Matranga, G. J., G. H. Robinson, and R. M. White. 1962. Resume of Handling Qualities of the X-15 Airplane. NASA-TM-X-715. NASA. https://ntrs.nasa.gov/citations/19650014322
• Matsumoto, Shuichi, Yoshinori Kondoh, Shinji Nagai, Rie Tagai, Takene Imada, and Eiichiro Nakano. 2016. “Aerodynamic Oscillation and Attitude Control Analysis for Reentry Capsule Using OREX Flight Data and Wind Tunnel Data.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-1131. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1131
• Matsuno, Kristen V., Robert E. Childs, Thomas H. Pulliam, Paul M. Stremel, Patrick J. Moran, and Joseph A. Garcia. n.d. “Comparison of OVERFLOW Computational and Experimental Results of the CobraMRV Mars Entry Vehicle Concept during Supersonic Retropropulsion.” In AIAA AVIATION Forum and Exposition. https://ntrs.nasa.gov/citations/20240007157
• Matsuno, Kristen V., Robert E. Childs, Thomas H. Pulliam, Paul M. Stremel, Patrick J. Moran, and Joseph A. Garcia. 2024. “Comparison of OVERFLOW Computational and Experimental Results of the CobraMRV Mars Entry Vehicle Concept during Supersonic Retropropulsion.” In AIAA Aviation 2024. https://ntrs.nasa.gov/citations/20230016504
• Matsuyama, Shingo. 2024. “DNS Study of Enthalpy Effects on Hypersonic Boundary-Layer Transition in High-Enthalpy Shock Tunnel HIEST.” In AIAA SCITECH 2024 Forum. AIAA 2024-1568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1568
• Matt, Justin J. n.d. “Comparison of Multisine Peak Factor Minimization Algorithms for Aircraft System Identification(Presentation).” In LaRC Flight Dynamics Branch Internal Presentation. https://ntrs.nasa.gov/citations/20240013263
• Matt, Justin J. 2024. Comparison of Multisine Peak Factor Minimization Algorithms for Aircraft System Identification. Langley Research Center. https://ntrs.nasa.gov/citations/20240009677
• Matt, Justin J., and George V. Altamirano. 2025. “System Identification of an Octocopter in Hover Using Full-Harmonic Orthogonal Multisine Inputs.” In AVIATION 2025 Conference Proceedings. https://ntrs.nasa.gov/citations/20250006234
• Matt, Justin J., and George V. Altamirano. 2026. System Identification of an Octocopter in Hover Using Full-Harmonic Orthogonal Multisine Inputs. Langley Research Center. https://ntrs.nasa.gov/citations/20250010439
• Mattaboni, Mattia, Giuseppe Quaranta, and Paolo Mantegazza. 2007. “Active Flutter Suppression for a Three Surface Transport Aircraft by Recurrent Neural Networks.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-2136. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2136
• Matthews, Alexander, and Terry Jones. 2005. “Design and Test of a Modular Waverider Hypersonic Intake.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3379
• Matz, R., and G. Smith. 1978. “Ejector-Powered Engine Simulators for Small-Scale Wind Tunnel Modelsof High Performance Aircraft.” In 10th Aerodynamic Testing Conference. AIAA 1978-826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-826
• Maughmer, Mark, Christopher J. Axten, and Leonard Metkowski. 2021. “Low-Turbulence Wind Tunnel Results for a Low-Reynolds Number Airfoil.” In AIAA Aviation 2021 Forum. AIAA 2021-2514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2514
• Maunder, D. 1979. “AFFTC Parameter Identification Experiencefor Aircraft Flight Characteristics.” In Aircraft Systems and Technology Meeting. AIAA 1979-1803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1803
• Maus, J., B. Griffith, D. Tolbert, and J. Best. 1983. “Understanding Space Shuttle Flight Data by Use of Wind Tunnel and CFD Results.” In 2nd Flight Testing Conference. AIAA 1983-2745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2745
• Mavriplis, D. J., and David W. Levy. 2001. “Transonic Drag Prediction Using an Unstructured Multigrid Solver.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20020019227
• Mavriplis, D., and D. Levy. 2002. “Transonic Drag Prediction Using an Unstructured Multigrid Solver.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-838
• Mavriplis, Dimitri J., Zhi Yang, and Evan M. Anderson. 2020. “Adjoint Based Optimization of a Slotted Natural Laminar Flow Wing for Ultra Efficient Flight.” In AIAA Scitech 2020 Forum. AIAA 2020-1292. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1292
• Maxwell, Jesse R. 2016. “Hypersonic Waverider Stream Surface Actuation for Variable Design Point Operation.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-4706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4706
• Maydew, R. C. 1964. Comparison of Wind Tunnel and Flight Data for a Hypersonic Instrumentation Rocket. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4000106
• Mayer, Gerhard, and Timothy Chalfant. 2023. “Trends in Aeronautical Flight Test Telemetry.” Journal of Aerospace Sciences and Technologies: 252–58. https://doi.org/10.61653/joast.v61i1.2009.648
• Mayfield, J., and R. Smith. 1978. “Software Engineering a Must for Success in Computerized Flight Test.” In Aircraft Systems and Technology Conference. AIAA 1978-1463. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1463
• Maykapar, G. I. 1968. Aerodynamic Heating of the Lifting Bodies. NASA-CR-97576. NASA. https://ntrs.nasa.gov/citations/19690001128
• Mayne, A., Jr. 1979. “Boundary-Layer Calculations for Spinning Sharp and Blunt Cones in Supersonic and Hypersonic Flow.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1634. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1634
• Mayya, Adithya K., Ashish Srivastava, Madhusudan A. Padmanabhan, and Kartik Venkatraman. 2023. “Roll Performance of a Flexible Aircraft with Active Aeroelastic Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-1565. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1565
• Mazurov, A. P., and S. A. Takovitskii. 2022. “Nose Part of the Body of Revolution Having Minimum Aerodynamic Drag in the Range of Large Subsonic Velocities.” Fluid Dynamics 57 (1): 86–95. https://doi.org/10.1134/s0015462822010074
• Mbagwu, Chukwuka, and James F. Driscoll. 2018. “An Examination of Vehicle Design Tradeoffs and Trajectory Optimization for Trimmed Scramjet-Powered Hypersonic Vehicles on Ascent.” In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2018-0417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0417
• McCandless, R., and C. Cruz. 1985. “Hypersonic Characteristics of an Advanced Aerospace Plane.” In 23rd Aerospace Sciences Meeting. AIAA 1985-346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-346
• McCarthy, Dennis, Darryl Toni, Matt Spies, Dan Solari, and Jasmina Maack. 2018. “Joint Multi-Role Technology Demonstrator Fuselage Proof Test.” In Proceedings of the Vertical Flight Society 74th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0074-2018-12880
• McCauley, R., J. Davidson, and Guillermo Gonzalez. 2015. “Orion Launch Abort System Performance on Exploration Flight Test 1.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20150016489
• McClinton, C., S. Ferleman, K. Rock, and P. Ferlemann. 2002. “The Role of Formal Experiment Design in Hypersonic Flight System Technology Development.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-543. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-543
• McClinton, C. R., S. D. Holland, K. E. Rock, et al. 1998a. Hyper-X Wind Tunnel Program. NASA/TM-1998-207317. NASA. https://ntrs.nasa.gov/citations/19980047114
• McClinton, C. R., V. L. Rausch, J. Sitz, and P. Reukauf. 2001. Hyper-X Program Status. AIAA Paper 2001-0828. Langley Research Center. https://ntrs.nasa.gov/citations/20010021138
• McClinton, C., R. Voland, S. Holland, W. Engelund, J. White, and J. Pahle. 1998b. “Wind Tunnel Testing, Flight Scaling and Flight Validation with Hyper-X.” In 20th AIAA Advanced Measurement and Ground Testing Technology Conference. AIAA 1998-2866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2866
• McClure, Wallace. 1998. “Decision Criteria for a Reusable Launch Vehicle Investment Decision.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5139
• McConkey, Ryley, Nikhila Kalia, Eugene Yee, and Fue-Sang Lien. 2025. “Realisability-Informed Machine Learning for Turbulence Anisotropy Mappings.” Journal of Fluid Mechanics 1019: A49. https://doi.org/10.1017/jfm.2025.10618
• McConnaughey, H., R. Thompson, and J. Burton. 1995. “Propulsion Testing at NASA/Marshall Space Flight Center for Next-Generation Reusable Launch Vehicle Propulsion Technology Development.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-3125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3125
• McCracken, R. C. 1979. Quiet Short-Haul Research Aircraft Familiarization Document. NASA-TM-81149. NASA. https://ntrs.nasa.gov/citations/19800005852
• McCracken, Brendan, and Timothy Jorris. 2011. “Aircraft System Identification Using Pseudospectral Parameter Optimization with Adaptive Nodes.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6444
• McCutcheon, Richard. 1972. “S-67 Flight Test Program.” In Proceedings of the Vertical Flight Society Forum 28 - Washington, D.C. 1972. The Vertical Flight Society. https://doi.org/10.4050/vfs-f28-030
• McDaniel, James C. 2005. “Dual-Mode Scramjet Operation at a Mach 5 Flight Enthalpy in a Clean Air Test Facility.” In AIP Conference Proceedings, vol. 762. AIP. https://doi.org/10.1063/1.1941709
• McDearmon, Russell W. 1956. Wind-Tunnel Investigation of the Damping in Roll of the Douglas D-558-II Research Airplane and Its Components at Supersonic Speeds. NACA-RM-L56F07. NASA. https://ntrs.nasa.gov/citations/19930089379
• McDonald, John F. 1966. “Airports and the Supersonic Transport.” Journal of the Aero-Space Transport Division 92 (1): 107–30. https://doi.org/10.1061/jatdaz.0000062
• McDonald, H., S. J. Shamroth, and W. R. Briley. 1982. “Transonic Flows with Viscous Effects.” In Transonic, Shock, and Multidimensional Flows. Elsevier. https://doi.org/10.1016/b978-0-12-493280-7.50014-0
• McFadden, Evan J., and Jeffrey P. Bons. n.d. “Fluidic Fence Flow Control on a 30° Swept Wing in Compressible Freestreams.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20240016025
• McFarland, John, and David Riha. 2009. “Uncertainty Quantification Methods for Helicopter Fatigue Reliability Analysis.” In Proceedings of the Vertical Flight Society 65th Annual Forum, Grapevine, Texas, May 27-29, 2009. The Vertical Flight Society. https://doi.org/10.4050/vfs-f65-000281
• McGary, J., and Chien P. Li. 1989. “Aerodynamic Stability and Heating Analyses for the Aeroassist Flight Experiment Vehicle.” In NASA, Ames Research Center, NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12. https://ntrs.nasa.gov/citations/19910001586
• McGhee, Robert J., and Gene J. Bingham. 1972. Low-Speed Aerodynamic Characteristics of a 17-Percent-Thick Supercritical Airfoil Section, Including a Comparison between Wind-Tunnel and Flight Data. NASA-TM-X-2571. NASA. https://ntrs.nasa.gov/citations/19830002764
• McGhee, Robert, Gregory Jones, and Remi Jouty. 1988. “Performance Characteristics from Wind-Tunnel Tests of a Low-Reynolds-Number Airfoil.” In 26th Aerospace Sciences Meeting. AIAA 1988-607. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-607
• McGinley, Catherine B., Scott A. Berry, Gerald R. Kinder, maria Barnell, Kuo C. Wang, and Benjamin S. Kirk. 2006. “Review of Orbiter Flight Boundary Layer Transition Data.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20060020708
• McGowan, William A., and T. V. Cooney. 1957. An Analysis of Vertical-Tail Loads Measured in Flight on a Swept-Wing Bomber Airplane. NACA-RM-L57B19. NASA. https://ntrs.nasa.gov/citations/19930089618
• McKenzie, J. 1973. “B-52 Control Configured Vehicles Ride Control Analysis and Flight Test.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-782. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-782
• McKillip, Robert, Jr. 1988. “Experimental Studies in System Identification of Helicopter Rotor Dynamics.” Vertica 12 (4 19). https://ntrs.nasa.gov/citations/19890051183
• McKinney, L. W., and D. D. Baals. 1982. Wind-Tunnel/Flight Correlation, 1981. NASA-CP-2225. NASA. https://ntrs.nasa.gov/citations/19820017320
• McKinney, M. O., and W. A. Newsom. 1962. Experimental Research on 4-Duct Tandem VTOL Aircraft Configurations. No Number:. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19620001441
• McKown, Q., C. D. Kazemba, E. C. Stern, and J. M. Brock. n.d. Comparison of Pre- and Post-Flight Estimations of Pitch Damping Coefficients for Unguided Entry Vehicles. Analytical Mechanics Associates (United States). https://ntrs.nasa.gov/citations/20230011053
• McLaud, E. C., and K. C. Hansen. 1977. “Structural Design Flight Maneuver Loads Using PDP-10 Flight Dynamics Model.” In Proceedings of the Helicopter Structures Technology Specialists Meeting - Moffett Field, California 1977. The Vertical Flight Society. https://doi.org/10.4050/sm_struct_1977-4347
• McLaughlin, Thomas, Michael Robinson, and Marvin Luttges. 1993. “Aerodynamic Foundations for Use of Unsteady Aerodynamic Effects in Flight Control.” In 31st Aerospace Sciences Meeting. AIAA 1993-188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-188
• McMaster, J., and F. Schenk. 1973. “The Development of the F-12 Series Aircraft Manual and Automatic Flight Control System.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-822
• McMurtry, Kate Maureen, and Sasha Congiu Ellis. 2024. Benefiting Humanity through Flight Research of Advanced Technologies. Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20240001984
• McMurtry, T., A. Sim, and W. Andrews. 1981. “AD-1 Oblique Wing Aircraft Program.” In 1st Flight Test Conference. AIAA 1981-2354. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2354
• McNally, B., and Ralph Bach Jr. 1988. “Flight Testing a V/STOL Aircraft to Identify a Full-Envelope Aerodynamic Model.” In 4th Flight Test Conference. AIAA 1988-2134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2134
• McNeill, W. E. 1968. Calculated and Flight Measured Handling- Qualities Factors of Three Subsonic Jet Transports. NASA-TN-D-4832. NASA. https://ntrs.nasa.gov/citations/19690001164
• McNichols, Ezra. n.d. “Thermal Management for Electrified Aircraft.” In 2022 Ohio Federal Research Network. https://ntrs.nasa.gov/citations/20220005430
• McPherson, R. 1977. “YC-14 Flight Test Results.” In Aircraft Systems and Technology Meeting. AIAA 1977-1259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1259
• McQuellin, Liam P., and David R. Buttsworth. 2024. “Free-Flight of a Propelled Axisymmetric Vehicle in a Hypersonic Ground-Test Facility.” In AIAA SCITECH 2024 Forum. AIAA 2024-2889. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2889
• McQuellin, Liam P., Andrew Neely, and Gaetano Currao. 2020. “Considerations for a Hypersonic Flight Test Investigating Fluid-Thermal-Structural Interactions.” In 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2020-2419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2419
• McTavish, Sean. n.d. “Advanced Aeroelastic Simulations for Practical Fixed-Wing and Rotary-Wing Applications.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2008-08205
• McTigue, John G. 1970. “Background and Current Status of the Lifting Body Program.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000628
• McTigue, John G., and Garrison P. Layton. 1969. “Lifting Body Flight Tests and Analysis.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/690662
• McVey, Francis D., John V. Rejeske, and Edward J. Phillips. 1969. Experimental Evaluation of Inlet Drag Characteristics in the Transonic Mach Number Regime. Defense Technical Information Center. https://doi.org/10.21236/ad0861763
• Mead, Frank. 1998. The Lightcraft Technology Demonstrator (LTD) Program. Defense Technical Information Center. https://doi.org/10.21236/ada405839
• Mead, Franklin, and C. Larson. 2001. “Laser-Powered, Vertical Flight Experiments at the High Energy Laser System Test Facility.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3661. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3661
• Mease, K., and N. Vinh. 1988. “Optimal Plane Change during Constant Altitude Hypersonic Flight.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4341. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4341
• Meckelnborg, S., and M. Hölling. 2026. “A High Reynolds Number Wind Tunnel Set-up for Research on Static and Oscillating Cylinder.” Journal of Physics: Conference Series 3224 (4): 042023. https://doi.org/10.1088/1742-6596/3224/4/042023
• Medina, Jose A., Harinkumar Patel, and Bernd Chudoba. 2021. “Inlet Sizing of Hypersonic Vehicles for Conceptual Design.” In ASCEND 2021. AIAA 2021-4096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-4096
• Meersman, John A., Christoph Hader, and Hermann F. Fasel. 2022. “Numerical Investigation of Hypersonic Boundary-Layer Transition for an Ogive Cone.” In AIAA SCITECH 2022 Forum. AIAA 2022-0946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0946
• Meheut, Michael, Aurelien Arntz, and Gerald Carrier. 2012. “Aerodynamic Shape Optimizations of a Blended Wing Body Configuration for Several Wing Planforms.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3122
• Mehra, R. K., and N. K. Eupta. 1975. “Status of Input Design for Aircraft Parameter Identification.” In AGARD Methods for Aircraft State and Parameter Identification. https://ntrs.nasa.gov/citations/19750021936
• Mehra, R. K., and J. S. Tyler. 1973. Case Studies in Aircraft Parameter Identification. Harvard University. https://ntrs.nasa.gov/citations/19740042090
• Mehrotra, S., and J. Robinson. 1982. “Structural Modeling of High Reynolds Number Wind Tunnel Models.” In 12th Aerodynamic Testing Conference. AIAA 1982-602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-602
• Mehta, Unmeel. 1989. “Computational Requirements for Hypersonic Flight Performance Estimates.” In 24th Thermophysics Conference. AIAA 1989-1670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1670
• Mehta, R., and R. Mehta. 1997. “Flowfield Study over a Bulbous Payload Shroud in Transonic and Low Supersonic Mach Number.” In 15th Applied Aerodynamics Conference. AIAA 1997-2256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2256
• Mehta, Manish, Christopher I. Morris, Brandon L. Mobley, and Terry L. Prickett. n.d. “Space Launch System Core Stage Green Run Base Heating: Anomaly, Mitigation and Flight Redesign.” In 2023 AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20230000630
• Meineke, Wolfgang, and David Urry. 1992. “Flight Testing of the Forward Looking Infra-Red (FLIR) Sensor on the Electronic Combat and Reconnaissance (ECR) Tornado.” In 6th AIAA Biennial Flight Test Conference. https://ntrs.nasa.gov/citations/19930027272
• Meirovitch, Leonard. 1995. Performance Improvement of Composite Wings through Aeroelastic Tailoring and Modern Control. Defense Technical Information Center. https://doi.org/10.21236/ada293689
• Melander, Luke J., and Graham V. Candler. 2024. “Effect of Atmospheric Turbulence on Hypersonic Boundary Layer Transition in the HIFiRE-1 Flight Experiment.” In AIAA SCITECH 2024 Forum. AIAA 2024-0701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0701
• Melgaard, P. 1986. “STOL/Maneuver Technology Demonstrator Test Program.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9762
• Melo, César Abrahão Pereira. n.d. “Aerodynamic Noise in Distributed Electric Propulsion Rotor-Wing Systems Investigated Using Experimental and Numerical Methods.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/t.18.2026.tde-07052026-101521
• Melton, John R., and Gary C. Hall. 1968. Engineering Flight Test of the AH-1G Helicopter (Hueycobra). Phase b. Part 1. Defense Technical Information Center. https://doi.org/10.21236/ad0830136
• Melvill Jones, B. 1938. “The Boundary Layer in Flight: Some Recent Flight Experiments on the Transition from Laminar to Turbulent Flow.” Aircraft Engineering and Aerospace Technology 10 (5): 135–41. https://doi.org/10.1108/eb030310
• Melville, Michael. 2021. “Modeling of Gust Energy Extractions through Aeroelastic Tailoring.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14646720
• Mendenhall, M., M. Hegedus, G. Budd, et al. 1997. “Aerodynamic Analysis of the Deep-Stall Flight Characteristics of the Pegasus XL Booster.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3583
• Mendenhall, M., and S. Perkins Jr. 1996. “Predicted High-Alpha Aerodynamic Characteristics on Maneuvering Aircraft.” In 14th Applied Aerodynamics Conference. AIAA 1996-2433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2433
• Meng, Xufei, Peng Bai, and Chuanzhen Liu. 2024b. “Planform-Customized Waverider Design Using Flows with Variable Mach Numbers.” Preprint, . https://doi.org/10.2139/ssrn.5059953
• Meng, Yu, Wenming Sun, Hongbin Gu, and Fang Chen. 2024a. “Experimental Investigation of Mode Transition Process in a Cavity-Based Scramjet.” Physics of Fluids 36 (4): 044101. https://doi.org/10.1063/5.0193282
• Menges, Pamela. 1995. “Expert System Data Bases in Flight Test Engineering.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3878
• Mennebeuf, L., B. Mouchet, D. Cumer, K. Veerabadran, and L. Malard. 2024. “A5.1: In Flight Optical Fiber Measurement on Flight Test Aircraft.” In ETTC 2024. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2024/a5.1
• Menon, P. K. A., H. A. Saberi, R. A. Walker, and E. L. Duke. 1985. Flight Test Trajectory Controller Synthesis with Constrained Eigenstructure Assignment. Integrated Systems, Inc. https://ntrs.nasa.gov/citations/19860050666
• Menon, P. K. A., and R. A. Walker. 1988. Aircraft Flight Test Trajectory Control. NASA-CR-179428. NASA. https://ntrs.nasa.gov/citations/19880007324
• Menon, P., R. Walker, and E. Duke. 1986. “Flight Test Maneuver Modeling and Control.” In 24th Aerospace Sciences Meeting. AIAA 1986-426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-426
• Menzies, Margaret, and Osama Kandil. 1996. “Natural Rolling Responses of a Delta Wing in Transonic and Subsonic Flows.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3391
• Merceruio, Zachary J. n.d. “Modeling and Flight Testing of Differential Thrust and Thrust Vectoring on a Small UAV.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.291
• Merkhofer, Miley Wesson. 1975. The Value of Information Given Decision Flexibility. Defense Technical Information Center. https://doi.org/10.21236/ada016836
• Merlet, Charles F. 1954. Pressure Recovery and Drag Characteristics of a Forward Located Circular Scoop Inlet as Determined from Flight Tests for Mach Numbers from 0.8 to 1.6. NACA-RM-L54B23. NASA. https://ntrs.nasa.gov/citations/19930090333
• Merlin, Peter William. 2014. “Human Factors Lessons Learned from Flight Testing Wingless Lifting Body Vehicles.” In Aerospace Medical Association. https://ntrs.nasa.gov/citations/20140008618
• Merrett, Craig G., and Harry H. Hilton. 2012. “Highly Flexible Flight Vehicle Aeroelastic and Aero-Viscoelastic Flutter Issues.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.4765530
• Merrett, Craig, Harry Hilton, Sahithi Kalidindi, and Elliot Schwartz. 2011. “Suppression of Bending-Torsion Flutter in Accelerated Flight with Aero-Servo-Viscoelastic Controls.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6208
• Mertens, J., K. Klevenhusen, and H. Jakob. 1986. “Accurate Transonic Wave Drag Prediction Using Simple Physical Models.” In 24th Aerospace Sciences Meeting. AIAA 1986-512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-512
• “Methods for Drag Determination in Flight.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0161.0168
• “Methods for Predicting off-Stagnation-Point Flowfields for Planetary Entry Probes.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0026.0051
• “Methods for Predicting Radiation-Coupled Flowfields about Planetary Entry Probes.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0120.0136
• “Methods for Reducing Data Uncertainty in Flight Test Data.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0019.0028
• Metodiev, Konstantin. 2024. “System Identification of Aircraft Longitudinal Motion by Means of Flight Simulator Data.” Aerospace Research in Bulgaria 36: 115–23. https://doi.org/10.3897/arb.v36.e10
• Metzger, Michael A. 1997. Graphite Heating Element Operating Temperature Measurements in the NSWC Hypervelocity Wind Tunnel 9. Defense Technical Information Center. https://doi.org/10.21236/ada329681
• Meuwly, Markus. 2014. Investigations of Reactive Processes at Temperatures Relevant to the Hypersonic Flight Regime. Defense Technical Information Center. https://doi.org/10.21236/ada611797
• Meyer, Rudolf X. 1938. Magnetohydrodynamics and Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0608024
• Meyer, R. A. 1958. Wind Tunnel Investigation of Conventional Types of Parachute Canopies in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0208856
• Meyer, Robert R., Jr. 1992. “Overview of the NASA Dryden Flight Research Facility Aeronautical Flight Projects Testing.” In AGARD, Flight Testing. https://ntrs.nasa.gov/citations/19930010727
• Meyer, Robert R., Jr. 2007. Dryden Flight Research Center Overview. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070036800
• Meyer, R. R., Jr., and V. M. Deangelis. 1978. “Flight-Measured Aerodynamic Loads on a 0.92 Aspect Ratio Lifting Surface.” In YF-12 Experiments Symp., Vol. 1. https://ntrs.nasa.gov/citations/19780024115
• Meyers, D. N., L. V. Tompkins, and J. H. Goldberg. 1968. 16H-1A Flight Test Research Program. Defense Technical Information Center. https://doi.org/10.21236/ad0675443
• Meyerson, Robert E. 1998. “Development Status of the Kistler Aerospace K-1 Reusable Launch Vehicle.” In Space 98. American Society of Civil Engineers. https://doi.org/10.1061/40339(206)21
• Meyn, Larry A., Peter T. Zell, John L. Hagan, and David Schoch. 1993. “Full-Scale Wind-Tunnel Tests of High-Lift System Modifications on a Carrier Based Fighter Aircraft.” In AIAA. https://ntrs.nasa.gov/citations/19930046932
• Miao, W. L., T. Edwards, and D. E. Brandt. 1976. “Investigation of Aeroelastic Stability Phenomena of a Helicopter by in-Flight Shake Test.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014096
• Michek, Nathaniel, Piyush Mehta, and Wade Huebsch. 2024. “Flight Dynamic Uncertainty Quantification Modeling Using Physics-Informed Neural Networks.” In AIAA SCITECH 2024 Forum. AIAA 2024-0575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0575
• Michel, Ulf. 1987. “How to Satisfy the Takeoff Noise Requirements for a Supersonic Transport.” In 11th Aeroacoustics Conference. AIAA 1987-2726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2726
• Mickola, Richard H. 1961. Performance Summary of the Supersonic Diffuser and Its Application to Altitude Testing of Captive Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ad0256347
• Micol, John. 1990. “Experimental and Predicted Aerodynamic Characteristics of a proposedAssured Crew Return Vehicle (ACRV) Lifting-Body Configuration at Mach 6 and 10.” In 16th Aerodynamic Ground Testing Conference. AIAA 1990-1403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1403
• Miele, Angelo. 1959. “General Variational Theory of the Flight Paths of Rocket-Powered Aircraft, Missiles and Satellite Carriers.” In IXth International Astronautical Congress/IX. Internationaler Astronautischer Kongress/IXe Congrès International D’astronautique. Springer Vienna. https://doi.org/10.1007/978-3-7091-4745-0_32
• Miele, A. 1968. “Optimum Transversal Contour of a Lifting Body at Hypersonic Speeds.” In INTERNATIONAL ASTRONAUTICAL FEDERATION. https://ntrs.nasa.gov/citations/19690039651
• Mihaila-Andres, Mihai, Ciprian Larco, Paul-Virgil Rosu, and Constantin Rotaru. 2017a. “Aeroelastic Tailoring of Composite Aircraft Wings.” In AIP Conference Proceedings, vol. 1863. Author(s). https://doi.org/10.1063/1.4992590
• Mihaloew, James R., and Colin K. Drummond. 1989. “STOVL Aircraft Simulation for Integrated Flight and Propulsion Control Research.” In Applied Dynamics International Users Society Annual Conference. https://ntrs.nasa.gov/citations/19900004073
• Mikhail, Ameer. 1989. “Lift Losses for Fin-Body Gaps in Transonic and Supersonic Speeds: Data Correlation and Modeling.” In 27th Aerospace Sciences Meeting. AIAA 1989-332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-332
• Mikula, D., Mark Holthaus, Todd Jensen, Douglas Kubo, and Marianne Redgate. 2000. “X-37 Flight Demonstrator System Safety Program and Challenges.” In Space 2000 Conference and Exposition. AIAA 2000-5073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5073
• Miles, Richard B., and Garry L. Brown. 2002. Radiatively Driven Hypersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada403037
• Miley, Stan, Michael Fisher, Bianca Anderson, and Robert Geenen. 1992. “Measurement of Attachment-Line Location in a Wind-Tunnel and in Supersonic Flight.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4089
• Miley, S. J., Leonard S. Miller, Ken Hall, and Houg-Jen Tsai. 1981. “Investigation of a Flight Test Method for the Measurement of Propeller Thrust.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/810603
• Milholen, William, and Lewis Owens. 2005. “On the Application of Contour Bumps for Transonic Drag Reduction (Invited).” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-462
• Milillo, J. R. 1972. Post-Stall Testing of Aircraft with a Wind Tunnel Captive System. Defense Technical Information Center. https://doi.org/10.21236/ad0751461
• Miller, E. 1983. “Performance of a Forward Swept Wing Fighter Utilizing Thrust Vectoring.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2482
• Miller, Glen E. 1991. “Application of Analog Fiber Optic Position Sensors to Flight Control Systems.” In SPIE Proceedings, vol. 1367, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.24770
• Miller, Charles G. 1993. “Aerothermodynamic Measurement Techniques Employed in NASA Langley Hypersonic Facilities.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_40
• Miller, Dean R. 2000. Supercooled Large Droplet Icing Flight Research Program. NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20050192376
• Miller, Chris. 2007a. “NASA Dryden Flight Research Center C-17 Research Overview.” In Air Force/Boeing - Test Program management Review. https://ntrs.nasa.gov/citations/20070021636
• Miller, Chris J. 2007b. NASA Dryden Overview. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070021479
• Miller, Christopher. 2014. “Full Scale Advanced Systems Testbed (FAST): Capabilities and Recent Flight Research.” In Aerospace Control and Guidance Systems Committee Meeting. https://ntrs.nasa.gov/citations/20140006737
• Miller, Chris. 2023. “NASA Armstrong Flight Research Center Dynamics and Controls (530).” In Aerospace Control and Guidance Systems Committee (ACGSC) Meeting #130. https://ntrs.nasa.gov/citations/20230003167
• Miller, Christopher J., and Dan Goodrick. 2017. “Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression, Flight-Test Performance.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170000458
• Miller, Lilia R., Ralph H. Jansen, and Ariel E. Dimston. 2023. “Structural Requirements for Design and Analysis of 25% Scale Subsonic Single Aft Engine (SUSAN) Research Aircraft.” In AIAA SciTech 2023. https://ntrs.nasa.gov/citations/20220016875
• Miller, Jay, and Dennis R. Jenkins. 2000. American X-Vehicles: An Inventory, X-1 to X-45. HHR-69. NASA Headquarters. https://ntrs.nasa.gov/citations/20010072175
• Miller, Eric J., Francisco Pena, Ashante Jordan, Larry Hudson, and William Lokos. 2019. “Evaluation of Wing Load Calibration and Sensing Methods Using Conventional Strain Gages and a Fiber Optic Sensing System Installed on a Straight Tapered Wing.” In AIAA Scitech 2019 Forum. AIAA 2019-0227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0227
• Miller, Kia, and Roger Truax. 2018. “X-57 and Whirl Flutter Discussion.” In Aerospace Flutter and Dynamics Council 2018. https://ntrs.nasa.gov/citations/20180002829
• Miller, G., J. Wykes, and M. Brosnan. 1982. “Rigid Body-Structural Mode Coupling on a Forward Swept Wing Aircraft.” In 23rd Structures, Structural Dynamics and Materials Conference. AIAA 1982-683. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-683
• Miller, R., Jr. 1973. “Flight Testing the F-12 Series Aircraft.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-823
• Milligan, M. W., and J. F. Bailey. 1963. Low-Density Hypervelocity Wind Tunnel Diffuser Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0295507
• Mills, Michael. 2015. “Hypersonic Test Capabilities in Tunnels B and C at AEDC’s Von Karman Facility.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1336
• Milne, Garrett, and Borja Martos. 2012. “Flight Test Results of Efficient Maneuver Development for a GPS-Based Pitot-Static Calibration Method Using Output-Error Optimization.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-2855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2855
• Minami, Yoshinori, and Taro Tsukamoto. 2006. “A Subscale Flight Experiment for the Approach and Landing of a Lifting Body Re-Entry Vehicle.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8120
• Minervino, Mauro, and Renato Tognaccini. 2023. “Wave Drag and Vorticity in Two-Dimensional Viscous and Inviscid Flows.” In AIAA SCITECH 2023 Forum. AIAA 2023-1032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1032
• Minier, Elizabeth A., and William T. Suit. 1988. Effect of Transition Aerodynamics on Aeroassist Flight Experiment Trajectories. NASA-TM-100546. NASA. https://ntrs.nasa.gov/citations/19880009236
• Minnema, Jeroen, Igor Mayer Soares, Luiz Carlos Sandoval, Leandro Rodrigues Cunha, and Gerrit Adriaan Folkertsma. 2019. “Using Bond Graphs for Modelling,identification and Control of a Fixed Wing UAV for Subscale Flight Testing.” In 25th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2019.cob2019-1726
• Minor, John, and Steven Shimer. 1986. “Facilities and Procedures for Test and Evaluation of Airborne Infrared Imaging Systems at Edwards Air Force Base.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9816. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9816
• Minwalla, Cyrus, Paul Thomas, Kristopher Ellis, Richard Hornsey, and Sion Jennings. 2016. “Range Performance Evaluation from the Flight Tests of a Passive Electro-Optical Aircraft Detection Sensor for Unmanned Aircraft Systems.” Journal of Unmanned Vehicle Systems 4 (2): 96–114. https://doi.org/10.1139/juvs-2014-0022
• Miotto, Piero, and Robert LePome. 2003. “Design of a Model Predictive Control Flight Control System for a Reusable Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5360
• Miró Miró, Fernando. n.d. “Numerical Investigation of Hypersonic Boundary-Layer Stability and Transition in the Presence of Ablation Phenomena.” PhD diss., Université libre de Bruxelles. https://doi.org/10.35294/phdt202004
• Mirowitz, L. I. 1975. “Transonic Flight Flutter Tests of a Control Surface Utilizing an Impedance Response Technique.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003026
• Mishra, Nirmith Kumar, A. Sai Kumar, M. Ganesh, and Mohd Abdul Rehman Alam. 2019. “Design of Minimum Length Supersonic Nozzle Using the Method of Characteristics.” International Journal of Innovative Technology and Exploring Engineering 9 (2): 1370–74. https://doi.org/10.35940/ijitee.b6183.129219
• Mishra, Rishabh, Ingrid Neunaber, Emmanuel Guilmineau, and Caroline Braud. 2022. “Wind Tunnel Study: Is Turbulent Intensity a Good Candidate to Help in Bypassing Low Reynolds Number Effects on 2d Blade Sections?” Journal of Physics: Conference Series 2265 (2): 022095. https://doi.org/10.1088/1742-6596/2265/2/022095
• Mitcham, Grady L., Willard S. Blanchard Jr., and Earl C. Hastings Jr. 1951. Flight-Determination of the Low-Lift Drag and Longitudinal Stability of a 1/10-Scale Rocket-Powered Model of the Douglas XF4D-1 Airplane at Mach Numbers from 0.7. NACA-RM-SL51L07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030030
• Mitchell, W. 1973. “Dynamic Simulation of CONFLOW: A Facility to Provide Hot-Gas Groundtesting of Air-Breathing Missiles under Simulated Flight Conditions.” In 9th Propulsion Conference. AIAA 1973-1281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1281
• Mitchell, Jesse L., and Robert F. Peck. 1949. An NACA Vane-Type Angle-of-Attack Indicator for Use at Subsonic and Supersonic Speeds. NACA-RM-L9F28a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050080746
• Mixson, J. S., R. L. Oneal, and F. W. Grosveld. 1984. Investigation of Fuselage Acoustic Treatment for a Twin-Engine Turboprop Aircraft in Flight and Laboratory Tests. NASA-TM-85722. NASA. https://ntrs.nasa.gov/citations/19840008879
• Miyakawa, J., N. Hirose, and N. Kawai. 1985. “Comparison of Transonic Airfoil Characteristics by Navier-Stokes Computation and by Wind Tunnel Test at High Reynolds Number.” In 3rd Applied Aerodynamics Conference. AIAA 1985-5025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-5025
• Miyakawa, Junichi, Takeshi Ohnuki, and Nobuhiko Kamiya. 1991. “Aero-Structural Integrated Design of Forward Swept Wing.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/912021
• Mizobata, Kazuhide, Ryojiro Minato, Katsuyoshi Fukiba, Kazuyuki Higashino, and Nobuhiro Tanatsugu. 2011. “Development of a Small-Scale Supersonic Flight Experiment Vehicle as a Flying Test Bed.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2289. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2289
• Mizukami, Masahi. 2004. Computer-Aided Systems Engineering for Flight Research Projects Using a Workgroup Database. NASA/TM-2004-212860. NASA. https://ntrs.nasa.gov/citations/20050019536
• Mo, Ran, Wenting Li, and Shanwei Su. 2022. “UDE-Based Adaptive Dynamic Surface Control for Attitude-Constrained Reusable Launch Vehicle.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2061133/v1
• Mobley, T. 1999. Reusable First Stage Flight Demonstrator. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990092478
• Mobley, Brandon L., and Samantha Summers. n.d.-a. “NASA Space Launch System Artemis I & II Post Flight Ascent Aerothermal Environments Overview.” In Thermal and Fluids Analysis Workshop (TFAWS). https://ntrs.nasa.gov/citations/20260007712
• Mobley, Brandon L., and Samantha Summers. n.d.-b. “Validation of Artemis I Aerothermal Design Models Using Developmental Flight Instrumentation.” In NASA Thermal & Fluids Analysis Worshop (TFAWS). https://ntrs.nasa.gov/citations/20240009390
• Moes, Timothy R., and Kenneth Iliff. 2002. Stability and Control Estimation Flight Test Results for the SR-71 Aircraft with Externally Mounted Experiments. NASA/TP-2002-210718. NASA. https://ntrs.nasa.gov/citations/20020057965
• Moes, Timothy R., Gregory K. Noffz, and Kenneth W. Iliff. 2000. Results from F-18B Stability and Control Parameter Estimation Flight Tests at High Dynamic Pressures. NASA/TP-2000-209033. NASA. https://ntrs.nasa.gov/citations/20010002099
• Moes, Timothy R., Mark S. Smith, and Eugene A. Morelli. 2003. Flight Investigation of Prescribed Simultaneous Independent Surface Excitations for Real-Time Parameter Identification. NASA/TM-2003-212029. NASA. https://ntrs.nasa.gov/citations/20030107571
• Moes, Tim, Mark Smith, and Gene Morelli. 2006. Excitations for Rapidly Estimating Flight-Control Parameters. DRC-03-06. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110012932
• Moffitt, R. C., J. B. Rorke, and J. F. Ward. 1972. “Wind Tunnel Simulation of Full Scale Vortices.” In Proceedings of the Vertical Flight Society Forum 28 - Washington, D.C. 1972. The Vertical Flight Society. https://doi.org/10.4050/vfs-f28-014
• Moga, Nicholas J. 1980. Optimal Bodies for Minimum Total Drag at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada091235
• Mogfhadam, Amir, and Ken Farsi. 1995. “Business Aircraft: Cost of Performance.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3955
• Mohamed, Majeed, and Vikalp Dongare. 2018. “Aircraft Neural Modeling and Parameter Estimation Using Neural Partial Differentiation.” Aircraft Engineering and Aerospace Technology 90 (5): 764–78. https://doi.org/10.1108/aeat-02-2016-0021
• Mohamed, Majeed, and Vikalp Dongare. 2021b. “Aircraft System Identification.” In SpringerBriefs in Applied Sciences and Technology. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0_1
• Mohamed, Majeed, and Vikalp Dongare. 2021c. “Identification of a Flexible Aircraft Derivatives.” In SpringerBriefs in Applied Sciences and Technology. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0_5
• Mohamed, Majeed, and Vikalp Dongare. 2021d. “Identification of Aircraft Lateral-Directional Derivatives.” In SpringerBriefs in Applied Sciences and Technology. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0_4
• Mohamed, Majeed, and Vikalp Dongare. 2021e. “Identification of Aircraft Longitudinal Derivatives.” In SpringerBriefs in Applied Sciences and Technology. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0_3
• Mohieldin, Taj, and Robert Carson. 2003. “Numerical Study of Two-Dimensional Dual-Mode Scramjet Combuster.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7036. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7036
• Mohieldin, T., S. Tiwari, and M. Olynciw. 2001. “Asymmetric Flow-Structures in Dual Mode Scramjet Combustor with Significant Upstream Interaction.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3296
• Mohr, R. L. 1975. Flight Instrumentation Specification for Parameter Identification: Program User’s Guide. NASA-CR-132676. NASA. https://ntrs.nasa.gov/citations/19750024040
• Mokry, M. 1974. “Integral Equation Method for Calculation of Subsonic Flow past Airfoils in a Ventilated Wind Tunnel: Comparison with NAE High Reynolds Number Measurements.” In 12th Aerospace Sciences Meeting. AIAA 1974-83. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-83
• Mokry, Miroslav. 2001. “Theory of Subsonic Wall Interference in a Cylindrical-Boundary Wind Tunnel Revisited.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-160
• Molina, Rafael, O. Bayle, and M. Caporicci. 2005. “EVD: A Flight Demonstrator for the Mars Sample Return Earth Reentry Capsule.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3342. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3342
• Molina, Carlos, Alan Johnson, and August Roesener. 2009. “Reusable Launch Vehicle Design Implications for Regeneration Time.” In AIAA SPACE 2009 Conference & Exposition. AIAA 2009-6471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6471
• Molina, R.-C., G. Simeonides, and L. Walpot. 1996. “Pre-Flight Aerothermodynamic Analysis of the Atmospheric Reentry Demonstrator.” In 14th Applied Aerodynamics Conference. AIAA 1996-2468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2468
• Molloe-Christensen, E. 1975. “A Theory of Flight Flutter Testing.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003008
• Molloy, Matthew H. 1999. High-Speed Flight and the Military. Defense Technical Information Center. https://doi.org/10.21236/ada389456
• Molusis, J. H., and S. Briczinski. 1974. “Helicopter Derivative Identification from Analytic Models and Flight Test Data.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017466
• Molvik, Gregory, Jeffrey Bowles, and Loc Huynh. 1993. “A Hypersonic Waverider Research Vehicle with Hydrocarbon Scramjet Propulsion: Design and Analysis.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5097
• Monaghan, R. C. 1978. Flight-Measured Buffet Characteristics of a Supercritical Wing and a Conventional Wing on a Variable-Sweep Airplane. NASA-TP-1244. NASA. https://ntrs.nasa.gov/citations/19780015113
• Monteil, F. 2024. “A1.4: H175 De-Icing Flight Test Campaign: Focus on Flight Test Instrumentation.” In ETTC 2024. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2024/a1.4
• Montel, Mike, and Frank Thielecke. 2015. “Validation of a Model Based Structural Loads Monitoring System Using the Flight Test Aircraft UW-9 Sprint.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2237
• Monterzino, Guido, Craig Lawson, and John Fielding. 2010. “A Methodology for Low-Cost, Rapidimplementation Solutions for Airframe Systems of UAV Prototypes.” In 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. AIAA 2010-9390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9390
• Montgomery, R., and A. Caglayan. 1974. “A Self-Reorganizing Digital Flight Control System for Aircraft.” In 12th Aerospace Sciences Meeting. AIAA 1974-21. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-21
• Montgomery, Peter, and Doug Garrard. 2005. “Test and Evaluation of Hypersonic Aeropropulsion Systems along Flight Trajectories in a Time-Varying Flight Environment.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-3900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3900
• Montgomery, Zachary S., and Douglas F. Hunsaker. 2022. “Control Mapping Methodology for Roll, Pitch, and Yaw Control on Morphing-Wing Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-2531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2531
• Montgomery, R., R. Mekel, and S. Nachmias. 1978. “A Learning Flight Control System for the F8-DFBW Aircraft.” In Guidance and Control Conference. AIAA 1978-1288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1288
• Montoro, Juan, William L. Carbaugh, and Daniel N. Miller. 2023. “DARPA CRANE Program Overview by Lockheed Martin.” In AIAA SCITECH 2023 Forum. AIAA 2023-1808. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1808
• Mooij, H. A. 1973. “In-Flight Measured Human Pilot Describing Function and Remnant for Pitch Attitude Control.” In MIT Proc. of the 9th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19750011079
• Mooij, Erwin. 2024. “Thermal Protection Systems.” In Springer Aerospace Technology. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-62174-1_10
• Moon, Seong, and Seung Kim. 2001. “Active/passive Hybrid Suppression Method of Nonlinear Panel Flutter Using a Piezoelectric Material.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1658. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1658
• Moore, M., and D. Frei. 1983. “X-29 Forward Swept Wing Aerodynamic Overview.” In Applied Aerodynamics Conference. AIAA 1983-1834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1834
• Moore, Archie L., and Constance D. Harney. 1988. “Development of an Integrated Set of Research Facilities for the Support of Research Flight Test.” In AIAA Flight Test Conference. https://ntrs.nasa.gov/citations/19880051485
• Moore, F., T. Hymer, and F. Wilcox. 1993. “Base Drag Prediction on Missile Configurations.” In Flight Simulation and Technologies. AIAA 1993-3629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3629
• Moore, Kevin R., and Andrew Ning. 2018. “Distributed Electric Propulsion Effects on Existing Aircraft through Multidisciplinary Optimization.” In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2018-1652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1652
• Moore, W., A. Skow, and D. Lorincz. 1980. “Enhanced Departure/spin Recovery of Fighter Aircraft through Controlof the Forebody Vortex Orientation.” In 18th Aerospace Sciences Meeting. AIAA 1980-173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-173
• Moorhouse, David. 1990. “Status of the STOL and Maneuver Technology Demonstrator Flight Test Program.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3306
• Moosavian, Amin. 2021. “Variable Geometry Wing-Box: Toward a Robotic Morphing Wing.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14654676
• Morani, Gianfranco, Luca Garbarino, Nicola Genito, and Gianluigi Di Capua. 2024. “Multivariable Fault Tolerant Control for a Distributed Electric Propulsion Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-2358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2358
• Morelli, Eugene A. 1991. “Optimal Input Design for Aircraft Instrumentation Systematic Error Estimation.” In AIAA Atmospheric Flight Mechanics Conference. https://ntrs.nasa.gov/citations/19910062534
• Morelli, Eugene A. 1993. “Practical Input Optimization for Aircraft Parameter Estimation Experiments.” PhD diss., Joint Inst. for Advancement of Flight Sciences. https://ntrs.nasa.gov/citations/19930018075
• Morelli, Eugene A. 1995b. F-18 High Alpha Research Vehicle (HARV) Parameter Identification Flight Test Maneuvers for Optimal Input Design Validation and Lateral Control Effectiveness. NASA-CR-198248. NASA. https://ntrs.nasa.gov/citations/19960012190
• Morelli, Eugene A. 1997. Flight Test Validation of Optimal Input Design and Comparison to Conventional Inputs. AIAA Paper 97-3711. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040105626
• Morelli, Eugene. 1998. “In-Flight System Identification.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4261
• Morelli, Eugene A. 2000a. Identification of Low Order Equivalent System Models from Flight Test Data. NASA/TM-2000-210117. NASA. https://ntrs.nasa.gov/citations/20000085030
• Morelli, Eugene. 2000b. “Low Order Equivalent System Identification for the Tu-144LL Supersonic Transport Aircraft.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3902. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3902
• Morelli, Eugene. 2002. “System Identification Programs for AirCraft (SIDPAC).” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4704
• Morelli, Eugene. 2006. “Practical Aspects of the Equation-Error Method for Aircraft Parameter Estimation.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6144. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6144
• Morelli, Eugene. 2008. “Flight Test Experiment Design for Characterizing Stability and Control of Hypersonic Vechicles.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1682
• Morelli, Eugene. 2010. “Real-Time Aerodynamic Parameter Estimation without Air Flow Angle Measurements.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7951. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7951
• Morelli, Eugene. 2011. “Flight Test Maneuvers for Efficient Aerodynamic Modeling.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6672
• Morelli, Eugene A. 2021a. “Determining Aircraft Moments of Inertia from Flight Test Data.” In AIAA Scitech 2021 Forum. AIAA 2021-1642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1642
• Morelli, Eugene A. 2021c. “Practical Aspects of Multiple-Input Design for Aircraft System Identification Flight Tests.” In AIAA Aviation 2021 Forum. AIAA 2021-2795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2795
• Morelli, Eugene, Stephen Derry, and Mark Smith. 2005. “Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-5921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5921
• Morelli, Eugene A., and Jared A. Grauer. 2018. “Practical Aspects of the Frequency Domain Approach for Aircraft System Identification.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20190001862
• Morelli, Eugene A., and Vladislav Klein. 1995. “Determining the Accuracy of Aerodynamic Model Parameters Estimated from Flight Test Data.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19970012888
• Morelli, Eugene A., and Vladislav Klein. 1997. Accuracy of Aerodynamic Model Parameters Estimated from Flight Test Data. NASA/TM-97-208111. NASA. https://ntrs.nasa.gov/citations/19980048414
• Morelli, M., A. Rausa, T. Bellosta, and A. Guardone. 2023. “Numerical Simulation of Rotorcraft in-Flight Icing and Shedding via a High-Fidelity Method.” In Handbook of Numerical Simulation of In-Flight Icing. Springer International Publishing. https://doi.org/10.1007/978-3-030-64725-4_34-1
• Morgan, W. R., H. C. True, and H. B. Starkey. 1964. “The Army XV-5A Lift Fan Flight Research Airplane.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/640074
• Morgan, Philip E., and Miguel R. Visbal. 2019. “Numerical Simulation of Transonic and Supersonic Flow over a Wall-Mounted Hemisphere.” In AIAA Aviation 2019 Forum. AIAA 2019-2921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2921
• Morgenfeld, Thomas. 1992. “YF-22A Prototype Advanced Tactical Fighter Demonstration/validation Flight Test Program Overview.” In Aerospace Design Conference. AIAA 1992-1087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1087
• Morgenstern, John M. 1998. “Low Sonic Boom Shock Control/alleviation Surface.” Journal of the Acoustical Society of America 104 (5): 2553. https://doi.org/10.1121/1.423821
• Morgenstern, John M. 1999. “Potential for Sonic Boom Reduction of the 2.4-H5085 Arrow Wing HSCT.” In 1995 NASA High-Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/20000027654
• Morgenstern, John. 2012a. “Distortion Correction of Low Sonic Boom Measurements in Wind Tunnels.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3216
• Morgenstern, John. 2012b. “How to Accurately Measure Low Sonic Boom or Model Surface Pressure in Supersonic Wind Tunnels.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3215
• Morgenstern, John. 2012c. “Optimum Signature Shaping for Low Sonic Boom.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3218. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3218
• Morgenstern, John. 2013. “Full Configuration Low Boom Model and Grids for 2014 Sonic Boom Prediction Workshop.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-647
• Morgenstern, John M. 2017. “Removing Distortions from Ground Sonic Boom Measurements for Certification of over Land Flight.” Journal of the Acoustical Society of America 141 (5_Supplement): 3729–3729. https://doi.org/10.1121/1.4988184
• Morgenstern, John, Alan Arslan, Victor Lyman, and Joseph Vadyak. 2005. “F-5 Shaped Sonic Boom Demonstrator’s Persistence of Boom Shaping Reduction through Turbulence.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-12. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-12
• Morger, K. 1988. “Computer Aided Requirements Management System (CARMS) and Flight Test.” In 4th Flight Test Conference. AIAA 1988-2091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2091
• Mori, Takashige, Takeshi Tsuchiya, and Ko Ogasawara. 2002. “Glide-Back Flying Test Bed Concept for Hypersonic Flight Test.” In AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2002-5221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5221
• Mori, Yuji, Aiko Yakeno, and Shigeru Obayashi. 2024. “DNS of Boundary-Layer Transition over a Transonic Swept Wing under Real Flight Condition.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4486. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4486
• Morita, Naoto, and Takeshi Tsuchiya. 2019. “Simultaneous Design and Trajectory Optimization of Waverider-Winged Space Planes.” Journal of the Japan Society for Aeronautical and Space Sciences 67 (5): 152–58. https://doi.org/10.2322/jjsass.67.152
• Morrell, F., M. Bailey, and P. Motyka. 1988. “Flight Test Results of a Vector-Based Failure Detection and Isolation Algorithm for a Redundant Strapdown Inertial Measurement Unit.” In 4th Flight Test Conference. AIAA 1988-2172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2172
• Morrida, Jacob J., Nicholas G. De Lucca, Stanislav Gordeyev, and Eric J. Jumper. 2017. “Simultaneous Pressure and Optical Measurements around a Hemispherical in Subsonic and Transonic Flight.” In AIAA Flight Testing Conference. AIAA 2017-3654. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3654
• Morrida, Jacob J., Stanislav Gordeyev, and Eric J. Jumper. 2016. “Transonic Flow Dynamics over a Hemisphere in Flight.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1349
• Morris, Robert. 1963. “Parameter Selection for in-Flight Recording.” In Testing of Manned Flight Systems Conference. AIAA 1963-1814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1814
• Morris, Charles, James Sheahan, John Dykman, Dan Clingman, and James M. Urnes. 2014. “Control System Design for a Variable Camber Continuous Trailing Edge Flap System on an Elastic Wing.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0835
• Morris, Stephen, and Benjamin Tigner. 1995. “Flight Tests of an Oblique Flying Wing Small Scale Demonstrator.” In Guidance, Navigation, and Control Conference. AIAA 1995-3327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3327
• Morris, Charles E. K., Jr. 1978. “Rotor-Airfoil Flight Investigation: Preliminary Results.” In Proceedings of the Vertical Flight Society Forum 34 - Washington, D.C. 1978. The Vertical Flight Society. https://doi.org/10.4050/vfs-f34-005
• Morris, C., Jr. 1995. “National Aero-Space Plane Achievements and U.S. Space-Launch Goals.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6052
• Morrison, Joseph H., and Anthony E. Washburn. n.d. “NASA/DOD Flight Prediction Workshop.” In NASA/DOD Flight Prediction Workshop. https://ntrs.nasa.gov/citations/20200009682
• Morse, A., and H. Newhouse. 1961. VTOL Downwash Impingement Study. Duct Adapter Test Program. Defense Technical Information Center. https://doi.org/10.21236/ad0253044
• Mort, Kenneth W. 2020. The World’s Largest Wind Tunnels: Their History, Contributions to Aeronautics, and Importance to Flight: A History of the NASA Ames 40- by 80-Foot and 80- by 120-Foot Wind Tunnels. Ames Research Center. https://ntrs.nasa.gov/citations/20205009237
• Mosbah, Ben, Ruxandra M. Botez, and Thien My Dao. 2013. “New Methodology for Calculating Flight Parameters with Neural Network: Extended Great Deluge Method Applied on a Reduced Scale Wind Tunnel Model of an ATR-42 Wing.” In AIAA Modeling and Simulation Technologies (MST) Conference. AIAA 2013-5074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5074
• Moses, Paul L. 2003. X-43C Flight Demonstrator Project Overview. Paper-2C-3. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040042495
• Moses, Robert W., and Gautam H. Shah. 1998. Spatial Characteristics of F/A-18 Vertical Tail Buffet Pressures Measured in Flight. AIAA Paper 98-1956. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040087341
• Moses, Robert W., and Gautam H. Shah. 1999. “Correlation of Fin Buffet Pressures on an F/A-18 with Scaled Wind-Tunnel Measurements.” In CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999. https://ntrs.nasa.gov/citations/19990052691
• Mosher, Michael W. 2005. Chapter 12A: Rotorcraft Flight Envelope Unique Considerations. RTO-AG-300-V14. US Naval Test Pilot School. https://ntrs.nasa.gov/citations/20050209995
• Mosley, R. L. 1972. Space Shuttle Horizontal Flight Test Plan. NASA-TM-X-68515. NASA. https://ntrs.nasa.gov/citations/19720020265
• Moss, James N., Graeme A. Bird, and Virendra K. Dogra. 1988. Nonequilibrium Thermal Radiation for an Aeroassist Flight Experiment Vehicle. AIAA PAPER 88-0081. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880034830
• Moss, Steven, Stanley Cole, and Robert Doggett Jr. 1991. “Some Subsonic and Transonic Buffet Characteristics of the Twin-Vertical-Tails of a Fighter Airplane Configuration.” In 32nd Structures, Structural Dynamics, and Materials Conference. AIAA 1991-1049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1049
• Moszczynski, Gregory J., and Peter R. Grant. 2017. “Adaptive State Estimation for Flight Path Reconstruction and Aircraft System Identification.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-3893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3893
• Mottershead, John E., and J. E. Cooper. 2012. Extension of Flutter Boundaries Using in-Flight Receptance Data. Defense Technical Information Center. https://doi.org/10.21236/ada571493
• Motyka, P., and P. Reynolds. 1971. “The Theory and Flight Verification of the Model-Following Control System for the Air Force Total in-Flight Simulator.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-961
• Moua, Cheng. 2010. Use of ILTV Control Laws for LaNCETS Flight Research. DRC-009-039. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20100039414
• Moua, Cheng M., Timothy H. Cox, and Shaun C. McWherter. 2008. “Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080006639
• Moul, T. M., and L. W. Taylor Jr. 1980. “Determination of an Angle of Attack Sensor Correction for a General Aviation Airplane at Large Angles of Attack as Determined from Wind Tunnel and Flight Tests.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800059133
• Moulden, T., J. Wu, and D. Spring. 1974. “A Flow Field Model for, and Some Studies on the Drag of, an Engine Exhaust System at Transonic Flight Speeds.” In 10th Propulsion Conference. AIAA 1974-1175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1175
• Moulin, Boris. 2004. “Robust Controller Design for Active Flutter Suppression.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5115
• Moulin, Boris, Jie Zeng, and Sunil Kukreja. 2011. “Experimental Model Based Robust Aeroservoelastic Control for the S4T Wind-Tunnel Model.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6370
• Mourey, D. J. 1979. Study of the Feasibility Aspects of Flight Testing an Aeroelastically Tailored Forward Swept Research Wing on a BQM-34F Drone Vehicle. NASA-CR-159149. NASA. https://ntrs.nasa.gov/citations/19800001956
• Moyer, R. 1963. Scientific Passenger Pod, Addendum to Annex Flight Test Directive Missile N-24. Defense Technical Information Center. https://doi.org/10.21236/ad0408760
• Mueller, T. J., and B. Jansen Jr. 1982. “Aerodynamic Measurements at Low Reynolds Numbers.” In 12th Aerodynamic Testing Conference. AIAA 1982-598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-598
• Mueller, A. W., and J. S. Preisser. 1981. Flight Test of a Pure-Tone Acoustic Source. NASA-TP-1898. NASA. https://ntrs.nasa.gov/citations/19810025402
• Mueschke, Nicholas J., James D. Walker, and Donald Grosch. 2020. “Examination of Atmospheric Density Scaling Effects on Sub-Scale Hypersonic Flight Bodies Using a Ballistic Launch Facility.” In 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2020-2444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2444
• Muhamad Jayadi. 2025. “The Transient FSI Simulation for Aeroelastic Evaluation of a Low Subsonic Wing in Cruise Flight Regime.” Jurnal Teknologi Kedirgantaraan 10 (1): 89–98. https://doi.org/10.35894/jtk.v10i1.259
• Muhlstein, L., Jr., D. Petroff, and D. Jillie. 1974. “Experimental Evaluation of an Injector System for Powering a High Reynolds Number Transonic Wind Tunnel.” In 8th Aerodynamic Testing Conference. AIAA 1974-632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-632
• Mullen, Charles D., and Helen L. Reed. 2021. “Analysis of the BOLT II: Holden Mission Flight and Wind Tunnel Geometries.” In AIAA Scitech 2021 Forum. AIAA 2021-0852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0852
• Mullenix, Nathan, Alex Povitsky, and Datta Gaitonde. 2008. “Modeling of Local Intense Ablation in Hypersonic Flight.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2555. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2555
• Müller, Peter. 2005. “Simulation Based Optimal Design.” In Handbook of Statistics. Elsevier. https://doi.org/10.1016/s0169-7161(05)25017-4
• Muller, Mark, and Terrence Wesshaar. 1994. “Maximizing Deflections Produced by Induced Strain Beam-like Actuators for Transonic Drag Reduction.” In Adaptive Structures Forum. AIAA 1994-1775. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1775
• Mundt, Christian, Hannes Griebel, and Chris Welch. 2005. “Studies of Atmospheric Entry of Vehicles with Very Low Ballistic Coefficient.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3384. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3384
• Mungiguerra, S. 2023. “Mini-IRENE, a Successful Re-Entry Flight of a Deployable Heatshield Capsule.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-116
• Munk, M. M. 1921. The Minimum Induced Drag of Aerofoils. NACA-TR-121. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/19800006779
• Muñoz, Hernan Dario Ceron. n.d. “Estudo Da Interferência Aerodinâmica Do Sistema Motopropulsor Em Uma Aeronave Do Tipo \‘Blended Wing Body\’.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/t.18.2009.tde-15052024-152026
• Murakami, Akira. 2006. “Flight Demonstration Project for Low-Sonic Boom Design Technology.” Journal of the Acoustical Society of America 120 (5_Supplement): 3079–3079. https://doi.org/10.1121/1.4787418
• Murakami, Akira, Egon Stanewsky, and Paul Krogmann. 1995. “Boundary Layer Transition on Swept Cylinders at Hypersonic Speeds.” In Fluid Dynamics Conference. AIAA 1995-2276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2276
• Murakoshi, A. 1969. “Real Time, Real Temperature, Jet V/STOL Test Facility.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-310
• Muralidharan, G., V. J. Gilbertraj, and D. Vijay. 2025. “Supercritical Airfoil Analysis for Increasing Critical Mach Number in Subsonic Flight.” International Journal of Scientific Research in Engineering and Management 09 (08): 1–9. https://doi.org/10.55041/ijsrem52300
• Muraoka, Koji, Noriaki Okada, and Daisuke Kubo. 2009. “Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight.” In AIAA Infotech@Aerospace Conference. AIAA 2009-1834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-1834
• Murch, Austin, David Cox, and Kevin Cunningham. 2009. “Software Considerations for Subscale Flight Testing of Experimental Control Laws.” In AIAA Infotech@Aerospace Conference. AIAA 2009-2054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2054
• Murman, E. M. 1979. “A Correction Method for Transonic Wind Tunnel Wall Interference.” In 12th Fluid and Plasma Dynamics Conference. AIAA 1979-1533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1533
• Murman, E. M. 1982. “Application of Computational Fluid Dynamics (CFD) in Transonic Wind-Tunnel/flight-Test Correlation.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017335
• Murman, E., and J. Cole. 1974. “Inviscid Drag at Transonic Speeds.” In 7th Fluid and PlasmaDynamics Conference. AIAA 1974-540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-540
• Murphy, Patrick C. 1996. Closed-Loop System Identification Experience for Flight Control Law and Flying Qualities Evaluation of a High Performance Fighter Aircraft. NASA/TM-1998-207995. NASA. https://ntrs.nasa.gov/citations/19980200994
• Murphy, Patrick C. 1999. “Closed-Loop System Identification Experience for Flight Control Law and Flying Qualities Evaluation of a High Performance Fighter Aircraft.” In System Identification for Integrated Aircraft Development and Flight Testing, RTO Meeting Proceedings 11. https://ntrs.nasa.gov/citations/19990032463
• Murphy, Kelly, Thomas Horvath, Gary Erickson, and Joseph Green. 2002. “Supersonic Aerodynamic Characteristics of Proposed Mars ‘07 Smart Lander Configurations.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4409. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4409
• Murphy, Patrick C., and Vladislav Klein. 2005. Program of Research in Flight Dynamics, the George Washington University at NASA Langley Research Center. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050192561
• Murphy, Patrick, and Vladislav Klein. 2008. “Transport Aircraft System Identification from Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6202
• Murphy, Patrick, and Vladislav Klein. 2010. “Transport Aircraft System Identification Using Roll and Yaw Oscillatory Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8122
• Murphy, Patrick, Vladislav Klein, Neal Frink, and Dan Vicroy. 2011. “System Identification Applied to Dynamic CFD Simulation and Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6522
• Murphy, Patrick C., and Drew Landman. 2015. “Experiment Design for Complex VTOL Aircraft with Distributed Propulsion and Tilt Wing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-0017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0017
• Murphy, Kelly, Robert Nowak, Richard Thompson, Brian Hollis, and Ramadas Prabhu. 1999. “X-33 Hypersonic Aerodynamic Characteristics.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4162
• Murphy, J. D., and M. W. Rubesin. 1965. An Evaluation of Free-Flight Test Data for Aerodynamic Heating from Laminar, Turbulent, and Transitional Boundary Layers. Part II: The X-17 Reentry Body. NASA-CR-70931. NASA. https://ntrs.nasa.gov/citations/19660010795
• Murphy, C. H., and L. E. Schmidt. 1953. The Effect of Length on the Aerodynamic Characteristics of Bodies of Revolution in Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0023468
• Murray, Daniel. 1990. “The AVRO VZ-9 Experimental Aircraft: Lessons Learned.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3237
• Murray, James E., Joseph W. Pahle, Stephen V. Thornton, et al. 2002. Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft. NASA/TM-2002-210721. NASA. https://ntrs.nasa.gov/citations/20020039162
• Murray, Neil, and Johan Steelant. 2009. “Methodologies Involved in the Design of LAPCAT-MR1: A Hypersonic Cruise Passenger Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7399
• Murri, D., M. Croom, and L. Nguyen. 1983. “High Angle-of-Attack Flight Dynamics of a Forward-Swept Wing Fighterconfiguration.” In Applied Aerodynamics Conference. AIAA 1983-1837. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1837
• Murri, D. G., L. T. Nguyen, and S. B. Grafton. 1984. Wind-Tunnel Free-Flight Investigation of a Model of a Forward-Swept-Wing Fighter Configuration. NASA-TP-2230. NASA. https://ntrs.nasa.gov/citations/19840009116
• Murrow, Harold, Kermit Pratt, and John Houbolt. 1989. “NACA/NASA Research Related to Evolution of U.S. Gust Design Criteria.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1373
• Murthy, V., and W. Rose. 1977. “Form Drag, Skin Friction, and Vortex Shedding Frequencies for Subsonic and Transonic Crossflows on Circular Cylinder.” In 10th Fluid and Plasmadynamics Conference. AIAA 1977-687. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-687
• Murthy, S., and F. Steinle. 1986. “Effects of Compressibility and Free-Stream Turbulence on Boundary Layer Transition in High-Subsonic and Transonic Flows.” In 14th Aerodynamic Testing Conference. AIAA 1986-764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-764
• Murzionak, Aliaksandr. n.d. “Rocket Based Combined Cycle Exchange Inlet Performance Estimation at Supersonic Speeds.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2013-06868
• Musal Jr., H. M. Primich, R. I. Blore, and W. E. P. E. Robillard. 1964. Millimeter Radar Instrumentation for Studying Plasma Effects Associated with Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0449823
• Muse, Jonathan, Ali Kutay, and Anthony Calise. 2008. “A Novel Force Control Traverse for Simulating UAV Flight in a Wind Tunnel.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6714
• Mustopa, Opa. 2022. “The Concept of Stealth Unmanned Combat Aerial Vehicle (UCAV) to Support Air Defense Systems.” Defense and Security Studies 3: 74–82. https://doi.org/10.37868/dss.v3.id203
• Mutz, M., E. Pierce, and A. Sievers. 1964. “Supersonic Transport Engine Cycle Selection.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-601
• Muzzey, C. L., and E. A. Kidd. 1959. “Measurement and Interpretation of Flight Test Data for Dynamic Stability and Control.” In Stability and Control. Elsevier. https://doi.org/10.1016/b978-1-4831-9730-2.50020-x
• Mychalowycz, Evhen, and Brahmananda Panda. 1996. “Aeroelastic Stability Wind Tunnel Testing with Analytical Correlation of the Comanche Bearingless Main Rotor.” In Proceedings of the Vertical Flight Society Forum 52 - Washington, DC 1996. The Vertical Flight Society. https://doi.org/10.4050/vfs-f52-1026
• Myers, T. T., D. E. Johnston, and D. T. McRuer. 1984. Space Shuttle Flying Qualities Criteria Assessment, Phase 3. NASA-CR-170407. NASA. https://ntrs.nasa.gov/citations/19840012497
• Myers, T., and G. Stromberg. 1978. “Ground Test Facility for Integral Rocket Ramjets.” In 14th Joint Propulsion Conference. AIAA 1978-934. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-934
• Myers, Lawrence, and Kevin Walsh. 1988. “Performance Improvements of an F-15 Airplane with an Integrated Engine-Flight Control System.” In 4th Flight Test Conference. AIAA 1988-2175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2175
• Myschik, Stephan, Lukas Kinast, Michaela Huemer, Davide Vicca, Daniel Dollinger, and Florian Holzapfel. 2022. “Development of a Flight Control System for a Cyclocopter UAV Demonstrator.” In AIAA AVIATION 2022 Forum. AIAA 2022-3282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3282
• NACA Conference on Aerodynamic Problems of Transonic Airplane Design. 1949. NASA-TM-X-56649. NASA. https://ntrs.nasa.gov/citations/19650074048
• NACA Conference on Aircraft Loads, Flutter, and Structures Compilation of Papers. 1953. NASA-TM-X-57364. NASA. https://ntrs.nasa.gov/citations/19660012350
• NACA/NASA History at Dryden, Part 1 and 2. 1990. NASA-TM-104287. NASA. https://ntrs.nasa.gov/citations/19950004301
• Nadell, Samuel, Alex DiJoseph, Tom Berger, and Eric Huang. 2023. “Development, Simulation, and Flight Testing of Damage Tolerant Control Laws for the ADAPT™ Winged Compound Helicopter Scaled Demonstrator.” In Proceedings of the Vertical Flight Society 79th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0079-2023-17963
• Nae, Catalin. 1998. “Synthetic Jets Influence on NACA 0012 Airfoil at High Angles of Attack.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4523. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4523
• Nae, Cătălin, Ilie Nicolin, and Bogdan Adrian Nicolin. 2022. “Military Aircraft Flight Control.” In Aeronautics - New Advances. IntechOpen. https://doi.org/10.5772/intechopen.105491
• Nae, Catalin, Gabriela Liliana Stroe, Irina-Carmen Andrei, and Sorin Berbente. 2019. “Flutter Suppression by Active Control Technology.” In AIP Conference Proceedings, vol. 2133. AIP Publishing. https://doi.org/10.1063/1.5114362
• Naeseth, R. L. 1970. Model Wind-Tunnel and Flight Investigation of a Parawing Lifting Body Landing System. NASA-TN-D-5893. NASA. https://ntrs.nasa.gov/citations/19700031351
• Nagai, Hiroki. 2013. “Characteristics of Low-Reynolds Number Airfoils in a Mars Wind Tunnel.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-73. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-73
• Nagamatsu, Henry T. 1962. “Section h. Hypersonic Experimental Facilities.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-010
• Nagamatsu, H. T., B. C. Graber, and R. E. Sheer. 1965. “Transition of Hypersonic Boundary Layer.” Physics of Fluids 8 (2): 211–21. https://doi.org/10.1063/1.1761211
• Nagamatsu, H., and R. Orozco. 1984. “Porosity Effect on Supercritical Airfoil Drag Reduction by Shock Wave/boundary Layer Control.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1682
• Nagamatsu, Henry, and Russell Sheer. 1964. “Boundary-Layer Transition on a Highly Cooled 10 Degree Cone in Hypersonic Flows.” In Entry Technology Conference. AIAA 1964-1312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-1312
• Nagamatsu, H., T. Trilling, and J. Bossard. 1987. “Passive Drag Reduction on a Complete NACA 0012 Airfoil at Transonic Mach Numbers.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1263
• Nagata, John I., Herman P. Wolf, Shapley Jr., and John J. 1968. Engineering Flight Test (Product Improvement Test) of Production OH-6A Helicopter Unarmed and Armed with the XM-27E1 Weapon System Phase d. Defense Technical Information Center. https://doi.org/10.21236/ad0834574
• Nagel, A. L. 1967. Compressible Boundary Layer Stability by Time Integration of the Navier- Stokes Equations and an Extension of Emmons’ Transition Theory to Hypersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0661318
• Nagel, A. L. 1982. “Opportunities for Wind-Tunnel/flight Correlation with New Boeing Airplanes.” In NASA. Langley Research Center Wind-Tunnel-Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017330
• Nagel, A., and A. Thomas. 1965. “Analysis of the Correlation of Wind Tunnel and Ground Test Data to Flight Test Results.” In Flight Testing Conference. AIAA 1965-208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-208
• Nagy, Christopher J., and Paul W. Kirsten. 1976. Handling Qualities and Stability Derivatives of the X-24B Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/adb012970
• Nair, Pranay Prem, and Mayur Kukreja. 2025. “Reusable Launch Vehicle and Rocket Study.” Preprint, . https://doi.org/10.31224/4543
• Nakahashi, Kazuhiro, Fumiya Togashi, Takeshi Fujita, and Yasushi Ito. 2002. “Numerical Simulations on Separation of Scaled Supersonic Experimental Airplane from Rocket Booster at Supersonic Speed.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2843. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2843
• Nakatani, Hiroki, Hideyuki Taguchi, Kazuhisa Fujita, Shigemi Shindo, and Shinji Honami. 2009b. “Wind Tunnel Test of Mach 5 Class Hypersonic Airplane.” Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan 7 (ists26): Pe_71-Pe_76. https://doi.org/10.2322/tstj.7.pe_71
• Nakatani, Hiroki, Hideyuki Taguchi, Motoyuki Hongoh, and Shinji Honami. 2009a. “An Experimental Study on Aerodynamic Design of Hypersonic Airplane.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7434
• Nakatani, Hiroki, Hideyuki Taguchi, Atsushi Ueno, Motoyuki Hongoh, Naoyuki Okamura, and Shinji Honami. 2011. “Evaluation of Aerodynamic Performance of a Hypersonic Experimental Aircraft.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2339. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2339
• Nalianda, Devaiah, and Riti Singh. 2014. “Turbo-Electric Distributed Propulsion – Opportunities, Benefits and Challenges.” Aircraft Engineering and Aerospace Technology 86 (6): 543–49. https://doi.org/10.1108/aeat-03-2014-0035
• Nam, Changho, Youdan Kim, Jeffrey Layton, Changho Nam, Youdan Kim, and Jeffrey Layton. 1997. “Active Aeroelastic Wing Design for Gust Load Alleviation and Flutter Suppression.” In 38th Structures, Structural Dynamics, and Materials Conference. AIAA 1997-1265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1265
• Nance, Douglas V. 2013. Preliminary Study of Turbulence for a Lobed Body in Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada571259
• Nangia, R., M. Palmer, and C. Tilmann. 2003. “Unconventional High Aspect Ratio Joined-Wing Aircraft with Aft- and Forward-Swept Wing-Tips.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-605
• Napolitano, Marcello, Giampiero Campa, Brad Seanor, and Yongkyu Song. 2001a. “Comparison of on-Line and off-Line Parameter Estimation Techniques Using the NASA F/A-18 HARV Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4261
• Napolitano, Marcello, Alfonso Paris, Brad Seanor, and Albion Bowers. 1994. “Parameter Estimation for a Cessna U-206 Aircraft Using the Maximum Likelihood Method.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3481. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3481
• Nark, Douglas M., and Michael G. Jones. 2019. “Design of an Advanced Inlet Liner for the Quiet Technology Demonstrator 3.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20200002610
• Nark, Douglas M., William T. Jones, Pieter G. Buning, and Joseph M. Derlaga. 2017. “High-Lift Propeller Noise Prediction for a Distributed Electric Propulsion Flight Demonstrator.” In 23rd AIAA/CEAS Aeroacoustics Conference. AIAA 2017-3713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3713
• Narramore, J. C., and Jing G. Yen. 1982. “A New Transonic Airfoil Design Method and Its Application to Helicopter Rotor Airfoil Design.” In Proceedings of the Vertical Flight Society Forum 38 - Anaheim, CA 1982. The Vertical Flight Society. https://doi.org/10.4050/vfs-f38-002
• “NASA Glenn Research Center’s Hypersonic Tunnel Facility.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0427.0439
• NASA Langley Research Center (NASA LaRC). 2022. The Rowman & Littlefield Publishing Group. https://doi.org/10.5040/9781666997361.ch-8
• Nash, J. 1981. “The Advanced Range Instrumentation Aircraft Improvement and Modernization Program.” In 1st Flight Test Conference. AIAA 1981-2368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2368
• Nash, D., H. Katz, and W. Moody. 1975. “F-15 Flight Flutter Testing: Aircraft Systems and Test Operations.” In Aircraft Systems and Technology Meeting. AIAA 1975-1031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1031
• Nasir, Rizal E. M., and Wahyu Kuntjoro. 2013. “Longitudinal Flight Stability Augmentation of a Small Blended Wing-Body Aircraft with Canard as Control Surface.” Applied Mechanics and Materials 393: 329–37. https://doi.org/10.4028/www.scientific.net/amm.393.329
• Nasir, Rizal E. M., Firdaus Mohamed, Ramzyzan Ramly, Aman M. I. Mamat, Wirachman Wisnoe, and Wahyu Kuntjoro. 2015. “Flight Performance of Various Blended Wing-Body Small UAV Designs.” Jurnal Teknologi 75 (8). https://doi.org/10.11113/jt.v75.5214
• Nasu, Ken-Ichi. 1986. Tilt-Rotor Flutter Control in Cruise Flight. NASA-TM-88315. NASA. https://ntrs.nasa.gov/citations/19870009139
• Nath, Sri R., and Sah D. S. Ana. 2017. “Aerodynamic Analysis of Forward Swept Wing Using Prandtl-D Wing Concept.” International Journal of Engineering Trends and Technology 54 (2): 75–81. https://doi.org/10.14445/22315381/ijett-v54p212
• Nathan, Pranav. 2026. “Active Lateral-Directional Stabilisation of an Oblique Wing Using Distributed Electric Propulsion.” Preprint, . https://doi.org/10.2139/ssrn.7045238
• Naval Air Test Center Patuxent River MD. 1963. Flight Test and Evaluation of Astek Instrument Corporation Large Numeral Drum-Pointer Altimeters, Type A0009 20101 and Type B0001 22107. Defense Technical Information Center. https://doi.org/10.21236/ad0669901
• Navarro, Robert. 1997. Performance of an Electro-Hydrostatic Actuator on the F-18 Systems Research Aircraft. NASA/TM-97-206224. NASA. https://ntrs.nasa.gov/citations/19970034702
• Navarro, Robert. 2005. “2005 PathfinderPlus Aero-Elastic Research Flight.” In 31st Society of Mexican-American Engineers and Scientists (MAES) Symposium. https://ntrs.nasa.gov/citations/20070035091
• Navarro, Robert. 2009. “NASA Dryden Flight Research Center.” In Congreso “Evolucion 09,”. https://ntrs.nasa.gov/citations/20090042982
• Neal, Ronald D. 1970. “Correlation of Small-Scale and Full-Scale Wind Tunnel Data with Flight Test Data on the Lear Jet Model 23.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/700237
• Neal, Bradford, and Bradley Flick. 2017. “NASA Armstrong Flight Research Center Airworthiness and Flight Safety Review Process Overview.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170005549
• Neely, Amanda, Lamar Auman, and William Blake. 2003. “Missile DATCOM Transonic Drag Improvements for Hemispherical Nose Shapes.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3668
• Neely, Andrew, and W. Tjong. 2008. “Calibration of Thermal Paints for Hypersonic Flight Test.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2664. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2664
• Negaard, Gordon R. 1979. Analysis of a Pyroceram Radome Subjected to Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ada363019
• Negaard, Gordon. 1980. The History of the Aircraft Structural Integrity Program. Defense Technical Information Center. https://doi.org/10.21236/ada361289
• Nelson, Norman. 1956. “The Advantages of the Ducted Propeller in VTOL Aircraft Design.” In Proceedings of the American Helicopter Society Western Forum, Dallas, Texas 1956. The Vertical Flight Society. https://doi.org/10.4050/sm_wf_1956-4470
• Nelson, R. 1984. “The Influence of Airfoil Roughness on the Performance of Flight Vehicles at Low Reynolds Numbers.” In 22nd Aerospace Sciences Meeting. AIAA 1984-540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-540
• Nelson, R., A. Arena Jr., and D. Williams II. 1993. “The Use of Subscale Models to Predict Self-Induced Oscillations of Flight Vehicles.” In 31st Aerospace Sciences Meeting. AIAA 1993-93. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-93
• Nelson, Stewart L., Mark G. Ballin, Bryan A. Barrows, et al. 2024. “Designing a Flight Test of a Flight Path Management System for Advanced Air Mobility Research.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20230016894
• Nelson, R., D. Price, R. Nelson, and D. Price. 1997. “Some Simplifying Concepts for Conducting Lifting Body Model Flight Tests at near Orbital Speeds.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-195
• Nelson, Robert L., and William E. Stoney Jr. 1953. Pressure Drag of Bodies at Mach Numbers up to 2.0. NACA-RM-L53I22c. NASA. https://ntrs.nasa.gov/citations/19930093736
• Neogi, Natasha, Mallory Graydon, Jon Holbrook, Jeffrey Maddalon, and Frank McCormick. 2025. “Enabling Novel Collaborative Control Paradigms between Humans and Machines in Electric Vertical Takeoff and Landing (eVTOL) Aircraft.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0359
• Nepomuceno, Leonardo, and Roberto Gil Annes Da Silva. 2021. “Flight Simulator Model of a Subscale Generic Future Fighter.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-1010
• Nettleton, T. 1965. “Handling Qualities Research in the Development of a Stol Utility Transport Aircraft.” In Low-Speed Flight Meeting. AIAA 1965-713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-713
• Neuhaus, Jason R. 2018. Heads-Up Display with Virtual Precision Approach Path Indicator as Implemented in a Real-Time Piloted Lifting-Body Simulation. NASA/TM-2018-219803. NASA. https://ntrs.nasa.gov/citations/20180001968
• Neumann, S. 2005. “77. Health and Environmental Engineering Flight Test at the Air Force Flight Test Center.” In AIHce 2005. AIHA. https://doi.org/10.3320/1.2758668
• Neumannn, M., J. Moore, S. Pantham, M. Moodie, P. Noonan, and A. Whittington. 2016. “3.1: An Adaptable Constraints-Based Metadata Description Language (MDL) System for Flight Test Instrumentation Configuration.” In Proceeding - etc2016. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/etc2016/3.1
• Newberry, Conrad. 1995. “The Conceptual Design of Deck-Launched Waverider Configured Aircraft.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6155
• Newman, Brett, and Carey Buttrill. 1995. “Conventional Flight Control for an Aeroelastic, Relaxed Static Stability High-Speed Transport.” In Guidance, Navigation, and Control Conference. AIAA 1995-3250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3250
• Newman, P. A., W. B. Kemp, and J. A. Garriz. 1988. “Emerging Technology for Transonic Wind-Tunnel-Wall Interference Assessment and Corrections.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/881454
• Newsam, Mike, Alden S. Midmer, and Christoph Bruecker. 2024. “Experimental Development and Flight Testing of a Full-Span Morphing Wing Aircraft with Peregrine Falcon Wing Modalities.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4131. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4131
• Newsom, J. 1978. “Synthesis of Active Flutter Suppression Systems Using Optimal Control Theory.” In Guidance and Control Conference. AIAA 1978-1270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1270
• Newsom, J., and A. Pototzky. 1981. “Comparison of Analysis and Flight Test Data for a Drone Aircraft with Active Flutter Suppression.” In Dynamics Specialists Conference. AIAA 1981-640. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-640
• Newsom, W. A., Jr., D. R. Satran, and J. L. Johnson Jr. 1982. Effects of Wing-Leading-Edge Modifications on a Full-Scale, Low-Wing General Aviation Airplane: Wind-Tunnel Investigation of High-Angle-of-Attack Aerodynamic Characteristics. NASA-TP-2011. NASA. https://ntrs.nasa.gov/citations/19820018341
• Newton, F. J. P. 1965. “Application of the Vector Plotting Technique to Flight Flutter Testing of the Hawker Siddeley Trident.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50006-3
• “Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0345.0377
• Ngo, Tien Ken Kevin. n.d. “Effect of Injection Strategy and Mainstream Combustion on Skin Friction Reduction through Boundary Layer Combustion in Scramjet Combustors.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2017.193
• Ngoc, Hoang Thi Bich. 2007. “Influences of the Compressibility on Aerodynamic Characteristics of Profile under the Transonic Flow Theory.” Vietnam Journal of Mechanics 29 (4): 497–506. https://doi.org/10.15625/0866-7136/29/4/5598
• Nguyen, L. T. 1979. “Control System Techniques for Improved Departure/spin Resistance for Fighter Aircraft.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19800042469
• Nguyen, Luat T. 1989. Flight Dynamics Research for Highly Agile Aircraft. SAE PAPER 892235. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910033077
• Nguyen, Nhan T. 2017. “Flight Control of Flexible Aircraft.” In NASA NESC Guidance, Navigation and Control (GNC) Meeting 2017. https://ntrs.nasa.gov/citations/20170009881
• Nguyen, Ba, and Thomas Cord. 1999. “Comparison and Analysis of Pilot-Induced Oscillation Characteristics from Flight Test and Ground-Based Simulation.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4004. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4004
• Nguyen, Nhan T., Nick B. Cramer, Kelley E. Hashemi, et al. 2020. “Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System.” In AIAA Scitech 2020 Forum. AIAA 2020-0214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0214
• Nguyen, Nhan T., Nick B. Cramer, Kelley E. Hashemi, et al. 2019b. “Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System.” In AIAA Aviation 2019 Forum. AIAA 2019-3156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3156
• Nguyen, Nhan T., Michael Drew, and Sean S. Swei. 2016. “Adaptive Modal Identification for Flutter Suppression Control.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160008950
• Nguyen, Nhan T., Jason Fugate, Upender K. Kaul, and Juntao Xiong. 2019a. “Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction.” In AIAA Scitech 2019 Forum. AIAA 2019-0217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0217
• Nguyen, L., W. Gilbert, J. Gera, K. Iliff, and E. Enevoldson. 1980a. “Application of High-Alpha Control System Concepts to a Variable-Sweep Fighter Airplane.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1582. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1582
• Nguyen, Luat T., William P. Gilbert, and Marilyn E. Ogburn. 1980b. Control-System Techniques for Improved Departure/spin Resistance for Fighter Aircraft. NASA-TP-1689. NASA. https://ntrs.nasa.gov/citations/19800020743
• Nguyen, Nhan, Upender Kaul, Sonia Lebofsky, Eric Ting, Daniel Chaparro, and James Urnes. 2015c. “Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing.” In SAE AeroTech Congress & Exhibition. https://ntrs.nasa.gov/citations/20150023531
• Nguyen, Nhan T., Eli Livne, Nathan Precup, et al. 2014a. “Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2441
• Nguyen, L. T., M. E. Ogburn, W. P. Gilbert, K. S. Kibler, P. W. Brown, and P. L. Deal. 1979. Simulator Study of Stall/post-Stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability. NASA-TP-1538. NASA. https://ntrs.nasa.gov/citations/19800005879
• Nguyen, Nhan T., Nathan Precup, Eli Livne, et al. 2015d. “Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2417
• Nguyen, Nhan T., and Ezra A. Tal. 2015. “A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1843. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1843
• Nguyen, Cuong, Sebastien Terrana, and Jaime Peraire. 2023. “Implicit Large Eddy Simulation of Hypersonic Boundary-Layer Transition for a Flared Cone.” In AIAA SCITECH 2023 Forum. AIAA 2023-0659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0659
• Nguyen, Nhan T., Eric Ting, and Sonia Lebofsky. 2015a. “Aeroelastic Analysis of Wind Tunnel Test Data of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap (VCCTEF).” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1405. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1405
• Nguyen, Nhan T., Eric Ting, and Sonia Lebofsky. 2015b. “Aeroelasticity of Axially Loaded Aerodynamic Structures for Truss-Braced Wing Aircraft.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1840
• Nguyen, Nhan T., Eric B. Ting, Daniel Nguyen, Tung Dao, and Khanh Trinh. 2013. “Coupled Vortex-Lattice Flight Dynamic Model with Aeroelastic Finite-Element Model of Flexible Wing Transport Aircraft with Variable Camber Continuous Trailing Edge Flap for Drag Reduction.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4746
• Nguyen, Nhan T., Eric Ting, Daniel Y. Nguyen, and Khanh V. Trinh. 2014b. “Flutter Analysis of Mission-Adaptive Wing with Variable Camber Continuous Trailing Edge Flap.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0839
• Nguyen, Nhan, and James Urnes. 2012. “Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4642
• Nguyen, Nhan, and Juntao Xiong. n.d. “Nonlinear Time-Domain System Identification of Aircraft Stability and Control Derivatives.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20250011779
• Nguyen, Nhan T., and Juntao Xiong. 2021. “Transonic Correction Method for Flight Dynamic Stability Analysis of Mach 0.745 Transonic Truss-Braced Wing.” In AIAA Aviation 2021 Forum. AIAA 2021-2574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2574
• Nguyen, Nhan T., and Juntao Xiong. 2022a. “CFD-Based Frequency Domain Method for Dynamic Stability Derivative Estimation with Application to Transonic Truss-Braced Wing.” In AIAA AVIATION 2022 Forum. AIAA 2022-3596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3596
• Nguyen, Nhan T., and Juntao Xiong. 2022b. “Dynamic Aeroelastic Flight Dynamic Modeling of Mach 0.745 Transonic Truss-Braced Wing.” In AIAA SCITECH 2022 Forum. AIAA 2022-1325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1325
• Nguyen, Nhan T., and Juntao Xiong. 2023a. “Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing.” In AIAA AVIATION 2023 Forum. AIAA 2023-3945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3945
• Nguyen, Nhan T., and Juntao Xiong. 2023b. “High-Fidelity Flight Dynamic Analysis of Transonic Truss-Braced Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-0998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0998
• Nguyen, Nhan T., and Juntao Xiong. 2024a. “Computationally Efficient Frequency Domain Method for Dynamic Control Derivative Estimation with Application to Transonic Truss-Braced Wing.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4348. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4348
• Nguyen, Nhan T., and Juntao Xiong. 2024b. “Nonlinear Dynamic Control Derivative Analysis for Aircraft Application to Transonic Truss-Braced Wing.” In AIAA SCITECH 2024 Forum. AIAA 2024-0251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0251
• Nguyen, Nhan T., Juntao Xiong, and Jason Fugate. 2021b. “Multi-Point Jig Twist Optimization of Mach 0.745 Transonic Truss-Braced Wing Aircraft and High-Fidelity CFD Validation.” In AIAA Scitech 2021 Forum. AIAA 2021-0338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0338
• Nguyen, Nhan T., Juntao Xiong, and Jonathan Sager. 2021a. “Fuel-Optimal Trajectory Optimization of Mach 0.745 Transonic Truss-Braced Wing with Variable Camber Continuous Trailing Edge Flap.” In AIAA Aviation 2021 Forum. AIAA 2021-2575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2575
• Ni, Xu, Mingkai Wang, Xuejun Li, and Shuguang Zhang. 2025. “A Yaw-Roll Coupling Suppression Control Method for eVTOL Aircraft with Nonuniform Propulsion Layout.” Journal of Physics: Conference Series 3044 (1): 012001. https://doi.org/10.1088/1742-6596/3044/1/012001
• Nial, J. 1972. “Status of U.S. Navy Stall/post-Stall/spin Flight Testing.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-787
• Niazi, Saeid, Ram JanakiRam, and Roger L. Smith. 2006. “Airframe Aerodynamics of the CRW Demonstrator Aircraft in Hover with Winds.” In Proceedings of the Vertical Flight Society Forum 62 - Phoenix, AZ 2006. The Vertical Flight Society. https://doi.org/10.4050/vfs-f62-029
• Nichols, Herbert. 1988. “UDF engine/MD80 Flight Test Program.” In 24th Joint Propulsion Conference. AIAA 1988-2805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2805
• Nichols, J. 1990. “The Hiller X-18 Experimental Aircraft: Lessons Learned.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3203
• Nicholson, Robert, and Randall B. Lowry. 1966. XV-4A VTOL Research Aircraft Program. Defense Technical Information Center. https://doi.org/10.21236/ad0635106
• Nickerson, Joseph D., Jr., Joseph T. Driscoll, and Gregory P. Wright. 1991. “Handling Qualities of the H-76 Fantailtm Demonstrator.” In Proceedings of the Vertical Flight Society Forum 47 - Phoenix, AZ 1991. The Vertical Flight Society. https://doi.org/10.4050/vfs-f47-1009
• Nicolai, Leland, Keith Hunten, Paul Scott Zink, and Peter Flick. 2010b. “System Benefits of Active Flutter Suppression for a SensorCraft-Type Vehicle.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9349
• Nicolaides, J. 1970. “Parafoil Flight Performance.” In 3rd Aerodynamic Deceleration Systems Conference. AIAA 1970-1190. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1190
• Nicolaides, John D. 1971. Parafoil Wind Tunnel Tests. Defense Technical Information Center. https://doi.org/10.21236/ad0731564
• Nicolaides, John D. 1976. Flight Test Results of a Powered Parafoil System (Aeroflyer). Defense Technical Information Center. https://doi.org/10.21236/ada056569
• Nicolet, W., N. Vojvodich, and H. Morse. 1974. “Outer Planet Probe Entry Thermal Protection. I Aerothermodynamic Environment.” In Thermophysics and Heat Transfer Conference. AIAA 1974-700. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-700
• Nicolosi, Fabrizio, Agostino De Marco, and Pierluigi Della Vecchia. 2010. “Parameter Estimation and Flying Qualities of a Twin-Engine CS23/FAR23 Certified Light Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7947. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7947
• Nicolosi, Fabrizio, Valerio Marciello, and Francesco Orefice. 2022. “Conceptual Design of a Hydrogen-Propelled Aircraft with Distributed Electric Propulsion.” In AIAA AVIATION 2022 Forum. AIAA 2022-3205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3205
• Niebanck, Charles F. 1969. “A Comparison of Dynamically Scaled Model Rotor Test Data with Discrete Azimuth Aeroelastic Stability Theory.” In Proceedings of the Vertical Flight Society Forum 25 - Washington, D.C. 1969. The Vertical Flight Society. https://doi.org/10.4050/vfs-f25-025
• Niedling, L. G. 1982. “F-15 Wind-Tunnel/flight Correlations.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017327
• Niedzwiecki, A., and H. S. Ribner. 1977. Subjective Loudness of Sonic Boom: N-Wave and Minimized (‘Low-Boom’) Signatures. Defense Technical Information Center. https://doi.org/10.21236/ada050136
• Niehaus, Owen Q. 1962. “Army-Navy Instrumentation Program RH-1 Flight Test Results.” Journal of the American Helicopter Society 7 (1): 24–32. https://doi.org/10.4050/jahs.7.24
• Nielsen, J. 1985a. “Arrays for Minimum Wave Drag of Bodies of Revolution.” In 23rd Aerospace Sciences Meeting. AIAA 1985-449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-449
• Niemiec, Robert, Farhan Gandhi, and George Jacobellis. 2014. “Reversible Airfoil for Stopped Rotors in High Speed Flight.” In Proceedings of the Vertical Flight Society 70th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0070-2014-9426
• Niessen, F. R. 1969. Simultaneous Usage of Attitude Control for VTOL Maneuvering Determined by in-Flight Simulation. NASA-TN-D-5342. NASA. https://ntrs.nasa.gov/citations/19690022732
• Niewald, P., and S. Parker. 1999a. “Flight Test Techniques Employed to Successfully Verify F/A-18E in-Flight Lift and Drag.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-768
• Niewald, P., and S. Parker. 1999b. “Wind Tunnel Techniques Employed to Successfully Predict F/A-18E in-Flight Lift and Drag.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-767. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-767
• Nikfetrat, K., C. Van Dam, P. Vijgen, and I. Chang. 1992. “Prediction of Drag at Subsonic and Transonic Speeds Using Euler Methods.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-169
• Nikolic, Vojin, and Eric Jumper. 2004. “Zero-Lift Wave Drag Calculation Using Supersonic Area Rule and Its Modifications.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-217
• Ning, Simeon, and Ilan Kroo. 2011. “Compressibility Effects of Extended Formation Flight.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3812
• Nishanth, P., A. Arokkiaswamy, and Anthony Alen A. 2019. “Shape Optimization of Blended-Wing-Body Configuration- an Experimental Approach.” Preprint, . https://doi.org/10.2139/ssrn.3507300
• Nishikawa, Takaki, and Kenichi Rinoie. 2024. “A Comprehensive Study on Hydrogen and Hybrid Electric Aircraft with Distributed Electric Propulsion.” In AIAA SCITECH 2024 Forum. AIAA 2024-2311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2311
• Nissen, James M., and Burnett L. Gadeberg. 1944. Effect of Mach and Reynolds Numbers on the Power-Off Maximum Lift Coefficient Obtainable on a P-39N-1 Airplane as Determined in Flight. NACA-ACR-4F28. Ames Aeronautical Laboratory. https://ntrs.nasa.gov/citations/20150011305
• Nissen, James M., Burnett L. Gadebero, and William T. Hamilton. 1948. Correlation of the Drag Characteristics of a Typical Pursuit Airplane Obtained from High-Speed Wind-Tunnel and Flight Tests. NACA-TR-916. NASA. https://ntrs.nasa.gov/citations/19930091981
• Nissim, E. 1975. “Active Flutter Suppression Using Trailing-Edge and Tab Control Surfaces.” In 16th Structural Dynamics, and Materials Conference. AIAA 1975-822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-822
• Nissim, E. 1977. “Application of the Aerodynamic Energy Concept to the Selection of Transfer Functions for Flutter Suppression and Gust Alleviation Using Active Controls.” In 18th Structural Dynamics and Materials Conference. AIAA 1977-423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-423
• Nissim, E., and G. B. Gilyard. 1989. “Method for Experimental Determination of Flutter Speed by Parameter Identification.” In AIAA, ASME, ASCE, AHS, and ASC, Structures, Structural Dynamics and Materials Conference. https://ntrs.nasa.gov/citations/19890043430
• Nissim, E., and I. Lottati. 1979a. “Active Controls for Flutter Suppression and Gust Alleviation in Supersonic Aircraft.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-792
• Niu, Jian, and Ying Piao. 2016. “Numerical Simulation of Liquid Kerosene Combustion in a Dual-Mode Scramjet Combustor Using Flamelet/Progress Variable Approach.” In 46th AIAA Fluid Dynamics Conference. AIAA 2016-3959. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3959
• Niu, Menghao, and Caihong Su. 2023. “Receptivity and Its Influence on Transition Prediction of a Hypersonic Boundary Layer over a Small Bluntness Cone.” Physics of Fluids 35 (3): 034109. https://doi.org/10.1063/5.0141000
• Nixon, David. 2003. “A Relationship between Wave Drag and Induced Drag.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2003-01-3021
• Noll, T., R. Calico, and F. Eastep. 1983b. “Control of Forward Swept Wing Aeroelastic Instabilities Using Activefeedback Systems.” In Guidance and Control Conference. AIAA 1983-2220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2220
• Noll, T., F. Eastep, and R. Calico. 1983a. “Active Suppression of Aeroelastic Instabilities on a Forward Swept Wing.” In 24th Structures, Structural Dynamics and Materials Conference. AIAA 1983-991. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-991
• Noll, T., and L. Huttsell. 1978. “Wing/store Active Flutter Suppression: Correlation of Analyses and Wind Tunnel Data.” In Aircraft Systems and Technology Conference. AIAA 1978-1459. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1459
• Nompelis, Ioannis, and Graham Candler. 2007. “Investigation of Hypersonic Double-Cone Flow Experiments at High Enthalpy in the LENS Facility.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-203
• Nomura, Masayuki, Koji Fujita, and Hiroki Nagai. 2018. “Computational Study of Aerodynamic Characteristics on Reentry Capsule Aft-Body Shape in Transonic Flow.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0290
• Noneman, S. 2002. “Operations Analysis of the 2nd Generation Reusable Launch Vehicle.” In SpaceOps 2002 Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-t4-34
• “Nonequilibrium Viscous Flow and Convective Heating of a Jovian Entry Probe at High Altitudes.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0104.0123
• Nonsteady Flight in the Vertical Plane. 2006. Wiley. https://doi.org/10.1002/9780470117859.ch6
• Nonweiler, T. R. F. 1959. “Aerodynamic Problems of Manned Space Vehicles.” Journal of the Royal Aeronautical Society 63 (585): 521–28. https://doi.org/10.1017/s0368393100071662
• Nonweiler, T. R. F. 1973. “Revised Calculations of the NACA 6-Series of Low Drag Aerofoils.” Aeronautical Journal 77 (748): 190–92. https://doi.org/10.1017/s0001924000040707
• Norlin, Ken. 1995. “Flight Simulation Software at NASA Dryden Flight Research Center.” In Flight Simulation Technologies Conference. AIAA 1995-3419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3419
• Norman, David C., and John R. Somsel. 1967. “DETERMINATION OF HELICOPTER ROTOR BLADE COMPRESSIBILITY EFFECTS – PREDICTION vs FLIGHT TEST.” In Proceedings of the Vertical Flight Society Forum 23 - Washington, D.C. 1967. The Vertical Flight Society. https://doi.org/10.4050/vfs-f23-001
• Norris, R. 1979. “Simulation of Rocket Plume Interference on the X-24B at Transonic Speeds.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1666. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1666
• Norris, Stephen R., Edward A. Haering Jr., and James E. Murray. 1995. “Ground-Based Sensors for the SR-71 Sonic Boom Propagation Experiment.” In NASA High Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/19960008877
• Norris, Stephen R., Edward A. Haering Jr., and James E. Murray. 1996. “Ground-Based Sensors for the SR-71 Sonic Boom Propagation Experiment.” In The 1995 NASA High-Speed Research Program Sonic Boom Workshop. https://ntrs.nasa.gov/citations/19960055059
• North American Aviation INC LOS Angeles CA. 1964. Research on Photographic Window Problem in Supersonic and Hypersonic Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0607252
• Northrop Aircraft INC Hawthorne CA. 1952. Methods of Analysis and Synthesis of Piloted Aircraft Flight Control Systems. Volume 1. Defense Technical Information Center. https://doi.org/10.21236/ad0024361
• Northrop Aircraft INC Hawthorne CA. 1953. Dynamics of the Airframe. Defense Technical Information Center. https://doi.org/10.21236/ad0022941
• Norton, William. 1989. “Aeroelastic Design of a Composite Wing with Wind Tunnel Investigation.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1320. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1320
• Norton, William J. 1990a. Structures Flight Test Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada257262
• Norton, William J. 1990b. Volume III. Systems Phase, Chapter 10A: Structures Flight Test Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada320029
• “Nozzle Plume Effects on Sonic Boom Using the Gulfstream Study Vehicle Design.” 2013. Journal of Purdue Undergraduate Research 3 (1). https://doi.org/10.5703/1288284315158
• Nugent, Jack. 1954. Lift and Drag Characteristics of the Douglas D-558-II Research Airplane Obtained in Exploratory Flights to a Mach Number of 2.0. NACA-RM-L54F03. NASA. https://ntrs.nasa.gov/citations/19930088200
• Nugent, Jack, and Odis C. Pendergraft Jr. 1987. Comparison of Wind Tunnel and Flight Test Afterbody and Nozzle Pressures for a Twin-Jet Fighter Aircraft at Transonic Speeds. NASA-TP-2588. NASA. https://ntrs.nasa.gov/citations/19880001383
• Nugent, J., T. J. Plant, R. A. Davis, and N. V. Taillon. 1983. Pressures Measured in Flight on the Aft Fuselage and External Nozzle of a Twin-Jet Fighter. NASA-TP-2017. NASA. https://ntrs.nasa.gov/citations/19830017394
• Nugent, Joshua P., and Timothy T. Takahashi. 2026. “High-Speed Aircraft Controllability Due to High-Altitude Atmospheric Turbulence – a History.” In AIAA AVIATION 2026 Forum. AIAA 2026-4581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4581
• Nugroho, Larasmoyo, Rika Andiarti, Rini Akmeliawati, and Sastra Kusuma Wijaya. 2024. “Enhancing the Landing Guidance of a Reusable Launch Vehicle by Improving Genetic Algorithm-Based Deep Reinforcement Learning Using Hybrid Deterministic-Stochastic Algorithm.” PLOS ONE 19 (2): e0292539. https://doi.org/10.1371/journal.pone.0292539
• Numata, Daiju, Takaaki Tsuchiya, and Keisuke Asai. 2013. “Evaluation of Free-Stream Turbulence Intensity in the Mars Wind Tunnel under Low Reynolds Number Conditions.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-1023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1023
• “Numerical Calculation of Gaseous Transport Properties from the Hulburt-Hirschfelder Potential with Applications to Planetary Entry Thermal Protection.” 1982. In Thermophysics of Atmospheric Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865565.0003.0016
• “Numerical Optimization on Approach and Landing for Reusable Launch Vehicle.” 2016. International Journal of Science and Research (IJSR) 5 (6): 1279–83. https://doi.org/10.21275/v5i6.nov164465
• O’Callaghan, John J. 2013. “The Gulfstream G650 Flight Test Accident: Lessons Learned.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-5085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5085
• O’Donnell, Richard S., and Kamran Mohseni. 2018. “Aerodynamic Parameter Estimation from Wind Tunnel Testing of a Small UAS.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0294
• Obara, Clifford J. 1986. “Boundary Layer Flow Visualization for Flight Testing.” In NASA, Langley Research Center, Laminar Flow Aircraft Certification. https://ntrs.nasa.gov/citations/19880014358
• Obara, C., E. Hastings, J. Schoenster, T. Parrott, and B. Holmes. 1986. “Natural Laminar Flow Flight Experiments on a Turbine Engine Nacelle Fairing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9756
• Obara, C. J., and B. J. Holmes. 1985. Flight-Measured Laminar Boundary-Layer Transition Phenomena Including Stability Theory Analysis. NASA-TP-2417. NASA. https://ntrs.nasa.gov/citations/19850012808
• Obara, Clifford J., Cynthia C. Lee, and Paul M. H. W. Vijgen. 1991. Analysis of Flight-Measured Boundary-Layer Stability and Transition Data. AIAA PAPER 91-3282. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910069240
• Obara, Clifford J., Paul M. H. W. Vijgen, Cynthia C. Lee, and Michael S. Wusk. 1990. Boundary-Layer Stability Analysis of Flight-Measured Transition Data. SAE PAPER 901809. Lockheed Engineering and Sciences Co. https://ntrs.nasa.gov/citations/19910063919
• Obermark, Jeff. 2004. Verification of Simulation Results Using Scale Model Flight Test Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ada422954
• Oblique Wing Aircraft. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch10
• Obradovic, Borna, and Kamesh Subbarao. 2010. “Modeling of Dynamic Loading of Morphing Wing Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8236
• Obradovic, Borna, and Kamesh Subbarao. 2012. Modeling and Simulation of Morphing Wing Aircraft. Wiley. https://doi.org/10.1002/9781119964032.ch5
• Oelker, Hans-Christoph, and Holger Friehmelt. 1998. “Aerodynamic System Identification of Nonlinear Rudder Characteristics Based on Flight Test Data.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4263
• Ogawa, Shinichiro. 2023. “Dynamic Mode Decomposition of the Combustion Flow Field in a Scramjet Combustor with a Cavity Flameholder.” In AIAA AVIATION 2023 Forum. AIAA 2023-3787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3787
• Ogawa, S. 2024. “Mechanisms of Ignition and Combustion Instability in a Scramjet Combustor with Micro-Rocket Torch Using Dynamic Mode Decomposition.” Physics of Fluids 36 (10): 106123. https://doi.org/10.1063/5.0228287
• Ogawa, Hideaki, and Holger Babinsky. 2005. “Evaluation of Wave Drag Reduction by Flow Control.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-1415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1415
• Ogburn, Marilyn E., John V. Foster, and Keith D. Hoffler. 2005. “Application of Piloted Simulation to High-Angle-of-Attack Flight-Dynamics Research for Fighter Aircraft.” In AGARD FMP Symposium on Piloted Effectiveness. https://ntrs.nasa.gov/citations/20050041980
• Ogren, Harvey, Donald Sotanski, and LeRoy Genaw. 1974. Yaw Axis Stability Augmentation System Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ad0784134
• Ohta, H., P. Nikiforuk, and M. Gupta. 1984. “Control Law Synthesis for Active Flutter Suppression Based on the Modal Cost Analysis.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1931. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1931
• Oishi, Tomo, Sergey Gorbunov, Johnny Fu, and Ed Martinez. 2006. “Thermal Sensor Development and Testing for NASA Entry Probe Thermal Protection Systems.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-1247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-1247
• Okninski, Adam, Jan Kindracki, and Piotr Wolanski. 2016. “Rocket Rotating Detonation Engine Flight Demonstrator.” Aircraft Engineering and Aerospace Technology 88 (4): 480–91. https://doi.org/10.1108/aeat-07-2014-0106
• Okojie, Robert, Paul Danehy, Jay Grinstead, A. Watkins, and A. Mielke. 2009. “An Overview of NASA Hypersonic Experimental Diagnostic and Instrumentation Technologies for Ground and Flight Testing.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7279
• Okuhara, Mika, Torleiv H. Bryne, Kristoffer Gryte, and Tor Arne Johansen. 2022. “Phased Array Radio Navigation System on UAVs: In-Flight Calibration.” Preprint, TechRxiv. https://doi.org/10.36227/techrxiv.21456615
• Olds, John, and Peter Bellini. 1998. “Argus, a Highly Reusable SSTO Rocket-Based Combined Cycle Launch Vehicle with Maglifter Launch Assist.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1557
• Olejnik, Aleksander, Stanisław Kachel, Robert Rogólski, and Jarosław Milczarczyk. 2019. “The Concept and Methodical Assumptions for the Development of Dynamically Scaled Aircraft Model (Passenger Aircraft).” MATEC Web of Conferences 304: 02010. https://doi.org/10.1051/matecconf/201930402010
• Oleskiw, Myron, Fred Hyde, and Paul Penna. 2001. “In-Flight Icing Simulation Capabilities of NRC’s Altitude Icing Wind Tunnel.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-94. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-94
• Olhausen, J. 1975. “The Use of a Navigation Platform for Performance Instrumentation on the YF-16 Flight Test Program.” In 13th Aerospace Sciences Meeting. AIAA 1975-32. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-32
• Oliveira, Rafael, Dino Sejdinovic, David Howard, and Edwin Bonilla. 2024. “Bayesian Adaptive Calibration and Optimal Design.” In Advances in Neural Information Processing Systems 37. Neural Information Processing Systems Foundation, Inc. (NeurIPS). https://doi.org/10.52202/079017-1800
• Olivon, Frédéric, Jean-Étienne Durand, Aurélien Genot, and Estelle Piot. 2024. “High-Frequency Acoustic Propagation in a Thermally Choked Low-Mach Dual-Mode Ramjet.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3114
• Olney, Candida D., Heather Hillebrandt, and Eric Y. Reichenbach. 2000. An Evaluation Technique for an F/A-18 Aircraft Loads Model Using F/A-18 Systems Research Aircraft Flight Data. NASA/TM-2000-209028. NASA. https://ntrs.nasa.gov/citations/20000079998
• Olson, Roland E., and Ralph P. Bielat. 1955. An Aerodynamic and Hydrodynamic Investigation of Two Multijet Water-Based Aircraft Having Low Transonic Drag Rise. NACA-RM-L55A11a. NASA. https://ntrs.nasa.gov/citations/19930088632
• Omran, Ashraf, Drew Landman, and Brett Newman. 2008. “Stability Derivative Modeling Based on Aircraft Flight Modes Using Design of Experiments.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2532
• Ongarato, J. 1968. “Subsonic Wind Tunnel Wall Interference Studies Conducted in the NAR Trisonic Wind Tunnel.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-360
• Onozeki, Yusuke, Shunpei Shimizu, Maximilien Berthet, and Yuichiro Aoki. 2026. “Combined Aerodynamic and Structural Study on Hypersonic Aircraft with Lightweight Morphing Wing from Takeoff to Cruise.” In AIAA SCITECH 2026 Forum. AIAA 2026-2468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2468
• Ooda, Iman Jabbar. 2022. “Numerical Investigation of Aerodynamic Characteristics of Supercritical RAE2822 Airfoil with Gurney Flap.” Journal of Engineering 28 (6): 1–14. https://doi.org/10.31026/j.eng.2022.06.01
• Ordaz, Irian, Karl Geiselhart, and James W. Fenbert. 2014. “Conceptual Design of Low-Boom Supersonic Aircraft with Flight Trim Requirement.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2141
• Ordaz, Irian, Mathias Wintzer, and Sriram K. Rallabhandi. 2015b. “Full-Carpet Design of a Low-Boom Demonstrator Concept.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2261
• Orefice, Francesco, Fabrizio Nicolosi, Pierluigi Della Vecchia, and Danilo Ciliberti. 2020. “Aircraft Conceptual Design of Commuter Aircraft Including Distributed Electric Propulsion.” In AIAA Aviation 2020 Forum. AIAA 2020-2627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2627
• Oremland, Joshua, Vishvas S. Suryakumar, Thomas W. Strganac, and Arun S. Mangalam. 2017. “Flutter Suppression of an Aeroelastic Wing Using Aerodynamic Observables, Leading-Edge, and Trailing-Edge Control Surfaces.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4354. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4354
• Orlik, Evgeniy, Ivan Fedioun, and Dmitry Davidenko. 2009. “Boundary Layer Transition on a Hypersonic Forebody: Experiments and Calculations.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7352
• Orlik-Ruckemann, K. 1982. “Aerodynamic Aspects of Aircraft Dynamics at High Angles of Attack /AGARD Lecture/.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1363. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1363
• Orlik-Ruckemann, K., and J. Laberge. 1981. “Dynamic Wind Tunnel Tests of the Simulated Shuttle External Tank Cable Trays.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1879
• Ort, David, and Jeffrey J. Dosch. 2019. “Influence of Mountiing on the Accuracy of Piezoelectric Pressure Measurements for Hypersonic Boundary Layer Transition.” In AIAA Scitech 2019 Forum. AIAA 2019-2292. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2292
• Oruganti, Sreevishnu, Lorenzo Capponi, Benjamin M. Ringel, et al. 2024. “High-Enthalpy Testing of Thermal Protection Materials in the Plasmatron X for Titan Atmospheric Entry.” In AIAA SCITECH 2024 Forum. AIAA 2024-0863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0863
• Osborne, Robert S. 1957. Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair TF-102A Airplane at Transonic Speeds, Coord. No. AF-120. NACA-RM-SL57E22. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028481
• Osses, Tomas. 2020. “Tuning Neural Network Models for Improved Prediction of Boundary Layer Transition.” In Spring Interns 2020 Exit Deliverable Presentations. https://ntrs.nasa.gov/citations/20205000994
• Oswald, W. Bailey. 1932. General Formulas and Charts for the Calculation of Airplane Performance. NACA-TR-408. California Institute of Technology. https://ntrs.nasa.gov/citations/19930091482
• Ouellette, Jeffrey A. 2017. “Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0019
• Ouellette, Jeffrey A., Matthew J. Boucher, and Peter Suh. 2023. “Using Distributed Fiber-Optic Strain Sensing to Estimate Generalized Modal Coordinates from Flight-Test Data.” In AIAA SCITECH 2023 Forum. AIAA 2023-2069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2069
• Ouellette, Jeffrey A., Mayuresh Patil, and Craig A. Woolsey. 2014. “Flight Testing of a Subscale Aeroservoelastic Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0032
• Ouyang, Yan, Su Jia, Yan Li, and Huisong Wu. 2026. “Active Flutter Suppression of a Nonlinear Wing Section with Morphing Control Surface.” Advances in Engineering Technology Research 17 (1): 1413. https://doi.org/10.56028/aetr.17.1.1413.2026
• Ouyang, Yan, Kaichun Zeng, Xiping Kou, Yingsong Gu, and Zhichun Yang. 2021b. “Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model.” Shock and Vibration 2021 (1): 5535192. https://doi.org/10.1155/2021/5535192
• Ouzts, Peter. 2008. “Mode Transition Design Considerations for an Airbreathing Combined-Cycle Hypersonic Vehicle.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2621
• Ouzts, Peter, Donald Soloway, Daniel Moerder, David Wolpert, and Jose Benavides. 2009. “The Role of Guidance, Navigation, and Control in Hypersonic Vehicle Multidisciplinary Design and Optimization.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7329
• Owen, F. Kevin. 1993. “Measurement of Hypersonic Flows.” In New Trends in Instrumentation for Hypersonic Research. Springer Netherlands. https://doi.org/10.1007/978-94-011-1828-6_30
• Owens, D. Bruce, Jay M. Brandon, Mark A. Croom, C. Michael Fremaux, Eugene H. Heim, and Dan D. Vicroy. 2006b. “Overview of Dynamic Test Techniques for Flight Dynamics Research at NASA LaRC (Invited).” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080009757
• Owens, Bruce, David Cox, and Eugene Morelli. 2006a. “Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER Project.” In 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2006-3306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3306
• Owens, L. R., and R. A. Wahls. 2001. Reynolds Number Effects on a Supersonic Transport at Subsonic High-Lift Conditions (Invited). AIAA Paper 2001-0911. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010010363
• Owens, L. R., R. A. Wahls, M. B. Elzey, and M. P. Hamner. 2002. “Reynolds Number Effects on the Stability and Control Characteristics of a Supersonic Transport.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20020023445
• Owens, Lewis R., Richard A. Wahls, and S. Melissa Rivers. 2005. Off-Design Reynolds Number Effects for a Supersonic Transport. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20080001722
• Ozawa, Kazuki, and Paul Bruce. 2025. “Generation of Streaks by Non-Uniform Surface Temperature Distributions for Hypersonic Boundary Layer Transition Control.” In AIAA SCITECH 2025 Forum. AIAA 2025-0262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0262
• Ozbek, Emre, Selcuk Ekici, and Tahir Hikmet Karakoç. 2024. “A Comprehensive Review of State-of-Art FishBAC – Fishbone Active Camber Morphing Wing Surfaces–: A Promising Morphing Method.” Aircraft Engineering and Aerospace Technology 96 (7): 983–93. https://doi.org/10.1108/aeat-04-2024-0096
• Ozger, Erol. 2007. “Aerodynamic Model Validation of Eurofighter Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6718. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6718
• Özger, E. 2012. “Parameter Estimation of Highly Unstable Aircraft Assuming Linear Errors.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4511. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4511
• Ozger, Erol. 2013. “Parameter Estimation of Highly Unstable Aircraft Assuming Nonlinear Errors.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4751
• Öznalbant, Zafer, and Mehmet Ş. Kavsaoğlu. 2018. “Flight Control and Flight Experiments of a Tilt-Propeller VTOL UAV.” Transactions of the Institute of Measurement and Control 40 (8): 2454–65. https://doi.org/10.1177/0142331218754618
• Ożóg, Rafał, Mariusz Jacewicz, and Robert Głębocki. 2020. “Use of Wind Tunnel Measurements Data in Cold Launched Missile Flight Simulations.” Pomiary Automatyka Robotyka 24 (1): 49–60. https://doi.org/10.14313/par_235/49
• Oztekin, Ezgi, and Jeremy Bain. 2024. “Numerical Investigation of VTOL Propeller Icing.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4452
• Pack, L., N. Schaeffler, C. Yao, and A. Seifert. 2002. “Active Control of Flow Separation from the Slat Shoulder of a Supercritical Airfoil.” In 1st Flow Control Conference. AIAA 2002-3156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3156
• Pack, LaTunia, Chung-Sheng Yao, and Avi Seifert. 2003. “Active Control of Flow Separation from the Flap of a Supercritical Airfoil.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-4005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4005
• Pack-Melton, LaTunia, Norman Schaeffler, and John Lin. 2007. “High-Lift System for a Supercritical Airfoil: Simplified by Active Flow Control.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-707. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-707
• Padua, Felipe A., and Marcus Vinicius Preisighe Viana. 2025. “Analysis of Lateral Stability Variations across the Flight Envelope Using Flight Test Data.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3459. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3459
• Pagano, Antonio. 2018. “Aerodynamic Analyses of Tiltrotor Morphing Blades.” In Morphing Wing Technologies. Elsevier. https://doi.org/10.1016/b978-0-08-100964-2.00025-3
• Page, N. 1975. “Atmospheric Refraction of Sonic Boom from Aircraft at Low Supersonicspeeds.” In 2nd Aeroacoustics Conference. AIAA 1975-547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-547
• Page, Juliet. 2017. “Sonic Boom Weather Analysis of the F-18 Low Boom Dive Maneuver.” Journal of the Acoustical Society of America 141 (5_Supplement): 3626–3626. https://doi.org/10.1121/1.4987791
• Page, Juliet A., Kathleen K. Hodgdon, Robert P. Hunte, et al. 2020. Quiet Supersonic Flights 2018 (QSF18) Test: Galveston, Texas Risk Reduction for Future Community Testing with a Low-Boom Flight Demonstration Vehicle. NASA/CR–2020-220589/Volume I. NASA. https://ntrs.nasa.gov/citations/20200003223
• Pahle, Joe, Dave Berger, Mike Venti, Chris Duggan, Jim Faber, and Kyle Cardinal. 2012. “An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4802
• Pahle, Joseph W., Bruce Powers, Victoria Regenie, Vince Chacon, Steve Degroote, and Steven Murnyak. 1991. “Research Flight-Control System Development for the F-18 High Alpha Research Vehicle.” In High-Angle-of-Attack Technology Conference. https://ntrs.nasa.gov/citations/19910012818
• Painter, W. 1983. “AD-1 Oblique Wing Research Aircraft Pilot Evaluation Program.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2509
• Painter, W., and R. Erickson. 1984. “Rotor Systems Research Aircraft Airplane Configuration Flight-Test Results.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2465
• Pak, Chan-gi. 2011. Unsteady Aerodynamic Model Tuning for Precise Flutter Prediction. NASA/TM-2011-215963. NASA. https://ntrs.nasa.gov/citations/20110023913
• Pak, Chan-Gi. 2017. “Jig-Shape Optimization of Quiet Supersonic Technology X-Plane.” In Fall 2017 Aerospace Flutter and Dynamics Council (AFDC) Meeting. https://ntrs.nasa.gov/citations/20170010191
• Pak, Chan-gi, and Christine V. Jutte. 2009. New Flutter Analysis Technique for CFD-Based Unsteady Aeroelasticity. DFRC-934. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090025456
• Pak, Chan-gi, and Shun-fat Lung. 2010. “Reduced Uncertainties in the Flutter Analysis of the Aerostructures Test Wing.” In 27th Congress of the International Council of the Aeronautical Sciences. https://ntrs.nasa.gov/citations/20100038447
• Pak, Chan-Gi, and Shun Fat Lung. 2011. Reduced Uncertainties in the Flutter Analysis of the Aerostructures Test Wing. NASA/TM-2011-216421. NASA. https://ntrs.nasa.gov/citations/20110011618
• Pak, Chan-Gi, and Shun-Fat Lung. 2017. “New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170000462
• Palchekovskaya, Natalia. 2019. “Aerodynamic Peculiarities of Flow over a Space Vehicle at Transonic and Supersonic Velocities.” International Journal of Fluid Mechanics Research 46 (3): 211–18. https://doi.org/10.1615/interjfluidmechres.2018025652
• Palitz, M. 1966. Measured and Calculated Flow Conditions on the Forward Fuselage of the X-15 Airplane and Model at Mach Numbers from 3.0 to 8.0. NASA-TN-D-3447. NASA. https://ntrs.nasa.gov/citations/19660017559
• Pallister, Keith, Jon Parker, and Brian Probert. 1992. “Comparison of Recent Results from Different Wind Tunnel Facilities along with Comparisons of Measured Flight Results and Wind Tunnel Based Predictions.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3985. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3985
• Palmer, Grant. 1990. “Enhanced Thermochemical Nonequilibrium Computations of Flow around the Aeroassist Flight Experiment Vehicle.” In 5th Joint Thermophysics and Heat Transfer Conference. AIAA 1990-1702. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1702
• Palmer, Grant E., Charles H. Campbell, and Karen T. Berger. 2013. “CFD Simulations of Boundary Layer Transition Flight Experiment Catalytic Coating Data.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140004906
• Palmer, Grant, Bill Henline, Dave Olynick, and Thomas A. Edwards. 1994. Heating Analysis of the Lockheed Lifting Body. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20010120095
• Palmer, Joshua, and Victor W. Sparrow. 2015. “Measured N-Wave Sonic Boom Events and Sensitivity in Sonic Boom Metrics.” In AIP Conference Proceedings, vol. 1685. AIP Publishing LLC. https://doi.org/10.1063/1.4934478
• Palomino, J. 2022. “2.4 from Automotive to Flight Test Instrumentation: Wiring Reduction Using New Ethernet Standard.” In Proceedings - ettc2022. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2022/2.4
• Palumbo, Nate, M. Jake Vachon, Dave Richwine, Tim Moes, and Gray Creech. 2003. Propulsion Flight-Test Fixture. DRC-02-23. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110023583
• Pamadi, Bandu, Gregory Brauckmann, Michael Ruth, and Henri Fuhrmann. 2000. “Aerodynamic Characteristics, Database Development and Flight Simulation of the X-34 Vehicle.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-900
• Pan, Lijun, Kun Mao, Jun Liu, et al. 2026. “Development and Flight Testing of Scaled Flight Demonstrators.” Journal of Physics: Conference Series 3207 (1): 012030. https://doi.org/10.1088/1742-6596/3207/1/012030
• Panayotov, Hristian, and Martin Zikyamov. 2026. “Common-Form Statistical Relations for Conceptual Sizing of Electric and Hybrid VTOL Unmanned Aircraft.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-10915692/v1
• Panchal, Jitesh H., Christiaan J. J. Paredis, Janet K. Allen, and Farrokh Mistree. 2007. “Managing Design Process Complexity: A Value-of-Information Based Approach for Scale and Decision Decoupling.” In Volume 6: 33rd Design Automation Conference, Parts A and B. ASMEDC. https://doi.org/10.1115/detc2007-35686
• Panchal, Jitesh H., Christiaan J. J. Paredis, Janet K. Allen, and Farrokh Mistree. 2009. “Managing Design-Process Complexity: A Value-of-Information Based Approach for Scale and Decision Decoupling.” Journal of Computing and Information Science in Engineering 9 (2): 021005. https://doi.org/10.1115/1.3130791
• Panda, J. n.d. “Comparison of Surface Pressure Fluctuations from Flight and Wind Tunnel Tests on the Orion Multi-Purpose Crew Vehicle.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20210024926
• Panda, Jayanta. 2022. “Comparison of Surface Pressure Fluctuations from Flight and Wind Tunnel Tests on the Orion Multi-Purpose Crew Vehicle.” In AIAA SCITECH 2022 Forum. AIAA 2022-2127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2127
• Pandey, Vijitashwa, and Jeffrey W. Herrmann. 2021. “Attribute-Wise Value of Information in Engineering Systems: A Simulation-Based Study.” In Volume 6: Design, Systems, and Complexity. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2021-69783
• Papa, Regina, and Janice Stoliker. 1988. “Pilot Workload Assessment: A Flight Test Approach.” In 4th Flight Test Conference. AIAA 1988-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2105
• Papathakis, Kurt VonderHaar. n.d. “Inlet Shape Considerations for Split-Wing Electric Distributed Propulsion.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2015.49
• Papathakis, Kurt V., Philip A. Burkhardt, David W. Ehmann, and Alaric M. Sessions. 2017. “Safety Considerations for Electric, Hybrid-Electric, and Turbo-Electric Distributed Propulsion Aircraft Testbeds.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-5032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-5032
• Paradiso, M. A. 1961. “The Navigation System for Supersonic Transport Aircraft.” Navigation 8 (2): 80–84. https://doi.org/10.1002/j.2161-4296.1961.tb02467.x
• Parameswaran, Y., and R. Y. Jategaonkar. 2004. “Calibration of 5-Hole Probe for Flow Angles from Advanced Technologies Testing Aircraft System Flight Data.” Defence Science Journal 54 (2): 111–23. https://doi.org/10.14429/dsj.54.2073
• Paredes, Pedro, and Meelan M. Choudhari. 2018. “Transition Delay via Vortex Generators in a Hypersonic Boundary Layer at Flight Conditions.” In 2018 Fluid Dynamics Conference. https://ntrs.nasa.gov/citations/20200002316
• Paredes, Pedro, Anton Scholten, Meelan M. Choudhari, and Fei Li. 2021. “Hypersonic Boundary-Layer Transition on Blunted Cones at Angle of Attack.” In AIAA Aviation 2021 Forum. AIAA 2021-2886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2886
• Paredes, Pedro, Balaji Venkatachari, Meelan M. Choudhari, et al. 2020. “Toward Transition Modeling in a Hypersonic Boundary Layer at Flight Conditions.” In AIAA SciTech Exhibition and Forum. https://ntrs.nasa.gov/citations/20200002932
• Parello, Romain. n.d. “Development of a New Overall Aircraft Design Method Adapted to Hydrogen Blended Wing Body.” PhD diss., Université de Toulouse (EPE ; 2025-…). https://doi.org/10.70675/552ef228z4a56z4305z8fa7z20a49691720d
• Parikh, Paresh, Walter Engelund, Sasan Armand, and Robert Bittner. 2004. Evaluation of a CFD Method for Aerodynamic Database Development Using the Hyper-X Stack Configuration. AIAA Paper 2004-5385. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040110351
• Paris, Alfonso, and Omeed Alaverdi. 1998. “Post-Flight Inertial and Air-Data Sensor Calibration.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4450
• Park, Chul. 2005. “Calculation of Stagnation-Point Heating Rates Associated with Stardust Vehicle.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-190. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-190
• Park, Michael A., and Melissa B. Carter. 2021. “Nearfield Summary and Analysis of the Third AIAA Sonic Boom Prediction Workshop C608 Low Boom Demonstrator.” In AIAA Scitech 2021 Forum. AIAA 2021-0345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0345
• Park, Kwang, Kwang Lee, Byoung Kim, and Jung Kang. 2001. “Estimation of Aircraft Lateral-Directional Aerodynamic Derivatives from Flying Quality Flight Test.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4014
• Parker, Thomas. 2022. A Novice’s Guide to Approximating the Material Stresses and System Requirements for Hypersonic Flight. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1180064
• Parks, E. K., and R. C. Wingrove. 1977. Flight-Test Measurements of Ground Effect: STOL Airplanes. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19780035524
• Parlier, C. 1983. “The Challenges of Maneuvering Flight Performance Testing in Modern Rotary Wing Aircraft.” In 2nd Flight Testing Conference. AIAA 1983-2739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2739
• Parlini, F. 1983. “Applications of Inertial Systems as Flight Test Sensors.” In 2nd Flight Testing Conference. AIAA 1983-2738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2738
• Parlini, F., and J. Combley. 1986. “Experience with Flight Testing Integrated Avionics Systems.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9804. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9804
• Pascioni, Kyle A., Austin D. Thai, and Jeremy J. Bain. 2026. Individual Propeller Source Noise Assessment from Full-Scale eVTOL Flight Test Measurements. Langley Research Center. https://ntrs.nasa.gov/citations/20260000259
• Patel, Vijay V., Girish Deodhare, and Shyam Chetty. 2023. “Accelerated Flight Envelope Expansion Using near Real Time Stability Margin Estimation.” Journal of Aerospace Sciences and Technologies: 274–86. https://doi.org/10.61653/joast.v58i4.2006.741
• Patil, Mayuresh, and Mayuresh Patil. 1997. “Aeroelastic Tailoring of Composite Box Beams.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-15. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-15
• Patrick, Chris. 2019. “Total Temperature Affects Hypersonic Boundary Layer Transition.” Scilight 2019 (47): 471107. https://doi.org/10.1063/10.0000281
• Pätzold, Andreas, Inken Peltzer, and Wolfgang Nitsche. 2013. “Sensors and Actuators for Laminar Flow Flight Experiments.” In Research Topics in Aerospace. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-34738-2_20
• Pausder, Heinz-Jürgen, Ulrich Butter, and Frank Steinmaier. 2000. “Safety Concept of Technology Demonstrator ACT/FHS.” In Proceedings of the Vertical Flight Society Forum 56 - Virginia Beach, VA 2000. The Vertical Flight Society. https://doi.org/10.4050/vfs-f56-00097
• Pavlock, Kate Maureen. 2013. Flight Test Engineering. DFRC-E-DAA-TN11035. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20140010192
• Pavlock, Kate Maureen, James L. Less, and David Nils Larson. 2011. Flight Test Approach to Adaptive Control Research. DFRC-E-DAA-TN4220. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110024034
• Pawlak, Robert Jon. 1968. “Future Aspects of Supersonic Transport Navigation.” Navigation 15 (2): 188–93. https://doi.org/10.1002/j.2161-4296.1968.tb01604.x
• Pawlak, Rex. 1994. “Real Time Display of Flight Test Data.” In Biennial Flight Test Conference. AIAA 1994-2116. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2116
• Paynter, Gerald C. 1988. “CFD Technology for Hypersonic Vehicle Design.” In Computational Structural Mechanics & Fluid Dynamics. Elsevier. https://doi.org/10.1016/b978-0-08-037197-9.50009-7
• Peach, I. L., Jr., J. S. Bull, D. J. Anderson, et al. 1980. NASA/FAA Flight-Test Investigation of Helicopter Microwave Landing System Approaches. AHS 80-55. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19810055776
• Pearson, E. 1986. “Tornado Avionic Flight Testing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9805
• Pearson, A. E. 1995. Aerodynamic Parameter Estimation via Fourier Modulating Function Techniques. NASA-CR-4654. NASA. https://ntrs.nasa.gov/citations/19950018210
• Pecora, Modesto, and Rosario Pecora. 2018. “Application of the Extra-Modes Method to the Aeroelastic Analysis of Morphing Wing Structures.” In Morphing Wing Technologies. Elsevier. https://doi.org/10.1016/b978-0-08-100964-2.00014-9
• Peebles, Curtis. 2006. The Road to Mach 10: A History of the X-43A Hypersonic Flight Test Program at NASA Dryden – Origins to First Flight. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070038171
• Peebles, Curtis. 2009. “Learning from Experience Case Studies of the Hyper-X Project.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090009758
• Peele, James R. 1953. Transonic Flight Measurement of the Aerodynamic Load on the Extended Slat of the Douglas D-558-II Research Airplane. NACA-RM-L53F29. NASA. https://ntrs.nasa.gov/citations/19930087819
• Peele, James R. 1954. Flight-Determined Pressure Measurements over the Wing of the Douglas D-558-II Research Airplane at Mach Numbers up to 1.14. NACA-RM-L54A07. NASA. https://ntrs.nasa.gov/citations/19930088105
• Pei, Jing, and Joh Wall. 2013. “Estimation of Aerodynamic Stability Derivatives for Space Launch System and Impact on Stability Margins.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4684. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4684
• Peigin, Sergey, and Boris Epstein. 2006. “CFD Driven Optimization of Blended Wing Body Aircraft.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3457
• Pellerito, Victoria R., Mallory Mott, Naomi Acosta, et al. 2024. “Flight Procedural Noise Assessment of a Blended Wing Body Aircraft with Variable Engine Thrust.” In AIAA SCITECH 2024 Forum. AIAA 2024-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2105
• Peloubet, R., Jr., R. Haller, and R. Bolding. 1983. “Recent Developments in the F-16 Flutter Suppression with Active Control Program.” In 24th Structures, Structural Dynamics and Materials Conference. AIAA 1983-995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-995
• Pelykh, Valentyn, and Volodymyr Andryushchenko. 2024. “Determination of the Features of Integrated Design of Civil Long-Range Aircraft with Transonic Truss-Braced Wing at the Preliminary Design Stage.” Technology audit and production reserves 1 (1(75)): 35–42. https://doi.org/10.15587/2706-5448.2024.298600
• Pena, Francisco, Benjamin Martins, and W. Lance Richards. 2018. “Adaptive Load Control of Flexible Aircraft Wings Using Fiber Optic Sensing.” In Optical Society of America. https://ntrs.nasa.gov/citations/20190033242
• Pendleton, L. 1965. “Survey of Polaris Shock and Vibration Flight Test Program.” In Flight Testing Conference. AIAA 1965-223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-223
• Pendleton, Ed, Denis Bessette, Pete Field, Gerry Miller, and Kenneth Griffin. 1998. “The Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development.” In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1998-1972. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1972
• Pendleton, Ed, Peter Flick, Donald Paul, Dave Voracek, Eric Reichenbach, and Ken Griffin. 2007. “The X-53 a Summary of the Active Aeroelastic Wing Flight Research Program.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-1855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1855
• Pendleton, Ed, Kenneth Griffin, Michael Kehoe, and Boyd Perry. 1996. “A Flight Research Program for Active Aeroelastic Wing Technology.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1574
• Pendley, Robert E. 1947. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Air-Stream Fluctuations at the Tail of the D-558-1 Airplane. NACA-RM-L7A15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019291
• Peng, Jie, and Cunxian Wang. 2026. “Prediction and Control Method of Boundary Layer Transition for Hypersonic Vehicles Based on Non-Equilibrium Thermodynamic Model.” Journal of Physics: Conference Series 3256 (1): 012063. https://doi.org/10.1088/1742-6596/3256/1/012063
• Penland, Jim A., and David E. Fetterman Jr. 1958. High-Speed Static Stability Characteristics of the X-15 Airplane. NASA. https://ntrs.nasa.gov/citations/19930092382
• Penland, J., and D. Romeo. 1971b. “Advances in Hypersonic Extrapolation Capability: Wind Tunnel to Flight.” In 9th Aerospace Sciences Meeting. AIAA 1971-132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-132
• Perera, Melanie, and Shijun Guo. 2008. “Structural and Aeroelastic Tailoring of a Seamless Aeroelastic Wing.” In 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2008-5969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-5969
• Perez, Guillermo. n.d. “Finite-Rate Chemistry Effects upon Convective and Radiative Heating of an Atmospheric Entry Vehicle.” PhD diss., Louisiana State University and Agricultural & Mechanical College. https://doi.org/10.31390/gradschool_disstheses.2754
• Pérez Rus, C., and S. Le Gal. 2024. “B3.2: Flight Test Instrumentation System: Tailoring MBSE Methodologies for Prototype Aerial Systems Development.” In ETTC 2024. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2024/b3.2
• Perez-Rivera, Kassandra. 2026. “Flight Test Preparation of an Ultra-Low Ballistic Coefficient Entry Vehicle.” In 2026 Regional Student Conferences. AIAA 2026-114907. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-114907
• Perini, L. 1972. Compilation and Correlation of Experimental, Hypersonic, Stagnation Point Convective Heating Rates. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4286219
• Perkins, Edward W., and Leland H. Jorgensen. 1956. Comparison of Experimental and Theoretical Normal-Force Distributions (Including Reynolds Number Effects) on an Ogive-Cylinder Body at Mach Number 1.98. NACA-TN-3716. NASA. https://ntrs.nasa.gov/citations/19930084497
• Perkins, Cody L., Zhi Yang, Dimitri J. Mavriplis, James G. Coder, Lawton Shoemake, and Christopher J. Axten. 2023. “Effect of Transition Modeling for Analysis of a Slotted, Natural-Laminar-Flow Transonic Truss-Braced Wing Aircraft Configuration.” In AIAA SCITECH 2023 Forum. AIAA 2023-2454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2454
• Perkins, Cody L., Zhi Yang, Ilker Topcuoglu, et al. 2022. “Coupled Analysis of a Slotted Natural-Laminar-Flow Transonic Truss-Braced Wing Aircraft Configuration.” In AIAA SCITECH 2022 Forum. AIAA 2022-2536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2536
• Perlini, Alberto, Mattia G. Bertolini, and Giulio Gori. 2026. “A Multi-Fidelity Bayesian Optimization Framework for Hypersonic Vehicle Design.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5058
• Perraud, Jean, Geza Schrauf, Itham Archambaud, et al. 2010. “Transonic High Reynolds Number Transition Experiments in the ETW Cryogenic Wind Tunnel.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1300. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1300
• Perrin, E. F. 1956. “High Speed Flight Planning*,.” Navigation 5 (1): 6–17. https://doi.org/10.1002/j.2161-4296.1956.tb01567.x
• Perry, Aaron T., Timothy Bretl, and Phillip J. Ansell. 2019. “System Identification and Dynamics Modeling of a Distributed Electric Propulsion Aircraft.” In AIAA Aviation 2019 Forum. AIAA 2019-3086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3086
• Perry, B., III. 1984. “Flight Test Technique for Evaluation of Gust Load Alleviation Analysis Methodology.” In Aeroservoelasticity Tech. Spec. Meeting. https://ntrs.nasa.gov/citations/19850006524
• Pestana, Mark. 2010. NASA Dryden Flight Research Center: Unmanned Aircraft Operations. DFRC-E-DAA-TN2386. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110008311
• Peter, Fabian, and Eike Stumpf. 2018. “The Development of Morphing Aircraft Benefit Assessment.” In Morphing Wing Technologies. Elsevier. https://doi.org/10.1016/b978-0-08-100964-2.00003-4
• Peters, W. 1985. “A Simulation Technique for Jet Temperature Effects on Nozzle-Afterbody Drag at Transonic Mach Numbers.” In 21st Joint Propulsion Conference. AIAA 1985-1463. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1463
• Petersen, K. 1981. “Flight Experience with a Remotely Augmented Vehicle Flight Test Technique.” In 1st Flight Test Conference. AIAA 1981-2417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2417
• Petersen, Shane, Jay Fantini, Ken Norlin, John Theisen, and Steven Krasiewski. 2004. Development and Testing of the Phase 0 Autonomous Formation Flight Research System. NASA/TM-2004-212040. NASA. https://ntrs.nasa.gov/citations/20040021341
• Peterson, J. H. 1982b. “Wind-Tunnel/flight-Drag Correlation.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017323
• Peterson, Tim, and Peter Grant. 2011. “Handling Qualities of a Blended Wing Body Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6542
• Peterson, J. B., Jr. 1982a. “Wind-Tunnel/flight Correlation Program on XB-70-1.” In Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017325
• Petley, Dennis, Stuart Jones, and William Dziedzic. 1991. “Analysis of Cooling Systems for Hypersonic Aircraft.” In 3rd International Aerospace Planes Conference. AIAA 1991-5063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-5063
• Peyada, Naba, and Ajoy Ghosh. 2009. “Aircraft Parameter Estimation Using Neural Network Based Algorithm.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5941
• Pfeiff, Robert. 1965. “X-22A Flight Test Program.” In Proceedings of the 1st National Symposium on V/STOL Aircraft, Subsystem Design and Testing and Operation - Ohio 1965. The Vertical Flight Society. https://doi.org/10.4050/sm_vstol_1965-5003
• Pfenneberger, F. 1966. “Experimental Control-Wing Hinge Moments of a Transonic-Supersonic, Rolling, Maneuvering, Guided Missile.” In 2nd Aerodynamic Testing Conference. AIAA 1966-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-755
• Pfenninger, W., and J. W. Bacon. 1961. “About the Development of Swept Laminar Suction Wings with Full Chord Laminar Flow.” In Boundary Layer and Flow Control. Elsevier. https://doi.org/10.1016/b978-1-4832-1323-1.50016-6
• Pfenninger, Werner, and Chandra S. Vemuru. 1992. “Design Philosophy of Long Range LFC Transports with Advanced Supercritical LFC Airfoils.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_5
• Pfifer, Harald, and Brian P. Danowsky. 2016. “System Identification of a Small Flexible Aircraft: Invited.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1750
• Philbrick, J. 1975. “Douglas Experience in Flight Flutter Testing.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003024
• Phillips, Kerri B. n.d. “Aircraft Parameter Identification for Application within a Fault-Tolerant Flight Control System.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.3049
• Phillips, William H. 1942. Comparison of Aileron Control Characteristics as Determined in Flight Tests of P-36, P-40, Spitfire, and Hurricane Pursuit Airplanes. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20150015694
• Phillips, William H. 1948. Effect of Steady Rolling on Longitudinal and Directional Stability. NACA-TN-1627. NASA. https://ntrs.nasa.gov/citations/19930082293
• Phillips, W., H. Compton, and J. Findlay. 1983. “Base Drag Determination for STS Flights 1-5.” In 2nd Flight Testing Conference. AIAA 1983-2719. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2719
• Phillips, Ben D., and Drew Landman. 2016. “Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing.” In AIAA Flight Testing Conference. AIAA 2016-3978. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3978
• Phillips, Pamela, and Edgar Waggoner. 1988. “A Transonic Wind Tunnel Wall Interference Prediction Code.” In 6th Applied Aerodynamics Conference. AIAA 1988-2538. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2538
• Phillips, Ben D., and Thomas K. West. 2017. “Trim Flight Conditions for a Low-Boom Aircraft Design under Uncertainty.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3047. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3047
• Piatak, David, Martin Sekula, and Russ Rausch. 2011. “Comparison of Ares I-X Wind-Tunnel Derived Buffet Environment with Flight Data.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3013
• Picard, Mary, and Scott Whitley. 2002. F/A-18A/B/C/D F404-GE-400/402 Engine Slotted Spraybar Inlet Flameholder Follow-On Flight Test Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada407860
• Picasso III, Downs Bartholomew D., Buckanin Gary T., Ottomeyer Robert M., and John D. 1982. Airworthiness and Flight Characteristics Test. Part 2. YAH-64 Advanced Attack Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ada125270
• Pidvysotskyi, Valentyn. 2021. “The Concept of an Inflatable Reusable Launch Vehicle.” Preprint, . https://doi.org/10.31224/osf.io/xbf8z
• Pieper, Carl W. 1965. Engine and Whirl Tests, XV-9A Hot Cycle Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0613339
• Pieper, Kyle C., Aaron T. Perry, Phillip J. Ansell, and Timothy Bretl. 2018. “Design and Development of a Dynamically Scaled Distributed Electric Propulsion Aircraft Testbed.” In 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. AIAA 2018-4996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4996
• Pierce, G., and W. White Jr. 1972. “Unsteady Rotor Aerodynamics at Low Inflow and Its Effect on Flutter.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-959. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-959
• Pierpont, P. K. 1957. A Note on the Ability to Predict Transonic Drag-Rise Changes Due to Model Modifications. NACA-RM-L57H07. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19660024789
• Pierpont, P. K. 1959. Transonic Wind-Tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane. NASA-MEMO-12-14-58L. NASA. https://ntrs.nasa.gov/citations/19660024792
• Pierson, W., and C. Unger. 1982. “Flight Control Stability and Trim Analysis Techniques.” In Guidance and Control Conference. AIAA 1982-1603. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1603
• Pietersen, O. 1986. “RASP: A System Generating Very Accurate Position Markers during Flight Testing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9802
• Pilyugin, N. N., R. F. Talipov, and S. V. Utyuzhnikov. 1994. “On the Applicability of Some Approximate Similitude Laws in Hypersonic Aerodynamics.” Fluid Dynamics 29 (2): 251–57. https://doi.org/10.1007/bf02324316
• Pinkelman, J., S. Batill, and M. Kehoe. 1995. “An Investigation of the Total Least-Squares Criteria in Time Domain Based, Parameter Identification for Flight Flutter Testing.” In 36th Structures, Structural Dynamics and Materials Conference. AIAA 1995-1247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1247
• Pinna, F., and P. Rambaud. 2013. “Effects of Shock on Hypersonic Boundary Layer Stability.” In Progress in Flight Physics, edited by P. Reijasse, D. Knight, M. Ivanov, I. Lipatov. EDP Sciences. https://doi.org/10.1051/eucass/201305093
• Piotrowski, M. G. H., and D. W. Zingg. 2023. “Compressibility Corrections to Extend a Smooth Local Correlation-Based Transition Model to Transonic Flows.” Aeronautical Journal 127 (1313): 1141–70. https://doi.org/10.1017/aer.2022.105
• Pipko, I. D. 1966. Supersonic Passenger Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0646293
• Pitt, Dale. 2004. “Static and Dynamic Aeroelastic Analysis of Structural Wing Fold Hinges That Are Employed as an Aeroelastic Tailoring Tool.” In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. AIAA 2004-1754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1754
• Pitts, W., and M. Murbach. 1982. “Flight Measurements of Tile Gap Heating on the Space Shuttle.” In 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference. AIAA 1982-840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-840
• Pittsburgh Univ Washington DC Research Staff. 1966. Research Aircraft, XV-5A. Defense Technical Information Center. https://doi.org/10.21236/ad0482131
• “Placement in Flight Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.015
• Plaetschke, E., and S. Weiss. 1988. “Aircraft System Identification — Determination of Flight Mechanics Parameters.” In Application of System Identification in Engineering. Springer Vienna. https://doi.org/10.1007/978-3-7091-2628-8_11
• Planeaux, James. 1991. “Thrust Contributions to the Spin Characteristics of a Model Fighter Aircraft.” In 18th Atmospheric Flight Mechanics Conference. AIAA 1991-2887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2887
• Plant, T. J., J. Nugent, and R. A. Davis. 1980. “Flight-Measured Effects of Boattail Angle and Mach Number on the Nozzle Afterbody Flow of a Twin-Jet Fighter.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800038839
• Platou, A. 1968. “The Wind Tunnel Free Flight Testing Technique.” In 3rd Aerodynamics Testing Conference. AIAA 1968-388. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-388
• Platus, D. 1980. “Roll Resonance Control of Angle of Attack for Reentry Vehicle Drag Modulation.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1574
• Platz, Stewart, and Elias Bounajem. 1992. “Methodology for the Critical Evaluation of Flight Test Data.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4071
• Plotkin, Kenneth. 1989. “Review of Sonic Boom Theory.” In 12th Aeroacoustic Conference. AIAA 1989-1105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1105
• Plotkin, Kenneth. 1990. “Sonic Boom Focal Zones Due to Tactical Aircraft Maneuvers.” In 13th Aeroacoustics Conference. AIAA 1990-4003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-4003
• Plotkin, Kenneth J. 2006. “Low-Amplitude Sonic Boom from a Descending Sounding Rocket.” In AIP Conference Proceedings, vol. 838. AIP. https://doi.org/10.1063/1.2210428
• Plotkin, K., and J. Cantril. 1976. “Prediction of Sonic Boom at a Focus.” In 14th Aerospace Sciences Meeting. AIAA 1976-2. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-2
• Plotkin, Kenneth, and Domenic Maglieri. 2013. “SCAMP: Experimental Design of a Sonic Boom Focus Flight Test.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-931. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-931
• Plotkin, Kenneth, Roy Martin, Domenic Maglieri, Edward Haering, and James Murray. 2005. “Pushover Focus Booms from the Shaped Sonic Boom Demonstrator.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-11. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-11
• Polhamus, Edward C., and Alexander D. Hammond. 1960. II. Aerodynamic Research Relative to Variable-Sweep Multimission Aircraft. Langley Research Center. https://ntrs.nasa.gov/citations/19670023743
• Polhamus, E. C., and T. A. Toll. 1981. “Research Related to Variable Sweep Aircraft Development.” In Meeting of the Air Force Historical Foundation. https://ntrs.nasa.gov/citations/19810016532
• Poll, D. I. A., and U. Schumann. 2024. “On the Conditions for Absolute Minimum Fuel Burn for Turbofan Powered, Civil Transport Aircraft and a Simple Model for Wave Drag.” Aeronautical Journal: 1–33. https://doi.org/10.1017/aer.2024.10
• Pollock, Luke, and Graham Wild. 2024. “Preliminary Design of a Thermally Morphing Hypersonic Vehicle Flap.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4139
• Polutchko, R. J. 1974. “Viking Entry Aerodynamics and Heating.” In Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11. https://ntrs.nasa.gov/citations/19750012311
• Polve, J. 1966. “The State of Ignorance of Flutter-Flight Testing.” In 3rd Annual Meeting. AIAA 1966-883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-883
• Pommier-Budinger, Valerie, Yannick Bury, Guilhem Michon, and Gael Napias. 2016. “In-Flight PIV for CROR Flight Test Demonstration.” In 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2016-3404. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3404
• Pool, A., and D. Bosman. 1974. AGARD Flight Test Instrumentation Series, Volume 1: Basic Principles of Flight Test Instrumentation Engineering. AGARD-AG-160-VOL-1. Advisory Group for Aerospace Research and Development. https://ntrs.nasa.gov/citations/19740017820
• Poomadath, Muhammed Shahan, and Rafic Ajaj. 2025. “Aeroelastic Tailoring of Hinged High Aspect Ratio Wing Using Tow-Steered Composites.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3472
• Popelka, David, David Lindsay, Tom Parham, Victor Berry, and Donald J. Baker. 1997. “Results of an Aeroelastic Tailoring Study for a Composite Tiltrotor Wing.” Journal of the American Helicopter Society 42 (2): 126–36. https://doi.org/10.4050/jahs.42.126
• Porter, Linda M. n.d. “High Enthalpy, Hypersonic Drag Measurements on Blunt Cones in an Impulse Facility.” PhD diss., The University of Queensland. https://doi.org/10.14264/1304176
• Porter, J. M. 1965. “Some Problems and Uses of Fuel Flow Measurement in Supersonic Aircraft.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50011-7
• Porter, B., and Z. Gu. 1991. “Design of Fast-Sampling Digital Controllers for Active Flutter Suppression.” In Navigation and Control Conference. AIAA 1991-2814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2814
• Porter, B., T. Merzougui, and Z. Gu. 1992a. “Design of Adaptive Fast-Sampling Digital Controllers for Active Flutter Suppression.” In Dynamics Specialists Conference. AIAA 1992-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2105
• Porter, B., T. Merzougui, and Z. Gu. 1992b. “Robustness Characteristics of Fast-Sampling Digital Controllers for Active Flutter Suppression.” In Dynamics Specialists Conference. AIAA 1992-2104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2104
• Porter, Kevin M., Jonathan Poggie, and Roger L. Kimmel. 2017. “Laminar and Turbulent Flow Calculations for the HIFiRE-5b Flight Test.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-3132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3132
• Portoni, Phillip, and Aaron T. Dufrene. 2023. “Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Ground-to-Flight Comparisons.” In AIAA SCITECH 2023 Forum. AIAA 2023-0683. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0683
• Posada, Daniel, and Claudia P. Moreno. 2019. “Ranger EX 757: A Flight Control Testbed for Future Flutter Analysis.” In AIAA Scitech 2019 Forum. AIAA 2019-1293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1293
• Post, Ethan A., Ian C. Dupzyk, Ashley M. Korzun, Artem A. Dyakonov, Rebekah L. Tanimoto, and Karl T. Edquist. 2011. “Supersonic Retropropulsion Flight Test Concepts.” In International Planetary Probe Workshop. https://ntrs.nasa.gov/citations/20150006769
• “The Post-War Sonic Boom.” 2013. In Electronic Music. Cambridge University Press. https://doi.org/10.1017/cbo9780511820540.004
• Potsawat, Boonjaipetch, Pramudita Satria Palar, Koji Shimoyama, and Shigeru Obayashi. 2019. “Multipoint Shape Optimization of Supersonic Waverider.” Proceedings of Design & Systems Conference 2019.29 (0): 1206. https://doi.org/10.1299/jsmedsd.2019.29.1206
• Potter, D. 1975. “MRCA Flight Flutter Testing.” In Aircraft Systems and Technology Meeting. AIAA 1975-1033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1033
• Potthast, A. J. 1980. “x-Wing Stability and Control Development and Wind Tunnel Demonstration Tests: Helicopter, Conversion and Fixed Wing Flight.” In Proceedings of the Vertical Flight Society Forum 36 - Washington, D.C. 1980. The Vertical Flight Society. https://doi.org/10.4050/vfs-f36-027
• Powell, Kenneth G., and Wei Shyy. 2013. Michigan/Air Force Research Laboratory (AFRL) Collaborative Center in Aeronautical Sciences (MACCAS). Defense Technical Information Center. https://doi.org/10.21236/ada594530
• “Powered Flight Performance.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.007
• Powers, B. G. 1972. Statistical Survey of XB-70 Airplane Responses and Control Usage with an Illustration of the Application to Handling Qualities Criteria. NASA-TN-D-6872. NASA. https://ntrs.nasa.gov/citations/19720019363
• Powers, B. G. 1978a. Analytical Study of Ride Smoothing Benefits of Control System Configurations Optimized for Pilot Handling Qualities. NASA-TP-1148. NASA. https://ntrs.nasa.gov/citations/19780010133
• Powers, S. G. 1978b. “Flight-Measured Pressure Characteristics of Aft-Facing Steps in Thick Boundary Layer Flow for Transonic and Supersonic Mach Numbers.” In YF-12 Experiments Symp., Vol. 1. https://ntrs.nasa.gov/citations/19780024120
• Powers, Sheryll. 1988. “Flight Tests of External Modifications Used to Reduce Blunt Base Drag.” In 6th Applied Aerodynamics Conference. AIAA 1988-2553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2553
• Powers, Sheryll Goecke. 1997. Women in Flight Research at NASA Dryden Flight Research Center from 1946 to 1995: Monographs in Aerospace History: Number 6. NASA-TM-112715. NASA. https://ntrs.nasa.gov/citations/19970018532
• Powers, Sheryll, Lannie Webb, Edward Friend, and William Lokos. 1992. “Flight Test Results from a Supercritical Mission Adaptive Wing with Smooth Variable Camber.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4101
• Powers, M., C. Zaretzky, and L. Myrabo. 1986. “Analysis of Beamed-Energy Ramjet/scramjet Performance.” In 22nd Joint Propulsion Conference. AIAA 1986-1761. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1761
• Praharaj, Sarat C., Carl D. Engel, and John D. Warmbrod. 1986a. Orbital Flight Test Shuttle External Tank Aerothermal Flight Evaluation, Volume 1. NASA-CR-179074. NASA. https://ntrs.nasa.gov/citations/19870011579
• Praharaj, Sarat C., Carl D. Engel, and John D. Warmbrod. 1986b. Orbital Flight Test Shuttle External Tank Aerothermal Flight Evaluation, Volume 2. NASA-CR-179075. NASA. https://ntrs.nasa.gov/citations/19870011581
• Praharaj, Sarat C., Carl D. Engel, and John D. Warmbrod. 1986c. Orbital Flight Test Shuttle External Tank Aerothermal Flight Evaluation, Volume 3. NASA-CR-179076. NASA. https://ntrs.nasa.gov/citations/19870011580
• Prajapati, Satish. 2026. “Self-Healing Porous Ultra-High Temperature Ceramics Enable Reusable Thermal Protection for Mars Atmospheric Entry.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9681901/v1
• Prandtl, L. 1928. Motion of Fluids with Very Little Viscosity. NACA-TM-452. NASA. https://ntrs.nasa.gov/citations/19930090813
• Prangle, Dennis, Sophie Harbisher, and Colin S. Gillespie. 2023. “Bayesian Experimental Design without Posterior Calculations: An Adversarial Approach.” Bayesian Analysis 18 (1): 133–63. https://doi.org/10.1214/22-ba1306
• Prasad, J. V. R., and Suraj Unnikrishnan. 2006. “Flight Evaluation of Reactionary Envelope Protection System for UAVs.” In Proceedings of the Vertical Flight Society Forum 62 - Phoenix, AZ 2006. The Vertical Flight Society. https://doi.org/10.4050/vfs-f62-094
• Pratt, David, and William Heiser. 1993. “Isolator-Combustor Interaction in a Dual-Mode Scramjet Engine.” In 31st Aerospace Sciences Meeting. AIAA 1993-358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-358
• Precup, Nathan, Marat Mor, and Eli Livne. 2015. “The Design, Construction, and Tests of a Concept Aeroelastic Wind Tunnel Model of a High-Lift Variable Camber Continuous Trailing Edge Flap (HL-VCCTEF) Wing Configuration.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1406
• Precup, Nathan, Marat Mor, and Eli Livne. 2018. “An Active Variable Camber Continuous Trailing Edge Flapped Wing Wind Tunnel Model for Aeroelastic ‘in-Flight’ Shape Optimization Tests.” In 2018 Multidisciplinary Analysis and Optimization Conference. AIAA 2018-3106. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3106
• “Prediction and Verification of Aerodynamic Drag, Part II: Wind-Tunnel/Flight Correlation of Lift, Drag, and Pitching Moment.” 1985. In Thrust and Drag: Its Prediction and Verification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865732.0173.0206
• Preisser, J., and D. Chestnutt. 1983. “Flight Effects on Fan Noise with Static and Wind Tunnel Comparisons.” In 8th Aeroacoustics Conference. AIAA 1983-678. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-678
• “Preliminary Design of the Thermal Protection System for Solar Probe.” 1983. In Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865626.0385.0415
• “A Preliminary Estimate of Airframe Cost Effectiveness in the 1980’s.” 1970. In Meeting on the Prospects for Improvement in Efficiency of Flight. AIAA 1970-870. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-870
• Preller, Dawid. n.d. “Multidisciplinary Design and Optimisation of a Pitch Trimmed Hypersonic Airbreathing Accelerating Vehicle.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2018.437
• Preller, Dawid, and Michael Smart. 2012. “Design of a Minimum Trim Hypersonic Airbreathing Accelerator Vehicle.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5825. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5825
• Prescott, Ford L. 1963. “Wave Drag of an Axisymmetric Body.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/630092
• Price, G. 1964. “Factors Affecting Design Requirements of Armed Tactical Support V/stol Aircraft.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-772
• Price, Earl A. 1978. A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ada050891
• Price, S., and B. Lee. 1992. “Development and Analysis of Flight Flutter Prediction Methods.” In Dynamics Specialists Conference. AIAA 1992-2101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2101
• Price, E., Jr. 1981. “Interference Effects of Downstream Support Hardware on Throttle-Dependent Drag at Transonic Mach Numbers.” In 17th Joint Propulsion Conference. AIAA 1981-1493. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1493
• Prichard, D. S., and L. N. Sankar. 1988. “Improvements to Transonic Flowfield Calculations.” In Proceedings of the Vertical Flight Society Forum 44 - Washington, D.C. 1988. The Vertical Flight Society. https://doi.org/10.4050/vfs-f44-066
• Prilliman, F., and H. Francis. 1980. “Aerodynamic and Flight Characteristics of the Air-Launched Low Volume Ramjet /ALVRJ/ Vehicles.” In 18th Aerospace Sciences Meeting. AIAA 1980-375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-375
• “Principles of Hypersonic Test Facility Development.” 2002. In Advanced Hypersonic Test Facilities. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866678.0017.0027
• Progress of the X-15 Research Airplane Program. 1965. NASA-SP-90. NASA. https://ntrs.nasa.gov/citations/19730062061
• “Properties and Design of Slender Aircraft for Supersonic Flight.” 2012. In The Aerodynamic Design of Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600869228.0338.0438
• “Propulsion Systems from Takeoff to High-Speed Flight.” 1991. In High-Speed Flight Propulsion Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866104.0021.0100
• Prosvirin, D. A., and V. P. Kharchenko. 2016. “Improvement of “Aircraft-Automatic Flight Control System” Control Loop Quality.” Electronics and Control Systems 1 (47). https://doi.org/10.18372/1990-5548.47.10265
• Protz, Alison, and Mindy Nettles. 2015. Thermal Protection System Application to Composite Cryotank Technology Demonstrator. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20160008019
• Pruett, C., H. Wolf, M. Heck, and P. Siemers III. 1981. “An Innovative Air Data System for the Space Shuttle Orbiter: Data Analysis Techniques.” In 1st Flight Test Conference. AIAA 1981-2455. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2455
• Pruitt, D., and L. Bates. 1992. “Starting and Test Rhombus Characteristics of Two-Dimensional Supersonic Free-Jet Nozzle/generic Supersonic Aircraft Inlet Configurations.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5091
• Pruyn, Richard, and Robert Taylor. 1970. “Design Considerations for Tilt-Rotor VTOL Aircraft to Minimize the Effects of the Recirculating Downwash Environment.” In Proceedings of the Specialists Meeting on Environmental Effects on VTOL Designs - Arlington, Texas 1970. The Vertical Flight Society. https://doi.org/10.4050/sm_env_1970-2300
• Pugh, Thomas. 1992. “The U-2A Flight Test Program.” In Aerospace Design Conference. AIAA 1992-1086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1086
• Pugsley, Alfred. 1987. “The History of the Aeronautical Research Council; a Personal View.” Aeronautical Journal 91 (908): 343–49. https://doi.org/10.1017/s0001924000021527
• Purcell, Madison V., Alexander M. Wicklund, and Nigam Vadecha. 2025. “Reusable Launch Vehicles: Designing Legs for Propulsive Rocket Landing.” In AIAA SCITECH 2025 Forum. AIAA 2025-0202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0202
• Pursel, R. 1977. “Integration, Installation, and Flight Test of a Fail Passive Digitalautomatic Flight Control System in a Jet Transport Aircraft.” In Computers in Aerospace Conference. AIAA 1977-1514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1514
• Pusztai, Daniel, Mark H. Lowenberg, and Simon A. Neild. 2024. “Flight Testing of a Dynamically Scaled Transport Aircraft Model for High-Alpha Wind Tunnel Data Validation.” In AIAA SCITECH 2024 Forum. AIAA 2024-1497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1497
• Puthisikamani, K., N. Sreenivasaraja, S. Balasundaram, and S. R. Arun. 2023. “Design and Analysis of Wing Tip Twist on a Forward Swept Wing Using Prandtl-d Wing Concept.” Journal of Aerospace Sciences and Technologies: 287–93. https://doi.org/10.61653/joast.v74i4.2022.47
• Putman, William F. 1961. Results of Experiments on a Tilt-Wing VTOL Aircraft Using the Princeton University Forward Flight Facility. Defense Technical Information Center. https://doi.org/10.21236/ad0270217
• Putnam, T. 1983. “X-29 Flight Research Program.” In 2nd Flight Testing Conference. AIAA 1983-2687. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2687
• Putnam, T. W. 1984a. “Digital Electronic Engine Control History.” In Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane. https://ntrs.nasa.gov/citations/19860015873
• Putnam, T. W. 1984b. “The X-29 Flight-Research Program.” AIAA Student Journal 22. https://ntrs.nasa.gov/citations/19850031744
• Putnam, Terrill W., and Theodore G. Ayers. 1988. Flight Research and Testing. NASA-TM-100439. NASA. https://ntrs.nasa.gov/citations/19880016977
• Putnam, Terrill W., and Theodore G. Ayers. 1989. “Flight Research and Testing.” In NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1. https://ntrs.nasa.gov/citations/19890011556
• Putnam, Zachary R., and Robert D. Braun. 2016. “Review and Assessment of the Steep Lifting Entry Closed-Form Trajectory Solution.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-0278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0278
• Putnam, Jacob, and Justin Littell. 2020. “Crashworthiness of a Lift Plus Cruise eVTOL Vehicle Design within Dynamic Loading Environments.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16258
• Pyle, J. S. 1971. Lift and Drag Characteristics of the HL-10 Lifting Body during Subsonic Gliding Flight. NASA-TN-D-6263. NASA. https://ntrs.nasa.gov/citations/19710009392
• Pyle, Jon S., and Lawrence G. Ash. 1970. “Performance Characteristics of the Lifting Body Vehicle.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000631
• Pyle, J. S., and L. L. Steers. 1975. Flight Determined Lift and Drag Characteristics of an F-8 Airplane Modified with a Supercritical Wing with Comparison to Wind-Tunnel Results. NASA-TM-X-3250. NASA. https://ntrs.nasa.gov/citations/19790024988
• Qaumi, Taruansh Singh. 2021. “Aerodynamic Optimization of the Von Karman Nose Cone for a Supersonic Sounding Rocket.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14635638
• Qiang, Y., H. Sobieczky, and Th. Eggers. 2000. “Waverider Design with Parametric Flow Quality Control by Inverse Method of Characteristics.” In Inverse Problems in Engineering Mechanics II. Elsevier. https://doi.org/10.1016/b978-008043693-7/50113-6
• Qin, Ning. 2012. “Drag Reduction for Transonic Wings Combining Reduced Wing Sweep with Shock Control.” In 28th International Symposium on Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-25688-2_7
• Quackenbush, Todd R. 1983. “Testing of a Stall Flutter Suppression System for Helicopter Rotors Using Individual-Blade-Control.” In Proceedings of the Vertical Flight Society Forum 39 - St. Louis, MO 1983. The Vertical Flight Society. https://doi.org/10.4050/vfs-f39-611
• Quadrio, Maurizio, Alessandro Chiarini, Jacopo Banchetti, Davide Gatti, Antonio Memmolo, and Sergio Pirozzoli. 2022. “Drag Reduction on a Transonic Airfoil.” Journal of Fluid Mechanics 942: R2. https://doi.org/10.1017/jfm.2022.369
• Quast, A., R. Henke, and F. Muench. 1990. “Natural Laminar Flow: A Wind Tunnel Test Campaign and Comparison with Flight Test Data.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3045
• Queijo, M. J., W. R. Wells, and D. A. Keskar. 1979. Inclusion of Unsteady Aerodynamics in Longitudinal Parameter Estimation from Flight Data. NASA-TP-1536. NASA. https://ntrs.nasa.gov/citations/19800004740
• Quigley, H. C., and C. A. Holzhauser. 1974. “Requirement for Simulation in V/STOL Research Aircraft Programs.” In AGARD V/STOL Aerodyn.. https://ntrs.nasa.gov/citations/19750005748
• Quinlan, Jesse. n.d. “Flamelet/Progress Variable Modeling for a Dual-Mode Scramjet Combustor.” PhD diss., University of Virginia. https://doi.org/10.18130/v3g26m
• Quinn, W. W. 1986. “Multivariable Control of a Forward Swept Wing Aircraft.” PhD diss., Massachusetts Inst. of Tech.. https://ntrs.nasa.gov/citations/19860019481
• Quinn, P. 2022. “7.3 Optimizing PCM Bandwidth Usage in Flight Test by Real-Time Data Analysis during Flight.” In Proceedings - ettc2022. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf, Germany. https://doi.org/10.5162/ettc2022/7.3
• Quinn, Robert D., and Leslie Gong. 1990. Real-Time Aerodynamic Heating and Surface Temperature Calculations for Hypersonic Flight Simulation. NASA-TM-4222. NASA. https://ntrs.nasa.gov/citations/19900019499
• Quinn, Robert D., and Leslie Gong. 2000. A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft. NASA/TP-2000-209034. NASA. https://ntrs.nasa.gov/citations/20010002830
• Quitter, Julius W., Matthew Marino, and J. Michael Bauschat. 2021. “Comparison of Aerodynamic Methods for Flight Mechanical Derivative Estimation of Unconventional Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-0324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0324
• Qureshi, Z. H., and T. S. Ng. 1982. “Optimal Input Design for Dynamic System Parameter Estimation: The Ds-Optimality Case.” SIAM Journal on Control and Optimization 20 (5): 713–21. https://doi.org/10.1137/0320052
• Raab, Christian. 2014. “Rapid Aerodynamic Parameter Identification on a Large Transport Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0730
• Raab, Christian. 2026. “From Flight Test to a Simulator Model: System Identification of the ISTAR Research Aircraft.” In Materials Research Proceedings, vol. 69. Materials Research Forum LLC. https://doi.org/10.21741/9781644904251-262
• Rabourdin, Antoine, Oliver Dieterich, Peter Konstanzer, and Jean-Baptiste Maurice. 2014. “Blue Pulse: Active Rotor Control at Airbus Helicopters: New EC145 Demonstrator & Flight Test Results.” In Proceedings of the Vertical Flight Society 70th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0070-2014-9488
• “Radiation at Hypersonic Speeds.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0255.0280
• “Radiobiological Aspects of the Supersonic Transport.” 1966. Health Physics 12 (2): 209???226. https://doi.org/10.1097/00004032-196602000-00006
• Radotich, Michael. 2026. “TVF 2026: Foundations of Vertical Flight: NASA Rotorcraft Outwash Test Overview by NASA Ames Research Center.” In Proceedings of the Vertical Flight Society Electric VTOL Symposium - San Jose, California, Jan 2026. The Vertical Flight Society. https://doi.org/10.4050/sm_evtol_2026-5239
• Raffel, Markus, Pascal Weinhold, Felix Wienke, and Andreas Dillmann. 2022. “Wind Tunnel and Flight Testing of Otto Lilienthal’s Experimental Monoplane from 1895.” In AIAA SCITECH 2022 Forum. AIAA 2022-1605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1605
• Rafla, Farid K. 2019. “Aerodynamic Heating Coupled with Structural Temperature Response Analysis for Hypersonic Flight Vehicles.” In AIAA Aviation 2019 Forum. AIAA 2019-3132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3132
• Raghavan, Brijesh, and N. Ananthkrishnan. 2005. “Small-Perturbation Analysis of Airplane Dynamics with Dynamic Stability Derivatives Redefined.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6029
• Ragheb, Adam, Or D. Dantsker, and Michael S. Selig. 2013. “Stall/Spin Mitigation Flight Testing with a Subscale Aerobatic Aircraft.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2806. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2806
• Rahman, Md Mashiur, and Muhammad Akbar. 2026. “Performance Comparison of Truss-Braced Wing Aircraft Model with Boeing 738–800 Aircraft Model Using CFD Simulation.” In AIAA AVIATION 2026 Forum. AIAA 2026-4063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4063
• Raible, Thorsten, and Dieter Jacob. 2003. “Sensitivity-Based Optimization of Two-Stage-To-Orbit Space Planes with Lifting Body and Waverider Lower Stages.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-6955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6955
• Raisinghani, S., G. Bhaskar Reddy, and A. Ghosh. 1999. “Parameter Estimation of an Augmented Aircraft Using Neural Networks.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4248
• Raisinghani, Sri, and Ajoy Ghosh. 2002. “Parameter Estimation of an Unstable Aircraft in Turbulent Atmosphere Using Neural Networks.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4623
• Raisinghani, S., and Hemant Kumar. 1995. “Unsteady Aerodynamic Modeling for Parameter Estimation of a Canard Aircraft.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3435. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3435
• Raju Kulkarni, Akshay, Carmine Varriale, Mark Voskuijl, Gianfranco La Rocca, and Leo L. Veldhuis. 2019. “Assessment of Sub-Scale Designs for Scaled Flight Testing.” In AIAA Aviation 2019 Forum. AIAA 2019-3089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3089
• Rakin, D. 1981. “Fleet Flight Loads Survey Monitoring and Analysis Techniques.” In 1st Flight Test Conference. AIAA 1981-2461. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2461
• Rallabhandi, Sriram K. n.d. “Propagation Analysis of the 3rd Sonic Boom Prediction Workshop Cases Using sBOOM.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20205010207
• Rallabhandi, Sriram. 2011. “Sonic Boom Adjoint Methodology and Its Applications.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3497
• Rallabhandi, Sriram K. 2014. “Application of Adjoint Methodology in Various Aspects of Sonic Boom Design.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2271
• Rallabhandi, Sriram K. 2022. “Secondary Sonic Boom Ray Path Prediction Using sBOOM.” In AIAA SCITECH 2022 Forum. AIAA 2022-0099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0099
• Rallabhandi, Sriram, and Alexandra Loubeau. 2017. “Summary and Progress Made in Modeling of Sonic Boom Propagation during AIAA Sonic Boom Prediction Workshops.” Journal of the Acoustical Society of America 141 (5_Supplement): 3462–3462. https://doi.org/10.1121/1.4987185
• Rallabhandi, Sriram, Eric Nielsen, and Boris Diskin. 2012. “Sonic Boom Mitigation through Aircraft Design and Adjoint Methodology.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3220
• Ram Prabhu, M., C. Balaji, T. Sundararajan, and M. J. Chacko. 2021. “Estimation of Aerodynamic Heating on Scramjet Inlets and Validation with Measurements.” Journal of Thermal Science and Engineering Applications 14 (1): 011010. https://doi.org/10.1115/1.4050838
• Ramachandran, S., and W. Wells. 1974. “Estimation of Nonlinear Aerodynamic Derivatives of a Variable Geometry Fighter Aircraft from Flight Data.” In Mechanics and Control of Flight Conference. AIAA 1974-790. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-790
• Raman, Kumar, Robert Anderson, Garry Brown, Richard Miles, and Marc Costantino. 2000. “An Ultra-High Pressure, Ultra-High Reynolds Number Blowdown Wind Tunnel: Design and Preliminary Experiments.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-534
• Ramm, Heinrich J. 1990. “Lift Slope and Drag Rise at Sonic Speed.” In Fluid Dynamics for the Study of Transonic Flow. Oxford University PressNew York, NY. https://doi.org/10.1093/oso/9780195060973.003.0005
• Ramnath, R. 1969. “Transition Dynamics of VTOL Aircraft.” In 7th Aerospace Sciences Meeting. AIAA 1969-130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-130
• Ramsen, John A., Kenneth L. Wadlin, and George R. Gray. 1951. Tank Investigation of the EDO Model 142 Hydro-Ski Research Airplane. NACA-RM-SL51I24. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029446
• Rana, Loveneesh. 2014. “Sizing Boeing X-20 DYNA-SOAR with USAF Space Planner’s Guide.” In AIAA SPACE 2014 Conference and Exposition. AIAA 2014-4452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-4452
• Rand, James L. 1963. The Aerodynamic Heating of a Composite Flat Plate. Defense Technical Information Center. https://doi.org/10.21236/ad0419249
• Raney, David L., and Martin R. Waszak. 2003. Biologically Inspired Micro-Flight Research. SAE-2003-01-3042. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040031588
• Rao, Anagha G., Umesh Siddharth, and Srisha M. V. Rao. 2023. “Artificial Neural Network-Based Streamline Tracing Strategy Applied to Hypersonic Waverider Design.” APL Machine Learning 1 (1): 016103. https://doi.org/10.1063/5.0127034
• Raol, J., and R. Jategaonkar. 1995. “Aircraft Parameter Estimation Using Recurrent Neural Networks: A Critical Appraisal.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3504. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3504
• Raol, Jitendra R., and Jatinder Singh. 2023a. “Aircraft Handling Qualities Analysis.” In Flight Mechanics Modeling and Analysis. CRC Press. https://doi.org/10.1201/9781003293514-11
• Raol, Jitendra R., and Jatinder Singh. 2023b. “System Identification and Parameter Estimation for Aircraft.” In Flight Mechanics Modeling and Analysis. CRC Press. https://doi.org/10.1201/9781003293514-10
• “Rarefied Hypersonic Flow over a Sphere.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0081.0106
• Rasky, Daniel, R. Bruce Pittman, and Mark Newfield. 2006. “The Reusable Launch Vehicle Challenge.” In Space 2006. AIAA 2006-7208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7208
• Rasky, Daniel J., Joan Salute, Paul Kolodziej, and Jeffrey Bull. 1998. The NASA Sharp Flight Experiment. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020051881
• Rasmussen, M. 1979. “Lifting-Body Configurations Derived from Supersonic Flows past Inclined Circular and Elliptic Cones.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1665. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1665
• Rasmussen, M. 1995. “Stability Derivatives for Hypersonic Waveriders According to Newtonian Theory.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3492
• Rasuo, Bosko. 2000. “An Experimental and Theoretical Study of Reynolds and Mach Number Effects at Two-Dimensional Wind Tunnel Testing.” In 2000 World Aviation Conference. AIAA 2000-5510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5510
• Rathsam, Jonathan, Alexandra Loubeau, and Jacob Klos. 2011. “Sonic-Boom Loudness Test Using New Indoor Sonic-Boom Subjective-Test Facility at NASA Langley Research Center.” Journal of the Acoustical Society of America 129 (4_Supplement): 2379–2379. https://doi.org/10.1121/1.3587710
• Ratnayake, Nalin Asela. 2007. Dryden Flight Research Center: The World’s Premiere Installation for Atmospheric Flight Research. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070021480
• Ratnayake, Nalin. 2009. Dryden Flight Research Center: Center Overview. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20090016338
• Ratnayake, Nalin A. 2010. “Analysis of a Channeled Centerbody Supersonic Inlet for F-15B Flight Research.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100001729
• Ratnayake, Nalin, Edwin Koshimoto, and Brian Taylor. 2011b. “Multi-Axis Identifiability Using Single-Surface Parameter Estimation Maneuvers on the X-48B Blended Wing Body.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6273
• Ratnayake, Nalin A., Erin R. Waggoner, and Brian R. Taylor. 2011a. “Lateral-Directional Parameter Estimation on the X-48B Aircraft Using an Abstracted, Multi-Objective Effector Model.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110015838
• Ratvasky, Thomas P. 2001. Wind Tunnel Tests Conducted to Develop an Icing Flight Simulator. NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20050196675
• Ratvasky, Tom. 2024. “Supercooled Large Droplet Ice Formations from Flight Research.” In SLD Engineering Tools Development Workshop. https://ntrs.nasa.gov/citations/20240013137
• Ratvasky, Thomas, Billy Barnhart, Sam Lee, and Jon Cooper. 2007. “Flight Testing an Iced Business Jet for Flight Simulation Model Validation.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-89. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-89
• Ratvasky, T. P., and R. J. Ranaudo. 1993. Icing Effects on Aircraft Stability and Control Determined from Flight Data: Preliminary Results. NASA-TM-105977. NASA. https://ntrs.nasa.gov/citations/19930005642
• Ratvasky, Thomas P., J. Walter Strapp, Lyle E. Lilie, Aaron Bransemer, and Ru-Ching Chen. n.d. “Air Data Probe Anomalies in Flight through Measured High Ice Water Content Conditions.” In AIAA Aviation Forum. https://ntrs.nasa.gov/citations/20240007205
• Ratvasky, Thomas P., J. Walter Strapp, Lyle E. Lilie, Aaron Bransemer, and Ru-Ching Chen. 2024. Air Data Probe Anomalies in Flight through Measured High Ice Water Content Conditions. NASA/TP-20240010882. NASA. https://ntrs.nasa.gov/citations/20240010882
• Ratvasky, Thomas, and Judith Van Zante. 1999. “In-Flight Aerodynamic Measurements of an Iced Horizontal Tailplane.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-638
• Rauk, Adam P., and Paul Faya. 2022. “Application of Bayesian Hierarchical Models to Experimental Design.” In Case Studies in Bayesian Methods for Biopharmaceutical CMC. Chapman and Hall/CRC. https://doi.org/10.1201/9781003255093-7
• Rausch, Vincent L., Charles R. McClinton, and J. Larry Crawford. 1997. Hyper-X: Flight Validation of Hypersonic Airbreathing Technology. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040110669
• Rausch, Vincent L., Charles R. McClinton, Joel Sitz, and Paul Reukauf. 2000. NASA’s Hyper-X Program. IAF Paper 00-V.4.01. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010075170
• Rauscher, E. 1983. “Structural Flight Load Testing Pre and Post Flight Analysis.” In 2nd Flight Testing Conference. AIAA 1983-2763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2763
• Raveh, Daniella, and Yuval Levy. 2004. “CFD-Based Aeroelastic Response of an Active Aeroelastic Wing.” In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. AIAA 2004-1515. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1515
• Ravetta, Patricio A., Mehdi R. Khorrami, and Ryan Ferris. 2024. “Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 2 – Acoustic Signature and Noise Source Identification.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3059
• Ray, E. 1982. “A Review of Reynolds Number Studies Conducted in the Langley 0.3-m Transonic Cryogenic Tunnel.” In 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference. AIAA 1982-941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-941
• Ray, Ronald. 1994. “Evaluating the Dynamic Response of in-Flight Thrust Calculation Techniques during Throttle Transients.” In Biennial Flight Test Conference. AIAA 1994-2115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2115
• Ray, Ronald J., Brent R. Cobleigh, M. Jake Vachon, and Clinton SaintJohn. 2002. Flight Test Techniques Used to Evaluate Performance Benefits during Formation Flight. NASA/TP-2002-210730. NASA. https://ntrs.nasa.gov/citations/20030005804
• Ray, R., J. Hicks, and R. Alexander. 1988. “Development of a Real-Time Aeroperformance Analysis Technique for the X-29A Advanced Technology Demonstrator.” In 4th Flight Test Conference. AIAA 1988-2145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2145
• Ray, Ronald J., John W. Hicks, and Keith D. Wichman. 1992. “Real-Time in-Flight Engine Performance and Health Monitoring Techniques for Flight Research Application.” In DLR, Proceedings of the 16th Symposium on Aircraft Integrated Monitoring Systems. https://ntrs.nasa.gov/citations/19930005980
• Ray, E., R. Kilgore, J. Adcock, and E. Davenport. 1974. “Test Results from the Langley High Reynolds Number Cryogenic Transonic Tunnel.” In 8th Aerodynamic Testing Conference. AIAA 1974-631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-631
• Raymer, Daniel. 1988. “The Impact of VTOL on the Conceptual Design Process.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4479. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4479
• Razon, Vincent, Gavin Maher, Khai Phan, Sean McEntire, Tommy Fuentes, and Subodh Bhandari. 2023. “Stabilization and Autonomous Flight of a Custom Designed Vertical Tailless Blended Wing-Body UAV.” In AIAA SCITECH 2023 Forum. AIAA 2023-1551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1551
• “Re-Entry Heating.” 1988. In Re-Entry Aerodynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862342.0081.0142
• Re-Entry Trajectory with Diveline Guidance. 1993. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861741.0548.0556
• “Re-Entry Vehicle Particle Mechanics.” 1993. In Dynamics of Atmospheric Re-Entry. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861741.0179.0222
• Reba, Imants. 1964. Gaseous Radiation in Hypersonic Stagnation Point Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0444094
• Reba, Imants, and W. J. Christian. 1963. Gaseous Radiation in Hypersonic Stagnation Point Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0297092
• Recine, Carl J., Dahlia D. V. Pham, Jeffrey V. Bowles, Kenneth R. Lyons, Benjamin W. L. Margolis, and Joseph A. Garcia. 2023. “Analysis and Optimization of Baseline Single Aisle Aircraft for Future Electrified Powertrain Flight Demonstrator Comparisons.” In AIAA/IEEE Electric Aircraft Technologies Symposium (EATS). https://ntrs.nasa.gov/citations/20220016441
• Recine, Carl, Michael Schuh, Noah S. Listgarten, and Kevin James. 2025. “Quantification of Design Trade-Offs When Comparing Transonic Truss-Braced Wing to Advanced Tube and Wing Aircraft.” In AIAA SCITECH 2025 Forum. AIAA 2025-0457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0457
• Redd, L. T., P. W. Hanson, and E. C. Wynne. 1979. Evaluation of a Wind-Tunnel Gust Response Technique Including Correlations with Analytical and Flight Test Results. NASA-TP-1501. NASA. https://ntrs.nasa.gov/citations/19800002782
• Redeker, G., K. Horstmann, H. Koester, P. Thiede, and J. Szodruch. 1990. “Design for a Natural Laminar Flow Glove for a Transport Aircraft.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3043
• Redeker, A., and P. Voersmann. 1988. “An Airborne Realtime Data Processing and Monitoring System for Research Aircraft.” In 4th Flight Test Conference. AIAA 1988-2165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2165
• Redelinghuys, Christiaan, Arthur Grunwald, Steven Rhodes, Jordan L. Adams, and Tracy D. Booysen. 2015. “Parafoil Flight Mechanics: A Novel Flight Test Facility.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2151. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2151
• Rediess, H. A. 1974. “An Overview of Parameter Estimation Techniques and Applications in Aircraft Flight Testing.” In Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017457
• Rediess, Herman, and Herschel Melton. 1994. “Integrated Flight Test Environment: A Concept for Integration of Simulation with Flight Test.” In Biennial Flight Test Conference. AIAA 1994-2172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2172
• Redifer, Matthew, Yohan Lin, Courtney Amos Bessent, and Carole Barklow. 2007. The Hyper-X Flight Systems Validation Program. NASA/TM-2007-214620. NASA. https://ntrs.nasa.gov/citations/20070021457
• Reding, J., and Harold Svendsen. 1988. “Lifting Entry Rescue Vehicle Configuration.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4342. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4342
• Redondo Gutierrez, Jose Luis R., David Seelbinder, Johannes Robens, and Paul Acquatella. 2022. “Design of a Control Allocation Solution for the Winged Reusable Launch Vehicle ReFEx.” In AIAA SCITECH 2022 Forum. AIAA 2022-1842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1842
• Reed, Robert D. 1955. Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Deg. NACA-RM-H55E20a. National Advisory Committee for Aeronautics. High-Speed Flight Station. https://ntrs.nasa.gov/citations/19930088802
• Reed, Helen L. 1997. Stability of Hypersonic Boundary-Layer Flows. Defense Technical Information Center. https://doi.org/10.21236/ada329724
• Reed, E. J., R. R. Horton, and J. B. Fyfe. 1982. “EAGLE: An Interactive Engine/Airframe Life Cycle Cost Model.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/82-gt-56
• Reed, R. Dale, Darlene Lister, and Chuck Yeager. 1997. Wingless Flight: The Lifting Body Story. NASA-SP-4220. NASA. https://ntrs.nasa.gov/citations/19980169231
• Reed, R. D., and J. D. Watts. 1961. Skin and Structural Temperatures Measured on the X-15 Airplane during a Flight to a Mach Number of 3.3. NASA-TM-X-468. NASA. https://ntrs.nasa.gov/citations/19630004036
• Reed, W. H., III. 1975a. “Comparison of Flight Measurements with Predictions from Aeroelastic Models in the NASA Langley Transonic Dynamics Tunnel.” In AGARD Flight Mech. Panel Symp. on Flight/Ground Facility Correlation. https://ntrs.nasa.gov/citations/19750015538
• Reed, W. H., III. 1975b. “A Flight Investigation of Oscillating Air Forces: Equipment and Technique.” In Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003013
• Reed, W. H., III. 1976a. “Comparisons of Flight Measurements with Predictions from Aeroelastic Models in the NASA Langley Transonic Dynamics Tunnel.” In AGARD Flight(Ground Testing Fac. Correlation. https://ntrs.nasa.gov/citations/19760018188
• Reed, W. H., III. 1976b. “Correlation with Flight of Some Aeroelastic Model Studies in the NASA Langley Transonic Dynamics Tunnel.” In Its Flutter Testing Tech.,. https://ntrs.nasa.gov/citations/19770014088
• Reeh, Andreas D., and Cameron D. Tropea. 2014. “Behavior of a NLF Airfoil in Flight through Atmospheric Turbulence.” In 52nd Aerospace Sciences Meeting. AIAA 2014-1274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1274
• Reeh, Andreas D., and C. Tropea. 2015. “Behaviour of a Natural Laminar Flow Aerofoil in Flight through Atmospheric Turbulence.” Journal of Fluid Mechanics 767: 394–429. https://doi.org/10.1017/jfm.2015.49
• Reeves, E. H., Jr., J. R. Stovall, and W. B. Threlkeld Jr. 1960. Space Vehicle Sa-4, Telemetry System. NASA-TM-X-53153. NASA. https://ntrs.nasa.gov/citations/19650002716
• Regenie, Victoria, Donald Gatlin, Robert Kempel, and Neil Matheny. 1992. The F-18 High Alpha Research Vehicle: A High-Angle-of-Attack Testbed Aircraft. NASA-TM-104253. NASA. https://ntrs.nasa.gov/citations/19920024160
• Rehman, Obaid Ur, Baris Fidan, and Ian Petersen. 2009. “Minimax LQR Control Design for a Hypersonic Flight Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7291. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7291
• Reich, Gregory, Daniella Raveh, and P. Zink. 2002. “Application of Active Aeroelastic Wing Technology to a Joined-Wing Sensorcraft.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1633. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1633
• Reich, hoor, Mart, Gregory, Charissa Lin, and Edward Crawley. 1995. “An Active Aeroelastic Wing Model for Vibration and Flutter Suppression.” In 36th Structures, Structural Dynamics and Materials Conference. AIAA 1995-1193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1193
• Reichenbach, Eric. 2003. “Aeroservoelastic Design and Test of the X-45A Unmanned Combat Air Vehicle.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1883
• Reichert, Carl E. 1950. “Supersonic and Transonic Aircraft Problems.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/500040
• Reichle, H. G., Jr. 1965. Flight-Test Results of Gamma Ray Scattering as a Technique for Air-Density Measurement. NASA-TM-X-56837. NASA. https://ntrs.nasa.gov/citations/19660020077
• Reid, David C., Abdelhak M. Zoubir, and Boualem Boashash. 1997. “Aircraft Flight Parameter Estimation Based on Passive Acoustic Techniques Using the Polynomial Wigner–Ville Distribution.” Journal of the Acoustical Society of America 102 (1): 207–23. https://doi.org/10.1121/1.419803
• Reif, Manfred, Norman A. Mattmuller, and John J. Shapley. 1966. Engineering Flight Test of UH-1B Helicopter Equipped with XM-47 Antipersonnel Mine Dispensing Subsystem. Defense Technical Information Center. https://doi.org/10.21236/ad0809915
• Reilly, James P. 1964. “Stagnation-Point Heating in Ionized Monatomic Gases.” Physics of Fluids 7 (12): 1905–12. https://doi.org/10.1063/1.1711099
• Reimer, L., C. Braun, and J. Ballmann. n.d. “Computational Study of the Aeroelastic Equilibrium Configuration of a Swept Wind Tunnel Wing Model in Subsonic Flow.” In High Performance Computing in Science and Engineering ’06. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-36183-1_31
• Reimer, Thomas, Giuseppe Di Martino, Lucas Dauth, et al. 2025. “STORT Hypersonic Flight Experiment Forebody Temperature Results.” In AIAA SCITECH 2025 Forum. AIAA 2025-1342. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1342
• Reimer, Thomas, Giuseppe Di Martino, Ivaylo Petkov, Lucas Dauth, Luis Baier, and Ali Gülhan. 2023. “Design, Manufacturing and Assembly of the STORT Hypersonic Flight Experiment Thermal Protection System.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3089
• Rein, M., H. Rosemann, and E. Schülein. 2009. “Wave Drag Reduction by Means of Aerospikes on Transonic Wings.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_83
• Reiner, Jacob. 1996. “In-Flight Transfer-Alignment Using Aircraft-to-Wing Stiff-Angle Estimation.” In Guidance, Navigation, and Control Conference. AIAA 1996-3818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3818
• Reinhardt, Thomas F. 1948. “Factors Affecting the Selection of Propellants for Rocket Powered Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/480049
• Reinmann, J. J., R. J. Shaw, and W. A. Olsen Jr. 1982. Aircraft Icing Research at NASA. NASA-TM-82919. NASA. https://ntrs.nasa.gov/citations/19820022421
• Rembetsy, C. T. 1966. Feasibility Study of Constructing a 1/10 Scale Apollo Service Module Similitude Model Final Report. NASA-CR-65426. NASA. https://ntrs.nasa.gov/citations/19660021240
• Rempt, R. 1981. “Comparison of Space Vehicle Thermal Flight Data with Solar Thermal Vacuum Test Data.” In 1st Flight Test Conference. AIAA 1981-2479. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2479
• Ren, Zhi. 2009. “Hypersonic Vehicle Multidisciplinary Design Optimization Based on Approximate Technology.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7321. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7321
• Ren, Jie, Jianxin Liu, and Song Fu. 2014. “The Role of Görtler Vortices in the Hypersonic Boundary Layer Transition.” In 44th AIAA Fluid Dynamics Conference. AIAA 2014-2642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2642
• Renaudie, J. 1971. “Concorde and C.E.V.- Cooperation between Firms and Government Officesor Establishment in the Flight Test Program: Certification Flights.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-784
• Renz, R. R. L., R. Clarke, M. A. Mosser, J. Roskam, and D. Rummer. 1981. “Development of a Simple, Self-Contained Flight Test Data Acquisition System.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19810058350
• “Research and Analysis on Development and Flight Test of Military Aircraft Flight Simulator.” 2022. Foreign Language Science and Technology Journal Database Engineering Technology. https://doi.org/10.47939/et.v3i2.102
• “Research and Design of Automatic Flight Control System Test System.” 2022. Foreign Language Science and Technology Journal Database Engineering Technology. https://doi.org/10.47939/et.v3i2.104
• “Research Instrumentation Requirements for Flight/Wind-Tunnel Tests of the YF-12 Propulsion System and Related Flight Experience.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0019.0039
• Research-Airplane-Committee Report on Conference on the Progress of the X-15 Project: A Compilation of the Papers Presented, Held at Langley Aeronautical Lab., Langley Field, VA on 25-26 October 1956. 1956. NASA. https://ntrs.nasa.gov/citations/19930092423
• Reshotko, E. 1970. “Boundary Layer Induced Pressures on a Flat Plate in Unsteady Hypersonic Flight.” In 8th Aerospace Sciences Meeting. AIAA 1970-184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-184
• Resler, E. L. 1969. “Lifting Aerodynamic Configurations with No Sonic Boom.” In Aerodynamic Noise. University of Toronto Press. https://doi.org/10.3138/9781487582869-023
• “Response Analysis of Landing Leg Deployment and Landing Transient Impact of Reusable Launch Vehicle.” 2026. Journal of Mechanical Engineering 62 (1): 159. https://doi.org/10.3901/jme.260010
• “Response of Heat-Shield Materials to Intense Laser Radiation.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0193.0209
• Reubush, David. 1992. “A Historical Perspective on Hypersonic Research at the NACA/NASA Langley Research Center (1944-1984).” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5034
• Reubush, David E. 1999. “Hyper-X Stage Separation: Background and Status.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20040087154
• Reubush, David E., John G. Martin, Jeffrey S. Robinson, David M. Bose, and Brian K. Strovers. 2001. Hyper-X Stage Separation: Simulation Development and Results. AIAA Paper 2001-1802. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010058883
• Reubush, D., L. Nguyen, and V. Rausch. 2003. “Review of X-43A Return to Flight Activities and Current Status.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7085
• Reukauf, P., W. Schweikhard, and H. Arnaiz. 1974. “Flight-Test Techniques for Obtaining Valid Comparisons of Wind-Tunnel and Flight Results from Tests on a YF-12 Mixed-Compression Inlet.” In 10th Propulsion Conference. AIAA 1974-1195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1195
• “Reusable Launch Vehicle Landing Gear Mechanism Technologies: A Review.” 2026. Journal of Mechanical Engineering 62 (1): 18. https://doi.org/10.3901/jme.260002
• Rey, René J. 2000. “Deriving an Acceptable Level of Reusable Launch Vehicle Flightworthiness.” In AIP Conference Proceedings, vol. 504. AIP. https://doi.org/10.1063/1.1290921
• Rezy, Bernard J. 1980. MINI-RPV Engine Demonstrator Program. Defense Technical Information Center. https://doi.org/10.21236/ada083282
• Rhea, Donald, and Archie Moore. 1988. “Development of a Mobile Research Flight Test Support Capability.” In 4th Flight Test Conference. AIAA 1988-2087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2087
• Rhoads, D. W. 1952. Flight-Test Measurement of Vertical and Horizontal Tail Loads during Rudder-Kick and Steady Sideslip Maneuvers. Rudder-Kick Maneuver Study. Part 1. Defense Technical Information Center. https://doi.org/10.21236/ad0014479
• Rhoads, Donald W. 1967. In-Flight Simulation and Pilot Evaluation of Selected Landing Approach Handling Qualities of a Large Logistics Transport Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0820790
• Rhoads, Donald W. 1970. In-Flight Evaluation of Four Cockpit Controller Configurations in a Variable Stability Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0876589
• Rhode, Richard V. 1935. The Influence of Tip Shape on the Wing Load Distribution as Determined by Flight Tests. NACA-TR-500. NASA. https://ntrs.nasa.gov/citations/19930091573
• Rhodes, W. 1969. “Initial Military Flight Tests of the X-22A VSTOL Research Aircraft.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-319
• Rhodes, M. D., and B. P. Selberg. 1982. Dual Wing, Swept Forward Swept Rearward Wing, and Single Wing Design Optimization for High Performance Business Airplanes. Missouri-Rolla, University. https://ntrs.nasa.gov/citations/19820057396
• Rhyne, Richard H., and Harold N. Murrow. 1957. Effects of Airplane Flexibility on Wing Strains in Rough Air at 5,000 Feet as Determined by Flight Tests of a Large Swept-Wing Airplane. NACA-TN-4107. NASA. https://ntrs.nasa.gov/citations/19930084850
• Ribeiro, Frederico, Renan Sanches Geronel, Carlos De Marqui Junior, and Douglas Bueno. 2021. “On the Use of PZT Transducers for Active Flutter Suppression.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-2324
• Ricci, Sergio, Federico Fonte, Alessandro De Gaspari, et al. 2019. “Development of a Wind Tunnel Model for Active Flutter Suppression Studies.” In AIAA Scitech 2019 Forum. AIAA 2019-2029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2029
• Ricciardi, Joseph M., and Cyrus Minwalla. 2016. “Non-Intrusive Flight Test Instrumentation Using Video Recognition.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2016-1435. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1435
• Rice, Brian. n.d. “Characterization of a Dual-Mode Scramjet via Stereoscopic Particle Image Velocimetry.” PhD diss., University of Virginia. https://doi.org/10.18130/v38v6p
• Rice, R. H. 1946. Flight Test Program for a Jet Propelled High Performance Medium Bombardment Airplane: AAF Model XB-45 (NAA Model Number NA-130). Revised. Defense Technical Information Center. https://doi.org/10.21236/adb803248
• Rice, L. E. P., and A. M. K. Cheng. n.d. “Timing Analysis of the X-38 Space Station Crew Return Vehicle Avionics.” In Proceedings of the Fifth IEEE Real-Time Technology and Applications Symposium. IEEE Comput. Soc. https://doi.org/10.1109/rttas.1999.777678
• Rice, Robert, and Douglas Hazlwood. 1994. “Flight Test Program on the Cessna CitationJet.” In Biennial Flight Test Conference. AIAA 1994-2166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2166
• Rich, M. 1969. “Advanced Materials Applications for VTOL Aircraft.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-764
• Richard, J. C., C. Morales, W. L. Smith, and L. N. Myrabo. 1990. “Laser-Boosted Lightcraft Technology Demonstrator.” In NASA. Lewis Research Center, Vision-21: Space Travel for the Next Millennium. https://ntrs.nasa.gov/citations/19910012843
• Richard, Robert E., John A. Rule, and Robert L. Clark. 2000. “Genetic Spatial Optimization of Active Elements on an Aeroelastic Delta Wing.” In Adaptive Structures and Material Systems. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2000-1708
• Richards, W. Lance. 1997. Finite-Element Analysis of a Mach-8 Flight Test Article Using Nonlinear Contact Elements. NASA-TM-4796. NASA. https://ntrs.nasa.gov/citations/19970020392
• Richardson, David F. 1976. Comparison of Flight Test and Wind Tunnel Performance Characteristics of the X-24B Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/adb012971
• Richey, G., M. Petersen, and E. Price Jr. 1976. “Wind Tunnel/flight Test Correlation Program on the B-1 Nacelle Afterbody/nozzle.” In 12th Propulsion Conference. AIAA 1976-673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-673
• Richwine, David M. 1996. F-15B/Flight Test Fixture 2: A Test Bed for Flight Research. NASA-TM-4782. NASA. https://ntrs.nasa.gov/citations/19970005357
• Richwine, David M., Robert E. Curry, and Gene V. Tracy. 1989. A Smoke Generator System for Aerodynamic Flight Research. NASA-TM-4137. NASA. https://ntrs.nasa.gov/citations/19900004056
• Richwine, David M., and John H. Del Frate. 1995. Flight-Test Fixture for Aerodynamic Research. DRC-95-27. PRC, Inc. https://ntrs.nasa.gov/citations/19950065585
• Richwine, David M., and John H. Delfrate. 1994. “Development of a Low-Aspect Ratio Fin for Flight Research Experiments.” In Biennial Flight Test Conference. https://ntrs.nasa.gov/citations/19950010443
• Rickard, W. 1978. “Modeling and Parameter Uncertainties for Aircraft Flight Control System Design.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1371
• Ricketts, Rodney H. 1990. “Experimental Aeroelasticity History, Status and Future in Brief.” In AIAA/ASME/ASCE/AHS/ASC 31st Structures, Structural Dynamics, and Materials Conference. https://ntrs.nasa.gov/citations/19900011731
• Ricketts, R. H., and R. V. Doggett Jr. 1980. Wind-Tunnel Experiments on Divergence of Forward-Swept Wings. NASA-TP-1685. NASA. https://ntrs.nasa.gov/citations/19800020786
• Riddle, D., R. Innis, J. Martin, and J. Cochrane. 1981. “Powered-Lift Takeoff Performance Characteristics Determined from Flight Test of the Quiet Short-Haul Research Aircraft /QSRA/.” In 1st Flight Test Conference. AIAA 1981-2409. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2409
• Riddle, Dennis W., Victor C. Stevens, and Joseph C. Eppel. 1988. “Quiet Short-Haul Research Aircraft: A Summary of Flight Research since 1981.” In International Powered Lift Conference and Exposition. https://ntrs.nasa.gov/citations/19880049959
• Riebe, J. M., and R. E. Kuhn. 1973. “Research on Future Short-Haul Aircraft at the NASA Langley Research Center.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730032814
• Riedel, H., and M. Sitzmann. 1997. “Flight Investigations of the Effect of Yaw on the Intake and Fan Nozzle Flow of a Natural Laminar Flow Nacelle.” Aeronautical Journal 101 (1008): 389–97. https://doi.org/10.1017/s0001924000066112
• Riggins, David, H. Nelson, and Eric Johnson. 1998. “Blunt Body Wave Drag Reduction Using Focused Energy Deposition.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1647
• “Rigid-Body Flight Dynamics.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.005
• Riis, Mehdi, Alessandro Piscopo, Alessandro Parente, and Axel Coussement. 2024. “Numerical Modelling of Combustion Phenomena Prediction in a Dual-Mode Ramjet with a Cavity Flameholder.” Preprint, . https://doi.org/10.2139/ssrn.4887318
• Riley, Christopher J., and Fred R. Dejarnette. 1992. An Engineering Aerodynamic Heating Method for Hypersonic Flow. AIAA PAPER 92-0499. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920043703
• Riley, Zachary B., and Jack J. McNamara. 2016. “Interaction between Aerothermally Compliant Structures and Boundary Layer Transition in Hypersonic Flow.” In 15th Dynamics Specialists Conference. AIAA 2016-1087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1087
• Rimer, M., R. Chipman, and R. Mercadante. 1983. “Divergence Suppression System for a Forward Swept Wing Configurationwith Wing-Mounted Stores.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2125
• Rimer, M., R. Chipman, and B. Muniz. 1984a. “Control of Forward Swept Wing Configurations Dominated by Flight-Dynamic/aeroelastic Interactions.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1866
• Rinehart, David, Jinu Idicula, Matthew Gray, and Paul Bean. 2025. The Systems Engineering Approach to the Streamlined Workflow for Innovative Flight Test Activity. NASA/TM-20250009540. NASA. https://ntrs.nasa.gov/citations/20250009540
• Risch, Timothy K. 2008. “X-48B Flight Research Progress Overview.” In NASA Fundamental Aeronautics 2nd Annual Meeting/NASA ARMD. https://ntrs.nasa.gov/citations/20080043567
• Risch, Tim, Gary Cosentino, Chris Regan, Michael Kisska, and Norman Princen. 2009a. “X-48B Flight Research Progress Overview.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090005167
• Risch, Tim, Gary Cosentino, Chris Regan, Michael Kisska, and Norman Princen. 2009b. “X-48B Flight Research: Test Progress and Instrumentation Needs for the Future.” In International Test and Evaluation Association (ITEA) 2009 Test Instrumentation Workshop. https://ntrs.nasa.gov/citations/20090020686
• Rittenhouse, L. E. 1959. Base Pressure Effects Resulting from Changes in Tunnel Pressure Ratio in a Transonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0207771
• Ritter, Markus, Johannes Dillinger, and Yasser M. Meddaikar. 2017. “Static and Dynamic Aeroelastic Validation of a Flexible Forward Swept Composite Wing.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0637
• Rivera, Jose, and James Florance. 2000. “Contributions of Transonic Dynamics Tunnel Testing to Airplane Flutter Clearance.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1768
• Rivers, Robert A., E. B. Jackson, and W. A. Ragsdale. 1991. “Piloted Simulator Studies of the HL-20 Lifting Body.” In SETP Symposium. https://ntrs.nasa.gov/citations/19920057409
• Rivers, Melissa B., Ralf Rudnik, and Jürgen Quest. 2015. “Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited).” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1093
• Rivers, Natale A., Cornielious P. vanDam, Phillip W. Brown, and Robert A. Rivers. 2001a. Flight Investigation of the Effects of Pressure-Belt Tubing Size on Measured Pressure Distributions. NASA/TM-2001-209857. NASA. https://ntrs.nasa.gov/citations/20020005142
• Rivers, Melissa B., and Richard A. Wahls. 1999. “Turbulence Model Comparisons and Reynolds Number Effects over a High-Speed Aircraft at Transonic Speeds.” In First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop. https://ntrs.nasa.gov/citations/20000044873
• Rivers, S. M. B., and R. A. Wahls. 2003. “Turbulence Model Comparisons for Supersonic Transports at Transonic and Supersonic Conditions.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3418
• Rivers, S. M. B., R. A. Wahls, and L. R. Owens. 2001b. Reynolds Number Effects on Leading Edge Radius Variations of a Supersonic Transport at Transonic Conditions. AIAA Paper 2001-2462. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010055248
• Rizk, M., and D. Lovell. 1986. “Two-Dimensional Transonic Wind-Tunnel Wall Interference Corrections Based on the Euler Equations.” In 24th Aerospace Sciences Meeting. AIAA 1986-124. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-124
• Ro, Kapscong, Jewel Barlow, and Gyunghyun Bae. 1992. “Integrated Flight Control Law Synthesis for an Aeroelastic Forward-Swept Wing Aircraft.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-46. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-46
• Roach, Robert, and H. Froning. 1996. “Drag Reduction of Transonic Airfoils by Freestream Perturbations and Heat Addition.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3413. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3413
• Roback, V. E., Long Yip, Daniel Banks, C. P. Dam, and Stephanie Los. 1996. “Attachment-Line Transition and Boundary-Layer Relaminarization on a High-Lift Wing in Flight.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-6001. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-6001
• Roberts, Sean C. 1963. A Flight Investigation of Profile Drag Measurements. Defense Technical Information Center. https://doi.org/10.21236/ad0420853
• Roberts, J. 1988a. “F-15E Flight Test Program Overview: March 1988.” In 4th Flight Test Conference. AIAA 1988-2077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2077
• Roberts, Nadia. 1988b. “The Weapons Range and Flight Test Support Facilities of Flight Research Inc. at Mojave Airport.” In 4th Flight Test Conference. AIAA 1988-2113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2113
• Roberts, Sean, and John Brown. 1988. “The National Test Pilot School: A Unique Solution to the Aircraft Manufacturers’ Flight Test Training Requirements.” In 4th Flight Test Conference. AIAA 1988-2083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2083
• Roberts, Matthew, Helen Reed, and William Saric. 2012. “A Transonic Laminar-Flow Wing Glove Flight Experiment: Computational Evaluation and Linear Stability.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2668
• Roberts, Sean, and Wendell Shawler. 1994. “Flight Test Education for the 21st Century.” In Biennial Flight Test Conference. AIAA 1994-2181. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2181
• Roberts, Sean C., Michael R. Smith, and David G. Clark. 1966. Flight Test Evaluation of a Distributed Suction High-Lift Boundary Layer Control System on a Modified L-19 Liaison Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0635953
• Roberts, Sean C., Aberdeen W. Stewart, Virgil L. Boaz, Glenn D. Bryant, and Lawrence J. Mertaugh Jr. 1967. XV-11A Description and Preliminary Flight Test. Defense Technical Information Center. https://doi.org/10.21236/ad0654469
• Roberts, Larry A., and Paul M. Wagner. 1973. Flight Test Evaluation of Folding Sidewall Expandable Tires on the C- 131B Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0762730
• Robertson, Scott, and Amy Hartfield. 1992. “Phase I Flight Test of MIAG Advanced Development Model.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4076. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4076
• Robinson, Harold L. 1948. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane-Dynamic Pressure and Comparison of Point and Effective Downwash at the Tail of the D-558-1. NACA-RM-L8H05. NASA. https://ntrs.nasa.gov/citations/19930085531
• Robinson, Donald W. 1959. “Design Considerations for a Propeller-Driven VTOL.” Journal of the American Helicopter Society 4 (1): 34–38. https://doi.org/10.4050/jahs.4.34
• Robinson, Daniel. 1995. “AV-8 Technology Demonstrator: Customer/contractor Collaboration.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3964. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3964
• Robinson, Jason. 2004. Structural Testing and Analysis of a Joined Wing Technology Demonstrator. Defense Technical Information Center. https://doi.org/10.21236/ada425641
• Robinson, C., R. Bauer, and R. Nichols. 1985. “Estimating Water Vapor Condensation Effects for Transonic and Supersonic Flow Fields.” In 3rd Applied Aerodynamics Conference. AIAA 1985-5020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-5020
• Robinson, Glenn H., George E. Cothren Jr., and Chris Pembo. 1955. Wing-Load Measurements at Supersonic Speeds of the Douglas D-558-II Research Airplane. NACA-RM-H54L27. NASA. https://ntrs.nasa.gov/citations/19930088812
• Robinson, Wesley, and Richard Gerwin. 2001. “MHD Flight Control for Hypersonic Vehicles.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1884
• Robinson, Jeffrey S., and John G. Martin. 2006. “SACD’s Support of the Hyper-X Program.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20060050110
• Robinson, M. R., and D. A. Robinson. 1980. “Forward Swept Wing (FSW) Designs: A High Payoff through Technology Integration.” In Aircraft Systems Meeting. AIAA 1980-1884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1884
• Robinson, Brandon M., Weixing Yuan, and Dominique Poirel. 2020. “Global Sensitivity Analysis of Shockwave Location during Transonic Flight.” In AIAA Aviation 2020 Forum. AIAA 2020-2726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2726
• Rocci Denis, Sara, Armin Brandstetter, and Hans-Peter Kau. 2003. “Experimental Study on Transition between Ramjet and Scramjet Modes in a Dual-Mode Combustor.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-7048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-7048
• Rocha Da Costa, Leandro. n.d. “Nonlinear Aeroelastic Modeling of a Flexible Wing and Comparison with Experiments.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2017-11781
• Rock, Lee C. 1964. Performance Parameters of the X-20 Dyna-Soar Prototype Full Pressure Assembly. Defense Technical Information Center. https://doi.org/10.21236/ad0603307
• “Rocket Powered Prototypes.” 1998. Aircraft Engineering and Aerospace Technology 70 (5). https://doi.org/10.1108/aeat.1998.12770eab.002
• “ROCKET-POWERED AIRCRAFT.” 2017. In The History of Human Space Flight. University Press of Florida. https://doi.org/10.2307/j.ctvx072b5.11
• Rockwell, Robert, Christoper Goyne, Willie Haw, Roland Krauss, James McDaniel, and Charles Trefny. 2010. “Experimental Study of Test Medium Vitiation Effects on Dual-Mode Scramjet Mode Transition.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1126
• Rodi, Patrick. 2012. “Preliminary Ramjet/Scramjet Integration with Vehicles Using Osculating Flowfield Waverider Forebodies.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3223
• Rodi, Patrick E. 2018a. “Waverider Vehicle Optimization with Volumetric Constraints for Sonic Boom.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0551
• Rodi, Patrick E. 2018b. “Waverider Vehicle Optimization with Volumetric Constraints for Wave Drag Minimization.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1048
• Rodi, Patrick E. 2021. “Effects of Viscosity on Capsule/Waverider Shape Optimization for Boost-Glide Missions.” In AIAA Aviation 2021 Forum. AIAA 2021-2542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2542
• Rodi, Patrick E. 2023. “Improved Waverider Vehicle Optimization with Volumetric and Lift Constraints for Shaped Sonic Booms.” In AIAA SCITECH 2023 Forum. AIAA 2023-2100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2100
• Rodi, Patrick E., Henry Stoldt, Colin Hill, and Craig T. Johansen. 2019. “Design of a Sounding Rocket Flight Experiment to Validate Transonic Drag Minimized Waveriders.” In AIAA Aviation 2019 Forum. AIAA 2019-2812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2812
• Rodriguez-Segade Alonso, Miguel, Santiago Hernández, Daniel Amenedo, and Jacobo Díaz. 2021. “An Application of Single and Multiobjective Optimization to the Design of the Hypersonic STRATOFLY-MR3 Vehicle.” In AIAA Aviation 2021 Forum. AIAA 2021-2419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2419
• Roepke, R. 1972. “The High Reynolds Number Transonic Wind Tunnel HIRT Proposed as Part of the National Aeronautical Facilities Program.” In 7th Aerodynamic Testing Conference. AIAA 1972-1035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1035
• Roeser, Mathias S., and Wulf Mönnich. 2024. “System Identification from Virtual Flight Test Data for a Flexible Transport Aircraft.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing. https://doi.org/10.1007/978-3-031-69425-7_5
• Rogalski, Tomasz. 2018. “Unmanned Aircraft Automatic Flight Control Algorithm in Loop Manoeuvre.” Aircraft Engineering and Aerospace Technology 90 (6): 877–84. https://doi.org/10.1108/aeat-02-2018-0088
• Rogalski, Tomasz, Paweł Rzucidło, and Jacek Prusik. 2020. “Unmanned Aircraft Automatic Flight Control Algorithm in a Spin Maneuver.” Aircraft Engineering and Aerospace Technology 92 (8): 1215–24. https://doi.org/10.1108/aeat-05-2019-0099
• Roger, K., G. Hodges, and L. Felt. 1974. “Active Flutter Suppression: A Flight Test Demonstration.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-402
• Rogers, Robert. 2002a. “Aerodynamic Parameter Estimation for Controlled Parachutes.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4708. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4708
• Rogers, R. C., A. T. Shih, and N. E. Hass. 2005. Scramjet Engine Flowpath Development for the Hyper-X Mach 10 Flight Test. ISABE-2005-1025. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050234608
• Rogers Jr. and Walter K. 1953. The Transonic Free Flight Range. Defense Technical Information Center. https://doi.org/10.21236/ad0013358
• Rogers Jr. and Walter K. 1958. The Transonic Free Flight Range. Defense Technical Information Center. https://doi.org/10.21236/ad0200177
• Roglin, H. R. 1975. “The Application of Measurement Techniques to Track Flutter Testing.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003014
• Roh, Hyun Woo, Yun Jin Park, Nam Eun Park, and Il Woo Lee. 2006. “Air Data System Calibration of T-50/A-50.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6282
• Rohit, Ram V. 2024. “Design, Analysis, and Simulation of the Hybrid Tri-Copter VTOL Tilt-Rotor UAV.” Revista Electronica de Veterinaria: 507–21. https://doi.org/10.69980/redvet.v24i4.1345
• Rohlmann, David, and Stefan Keye. 2015. “Stall Maneuver Simulation of an Elastic Transport Aircraft Based on Flight Test Data.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2570
• Roland, A. 1984. Model Research: The National Advisory Committee for Aeronautics, 1915-1958, Volume 1. NASA-SP-4103-VOL-1. NASA. https://ntrs.nasa.gov/citations/19850015372
• Roland, Alex, and John V. Becker. 1983. “The High-Speed Frontier: Case Histories of Four NACA Programs, 1920-1950.” Technology and Culture 24 (1): 144. https://doi.org/10.2307/3104192
• Rolls, L. Stewart. 1947. Comparison between Flight-Measured and Calculated Span Load Distribution at High Mach Numbers. NACA-RM-A7G17. NASA. https://ntrs.nasa.gov/citations/19930085791
• Rolls, L. S. 1965. Operational Experiences with the x-14a Deflected-Jet Vtol Aircraft. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19650021531
• Rolls, L. Stewart, and Rodney C. Wingrove. 1958. An Investigation of the Drag Characteristics of a Tailless Delta-Wing Airplane in Flight, Including Comparison with Wind-Tunnel Data. NASA-MEMO-10-8-58A. NASA. https://ntrs.nasa.gov/citations/19980228476
• Rom, Joseph, Mark Lewis, Ashwani Gupta, and John Sabean. 1995. “Hypersonic Aerodynamics Test Facility Using the External Propulsion Accelerator.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6138
• Romere, P., D. Eichblatt, J. Underwood, and D. Howes. 1978. “The Space Shuttle Orbiter Approach and Landing Tests: A Correlationof Flight and Predicted Performance Data.” In 10th Aerodynamic Testing Conference. AIAA 1978-793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-793
• Rona, Aldo, and Houssam Soueid. 2010. “Boundary Layer Trips for Low Reynolds Number Wind Tunnel Tests.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-399
• Ronald, Terence. 1989. “Materials Challenges for NASP.” In National Aerospace Plane Conference. AIAA 1989-5010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5010
• Rongqi, Shi, and Song Jianmei. 2013. “Dynamics and Control for an in-Plane Morphing Wing.” Aircraft Engineering and Aerospace Technology 85 (1): 24–31. https://doi.org/10.1108/00022661311294094
• Rongrong, Xue, Ye Zhengyin, Ye Kun, and Wang Gang. 2018. “Composite Material Structure Optimization Design and Aeroelastic Analysis on Forward Swept Wing.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (13): 4679–95. https://doi.org/10.1177/0954410018807810
• Roohani, H., and B. W. Skews. 2009. “Effect of Acceleration on Shock-Wave Dynamics of Aerofoils during Transonic Flight.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_98
• Rooker, J. 1970. “The Need for a Flight-Test Instrumentation Specification.” In Test Effectiveness in the 70’s Conference. AIAA 1970-376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-376
• Rooney, Brendan. 2003. “Reusable Launch Vehicle Ground Operational Challenges.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2953
• Rooney, E., R. Craig, and R. Lauer. 1977. “Correlation Full Scale Wind Tunnel and Flight Measured Aerodynamic Drag.” In 13th Propulsion Conference. AIAA 1977-996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-996
• Rooney, E., and C. Wilt. 1985. “Development of in-Flight Thrust Measurement Procedures for an Afterburning Turbofan Engine.” In 21st Joint Propulsion Conference. AIAA 1985-1405. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1405
• Roos, F. 1975. “Surface Pressure and Wake Flow Fluctuations in a Supercritical Airfoil Flowfield.” In 13th Aerospace Sciences Meeting. AIAA 1975-66. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-66
• Rosatelli, Patrizio, Carlos E. Cesnik, and Christopher A. Lupp. 2024. “Free-Flight Flutter Constraint in Gradient-Based Wing Structural Optimization.” In AIAA SCITECH 2024 Forum. AIAA 2024-2410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2410
• Rose, W., and A. Seginer. 1977. “Calculation of Transonic Flow over Supercritical Airfoil Sections.” In 10th Fluid and Plasmadynamics Conference. AIAA 1977-681. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-681
• Rosen, Aviv, and Ronith Yaffe. 2001. “Compressibility Effects on the Unsteady Aerodynamics of a Rotor in Hover or Axial Flight.” Journal of the American Helicopter Society 46 (1): 44–58. https://doi.org/10.4050/jahs.46.44
• Rosenbaum, R. 1974. Survey of Aircraft Subcritical Flight Flutter Testing Methods. NASA-CR-132479. NASA. https://ntrs.nasa.gov/citations/19740026355
• Rosenberg, R., and G. Schuch. 1983. “The M.C.A.-Method, a Flight Test Technique to Determine Thrust of Jet Aircraft in Flight.” In 2nd Flight Testing Conference. AIAA 1983-2749. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2749
• Rosenstein, Harald. 1989. “Conceptual Design of an Advanced V/STOL Special Electronic Mission Aircraft.” In Proceedings of the The Rotary Wing Aircraft Conceptual Design Process - Atlanta, Georgia, 1989. The Vertical Flight Society. https://doi.org/10.4050/sm_rotary_1989-2147
• Rosenthal, G. 1982. “NGT Sub-Scale Flight Demonstrator — A Cost-Effective Approach to Aircraft Development.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/821341
• Rosenthal, G., and G. Brandeau. 1983. “The Application of Low-Cost Demonstrators for Advancead Fighter Technology Evaluation.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1052
• Roskam, J., C. Van Dam, and M. Griswold. 1980. “Correlation of Predicted Longitudinal Aerodynamic Characteristics with Full-Scale Wind Tunnel Data on the ATLIT Airplane.” In 18th Aerospace Sciences Meeting. AIAA 1980-186. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-186
• Ross, A. 1972. “An Experimental and Analytical Study of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft.” In 10th Aerospace Sciences Meeting. AIAA 1972-62. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-62
• Ross, J. 1984. “Applicability of a Panel Method, Which Includes Nonlinear Effects, to a Forward-Swept-Wing Aircraft.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2402
• Ross, J. C., and A. D. Matarazzo. 1982. “Low-Speed Aerodynamic Characteristics of a Generic Forward-Swept-Wing Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/821467
• Ross, J., and D. Rogerson. 1983. “XB-70 Technology Advancements.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1048
• Rostkowski, Przemyslaw, and Marco Panesi. 2022. “Quantification of Uncertainty in Extrapolation of Charring Ablator Material Performance to Flight.” In AIAA SCITECH 2022 Forum. AIAA 2022-2360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2360
• Rosłowicz, Adam, and Paweł Bednarczyk. 2017. “Analysis of Heat Transfer in a Supersonic Rocket Head.” Transactions on Aerospace Research 2017 (1): 79–94. https://doi.org/10.2478/tar-2017-0008
• Roth, Dan. 2009. “Reinvigorating the Technical Excellence of the Engineering Workforce at the Air Force Flight Test Center.” In U.S. Air Force T&E Days 2009. AIAA 2009-1763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-1763
• Roth, Dan, William Kitto, and Megan Taylor. 2010. “Improving Air Force Flight Test Center Developmental Test and Evaluation through Increased Use of Statistical Methods.” In U.S. Air Force T&E Days 2010. AIAA 2010-1766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1766
• Rothacker, Benjamin A. 2017. “On the Numerical Stability of the Eminton-Lord Wave Drag Method.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3576
• Rothery, Claire, David Glynn, and Hendrik Koffijberg. 2023. “Rapid Value of Information Using Minimal Modelling.” In Value of Information for Healthcare Decision-Making. Chapman and Hall/CRC. https://doi.org/10.1201/9781003156109-9
• “Rotorcraft Handling Qualities Design.” 2011. In Eigenstructure Control Algorithms: Applications to aircraft/rotorcraft handling qualities design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e_ch11
• Roudakov, Alexander, Vyacheslav Semenov, and John Hicks. 1998. “Recent Flight Test Results of the Joint CIAM-NASA Mach 6.5 Scramjet Flight Program.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1643
• Roudakov, Alexander, Vyacheslav Semenov, Valeriy Kopchenov, and John Hicks. 1996. “Future Flight Test Plans of an Axisymmetric Hydrogen-Fueled Scramjet Engine on the Hypersonic Flying Laboratory.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4572
• Row, Perry, and Jack Fischel. 1963. “Operational Flight-Test Experience with the X-15 Airplane.” In Space Flight Testing Conference. AIAA 1963-75. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-75
• Roy, Abhishek Ghosh, and Naba Kumar Peyada. 2019. “Aircraft Aerodynamic Parameter Estimation Using Intelligent Estimation Algorithms.” In Advances in Computational Intelligence and Robotics. IGI Global. https://doi.org/10.4018/978-1-5225-5852-1.ch011
• Roy, R., and R. Walker. 1985. Real-Time Flutter Identification. NASA-CR-3933. NASA. https://ntrs.nasa.gov/citations/19860002751
• Roysdon, Paul, and Mahmood Khalid. 2011. “Blended-Wing-Body Lateral-Directional Stability Investigation Using 6DOF Simulation.” In Infotech@Aerospace 2011. AIAA 2011-1563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1563
• Ruan, Allen, and Tove Aagren. 2025. “Flight Dynamics Prediction for Scaled Mars Rotorcraft.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0283
• Rubin, Donald V. 1971. Rocket Plume Effects on Boattail and Flare Bodies of Revolution at Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0730669
• Rucci, John, Laura Slingerland, Rob Pupalaikis, et al. 2023. “CH-53K Maneuvering Envelope Expansion Challenges.” In Proceedings of the Vertical Flight Society 79th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0079-2023-18176
• Rudland, R. S., I. M. Kroenke, and A. R. Urbach. 1992. “Slush Hydrogen Quantity Gaging and Mixing for the National Aerospace Plane.” In Advances in Cryogenic Engineering. Springer US. https://doi.org/10.1007/978-1-4615-3368-9_48
• Ruetten, Markus. 2018. “Numerical Investigation of Thrust Vectoring for a High-Aspect Ratio Nozzle of an Unmanned Combat Air Vehicle.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3340
• Ruf, Joseph H., Alonzo L. Frost, Bruce Vu, and Francisco Canabal. 1996. “Assessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics.” In Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology. https://ntrs.nasa.gov/citations/19960029266
• Ruhlin, C., and A. Murphy. 1981. “Transonic Flutter and Gust-Response Tests and Analyses of a Wind-Tunnel Model of a Torsion-Free-Wing Fighter Airplane.” In Dynamics Specialists Conference. AIAA 1981-650. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-650
• Ruhlin, C., and C. Pratt-Barlow. 1981. “Transonic Flutter Study of a Wind-Tunnel Model of an Arrow-Wing Supersonic Transport.” In Dynamics Specialists Conference. AIAA 1981-654. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-654
• Runyan, L., and D. George-Falvy. 1979. “Amplification Factors at Transition on an Unswept Wing in Free Flight and on a Swept Wing in Wind Tunnelaircraft Stability Analysis.” In 17th Aerospace Sciences Meeting. AIAA 1979-267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-267
• Runyan, L. James, and Louis L. Steers. 1980. Boundary Layer Stability Analysis of a Natural Laminar Flow Glove on the F-111 TACT Airplane. Boeing (United States). https://ntrs.nasa.gov/citations/19810042099
• Rus, C. P., S. L. Gal, and S. G. Pintado. 2026. “A3.1: Model-Based Interface Management for Flight Test Instrumentation Systems.” In Lectures. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2026/a3.1
• Russell, Kenneth G. 2018. “Bayesian Experimental Design.” In Design of Experiments for Generalized Linear Models. Chapman and Hall/CRC. https://doi.org/10.1201/9780429057489-7
• Russell, Carl, and Sarah Conley. 2020. “The Multirotor Test Bed: A New NASA Test Capability for Advanced VTOL Rotorcraft Configurations.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16370
• Russo, M., M. Healy, and M. Brock. 1986. “X-29A Flight Flutter Data Analysis by Advanced Methods.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9737
• Russo, Samual C., Jack Levine, and Steven L. Prusha. 1994. NASA Technology Flight Experiments Program. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210004226
• Russo, M., P. Richards, and H. Perangelo. 1983. “Identification of Linear Flutter Models.” In 2nd Flight Testing Conference. AIAA 1983-2696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2696
• Russo, Gennaro, and Raffaele Savino. 2015. “HYPLANE: The Business Case of a Smallersonic Airplane for Point-to-Point and Space Tourism Flights.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3673
• Russo, Lorenzo, Renato Tognaccini, and Luciano Demasi. 2020a. “Box Wing and Induced Drag: Compressibility Effect in Subsonic and Transonic Regimes.” In AIAA Scitech 2020 Forum. AIAA 2020-0447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0447
• Ryan, John J., John T. Bosworth, John J. Burken, and Peter M. Suh. 2014. “Current and Future Research in Active Control of Lightweight, Flexible Structures Using the X-56 Aircraft.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140003966
• Ryan, Kevin M., Mark Lewis, and Kenneth H. Yu. 2013. “Comparison of Robust Optimization Methods Applied to Hypersonic Vehicle Design.” In AIAA Modeling and Simulation Technologies (MST) Conference. AIAA 2013-4680. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4680
• Ryan-Simmons, Dean, and Ramesh K. Agarwal. 2024. “Extension of Wray-Agarwal Algebraic Transition Model to Include the Compressibility Effects for the Analysis of External Transonic Flows.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3996
• Rydlo, Karol, Pawel Rzucidlo, and Peter Chudy. 2013. “Simulation and Prototyping of FCS for Sport Aircraft.” Aircraft Engineering and Aerospace Technology 85 (6): 475–86. https://doi.org/10.1108/aeat-10-2012-0186
• Rylko, Agata, Lorenzo Favaro, and Giuseppe Quaranta. 2025. “Sensitivity Analysis and Aerodynamic Modeling of eVTOL Low-Speed Predicted Handling Qualities.” In Proceedings of the Vertical Flight Society 11th Biennial Autonomous VTOL (AVTOL) Technical Meeting, Phoenix, AZ Feb 2025. The Vertical Flight Society. https://doi.org/10.4050/sm_avtol_2025-5322
• Rynaski, E., D. Andrisani II, and N. Weingarten. 1978. “Identification of the Stability Parameters of an Aeroelastic Airplane.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1328
• Rzucidło, Paweł. 2006. “Monitoring and Data Acquisition System for Experimental General Aviation Fly-by-Wire Aircraft.” Aviation 10 (3): 16–20. https://doi.org/10.3846/16487788.2006.9635935
• S-7 Flight Deck Handling Qualities Stds for Trans Aircraft. n.d.-a. Design Objectives for Flying Qualities of Civil Transport Aircraft. SAE International. https://doi.org/10.4271/arp842a
• S-7 Flight Deck Handling Qualities Stds for Trans Aircraft. n.d.-b. Design Objectives for Handling Qualities of Transport Aircraft. SAE International. https://doi.org/10.4271/arp842c
• S-7 Flight Deck Handling Qualities Stds for Trans Aircraft. n.d.-c. Flight Envelope Awareness/Protection. SAE International. https://doi.org/10.4271/arp4104/1
• Sabatini, Roberto. 2013. “Development and Flight Test of an Avionics Lidar for Helicopter and UAV Low-Level Flight.” Journal of Aeronautics & Aerospace Engineering 02 (03). https://doi.org/10.4172/2168-9792.1000114
• Sabatini, Andrea A., Eli Livne, and Giuliano Coppotelli. 2026. “Integrated Gust Load Alleviation and Active Flutter Suppression: Control Law Synthesis and Wind Tunnel Tests.” In AIAA SCITECH 2026 Forum. AIAA 2026-1443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1443
• Sabin, M. 1973. “Linear Filtering of Ballistic-Entry-Probe Data for Atmospheric Reconstruction.” In Guidance and Control Conference. AIAA 1973-904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-904
• Sacchi, Francesco, Joshua Sneddon, Fintan Healy, Djamel Rezgui, and Jonathan E. Cooper. 2026. “Aeroelastic Behavior of Forward-Swept Wings with Flared Folding Wingtips.” In AIAA SCITECH 2026 Forum. AIAA 2026-1445. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1445
• Sacher, Peter, and Bernhard Zellner. 1995. “Flight Testing Objectives for Small Hypersonic Flight Test Vehicles Featuring a Ramjet Engine.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6014
• Sachs, Gotfried, and Csaba Moravszki. 2002. “Simulation Experiments for Hypersonic Trajectory Control Using a Predictive Flight Path Display.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4696
• Sachs, Gottfried, and Wolfgang Schoder. 1991. “Optimal Separation of Lifting Vehicles in Hypersonic Flight.” In Navigation and Control Conference. AIAA 1991-2657. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2657
• Saderla, Subrahmanyam, Dhayalan Rajaram, and A. K. Ghosh. 2017. “Parameter Estimation of Unmanned Flight Vehicle Using Wind Tunnel Testing and Real Flight Data.” Journal of Aerospace Engineering 30 (1): 04016078. https://doi.org/10.1061/(asce)as.1943-5525.0000679
• Sadoff, Melvin. 1958. The Effects of Longitudinal Control-System Dynamics on Pilot Opinion and Response Characteristics as Determined from Flight Tests and from Ground Simulator Studies. NASA-MEMO-10-1-58A. NASA. https://ntrs.nasa.gov/citations/19980232012
• Saetti, Umberto, and Jonathan Rogers. 2020. “Explicit Uncertainty Quantification for Probabilistic Handling Qualities Assessment.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16389
• Sager, D. 1995. “Aerodynamic Investigation of a SSTO Vehicle Lifting Body Design.” In Space Programs and Technologies Conference. AIAA 1995-3859. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3859
• Saheby, Eiman B., Guoping Huang, and Anthony Hays. 2017. “Design of Hypersonic Forebody by the Combination of Bump and Waverider Surfaces.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2177
• Sahu, Jubaraj, and Joseph Steger. 1987. “Numerical Simulation of Three Dimensional Transonic Flows.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2293
• Saifuddin, Che Noureen Sabrina, Atikah Basyirah Abdul Muta’ali, and Rizal Effendy Mohd Nasir. 2025. “Flight Performance of a VTOL Version of a Transport Blended Wing-Body UAV.” International Journal of Integrated Engineering 17 (4). https://doi.org/10.30880/ijie.2025.17.04.012
• Saito, Yuta, Takahiro Ukai, Ko Miyakoshi, Kiyonobu Ohtani, and Shigeru Obayashi. 2014. “Sonic Boom Estimation Using the Multipole Method for Free-Flight Experiments.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0368
• Sakamoto, Hiroki, Shintaro Sato, and Naofumi Ohnishi. 2023. “Computation of Hypersonic Boundary Layer Transition behind Propagating Shock Wave.” In AIAA SCITECH 2023 Forum. AIAA 2023-1233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1233
• Sakata, K. 2002. “Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology: Development and Flight Test Plan for the Unmanned Scaled Supersonic Glider.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-527
• Sakraker, Isil, and Olivier Chazot. 2014. “A Flight-to-Ground Extrapolation Methodology for Subsonic Plasma Windtunnels and Its Validation by Real Flight Experiment QARMAN.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2567
• Salah El Din, I., M.-C. Le Pape, A. Minelli, R. Grenon, and G. Carrier. 2013. “Impact of Multipole Matching Resolution on Supersonic Aircraft Sonic Boom Assessment.” In Progress in Flight Physics, edited by P. Reijasse, D. Knight, M. Ivanov, I. Lipatov. EDP Sciences. https://doi.org/10.1051/eucass/201305601
• Salamone, Joe. 2006. “Portable Sonic Boom Simulation.” In AIP Conference Proceedings, vol. 838. AIP. https://doi.org/10.1063/1.2210441
• Salis Brasil Neto, Nei, Elder Hemerly, and Luiz Góes. 2006. “Aircraft Parameter Estimation Experiment Design Considering Measurement Colored Residuals.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6283
• Salkind, Mj. 1973. “VTOL Aircraft.” In Applications of Composite Materials. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp34130s
• Salloum, Joseph, Michael J. Candon, Andrew Ridings, Hideaki Ogawa, Masatoshi Kodera, and Shuichi Ueda. 2018. “Numerical Investigation of an RBCC Combustor during Ramjet/Scramjet Mode Transition.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0886
• Saltzman, Edwin J. 1957. Flight-Determined Induction-System and Surge Characteristics of the YF-102 Airplane with a Two-Spool Turbojet Engine. NACA-RM-H57C22. NASA. https://ntrs.nasa.gov/citations/19930089693
• Saltzman, E., and T. Ayers. 1981. “A Review of Flight-to-Wind Tunnel Drag Correlation.” In 1st Flight Test Conference. AIAA 1981-2475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2475
• Saltzman, Edwin J., and Theodore G. Ayers. 1995. Selected Examples of NACA/NASA Supersonic Flight Research. NASA-SP-513. NASA. https://ntrs.nasa.gov/citations/19960016997
• Saltzman, Edwin J., Donald R. Bellman, and Norman T. Musialowski. 1956. Flight-Determined Transonic Lift and Drag Characteristics of the YF-102 Airplane with Two Wing Configurations. NACA-RM-H56E08. NASA. https://ntrs.nasa.gov/citations/19930089423
• Saltzman, Edwin J., John W. Hicks, and Sue Luke. 1994. In-Flight Lift-Drag Characteristics for a Forward-Swept Wing Aircraft and Comparisons with Contemporary Aircraft). NASA-TP-3414. NASA. https://ntrs.nasa.gov/citations/19950012150
• Saltzman, Edwin, K. Wang, and Kenneth Iliff. 1999. “Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations with Truncated Bases.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-383
• Saltzman, Edwin J., K. Charles Wang, and Kenneth W. Iliff. 2002. Aerodynamic Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations. NASA/TP-2002-209032. NASA. https://ntrs.nasa.gov/citations/20030003696
• Salvetti, Augustine, and Harry Seidman. 1988. Noise and Sonic Boom Impact Technology. PCBOOM Computer Program for Sonic Boom Research. Volume 2. Program Users/Computer Operations Manual. Defense Technical Information Center. https://doi.org/10.21236/ada206291
• Sambamurthi, Jay, John Warmbrod, and Mark Seaford. 1989. “Engineering Methodology to Estimate the Aerodynamic Heating to the Base of the Aeroassist Flight Experiment Vehicle.” In 24th Thermophysics Conference. AIAA 1989-1732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1732
• Samikkannu, Raja. 2011. “Wind Tunnel Flutter Testing of Composite T-Tail Model of a Transport Aircraft with Fuselage Flexibility.” In Wind Tunnels and Experimental Fluid Dynamics Research. InTech. https://doi.org/10.5772/21628
• Sammonds, R. 1970. “Transonic Static- and Dynamic-Stability Characteristics of Two Large-Angle Spherically Blunted High-Drag Cones.” In Propulsion and ASW Meeting. AIAA 1970-564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-564
• Sams, Hershel. 1989. “The NASP Challenge: Management Innovation.” In National Aerospace Plane Conference. AIAA 1989-5006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5006
• Samuels, Jeffrey J., and Gordon A. Payne. 1990. “Preliminary Assessment of a Supersonic STOVL Flight Research and Demonstration Aircraft.” In AHS, Annual Forum. https://ntrs.nasa.gov/citations/19910032586
• Sandahl, Carl A. 1948. Free-Flight Investigation at Transonic and Supersonic Speeds of a Wing-Aileron Configuration Simulating the D-558-2 Airplane. NACA-RM-L8E28. NASA. https://ntrs.nasa.gov/citations/19930085394
• Sandahl, Carl A., William M. Bland Jr., and H. Kurt Strass. 1949. Effects of Some Airfoil-Section Variations on Wing-Aileron Rolling Effectiveness and Drag as Determined in Free Flight at Transonic and Supersonic Speeds. NACA-RM-L9D12. NASA. https://ntrs.nasa.gov/citations/19930085881
• Sandeep, Juluru. 2023. “Design and Performance of Hypersonic Intake for Scramjet Engine.” In Hypersonic and Supersonic Flight - Advances in Aerodynamics, Materials, and Vehicle Design. IntechOpen. https://doi.org/10.5772/intechopen.107840
• Sanders, K. 1964. “Optimum Vertifan Concepts for Tactical V/stol Aircraft.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-776
• Sanders, Thomas L. 1972. Flight Test Report of the Model OH-58A Helicopter with the 206-706-129-1 High Tubular Skid Gear Kit Installed. Defense Technical Information Center. https://doi.org/10.21236/ada036489
• Sanders, Newell D., and Edmund E. Callaghan. 1956. “Jet-Engine Noise Reduction Research at NACA.” Noise Control 2 (6): 43–48. https://doi.org/10.1121/1.2369235
• Sanderson, K. C. 1964. The x-15 Flight Test Instrumentation. NASA-TM-X-56000. NASA. https://ntrs.nasa.gov/citations/19640009985
• Sanderson, Kenneth C. 1965. “The X-15 Flight Test Instrumentation.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50017-8
• Sandford, M., I. Abel, and D. Gray. 1974. “A Transonic Study of Active Flutter Suppression Based on an Aerodymamic Energy Concept.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-403
• Sandig, Ludger. 2024. “Kirstine.jl: A Julia Package for Bayesian Optimal Design of Experiments.” Journal of Open Source Software 9 (97): 6424. https://doi.org/10.21105/joss.06424
• Sandlin, D. R. 1984. Development of Flight Testing Techniques. NASA-CR-176996. NASA. https://ntrs.nasa.gov/citations/19860019464
• Sandoz, F., G. Blanc, M. Cariou, and P. Klaeyle. 2024. “B7.6: Embedded Recording in Flight Test Telemetry Receiver.” In ETTC 2024. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2024/b7.6
• Sang, A., and J. Schetz. 2002. “Study of Rubber Damped Skin Friction Gages for Transonic Flight Research.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-533
• Sanmugadas, Varakini, Rikin Gupta, Wei Zhao, Rakesh K. Kapania, and David K. Schmidt. 2021. “Effect of Aeroelastic Tailoring of Composite Skin Laminates on Modal Controllability/Observability of Aircraft Structures.” In AIAA Aviation 2021 Forum. AIAA 2021-3084. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3084
• Sansica, Andrea, and Atsushi Hashimoto. 2023. “Global Stability Analysis of Turbulent Transonic Buffet on the NASA Common Research Model: From Wind Tunnel to Flight Reynolds Numbers.” In AIAA SCITECH 2023 Forum. AIAA 2023-1989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1989
• Santos, Davi, and Americo Cunha Jr. 2024. “Flight Control of a Hexa-Rotor Airship: Uncertainty Quantification for a Range of Temperature and Pressure Conditions.” Preprint, . https://doi.org/10.31224/3922
• Santos, João, Flávio Marques, and Cristina Riso. 2026. “Wing-Propeller Aeroelastic Stability under Aerodynamic Interactions Using the Unsteady Vortex-Lattice Method.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0072
• Santos, Jose, Tomo Oishi, and Edward Martinez. 2011. “Isotherm Sensor Calibration Program for Mars Science Laboratory Heat Shield Flight Data Analysis.” In 42nd AIAA Thermophysics Conference. AIAA 2011-3955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3955
• Sapkal, Kedar, and Peter Attar. 2011. “Experimental and Computational Aeroelastic Analysis of a Composite Material Delta Wing in Low Subsonic Flow.” In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2011-1743. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1743
• Saraswathi, L. 2000. “Estimation of Stability & Control Derivatives from Flight Test Data of Fighter Aircraft.” Defence Science Journal 50 (2): 123–36. https://doi.org/10.14429/dsj.50.3366
• Saric, William S. 2010. Flight Experiments on Swept-Wing Roughness Receptivity: Validation Data for Modeling and Computations. Defense Technical Information Center. https://doi.org/10.21236/ada564004
• Saric, William, and Helen Reed. 2004. “Toward Practical Laminar Flow Control: Remaining Challenges.” In 2nd AIAA Flow Control Conference. AIAA 2004-2311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2311
• Saric, William S., David E. West, Matthew W. Tufts, and Helen L. Reed. 2015. “Flight Test Experiments on Discrete Roughness Element Technology for Laminar Flow Control.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0539
• Sarigul-Klijn, Nesrin, and Jonathan Huber. 2006. “In-Flight Reconfigurable Autopilot for Unmanned Aircraft: Hardware Development and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6507
• Sarigul-Klijn, Nesrin, P. Nespeca, T. Marchelli, and M. Sarigul-Klijn. 2008. “An Approach to Predict Flight Dynamics and Stability Derivatives of Distressed Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6877
• Sarkar, A., M. Ananthasayanam, J. Umakant, T. Srinivasan, and P. Kar. 2009. “Flight Vehicle Aerodynamic Coefficients Estimation under Limited Measurements: New Flight-Test Results.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5940
• Sarkar, A., and S. Panneerselvam. 1998. “Aerodynamic Coefficients Estimation of a Tactical Flight Vehicle from Noisy Flight Test Data under Limited Measurements.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4260
• Sarker, Ripon, Anup Pudasaini, Pratribha Bhandari, et al. 2026. “Design, Development, and Subscale Flight Testing of an Emergency Response eVTOL Aircraft.” In Proceedings of the Vertical Lift Aircraft Design and Aeromechanics Specialists Conference, San Jose, California, Jan 2026. The Vertical Flight Society. https://doi.org/10.4050/sm-2026-vlada-5186
• Sarojini, Darshan, Heriberto D. Solano, Jason A. Corman, and Dimitri N. Mavris. 2022. “Parametric Wingbox Structural Weight Estimation of the CRM, PEGASUS and Truss-Braced Wing Concepts.” In AIAA AVIATION 2022 Forum. AIAA 2022-4054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4054
• Sarosh, Ali. 2021. “An Inverse Aerothermal Design (IAD) Methodology for Scramjet Integrated Waverider Configuration.” Academia Letters. https://doi.org/10.20935/al2998
• Sarrafian, S. K., and B. G. Powers. 1985. Application of Frequency Domain Handling Qualities Criteria to the Longitudinal Landing Task. NASA-TM-86728. NASA. https://ntrs.nasa.gov/citations/19850024811
• Satre, P. 1969. “The Supersonic Air Transport True Problems and Misconceptions.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-759
• Saturn 5 Launch Vehicle Flight Evaluation Report-AS-509 Apollo 14 Mission. 1971. NASA-TM-X-69536. NASA. https://ntrs.nasa.gov/citations/19730025091
• Saturn V Aerothermodynamics Flight Evaluation Summary: AS-501 through AS-503. 1969. D5-15796-1. Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20160013592
• Saunders, Trevor. 1996. “The European Transonic Wind Tunnel: Testing at Flight Reynolds Numbers.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-227
• Savage, H. F., and B. E. Tinling. 1959. Subsonic Aerodynamic Characteristics of Several Blunt, Lifting, Atmospheric-Entry Shapes. NASA-MEMO-12-24-58A. NASA. https://ntrs.nasa.gov/citations/19630004013
• Savu, G., and O. Trifu. 1993. “The Global Aerodynamic Optimization of a Hypersonic Transport Aircraft.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5139
• Sawyer, James Wayne, Jefferson Hodge, Brad Moore, and Kevin Snyder. 1999. “Aerothermal Test of Thermal Protection Systems for X-33 Reusable Launch Vehicle.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57501
• Sawyer, Richard H., and James P. Trant Jr. 1950. Effect of Various Modifications on Drag and Longitudinal Stability and Control Characteristics at Transonic Speeds of a Model of the XF7U-1 Tailless Airplane: NACA Wing-FLow Method, TED No. NACA DE 307. NACA-RM-SL50D18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028471
• Scafetta, D. 1983. “Simulator Fidelity and Flight Test Data: Improving the Flight Performance of the B-52H WST Production Unit Flight Station Simulator.” In Flight Simulation Technologies Conference. AIAA 1983-1075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1075
• Scala, S. M., and E. J. Nolan. 1960. “Aerothermodynamic Feasibility of Graphite for Hypersonic Glide Vehicles.” In Re-Entry and Vehicle Design. Elsevier. https://doi.org/10.1016/b978-1-4832-2885-3.50007-6
• Scallion, W. I. 1982. “Space-Vehicle Correlation of Ground and Flight Experiments.” In Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017332
• Scarselli, Gennaro, and Francesco Marulo. 2010. “Sonic Boom Minimization through a Simplified Approach for the Preliminary Design of Civil Supersonic Aircraft.” In 16th AIAA/CEAS Aeroacoustics Conference. AIAA 2010-4006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4006
• Scarth, Carl, Pia Sartor, Jonathan E. Cooper, Paul Weaver, and Gustavo Silva. 2015. “Robust Aeroelastic Design of a Composite Wing-Box.” In 17th AIAA Non-Deterministic Approaches Conference. AIAA 2015-0918. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0918
• Schade, Robert O. 1968. “VTOL Aircraft Terminal Area Operations Research.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/680663
• Schaefer, Jacob R., and Edward L. Burnett. 2019. “The Making of a MAD MUTT: The X-56A Multi-Utility Technology Testbed Aircraft.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20190002269
• Schaefer, John A., David S. Lazzara, and Stephen T. LeDoux. 2023b. “Robust Design of Sonic Boom Performance Using Spatially Accurate Polynomial Chaos.” In AIAA SCITECH 2023 Forum. AIAA 2023-1353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1353
• Schaefer, Jacob, Peter Suh, Matt Boucher, et al. 2023a. Flying beyond Flutter with the X-56A Aircraft. Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20220012337
• Schafer, Howard C. 1962. In-Flight Temperature Environments of Jet Fighter and Attack Bomber Aircraft Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ad0296912
• Schauerte, Christopher J., and Anne-Marie Schreyer. 2023. “Influence of Reynolds Number on Transonic Buffet Conditions on a Supercritical Airfoil.” In AIAA SCITECH 2023 Forum. AIAA 2023-0431. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0431
• Scheerer, M., Z. Djinovic, and M. Schüller. 2013. “Fiber Optic System for Deflection and Damage Detection in Morphing Wing Structures.” In SPIE Proceedings, vol. 8692, edited by Jerome P. Lynch, Chung-Bang Yun, Kon-Well Wang. SPIE. https://doi.org/10.1117/12.2009256
• Scheidenhelm, Ralph. 1963. “The Primary Guidance Subsystem for the X-20A (Dyna-Soar) Glider.” Navigation 10 (3): 247–65. https://doi.org/10.1002/j.2161-4296.1963.tb02052.x
• Scher, Stanley H. 1947a. Free-Spinning-Tunnel Tests of a 1/27-Scale Model of the Douglas XF3D-1 Airplane, TED No. NACA DE 312. NACA-RM-SL7K21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028509
• Scher, Stanley H. 1947b. Preliminary Evaluation of the Spin and Recovery Characteristics of the Douglas XF3D-1 Airplane. NACA-RM-L7F18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019396
• Scher, Stanley H. 1948. Wind-Tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane: Phases I and II. NACA-RM-L7K10. NASA. https://ntrs.nasa.gov/citations/19930085778
• Scherz, C., and P. Tucker. 1985. “Flight Test Evaluation of Active Ride Control System for Tactical Aircraft.” In Guidance, Navigation and Control Conference. AIAA 1985-1860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1860
• Schierbrock, Aaron J., and Timothy T. Takahashi. 2021. “Reconstruction of Flight-Path Dependent Aircraft Point-Performance, Stability & Control from Public Flight Data.” In AIAA Scitech 2021 Forum. AIAA 2021-0325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0325
• Schifferle, Paul, Paul Deppe, and Randall Bailey. 1999. “Large Aircraft Rate Limit Flight Test Program.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-3963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3963
• Schilling, Lawrence J., and Dale A. Mackall. 1993. “Flight Research Simulation Takes Off.” Aerospace America 31 (8). https://ntrs.nasa.gov/citations/19930069772
• Schiltgen, Benjamin, Andrew R. Gibson, Michael Green, and Jeffrey Freeman. 2013. “More Electric Aircraft: ‘Tube and Wing’ Hybrid Electric Distributed Propulsion with Superconducting and Conventional Electric Machines.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2013-01-2306
• Schiltgen, Benjamin, Michael Green, Jeffrey Freeman, and Andrew Gibson. 2014. “Terminal Area Operations for Hybrid Electric Distributed Propulsion.” Aircraft Engineering and Aerospace Technology 86 (6): 584–90. https://doi.org/10.1108/aeat-04-2014-0047
• Schiltgen, Benjamin, Michael Green, Andrew Gibson, David Hall, Darold Cummings, and Craig Hange. 2012. “Benefits and Concerns of Hybrid Electric Distributed Propulsion with Conventional Electric Machines.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-3769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3769
• Schindel, L. 1989. “Design of High-Performance Ramjet or Scramjet-Powered Vehicles.” In 27th Aerospace Sciences Meeting. AIAA 1989-379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-379
• Schkolnik, Gerard S. 1993. Identification of Integrated Airframe: Propulsion Effects on an F-15 Aircraft for Application to Drag Minimization. NASA-TM-4532. NASA. https://ntrs.nasa.gov/citations/19940019633
• Schkolnik, Gerard, John Orme, and Mark Hreha. 1995. “Flight Test Validation of a Frequency-Based System Identification Method on an F-15 Aircraft.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2362
• Schmidt, David. 1995. “On the Integrated Control of Flexible Supersonic Transport Aircraft.” In Guidance, Navigation, and Control Conference. AIAA 1995-3200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3200
• Schmidt, David K. 2016. “Stability Augmentation and Active Flutter Suppression of a Flexible Flying-Wing Drone.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-2099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2099
• Schmidt, Louis, and R. Duren. 2002. “Wing Induced Drag.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4878
• Schmidt, Sven, and Tim Jusko. 2025. “Abstraction of a Flight Test Maneuver to Evaluate Handling Qualities for Helicopter Air-to-Air Refueling.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0319
• Schmidt, Sven, and Tim Jusko. 2026. “Abstraction of a Flight Test Maneuver to Evaluate Handling Qualities for Helicopter Air-to-Air Refueling.” Preprint, . https://doi.org/10.2139/ssrn.6662535
• Schmidt, S. A., and A. W. Linden. 1972a. Rotor Systems Research Aircraft Predesign Study. Volume 2: Conceptual Study Report. NASA-CR-112153. NASA. https://ntrs.nasa.gov/citations/19720025365
• Schmidt, S. A., and A. W. Linden. 1972b. Rotor Systems Research Aircraft Predesign Study. Volume 3: Predesign Report. NASA-CR-112154. NASA. https://ntrs.nasa.gov/citations/19720025366
• Schmidt, R., and B. Mann. 1996. “Reusable Launch Vehicle/X-33 Preliminary Structural Analysis for Dynamic Launch Environments.” In Dynamics Specialists Conference. AIAA 1996-1199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1199
• Schmidt, David K., Wei Zhao, and Rakesh K. Kapania. 2016. “Flight-Dynamics and Flutter Modeling and Analyses of a Flexible Flying-Wing Drone: Invited.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1748
• Schmitt, Curtis, and Bradley Burchett. 2004. “Fuzzy IPPD Guidance for Approach and Landing of a Reusable Launch Vehicle.” In AIAA 1st Intelligent Systems Technical Conference. AIAA 2004-6254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6254
• Schmitz, Craig P., and Scott B. Tashakkor. 2011. Ares I-X First Stage Internal Aft Skirt Re-Entry Heating Data and Modeling. M11-0031. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20110014621
• Schneider, Steven. 1998. “Survey of Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-432. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-432
• Schneider, Steven P. 2006. Hypersonic Boundary-Layer Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada448081
• Schneider, Steven. 2007. “Effects of Roughness on Hypersonic Boundary-Layer Transition.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-305
• Schneider, Steven. 2008a. “Hypersonic Boundary-Layer Transition on Blunt Bodies with Roughness.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-501
• Schneider, Steven. 2008b. “Hypersonic Boundary-Layer Transition with Ablation and Blowing.” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-3730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-3730
• Schneider, Steven P. 2009. Towards High-Reynolds-Number Quiet Flow in Hypersonic Wind Tunnels. Defense Technical Information Center. https://doi.org/10.21236/ada500049
• Schneider, Steven P. 2013. “Developing Mechanism-Based Methods for Estimating Hypersonic Boundary-Layer Transition in Flight: The Role of Quiet Tunnels.” In 43rd Fluid Dynamics Conference. AIAA 2013-2608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2608
• Schneider, Steven P. 2015. “Developing Mechanism-Based Methods for Estimating Hypersonic Boundary-Layer Transition in Flight: The Role of Quiet Tunnels.” Progress in Aerospace Sciences 72: 17–29. https://doi.org/10.1016/j.paerosci.2014.09.008
• Schneider, Joshua, Reid Larson, and Thomas Hill. 2012. “Overview of the C-12J External Stores Flight Test Program.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-3164. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3164
• Schnerr, Guenter, and Ulrich Dohrmann. 1991. “Drag and Lift in Nonadiabatic Transonic Flow.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1716
• Schnulo, Sydney, and Dustin Hall. 2020. “X-57 Maxwell NASA’s First Electric X-Plane.” In COSI Science Festival. https://ntrs.nasa.gov/citations/20205001703
• Schrauf, G., and W. Schröder. 1999. “Comparison of N-Factor Strategies Using Wind Tunnel Experiments and Flight Tests.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-663-10901-3_51
• Schreckenberg, Dirk. 2021. “2pPA4: Concept for a Study on Community Responses to Low Sonic Boom in Europe.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f248b
• Schuelein, Erich. 2008. “Experimental Investigation of Laminar Flow Control on a Supersonic Swept Wing by Suction.” In 4th Flow Control Conference. AIAA 2008-4208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4208
• Schufflebarger, C. C., and Harry C. Mickleboro. 1950. Flight Investigation of the Effect of Transient Wing Response on Measured Accelerations of a Modern Transport Airplane in Rough Air. NACA-TN-2150. NASA. https://ntrs.nasa.gov/citations/19930082768
• Schumacher, Lloyd E. 1952. A Method for Evaluating Aircraft Stability Parameters from Flight Test Data. Defense Technical Information Center. https://doi.org/10.21236/ada075866
• Schuringa, T. 1974. “Flight Testing the Fokker F28 with Advanced Wing.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-944. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-944
• Schuster, David M. 2009. NASA Aerosciences Perspective on Proposed De-Scope of Ares I-X Development Flight Instrumentation. NASA/TM-2009-215909. NASA. https://ntrs.nasa.gov/citations/20090033663
• Schuster, Lawrence S., and William A. Lokos. 1988. Current Flight Test Experience Related to Structural Divergence of Forward-Swept Wings. NASA-TM-100445. NASA. https://ntrs.nasa.gov/citations/19880015249
• Schwanz, Robert C. 1972. Formulations of the Equations of Motion of an Elastic Aircraft for Stability and Control and Flight Control Applications. Defense Technical Information Center. https://doi.org/10.21236/ada006391
• Schwanz, R., and G. Grimes. 1980. “Parameter Identification of B-52E CCV Flight Test Data Including Aeroelastic Effects.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1635
• Schwartz, Ira R. 1968. Second Conference on Sonic Boom Research. NASA-SP-180. NASA. https://ntrs.nasa.gov/citations/19680025435
• Schwartz, Ira R. 1971. Third Conference on Sonic Boom Research. NASA-SP-255. NASA. https://ntrs.nasa.gov/citations/19710018887
• Schwartz, Samuel R., and Donald P. Wray. 1969. Engineering Flight Test. TH-55A Primary Helicopter Trainer Limited Performance Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ad0864071
• Schwegler - Lanl, E. C., and A. Place - Honeywell. 2000. Miniature Transducers for Flight Test Unit Instrumentation: Magnetic Field Detectors. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/764597
• Schweikhard, William. 1983. “Flight Test Made Easy – Doing Simple Flight Tests Simply.” In 2nd Flight Testing Conference. AIAA 1983-2715. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2715
• Schweikhard, W., and R. Renz. 1986. “Flight Testing for Better Flight Training Simulators.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9728. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9728
• Scientific and Technical Information Division. 1966. Conference on V/STOL and STOL Aircraft. NASA-SP-116. NASA. https://ntrs.nasa.gov/citations/19660015317
• Scigliano, Roberto, Valeria De Simone, and Mario De Stefano Fumo. 2018. “Finite Element Method for Ablative Thermal Protection Systems Design for Atmospheric Re-Entry Vehicles.” In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2018-5207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-5207
• Scott, R. 1983. “Air-to-Air Radar Flight Testing.” In 2nd Flight Testing Conference. AIAA 1983-2768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2768
• Scott, C. D., L. P. Murray, and J. D. Milhoan. 1977. “Shuttle Elevon Cove Aerodynamic Heating by Internal Flow.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19770054418
• Seanor, Brad A. n.d. “Flight Testing of a Remotely Piloted Vehicle for Aircraft Parameter Estimation Purposes.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.2470
• Sears, William R. 1947. “On Projectiles of Minimum Wave Drag.” Quarterly of Applied Mathematics 4 (4): 361–66. https://doi.org/10.1090/qam/20394
• Sebastian, C. 1966. “Thermal-Stability Aspects of Commercial Kerosine for the Supersonic Transport.” In 2nd Propulsion Joint Specialist Conference. AIAA 1966-670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-670
• Sebastiani, Paola, and Henry P. Wynn. 2000. “Maximum Entropy Sampling and Optimal Bayesian Experimental Design.” Journal of the Royal Statistical Society Series B: Statistical Methodology 62 (1): 145–57. https://doi.org/10.1111/1467-9868.00225
• Seber, Guclu, Hongjun Ran, Taeqoo Nam, Joseph Schetz, and Dimitri Mavris. 2011. “Multidisciplinary Design Optimization of a Truss Braced Wing Aircraft with Upgraded Aerodynamic Analyses.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3179. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3179
• “Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0037.0076
• Sedney, R. 1954. On Jones’ Criterion for Thin Wings of Minimum Drag. Defense Technical Information Center. https://doi.org/10.21236/ad0041671
• Seebass, R. 1968. A Survey of Sonic Boom Theory. NASA-CR-108898. NASA. https://ntrs.nasa.gov/citations/19700011162
• Seebass, R. 1969. Sonic Boom Theory. NASA. https://ntrs.nasa.gov/citations/19690056028
• Seebass, A. 1973. “The Design or Operation of Aircraft to Minimize Their Sonic Boom.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-817
• Seebass, A. R. 1974. Improvements to Embedded Shock Wave Calculations for Transonic Flow-Applications to Wave Drag and Pressure Rise Predictions. NASA-CR-139487. NASA. https://ntrs.nasa.gov/citations/19740022516
• Seebass, A. Richard. 1989. “Costs of the National Aerospace Plane.” Science 246 (4936): 1374–75. https://doi.org/10.1126/science.246.4936.1374-e
• Seebass, A. 1994. “The Prospects for Commercial Supersonic Transport.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-17. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-17
• Seebass, A. R. 1997. “The Prospects for Commercial Supersonic Transport.” In New Design Concepts for High Speed Air Transport. Springer Vienna. https://doi.org/10.1007/978-3-7091-2658-5_1
• Seebass, Richard, and Brian Argrow. 1998. “Sonic Boom Minimization Revisited.” In 2nd AIAA, Theoretical Fluid Mechanics Meeting. AIAA 1998-2956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2956
• Seebass, A., and A. George. 1973. “Sonic Boom Reduction through Aircraft Design and Operation.” In 11th Aerospace Sciences Meeting. AIAA 1973-241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-241
• Sefic, Walter J. 1981. NASA Dryden Flight Loads Research Facility. NASA-TM-81368. NASA. https://ntrs.nasa.gov/citations/19820007206
• Sefic, W., and W. Cutler. 1986. “X-29A Advanced Technology Demonstrator Program Overview.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9727. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9727
• Sefic, W. J., and C. M. Maxwell. 1986. “X-29A Technology Demonstrator Flight Test Program Overview.” In ISA Aerospace Industries/Test Measurement Symposium. https://ntrs.nasa.gov/citations/19860016856
• Sefic, Walter J., and Cleo M. Maxwell. 1987. Flight Research on a Forward-Swept-Wing Airplane. ISSN: 0145-319X. NASA Ames Research Center, Moffett Field, Calif. https://ntrs.nasa.gov/citations/19870000497
• Seginer, A., and I. Rosenwasser. 1983. “Magnus Effects on Spinning Transonic Missiles.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2146
• Sehgal, Ajay, and Dave Platz. 2004. “The USMC H-1 Upgrade Program – Initial Flight Test Status.” In Proceedings of the Vertical Flight Society Forum 60 - Baltimore, MD 2004. The Vertical Flight Society. https://doi.org/10.4050/vfs-f60-000178
• Sehnert, Paul. 1963. “A Generalized Approach to Real Time Flight Test Data.” In Testing of Manned Flight Systems Conference. AIAA 1963-1817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1817
• Seidel, D., M. Sandford, and C. Eckstrom. 1985. “Measured Unsteady Transonic Aerodynamic Characteristics of an Elastic Supercritical Wing with an Oscillating Control Surface.” In 26th Structures, Structural Dynamics, and Materials Conference. AIAA 1985-598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-598
• Seider, G., and D. Haenel. 1991. “Numerical Influence of Upwind TVD Schemes on Transonic Airfoil Drag Prediction.” In 29th Aerospace Sciences Meeting. AIAA 1991-184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-184
• Seiferth, David, Martin E. Kügler, and Matthias Heller. 2018. “In-Flight Verification of a Model-Based Designed Ground Controller for an Innovative Unmanned Air Vehicle (UAV).” In 2018 Flight Testing Conference. AIAA 2018-4276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4276
• Seiler, Peter, Gary J. Balas, and Andrew Packard. 2012. “Linear Parameter-Varying Control for the X-53 Active Aeroelastic Wing.” In Control of Linear Parameter Varying Systems with Applications. Springer US. https://doi.org/10.1007/978-1-4614-1833-7_19
• Seiner, John, and Eugene Krejsa. 1989. “Supersonic Jet Noise and the High Speed Civil Transport.” In 25th Joint Propulsion Conference. AIAA 1989-2358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2358
• Seitz, Arne, Martin Kruse, Tobias Wunderlich, Jens Bold, and Lars Heinrich. 2011. “The DLR Project LamAiR: Design of a NLF Forward Swept Wing for Short and Medium Range Transport Application.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3526
• Sekino, S., and M. Maki. 2024. “A Flow-Field Integrated Flight Control: Dynamic Wind Tunnel Testing and Simulation.” Aeronautical Journal 128 (1329): 2451–82. https://doi.org/10.1017/aer.2024.56
• Sekula, Martin K., David J. Piatak, and Russ D. Rausch. 2010. “Analysis of a Transonic Alternating Flow Phenomenon Observed during Ares Crew Launch Vehicle Wind Tunnel Tests.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100024500
• Sensburg, O., H. Hoenlinger, T. Noll, and L. Huttsell. 1980. “Active Flutter Suppression on an F-4F Aircraft.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-770. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-770
• Sepka, Steven, and Jamshid A. Samareh. 2015. “Thermal Protection System Mass Estimating Relationships for Blunt-Body, Earth Entry Spacecraft.” In 45th AIAA Thermophysics Conference. AIAA 2015-2507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2507
• Serdarevic-Kadic, Sabina, and Jasmin Terzic. 2019. “Effects of Base Shape to Drag at Transonic and Supersonic Speeds by CFD.” In DAAAM International Scientific Book. DAAAM International Vienna. https://doi.org/10.2507/daaam.scibook.2019.06
• “A Series of Airfoils Designed by Transonic Drag Minimization for Gates Learjet Aircraft.” 1982. In Transonic Aerodynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865558.0489.0509
• Serre, Laurent. 2009. “Development of S4 Free Jet Test Facility for the French LEA Flight Test Program.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7358
• Serre, Laurent, and Sabastien Defoort. 2009. “LAPCAT II: Towards a Mach 8 Civil Aircraft Concept, Using Advanced Rocket/Dual-Mode Ramjet Propulsion System.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7328
• Serre, Laurent, Pascal Denis, Nicolas Cortes, and François Falempin. 2011. “Development of S4 Free Jet Test Facility for the French LEA Flight Test Program.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2264
• Serre, Laurent, and Francois Falempin. 2008. “Development of S4 Free Jet Test Facility for the French LEA Flight Test Program.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2651
• Setoguchi, Nao, and Masahiro Kanazaki. 2020. “Low-Speed and High Angle of Attack Aerodynamic Characteristics of Supersonic Business Jet with Forward Swept Wing.” In AIAA Scitech 2020 Forum. AIAA 2020-0534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0534
• Seubert, Rainer. 1997. “The Preliminary Aircraft Design and Optimization Program for Supersonic Commercial Transport Aircraft PrADO-Sup.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-86573-1_40
• Seubert, Rainer. 1999. “Validation of the Preliminary Aircraft Design and Optimization Program for Supersonic Commercial Transport Aircraft PrADO-Sup.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-663-10901-3_57
• Sexton, H., Jr. 1964. “Flight Testing the f-104 Automatic Flight Control System.” In 1st Annual Meeting. AIAA 1964-328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-328
• Sforza, Pasquale M. 2018. “Estimating Zero-Lift Drag Coefficients and Maximum L/D in Subsonic Flight.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0273
• Sforza, Pasquale M. 2019. “Reinterpreting the Volume Parameter in Hypersonic Flight.” In AIAA Scitech 2019 Forum. AIAA 2019-0810. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0810
• Sforza, P. M., and Chris Anderson. 2003. An Advanced Free Flight Research Facility. Defense Technical Information Center. https://doi.org/10.21236/ada415973
• Sgubin, Leonardo, Lucas Ribeiro, Matheus Alvarenga, Marco Minucci, Lucas Galembeck, and Israel da Silveira Rego. 2024. “Shock-Tunnel Studies of the Aerodynamic Heating of a Scramjet Inlet at Flight Mach Number 7.” Preprint, . https://doi.org/10.2139/ssrn.4965075
• Sgueglia, Alessandro. n.d. “Methodology for Sizing and Optimising a Blended Wing-Body with Distributed Electric Ducted Fans.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/2046c996z7c68z4b65za4ffz08317a09ee02
• Shafer, M. 1980. “Low Order Equivalent Models of Highly Augmented Aircraft Determined from Flight Data Using Maximum Likelihood Estimation.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1627
• Shafer, M. F. 1982. “Flight-Determined Correction Terms for Angle of Attack and Sideslip.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820056755
• Shafer, M. 1984. “Flight Investigation of Various Control Inputs Intended for Parameter Estimation.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2073
• Shafer, Mary F. 1991. “In-Flight Simulation at the NASA Dryden Flight Research Facility.” In AIAA Flight Simulation Technologies Conference. https://ntrs.nasa.gov/citations/19910063180
• Shafer, Mary F. 1992. “In-Flight Simulation Studies at the NASA Dryden Flight Research Facility.” In AIAA Simulation Technology Conference. https://ntrs.nasa.gov/citations/19920019867
• Shafer, Mary F. 1994. “In-Flight Simulation Studies at the NASA Dryden Flight Research Facility.” In NASA. Ames Research Center, 1993 Technical Paper Contest for Women. Gear Up 2000: Women in Motion. https://ntrs.nasa.gov/citations/19940031462
• Shafer, Mary F., and Paul Steinmetz. 2001. Pilot-Induced Oscillation Research: The Status at the End of the Century. NASA/CP-2001-210389/VOL1. NASA. https://ntrs.nasa.gov/citations/20010038270
• Shang, Maixia, Jinglin Liu, and Chao Gong. 2025. “Reference Prototype of High Lift Motor for Distributed Electric Propulsion All-Electric Aircraft.” IET Power Electronics 18 (1): e70134. https://doi.org/10.1049/pel2.70134
• Shanks, Robert E., and Charles C. Smith Jr. 1960. Low-Speed Measurements of Static and Oscillatory Lateral Stability Derivatives of a 1/5-Scale Model of a Jet-Powered Vertical-Attitude VTOL Research Airplane. NASA-TN-D-433. NASA. https://ntrs.nasa.gov/citations/19980230619
• Shantz, I. 1953. Wind-Tunnel Investigation of the Cvac Supersonic Bomber (HUSTLER-MX-1964). Defense Technical Information Center. https://doi.org/10.21236/ad0037850
• Sharif, Muqeeth, Mohammed Abbas, and Mukarram Hussain. 2022. “Aerodynamics of Forward Swept Wing.” Graduate Research in Engineering and Technology: 83–85. https://doi.org/10.47893/gret.2022.1084
• Sharipkhojaevic, Tukhtabaev. 2025. “History of Aircraft Construction (Former Tashkent Aviation Factory).” Academicia Globe: Inderscience Research 5 (4): 7. https://doi.org/10.47134/academicia.v5i4.21
• Sharma, Surendra. 1992. “NASA Ames’s Electric Arc-Driven Shock Tube Facility and Research on Nonequilibrium Phenomena in Low Density Hypersonic Flows.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3975. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3975
• Sharpe, Peter, and Ramesh K. Agarwal. 2019. “Numerical Analysis of Propeller-Wing Interaction in Aircraft with Distributed Electric Propulsion.” In AIAA Aviation 2019 Forum. AIAA 2019-3691. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3691
• Sharpe, Peter, and R. J. Hansman. 2024. “Physics-Informed Regression and Uncertainty Quantification of Aircraft Performance from Minimal Flight Data.” In AIAA SCITECH 2024 Forum. AIAA 2024-1306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1306
• Sharpes, R. E., and W. J. Carroll. 1973. “Model Support Roll Balance and Roll Coupling.” In The 8th Aerospace Mech. Symp. te. https://ntrs.nasa.gov/citations/19740003568
• Sharqi, Bilal, Carlos E. Cesnik, Noam Yechieli, Wrik Mallik, Daniella E. Raveh, and Moti Karpel. 2021. “Aeroelastic Analyses of the Free Flight of the Active Aeroelastic Aircraft Testbed (A3TB) Platform.” In AIAA Scitech 2021 Forum. AIAA 2021-0905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0905
• Shaw, R., and G. Richter. 1985. “The UH-1H Helicopter Icing Flight Test Program: An Overview.” In 23rd Aerospace Sciences Meeting. AIAA 1985-338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-338
• Shawler, W. 1981. “62% Manned Aircraft Demonstrator: Next Generation Trainer.” In 1st Flight Test Conference. AIAA 1981-2519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2519
• Shawler, W. 1983. “Winning the T-46A Program through Flight Test.” In 2nd Flight Testing Conference. AIAA 1983-2713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2713
• Shawler, W. 1986. “T-46A Flight Test Results.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9766
• Shea, Patrick R., David T. Chan, Morgan A. Walker, et al. n.d. “Force and Moment Analysis for the High Reynolds Number Wind Tunnel Test of the Space Launch System at Ascent Conditions.” In 2023 AIAA SCITECh Forum. https://ntrs.nasa.gov/citations/20220018078
• Sheetz, N., Jr. 1965. “Free-Flight Boundary Layer Transition Investigations at Hypersonic Speeds.” In 2nd Aerospace Sciences Meeting. AIAA 1965-127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-127
• Sheffer, Scott, and George Dulikravich. 1993. “Constrained Optimization of Three-Dimensional Hypersonic Vehicle Configurations.” In 31st Aerospace Sciences Meeting. AIAA 1993-39. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-39
• Sheibani, Mohammad, Seyyed Majid Malek Jafarian, and Mohammadmahdi Abdollahzadehsangroudi. 2024. “Impact of Annular Nanosecond Plasma Actuators on Drag Reduction in Transonic Flow.” Physics of Fluids 36 (11): 116121. https://doi.org/10.1063/5.0237182
• Sheldon, G. J. 1967. Re-Entry Module/Adapter Interconnect Fairing Aerodynamic Heating Wind Tunnel Tests AEDC Tunnel B. Defense Technical Information Center. https://doi.org/10.21236/ad0856658
• Shen, Lin, Da Huang, and Genxing Wu. 2016. “Studies on Unsteady Aerodynamic Modeling and Flight Simulation at High Angles of Attack.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3102
• Shepard, G. D., J. C. Callahan, and J. A. McElman. 1981. Structural Response and Input Identification. NASA-CR-164079. NASA. https://ntrs.nasa.gov/citations/19810011936
• Shepard, Thomas, Jr. 1965. “The XC-142A Flight Test Program.” In Proceedings of the 1st National Symposium on V/STOL Aircraft, Subsystem Design and Testing and Operation - Ohio 1965. The Vertical Flight Society. https://doi.org/10.4050/sm_vstol_1965-4662
• Shepheard, Fred W. 1965. Wind Tunnel Test of 1/7 Scale Model OV-1. Defense Technical Information Center. https://doi.org/10.21236/ad0630924
• Sherman, Tristan M., Jet Ericson C. Tirona, Yahia Haggag, et al. 2021. “Manufacturing and Flight Testing of a Vertical Tailless Blended Wing-Body UAV Design.” In AIAA Scitech 2021 Forum. AIAA 2021-0819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0819
• Sherrer, V., T. Hertz, and M. Shirk. 1980. “A Wind Tunnel Demonstration of the Principle of Aeroelastic Tailoring Applied to Forward Swept Wings.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-796
• Sherrow, Brady R., Ahmed Arabi Hassen, and Saman Farhangdoust. 2026. “Meta-Structures for Aircraft Morphing Wing Design.” In AIAA SCITECH 2026 Forum. AIAA 2026-0697. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0697
• Shi, Lei. 2016. “Numerical Analysis of a Dual-Mode Scramjet Engine VS a Rocket-Based Combined-Cycle Engine.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-4874. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4874
• Shi, Yijian, Bor-Jang Tsai, John Miles, and Kakkattukuzhy Issac. 1994. “Cone-Derived Waverider Flowfield Simulation Including Turbulence and off-Design Conditions.” In 12th Applied Aerodynamics Conference. AIAA 1994-1822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1822
• Shields, E. 1981. “F/A-18 Flight Test Program Overview: 1 September 1981.” In 1st Flight Test Conference. AIAA 1981-2351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2351
• Shields, E., and Wu Li. 2011. “CFD-Based Redesign of a Low-Boom Supersonic Demonstrator Concept (Invited).” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3499
• Shields, Matthew, and Kamran Mohseni. 2011. “Experimental Complications Inherent to Low Reynolds Number Wind Tunnel Testing.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-873
• Shih, W. 1976. “Ballistics Range Measurements of Aerodynamic Heating in Erosion Environments.” In 9th Fluid and PlasmaDynamics Conference. AIAA 1976-319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-319
• Shih, Peter, Allen Zwan, and Michael Kelley. 1988. “Thermal Protection System Optimization for a Hypersonic Aerospace Vehicle.” In 23rd Thermophysics, Plasmadynamics and Lasers Conference. AIAA 1988-2739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2739
• Shin, Jong-Yeob, Gary Balas, and Andrew Packard. 1999. “Worst Case Analysis of the Flight Control System X-38 Crew Return Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4052
• Shin, Jong-Yeob, Christine Belcastro, and thuan Khong. 2006. “Closed-Loop Evaluation of an Integrated Failure Identification and Fault Tolerant Control System for a Transport Aircraft.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. https://ntrs.nasa.gov/citations/20060046667
• Shinoda, Patrick M. 1996. Full-Scale S-76 Rotor Performance and Loads at Low Speeds in the NASA Ames 80- by 120-Foot Wind Tunnel. NASA-TM-110379. NASA. https://ntrs.nasa.gov/citations/19960026432
• Shiplyuk, A., S. Lukashevich, D. Bountin, A. Maslov, and H. Knaus. 2012. “Experiments on Hypersonic Boundary Layer Transition on Blunt Cones with Acoustic-Absorption Coating.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203295
• Shipman, K. W., and E. R. Wood. 1970. “A Theoretical Method for Rotor Blade Flutter in Forward Flight.” In Proceedings of the Vertical Flight Society Forum 26 - Washington, D.C. 1970. The Vertical Flight Society. https://doi.org/10.4050/vfs-f26-006
• Shirouzu, Masao, and Shigeya Watanabe. 1993. “On the Hypersonic Flight Experiment (HYFLEX) for the Development of HOPE.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5080
• Shivaji, Mrudhula, Daksha Basavaraju, Dhuleep Ravi, and Bino Prince Raja Dennis. 2025. “Characterization of Aeroelastic Divergence Behaviour of an Additively Manufactured Wing Structure.” In AIP Conference Proceedings, vol. 3259. AIP Publishing. https://doi.org/10.1063/5.0265477
• Shlien, J. 1991. “Instrument Aircraft Flight Test: A Simulator Manufacturer’s Experience.” In Flight Simulation Technologies Conference. AIAA 1991-2931. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2931
• Shmul, Menahem, Eli Erenthal, and Moshe Attar. 2018. “Lavi Flight Control System.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-10
• “Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0379.0420
• Shovlin, M. D., and J. A. Cochrane. 1978. An Overview of the Quiet Short-Haul Research Aircraft Program. NASA-TM-78545. NASA. https://ntrs.nasa.gov/citations/19790002863
• Shrestha, Prakash, and Graham V. Candler. 2018. “Numerical Study of Trip Spacing in Hypersonic Boundary Layer Transition.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1098
• Shrestha, Prakash, Joseph W. Nichols, Mihailo R. Jovanovic, and Graham V. Candler. 2017. “Study of Trip-Induced Hypersonic Boundary Layer Transition.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-4513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4513
• Shtessel, Y., and D. Krupp. n.d. “Sliding Mode Control of Reusable Launch Vehicle in Launch and Re-Entry Modes.” In Proceedings The Twenty-Ninth Southeastern Symposium on System Theory. IEEE Comput. Soc. Press. https://doi.org/10.1109/ssst.1997.581723
• “Shuttle Eleven Cove Aerodynamic Heating by Ingested Flow.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0027.0048
• “Shuttle Sonic Boom: Technology and Predictions.” 1973. In Aeroacoustics Conference. AIAA 1973-1039. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1039
• “Shuttle Sonic Boom: Technology and Predictions.” 1975. In Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865121.0397.0411
• Shweyk, Kamal, and David Hyde. 2013. “Overview of Aerodynamic Model and Flight Control System of a Speed Agile Concept Demonstrator.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-1101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1101
• Siclari, M., and F. Austin. 1998. “Optimization of a Realistic Flap Design for in-Flight Transonic Performance Enhancement.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-596
• Siclari, M., and C. Darden. 1991. “CFD Prediction of the near-Field Sonic Boom Environment for Two Low Boom HSCT Configurations.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1631
• Siddiqi, Shahid, and J. Abraham. 1988. “Integrated Aircraft Flight Test Approaches for Fault-Tolerant Avionics Systems.” In 4th Flight Test Conference. AIAA 1988-2170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2170
• Siddiqi, Shahid, and Richard Neate. 1986. “The Organization of Flight Testing in an University Environment.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9820
• Siddiqui, Md Shahriar Rahim, Arman Rahmim, and Eldad Haber. 2024. “Deep Optimal Experimental Design for Parameter Estimation Problems.” Physica Scripta 100 (1): 016005. https://doi.org/10.1088/1402-4896/ad88b1
• Sidharth, G. S., and Anubhav Dwivedi. 2026. “Hypersonic Boundary Layer Transition to Turbulence on a Spherical Forebody.” In AIAA SCITECH 2026 Forum. AIAA 2026-1149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1149
• Sidorenko, A., Yu. Gromyko, D. Bountin, P. Polivanov, and A. Maslov. 2015. “Effect of the Local Wall Cooling/heating on the Hypersonic Boundary Layer Stability and Transition.” In Progress in Flight Physics – Volume 7, edited by D. Knight, I. Lipatov, P. Reijasse. EDP Sciences. https://doi.org/10.1051/eucass/201507549
• Siegel, S. 1972. “A Flutter Optimization Program for Aircraft Structural Design.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-795
• Sieker, W. D. 1966. Protuberance Heating Test Program. NASA-CR-128400. NASA. https://ntrs.nasa.gov/citations/19730002232
• Siemers, P., III, H. Wolf, and P. Flanagan. 1983. “Shuttle Entry Air Data System Concepts Applied to Space Shuttle Orbiter Flight Pressure Data to Determine Air Data: STS 1-4.” In 21st Aerospace Sciences Meeting. AIAA 1983-118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-118
• Sigal, A. 1984. “An Experimental Investigation of the Aerodynamic Characteristics of Bodies Having Square Cross-Section at Transonic Speeds.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2091
• Silhouette, Xavier, and Robert Stengel. 1987. “Estimation of the Aerodynamic Coefficients of the Navion Aircraft Athigh Angles of Attack and Sideslip.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2622
• Silva, Murilo Caetano da. n.d.-a. “Prediction of Wing Divergence and Control Reversal Speeds by Means of an Aeroelastic Finite Element.” PhD diss., Universidade de São Paulo. Escola de Engenharia de São Carlos. https://doi.org/10.11606/003273318
• Silva, Marcos Vinícius Teixeira. n.d.-b. “Projeto Conceitual De Uma Aeronave Comercial Em Configuração Blended Wing Body.” PhD diss., Universidade de São Paulo. Escola de Engenharia de São Carlos. https://doi.org/10.11606/003239828
• Silva, Higor. n.d.-c. “Structural and Aeroelastic Design Optimization of Truss-Based Modular Wing Structures.” PhD diss., Universidade Federal de Uberlândia. https://doi.org/10.14393/ufu.te.2022.345
• Silva, Bruno. 2011. “Data Gathering and Preliminary Results of the System Identification of a Flexible Aircraft Model.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6355. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6355
• Silva, Walter A., and Shane Dunn. 2005. “Higher-Order Spectral Analysis of F-18 Flight Flutter Data.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20050176407
• Silva, Maurício G., Victor O. R. Gamarra, and Vitor Koldaev. 2009. “Control of Reynolds Number in a High Speed Wind Tunnel.” Journal of Aerospace Technology and Management 1 (1): 69–77. https://doi.org/10.5028/jatm.2009.01016977
• Silva, Mark, Alan Wadcock, Mark Betzina, Ethan Romander, and Gloria Yamauchi. 2006. “Investigating Tiltrotor Formation Flight via 1/48-Scale Wind Tunnel Experiment.” In Proceedings of the Vertical Flight Society Forum 62 - Phoenix, AZ 2006. The Vertical Flight Society. https://doi.org/10.4050/vfs-f62-222
• Silvers, H. Norman, and Kenneth P. Spreemann. 1947. Wind-Tunnel Tests of a 0.182-Scale Model of an F4U-1 Airplane with External Stores. NACA-RM-SL7E20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090022392
• Silz, Richard. 1992. “An Overview of the F-117A Avionics Flight Test Program.” In Aerospace Design Conference. AIAA 1992-1228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1228
• Sim, A. G. 1973. Flight-Determined Stability and Control Characteristics of the M2-F3 Lifting Body Vehicle. NASA-TN-D-7511. NASA. https://ntrs.nasa.gov/citations/19740004421
• Sim, Alex G. 1976. A Correlation between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft. NASA-SX-3371. NASA. https://ntrs.nasa.gov/citations/20080036216
• Sim, Alex G. 1997. A Correlation between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft. NASA-TM-113084. NASA. https://ntrs.nasa.gov/citations/19970027378
• Sim, A. G., and R. E. Curry. 1978. Flight-Determined Stability and Control Derivatives for the F-111 Tact Research Aircraft. NASA-TP-1350. NASA. https://ntrs.nasa.gov/citations/19790001897
• Sim, A. G., and R. E. Curry. 1984. Flight-Determined Aerodynamic Derivatives of the AD-1 Oblique-Wing Research Airplane. NASA-TP-2222. NASA. https://ntrs.nasa.gov/citations/19870001438
• “Similitude and Dimensional Analysis.” 2000. In Hydraulic Modeling. American Society of Civil Engineers. https://doi.org/10.1061/9780784404157.ch02
• Similitude, Dimensional Analysis and Modelling. 2007. Wiley. https://doi.org/10.1002/9783527611096.ch6
• Simmons, Benjamin M. n.d. “Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft.” In AIAA AVIATION 2022 Forum. https://ntrs.nasa.gov/citations/20220005627
• Simmons, Benjamin M. 2022. “System Identification for eVTOL Aircraft Using Simulated Flight Data.” In AIAA SCITECH 2022 Forum. AIAA 2022-2409. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2409
• Simmons, Benjamin M. 2023a. “Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data.” PhD diss., Langley Research Center. https://ntrs.nasa.gov/citations/20230004001
• Simmons, Benjamin M., and Kasey A. Ackerman. 2026. “System Identification for a Subscale Tiltrotor eVTOL Aircraft from Hover Flight-Test Data.” In AIAA SCITECH 2026 Forum. AIAA 2026-2088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2088
• Simmons, Benjamin M., Kasey A. Ackerman, and Garrett D. Asper. n.d.-a. “Aero-Propulsive Damping Characterization for eVTOL Aircraft Using Free Motion Wind-Tunnel Testing.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20240014699
• Simmons, Benjamin M., Kasey A. Ackerman, Garrett D. Asper, et al. n.d.-c. “Subscale Tiltrotor eVTOL Aircraft Dynamic Modeling and Flight Control Software Development.” In The Vertical Flight Society’s 81st Annual Forum & Technology Display. https://ntrs.nasa.gov/citations/20250003662
• Simmons, J. M., J. W. Benson, and J. P. Fiedler. 1969. “A Hybrid Frequency Response Technique and Its Application to Aircraft Flight Flutter Testing.” In Proceedings of the November 18-20, 1969, fall joint computer conference on - AFIPS ‘69 (Fall). ACM Press. https://doi.org/10.1145/1478559.1478655
• Simmons, Benjamin M., Pieter G. Buning, and Patrick C. Murphy. n.d.-b. “Full-Envelope Aero-Propulsive Model Identification for Lift+Cruise Aircraft Using Computational Experiments.” In 2021 AIAA AVIATION Forum. https://ntrs.nasa.gov/citations/20210017459
• Simmons, Benjamin M., Andrew J. Lofthouse, and Dan D. Vicroy. n.d.-d. “Summary of the Second AIAA Stability and Control Prediction Workshop.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20250010706
• Simmons, Benjamin M., and Patrick C. Murphy. n.d. “Wind Tunnel-Based Aerodynamic Model Identification for a Tilt-Wing, Distributed Electric Propulsion Aircraft.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20205010555
• Simmons, Benjamin M., and Patrick C. Murphy. 2021. “Wind Tunnel-Based Aerodynamic Model Identification for a Tilt-Wing, Distributed Electric Propulsion Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-1298. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1298
• Simmons, Benjamin, Andrew Rapsomanikis, George Jacobellis, Nk Ofodile, Thomas Hamilton, and Max Ma. 2025a. “Flight-Test System Identification Methodology and Hover Results for a Vectored-Thrust eVTOL Aircraft.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0220
• Simmons, Gray, Cristina Riso, Carlos Cesnik, and Jasmine Chang. 2025b. “Influence of Wing-Propeller Aerodynamic Interactions on Aeroelastic Damping.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-0208
• Simon, Duane R., and Jimmie C. Savage. 1975a. “Army Preliminary Evaluation of the HLH ATC Demonstrator Fly-By-Wire Flight Control System.” In Proceedings of the Vertical Flight Society Forum 31 - Washington, D.C. 1975. The Vertical Flight Society. https://doi.org/10.4050/vfs-f31-036
• Simon, Duane R., and Jimmie C. Savage. 1975b. Flight Test of the Aerospatiale SA-342 Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ada016921
• Simons, Girard A. 1975. Advanced Reentry Aeromechanics. Volume II. Aerodynamic Shattering of Ice Crystals in Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada019517
• Simpson, W. 1972. “The Development of Dynamic Flight Test Techniques for the Extraction of Aircraft Performance.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-785
• Simpson, William R. 1979. The Accelerometer Methods of Obtaining Aircraft Performance from Flight Test Data (Dynamic Performance Testing). Defense Technical Information Center. https://doi.org/10.21236/ada075226
• Simpson, Andrew, Suzanne Smith, and Jamey Jacob. 2007. “Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1069
• Sims, R., and A. Carter. 1981. “Comparison of Wind Tunnel and Theoretical Aeroelastic Predictions with Flight Measured Airloads for the B-1 Aircraft.” In 1st Flight Test Conference. AIAA 1981-2387. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2387
• Sims, J., and Ralph Kimberlin. 1995. “Use of Variable Stability Demonstrators to Enhance Aerospace and Flight Test Engineer Training.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3938
• Simsek, Orkun, and Ozan Tekinalp. 2015. “System Identification and Handling Quality Analysis of a UAV from Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-1480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1480
• “Simulating Flight Condition of Hfssb on Ground.” 2015. In Icrbit: 2015. ELK ASIA PACIFIC JOURNAL. https://doi.org/10.16962/elkapj/si.it.icrbit-2015.35
• “Simulation in Support of Flight Test: In Retrospect.” 1988. In 4th Flight Test Conference. AIAA 1988-2130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2130
• Singh, Yogendra, Manoj Kumar K. Devaraj, S. N. Omkar, and Gopalan Jagadeesh. 2017. “Optimization of Hypersonic Power Law Derived Waverider Using TLBO.” In 30th International Symposium on Shock Waves 1. Springer International Publishing. https://doi.org/10.1007/978-3-319-46213-4_26
• Singh, Sanjay, and Ajoy Ghosh. 2006. “Parameter Estimation from Flight Data of a Missile Using Maximum Likelihood and Neural Network Method.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6284
• Singh, S., and A. K. Ghosh. 2023. “Longitudinal Parameter Estimation Using Wind Tunnel and Simulated Flight Data of Missile Configuration.” Journal of Aerospace Sciences and Technologies: 102–20. https://doi.org/10.61653/joast.v59i2.2007.567
• Singh, Sunayna, Briek Luyten, and Marco Sagliano. 2024. “Relative Navigation for the ‘in-Air Capturing’ of a Winged Reusable Launch Vehicle.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4674857/v1
• Singh, Kumar V., and Laura A. McDonough. 2014. “Optimization of Control Surface Parameters with Augmented Flutter Boundary Constraints.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2050. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2050
• Singh, Jatinder, Jitendra Raol, and Kumar Basappa. 2005. “Modeling and Parameter Estimation for a Fly-by-Wire Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-5924. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5924
• Singh, Amarjit, and J. Stollery. 1995. “Experimental Investigation of Hypersonic Flow over a Wing-Body Combination.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6083
• Sinha, Pakhee. 2026. “Performance Analysis of a Blended Wing Body Aircraft Utilizing Hybrid-Electric Distributed Propulsion and Boundary Layer Ingestion.” Preprint, . https://doi.org/10.31224/7339
• Sisk, Thomas R., and Duane O. Muhleman. 1955. Lateral Stability and Control Characteristics of the Convair XF-92A Delta-Wing Airplane as Measured in Flight. NACA-RM-H55A17. NASA. https://ntrs.nasa.gov/citations/19930088671
• Sitz, Joel R. 1992. “The F-18 Systems Research Aircraft Facility.” In 1992 Aerotech Conference. https://ntrs.nasa.gov/citations/19930007564
• Sivan, K., and S. Pandian. 2018. “An Overview of Reusable Launch Vehicle Technology Demonstrator.” Current Science 114 (01): 38. https://doi.org/10.18520/cs/v114/i01/38-47
• Sivanandi, Periyasamy, Chirag Gupta, and Hari Durai. 2022. “Periyasamy Et Al. Advances in Aerodynamics CFD and XFLR5 Analysis of an Active Aeroelastic Wing.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2263166/v1
• Sivells, J. 1969. “Aerodynamic Design of Axisymmetric Hypersonic Wind Tunnel Nozzles.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-337
• Sivia, D. S. 2006. “Experimental Design.” In Data Analysis. Oxford University PressOxford. https://doi.org/10.1093/oso/9780198568315.003.0007
• Sjoberg, S. A., and R. A. Champine. 1949. Preliminary Flight Measurements of the Static Longitudinal Stability and Stalling Characteristics of the Douglas D-558-II Research Airplane (BuAero No. 37974). NACA-RM-L9H31a. NASA. https://ntrs.nasa.gov/citations/19930085989
• Skelly, Thomas. 1989. “Recoverable Test Vehicle, an Innovative Approach to a Low Cost Composite Airframe for Aerospace Application.” In 27th Aerospace Sciences Meeting. AIAA 1989-378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-378
• Skillen, Michael, and William Crossley. 2008. “Conceptual Morphing Aircraft Sizing Using a Multi-Level Optimization Strategy.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-166
• Skujins, Torstens, and Carlos Cesnik. 2011. “On the Applicability of an Unsteady Aerodynamic ROM to the Transonic Flight Regime.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6525. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6525
• Sleesongsom, Suwin, and Sujin Bureerat. 2011. “Effect of Actuating Forces on Aeroelastic Characteristics of a Morphing Aircraft Wing.” Applied Mechanics and Materials 52-54: 308–17. https://doi.org/10.4028/www.scientific.net/amm.52-54.308
• “Slender Aircraft for Flight at Subsonic Speeds over Short Ranges.” 2012. In The Aerodynamic Design of Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600869228.0439.0447
• “Slender Wings at High Angles of Attack in Hypersonic Flows.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0321.0343
• Sliwa, S. 1979. “Some Flight Data Extraction Techniques Used on a General Aviation Spin Research Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1979-1802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1802
• Sloan Jr. and E. H. M. W. Davis. 1962. Feasibility of a Diffuser Centerbody Injector for the 16-FOOT Supersonic Tunnel of the Propulsion Wind Tunnel Facility. Defense Technical Information Center. https://doi.org/10.21236/ad0274219
• Slooff, J. W. 1986. “Aircraft Drag Prediction and Reduction. Addendum 1: Computational Drag Analyses and Minimization; Mission Impossible?” In von Karman Inst.. https://ntrs.nasa.gov/citations/19860017715
• Smayda, Michael. n.d. “Test Program for a Dual-Mode Scramjet.” PhD diss., University of Virginia. https://doi.org/10.18130/v3dr44
• Smayda, Michael, and Christopher Goyne. 2011. “Dispersion Reduction for a Sounding Rocket Scramjet Flight Experiment.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2324
• Smeltzer, D., R. Smith, and R. Cubbison. 1974. “Wind Tunnel and Flight Performance of the YF-12 Inlet System.” In 8th Aerodynamic Testing Conference. AIAA 1974-621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-621
• Smetana, F. O., and S. R. Fox. 1979. Flight Test Evaluation of Predicted Light Aircraft Drag, Performance, and Stability. NASA-CR-159062. NASA. https://ntrs.nasa.gov/citations/19810018540
• Smit, Benjamin, and Adam Gorrell. 2026. “Supersonic Ballistic Trajectory Error Analysis for High Powered Rocket Systems.” In 2026 Regional Student Conferences. AIAA 2026-107627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-107627
• Smith, Turner L. 1953. Balance System for the Aberdeen 13 x 15” Supersonic Wind Tunnel”. Defense Technical Information Center. https://doi.org/10.21236/ad0007625
• Smith, H. J. 1965. Evaluation of the Lateral-Directional Stability and Control Characteristics of the Lightweight m2-f1 Lifting Body at Low Speeds. NASA-TN-D-3022. NASA. https://ntrs.nasa.gov/citations/19650024238
• Smith, H. J. 1966. Human Describing Functions Measured in Flight and on Simulators. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19670006542
• Smith, H. J. 1967. Human Describing Functions Measured in Flight and on Simulators. NASA. https://ntrs.nasa.gov/citations/19680039690
• Smith, C. R. 1968. Hot Cycle Rotor/wing Composite Research Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0684315
• Smith, H. C. 1974. Effect of the Six Engine Air Breathing Propulsion System on Space Shuttle Orbiter Subsonic and Transonic Stability and Control Characteristics (OA91). NASA-CR-134088. NASA. https://ntrs.nasa.gov/citations/19740013410
• Smith, H. J. 1975. Flight-Determined Stability and Control Derivatives for an Executive Jet Transport. NASA-TM-X-56034. NASA. https://ntrs.nasa.gov/citations/19760004017
• Smith, Stephen B. 1977. Limited Flight Evaluation of Side Stick Controller Force-Deflection Characteristics on Aircraft Handling Qualities. Defense Technical Information Center. https://doi.org/10.21236/ada069198
• Smith, R. 1978. “Antecedents and Analogues: Experimental Aircraft.” In Diamond jubilee of powered flight: The evolution of aircraft design; Proceedings of the Conference. AIAA 1978-3008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-3008
• Smith, P. R. 1991. “Aircraft Flight Control System Design Concepts.” Measurement and Control 24 (3): 73–77. https://doi.org/10.1177/002029409102400303
• Smith, Robert E. 1995. “Rapid Airplane Parametric Input Design (RAPID).” In NASA. Lewis Research Center, Surface Modeling, Grid Generation, and Related Issues in Computational Fluid Dynamic (CFD) Solutions. https://ntrs.nasa.gov/citations/19950022309
• Smith, T. 1996. “The Use of in Flight Analysis Techniques for Model Validation on Advanced Combat Aircraft.” In Test and Evalution International Aerospace Forum. AIAA 1996-3355. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3355
• Smith, Stephen C. 1997. “Trefftz-Plane Drag Minimization at Transonic Speeds.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/971478
• Smith, L. A., and J. B. Adcock. 1986. Effect of Reynolds Number and Mach Number on Flow Angularity Probe Sensitivity. NASA-TM-87750. NASA. https://ntrs.nasa.gov/citations/19860020302
• Smith, J. H., G. M. Allen, and D. Vensel. 1973. Design, Fabrication, and Flight Test of the Active Arm External Load Stabilization System for Cargo Handling Helicopters. Defense Technical Information Center. https://doi.org/10.21236/ad0773025
• Smith, Robert E., Malcolm I. G. Bloor, Michael J. Wilson, and Almuttil M. Thomas. 2004. Rapid Airplane Parametric Input Design(RAPID). AIAA Paper 95-1687. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040111295
• Smith, Thomas, Kevin Bowcutt, John Selmon, et al. 2011. “HIFiRE 4: A Low-Cost Aerodynamics, Stability, and Control Hypersonic Flight Experiment.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2275
• Smith, Kenneth, Jeffrey Butt, Michael von Spakovsky, and David Moorhouse. 2007. “A Study of the Benefits of Using Morphing Wing Technology in Fighter Aircraft Systems.” In 39th AIAA Thermophysics Conference. AIAA 2007-4616. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4616
• Smith, S., S. Cliff, and I. Kroo. 1987. “The Design of a Joined Wing Flight Demonstrator Aircraft.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2930
• Smith, G. A., J. M. Hammer, and R. E. Rose. 1971. Conceptual Study to Apply Advanced Flight Control Technology to the Coin or Trim Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0730571
• Smith, Andrew, and Phil Harrison. 2010. Ares I-X Launch Abort System, Crew Module, and Upper Stage Simulator Vibroacoustic Flight Data Evaluation, Comparison to Predictions, and Recommendations for Adjustments to Prediction Methodology and Assumptions. M10-0477. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20100025979
• Smith, Nathanial T., James T. Heineck, and Edward T. Schairer. 2017. “Optical Flow for Flight and Wind Tunnel Background Oriented Schlieren Imaging.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20180002139
• Smith, Mark, Timothy Moes, and Eugene Morelli. 2003. “Real-Time Stability and Control Derivative Extraction from F-15 Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5701
• Smith, L., and E. Ramirez. 1986. “Air Force Flight Test Center Range Overview.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9748
• Smith, O. E., J. R. Redus, J. A. Forney, and M. J. Dash. 1972. Effects of Atmospheric Models on Space Shuttle Trajectories and Aerodynamic Heating. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19720045147
• Smith, Theodore, Joseph Schetz, and Trong Bui. 2002a. “Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests.” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3134
• Smith, John P., Lawrence J. Schilling, and Charles A. Wagner. 1989. “Simulation at Dryden Flight Research Facility from 1957 to 1982.” In SES/SFTE Simulation-Aircraft Test and Evaluation Symposium. https://ntrs.nasa.gov/citations/19890011612
• Smith, Russell W., Joseph G. Sikora, and Michael C. Lindell. 2005. Test and Analysis of a Hyper-X Carbon-Carbon Leading Edge Chine. NASA/TM-2005-213765. NASA. https://ntrs.nasa.gov/citations/20050186551
• Smith, Terry, and Terry Smith. 1997. “Flight Testing a Modern Flight Control System.” In 1997 World Aviation Congress. AIAA 1997-5520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-5520
• Smith, Theodore, Greg Walker, and Joseph Schetz. 2002b. “Development and Ground Testing of Heat Flux Gages for High Enthalpy Supersonic Flight Tests.” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3133
• Smith, Raymond B., George M. Yamakawa, John R. Niemann, Joseph C. Watts, and Jerry R. Guin. 1979. Airworthiness and Flight Characteristics Test, OV-1C Takeoff Performance. Defense Technical Information Center. https://doi.org/10.21236/ada069827
• Smith, Charles C., Jr. 1958. Hovering and Transition Flight Tests of a 1/5-Scale Model of a Jet-Powered Vertical-Attitude VTOL Research Airplane. NASA-MEMO-1-10-27-58L. NASA. https://ntrs.nasa.gov/citations/19980227972
• Smith, Charles C., Jr. 1961. Hovering and Transition Flight Tests of a 1/5-Scale Model of a Jet-Powered Vertical-Attitude VTOL Research Airplane. NASA-TN-D-404. NASA. https://ntrs.nasa.gov/citations/19980230621
• Smith-Velazquez, Laura M., and Erik Theunissen. 2018. “Real-Time Sonic Boom Prediction with Flight Guidance.” In Degraded Environments: Sensing, Processing, and Display 2018, edited by John (Jack) N. Sanders-Reed, Jarvis (Trey) J. Arthur. SPIE. https://doi.org/10.1117/12.2304853
• Sneddon, Joshua, Fintan Healy, Mark H. Lowenberg, and Jonathan E. Cooper. 2026. “Testing of Active Flutter Suppression for Wings Incorporating Floating Wingtips.” In AIAA SCITECH 2026 Forum. AIAA 2026-1060. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1060
• Snyder, Thomas L. 1947a. Estimation of the Spin and Recovery Characteristics of the North American XSN2J-1 Airplane. NACA-RM-L7F23b. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019393
• Snyder, Thomas L. 1947b. Free-Spinning-Tunnel Tests of a 1/35-Scale Model of the Douglas XB-43 Airplane. NACA-RM-L7G01. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019397
• Snyder, Christopher. 2020. “More / All Electric Vertical Take-Off and Landing (VTOL) Vehicle Sensitivities to Propulsion and Power Performance.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16447
• Snyder, W. J., and M. B. Schoultz. 1976. “Civil Helicopter Flight Research.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19760062417
• Soares, Fola. 2007a. “A Flight Test Demonstration of on-Line Neural Network Applications in Advanced Aircraft Flight Control System.” In AIAA Infotech@Aerospace 2007 Conference and Exhibit. AIAA 2007-2942. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2942
• Soares, Fola. 2007b. “Neural Network Applications in Advanced Aircraft Flight Control System, a Hybrid System, a Flight Test Demonstration.” In AIAA Infotech@Aerospace 2007 Conference and Exhibit. AIAA 2007-2943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2943
• Sóbester, András. 2010. Propulsion Integration: Supersonic Transport Aircraft. Wiley. https://doi.org/10.1002/9780470686652.eae489
• Sobieczky, H. 1984. “Supercritical Airfoil and Wing Design.” Annual Review of Fluid Mechanics 16 (1): 337–63. https://doi.org/10.1146/annurev.fluid.16.1.337
• Sobieczky, H., and F. Dougherty. 1991. “Interactive Design of Hypersonic Waverider Geometries.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1697. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1697
• Softley, E. 1969. “Boundary Layer Transition on Hypersonic Blunt, Slender Cones.” In 2nd Fluid and Plasma Dynamics Conference. AIAA 1969-705. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-705
• Soikkeli, Johannes S., Drago Matko, and Thomas Koopman. 2023. “Cascaded Nonlinear Dynamic Inversion Applied to a Fixed-Wing Distributed Electric Propulsion Aircraft.” In AIAA AVIATION 2023 Forum. AIAA 2023-4048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4048
• Soistmann, David, and Charles Spain. 1993. “An Experimental and Analytical Study of a Lifting-Body Wind-Tunnel Model Exhibiting Body-Freedom Flutter.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1316
• Solano, Heriberto D., Darshan Sarojini, and Dimitri N. Mavris. 2023. “Computationally Efficient Analysis and Sizing of the PEGASUS and Truss-Braced Wing Structures Subjected to Dynamic Loads.” In AIAA AVIATION 2023 Forum. AIAA 2023-3943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3943
• “Solid Rocket Motor Plume and Ablation Study.” 1979. In Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865381.0265.0277
• Solies, U. 1992. “Effects of Thrust Line Offset on Neutral Point Determination in Stability Flight Testing.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4082. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4082
• Somers, Dan M. 1992. “Subsonic Natural-Laminar-Flow Airfoils.” In ICASE/NASA LaRC Series. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1_4
• Son, Jiwon, Hyosang Ko, Han-Lim Choi, and Kwanjung Yee. 2024a. “Refined Mode Classification and Performance Analysis Method of Dual-Mode Scramjet Vehicles for Flight Trajectory Optimization.” Preprint, . https://doi.org/10.2139/ssrn.4795428
• Son, Jiwon, Hyosang Ko, Hanlim Choi, and Kwanjung Yee. 2024b. “Trajectory Optimization of Dual Mode Scramjet Engine Vehicle Using a Refined Quasi One-Dimensional Combustion Model.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3892. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3892
• Song, Hongqing. 2018. “Similitude and Dimensional Analysis.” In Engineering Fluid Mechanics. Springer Singapore. https://doi.org/10.1007/978-981-13-0173-5_8
• Song, Jinsheng, Ziqiao Chen, Dong Wang, and Xin Wen. 2024. “A Data-Driven Hybrid Sensor Fault Detection/diagnosis Method with Flight Test Data.” Measurement Science and Technology 35 (7): 076109. https://doi.org/10.1088/1361-6501/ad3976
• “Sonic Boom.” 2012. Physics World 25 (11): 51–51. https://doi.org/10.1088/2058-7058/25/11/42
• “Sonic Boom Analysis for High-Altitude Flight at High Mach Number.” 1975. In Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865121.0301.0320
• Sonneveldt, Bryan S., Ian G. Clark, and Clara O’Farrell. 2019. “Summary of the Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) Sounding Rocket Tests with a Disk-Gap-Band Parachute.” In AIAA Aviation 2019 Forum. AIAA 2019-3482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3482
• Sopher, Robert, and S. B. R. Kottapalli. 1982. “Correlation of Predicted Vibrations and Test Data for a Wind Tunnel Helicopter Model.” In Proceedings of the Vertical Flight Society Forum 38 - Anaheim, CA 1982. The Vertical Flight Society. https://doi.org/10.4050/vfs-f38-010
• Sorensen, J. A. 1972. Analysis of Instrumentation Error Effects on the Identification Accuracy of Aircraft Parameters. NASA-CR-112121. NASA. https://ntrs.nasa.gov/citations/19720024390
• Sorensen, Peter Nicholas, Patrick Laverty, and Daniel R. Cuppoletti. 2025. “Semi-Empirical Acoustic Noise Estimation for Distributed Electric Propulsion Systems.” Preprint, . https://doi.org/10.2139/ssrn.5304795
• Sorensen, J. A., R. L. Mohr, and T. B. Cline. 1975. Instrumentation Requirements for Aircraft Parameter Identification with Application to the Helicopter. NASA-CR-132675. NASA. https://ntrs.nasa.gov/citations/19750024039
• Sorensen, J., J. Tyler Jr., and J. Powell. 1972. “Evaluation of Flight Instrumentation for the Identification of Stability and Control Derivatives.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-963
• Sorenson, Lloyd R. 1971. “Edwin P. Hartman. Adventures in Research: A History of Ames Research Center, 1940–1965. (NASA SP-4302. NASA Center History Series.) Washington: Scientific and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration. 1970. Pp. Xviii, 555. $4.75.” American Historical Review 76 (4): 1239–1239. https://doi.org/10.1086/ahr/76.4.1239
• Sotoudeh, Zahra, and Anthony Ferman. 2019. “Aeroelastic Analysis of a Composite Pre-Twisted Wing for Minimum Induced Drag.” In AIAA Scitech 2019 Forum. AIAA 2019-0762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0762
• Sotoudeh, Zahra, and Nathan S. Hosking. 2018. “Comprehensive Aeroelastic Analysis of a Smart Composite Wing.” In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2018-1203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1203
• Soudakov, Georgiy Grigoryevich. 2016. “Calculation of Aircraft Drag Components in a Transonic Flow Described by Reynolds-Averaged Navier-Stokes Equations.” TsAGI Science Journal 47 (1): 1–13. https://doi.org/10.1615/tsagiscij.2016017055
• Soule, Hartley A. 1931. The Effect of Slots and Flaps on the Lift and Drag of the Mcdonnell Airplanes Determined in Flight. NACA-TN-398. NASA. https://ntrs.nasa.gov/citations/19930081163
• Soule, V. A. 1973. V/STOL Tilt Rotor Aircraft Study. Volume 5: Definition of Stowed Rotor Research Aircraft. NASA-CR-114598. NASA. https://ntrs.nasa.gov/citations/19730021277
• Soule, H. A., and W. Gracey. 1938. Improvement of Aileron Effectiveness by the Prevention of Air Leakage through the Hinge Gap as Determined in Flight. NACA-TN-632. NASA. https://ntrs.nasa.gov/citations/19930081459
• Soule, Hartley A., and J. W. Wetmore. 1933. The Effects of Slots and Flaps on Lateral Control of a Low-Wing Monoplane as Determined in Flight. NACA-TN-478. NASA. https://ntrs.nasa.gov/citations/19930081319
• Soule, Hartley A., and John B. Wheatley. 1934. A Comparison between the Theoretical and Measured Longitudinal Stability Characteristics of an Airplane. NACA-TR-442. NASA. https://ntrs.nasa.gov/citations/19930091516
• South, D. 1974. “Real-Time Optimal Guidance of Lifting Re-Entry Vehicles.” In Mechanics and Control of Flight Conference. AIAA 1974-928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-928
• Southerland, Louis C., Davis Platus, and Robin Shepherd. 1986. Detailed Research Plans for a Study of Aircraft Noise and Sonic Boom Effects and Measurements. Volume VI: Effects of Sonic Boom and Low Frequency Noise on Structures and Terrain. Defense Technical Information Center. https://doi.org/10.21236/ada401387
• Soykasap, Omer, and Dewey Hodges. 1999. “Performance Enhancement of a Composite Tilt-Rotor Using Aeroelastic Tailoring.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1475
• “Space Shuttle Laminar Heating with Finite-Rate Catalytic Recombination.” 1982. In Thermophysics of Atmospheric Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865565.0273.0289
• Space Vehicle Sa-6 Telemetry System. 1965. NASA-TM-X-53284. NASA. https://ntrs.nasa.gov/citations/19650021022
• “SpaceShipOne: An Illustrated History.” 2008. Aircraft Engineering and Aerospace Technology 80 (5). https://doi.org/10.1108/aeat.2008.12780eae.001
• Spacht, G. 1980. “The Forward Swept Wing: A Unique Design Challenge.” In Aircraft Systems Meeting. AIAA 1980-1885. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1885
• Spacht, G. 1983. “X-29 Integrated Technology Demonstrator and ATF.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1058
• Spahr, J. Richard. 1947. Lateral-Control Characteristics of Various Spoiler Arrangements as Measured in Flight. NACA-TN-1123. NASA. https://ntrs.nasa.gov/citations/19930081791
• Spaid, F. 1964. “Secondary Injection of Gases into a Supersonic Flow.” In Solid Propellant Rocket Conference. AIAA 1964-110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-110
• Spaid, F. 1979. “Supercritical Airfoil Boundary-Layer Measurements.” In 12th Fluid and Plasma Dynamics Conference. AIAA 1979-1501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1501
• Spain, Charles V., Thomas A. Zeiler, Michael D. Gibbons, et al. 1993. “Aeroelastic Character of a National Aerospace Plane Demonstrator Concept.” In In: AIAA(ASME)ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pt. 1 (A93-33876 1. https://ntrs.nasa.gov/citations/19930049893
• Spanos, Theodoros A. 2009. “Boundary Layer Transition Flight Experiment Implementation on OV-103.” In Kennedy Engineering Academy. https://ntrs.nasa.gov/citations/20110008506
• Sparrow, Victor W. 2010. Sonic Boom. Wiley. https://doi.org/10.1002/9780470686652.eae342
• Spearman, M. L. 1981. “Historical Trend in the Research and Development of Aircraft.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19810059530
• Spearman, M. 1985a. “The Application of Some Lifting-Body Reentry Concepts to Missile Design.” In 23rd Aerospace Sciences Meeting. AIAA 1985-497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-497
• Spearman, M. 1985b. “Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack up to 90 Deg.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1795
• Spearman, Leroy. 2003. “NACA/NASA Aerodynamic Research in the 20th Century.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-287. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-287
• Spearman, M. Leroy. 2004. “High-Speed Aerodynamic Research at the NACA/NASA Langley Research Center.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-107
• Spearman, M. Leroy. 2005. “Lessons Learned in the High-Speed Aerodynamic Research Programs of the NACA/NASA.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-327
• Spearman, M. Leroy. 2009. “Significant Aerodynamic Research at NACA/NASA Langley during the First Century of Flight.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-966
• Spearman, M. 2012. “Some NACA/NASA Aerodynamic Research Related to Security and Defense.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-957. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-957
• Spearman, M. L., and C. Driver. 1980. “Supersonic Flight: Past, Present, and Future.” AIAA Student Journal 18. https://ntrs.nasa.gov/citations/19800052274
• Spearman, M., and R. Fournier. 1978. “Supersonic Aerodynamic Characteristics of a Tail-Control Cruciform Maneuverable Missile with and without Wings.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1351
• Spearman, M., R. Fournier, and M. Lamb. 1977. “Aerodynamic Characteristics of Supersonic Fighter Airplane Configurations Based on Soviet Design Concepts.” In Guidance and Control Conference. AIAA 1977-1162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1162
• Spencer, Robert B. 1999. “The Reusable First Stage (RFS) Vehicle-an Enabler for Future Launch Systems.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57511
• Spiegel, J., F. Wolf, and D. Zeh. 1968. “Simulation of Venus Atmospheric Entry by Earth Re-Entry.” In Entry Vehicle Systems and Technology Meeting. AIAA 1968-1148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1148
• Spitzer, R. E. 1972. Predicted Flight Characteristics of the Augmentor Wing Jet STOL Research Aircraft. NASA-CR-114463. NASA. https://ntrs.nasa.gov/citations/19720020367
• Spitzer, R., P. Rumsey, and H. Quigley. 1972. “Use of the Flight Simulator in the Design of a STOL Research Aircraft.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-762
• Spivey, Natalie, Rachel Saltzman, Carol Wieseman, Kevin Napolitano, and Benjamin Smith. 2020. “Passive Aeroelastic Tailored Wing Modal Test Using the Fixed Base Correction Method.” In Conference and Exposition on Structural Dynamics: IT’S NOT JUST MODAL ANYMORE. https://ntrs.nasa.gov/citations/20200001757
• Spivey, Natalie Dawn, Samson Truong, and Roger Truax. n.d. “All-Electric X-Plane, X-57 Mod II Ground Vibration Test.” In IMAC 39. https://ntrs.nasa.gov/citations/20205006955
• Spivey, Natalie Dawn, Samson Siu Truong, and Roger Truax. 2021. “NASA’s All-Electric X-Plane X-57 Mod II Ground Vibration Test.” In IMAC 39. https://ntrs.nasa.gov/citations/20205011681
• Spravka, John J., and Timothy R. Jorris. 2015a. Current Hypersonic and Space Vehicle Flight Test and Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ada619521
• Spravka, John J., and Timothy R. Jorris. 2015b. “Current Hypersonic and Space Vehicle Flight Test Instrumentation Challenges.” In AIAA Flight Testing Conference. AIAA 2015-3224. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3224
• Spreiter, John R., and Paul J. Steffen. 1946. “An NACA Flight and Wind Tunnel Investigation of Maximum Lift as Affected by Variations of Mach and Reynolds Numbers.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/460118
• Springer, Anthony. 1994. “The George C. Marshall Space Flight Center’s 14 x 14-Inch Trisonic Wind Tunnel: A Historical Perspective.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-539
• Springer, Anthony M. 1998. Comparison of the Aerodynamic Characteristics of Similar Models in Two Size Wind Tunnels at Transonic Speeds. NASA/TM-1998-208264. NASA. https://ntrs.nasa.gov/citations/19980210402
• Spurlin, C., and H. Lueck. 1984. “Comparison of Flight and Wind Tunnel Data on the Dornier TST Configuration.” In 13th Aerodynamic Testing Conference. AIAA 1984-612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-612
• Squire, L. C., and S. H. Nasser. 1993. “Cavity Drag at Transonic Speeds.” Aeronautical Journal 97 (967): 247–56. https://doi.org/10.1017/s000192400002635x
• Squires, Patrick, and William Warmbrodt. 1983. “Correlation of Full-Scale and Small-Scale Wind-Tunnel Tests of a Helicopter Fuselage.” In Applied Aerodynamics Conference. AIAA 1983-1786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1786
• Sragow, Michael. 2013. “Test Pilot.” In Victor Fleming. University Press of Kentucky. https://doi.org/10.5810/kentucky/9780813144412.003.0020
• Srijayantha, M. 1983. “Data Acquisition for Stall/spin Flight Research.” In NASA. Langley Research Center Joint Univ. Program for Air Transportation Res.. https://ntrs.nasa.gov/citations/19840003043
• Srinathkumar, S., and W. Adams Jr. 1989. “Active Flutter Suppression Using Invariant Zeros/eigensystem Assignment.” In Guidance, Navigation and Control Conference. AIAA 1989-3610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3610
• Srinathkumar, S., V. Parameswaran, and J. Raol. 1995. “Flight Test Determination of Neutral and Maneuver Points of Aircraft.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3501
• Srinivasan, G., and R. Chamberlain. 2004. “Drag Reduction of Spiked Missile by Heat Addition.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4714
• St. John, Clinton W., and Michael Alan Frederick. 2013. “Flight Test Results of an Axisymmetric Channeled Center Body Supersonic Inlet at off-Design Conditions.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140000927
• “Stability and Control.” 2009. In Flight Physics. Springer Netherlands. https://doi.org/10.1007/978-1-4020-8664-9_7
• Stadler, R. 1993. “Lifting-Body Reentry Vehicle.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5102
• Stahara, S. S., and J. R. Spreiter. 1979. A Transonic Wind Tunnel Interference Assessment: Axisymmetric Flows. Defense Technical Information Center. https://doi.org/10.21236/ada068767
• Stahl, Joseph W., Joseph A. Arena, and Mark I. Knapp. 1984. Cost-Estimating Relationships for Tactical Combat Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada151575
• Stalcup, Erik J., and Nic Heersema. 2023. “Thermal Requirements for Design and Analysis of Subsonic Single Aft Engine (SUSAN) Research Aircraft.” In AIAA Science and Technology (SciTech) Forum and Exposition 2023. https://ntrs.nasa.gov/citations/20220018486
• Staley, James A. 1976. Validation of Rotorcraft Flight Simulation Program through Correlation with Flight Data for Soft-in-Plane Hingeless Rotors. Defense Technical Information Center. https://doi.org/10.21236/ada021176
• Stalford, Harold L. 1979. Application of the Estimation-Before-Modeling (EBM) System Identification Method to the High Angle of Attack/Sideslip Flight of the T-2C Jet Trainer Aircraft. Volume 1. Executive Summary. Defense Technical Information Center. https://doi.org/10.21236/ada080025
• Stalla, Felix, Gertjan Looye, Manuel Pusch, and Spilios Theodoulis. 2026. “Integrating Aeroelastic and Primary Flight Control: Robust Design and Wind Tunnel Demonstration.” In AIAA SCITECH 2026 Forum. AIAA 2026-1557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1557
• Stallings, D. W. 1981. Wind Tunnel Tests of Elevon Gap Heating on the Space Shuttle Orbiter (OH-107). Defense Technical Information Center. https://doi.org/10.21236/ada107287
• Stallings, D. W., and A. S. Hartman. 1981. Wind Tunnel Testing of a Windshield Material for Supersonic Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada103383
• Stallings, R. L., Jr., and M. Lamb. 1980. Wind-Tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3. NASA-TP-1789. NASA. https://ntrs.nasa.gov/citations/19810006460
• Stanewsky, E., and P. Freimuth. 1989. “Comparison of Conventional and Adaptive Wall Wind Tunnel Results with Regard to Reynolds Number Effects.” In NASA, Langley Research Center, CAST-10-2(DOA 2 Airfoil Studies Workshop Results. https://ntrs.nasa.gov/citations/19900008333
• Stanford, Bret. 2016. “Static and Dynamic Aeroelastic Tailoring with Variable Camber Control.” In 15th Dynamics Specialists Conference. AIAA 2016-1097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1097
• Stange, Robert A. 1959. Flight Test Rotary Wing Manual. Defense Technical Information Center. https://doi.org/10.21236/ada955359
• Staniszewski, Edgar. 1999. “Semi-Reusable Launch Vehicle: A Next Step for Europe?” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4826
• Stansbery, Eugene G., Daniel G. Baize, and Domenic, J. Maglieri. 1999. “In-Flight Technique for Acquiring Mid- and Far-Field Sonic Boom Signatures.” In High-Speed Research: 1994 Sonic Boom Workshop. Configuration, Design, Analysis and Testing. https://ntrs.nasa.gov/citations/20000027454
• Stargill, S. 1983. “Transonic Wind Tunnel Test on an Oscillating Flap.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2132
• Starkey, Ryan. 2005. “Design and Optimization of Waverider Based Re-Entry Vehicles.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3390
• Starkey, Ryan, Brian Argrow, and Zachary Krevor. 2012. “Design and Flight Testing of a 15% Dynamically Scaled HL-20 Vehicle Model.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-1048
• Starkey, Ryan P., Matthew S. Cannella, John Brendel, and Steve M. Harrington. 2014. “Development of a Pistonless Rocket Engine Pump Suborbital Flight Test Demonstrator.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3784
• Starkey, Ryan, Falcon Rankins, and Darryll Pines. 2005. “Coupled Waverider/Trajectory Optimization for Hypersonic Cruise.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-530
• Starkey, Ryan, Falcon Rankins, and Darryll Pines. 2006. “Effects of Hypersonic Cruise Trajectory Optimization Coupled with Airbreathing Vehicle Design.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-337
• Starr, R., and C. Schueler. 1973. “Experimental Studies of a Ludwieg Tube High Reynolds Number Transonic Tunnel.” In 11th Aerospace Sciences Meeting. AIAA 1973-212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-212
• Starr, R., and M. Varner. 1976a. “Experimental and Theoretical Observations on the Drag of Bodies of Revolution at Transonic Speeds.” In 14th Aerospace Sciences Meeting. AIAA 1976-90. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-90
• “Static Flight Stability and Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.011
• “Static Longitudinal Stability Flight Test Methods.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0223.0234
• “Static Stability and Control.” n.d. In Fundamentals of Airplane Flight Mechanics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-46573-7_9
• “Static Stability and Control.” 1998. In Introduction to Aircraft Flight Dynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862052.0067.0092
• Stauffer, W. 1964. “Remarks on Structural Design Criteria for the Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-627
• “Steady Flight Performance.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.008
• Steelant, Johan. 2008. “Achievements Obtained for Sustained Hypersonic Flight within the LAPCAT Project.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2578
• Steelant, Johan. 2009. “Sustained Hypersonic Flight in Europe: Technology Drivers for LAPCAT II.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7240. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7240
• Steelant, Johan. 2011. “Sustained Hypersonic Flight in Europe: First Technology Achievements within LAPCAT II.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2243
• Steer, A. 2000. “Integrated Control of a Second Generation Supersonic Commercial Transport Aircraft Using Thrust Vectoring.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4109
• Steers, S. T., and K. W. Iliff. 1975. Effects of Time-Shifted Data on Flight Determined Stability and Control Derivatives. NASA-TN-D-7830. NASA. https://ntrs.nasa.gov/citations/19750010172
• Stefko, George, Gary Podboy, and Gayle Rose. 1987. “Wind Tunnel Performance Results of an Aeroelastically Scaled 2/9 Model of the PTA Flight Test Prop-Fan.” In 23rd Joint Propulsion Conference. AIAA 1987-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1893
• Stein, Jenny M. 2005. “Parachute Testing for the NASA X-38 Crew Return Vehicle.” In Society of Flight Test Engineers. https://ntrs.nasa.gov/citations/20060056201
• Steinle, F. W., Jr. 1982. “Tunnel-to-Tunnel Correlation.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017324
• Steinmetz, Ronald, and Bob Hines. 1987. “Engine Variable Geometry Effects on Commercial Supersonic Transport Development.” In 23rd Joint Propulsion Conference. AIAA 1987-2101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2101
• Stelmach, Anna. 2012. “Modeling of Selected Aircraft Flight Phases Using Data from Flight Data Recorder.” Archives of Transport 23 (4). https://doi.org/10.2478/v10174-011-0037-2
• Stemmer, Christian. 2005. “Hypersonic Transition Investigations in a Flat-Plate Boundary-Layer Flow at M=20.” In 35th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2005-5136. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5136
• Stengel, R. 1983. “Identification of Aerodynamic Coefficients Using Flight Testing Data.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2099
• Stephan, K., and E. Obermeier. 1974. “Correlation of Heat Transfer Coefficients in Hypersonic Stagnation Point Flow.” In Proceeding of International Heat Transfer Conference 5. Begellhouse. https://doi.org/10.1615/ihtc5.2210
• Stephan, Ralph, Nicolas Schneiders, Florian Schueltke, Fabian Peter, and Eike Stumpf. 2022. “Evaluation of a Distributed Variable-Camber Trailing-Edge Flap System at Preliminary Aircraft Design Stage.” In AIAA AVIATION 2022 Forum. AIAA 2022-3519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3519
• Stephens, Emily W. 1959. Free-Flight Investigation of a Rocket-Propelled Model to Determine the Aerodynamic Heating on a Thin, Unswept, Untapered, Multispar, Aluminum-Alloy Wing at Mach Numbers up to 2.22. NASA-MEMO-12-15-58L. NASA. https://ntrs.nasa.gov/citations/19980232232
• Stephenson, R. Y. 1999. “Update of NACA History: 1995-1999.” Clean Air Journal 10 (4). https://doi.org/10.17159/caj/1999/10/4.7333
• Stephenson, James, Kyle Pascioni, Mary Houston, Colin Stutz, and Preston Martin. 2025. “Overview of a Comprehensive MD530F Acoustic Flight Test.” In Vertical Flight Society’s (VFS) 81st Annual Forum & Technology Display. https://ntrs.nasa.gov/citations/20250004880
• Stepner, D. E., and R. K. Mehra. 1973. Maximum Likelihood Identification and Optimal Input Design for Identifying Aircraft Stability and Control Derivatives. NASA-CR-2200. NASA. https://ntrs.nasa.gov/citations/19730012344
• Stepner, D. E., and J. A. Sorensen. 1974. “A Unified Approach to Aircraft Parameter Identification.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017471
• Steppert, Michael, and Philipp Epple. 2017. “Numerical Investigation of the Drag of Rockets at Subsonic, Transonic and Supersonic Speeds.” In Volume 7: Fluids Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2017-71872
• Sterk, Steve, Olivia Alexander, and Abigail Kosiak. 2018. “Using Historical Cost and Schedule Data to Predict Cost Risk for Future NASA X-Planes.” In NASA Cost Symposium. https://ntrs.nasa.gov/citations/20180006109
• Sterk, Steve, and Aaron McAtee. 2015. “X-1 to X-Wings: Developing a Parametric Cost Model.” In NASA. https://ntrs.nasa.gov/citations/20150018064
• Sterk, Steve, Anthony Ogluin, and Marc Greenberg. 2016. “NASA’s X-Plane Database and Parametric Cost Model v 2.0.” In ICEAA Symposium and Workshop. https://ntrs.nasa.gov/citations/20160012681
• Stern, A., and A. Peracchio. 1989. “The Challenge of Reducing Supersonic Civil Transport Propulsion Noise.” In 25th Joint Propulsion Conference. AIAA 1989-2363. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2363
• Sternberg, Natalia. 2010. Transmission of Radio-Frequency Signals through Plasma during Hypersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada518365
• Stetson, K. 1983. “Nosetip Bluntness Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow.” In 16th Fluid and Plasmadynamics Conference. AIAA 1983-1763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1763
• Stetson, Kenneth F. 1986. Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack. Defense Technical Information Center. https://doi.org/10.21236/ada178877
• Stetson, Kenneth F. 1990. Comments on Hypersonic Boundary-Layer Transition. Defense Technical Information Center. https://doi.org/10.21236/ada227242
• Stetson, Kenneth F. 1992. “Hypersonic Boundary-Layer Transition.” In Advances in Hypersonics. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-0379-7_7
• Stetson, K., and F. Sawyer. 1977. “A Comparison of Hypersonic Wind Tunnel Data Obtained by Static and Free Oscillation Testing Techniques.” In 10th Fluid and Plasmadynamics Conference. AIAA 1977-690. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-690
• Steva, Thomas. n.d. “Comparison of a Direct-Connect and Freejet Dual-Mode Scramjet.” PhD diss., University of Virginia. https://doi.org/10.18130/v3hm1j
• Stevens, Joseph E. 1950. Preliminary Results of a Flight Investigation of 1/6-Scale Rocket-Powered Models of the Bell MX-776 to Determine Aileron Rolling Effectiveness and Total Drag. NACA-RM-SL51D27. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030014
• Stevens, James R., Maurice S. Cahn, and William E. Grahame. 1966. A Theoretical Study of the Aerodynamic Characteristics of Lifting-Body Entry Vehicles Summary Report, Mar. 1965: Mar. 1966. NASA-CR-80436. NASA. https://ntrs.nasa.gov/citations/19670003792
• Stewart, James. 1992. “Integrated Flight Propulsion Control Research Results Using the NASAF-15 HIDEC Flight Research Facility.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4106. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4106
• Stewart, J. 1993. “AEDC H2 Facility: New Test Capabilities for Hypersonic Air-Breathing Vehicles.” In 28th Thermophysics Conference. AIAA 1993-2781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2781
• Stewart, James P. 2016. “Teaching Flight Testing through Soaring: Invited.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-0274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0274
• Stewart, J., and C. Bauer. 1983. “A Project Management System for the X-29A Flight Test Program.” In 2nd Flight Testing Conference. AIAA 1983-2712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2712
• Stewart, James F., Frank W. Burcham Jr., and Donald H. Gatlin. 1992. Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems. NASA-TM-4393. NASA. https://ntrs.nasa.gov/citations/19920018344
• Stewart, V. R., and M. Walters. 1996. “Correlation of Powered Lift Ground Effects Determined from Wind Tunnel Tests and Moving Models.” In Proceedings of the Vertical Flight Society Forum 52 - Washington, DC 1996. The Vertical Flight Society. https://doi.org/10.4050/vfs-f52-2032
• Sticchi, Emanuele, Daniele Ragni, Damiano Casalino, and Francesco Avallone. 2024. “Aerodynamic Noise Prediction of Strut-Braced Wing Aircraft.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3012
• Stiles, Rus. 2022. “The Flight Test Program.” In The RAH-66 Comanche Helicopter: Technical Accomplishment, Program Frustration, edited by Comanche Chief Pilot. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624106255.0275.0310
• Stilla, J. 1993. “Engineering Transition Prediction for a Hypersonic Axisymmetric Boundary Layer.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5114
• Stillwell, W. H., and J. V. Wilmerding. 1951. Flight Measurements with the Douglas D-558-II (Buaero No. 37974) Research Airplane: Dynamic Lateral Stability. NACA-RM-L51C23. NASA. https://ntrs.nasa.gov/citations/19930086606
• Stillwell, W. H., J. V. Wilmerding, and R. A. Champine. 1950. Flight Measurements with the Douglas D-558-II (Buaero No. 37974) Research Airplane: Low-Speed Stalling and Lift Characteristics. NACA-RM-L50G10. NASA. https://ntrs.nasa.gov/citations/19930086379
• Stodieck, Olivia, Jonathan E. Cooper, Paul Weaver, and Paul Kealy. 2014. “Optimisation of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0343
• Stoia, Tina, Shailesh Atreya, and Patrick O’Neil. 2016. “A Highly Efficient Solid Oxide Fuel Cell Power System for an All-Electric Commuter Airplane Flight Demonstrator.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1024. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1024
• Stojakovic, Predrag. n.d. “Analysis of the External Stores and Asymmetric Loads Influence on the Airplane Flight Dynamics.” PhD diss., University of Belgrade. https://doi.org/10.2298/bg20120711stojakovic
• Stokes, Joshua T., and Thomas Lombaerts. 2023. “Control System Design for a Hypersonic Re-Entry Vehicle.” In AIAA SCITECH 2023 Forum. AIAA 2023-1638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1638
• Stolarik, Brian. 2007. Intelligent Flight Control Simulation Research Program. Defense Technical Information Center. https://doi.org/10.21236/ada470308
• Stoliker, Patrick C. 2014. “SCI-272 Task Group Flight Test Technical Team Overview.” In NATO Flight Test Technical Team Meeting. https://ntrs.nasa.gov/citations/20140008852
• Stoliker, Patrick C., and John Carter. 2003. Flight Tests of a Ministick Controller in an F/A-18 Airplane. DRC-01-33. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110023811
• Stoll, Alex M., and Gregor Veble Mikic. 2016. “Design Studies of Thin-Haul Commuter Aircraft with Distributed Electric Propulsion.” In 16th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2016-3765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3765
• Stollery, J. L., and A. V. Murthy. 1977. “An Intermittent High-Reynolds-Number Wind Tunnel.” Aeronautical Quarterly 28 (4): 259–64. https://doi.org/10.1017/s0001925900008167
• Stollery, J., and A. Murthy. 1978. “An Intermittent High Reynolds Number Wind Tunnel.” In 10th Aerodynamic Testing Conference. AIAA 1978-766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-766
• Stone, Howard W., and William M. Piland. 1991. The HL-20 Lifting-Body Personnel Launch System. SAE PAPER 911970. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920055524
• Stoney, William E., Jr., and Andrew G. Swanson. 1957. Heat Transfer Measured on a Flat-Face Cylinder in Free Flight at Mach Numbers up to 13.9. NACA-RM-L57E13. NASA. https://ntrs.nasa.gov/citations/19930089699
• Stortz, Michael W., and Dennis P. ODonoghue. 1995. “V/STOL Systems Research Aircraft: A Tool for Cockpit Integration.” In Report to the Aerospace Profession: 39th SETP Symposium. https://ntrs.nasa.gov/citations/19960020260
• Stottier, Richard H. 1995. Artificial Intelligence Techniques for Flight Test Planning. Phase 1. Defense Technical Information Center. https://doi.org/10.21236/ada293962
• Stough, H. Paul, III, Daniel J. Decarlo, and James M. Patton Jr. 1987. Spin Resistance Evaluation of a Light Airplane. SAE PAPER 871021. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19870061484
• Stough, H. Paul, III, and Bruce J. Nolmes. 1987. NASA Small Civil Airplane Research. SAE PAPER 872404. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880043748
• Stough, H. P., III, and J. M. Patton Jr. 1979. “The Effects of Configuration Changes on Spin and Recovery Characteristics of a Low-Wing General Aviation Research Airplane.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19790063863
• Strapp, Walter, Alexei Korolev, Ed Emery, Tom Ratvasky, Craig Davison, and Lyle Lilie. 2011. “Instrumentation for the High Ice Water Content (HIWC) Flight Campaigns.” In Aviation Safety Program Annual Technical Meeting. https://ntrs.nasa.gov/citations/20150010147
• Stratford, Alan H. 1973b. “Supersonic Transport.” In Air Transport Economics in the Supersonic Era. Palgrave Macmillan UK. https://doi.org/10.1007/978-1-349-01549-8_9
• Strauss, E. 1974. “Ablative Thermal Protection for Space Tug Multipass, Aerobraking Entry.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-400
• Streby, Gary D. 1990. Research in Flight Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada226123
• Streett, Craig. 2003. “Designing a Hybrid Laminar-Flow Control Experiment via CFD (Invited).” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-977. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-977
• Strike, W. T., Jr. 1982. Calibration and Performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada116279
• Stringham, R. H., Jr., and E. J. Lenk. 1975. “Flight Flutter Testing Using Pulse Techniques.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003016
• Strock, O. 1983. “Telemetry Ground Station Offers Increased Productivity in Flight Testing.” In 2nd Flight Testing Conference. AIAA 1983-2759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2759
• Stroscher, F., Z. Sika, and O. Petersson. 2013. “Reduced Order Model of a Blended Wing Body Aircraft Configuration.” In Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics, edited by C. Vallet, D. Choukroun, C. Philippe, G. Balas, A. Nebylov, O. Yanova. EDP Sciences. https://doi.org/10.1051/eucass/201306635
• Stroub, Robert H. 1978. “Full-Scale Wind Tunnel Test of a Modern Helicopter Main Rotor — Investigation of Tip Mach Number Effects and Comparisons of Four Tip Shapes.” In Proceedings of the Vertical Flight Society Forum 34 - Washington, D.C. 1978. The Vertical Flight Society. https://doi.org/10.4050/vfs-f34-002
• Strout, F. G., and A. Atencio Jr. 1976. “Flight Effects on JT8D Engine Jet Noise as Measured in the NASA Ames 40-by 80-Foot Wind Tunnel.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19760055107
• “Structured Risk Management and the Value of Information and Delay.” 2011. In Value-Added Decision Making for Managers. Chapman and Hall/CRC. https://doi.org/10.1201/b11458-15
• Strutz, L. W. 1972. Flight-Determined Derivatives and Dynamic Characteristics for the HL-10 Lifting Body Vehicle at Subsonic and Transonic Mach Numbers. NASA-TN-D-6934. NASA. https://ntrs.nasa.gov/citations/19720023253
• Studies of Sonic Boom Induced Damage. 1965. NASA-CR-227. NASA. https://ntrs.nasa.gov/citations/19650013651
• “A Study of the Aerothermal Entry Environment for the Galileo Probe.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0003.0025
• Study of the Influence of Size of a Manned Lifting Body Entry Vehicle on Research Potential and Cost. Part I: Summary Final Report. 1967. NASA-CR-66352. NASA. https://ntrs.nasa.gov/citations/19670020694
• “Study on the Flight Characteristics of an Aircraft after Icing.” 2022. Foreign Language Science and Technology Journal Database Engineering Technology. https://doi.org/10.47939/et.v3i2.103
• “A Study to Determine the Feasibility of a Low-Sonic-Boom Supersonic Transport.” 1975. In Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865121.0321.0335
• Stuessy, W., Jennifer Peeples, Baxter Mullins Jr., W. Stuessy, Jennifer Peeples, and Baxter Mullins Jr. 1997. “Improvements to the UTA High Reynolds Number Transonic Wind Tunnel.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-663
• Stull, F. 1989. “Scramjet Propulsion.” In National Aerospace Plane Conference. AIAA 1989-5012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5012
• Su, Xinbing, Ning Wang, Binlin Ma, Jingyi Du, and Xiaofei Zhang. 2018. “Numerical Study on Effects of Mult-Control Surface Position on Aeroelastic Behavior of Forward-Swept Wing.” In Proceedings of the 2018 International Conference on Service Robotics Technologies. ACM. https://doi.org/10.1145/3208833.3208850
• Subbareddy, Pramod, and Graham Candler. 2011. “DNS of Transition to Turbulence in a Hypersonic Boundary Layer.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3564
• Subcommittee on Similarity of Wind Tunnel Experime. 1994. “Study on Similarity of Wind Tunnel Experiments.” Doboku Gakkai Ronbunshu 1994 (489): 17–25. https://doi.org/10.2208/jscej.1994.489_17
• “Subscale Modeling and Wind Tunnel Testing of Propellers.” 2013. In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-499
• “Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration.” 1986. In Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865763.0350.0398
• Sudderth, R. W., and W. E. McNeill. 1976. “Development of Longitudinal Handling Qualities Criteria for Large Advanced Supersonic Aircraft.” In Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011062
• Sudha, U. P. V., Girish S. Deodhare, and Kartik Venkatraman. 2025. “Prediction of Aeroelastic Flutter Stability in a Fighter Aircraft during Wake Penetration Flight Testing Using Autoregressive Model.” In Volume 5: Structures, Structural Dynamics & Materials. American Society of Mechanical Engineers. https://doi.org/10.1115/imece-india2025-161192
• Suhanov, D. B., L. I. Serebryakov, P. A. Radchenko, and S. V. Strijhak. 2023. “To the Problem of Selecting the Anti-Icing System for the Swept Wing of Supersonic Flight Demonstrator.” In Springer Aerospace Technology. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9010-6_12
• Suit, W. T. 1986. Summary of Longitudinal Stability and Control Parameters as Determined from Space Shuttle Columbia Flight Test Data. NASA-TM-87768. NASA. https://ntrs.nasa.gov/citations/19870000668
• Suit, William T. 1989. Summary of Longitudinal Stability and Control Parameters as Determined from Space Shuttle Challenger Flight Test Data. NASA-TM-101605. NASA. https://ntrs.nasa.gov/citations/19890018300
• Suit, W. T., and J. G. Batterson. 1986. Lateral and Longitudinal Aerodynamic Stability and Control Parameters of the Basic Vortex Flap Research Aircraft as Determined from Flight Test Data. NASA-TM-87711. NASA. https://ntrs.nasa.gov/citations/19860015232
• Suit, W., and J. Schiess. 1985. “Supplement to the Shuttle Aerodynamic Database Using Discovery Flight Tests.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1765
• Suit, William T., and James R. Schiess. 1988. Lateral and Longitudinal Stability and Control Parameters for the Space Shuttle Discovery as Determined from Flight Test Data. NASA-TM-100555. NASA. https://ntrs.nasa.gov/citations/19880010925
• Sulaeman, E., and H. Djojodihardjo. 1995. “An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations.” In Contemporary Research in Engineering Science. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-80001-6_38
• Suleman, Afzal. 2007. Aeroelastic Scaling of a Joined Wing Sensorcraft Concept. Defense Technical Information Center. https://doi.org/10.21236/ada525877
• Sullins, G., D. Carpenter, M. Thompson, F. Kwok, and L. Mattes. 1991. “A Demonstration of Mode Transition in a Scramjet Combustor.” In 27th Joint Propulsion Conference. AIAA 1991-2395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2395
• Sullivan, R., and Stephen Finberg. 1989. “The Flight Control System for the Daedalus Human Powered Aircraft.” In Guidance, Navigation and Control Conference. AIAA 1989-3593. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3593
• Suman, Saurav, Aakash Maheshwari, and Air Cmde Devender Sharma. 2021. “Investigation of Lift and Drag Characteristics of Traditional Symmetrical, Cambered and Supercritical Airfoils at Different Angles of Attack and Mach Nos.” Gedrag & Organisatie Review 34 (02). https://doi.org/10.37896/gor34.02/017
• Suminsby, Robert E. 2002. Fear No Evil: Unmanned Combat Air Vehicles for Suppression of Enemy Air Defenses. Defense Technical Information Center. https://doi.org/10.21236/ada420687
• “Summary of Current Economic Studies of the United States Supersonic Transport. Federal Aviation Authority, Office of Supersonic Transport Development, Washington, D.C. September 1969. 50p.” 1970. Travel Research Bulletin 9 (1): 15–15. https://doi.org/10.1177/004728757000900123
• Sun, Hongsheng. n.d. “Closed-Loop Endo-Atmospheric Ascent Guidance for Reusable Launch Vehicle.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-14281
• Sun, Jianyu. 2026. “Cost Model of Airframe Structural Parts Based on Engineering Method.” Journal of Physics: Conference Series 3207 (1): 012034. https://doi.org/10.1088/1742-6596/3207/1/012034
• Sun, Zhi Wei, and Jun Qiang Bai. 2014. “Time-Domain Aeroservoelastic Modeling and Active Flutter Suppression by Model Predictive Control.” Advanced Materials Research 898: 688–95. https://doi.org/10.4028/www.scientific.net/amr.898.688
• Sun, Jian, Qinghua Guan, Yanju Liu, and Jinsong Leng. 2016. “Morphing Aircraft Based on Smart Materials and Structures: A State-of-the-Art Review.” Journal of Intelligent Material Systems and Structures 27 (17): 2289–2312. https://doi.org/10.1177/1045389x16629569
• Sun, J., and S. Hansen. 1982. “Transonic Nose Wave Drag of Axisymmetric Bodies.” In 20th Aerospace Sciences Meeting. AIAA 1982-308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-308
• Sun, Ne-Zheng, and Alexander Sun. 2015. “Optimal Experimental Design.” In Model Calibration and Parameter Estimation. Springer New York. https://doi.org/10.1007/978-1-4939-2323-6_11
• Sun, H., J. Wu, G. Li, L. Du, and C. Su. 2023. “Uncertainty Optimization Design of Hypersonic Vehicle Propulsion System.” IET Conference Proceedings 2022 (21): 1395–99. https://doi.org/10.1049/icp.2022.3063
• Sun, Huajun, Heng Zhang, Ziyan Wei, and Jie Li. 2025. “Aerodynamic Shape Design of Oblique Wing for Transonic/Supersonic Conditions: Integrating Coupled Drag and Lateral Performance Using the Adjoint Method.” Preprint, . https://doi.org/10.2139/ssrn.5251753
• Sunami, Tetsuji, Katsuhiro Itoh, Kazuo Satoh, and Tomoyuki Komuro. 2006. “Mach 8 Ground Tests of the Hypermixer Scramjet for HyShot-IV Flight Experiment.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8062. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8062
• “Supercritical Airfoil Design.” n.d. In Lecture Notes in Physics. Springer Berlin Heidelberg. https://doi.org/10.1007/3-540-11499-8_5
• “Supersonic Flows over Wings and Airplane Configurations.” 2021. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009105842.012
• “Supersonic Flows over Wings and Airplane Configurations.” 2025. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009501293.012
• “Supersonic Transport Wing Minimum Weight Design Integrating Aerodynamics and Structures.” 1992. In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2372
• Suppe, Frederick. 2000. “The Changing Nature of Flight and Ground Test Instrumentation and Data: 1940–1969.” In Archimedes. Springer Netherlands. https://doi.org/10.1007/978-94-011-4379-0_3
• Suppes, Adam Bradford, and Galen Suppes. 2024. “Thin Cambered Lifting Bodies in Ground Effect Flight.” Preprint, . https://doi.org/10.31224/4136
• Suppes, Adam, and Galen Suppes. 2026. “Qualitative Validation Lifting Body VTOL with Stagnation Plates.” Preprint, . https://doi.org/10.33774/coe-2026-7rzmb
• “Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0651.0662
• “Survey of the Supporting Research and Technology for the Thermal Protection of the Galileo Probe.” 1982. In Thermophysics of Atmospheric Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865565.0293.0327
• Sutherland, Reginald J. 1961. “Summary of Symposium on Supersonic Air Transport.” Journal of the Air Transport Division 87 (2): 89–97. https://doi.org/10.1061/jaceal.0000114
• Sutton, K., and R. A. Graves Jr. 1971. A General Stagnation-Point Convective Heating Equation for Arbitrary Gas Mixtures. NASA-TR-R-376. NASA. https://ntrs.nasa.gov/citations/19720003329
• Sutton, K., J. Jones, and R. Powell. 1978. “Effects of Atmospheric Structure on Radiative Heating for Jupiter Entry Probe.” In 16th Aerospace Sciences Meeting. AIAA 1978-185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-185
• Suzuki, S. 1990. “Structure/control Design Synthesis of Active Flutter Suppression System by Goal Programming.” In Guidance, Navigation and Control Conference. AIAA 1990-3325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3325
• Suzuki, Kojiro. 2016. “Aerodynamic Shape Design of Hypersonic Booster with RBCC Engine for TSTO Vehicle.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 14 (ists30): Pe_71-Pe_76. https://doi.org/10.2322/tastj.14.pe_71
• Suzuki, Yudai, William Dunham, Ilya Kolmanovsky, and Anouck Girard. 2019. “Failure Detection and Control of Distributed Electric Propulsion Aircraft Engines.” In AIAA Scitech 2019 Forum. AIAA 2019-0109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0109
• Svec, R. 1981. “Flight Testing the Suspended Maneuvering System.” In 1st Flight Test Conference. AIAA 1981-2498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2498
• Svendsen, Keith. 1994. “DT&E Flight Test Management Initiatives.” In Biennial Flight Test Conference. AIAA 1994-2160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2160
• Swain, R. L. 1982. “Status of the National Transonic Facility.” In Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017321
• Swamy, M., S. Ahmed, and G. Sreenath. 1978. “Model Support System Interference on Zero-Lift Drag at Transonic Speeds.” In 10th Aerodynamic Testing Conference. AIAA 1978-809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-809
• Swann, M., E. Duke, E. Enevoldson, and T. Wolf. 1981. “Experience with Flight Test Trajectory Guidance.” In 1st Flight Test Conference. AIAA 1981-2504. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2504
• Swanson, A. G. 1958. Free-Flight Investigation of Aerodynamic Heat Transfer to a Simulated Glide-Rocket Shape at Mach Numbers up to 10. NACA-RM-L58G03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19630010650
• Swanson, Taylor, and Derick Daniel. 2016. “Hypersonic Boundary Layer Transition Experiments in Hypervelocity Ballistic Range G.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-2118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2118
• Swanson, Andrew G., and Charles B. Rumsey. 1956. Aerodynamic Heating of a Wing as Determined from a Free-Flight Rocket-Model Test to Mach Number 3.64. NACA-RM-L56F11a. NASA. https://ntrs.nasa.gov/citations/19930089374
• Swanson, Greg, Brandon Smith, Robert Akamine, et al. 2018. “The HIAD Orbital Flight Demonstration Instrumentation Suite.” In International Planetary Probe Workshop. https://ntrs.nasa.gov/citations/20180005723
• Swassing, Margaret. 2008. “Flight Testing an Airborne Weather Radar System at Edwards AFB, California.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1652
• Sweberg, Harold H., and Roy H. Lange. 1947. Summary of Available Data Relating to Reynolds Number Effects on the Maximum Lift Coefficients of Swept-Back Wings. NACA-RM-L6L20a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20030063156
• Sweetman, Bill. 1990. “Stealth Aircraft-History, Technology and Outlook.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-172
• Swihart, J. 1967. “The United States Supersonic Transport: A Progress Report.” In 10th Anglo-American Aeronautical Conference. AIAA 1967-750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-750
• Świtała, Andrzej, and Adam Lipski. 2026. “Morphing Wing with Variable Camber near Trailing Edge.” In AIP Conference Proceedings, vol. 3368. AIP Publishing. https://doi.org/10.1063/5.0302401
• Syed, Aqib, Mojtaba Moshtaghzadeh, Dewey H. Hodges, and Pezhman Mardanpour. 2022. “Effects of Morphing on Aeroelastic Stability of Flying Wing Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-2557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2557
• Symington, W. W. 1940. “Correlation of Wind Tunnel and Flight Test Results.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/400114
• Synodinos, Athanasios, Rod Self, and Antonio Torija. 2018. “Preliminary Noise Assessment of Aircraft with Distributed Electric Propulsion.” In 2018 AIAA/CEAS Aeroacoustics Conference. AIAA 2018-2817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2817
• Sypniewski, Carl. 1989. “The NASP Challenge: Technical Breakthrough.” In National Aerospace Plane Conference. AIAA 1989-5017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5017
• System in-Flight Testing. 2010. Wiley. https://doi.org/10.1002/9780470664797.ch20
• Szalai, K. J. 1984. Role of Research Aircraft in Technology Development. AIAA PAPER 84-2473. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19850033955
• Szilder, Krzysztof, and Stuart McIlwain. 2012. “In-Flight Icing of UAVs – the Influence of Flight Speed Coupled with Chord Size.” Canadian Aeronautics and Space Journal 58 (02): 83–94. https://doi.org/10.5589/q12-007
• Szymanski, Maxime, Georges Ghazi, and Ruxandra M. Botez. 2025. “Enhanced Neural Network Model for Aircraft Flight Dynamics Prediction from Flight Test Data: Business Aircraft Application.” In AIAA SCITECH 2025 Forum. AIAA 2025-2228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2228
• Taflan, Murat, and Mert Gulum. 2026. “Hierarchical Mass Breakdown for Transport Aircraft with Truss Braced Wings.” In MATTER: International Journal of Science and Technology (ISSN 2454-5880). Global Research & Development Services Publishing. https://doi.org/10.20319/stra.2026.1726
• Taguchi, Hideyuki, Kenya Harada, Hiroaki Kobayashi, et al. 2009. “Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7311
• Taguchi, Hideyuki, Hiroaki Kobayashi, Takayuki Kojima, et al. 2012. “Hypersonic Flight Experiment Plan of Pre-Cooled Turbojet Engine.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5840
• Takahashi, Timothy T., Stefan Boccieri, Joseph Elvig, et al. 2019b. “Troubling Problems Configuring a Forward Swept Wing Transonic Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-0813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0813
• Takahashi, Hidemi, Tomonari Hirotani, and Hideyuki Taguchi. 2025. “Flush Air-Data Sensing System for Hypersonic Flight Experimental Vehicle with Ogive-Shaped Nose.” In AIAA SCITECH 2025 Forum. AIAA 2025-1340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1340
• Takahashi, Hidemi, Junichi Oki, Tomonari Hirotani, and Hideyuki Taguchi. 2023. “Tomographic Reconstruction of Hypersonic Winged-Aircraft Model Flowfields in Large-Scale Hypersonic Wind Tunnel Experiment.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3029
• Takahashi, Yusuke, Kazuhiko Yamada, Takashi Abe, and Kojiro Suzuki. 2013. “Aerodynamic Heating around an Inflatable Vehicle during a Reentry Demonstration Flight by a Sounding Rocket.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1303. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1303
• Takaki, Ryoji, Minoru Takizawa, Ryoji Takaki, and Minoru Takizawa. 1997. “ADS Measurement of HYFLEX (HYpersonic FLight EXperiment).” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-193
• Takashima, N., and M. Lewis. 1995. “Powered Hypersonic Waverider Vehicles for Optimization with Mission-Oriented Constraints.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-846. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-846
• Takovitskii, S. A. 2003a. “Analytic Solution in the Problem of Constructing an Airfoil with Minimum Wave Drag.” Fluid Dynamics 38 (6): 933–41. https://doi.org/10.1023/b:flui.0000015235.61628.78
• Takovitskii, S. A. 2006a. “Analytical Solution in the Problem of Constructing Axisymmetric Noses with Minimum Wave Drag.” Fluid Dynamics 41 (2): 308–12. https://doi.org/10.1007/s10697-006-0045-8
• Takovitskii, S. A. 2024. “Conical Bodies with Star-Shaped Transverse Contour Having the Minimum Wave Drag.” Fluid Dynamics 59 (1): 122–29. https://doi.org/10.1134/s0015462823602966
• Tal, Ezra A., and Nhan T. Nguyen. 2015. “Unsteady Aeroservoelastic Modeling of Flexible Wing Generic Transport Aircraft with Variable Camber Continuous Trailing Edge Flap.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2722
• Talay, Theodore A., and Howard W. Stone. 1991. The Personnel Launch System: A Lifting Body Approach. IAF PAPER 91-202. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920029948
• Talmage, Donald B. 1947. A Time History of Control Operation of a C-54 Airplane in Blind Landing Approaches. NACA-RM-L7F20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019332
• Talmage, Robert. 2008. “A Safe, Economical and Versatile Space Flight Test Vehicle.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2659
• Tambova, S., M. Seeman, O. B. Ozseven, and D. F. M. Heckmeier. 2026. “B7.2: Automated Post-Flight Data and Signal Analysis in Flight Test Instrumentation Applications.” In Lectures. AMA Service GmbH, Von-Münchhausen-Str. 49, 31515 Wunstorf. https://doi.org/10.5162/ettc2026/b7.2
• Tang, Ming H. 1970. “Correlation of Flight-Test Loads with Wind- Tunnel Predicted Loads on Three Lifting Body Vehicles.” In Flight Test Results Pertaining to the Space Shuttlecraft. https://ntrs.nasa.gov/citations/19710000632
• Tang, Lei, and James Baeder. 2003. “Adaptive Euler Simulation of Supercritical Interaction of Airfoil and Vortex.” In 16th AIAA Computational Fluid Dynamics Conference. AIAA 2003-3826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3826
• Tang, Ming, and Ramon Chase. 2008. “The Quest for Hypersonic Flight with Air-Breathing Propulsion.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2546
• Tang, Deman, Denis Kholodar, Jer-Nan Juang, and Earl H. Dowell. 2001. System Identification and POD Method Applied to Unsteady Aerodynamics. NASA/TM-2001-211243. NASA. https://ntrs.nasa.gov/citations/20020015800
• Tang, M. H., and G. P. E. Pearson. 1971. Flight-Measured HL-10 Lifting Body Center Fin Loads and Control Surface Hinge Moments and Correlation with Wind-Tunnel Predictions. NASA-TM-X-2419. NASA. https://ntrs.nasa.gov/citations/19710029224
• Tang, M. H., and G. P. E. Pearson. 1973. Flight-Measured X-24A Lifting Body Control Surface Hinge Moments and Correlation with Wind Tunnel Predictions. NASA-TM-X-2816. NASA. https://ntrs.nasa.gov/citations/19730016322
• Tang, M. H., W. J. Sefic, and R. G. Sheldon. 1978. Comparison of Concurrent Strain Gage- and Pressure Transducer-Measured Flight Loads on a Lifting Reentry Vehicle and Correlation with Wind Tunnel Predictions. NASA-TP-1331. NASA. https://ntrs.nasa.gov/citations/19780025110
• Tang, Chun Y., Kerry A. Trumble, Charles H. Campbell, Victor R. Lessard, and William A. Wood. 2010. “Numerical Simulations of the Boundary Layer Transition Flight Experiment.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110008525
• Tang, Jian, Zhigang Wu, and Chao Yang. 2015. “Uncertainty Quantification and Sensitivity Analysis of Aeroservoelastic Stability for a Slender Flight Vehicle.” In 17th AIAA Non-Deterministic Approaches Conference. AIAA 2015-0664. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0664
• Tangler, James L. 1979. Analysis of Low-Speed Helicopter Flight Test Data. Defense Technical Information Center. https://doi.org/10.21236/ada074141
• Tani, Itiro. 1952. On the Design of Airfoils in Which the Transition of the Boundary Layer Is Delayed. NACA-TM-1351. NASA. https://ntrs.nasa.gov/citations/19930093879
• Tani, Kouichiro, Maso Takegoshi, Koichi Takasaki, and Shinichiro Tokudome. 2023. “JAXA RD1 Flight Experiment on Supersonic Combustion: Part 1. Overview.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3009
• Taniguchi, N. 1972. SCIP2 Flight Instrumentation Specification for Parameter Identification: User’s Guide. NASA-CR-112122. NASA. https://ntrs.nasa.gov/citations/19720024391
• Tao, Yanhong, Xiaohui Zheng, and Yang Cui. 2023. “Civil Airplane Initial Buffeting Flight-Test Data Analysis and Boundary Expansion.” In Third International Conference on Mechanical Design and Simulation (MDS 2023), edited by Mohamed Arezki Mellal, Yunqing Rao. SPIE. https://doi.org/10.1117/12.2681882
• Taranto, Jordan, and Mujahid Abdulrahim. 2023. “Development of Autonomous Flight Envelope Supervisor for UAS Platform Flight Testing.” In 2023 Regional Student Conferences. AIAA 2023-71776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-71776
• Tarnowski, Andrzej. 2017. “Morphing Wing with Skin Discontinuity – Kinematic Concept.” Aircraft Engineering and Aerospace Technology 89 (4): 535–46. https://doi.org/10.1108/aeat-11-2016-0208
• Tarpley, Christopher, and Mark Lewis. 1995. “Optimization of an Engine-Integrated Waverider with Steady State Flight Constraints.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-848
• Tartabini, Paul V., David M. Bose, John D. McMinn, John G. Martin, and Brian K. Strovers. 2003. Hyper-X Stage Separation Trajectory Validation Studies. AIAA Paper 2003-5819. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040031535
• Tartinville, Benoit, Virginie Barbieux, and Lionel Temmerman. 2018. “High Fidelity Gust Simulations over a Supercritical Airfoil.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3634. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3634
• Tashakkor, Scott B., Francisco Canabal, and Jason E. Mishtawy. 2011. CFD Modeling of Launch Vehicle Aerodynamic Heating. M11-0030. Jacobs Engineering Group, Inc. https://ntrs.nasa.gov/citations/20110014627
• Tatarewicz, Joseph N., and James R. Hansen. 1996. “The Spaceflight Revolution: NASA Langley Research Center from Sputnik to Apollo.” Journal of Military History 60 (3): 587. https://doi.org/10.2307/2944563
• Tatman, Benjamin. n.d. “Experimental Study of Vitiation Effects on Flameholding in a Hydrocarbon Fueled Dual-Mode Scramjet Combustor.” PhD diss., University of Virginia. https://doi.org/10.18130/v3g36z
• Tauber, M. 1968. “Atmospheric Entry into Jupiter.” In Entry Vehicle Systems and Technology Meeting. AIAA 1968-1150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1150
• Tauber, Michael E. 1989. A Review of High-Speed, Convective, Heat-Transfer Computation Methods. NASA-TP-2914. NASA. https://ntrs.nasa.gov/citations/19890017745
• Tauber, M. E., and M. E. Wilkins. 1966. Boundary-Layer Transition on Ablating Cones at Speeds up to 7 Km/sec. AIAA PAPER 66-27. NASA. https://ntrs.nasa.gov/citations/19660038599
• Taubert, Lutz, Garrett A. Kay, and Israel J. Wygnanski. 2021. “On the Hybrid Tilt-Wing, Tilt Propeller, Active Flow Control Enabled Runway Independent Airplane.” In AIAA Aviation 2021 Forum. AIAA 2021-2815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2815
• Tava, Marcello, and Shinji Suzuki. 2001. “Multidisciplinary Design Optimization of a Re-Entry Vehicle Shape and Trajectory.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1920. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1920
• Taylor, J. 1968. “Engine Compatibility Programs for the Supersonic Transport Propulsionsystem.” In 5th Annual Meeting and Technical Display. AIAA 1968-993. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-993
• Taylor, K. 1977. “A Transformation of the Acoustic Equation with Implications for Low-Speed Flight and Wind-Tunnel Tests.” In 4th Aeroacoustics Conference. AIAA 1977-1307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1307
• Taylor, Terry L. 2004. X-37 Flight Demonstrator: Approach and Landing Test Vehicle Flight Test Approach. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20040037790
• Taylor, Brian. 2012. “A Full-Envelope Air Data Calibration and Three Dimensional Wind Estimation Method Using Global Output-Error Optimization and Flight-Test Techniques.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4410
• Taylor, A., and L. Jackson. 1977. “Heat Sink Structural Design Concepts for a Hypersonic Research Airplane.” In 18th Structural Dynamics and Materials Conference. AIAA 1977-392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-392
• Taylor, Paul F., Ruben Moreno, Nagaraj Banavara, Raj K. Narisetti, and Lloyd Morgan. 2017. “Flutter Flight Testing at Gulfstream Aerospace Using Advanced Signal Processing Techniques.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-1823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1823
• Taylor, Brian, and Nalin Ratnayake. 2011. “Flight Test of Orthogonal Square Wave Inputs for Hybrid-Wing-Body Parameter Estimation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6276
• Taylor, Brian, Nalin Ratnayake, and James Murray. 2010. “Simulation and Flight Evaluation of a Parameter Estimation Input Design Method for Hybrid-Wing-Body Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7949
• Taylor, L. W., Jr. 1982. “Applications of Parameter Estimation in the Study of Spinning Airplanes.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820055555
• Taylor, Lawrence W., Jr., and Richard E. Day. 1961. Flight Controllability Limits and Related Human Transfer Functions as Determined from Simulator and Flight Tests. NASA-TN-D-746. NASA. https://ntrs.nasa.gov/citations/20040006313
• Taylor, L. W., Jr., and V. Klein. 1981. “Analytical Techniques for the Analysis of Stall/spin Flight Test Data.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19810058352
• “Technical Applications for an Experimental Supersonic Cruise Aircraft.” 1976. In Aircraft Systems and Technology Meeting. AIAA 1976-892. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-892
• “A Technology and Operations Assessment of Single Stage Rocket Technology Flight Test Program Results.” 1993. In Space Programs and Technologies Conference and Exhibit. AIAA 1993-4163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4163
• “Technology Demonstrator, Close Air Support, and Legacy Programs.” 2023. In The Aircraft Designers. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624106965.0259.0354
• Teets, Edward H. 2016. “Atmospheric Measurements for Flight Test at NASAs Neil a. Armstrong Flight Research Center.” In STEM Outreach. https://ntrs.nasa.gov/citations/20160012047
• Teitelbaum, Jerome M. 1949. Flight Investigation of Flutter Models with 1/10-Scale Douglas D-558-2 Wing Panels. NACA-RM-L9A06. NASA. https://ntrs.nasa.gov/citations/19930085854
• Tekinalp, Ozan, and Nesrin Cavus. 2012. “Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle.” In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2012-5532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5532
• Tempelmeyer, Kenneth E., and Robert S. Osborne. 1955. Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Transonic Speeds. Rept-4990. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029389
• Tendero Ventanas, Juan Ángel. n.d. “Instability Analysis of Vortex Systems in Lifting-Body Wakes.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.43277
• Teng, Ying. 2007. “Robust Analysis of Active Flutter Suppression Using Multiple Control Surfaces via Second-Order Controllers.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2007-01-3921
• Teng, Ying, and Hsin-Piao Chen. 2006. “u-Synthesis for an Active Aeroelastic Wing with Leading and Trailing Edge Control Surfaces.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-443
• Tenhave, Jackson, Keith Joiner, and Dominic Hill. 2025. “Sub-Scale Flight Testing of Drag Reduction Features for Amphibious Light Sport Aircraft.” Preprint, . https://doi.org/10.20944/preprints202510.2408.v1
• Teramoto, Susumu, Kouji Hiraki, and Kozo Fujii. 1998. “Numerical Analysis of Dynamic Stability of a Reentry Capsule at Transonic Speeds.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4451
• Terejanu, G., C. M. Bryant, and K. Miki. 2013. “Bayesian Optimal Experimental Design for the Shock-Tube Experiment.” Journal of Physics: Conference Series 410: 012040. https://doi.org/10.1088/1742-6596/410/1/012040
• “Testing of Advanced Carbon Fibre Wings for New Experimental Aircraft.” 1986. Aircraft Engineering and Aerospace Technology 58 (3): 24–24. https://doi.org/10.1108/eb036259
• Teter, John E., Jr. 2006. “Planetary Airplane Extraction System Development and Subscale Testing.” In 38th Aerospace Mechanisms Symposium. https://ntrs.nasa.gov/citations/20060028226
• Tetlow, M., U. Schoettle, and G. Schneider. 2000. “Optimisation of a Reusable Launch Vehicle Concept.” In Modeling and Simulation Technologies Conference. AIAA 2000-4180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4180
• Tetrault, P.-A., J. Schetz, and B. Grossman. 2000. “Numerical Prediction of the Interference Drag of a Streamlined Strut Intersecting a Surface in Transonic Flow.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-509
• Tewari, Ashish. 1998. “Robust Optimal Controllers for Active Flutter Suppression.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4142
• Tewari, Ashish. 1999. “Output Rate Weighted Active Flutter Suppression.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4312
• Tewell, J. 1984. “An Unmanned Reentry/recovery Vehicle for a Reusable Launch System.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-781
• Thacker, Michael, and C. Lan. 1993. “Calculation of Transonic Longitudinal and Lateral-Directional Characteristics of Aircraft by the Small Disturbance Theory.” In Flight Simulation and Technologies. AIAA 1993-3617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3617
• Thake, Michael, Nathan Packard, Carlos Bonilla, and Jeffrey Bons. 2010. “Low Reynolds Number Laminar Airfoil with Active Flow Control.” In 5th Flow Control Conference. AIAA 2010-4579. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4579
• Theis, Julian, Harald Pfifer, and Peter J. Seiler. 2016. “Robust Control Design for Active Flutter Suppression.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1751
• Thelander, J. A. 1965. Aircraft Motion Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0617354
• Theodore, Colin R., Carlos A. Malpica, and Ben Lawrence. 2014a. “Rotorcraft Flight Dynamics and Controls Research at NASA.” In Australian Pacific Vertiflite Conference on Helicopter Technology. https://ntrs.nasa.gov/citations/20190027087
• Theodore, Colin R., Gina C. Willink, Carl R. Russell, Alexander R. Amy, and Ashley E. Pete. 2014b. “Wind Tunnel Testing of a 120th Scale Large Civil Tilt-Rotor Model in Airplane and Helicopter Modes.” In Decennial AHS Aeromechanics Specialists’’ Conference. https://ntrs.nasa.gov/citations/20140012545
• Theodorsen, Theodore. 1935. General Theory of Aerodynamic Instability and the Mechanism of Flutter. NACA-TR-496. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19800006788
• Theofanous, Theo, and Chih-Hao Chang. 2008. “On the Computation of Multiphase Interactions in Transonic and Supersonic Flows.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-1233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1233
• “The Theoretical Study of the Aerothermodynamics Characteristics for Dual-Mode SCRAMJET Combustor.” 2012. In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5911
• “Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow.” 1962. In Hypersonic Flow Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864810.0421.0470
• “Thermal Design of a Saturn/Uranus Atmospheric Entry Probe.” 1974. In Thermophysics and Spacecraft Thermal Control. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865084.0499.0516
• “Thermal Protection for a Re-Entry Vehicle Using Heat Ablation Process.” 2015. International Journal of Science and Research (IJSR) 4 (11): 2193–95. https://doi.org/10.21275/v4i11.nov151618
• “Thermal Protection System Conception.” 2013. In Ablative Thermal Protection Systems Modeling. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624101717.0001.0030
• “Thermal Protection System for the Galileo Mission Atmospheric Entry Probe.” 1981. In Aerothermodynamics and Planetary Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865510.0309.0334
• Thi Kim Dung, Hoang, and Nguyen Phu Khanh. 2021. “Research on Aeroelasticity Phenomenon in Aeronautical Engineering.” In Aerodynamics. IntechOpen. https://doi.org/10.5772/intechopen.91748
• Thigpen, D., and R. Whitmoyer. 1976. “Flight Test Status of the Fighter CCV.” In Aircraft Systems and Technology Meeting. AIAA 1976-884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-884
• Thomas, R. 1981. “An Investigation of the Impact of Aerodynamic Lags on Dynamic Flight Characteristics.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1892. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1892
• Thomas, Bryce, and Ramesh K. Agarwal. 2023. “Evaluation of Sustainable Transonic Truss-Braced Wing Aircraft Configurations Using Liquid Hydrogen Fuel.” In AIAA SCITECH 2023 Forum. AIAA 2023-2175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2175
• Thomas, Bryce, and Ramesh K. Agarwal. 2025. “Application of a Co-Flow Jet Airfoil in Development of a Transonic-Truss Braced Wing.” In AIAA SCITECH 2025 Forum. AIAA 2025-0031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0031
• Thomas, F. M., and H. W. Fairchild. 1933. “Airplane Flight Testing for Maximum Speed.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/330004
• Thomas, Russell H., Yueping Guo, Ian A. Clark, and Jason C. June. n.d. “Propulsion Airframe Aeroacoustics and Aircraft System Noise Flight Research Test: NASA Overview.” In 28th AIAA/CEAS Aeroacoustics Conference. https://ntrs.nasa.gov/citations/20220006784
• Thomas, Russell H., Yueping Guo, Ian A. Clark, and Jason C. June. 2018. “Challenges and Opportunities for Subsonic Transport X-Plane Acoustic Flight Research.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20190027211
• Thomas, Russell H., Yueping Guo, Eric H. Nesbitt, Ian A. Clark, and Jason C. June. 2024. “Refined Predictions Compared with the Propulsion Airframe Aeroacoustics and Aircraft System Noise Flight Research Test Data.” In 34th Congress of the International Council of the Aeronautical Sciences. https://ntrs.nasa.gov/citations/20240007676
• Thomason, T. 1983. “Bell-Boeing JVX Tilt Rotor Program: Flight Test Program.” In 2nd Flight Testing Conference. AIAA 1983-2726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2726
• Thomason, T. 1990. “The Bell Helicopter XV-3 and XV-15 Experimental Aircraft: Lessons Learned.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3265
• Thompson, M. O. 1964. Aerospace Medical and Bioengineering Considerations in Lifting-Body and Research- Aircraft Operations. NASA-TM-X-56005. NASA. https://ntrs.nasa.gov/citations/19640012526
• Thompson, M. 1966. “Progress Report on the Manned Lifting Body Flight Test Program.” In 3rd Annual Meeting. AIAA 1966-838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-838
• Thompson, M. O. 1970a. Lifting-Body Progress Report. NASA-TM-X-66712. NASA. https://ntrs.nasa.gov/citations/19710008953
• Thompson, M. O. 1970b. “A Progress Report on the Lifting Body Flight Test Program.” In AMERICAN ASTRONAUTICAL SOCIETY. https://ntrs.nasa.gov/citations/19710034122
• Thompson, Randy. 2016. “X-Plane Structures Challenges Lessons Learned.” In 2016 NESC Structures TDT F2F Meeting. https://ntrs.nasa.gov/citations/20160006108
• Thompson, Avery. 2022. “Cooling Rocket Nozzle Extensions with Supersonic Gas Injection.” Scilight 2022 (7): 071105. https://doi.org/10.1063/10.0009660
• Thompson, K., and K. G. Eitenmiller. 1983. “An Electromechanical Primary Flight Control Actuation System for Military Transport Aircraft.” In Guidance and Control Conference. AIAA 1983-2195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2195
• Thompson, Randy, Bill Lokos, Natalie Spivey, and Matt Moholt. 2017. “Aerostructures X-Plane Airworthiness Guidelines and Best Practices.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170005546
• Thompson, M., and P. Pandolfini. 1995. “The DCAF: A High-Enthalpy, Long-Duration, Direct-Connect Scramjet Test Facility.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6130
• Thompson, Jim R., and John E. Parnell. 1967. “Sonic Boom and the SST: An Examination of the Sonic Boom and Its Effects.” Aircraft Engineering and Aerospace Technology 39 (3): 14–18. https://doi.org/10.1108/eb034241
• Thomson, Douglas G. 2024. “A Brief History of Aerospace Engineering at the University of Glasgow.” Aeronautical Journal: 1–3. https://doi.org/10.1017/aer.2024.116
• Thomson, Douglas. 2025. “A Brief History of Aerospace Engineering at the University of Glasgow.” Aeronautical Journal: 1–3. https://doi.org/10.1017/aer.2025.10102
• Thornburgh, Robert, Andrew Kreshock, Hao Kang, Martin Sekula, Thomas Ivanco, and Garrett McHugh. 2025. “An Experimental Parametric Study on the Whirl-Flutter Stability of Tiltrotors.” In Proceedings of the Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0081-2025-205
• Thornton, Charles. 1994. “Program Management and Control of the B-2 Flight Test Program.” In Biennial Flight Test Conference. AIAA 1994-2163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2163
• Thornton, Charles, and Perry Lamy. 1992. “Measuring Flight Test Progress on Large Scale Development Programs.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4070. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4070
• Thrall, E., Jr. 1975. “PABST: A Technology Demonstrator.” In Aircraft Systems and Technology Meeting. AIAA 1975-989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-989
• Throckmorton, D. 1981. “Research Analysis of Space Shuttle Orbiter Entry Aerothermodynamic Flight Data at the NASA Langley Research Center.” In 1st Flight Test Conference. AIAA 1981-2429. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2429
• Throckmorton, D. A. 1982. “Benchmark Aerodynamic Heat-Transfer Data from the First Flight of the Space Shuttle Orbiter.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820036242
• Throckmorton, David. 1989. “Enabling Technologies Research and Development for the National Aero-Space Plane.” In National Aerospace Plane Conference. AIAA 1989-5009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5009
• Throckmorton, D. A., and L. C. Hartung. 1984a. Analysis of Entry Aerodynamic Heat-Transfer Data for the Orbiter Wing Lower Surface. AIAA PAPER 84-0227. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840035171
• Throckmorton, D. A., and L. C. Hartung. 1984b. Computer Graphic Visualization of Orbiter Lower Surface Boundary-Layer Transition. AIAA PAPER 84-0228. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840035172
• Thumati, Balaje T., and Marco P. Schoen. 2005. “Frequency Based Optimal Input Signal Determination for ARX Parameter Estimation of Constraint Systems.” In Dynamic Systems and Control, Parts A and B. ASMEDC. https://doi.org/10.1115/imece2005-79772
• Tian, Xudong, Lihong Chen, Hongbin Gu, Can Liu, Liuwei Cheng, and Xinyu Chang. 2015. “Experimental Study of Combustion Oscillations in a Dual-Mode Scramjet.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3587. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3587
• Tian, Wei, Zhichun Yang, Yingsong Gu, and Yan Ouyang. 2016a. “Aeroelastic Tailoring of a Composite Forward-Swept Wing Using a Novel Hybrid Pattern Search Method.” Journal of Aerospace Engineering 29 (6): 04016056. https://doi.org/10.1061/(asce)as.1943-5525.0000652
• Tiarn, Weihnurng, and Robert Cavalleri. 1991. “CFD Evaluation of Transonic-Supersonic Wave Front Propagation Effects.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1657. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1657
• Tice, David, and Glenn Martin. 1992. “A Study of Altitude-Constrained Supersonic Cruise Transport Concepts.” In Aerospace Design Conference. AIAA 1992-1027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1027
• Tihansky, Dennis P. 1976. “Confidence Assessment of Military Airframe Cost Predictions.” Operations Research 24 (1): 26–43. https://doi.org/10.1287/opre.24.1.26
• Tijerina, Nicholas, Karolos Grigoriadis, and Edwin E. Forster. 2025. “State-Space Modeling and Analysis of Morphing Trailing Edge Flaps for Active Flutter Suppression.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3555. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3555
• “Tile-Gap Flow in the Shuttle Orbiter Thermal Protection System.” 1983. In Entry Vehicle Heating and Thermal Protection Systems: Space Shuttle, Solar Starprobe, Jupiter Galileo Probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865626.0271.0299
• Timme, S., S. Marques, and K. Badcock. 2010. “Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8228
• Timme, Sebastian, and Reik Thormann. 2016. “Towards Three-Dimensional Global Stability Analysis of Transonic Shock Buffet.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3848
• Timmer, W. A. 2008. “Two-Dimensional Low-Reynolds Number Wind Tunnel Results for Airfoil NACA 0018.” Wind Engineering 32 (6): 525–37. https://doi.org/10.1260/030952408787548848
• Ting, L. 1978. Sonic Boom Research. NASA-CR-157964. NASA. https://ntrs.nasa.gov/citations/19790007589
• Ting, Kuang-Ying, John Berg, Mehran Mesbahi, and Eli Livne. 2026. “Aeroservoelastic Wind Tunnel Evaluation of H∞ Active Flutter Suppression.” In AIAA SCITECH 2026 Forum. AIAA 2026-1058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1058
• Ting, Eric, Daniel Chaparro, and Nhan T. Nguyen. 2017a. “Aero-Structural Optimization of Variable Camber Continuous Trailing Edge Flap Configurations Using Transonic and Viscous Potential Flow Method.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-4220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4220
• Ting, Eric, Daniel Chaparro, and Nhan T. Nguyen. 2017b. “Development of an Integrated Nonlinear Aeroservoelastic Flight Dynamic Model of the Truss-Braced Wing Aircraft.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-1815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1815
• Ting, Eric, Tung Dao, and Nhan T. Nguyen. 2015. “Aerodynamic Load Analysis of a Variable Camber Continuous Trailing Edge Flap System on a Flexible Wing Aircraft.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1839
• Ting, Eric, Kevin W. Reynolds, Nhan T. Nguyen, and Joseph Totah. 2014. “Aerodynamic Analysis of the Truss-Braced Wing Aircraft Using Vortex-Lattice Superposition Approach.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2597. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2597
• Ting, P. C., W. C. Rochelle, and D. M. Curry. 1986. Comparison of Viscous Shock Layer and Boundary Layer Reentry Heating Techniques for Orbiter Nose Cap. AIAA PAPER 86-1350. NASA Lyndon B. Johnson Space Center. https://ntrs.nasa.gov/citations/19860055208
• Ting, Paul C., William C. Rochelle, and Donald M. Curry. 1988. “Prediction of Aerodynamic Heating and Pressures on Shuttle Entry Air Data System (SEADS) Nose Cap and Comparison with STS-61C Flight Data.” In International Conference on Hypersonic Flight in the 21st Century. https://ntrs.nasa.gov/citations/19890066979
• Tirtey, Sandy, H. Bolnot, H. Bottini, S. Paris, Douglas Fletcher, and Olivier Chazot. 2008. “In-Flight Hypersonic Roughness Induced Transition Experiment.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-250
• Tirtey, Sandy, Russell Boyce, L. Brown, and M. Creagh. 2011. “The SCRAMSPACE I Hypersonic Flight Experiment Feasibility Study.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2277
• Tirtey, Sandy, Louis Walpot, and Olivier Chazot. 2009. “Characterization of Hypersonic Roughness­ Induced Transition for the EXPERT Flight Experiment.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7215
• Tirtey, Sandy, L. Walpot, Olivier Chazot, and Douglas Fletcher. 2006. “Experimental Characterization of Hypersonic Boundary Layer in Flight and in Wind-Tunnel Condition.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7940
• Tischler, Mark B. 1988. “Advancements in Frequency-Domain Methods for Rotorcraft System Identification.” In International Conference on Rotorcraft Basic Research. https://ntrs.nasa.gov/citations/19880064541
• Tischler, Mark B. 1989. “Advancements in Frequency-Domain Methods for Rotorcraft System Identification.” Vertica 13 (3, 19). https://ntrs.nasa.gov/citations/19900025716
• Tischler, Mark B. 1995. System Identification Methods for Aircraft Flight Control Development and Validation. NASA-TM-110369. NASA. https://ntrs.nasa.gov/citations/19960003220
• Tischler, Mark B. 2018. “System Identification Methods for Aircraft Flight Control Development and Validation.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-2
• Tischler, Mark B., and Chris A. Tomashofski. 1999. “Flight Test Identification of SH-2G Dynamics in Support of Digital Flight Control System Development.” In Proceedings of the Vertical Flight Society Forum 55 - Montreal, Canada 1999. The Vertical Flight Society. https://doi.org/10.4050/vfs-f55-00083
• Tishkoff, Julian M. 2016. “Dyna-Soar: What Might Have Been.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1643
• “Titan II Research and Development Flight Test History.” 2002. In Titan II. University of Arkansas Press. https://doi.org/10.2307/j.ctvvng4n.10
• Tiwari, S., T. Abdel-Salam, S. Chaturvedi, and T. Mohieldin. 2001. “Study of Dual-Mode Flowfield in Scramjet Combustor.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-380
• Tjatra, I., and Wijaya Sekar. 1998. “Calculation of Three-Dimensional Unit Impulse Response Using Nonlinear Transonic Flow Equations.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4452
• Tkalenko, R. A. 1969. “Slender Bodies of Revolution with Minimum Wave Drag in Nonequilibrium Supersonic Flow.” Fluid Dynamics 4 (6): 47–49. https://doi.org/10.1007/bf01032473
• Tobiason, E., and R. McShea. 1986. “X-29 Ground and Flight Subsystem Testing.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9781
• Toker, O., and H. Ozbay. 1995. “Robustness Analysis of Controllers Designed for Active Flutter Suppression.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 1. American Autom Control Council. https://doi.org/10.1109/acc.1995.529233
• Tokugawa, Naoko, and Kenji Yoshida. 2006. “Transition Detection on Supersonic Natural Laminar Flow Wing in the Flight.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3165
• Tokuyama, Ayano, Kenji Sakai, and Hideto Taya. 1993. “Experimental Study of Sonic Boom Acceptance.” In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-3961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3961
• Tom, Jonathan, Michael Brennison, and David Royer. 2009. “Instrumenting a Cessna 182RG for Data Acquisition Flight Test.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5733. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5733
• Tomaine, R. L., W. H. Bryant, and W. F. Hodge. 1978. “VALT Parameter Identification Flight Test.” In European Rotorcraft and Powered Lift Aircraft Forum. https://ntrs.nasa.gov/citations/19780061530
• Tomek, W. G., R. M. Hall, R. A. Wahls, J. M. Luckring, and L. R. Owens. 2002. Investigation of Reynolds Number Effects on a Generic Fighter Configuration in the National Transonic Facility. AIAA Paper 2002-0418. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20020017577
• Tomek, W. G., R. A. Wahls, L. R. Owens, A. B. Burner, S. S. Graves, and J. M. Luckring. 2003. “Investigation of Aerodynamics Scale Effects for a Generic Fighter Configuration in the National Transonic Facility (Invited).” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030007788
• Tomić, Miloš C., Zoran V. Djinović, Michael Scheerer, and Slobodan J. Petricevic. 2017. “Measurement of Morphing Wing Deflection by a Cross-Coherence Fiber Optic Interferometric Technique.” Smart Materials and Structures 27 (1): 015017. https://doi.org/10.1088/1361-665x/aa9afe
• Tomioka, Sadatake, Masahiro Takahashi, Kan Kobayashi, Kouichiro Tani, Kiyoshi Nojima, and Takuya Arakawa. 2016. “Performance Prediction of Diverging Dual-Mode Combustors at Ramjet-Mode Operation.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-4758. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4758
• Tongue, Stephen, and Charles W. Dingell. 1999. “The Porous Plate Sublimator as the X-38/CRV (Crew Return Vehicle) Orbital Heat Sink.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/1999-01-2004
• Tongue, Stephen, Vern Swartley, and Charles W. Dingell. 1997. “The Porous Plate Sublimator as the X-38/CRV(Crew Return Vehicle) Orbital Heat Sink.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/972411
• Torenbeek, Egbert. 2016. Blended Wing Body Aircraft: A Historical Perspective. Wiley. https://doi.org/10.1002/9780470686652.eae1003
• Torok, Michael S. 1996. “Aeroelastic Analysis of Active Rotor Control Concepts for Vibration Reduction.” In Proceedings of the Vertical Flight Society Forum 52 - Washington, DC 1996. The Vertical Flight Society. https://doi.org/10.4050/vfs-f52-1022
• Torres, Antonio J. Conesa. 2017. Flow Structure Modification Using Plasma Actuation for Enhanced UAV Flight Control. Wiley. https://doi.org/10.1002/9781118928691.ch16
• Torrez, Sean, Derek Dalle, and James Driscoll. 2011. “Multidisciplinary Optimization of the Fuel Consumption of a Dual Mode Scramjet-Ramjet.” In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2011-5757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-5757
• Tournes, Christian H. 2013. “Compendium of Flight Mechanics Formulae Applied to Hypersonic Gliders.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4609
• Tournes, Christian, and C. Johnson. 1998. “Ramjet-Powered Reusable Launch Vehicle Control by Subspace Stabilization.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4151. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4151
• Tow, David. 2010. Implementation of the Enhanced Flight Termination System at National Aeronautics and Space Administration Dryden Flight Research Center. DFRC-E-DAA-TN1609. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20110003558
• Townsend, Guy M., and Alfred D. Phillips. 1955. Phase 4 Flight Test of the Boeing B-52A Airplane, USAF No. 52-003. Defense Technical Information Center. https://doi.org/10.21236/ad0080282
• Townsend, Guy M., and Alfred D. Phillips. 1956. Phase IV Flight Test of the Boeing B-52A Airplane USAF No. 52-003. Addendum i. Defense Technical Information Center. https://doi.org/10.21236/ad0088187
• Toyoda, Atsushi, Akihiro Sasoh, Takahiro Imaizumi, Takeshi Ooyama, Masashi Kanamori, and Takashi Aoyama. 2015. “Near Field Pressure Measurement around Free Flight 69 Degree Swept Back Delta Wing Model.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1253
• Tracy, H. 1981. “F-4 Advanced Avionics Flight Test.” In 1st Flight Test Conference. AIAA 1981-2464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2464
• Tran, Dong, and Rick Lind. 2010. “Parameterizing Stability Derivatives and Flight Dynamics with Wing Deformation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8227
• Tran, Steven, US Army CCDC AvMC, and Joon Lim. 2020. “Investigation of the Interactional Aerodynamics of the XV-15 Tiltrotor Aircraft.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16464
• Trankle, Thomas, and Stephen Bachner. 1993. “Identification of a Full Subsonic Envelope Nonlinear Aerodynamic Model of the F-14 Aircraft.” In Flight Simulation and Technologies. AIAA 1993-3634. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3634
• Trankle, T., and U. Rabin. 1983. “Filtering Flight Data Prior to Aerodynamic System Identification.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2098
• “The Transformation of Aerodynamic Stability Derivatives from a Body Axes Reference to a Wind Axes Reference.” 1997. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-340-63200-0.50025-3
• “The Transformation of Aerodynamic Stability Derivatives from a Body Axes Reference to a Wind Axes Reference.” 2007. In Flight Dynamic Principles. Elsevier. https://doi.org/10.1016/b978-075066927-6/50026-x
• “Transformation of Aerodynamic Stability Derivatives from a Body Axes Reference to a Wind Axes Reference.” 2013. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-08-098242-7.00032-8
• “Transonic Aircraft Configurations.” 2012. In Aerodynamic Principles of Flight Vehicles. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600869174.0171.0220
• “Transonic and Supersonic Flight.” 1992. In Aircraft Performance. Cambridge University Press. https://doi.org/10.1017/cbo9780511607134.012
• “Transonic and Supersonic Flows.” 2012. In Aerodynamic Principles of Flight Vehicles. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600869174.0129.0170
• “Transonic Flight Test of a Laminar Flow Leading Edge with Surface Excrescences.” 1994. In Biennial Flight Test Conference. AIAA 1994-2142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2142
• “Transonic Maneuver/Cruise Airfoil Design Employing Active Diffusion Control.” 1980. In Viscous Flow Drag Reduction. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865466.0187.0211
• “Transonic Wind Tunnel Wall Interference Corrections for Three-Dimensional Models.” 1982. In 12th Aerodynamic Testing Conference. AIAA 1982-588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-588
• Travassos, R., N. Gupta, K. Iliff, and R. Maine. 1980. “Determination of an Oblique Wing Aircraft’s Aerodynamic Characteristics.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1630
• Travassos, R., and H. Kaufman. 1979. “Parallel Procedures for Aircraft Parameter Identification and State Estimation.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1636
• Traven, Ricardo, and Susan E. Whitley. 1995. Developing Flight Test Techniques to Ensure Proper Rigging of Highly Augmented Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada300965
• Traybar, J. 1970. “An Analysis and Comparison of VTOL-Type Aerodynamic Data Obtained Ina Large Wind Tunnel and a Moving-Model/track Facility.” In Propulsion and ASW Meeting. AIAA 1970-574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-574
• “Trends in Unmanned Planetary Entry.” 1982. In Thermophysics of Atmospheric Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865565.0415.0429
• Trevino, Luis, Gary Schwartz, Peter Paceley, Michael P. J. Benfield, and Michael Griffin. 2012. “Flight Technology Demonstrator Launch Vehicle.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-797. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-797
• “Trim Drag and Maneuvering Flight.” 2010. In Fundamentals of Aircraft and Airship Design. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600867538.0601.0612
• Triplett, W. 1980. “Aeroelastic Tailoring of a Forward Swept Wing and Comparisons with Three Equivalent Aft Swept Wings.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-794
• Triplett, William C., and Stuart, C. Brown. 1952. Lateral and Directional Dynamic-Response Characteristics of a 35 Degree Swept-Wing Airplane as Determined from Flight Measurements. NACA-RM-A52I17. NASA. https://ntrs.nasa.gov/citations/19930087349
• Triplett, William C., Stuart C. Brown, and G. Allan Smith. 1955. The Dynamic-Response Characteristics of a 35 Degree Swept-Wing Airplane as Determined from Flight Measurements. NACA-TR-1250. NASA. https://ntrs.nasa.gov/citations/19930092251
• Trippensee, Gary A., and David P. Lux. 1987. “X-29A Forward-Swept-Wing Flight Research Program Status.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/872418
• Trittler, Martin, Walter Fichter, Rudolf Voit-Nitschmann, Robert Schmoldt, and Klaus Kittmann. 2008. “Preliminary System Identification of the Blended Wing Body Flight Demonstrator VELA 2 from Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6896
• Trotta, Roberto, Martin Kunz, Pia Mukherjee, and David Parkinson. 2009. “Bayesian Experimental Design and Model Selection Forecasting.” In Bayesian Methods in Cosmology. Cambridge University Press. https://doi.org/10.1017/cbo9780511802461.006
• Trudgian, Matthew Allan, Tristan Vanyai, Will O. Landsberg, Hugh Russell, and Ananthanarayanan Veeraragavan. 2025. “A Supercritical Ethylene Fuel Injection System for the T4 Hypersonic Test Facility.” Preprint, . https://doi.org/10.2139/ssrn.5125588
• Truitt, R. W. 1968. Some Aspects of Aerodynamic Heating. North Carolina State Univ. https://ntrs.nasa.gov/citations/19700009384
• Trujillo, B., R. Meyer Jr., and P. Sawko. 1983. “In-Flight Load Testing of Advanced Thermal Protection Systems.” In 2nd Flight Testing Conference. AIAA 1983-2704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2704
• Try, K. W., S. P. Fuad, and A. Gunta. 2020. “Perancangan Awal Flight Test Instrumentation (FTI) Untuk Pesawat Terbang Tanpa Awak Di Pustekbang Lapan.” Technologic 11 (2). https://doi.org/10.52453/t.v11i2.302
• Tsilifis, Panagiotis, Roger G. Ghanem, and Paris Hajali. 2017. “Efficient Bayesian Experimentation Using an Expected Information Gain Lower Bound.” SIAM/ASA Journal on Uncertainty Quantification 5 (1): 30–62. https://doi.org/10.1137/15m1043303
• Tsohas, John, and Stephen Heister. 2010. “Flight-Testing of Pressure Regulated Hydrogen-Peroxide Hybrid Rocket Technology Demonstrator.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6632
• Tsoubanos, Christos M. 1979. Stabilized Terrain Optical Position Sensor (STOPS) Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ada065018
• Tsukamoto, Taro, Dianne DeTurris, and Trevor Foster. 2003. “Separation Flight Testing of a Subsonic Glideback Booster Demonstrator.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-911
• Tsushima, Natsuki, Tomohiro Yokozeki, Weihua Su, and Hitoshi Arizono. 2018. “Nonlinear Aeroelastic Analysis of Composite Morphing Wing with Corrugated Structures.” In American Society for Composites 2018. DEStech Publications, Inc. https://doi.org/10.12783/asc33/26174
• Tuck, Dennis. 1970. “IFR Airworthiness Standards for VTOL Aircraft.” In Proceedings of the Specialists Meeting on Environmental Effects on VTOL Designs - Arlington, Texas 1970. The Vertical Flight Society. https://doi.org/10.4050/sm_env_1970-3097
• Tucker, Warren A., and Robert L. Nelson. 1947. Drag Characteristics of Rectangular and Swept-Back NACA 65-009 Airfoils Having Various Aspect Ratios as Determined by Flight Tests at Supersonic Speeds. NACA-RM-L7C05. NASA. https://ntrs.nasa.gov/citations/19930085612
• Tucker, Aaron A., Helen L. Reed, and William S. Saric. 2016a. “Aircraft Suitability Model Applied to a Laminar Flow Control Flight Experiment.” International Journal of Engineering Systems Modelling and Simulation 8 (3): 157. https://doi.org/10.1504/ijesms.2016.077645
• Tucker, Aaron A., Helen L. Reed, William S. Saric, and Donald T. Ward. 2016b. “Design of Experiments with an Application to Laminar Flow Control Flight Research.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1758. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1758
• Tucker, Aaron A., William S. Saric, and Helen L. Reed. 2014a. “A Flight Test Technique for Precise Angle-of-Attack Measurements with Application to Laminar Flow Control Flight Research.” In 52nd Aerospace Sciences Meeting. AIAA 2014-1117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1117
• Tucker, Aaron A., William S. Saric, and Helen L. Reed. 2014b. “Laminar Flow Control Flight Experiment Design and Execution.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0909
• Tufts, Matthew W., Helen L. Reed, and William S. Saric. 2013. “Design of an Infinite Swept Wing Glove for an in-Flight DRE Experiment.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2411
• Tumuklu, Ozgur, Matthew Jouffray, and Deborah A. Levin. 2021. “Modeling of NO Emissions from a Hypersonic Ground-Based Facility.” In AIAA Scitech 2021 Forum. AIAA 2021-0105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0105
• Tuohy, Seamus. 1998. “An Integrated Vehicle Simulation for the Development and Validation of a Commercial Reusable Launch Vehicle.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 1998-4177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4177
• Tuohy, Ian. 2006. “Advantages of the Woomera Test Facility for Hypersonic Flight Programs.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7909
• Turbeville, Franklin D., Casey Broslawski, and Jonathan S. Cheatwood. 2024. “Progress on Quantitative Infrared Thermography at the NASA Langley Aerothermodynamic Laboratory.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4281
• “Turbojet and Turbofan Engines for a Mach 3 Supersonic Transport.” 1964. In 1st Annual Meeting. AIAA 1964-244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-244
• Turk, Robert N., and Joseph C. Watts. 1964. Engineering Flight Test of the CH-37B. Defense Technical Information Center. https://doi.org/10.21236/ada951589
• Turk, Robert N., and Joseph C. Watts. 1965. Engineering Flight Test of the CH-37B. Defense Technical Information Center. https://doi.org/10.21236/ad0884897
• TÜRkoĞLu, Murat Metehan, Emirhan Dönmez, and İbrahim Özkol. 2026. “A Locally Validated Surrogate-Assisted Design Strategy for a Hypersonic Waverider UnderCoupled Aerodynamic and Aerothermal Constraints.” Preprint, . https://doi.org/10.2139/ssrn.6570198
• Turner, K. J. 1965. “Free-Flight Model Techniques for Aerodynamic Research at Supersonic and Hypersonic Speeds.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50015-4
• Turner, Susan. 2003. “Flight Demonstration of OSP Technologies: Orbital Flight Test of the X-37.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2710. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2710
• Turner, Howard L., and George E. Cooper. 1947. Partial Measurements in Flight of the Flying Qualities of a Grumman XF7F-1 Airplane with a Modified Vertical Tail. NACA-RM-A7D15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20030063925
• Turner, John, Marcus Hoerschgen, Wolfgang Jung, Andreas Stamminger, and Peter Turner. 2006. “SHEFEX: Hypersonic Re-Entry Flight Experiment Vehicle and Subsystem Design, Flight Performance and Prospects.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8115
• Tusharika. 2015. “Application of Kalman Filter for Estimation of Aerodynamic Parameters of an Aircraft Using Simulated Flight Data.” International Journal of Engineering Research and V4 (10). https://doi.org/10.17577/ijertv4is100422
• Tuttle, M. H. 1980. Supersonic Cruise Aircraft Research: An Annotated Bibliography. NASA-TM-81781. NASA. https://ntrs.nasa.gov/citations/19800012831
• Twesme, Joe, and Andy Corzine. 2003. “Naval Air Systems Command (NAVAIR) Unmanned Aerial Vehicle (UAV) Unmanned Combat Aerial Vehicle (UCAV) Distributed Simulation Infrastructure.” In 2nd AIAA “Unmanned Unlimited” Conf. and Workshop & Exhibit. AIAA 2003-6612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6612
• “A Typical Avionics Integration Flight Test Program.” n.d. In Test and Evaluation of Avionics and Weapon Systems. Institution of Engineering and Technology. https://doi.org/10.1049/sbra507e_ch11
• “A Typical Avionics Integration Flight Test Program.” 2010. In Test and Evaluation of Aircraft Avionics and Weapons Systems. Institution of Engineering and Technology. https://doi.org/10.1049/sbra033e_ch11
• UAV Flight Testing. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch16
• Uddin, Naseem. 2022. “Dimensional Analysis and Similitude.” In Fluid Mechanics. CRC Press. https://doi.org/10.1201/9781003315117-5
• Ueba, Masazumi, Tomohiro Kamata, Sakurako Nakajima, and Yosuke Maeda. 2021. “Verification of Fully Autonomous Flight from Takeoff to Landing of a Low-Speed Model Airplane with Application to a Small Unmanned Supersonic Airplane.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 19 (5): 667–75. https://doi.org/10.2322/tastj.19.667
• Ueba, Masazumi, Yuichi Takaku, Kouhei Takahashi, and Tomohiro Kamata. 2019. “Design and Tests of Guidance and Control Systems for Autonomous Flight of a Low-Speed Model Airplane for Application to a Small-Scale Unmanned Supersonic Airplane.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 17 (2): 220–26. https://doi.org/10.2322/tastj.17.220
• Ueno, Atsushi, Shunsuke Imamura, and Hideyuki Taguchi. 2011. “Experimental and Numerical Study on Aerodynamic Design of Hypersonic Vehicle.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2340
• Ueno, Atsushi, Hiroaki Ishikawa, Shinya Koganezawa, and Yoshikazu Makino. 2023. “Robust Sonic Boom Reduction in Primary Boom Carpet.” In Proceedings of Meetings on Acoustics, vol. 52. ASA. https://doi.org/10.1121/2.0001900
• Ueno, Atsushi, and Yoshikazu Makino. 2021. “Robust Low-Boom Design in Primary Boom Carpet.” In AIAA Scitech 2021 Forum. AIAA 2021-1270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1270
• Ueno, Makoto, Wataru Sarae, Takeshi Tsujimoto, Masaaki Yanagihara, Tomonari Hirotani, and Stephanie Venel. 2004. “Aerodynamic Characteristics Estimation of the High Speed Flight Demonstrator Phase II Using Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4943
• Ueno, Makoto, Yukimitsu Yamamoto, Akira Koike, Masaaki Yanagihara, and Yoshikazu Miyazawa. 2002. “Pre-Flight Wind Tunnel Test of High Speed Flight Demonstration Phase II.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-3064. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3064
• Ueno, Makoto, Yukimitsu Yamamoto, Masaaki Yanagihara, Michel Leplat, and Jean Oswald. 2007. “Assessment of Wind Tunnel and CFD Transonic Base Pressure Using Flight Data.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4566
• Uhl, Tadeusz, and Maciej Petko. 2007. “Real-Time Flutter Detection from in-Flight Vibration Data.” Key Engineering Materials 347: 679–84. https://doi.org/10.4028/www.scientific.net/kem.347.679
• Ulbrich, Norbert. 2010. “Correlation of Wind Tunnel and Flight Test Results for a P-51B Airplane.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-742. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-742
• Ulbrich, Norbert, and Alan Boone. 2004. “Uncertainty Analysis of Test Data in the Ames 11-Foot Transonic Wind Tunnel.” In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2004-2195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2195
• Ulbrich, N., and F. Steinle Jr. 1994. “Real-Time Wall Interference Calculation in Three-Dimensional Subsonic Wind Tunnel Testing.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-771
• Unnikrishnan, Sasidharan, and Datta V. Gaitonde. 2018. “Kovasznay-Type Analysis of Transition Modes in a Hypersonic Boundary Layer.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-2086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2086
• “Unstable Aircraft Identification.” 2006. In Flight Vehicle System Identification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866852.0295.0334
• “Unstable Aircraft Identification.” 2015. In Flight Vehicle System Identification: A Time-Domain Methodology, Second Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102790.0335.0378
• Uppoor, Vivek, Inderjit Chopra, and Chloe Johnson. 2026. “Wind Tunnel Flowfield and Performance Measurements of a Dynamically-Scaled Lift- and Thrust-Compounded Rotorcraft in High-Speed Flight.” In Proceedings of the Vertical Flight Society 82nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0082-2026-0148
• Uribe Quintero, Everardo, Timothy T. Takahashi, and Ramana Grandhi. 2024. “Flight Dynamics Issues of Control Coupling / Inertia Coupling Prone High-Speed Aircraft.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4048
• Urnes, James M., Stephen E. Hoy, Robert N. Ladage, and James Stewart. 1993. “A Neural Based Intelligent Flight Control System for the NASA F-15 Flight Research Aircraft.” In NASA. Johnson Space Center, Proceedings of the Third International Workshop on Neural Networks and Fuzzy Logic, Volume 1. https://ntrs.nasa.gov/citations/19930013179
• Urnes, James, and Robert Yeager. 1991. “Flight Demonstration of the Self-Repairing Flight Control System in a NASA F-15 Aircraft.” In Aircraft Design and Operations Meeting. AIAA 1991-3106. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3106
• Urschel, Peter, and Timothy Cox. 2003. “Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5544
• Ursu, Ioan, Dragos Daniel Ion Guta, Daniela Enciu, George Tecuceanu, and Aurelian Andrei Radu. 2018. “Flight Envelope Expansion Based on Active Mitigation of Flutter via a V-Stack Piezoelectric Actuator.” Journal of Physics: Conference Series 1106: 012033. https://doi.org/10.1088/1742-6596/1106/1/012033
• Usry, J. W., and J. W. Wallace. 1971. Drag of a Supercritical Body of Revolution in Free Flight at Transonic Speeds and Comparison with Wind Tunnel Data. NASA-TN-D-6580. NASA. https://ntrs.nasa.gov/citations/19720004249
• Utomo, Muhammad Adnan, and Romie Oktavianus Bura. 2019. “Design of Inward-Turning External Compression Supersonic Inlet for Supersonic Transport Aircraft.” INSIST 2 (2): 104. https://doi.org/10.23960/ins.v2i2.90
• Utsumi, Yuki, and Shigeru Obayashi. 2010. “Design of Supersonic Biplane Aircraft Concerning Sonic Boom Minimization.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4962. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4962
• V/STOL Tilt Rotor Aircraft Study. Volume 2: Preliminary Design of Research Aircraft. 1972. NASA-CR-114438. NASA. https://ntrs.nasa.gov/citations/19730014238
• Vachon, Jake, Ronald Ray, and Carl Calianno. 2004. “Calculated Drag of an Aerial Refueling Assembly through Airplane Performance Analysis.” In Cal Tech GALCIT Seminar. https://ntrs.nasa.gov/citations/20060047787
• Vadillo, Jose, and Ramesh Agarwal. 2007. “Numerical Study of Transonic Drag Reduction for Flow past Airfoils Using Active Flow Control.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-712
• Vadillo, Jose, and Ramesh K. Agarwal. 2009. “Numerical Study of Transonic Drag Reduction for Flow past Airfoils Using Active Flow Control.” In Computational Fluid Dynamics 2006. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-92779-2_91
• Vadyak, J., J. D. Hoffman, and A. R. Bishop. 1979. Calculation of the Flow Field in Supersonic Inlets Using a Bicharacteristics Method with Shock Wave Fitting. Purdue Univ. https://ntrs.nasa.gov/citations/19810036808
• Vagianos, Nicholas J., and Eugene C. Rooney. 1964. Flight Test Evaluation of the Uf-Xs Japanese STOL Seaplane. Defense Technical Information Center. https://doi.org/10.21236/ad0625722
• Valasek, John. 1996. “An Eclectic Approach to Undergraduate Flight Dynamics, Stability, and Control Education.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3373
• Valasek, John, and Kenneth Dorsett. 2001. “A Modern Approach to Graduate Flight Dynamics, Stability, and Control Courses.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4312
• Valasek, John, and John Valasek. 1997. “Considerations for Graduate Courses in Flight Dynamics, Stability, and Control.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3569
• Vallone, Michael. n.d. “Parameter Estimation of Fundamental Technical Aircraft Information Applied to Aircraft Performance.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2010.146
• van ‘t Hoff, Stefan, Kees Kapteijn, Oliver Schneider, Keith Soal, and Federico Fonte. 2024. “Whirl Flutter Testing of ATTILA Tiltrotor Testbed: Initial Results.” In Proceedings of the Vertical Flight Society 80th Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0080-2024-1117
• Van Bavel, Luc. 2014. “A Takeoff Rotation Model Including Pilot Technique Parameters for Flight Test Data Reduction and Expansion.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2059
• Van Camp, V., and E. Williams. 1974. “Hypersonic Research Airplane Propulsion for Boost and Test.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-990. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-990
• Van Dalsem, William R. 2019. “Future of Flight: Flying Cars to X-Planes.” In Santa Clara High School - NASA Ames Speakers Event. https://ntrs.nasa.gov/citations/20190027513
• Van Dam, C., B. Holmes, and C. Pitts. 1980. “Effect of Winglets on Performance and Handling Qualities of General Aviation Aircraft.” In Aircraft Systems Meeting. AIAA 1980-1870. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1870
• Van den Borre, Karel, Bayindir H. Saracoglu, and Axel Coussement. 2023. “Numerical Modelling of Hydrogen Combustion Phenomena in a Dual-Mode Ramjet Engine with Cavity Flameholder.” In AIAA SCITECH 2023 Forum. AIAA 2023-0499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0499
• Van der lee, Joel, Neta Yokev, and Dan Michaels. 2021. “Combustion Instability Due to Combustion Mode Transition in a Cavity-Stabilized Scramjet.” In ASCEND 2021. AIAA 2021-4165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-4165
• van der Linden, C. A. A. M., J. K. Sridhar, and J. A. Mulder. 1995. “Multi-Input Design for Aerodynamic Parameter Estimation.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 1. American Autom Control Council. https://doi.org/10.1109/acc.1995.529341
• van der Maas, H. J. 1959. “Lateral and Directional Control and the Measurement of Aerodynamic Coefficients in Steady Asymmetric Flight and in Flight on Asymmetric Power.” In Stability and Control. Elsevier. https://doi.org/10.1016/b978-1-4831-9730-2.50014-4
• Van Der Vooren, J., and A. Van Der Wees. 1990. “Inviscid Drag Prediction for Transonic Transport Wings Using a Full-Potential Method.” In 28th Aerospace Sciences Meeting. AIAA 1990-576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-576
• Van Driest, E. R. 1952. Investigation of Laminar Boundary Layer in Compressible Fluids Using the Crocco Method. NACA-TN-2597. North American Aviation, Inc. https://ntrs.nasa.gov/citations/19930083425
• Van Fossen, G., and Kenneth Dewitt. 1988. “Measurement of Local Convective Heat Transfer Coefficients from a Smooth and Roughened NACA-0012 Airfoil: Flight Test Data.” In 26th Aerospace Sciences Meeting. AIAA 1988-287. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-287
• Van Gaasbeek, James R. 1980. Validation of the Rotorcraft Flight Simulation Program (C81) Using Operational Loads Survey Flight Test Data. Defense Technical Information Center. https://doi.org/10.21236/ada089008
• Van Gool, M., and N. Weingarten. 1981. “Comparison of Low-Speed Handling Qualities in Ground-Based and in-Flight Simulator Tests.” In 1st Flight Test Conference. AIAA 1981-2478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2478
• Van Graas, Frank, and Michael Braasch. 1992. “GPS Interferometric Attitude and Heading Determination: Initial Flight Test Results.” Navigation 38. https://ntrs.nasa.gov/citations/19920047399
• Van Pelt, L. 1981. “Flight Test Concept Evolution.” In 1st Flight Test Conference. AIAA 1981-2375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2375
• van Rooij, Michel, and Russell M. Cummings. 2018. “Aerodynamic Design of an Unmanned Combat Air Vehicle in a Collaborative Framework.” In 2018 Applied Aerodynamics Conference. AIAA 2018-2840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2840
• van Rooij, Michel, Neal T. Frink, Brett R. Hiller, Mehdi Ghoreyshi, and Mark Voskuijl. 2018. “Generation of a Reduced Order Model of an Unmanned Combat Air Vehicle Using Indicial Response Functions.” In 2018 Applied Aerodynamics Conference. AIAA 2018-2998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2998
• Van Wyckhouse, James F. 1966. High-Performance UH-1 Compound Helicopter Maneuver Flight Test Program. Defense Technical Information Center. https://doi.org/10.21236/ad0630927
• Van Zante, Judith F. 2018. “Ground & in-Flight Icing.” In FAA Safety Team Seminar. https://ntrs.nasa.gov/citations/20190002837
• Vanatta, Nicholas, and Michael Inderhees. 1988. “AQM-127A Full Scale Engineering Development Flight Test Program.” In 4th Flight Test Conference. AIAA 1988-2121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2121
• vanDam, C. P., S. M. Los, S. J. Miley, et al. 1995. “Analysis of in-Flight Boundary-Layer State Measurements on a Subsonic Transport Wing in High-Lift Configuration.” In 1st AIAA Aircraft Engineering, Technology, and Operations Congress. https://ntrs.nasa.gov/citations/19960016119
• Vanek, Balint. 2024. “Flight Testing of Active Flutter Control Technology on a Conventional Configuration UAS.” Preprint, . https://doi.org/10.52843/cassyni.xhb81s
• Vanek, Balint, Béla Takarics, Daniel Balogh, et al. 2025. “Flight Testing Active Flutter Suppression Technologies, the Euroean FliPASED Perspective.” In AIAA SCITECH 2025 Forum. AIAA 2025-1851. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1851
• Vanharen, Julien, Adrien Loseille, Frederic Alauzet, and Michael A. Park. n.d. “Nearfield Anisotropic Mesh Adaptation for the Third AIAA Sonic Boom Workshop.” In 2021 AIAA SciTech. https://ntrs.nasa.gov/citations/20205009721
• Varela Martínez, Pau. n.d. “On the Analysis and Design of Series Hybrid Distributed Electric Propulsion with Boundary Layer Ingestion of Remotely Piloted Aircraft.” PhD diss., Universitat Politècnica de València. https://doi.org/10.4995/thesis/10251/192805
• Vassberg, John C., Pieter G. Buning, and Christopher L. Rumsey. 2002. “Drag Prediction for the DLR-F4 Wing/Body Using OVERFLOW and CFL3D on an Overset Mesh.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030005441
• Vaughn, Dusty, Doug Garrard, and Drew Landman. 2012. “Hypersonic Ground Testing Combustion Air Heater Ignition Optimization via Design of Experiments.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-2729. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2729
• Vaughn, Val, and Robert Lindsay. 1988. “Flight Test Imagery: Getting More for Less.” In 4th Flight Test Conference. AIAA 1988-2102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2102
• Vedrenne, M. 1983. “Ariane Flight Testing.” In 2nd Flight Testing Conference. AIAA 1983-2727. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2727
• Vekinis, G., and G. Xanthopoulou. 2010. “Hybrid TPS: A Novel Hybrid Thermal Protection System for Atmospheric Entry Space Probes Based on SHS-Produced MgO/spinel Refractories.” International Journal of Self-Propagating High-Temperature Synthesis 19 (4): 258–75. https://doi.org/10.3103/s1061386210040059
• Velasquez, Andrew. 2013. “Design of NACA 0012 Airfoil and Calibration Setup for Transonic Wind Tunnel.” McNair Scholars Research Journal 17 (1). https://doi.org/10.32855/2642-2492.1597
• Velden, A. 1997. “Multi-Disciplinary Supersonic Transport Design.” In New Design Concepts for High Speed Air Transport. Springer Vienna. https://doi.org/10.1007/978-3-7091-2658-5_17
• Veletas, Mihalis. 2026. “XB-1 Supersonic Demonstrator: Development and Flight Testing from a Flight Analysis Perspective.” In AIAA SCITECH 2026 Forum. AIAA 2026-2636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2636
• Venti, Michael William. 2012. “Prognostics through Ground/Flight Test.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20120011536
• Vepa, Ranjan. 2023a. “Aircraft Flight Control.” In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/9781003266310-8
• Vepa, Ranjan. 2023b. “Longitudinal and Lateral Linear Stability and Control.” In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/9781003266310-6
• Veraar, Ronald. 2008. “Development of a Scaling Technique for Duplication of in-Flight Aerodynamic Heat Flux Distribution in Ground Test Facilities.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2670
• Veraar, Ronald. 2009. “On-Ground Test Conditions to Duplicate Hypersonic Vehicle in-Flight Local Heat Flux Levels.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7379
• Véras, Vinícius Leite de Morais, Leandro Souza de Moura Lima, and Rodrigo Milare Granzoto. 2022. “Air Data Calibration Flight Test Campaign Optimization Using CFD (SAE Paper 2022-01-0025).” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2022-01-0025
• Verma, Hari O., and Nk Peyada. 2018. “Parameter Estimation of Stable and Unstable Aircraft Using Extreme Learning Machine.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0526
• Verma, Hari Om, and Naba Kumar Peyada. 2020. “Aircraft Parameter Estimation Using ELM Network.” Aircraft Engineering and Aerospace Technology 92 (6): 895–907. https://doi.org/10.1108/aeat-01-2019-0003
• Vernon, Lura. 1993. “In-Flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1537. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1537
• Verrastro, Maurizio, and Sylvain Metge. 2015. “Morphing Wing Integrated Safety Approach and Results.” In Smart Intelligent Aircraft Structures (SARISTU). Springer International Publishing. https://doi.org/10.1007/978-3-319-22413-8_2
• “Versa Power, Boeing in DARPA Contract for Ultra-Long-Flight Aircraft.” 2011. Fuel Cells Bulletin 2011 (1): 4–5. https://doi.org/10.1016/s1464-2859(11)70010-4
• Verstynen, H., Jr. 1974. “NASA Flight Research on Aircraft Wake Vortices and Minimization Concepts.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-953
• “Vertical Takeoff and Landing (VTOL), Airships, and Unconventional Vehicles.” 2014. In Designing Unmanned Aircraft Systems. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102615.0461.0492
• Veselenak, Jeff, and Loretta Beutelman. 2004. “The Evolving Role of Developmental Test and Evaluation at the Air Force Flight Test Center.” In USAF Developmental Test and Evaluation Summit. AIAA 2004-6856. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6856
• Vesely, P. 1986. “Computer Graphics Support of a New Era in Flight Test Ground Stations.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9769
• Vetter, H. 1966. “Unified Approach to Lifting-Body Sizing.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-47. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-47
• Vicente, F. A., and Nancy S. Foy. 1963a. Hypersonic Wind Tunnel Facilities in the United States. Defense Technical Information Center. https://doi.org/10.21236/ad0405493
• Vicente, F. A., and Nancy S. Foy. 1963b. Hypersonic Wind Tunnel Facilities in the United States. Revison 1. Defense Technical Information Center. https://doi.org/10.21236/ad0458212
• Vicroy, Dan. 2009. “Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results (Invited).” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-933. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-933
• Vicroy, Dan. 2011. “X-48B Blended Wing Body Ground to Flight Correlation Update.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110011973
• Vidal, R. J. 1974. Correlation Parameters for the Study of Leeside Heating on a Lifting Body at Hypersonic Speeds. Calspan Corp. https://ntrs.nasa.gov/citations/19750012378
• Vijgen, P. M. H. W., J. D. Hardin, and L. P. Yip. 1992. “Flow Prediction over a Transport Multi-Element High-Lift System and Comparison with Flight Measurements.” In California State Univ., The Fifth Symposium on Numerical and Physical Aspects of Aerodynamic Flows. https://ntrs.nasa.gov/citations/19930018259
• Viken, Jeffrey K., Sally Viken, Karen A. Deere, and Melissa Carter. 2017. “Design of the Cruise and Flap Airfoil for the X-57 Maxwell Distributed Electric Propulsion Aircraft.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3922. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3922
• Viladegut Farran, Alan. n.d. “Assessment of Gas-Surface Interaction Modelling for Lifting Body Re-Entry Flight Design.” PhD diss., Universitat Politècnica de Catalunya. https://doi.org/10.5821/dissertation-2117-114631
• Villanueva, Diane C., and Benjamin P. Smarslok. 2015. “Using Expected Information Gain to Design Aerothermal Model Calibration Experiments.” In 17th AIAA Non-Deterministic Approaches Conference. AIAA 2015-0660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0660
• Vincent, J., and S. Franklin. 1981. “Integrated Flight Testing Based on Nonlinear System Identification Data Processing Techniques.” In 1st Flight Test Conference. AIAA 1981-2449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2449
• Vinh, Lam-Son, John Edwards, David Seidel, and John Batina. 1988. “Transonic Stability and Control of Aircraft Using CFD Methods.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4374. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4374
• Vinh, N. X., and Sudhakar Medepalli. 1994. “Optimal Thrust and Aerodynamic Controls in Hypersonic Flight.” In Mechanics and Control. Springer US. https://doi.org/10.1007/978-1-4615-2425-0_14
• Viotto, Roberto, Daniele Francesconi, Samantha Ianelli, et al. 2012. “Advanced Thermal Protection and Locking System for Atmospheric Re-Entry Applications.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5847
• Viswanath, P. R., and G. Rajendra. 1990. “Sting Corrections to Zero-Lift Drag of Axisymmetric Bodies in Transonic Flow.” Aeronautical Journal 94 (938): 279–88. https://doi.org/10.1017/s0001924000023095
• Viviand, H. 1991. “Similitude in Hypersonic Aerodynamics.” In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-84580-2_7
• Vogel, Anja, and Sven Schmitz. 2025. “Extraction of Induced and Wave Drag from CFD Solutions.” In 2025 Regional Student Conferences. AIAA 2025-97647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-97647
• Vogeley, A. W. 1966. Piloted Space-Flight Simulation at Langley Research Center. ASME PAPER 66-WA/AV-2. NASA. https://ntrs.nasa.gov/citations/19670036666
• Voland, R., A. Auslender, M. Smart, A. Roudakov, V. Semenov, and V. Kopchenov. 1999. “CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4848
• Voland, Randall T., Lawrence D. Huebner, and Charles R. McClinton. 2005. “X-43 Hypersonic Vehicle Technology Development.” In 56th International Astronautical Congress 2005. https://ntrs.nasa.gov/citations/20050239566
• Voland, R. T., K. E. Rock, L. D. Huebner, D. W. Witte, K. E. Fischer, and C. R. McClinton. 1998. “Hyper-X Engine Design and Ground Test Program.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20040088578
• Volpe, G. 1988. “Solutions of the Euler Equations for Transonic and Supersonic Aircraft.” In Computational Structural Mechanics & Fluid Dynamics. Elsevier. https://doi.org/10.1016/b978-0-08-037197-9.50011-5
• Vomaske, R. F., R. C. Innis, B. E. Swan, and S. W. Grossmith. 1978. A Flight Investigation of the Stability, Control, and Handling Qualities of an Augmented Jet Flap STOL Airplane. NASA-TP-1254. NASA. https://ntrs.nasa.gov/citations/19780018208
• Vomaske, Richard F., Melvin Sadoff, and Fred J. Drinkwater III. 1961. The Effect of Lateral-Directional Control Coupling on Pilot Control of an Airplane as Determined in Flight and in a Fixed-Base Flight Simulator. NASA-TN-D-1141. NASA. https://ntrs.nasa.gov/citations/19980227082
• Voracek, David F. 1993. Ground Vibration and Flight Flutter Tests of the Single-Seat F-16XL Aircraft with a Modified Wing. NASA-TM-104264. NASA. https://ntrs.nasa.gov/citations/19940006761
• Voracek, David F., Mercedes C. Reaves, Lucas G. Horta, Starr Potter, and David Richwine. 2002. Ground and Flight Test Structural Excitation Using Piezoelectric Actuators. NASA/TM-2002-210724. NASA. https://ntrs.nasa.gov/citations/20020065233
• Vorburger, T., M. McLay, F. Scire, D. Gilsinn, and C. Giauque. 1985. “Surface Roughness Studies for Wind Tunnel Models Used in High Reynolds Number Testing.” In 23rd Aerospace Sciences Meeting. AIAA 1985-228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-228
• Voronin, V. I., and A. I. Shvets. 1981. “Aerodynamic Characteristics of Inverted-V Wings at Subsonic Flight Velocities.” Fluid Dynamics 16 (6): 886–91. https://doi.org/10.1007/bf01089718
• Vos, David, Chris Brown, and Shirley Kozler. 2002. “Implementation and Flight Testing Multivariable Parameter Dependent Control Laws on a Quarter Scale Tailless UCAV Demonstrator Aircraft.” In 1st UAV Conference. AIAA 2002-3428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3428
• Vos, Roelof, Vijayakumari Hodigere-Siddaramaiah, and Jonathan Cooper. 2007a. “Aeroelastic Flight Control for Subscale UAVs.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-1706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1706
• Voss, Arne, Martin Tang, and Julian Sinske. 2026. “Flight Test Instrumentation for Loads and Aeroelastic Analyses of a High Altitude, Long Endurance, Solar Electric Aircraft.” In AIAA SCITECH 2026 Forum. AIAA 2026-1156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1156
• VSTOL Systems Research Aircraft (VSRA) Harrier. 1994. NASA-TM-110117. NASA. https://ntrs.nasa.gov/citations/19950011932
• Vu, Carter, and Graham V. Candler. 2026. “DNS of Hypersonic Boundary Layer Transition in the BOLT II Side a Descent Trajectory.” In AIAA SCITECH 2026 Forum. AIAA 2026-0083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0083
• Wada, Daichi, and Hirotaka Igawa. 2021. “Distributed Fiber Optic Sensing for Aircraft towards in- Flight Structural Control.” In Optical Fiber Sensors Conference 2020 Special Edition. Optica Publishing Group. https://doi.org/10.1364/ofs.2020.w2b.1
• Wada, Daichi, Hirotaka Igawa, Masato Tamayama, Tokio Kasai, Hitoshi Arizono, and Hideaki Murayama. 2018. “Development of Fiber Optic Distributed Sensing System for Aircraft Wing and Its on-Board Monitoring during Flight Tests.” In 26th International Conference on Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.2018.wf98
• Waddington, Michael Jon. n.d. “Development of an Interactive Wave Drag Capability for the OpenVSP Parametric Geometry Tool.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2015.126
• Waddoups, M. 1983. “AFTI/F-16 Technology Demonstrator.” In Aircraft Prototype and Technology Demonstrator Symposium. AIAA 1983-1059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1059
• Wadhams, Tim P., Matthew G. MacLean, Michael S. Holden, and Erik Mundy. 2008. Pre-Flight Ground Testing of the Full-Scale HIFiRE-1 at Fully Duplicated Flight Conditions. Defense Technical Information Center. https://doi.org/10.21236/ada481623
• Waggoner, Erin, Larry J. Cliatt, Michael A. Hill, and Edward A. Haering. 2018. “An Overview of Lessons Learned from Sonic Boom Flight Research Projects Conducted by NASA Armstrong Flight Research Center.” In 2018 Flight Testing Conference. AIAA 2018-3412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3412
• Waggoner, Erin R., Larry James Cliatt, Michael Alan Hill, and Edward A. Haering. 2020. Lessons Learned from Sonic Boom Flight Research Projects Conducted by NASA Armstrong Flight Research Center. AFRC-E-DAA-TN43765. Armstrong Flight Research Center. https://ntrs.nasa.gov/citations/20200011462
• Wagner, R. D., D. V. Maddalon, D. W. Bartlett, and F. S. Collier. 1988. “Fifty Years of Laminar Flow Flight Testing.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/881393
• Wagner, R. D., D. V. Maddalon, D. W. Bartlett, F. S. Collier Jr., and A. L. Braslow. 1992. Laminar Flow Flight Experiments: A Review. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19930057781
• Wagner, D., R. Smith, J. Gunn, and S. Hasegawa. 1990. “Hypersonic Test Facility Requirements for the 1990’s.” In 16th Aerodynamic Ground Testing Conference. AIAA 1990-1389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1389
• Wagner, Mike, and Chuck Webb. 2000. VMCA Flight Test of the Carrier-Landin’, Mail-Hauling’ C-2A. Defense Technical Information Center. https://doi.org/10.21236/ada377905
• Wagner, R. D., Jr., and R. Watson. 1963. Reynolds Number Effects on the Induced Pressures of Cylindrical Bodies with Different Nose Shapes and Nose Drag Coefficients in Helium at a Mach Number of 24. NASA-TR-R-182. NASA. https://ntrs.nasa.gov/citations/19630013806
• Wahls, R., L. Owens, and S. Rivers. 2001. “Reynolds Number Effects on a Supersonic Transport at Transonic Conditions.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-912. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-912
• Waidmann, Winfried, Uwe Brummund, and Joachim Nuding. 2024. “Experimental Investigation of Supersonic Ramjet Combustion (Scramjet).” In Transport Phenomena In Combustion. Routledge. https://doi.org/10.1201/9780203735138-143
• Waisanen, P., and H. Perangelo. 1972. “Real Time Flight Flutter Testing via Z-Transform Analysis Technique.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-784
• Waite, Timothy. 2018. “Singular Prior Distributions in Bayesian D-Optimal Design for Nonlinear Models.” Statistica Sinica. https://doi.org/10.5705/ss.202015.0293
• Waite, Josiah, Bret Stanford, Robert E. Bartels, and Walter A. Silva. 2019. “Active Flutter Suppression Using Reduced Order Modeling for Transonic Aeroservoelastic Control Law Development.” In AIAA Aviation 2019 Forum. AIAA 2019-3025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3025
• Wakayama, Sean. 2000. “Blended-Wing-Body Optimization Problem Setup.” In 8th Symposium on Multidisciplinary Analysis and Optimization. AIAA 2000-4740. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4740
• Walan, Alexander M., and Jeffrey Lydecker. 2023. “DARPA CRANE Program Overview.” In AIAA SCITECH 2023 Forum. AIAA 2023-1807. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1807
• Walberg, G. D., P. M. Siemers III, R. L. Calloway, and J. J. Jones. 1987. The Aeroassist Flight Experiment. IAF PAPER 87-197. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880028707
• Walchli, Lawrence, Robert Guyton, Frank Luria, and Williamj. Gillard. 1992. “High Angle-of-Attack Control Enhancement on a Forward Swept Wing Aircraft.” In Guidance, Navigation and Control Conference. AIAA 1992-4427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4427
• Walchner, O. 1974. Research on Hypersonic Stability Problems. Defense Technical Information Center. https://doi.org/10.21236/ada007045
• Waldersen, Matt. 2018. “Software Defined Wireless Avionics for Flight Test.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20180008673
• Waldersen, Matt, and Otto Schnarr III. 2017. “An Evaluation and Demonstration of a Network Based Aircraft Telemetry System.” In International Test and Evaluation Association. https://ntrs.nasa.gov/citations/20170004612
• Walker, J. H. 1949. “Rocket and Ramjet Supersonic Powerplants.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/490123
• Walker, S. 1973. “Afterbody Drag Flight Test of the a-7E Airplane.” In 9th Propulsion Conference. AIAA 1973-1306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1306
• Walker, B. 1985. “Stability of Adaptive Control Algorithms: Theoretical Examination and Simulation for F-4 Flight Control.” In 7th Computational Fluid Dynamics Conference. AIAA 1985-1966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1966
• Walker, Robert W., and John Y. Kaufman. 1977. A-37B Fatigue Sensor Evaluation Program: Full Scale Test and Field Aircraft Instrumentation,. Defense Technical Information Center. https://doi.org/10.21236/ada042114
• Walker, Gregory W., Arthur E. Phelps III, and W. Todd Hodges. 1993. “A Teleoperated Unmanned Rotorcraft Flight Test Technique.” In NASA. Johnson Space Center, Proceedings of the Third International Workshop on Neural Networks and Fuzzy Logic, Volume 1. https://ntrs.nasa.gov/citations/19930013180
• Walker, Steven, Ming Tang, and Caesar Mamplata. 2009. “TBCC Propulsion for a Mach 6 Hypersonic Airplane.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7238. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7238
• Walker, H. J., and C. H. Wolowicz. 1960. Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-Tunnel Results. NASA-TM-X-287. NASA. https://ntrs.nasa.gov/citations/19650014459
• Walkley, K. 1986. “Wave Drag Analysis of Realistic Fighter Aircraft Using a Full Potential Method.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2627
• Walko, L. C., and J. G. Schneider. 1980. “Full Scale Lightning Test Technique.” In NASA. Langley Res. Center Lightning Technol.. https://ntrs.nasa.gov/citations/19800013466
• Wallace, E. 1978. “Use of Onboard Computerized Flight Test Analysis Systems.” In Aircraft Systems and Technology Conference. AIAA 1978-1462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1462
• Wallace, R. O. 1982. “Aerodynamic Comparisons of Space Shuttle Ascent: STS-1 Flight versus Wind-Tunnel Predictions.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017329
• Wallace, Lane E. 1996. Flights of Discovery: 50 Years at the NASA Dryden Flight Research Center. NASA-SP-4309. NASA. https://ntrs.nasa.gov/citations/19970004281
• Wallace, Elah. 2000. Large Aircraft Coatings Flight Testing. Defense Technical Information Center. https://doi.org/10.21236/ada382563
• Wallskog, Harvey A. 1954. Summary of Free-Flight Zero-Lift Drag Results from Tests of 1/5-Scale Models of the Convair YF-102 and F-102A Airplanes and Several Related Small Equivalent Bodies at Mach Numbers from 0.70 to 1.46. NACA-RM-SL54J25. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090022754
• Walsh, Kevin R. 1992. Summary of the Effects of Engine Throttle Response on Airplane Formation-Flying Qualities. AIAA PAPER 92-3318. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19920066278
• Walsh, Kevin R. 1993. “Summary of the Effects of Engine Throttle Response on Airplane Formation-Flying Qualities.” In AIAA 28th Joint Propulsion Conference and Exhibit. https://ntrs.nasa.gov/citations/19930013934
• Walsh, E., and P. Hart. 1981. “Flight-Measured Liftoff Ignition Overpressure: A Correlation with Subscale Model Tests.” In 1st Flight Test Conference. AIAA 1981-2458. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2458
• Walsh, Michael, William Sellers III, and Catherine McGinley. 1988. “Riblet Drag Reduction at Flight Conditions.” In 6th Applied Aerodynamics Conference. AIAA 1988-2554. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2554
• Walsh, Scott N., Tim M. Wildey, and John D. Jakeman. 2017. “Optimal Experimental Design Using a Consistent Bayesian Approach.” ASCE-ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering 4 (1): 011005. https://doi.org/10.1115/1.4037457
• Walters, Edward, and Joseph Butler. 1992. “Extended Range Interceptor (ERINT-1) Flight Test Program.” In Annual Interceptor Technology Conference. AIAA 1992-2756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2756
• Waltrup, P., F. Billig, and M. Evans. 1980. “Critical Considerations in the Design of Supersonic Combustion Ramjet /Scramjet/ Engines.” In 16th Joint Propulsion Conference. AIAA 1980-1284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1284
• Wan, Zhiqiang, Chao Yang, and Congqing Zou. 2003a. “Design Studies of Aeroelastic Tailoring of Forward-Swept Composite Aircraft Using Hybrid Genetic Algorithm.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1491. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1491
• Wan, Zhiqiang, Chao Yang, and Congqing Zou. 2003b. “Divergence Experiment Prediction Techniques of Flat-Plate Forward-Swept Wing in Wind Tunnel.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1416
• Wang, Junli. 2019. “Transonic Static Aeroelastic and Longitudinal Aerodynamic Characteristics of a Low-Aspect-Ratio Swept Wing.” AIP Advances 9 (4): 045203. https://doi.org/10.1063/1.5087963
• Wang, Shaonan. 2024a. “Application of a Modal Parameter Identification Method Based on Variational Mode Decomposition in Flight Flutter Testing.” Journal of Physics: Conference Series 2762 (1): 012050. https://doi.org/10.1088/1742-6596/2762/1/012050
• Wang, Lei. 2024b. “Research on Minimum Unstick Speed Flight Test Method for Civil Aircraft.” Advances in Computer and Engineering Technology Research 1 (4): 120. https://doi.org/10.61935/acetr.4.1.2024.p120
• Wang, J., M. Demiroz, and P. Talbot. 1986. “Flight Test Planning and Parameter Extraction for Rotorcraft System Identification.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9772
• Wang, Wei, He Feng, Shenao Cui, and Zhandong Li. 2025c. “Multi-Objective Optimization of Transonic Variable-Camber Airfoil with Leading and Trailing Edge Deflections Using Kriging Surrogate Model.” Preprint, . https://doi.org/10.20944/preprints202501.2203.v1
• Wang, Na, and Chao Gao. 2013. “Variable Reynolds Number Experimental Study on Aerodynamic Characteristic of Supercritical Airfoil RAE2822.” Applied Mechanics and Materials 420: 42–46. https://doi.org/10.4028/www.scientific.net/amm.420.42
• Wang, Zhongyu, and Shiqiang Hu. 2026. “Iso-Performance Control Allocation for Distributed Electric Propulsion Systems.” In AIAA AVIATION 2026 Forum. AIAA 2026-4730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4730
• Wang, Xiaowen, and Eswar Josyula. 2016. “Computational Study of Non-Equilibrium Effects on Hypersonic Boundary-Layer Transition.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1248
• Wang, Zhongjun, C. Lan, and Jay Brandon. 2000. “Unsteady Aerodynamic Effects on the Flight Characteristics of an F-16XL Configuration.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3910. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3910
• Wang, Yongzhi, Feng Li, and Andrea Da Ronch. 2016a. “Adaptive Feedback Control for Gust Loads Alleviation: From Simulation to Wind Tunnel Test.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-2006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2006
• Wang, Kaiqiang, and Fanxi Lyv. 2025. “Rapid Geometric Modeling and Performance Analysis of Hypersonic Airplane for Conceptual Design.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-3576-4_39
• Wang, Ning, Xinbing Su, Binlin Ma, and Xiaofei Zhang. 2018b. “Numerical Study on Influence of Canard Height on Aeroelastic Behavior of Forward-Swept Wing.” IOP Conference Series: Materials Science and Engineering 452: 042048. https://doi.org/10.1088/1757-899x/452/4/042048
• Wang, Zexi, Zhiqiang Wan, Siyan Zhu, and Chao Yang. 2019. “Structure Analysis and Aeroelastic Optimization Method for Composite Wing-Box Structure with Curved Fiber.” In AIAA Scitech 2019 Forum. AIAA 2019-0419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0419
• Wang, Yu, Wei Yao, and Zheng Zhang. 2024a. “IDDES Simulation of the Combustion Mode Transition Process in a Dual-Mode Scramjet Based on Dynamic Zone Flamelet Model.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4412
• Wang, Shujie, Rongxi Yuan, and Ruiqin Chang. 1987. “Investigation of Wall Interference at High Angle of Attack in a Low Speed Wind Tunnel with Slotted Wall.” In 5th Applied Aerodynamics Conference. AIAA 1987-2611. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2611
• Wang, Guichen, Zhou Zhou, Jianxing Wang, Yilin Chen, and Rui Wang. 2026b. “A Short Landing Control Strategy for a Distributed Electric Propulsion UAV Incorporating Propulsion-Induced Lift.” Preprint, . https://doi.org/10.2139/ssrn.7589121
• Wangu, Srimal, and William Mouyos. 1998. “Reusable Launch Vehicle System Health Management.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5239
• Ward, J. 1984. “An Updated History of NACA/NASA Rotary-Wing Aircraft Research 1915-1984.” Vertiflite 30. https://ntrs.nasa.gov/citations/19840050373
• Ward, Donald. 1988. “A Project-Oriented Introduction to Flight Test Engineering.” In 4th Flight Test Conference. AIAA 1988-2116. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2116
• Ward, D., and A. Bennett Jr. 1974. “Flight Test Investigation of the Sailplane as a Post-Stall Research Vehicle.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-951. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-951
• Ward, D., and S. Miley. 1983. “An Evaluation of Flight Test Measurement Techniques for Obtaining Airfoil Pressure Distributions and Boundary Layer Transition Locations.” In 2nd Flight Testing Conference. AIAA 1983-2689. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2689
• Ward, L. K., and A. W. Myers. 1967. Free-Flight Testing of Aerodynamic Decelerators in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0815090
• Ward, D. T., F. C. Taylor, and J. T. P. Doo. 1985. Comparison of Predicted and Measured Drag for a Single-Engine Airplane. AIAA PAPER 85-4038. Texas A&M University. https://ntrs.nasa.gov/citations/19860026229
• Wardana, T. K., F. S. Pranoto, and G. Akhiri. 2021. “Performance Comparison of Unmanned Aircraft System (UAS) Flight Controller with Independent Flight Test Instrumentation (FTI) during Flight.” In AIP Conference Proceedings, vol. 2366. AIP Publishing. https://doi.org/10.1063/5.0060371
• Warner, D. N., and F. J. Moran. 1979. Flight Test of Navigation and Guidance Sensor Errors Measured on STOL Approaches. NASA-TM-81154. NASA. https://ntrs.nasa.gov/citations/19800004786
• Warsop, Clyde, and William Crowther. 2019. “NATO AVT-239 Task Group: Flight Demonstration of Fluidic Flight Controls on the MAGMA Subscale Demonstrator Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-0282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0282
• Wassel, A., F. Issacci, and Va. 1995. “An Integrated Modeling Approach for Hypersonic Aircraft Thermal Management.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6022
• Wasson, R., Jr. 1977. “A Unique Ground Test Facility for Exhaust Plume Investigations at Simulated Altitude Flight Conditions.” In 15th Aerospace Sciences Meeting. AIAA 1977-152. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-152
• Waszak, Martin. 1996. “Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3437. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3437
• Waszak, Martin, and Carey Buttrill. 1991. “Design of an Active Flutter Suppression System for the Active Flexible Wing.” In Aircraft Design and Operations Meeting. AIAA 1991-3111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3111
• Waszak, Martin, John Davidson, and Peter Ifju. 2002. “Simulation and Flight Control of an Aeroelastic Fixed Wing Micro Aerial Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4875
• Waszak, Martin, and Jimmy Fung. 1996. “Parameter Estimation and Analysis of Actuators for the BACT Wind-Tunnel Model.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3362
• Waszak, Martin, and S. Srinathkumar. 1991. “Active Flutter Suppression: Control System Design and Experimental Validation.” In Navigation and Control Conference. AIAA 1991-2629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2629
• Waszak, M., and S. Srinathkumar. 1992. “Flutter Suppression for the Active Flexible Wing: Control System Design and Experimental Validation.” In Dynamics Specialists Conference. AIAA 1992-2097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2097
• Waszkowski, Peter, and Nicholas Pisani. 2025. “A Review of Hypersonic Vehicle Engine Optimization.” In 2025 Regional Student Conferences. AIAA 2025-99583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-99583
• Watanabe, Shigeya, Shinji Ishimoto, and Yukimitsu Yamamoto. 1996. “Aerodynamic Characteristics Evaluation of the Hypersonic Flight Experiment (HYFLEX) Vehicle Based on Flight Data.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4527
• Watanabe, Shigeya, Ryoji Takaki, Yukimitsu Yamamoto, Shigeya Watanabe, Ryoji Takaki, and Yukimitsu Yamamoto. 1997b. “RCS Gas-Jet Interaction in the Hypersonic Flight Experiment, HYFLEX.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-524
• Waterhouse, Timothy Hugh. n.d. “Optimal Experimental Design for Nonlinear and Generalised Linear Models.” PhD diss., The University of Queensland. https://doi.org/10.14264/107285
• Watson, D. M., and G. H. Hardy. 1983. A Flight-Test Evaluation of a Go-around Control System for a Twin Engine Powered-Lift STOL Airplane. NASA-TM-84408. NASA. https://ntrs.nasa.gov/citations/19840003110
• Wauters, Jolan. 2022. “Design Optimization-under-Uncertainty of a Forward Swept Wing Unmanned Aerial Vehicle Using SAMURAI.” International Journal of Micro Air Vehicles 14: 17568293221092139. https://doi.org/10.1177/17568293221092139
• “Waverider Aircraft.” 2012. In The Aerodynamic Design of Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600869228.0448.0510
• Weatherston, R. 1969. “The Multi-Recompression Heater, a New Concept for Large Scale Hypersonic Testing.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-332
• Webb, L. D., S. A. Whitmore, and R. L. Janssen. 1979. “Preliminary Flight and Wind Tunnel Comparisons of the Inlet/airframe Interaction of the F-15 Airplane.” In American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19790039500
• Weber, Richard J. 1975. “The NASA Research Program on Propulsion for Supersonic Cruise Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/750629
• Weber, C., R. Behr, and C. Weiland. 2000. “Investigation of Hypersonic Turbulent Flow over the X-38 Crew Return Vehicle.” In Fluids 2000 Conference and Exhibit. AIAA 2000-2601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2601
• Weeks, T. 1969. “Effects of Flow Unsteadiness on Hypersonic Wind Tunnel Spectroscopicdiagnostics.” In 3rd Flight Test, Simulation, and Support Conference. AIAA 1969-331. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-331
• Wegener, Peter P., and R. Kenneth Lobb. 1952. An Experimental Study of a Hypersonic Wind-Tunnel Diffuser. Defense Technical Information Center. https://doi.org/10.21236/ad0012779
• Wei, Jun, Wei Gao, Wenxuan Gao, Bei Lu, and Qifu Li. 2024. “Aerodynamic Simulations of an Electric Vertical Takeoff and Landing Aircraft Using Reformulated Vortex Particle Method.” Physics of Fluids 36 (6): 065114. https://doi.org/10.1063/5.0212347
• Wei, Baoxi, Yan Zhang, Liang Tian, Ganglin Song, and Xu Xu. 2012. “Experimental Study on Combustion Mode Transition in an Aero-Ramp Based Scramjet.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-3923. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3923
• Weichsel, H. 1949. “Helicopter Flight Test Technique Variable Blade Stiffness Program.” In Proceedings of the Vertical Flight Society Forum 5 - New York, N.Y. 1949. The Vertical Flight Society. https://doi.org/10.4050/vfs-f5-506
• Weick, Fred E. 1928. Full Scale Drag Tests on Various Parts of Sperry Messenger Airplane. NACA-TN-271. NASA. https://ntrs.nasa.gov/citations/19930081033
• Weidner, J., W. Small, and J. Penland. 1976. “Scramjet Integration on Hypersonic Research Airplane Concepts.” In 12th Propulsion Conference. AIAA 1976-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-755
• Weihs, Hendrik, J. Longo, and J. Turner. 2008. “The Sharp Edge Flight Experiment SHEFEX II, a Mission Overview and Status.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2542
• Weil, Joseph. 1962. Review of the X-15 Program. NASA-TN-D-1278. NASA. https://ntrs.nasa.gov/citations/19620003289
• Weil, J. 1981. Correlation of Predicted and Flight Derived Stability and Control Derivatives with Particular Application to Tailless Delta Wing Configurations. NASA-TM-81361. NASA. https://ntrs.nasa.gov/citations/19810017618
• Weil, Joseph, and Margaret Spear. 1947. Estimated Flying Qualities of the Martin Model 202 Airplane. NACA-RM-L7A31. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019466
• Weilmuenster, K. J., and H. H. Hamilton II. 1982. “A Comparison of Computed Space Shuttle Orbiter Surface Pressures with Flight Measurements.” In Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference. https://ntrs.nasa.gov/citations/19820048389
• Weilmuenster, K., and H. Hamilton II. 1986. “A Comparison of Computed and Measured Aerodynamic Characteristics Ofa Proposed Aeroassist Flight Experiment Configuration.” In 4th Thermophysics and Heat Transfer Conference. AIAA 1986-1366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1366
• Weingarten, N., and C. Chalk. 1982. “In-Flight Investigation of Large Airplane Flying Qualities for Approach and Landing.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1296
• Weinstein, Leonard M. 1994. “An Optical Technique for Examining Aircraft Shock Wave Structures in Flight.” In High-Speed Research: 1994 Sonic Boom Workshop: Atmospheric Propagation and Acceptability Studies. https://ntrs.nasa.gov/citations/19950008465
• Weinstein, W., W. Posingies, R. Eslinger, and H. Gross. 1986. “Control Reconfigurable Combat Aircraft Flight Control System Development.” In Astrodynamics Conference. AIAA 1986-2236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2236
• Weissenburger, J., and N. Zimmerman. 1963. “Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds.” In Testing of Manned Flight Systems Conference. AIAA 1963-1803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1803
• Weisshaar, T. A. 1975. An Investigation of Supersonic Aeroelastic Characteristics of Oblique Winged Aircraft. NASA-CR-146141. NASA. https://ntrs.nasa.gov/citations/19760008948
• Weisshaar, Terrence A. 1978. Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing Structures. Defense Technical Information Center. https://doi.org/10.21236/adb032318
• Weisshaar, T. 1979a. “Divergence of Forward Swept Composite Wings.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-722
• Weisshaar, Terrence A. 1979b. Forward Swept Wing Static Aeroelasticity. Defense Technical Information Center. https://doi.org/10.21236/adb042815
• Weisshaar, T. 1980a. “Aeroelastic Tailoring of Forward Swept Composite Wings.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-795
• Weisshaar, T. A. 1983. Aeroelastic Stability of Forward Swept Composite Winged Aircraft. Purdue University. https://ntrs.nasa.gov/citations/19840055636
• Weisshaar, T. 1990. “Static Aeroelastic Behavior of an Adaptive Laminated Piezoelectric Composite Wing.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-1078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1078
• Weisshaar, T. A., and J. B. Crittenden. 1976. Flutter of Asymmetrically Swept Wings. NASA-CR-146815. NASA. https://ntrs.nasa.gov/citations/19760014076
• Weisshaar, Terrence, and D-H. Lee. 2002. “Aeroelastic Tailoring of Joined-Wing Configurations.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1207
• Weisshaar, T., and T. Zeiler. 1982. “Dynamic Stability of Flexible Forward Swept Wing Aircraft.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1325
• Wells, William. 1987. “Wind-Tunnel Preflight Test Program for Aeroassist Flight Experiment.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2367
• Wells, William L. 1989a. Measured and Predicted Aerodynamic Coefficients and Shock Shapes for Aeroassist Flight Experiment (AFE) Configuration. NASA-TP-2956. NASA. https://ntrs.nasa.gov/citations/19900004869
• Wells, William. 1989b. “Measured and Predicted Aerodynamic Heating on a Cylinder in Wake of AFE Configuration at Incidence.” In 7th Applied Aerodynamics Conference. AIAA 1989-2162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2162
• Wells, Douglas P. 2017. “Cruise Speed Sensitivity Study for Transonic Truss Braced Wing.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1628. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1628
• Wells, W., S. Banda, and D. Quam. 1979. “A Model for Unsteady Effects in Lateral Dynamics for Use in Parameter Estimationaircraft Stability.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1638
• Wells, W., S. Banda, and D. Quam. 1981. “Aircraft Lateral Parameter Estimation from Flight Data with Unsteady Aerodynamic Modelling.” In 19th Aerospace Sciences Meeting. AIAA 1981-221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-221
• Wells, W., and V. Klein. 1982. “Parameter Estimation Applied to General Aviation Aircraft: A Case Study.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1313
• Welsch, Clement J. 1953. The Drag of Finite-Length Cylinders Determined from Flight Tests at High Reynolds Numbers for a Mach Number Range from 0.5 to 1.3. NACA-TN-2941. NASA. https://ntrs.nasa.gov/citations/19930083676
• Welsh, Clement J. 1952. Combustion in the Wake as a Means of Body-Drag Reduction as Determined from Free-Flight Tests of 40-Millimeter Shells. NACA-RM-SL53D01A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029460
• Welsh, Clement J., and John D. Morrow. 1950. Effect of Wing-Tank Location on the Drag and Trim of a Swept-Wing Model as Measured in Flight at Transonic Speeds. NACA-RM-L50A19. NASA. https://ntrs.nasa.gov/citations/19930086176
• Welstead, Jason, Peter C. Frederic, Michael A. Frederick, Steven R. Jacobson, and Jeffrey J. Berton. 2017. “Cost-Driven Design of a Large Scale X-Plane.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1388. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1388
• Welton, J. T. 1965. Free-Flight Telemetry Testing in the Jet Propulsion Laboratory Wind Tunnels. NASA-CR-67114. NASA. https://ntrs.nasa.gov/citations/19650024803
• Wendel, Nathanael J., and Datta V. Gaitonde. 2026. “Numerical Comparison of Square and Circular Cross-Section Dual-Mode Scramjet Isolators.” In AIAA AVIATION 2026 Forum. AIAA 2026-4488. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4488
• Wentz, W. H., A. Ahmed, and R. Nyenhuis. 1985. “Further Results of Natural Laminar Flow Flight Test Experiments.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/850862
• Wentz, W., Jr., and R. Nyenhuis. 1984. “Natural Laminar Flow Flight Experiments on a Swept-Wing Business Jet.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2189. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2189
• Wenxuan, Zhu. 1991. Methods of Guidance Flight Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada254248
• Wercinski, Paul F. 2017. ADEPT SR-1 Flight Experiment. NASA FS-2017-02-01-ARC. NASA. https://ntrs.nasa.gov/citations/20170001940
• Werdes, R. J. 1975. “Transient Flight Flutter Test of a Wing with Tip Tanks.” In NASA, Washington Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003020
• Wernicke, R. 1980. “A Tilt Rotor Design That Provides Economical Extended Range VTOL Transportation to Offshore Oil Platforms.” In Aircraft Systems Meeting. AIAA 1980-1822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1822
• Westbrook, C. 1964. “Handling Qualities of Vtol Aircraft.” In Military Aircraft Systems and Technology Meeting. AIAA 1964-777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-777
• Westerwelt, Pj. 2024. “An Experimental Determination of the Wave Drag Coefficient on Spheres.” In Spring Conference 1985. Institute of Acoustics. https://doi.org/10.25144/22473
• Westhelle, Carlos, and James Masciarelli. 2003. “Assessment of Aerocapture Flight at Titan Using a Drag-Only Device.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5389
• Westphal, Russell, Mark Bleazard, Aaron Drake, Anne Bender, Donald Frame, and Steven Jordan. 2006. “A Compact, Self-Contained System for Boundary Layer Measurements in Flight.” In 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2006-3828. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3828
• Wetmore, J. W. 1947. “A Review of Recent Information Relating to the Drag Rise of Airplanes.” In NACA. Ames Aeron. Lab. NACA Conf. on Aerodyn. Probl. of Transonic Airplane Design. https://ntrs.nasa.gov/citations/19790079920
• Wetzel, Todd Andrew. n.d. “Development of a Finite-Difference Neighboring Optimal Control Law and Application to the Optimal Landing of a Reusable Launch Vehicle.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-10526
• Wey, Pierre, Friedrich Seiler, Julio Srulijes, Myriam Bastide, Bastien Martinez, and Patrick Gnemmi. 2012. “Determination of Aerodynamic Coefficients from Shock Tunnel Free Flight Trajectories.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-3321. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3321
• Whalley, Matthew S., Robert Buckanin, James Roos, and James F. Keller. 2001. “Helicopter Active Control Technology Demonstrator Program.” In Proceedings of the Vertical Flight Society Forum 57 - Washington, D.C. 2001. The Vertical Flight Society. https://doi.org/10.4050/vfs-f57-00090
• Wheatley, John B. 1933. Lift and Drag Characteristics and Gliding Performance of an Autogiro as Determined in Flight. NACA-TR-434. NASA. https://ntrs.nasa.gov/citations/19930091508
• Wheatley, John B. 1934. The Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Autogiro as Determined in Flight. NACA-TR-523. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930091596
• Wheatley, John B. 1935. Wing Pressure Distribution and Rotor-Blade Motion of an Autogiro as Determined in Flight. NACA-TR-475. NASA. https://ntrs.nasa.gov/citations/19930091549
• Wheeler, John. 2000. “Flight Test Applications of Uncertainty Analysis.” In 21st Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2000-2207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2207
• Wheldon, W., and R. Whites. 1966. “Flight Testing of the X-21A Laminar Flow Control Airplane.” In 2nd Aerodynamic Testing Conference. AIAA 1966-734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-734
• Whitbeck, Richard F., James C. Smith, and Thomas T. Myers. 1982. Flight Test of Advanced Digital Control Concepts. Defense Technical Information Center. https://doi.org/10.21236/ada134175
• Whitcomb, Richard T. 1952. A Study of the Zero-Lift Drag-Rise Characteristics of Wing-Body Combinations near the Speed of Sound. NACA-TR-1273. NASA. https://ntrs.nasa.gov/citations/19930092271
• Whitcomb, Richard T. 1953. Recent Results Pertaining to the Application of the “Area Rule”. NACA-RM-L53I15a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019402
• Whitcomb, Richard T. 1956. “Zero-Lift-Drag Characteristics of Wing-Body Combinations at Transonic Speeds.” In 24th Annual Meeting of the Institute of the Aeronautical Sciences. https://ntrs.nasa.gov/citations/19650070830
• Whitcomb, R. T. 1983. “Transonic Empirical Configuration Design Process.” In AGARD Spec. Course on Subsonic(Transonic Aerodyn. Interference for Aircraft. https://ntrs.nasa.gov/citations/19840004011
• Whitcomb, Richard T., and Larry R. Clark. 1965. An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers. NASA-TM-X-1109. NASA. https://ntrs.nasa.gov/citations/19720066117
• White, Maurice D. 1944. Effect of Power on the Stick-Fixed Neutral Points of Several Single-Engine Monoplanes as Determined in Flight. NACA-CB-L4H01. NASA. https://ntrs.nasa.gov/citations/19930092550
• White, J. 1993. “Supersonic/hypersonic Flight Vehicle Forebody Wave Drag Determination Using an Euler-Based CFD Approach.” In Aerospace Design Conference. AIAA 1993-971. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-971
• White, Edward B. 2004. Instrumentation for Wind Tunnel Transient Growth Studies. Defense Technical Information Center. https://doi.org/10.21236/ada421045
• White, Richard P., and Peter Crimi. 1961. Theoretical Investigation of the Flutter Characteristics of a Jet-Flap Rotor System in Hovering Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0275102
• White, Tomas, Alejandro Fonnegra, and Omar Hazbon. 2024a. “Development of a Low Cost and Low Weight Small UAS Flight Test Instrumentation System.” In 2024 Regional Student Conferences. AIAA 2024-85725. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-85725
• White, P., and Tom Gibson. 2004. “Exploitation by Airbus of High Reynolds Number Test Capabilities in the European Transonic Wind Tunnel.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-768
• White, Maurice D., and Robert C. Innis. 1959. A Flight Investigation of the Low-Speed Handling Qualities of a Tailless Delta-Wing Fighter Airplane. NASA-MEMO-4-15-59A. NASA. https://ntrs.nasa.gov/citations/19980232080
• White, Todd R., Milad Mahzari, Deepak Bose, and Jose A. Santos. 2013. “Post-Flight Analysis of Mars Science Laboratory’s Entry Aerothermal Environment and Thermal Protection System Response.” In 44th AIAA Thermophysics Conference. AIAA 2013-2779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2779
• White, Todd R., Milad Mahzari, Ruth A. Miller, et al. 2022b. “Mars Entry Instrumentation Flight Data and Mars 2020 Entry Environments.” In AIAA SciTech Proceedings. https://ntrs.nasa.gov/citations/20210025515
• White, Laura, Joanna Schmidt, Will Doebler, and Forrest Carpenter. 2024b. “Uncertainty Quantification Methodology for Sonic Boom Loudness of a Low-Boom Supersonic Concept.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4668
• White, Rebekah, Bart van Bloemen Waanders, Alen Alexanderian, and Arvind Saibaba. 2023. “A Bayesian Framework for Coupling Optimal Experimental Design and Optimal Control.” In Society for Industrial and Applied Mathematics conference on Computational Science and Engineering - Amsterdam, , Netherlands - February - 2023. US DOE. https://doi.org/10.2172/2431931
• White, Rebekah, Bart van Bloemen Waanders, John Jakeman, Alexanderian Alen, and Drew Kouri. 2022a. “Exploring Risk-Averse Design Criteria for Sequential Optimal Experimental Design in a Bayesian Setting.” In Proposed for presentation at the SIAM UQ held April 5-8, 2022 in Atlanta, Georgia US. US DOE. https://doi.org/10.2172/2002238
• White, Rebekah, Bart van Bloemen Waanders, John Jakeman, Drew Kouri, and Alen Alexanderian. 2022c. “Risk-Aware Bayesian Goal-Oriented Optimal Experimental Design.” In Proposed for presentation at the SIAM MDS held September 26-29, 2022 in San Diego, California US. US DOE. https://doi.org/10.2172/2004805
• White, S., Jr., and G. W. Condon. 1978. Flight Research Capabilities of the NASA/Army Rotor Systems Research Aircraft. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19790034690
• Whitefield, J., B. Griffith, R. Butler, and C. Bang. 1981. “Overview of Flight and Ground Testing with Emphasis on the Wind Tunnel.” In 1st Flight Test Conference. AIAA 1981-2474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2474
• Whitehead, Allen, Jr. 1989. “NASP Aerodynamics.” In National Aerospace Plane Conference. AIAA 1989-5013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5013
• Whiteside, Siena, and Jason Welstead. 2026. “Open eVTOL: RAVEN Research Aircraft for eVTOL Enabling techNologies (RAVEN).” In Vertical Flight Society Forum 82. https://ntrs.nasa.gov/citations/20260002152
• Whitfield, A. A., and W. E. Blackburn. 1965. UH-2 Helicopter High-Speed Flight Research Program Utilizing Jet Thrust Augmentation. Defense Technical Information Center. https://doi.org/10.21236/ad0616104
• Whitlow, W., Jr., and W. Harris. 1976. “Sonic Boom Propagation through Nonuniform Flow Fields.” In 3rd Aeroacoustics Conference. AIAA 1976-586. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-586
• Whitmore, Stephen A., and Timothy R. Moes. 1994. “Measurement Uncertainty and Feasibility Study of a Flush Airdata System for a Hypersonic Flight Experiment.” In Applied Aerodynamics Conference. https://ntrs.nasa.gov/citations/19940032870
• Whitnah, A. M. 1967. Flight Angle of Attack Determined from Ablative Heat-Shield Patterns. NASA. https://ntrs.nasa.gov/citations/19670050718
• Whittley, D. C. 1973. “The Buffalo/Spey Jet-STOL Research Aircraft.” In AGARD Mil. Appl. of V(STOL Aircraft, Vol. 1. https://ntrs.nasa.gov/citations/19730018283
• “Why Do Aircraft Cost So Much?” n.d. In Introduction to Aircraft Design. Cambridge University Press. https://doi.org/10.1017/9781139542418.009
• “Why Do Aircraft Cost So Much?” 1999. In Introduction to Aircraft Design. Cambridge University Press. https://doi.org/10.1017/cbo9780511808906.009
• Wichgers, Joel Micheal. n.d. “Applying Fault-Tolerant Design Techniques to Critical, Computer-Based Aircraft Flight Control Systems.” PhD diss., Iowa State University. https://doi.org/10.31274/td-20260812-325
• Wichman, Keith D., Joseph W. Pahle, Catherine Bahm, et al. 1996. High-Alpha Handling Qualities Flight Research on the NASA F/A-18 High Alpha Research Vehicle. NASA-TM-4773. NASA. https://ntrs.nasa.gov/citations/19970001693
• Wickersheim, Robin, Manuel Keßler, and Ewald Krämer. 2025. “Numerical Identification of Tonal Noise Sources and Comparison with Fly-Over Measurements of a Distributed Electric Propulsion-Flight Demonstrator.” In AIAA SCITECH 2025 Forum. AIAA 2025-1047. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1047
• Widmayer, Edward, and J. Tomassoni. 1971. 1/3 Scale V/STOL Cyclic Pitch Propellers: Results of Wind Tunnel Tests. Defense Technical Information Center. https://doi.org/10.21236/ad0734237
• Widnall, William S., and Peter A. Grundy. 1974. Doppler Velocity Sensor APN-200 Error Model and Flight Test Results. Defense Technical Information Center. https://doi.org/10.21236/ada002879
• Wierzbanowski, Theodore, and Johnny G. Armstrong. 1991. “The Flight Test Program for the Hydrogen Powered NASP/X-30 Research Aircraft.” In In: Aerospace Testing Seminar, 13th, Manhattan Beach, CA, Oct. 8-10, 1991, Proceedings (A93-36201 14-14). https://ntrs.nasa.gov/citations/19930052226
• Wierzbanowski, Scott, and Vijay Ramasubramanian. 2020. “The DARPA Experimental Spaceplane Program (XSP): Observations, Findings, and Recommendations for Future Reusable Launch Systems.” In ASCEND 2020. AIAA 2020-4205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-4205
• Wieselsberger, C. 1935. “Airplane Body (Non Lifting System) Drag and Influence on Lifting System.” In Aerodynamic Theory. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-91487-4_2
• Wieseman, Carol, Walt Silva, Charles Spain, and Jennifer Heeg. 2005. “Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program.” In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2005-1995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1995
• Wijerathna, A., and B. Annasiwaththa. 2025. “Aerodynamic Analysis of a VTOL Fixed-Wing UAV Aircraft with Conventional Control Surfaces.” In Proceedings of the ERU Symposium 2025. Engineering Research Unit. https://doi.org/10.31705/eru.2025.4
• Wilcox, F. 1973. “Comparison of Ground and Flight Test Results Using a Modified F106B Aircraft.” In 9th Propulsion Conference. AIAA 1973-1305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1305
• Wilcox, Zachary, and Martin Brenner. 2011. “Adaptive Lateral Flight Control with Active Flutter Suppression for Aeroservoelastic Aircraft Systems.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6210
• Wilcox, F. A., and R. Chamberlin. 1974. “Reynolds Number Effects on Boattail Drag of Exhaust Nozzles from Wind Tunnel and Flight Tests.” In AGARD. https://ntrs.nasa.gov/citations/19740062629
• Wilcox, F. A., and R. Chamberlin. 1975. “Reynolds Number Effects on Boattail Drag of Exhaust Nozzles from Wind Tunnel and Flight Tests.” In AGARD Airframe(Propulsion Interference. https://ntrs.nasa.gov/citations/19750015434
• Wilcox, D. E., and H. C. Quigley. 1978. “V/STOL Aircraft Simulation: Requirements and Capabilities at Ames Research Center.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780065881
• Wildschek, Andreas. 2014. “Flight Dynamics and Control Related Challenges for Design of a Commercial Blended Wing Body Aircraft.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-0599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0599
• Wilhite, Jarred M., Nicholas K. Borer, and Michael Frederick. 2024. “Thermal Environments and Margin Guidelines for NASA’s X-57 “Maxwell” Flight Demonstrator.” In AIAA SCITECH 2024 Forum. AIAA 2024-1475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1475
• Wilkerson, Joseph B., and Drew W. Linck. 1975. “A Model Rotor Performance Validation for the CCR Technology Demonstrator.” In Proceedings of the Vertical Flight Society Forum 31 - Washington, D.C. 1975. The Vertical Flight Society. https://doi.org/10.4050/vfs-f31-003
• Wilkin Perry, Harry. 1943. “A Radio Flight-Test Recorder: Observations Made in the Aeroplane Recorded on the Ground.” Aircraft Engineering and Aerospace Technology 15 (6): 174–78. https://doi.org/10.1108/eb031027
• Willard, Richard S., and Stan K. Kranzler. 1996. Improved Wind Tunnel Data Reduction Procedure. Defense Technical Information Center. https://doi.org/10.21236/ada345019
• Willemsen, E., C. Ceynse, and G. Graaf. 1985. “Analysis of High-Reynolds Number Wind-Tunnel Tests of the Semi-Spar.” In Offshore Technology Conference. OTC. https://doi.org/10.4043/4956-ms
• William, Christopher, Jonathan Cooper, and Jan Wright. 2002. “Force Appropriation for Flight Flutter Testing Using SMART Devices.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1652
• Williams, Walter C. 1948a. Flight Measurement of the Stability Characteristics of the Douglas D-558-1 Airplane (BuAero No. 37971) in Sideslips. NACA-RM-L8E14a. NASA. https://ntrs.nasa.gov/citations/19930085398
• Williams, Walter C. 1948b. Limited Measurements of Static Longitudinal Stability in Flight of Douglas D-558-1 Airplane (Buaero No. 37971). NACA-RM-L8E14. NASA. https://ntrs.nasa.gov/citations/19930085380
• Williams, D. D. 1965. “Aerodynamic Requirements for Thrust Measurement in Supersonic Aircraft.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50012-9
• Williams, L. J. 1978. “Short-Haul CTOL Aircraft Research.” In NASA. Langley Res. Center CTOL Transport Technol., 1978. https://ntrs.nasa.gov/citations/19780021118
• Williams, Jeffrey H. 2021. “Scaling and Similitude.” In Dimensional Analysis. IOP Publishing. https://doi.org/10.1088/978-0-7503-3655-0ch6
• Williams, Darryl, Matt Bartkowicz, and Graham V. Candler. 2024. “Shape Optimization for a Parametrically-Defined Hypersonic Glide Vehicle.” In AIAA SCITECH 2024 Forum. AIAA 2024-0562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0562
• Williams, Mark, and Mark Hartford. 1987. “Integration of Manned Simulation and Flight Test in an Operational Test and Evaluation Program.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2924. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2924
• Williams, T., and B. Hunt. 1980. “Top Inlet System Feasibility for Transonic-Supersonic Fighter Aircraft Applications.” In Aircraft Systems Meeting. AIAA 1980-1809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1809
• Williams, David L., II, Robert C. Nelson, and David F. Fisher. 1994a. “Free-to-Roll Tests of X-31 and F-18 Subscale Models with Correlation to Flight Test Results.” In Fourth High Alpha Conference: Volume 1. https://ntrs.nasa.gov/citations/19950007823
• Williams, D., II, R. Nelson, and David Fisher. 1994b. “An Investigation of X-31 Roll Characteristics at High Angle-of-Attack through Subscale Model Testing.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-806. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-806
• Williamson, G. Glen. 1963. “A Talk on Supersonic Transport.” Navigation 10 (3): 207–13. https://doi.org/10.1002/j.2161-4296.1963.tb02047.x
• Williamson, W. 1992. “Hypersonic Flight Testing.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3989
• Williamson, David T., Timothy P. Barry, and Kristen K. Liggett. 1996. Flight Test Results of ITT VRS-1290 in NASA OV-10. Defense Technical Information Center. https://doi.org/10.21236/ada430691
• Willier, Brenton, Alexandra M. Hickey, Bradford E. Robertson, and Dimitri N. Mavris. 2024. “Unsteady Aerodynamic Uncertainty Quantification of a Blunt-Body Entry Vehicle in Free-Flight.” In AIAA SCITECH 2024 Forum. AIAA 2024-1917. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1917
• Wills, Colin. 2015b. “Unmanned Combat Air Systems: Technical and Legal Challenges.” In Unmanned Combat Air Systems in Future Warfare. Palgrave Macmillan UK. https://doi.org/10.1057/9781137498496_4
• Willshire, William L., Donald P. Garber, and David W. DeVilbiss. 1992. “Flight Test Measurements of the Effect of Turbulence on Sonic Boom Peak Overpressure and Rise Time.” Journal of the Acoustical Society of America 92 (4_Supplement): 2329–30. https://doi.org/10.1121/1.405019
• Wilmoth, R. G. 1977. Computation of Transonic Boattail Flow with Separation. NASA-TP-1070. NASA. https://ntrs.nasa.gov/citations/19780005074
• Wilner, D. O. 1979. AIFTDS Stand-Alone RMDU Flight Test Report. NASA-TM-72866. NASA. https://ntrs.nasa.gov/citations/19790019996
• Wilson, Zachary David. n.d. “Flight Test Data System for Strain Measurement.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2020.2
• Wilson, R. J. 1967. Statistical Analysis of Landing Contact Conditions of the X-15 Airplane. NASA-TN-D-3801. NASA. https://ntrs.nasa.gov/citations/19670005606
• Wilson, J. R. 2012. “Mining the ‘Far Side’ of Technology to Develop Revolutionary Aircraft Prototypes: The Defense Advanced Research Projects Agency (DARPA) Approach.” In Innovation in Aeronautics. Elsevier. https://doi.org/10.1533/9780857096098.2.225
• Wilson, D., and S. Chou. 1985. “Development of the UTA High Reynolds Number Transonic Wind Tunnel.” In 23rd Aerospace Sciences Meeting. AIAA 1985-315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-315
• Wilson, S. B., III, G. H. Kidwell Jr., G. E. Turney, and A. Rogers. 1982. Supersonic STOVL Research Aircraft. SAE PAPER 821375. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19830056747
• Wilson, Herbert A., Jr. 1964. “Flight Reentry Experiments.” In Proceedings of the Conference on the Role of Simulation in Space Technology, Part B. https://ntrs.nasa.gov/citations/19690009639
• Winchenbach, G., R. Chelekis, B. Uselton, and W. Hathaway. 1982. “Comparison of Free-Flight and Wind Tunnel Data for a Generic Fighterconfiguration.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1365
• “Wind Tunnel/Flight Test Correlation Program on the B-1 Nacelle Afterbody/nozzle at Transonic Conditions.” 1978. In 14th Joint Propulsion Conference. AIAA 1978-989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-989
• “Wind-Tunnel Study of Ascent Heating of Multiple Re-Entry Vehicle Configurations.” 1981. In Aerothermodynamics and Planetary Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865510.0260.0286
• Windham, John O. 1956. Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384. NACA-RM-SL56G03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028460
• Windhorst, Robert, and Mark Ardema. 2000. “Supersonic Transport Trajectories.” In 18th Applied Aerodynamics Conference. AIAA 2000-4247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4247
• Windolph, G. 1969. “System Safety Analysis Techniques for V/STOL Aircraft.” In VTOL Research, Design, and Operations Meeting. AIAA 1969-216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-216
• Winebarger, R., and W. Neely Jr. 1984. “Flight Test Techniques for Validating Simulated Nuclear Electromagnetic Pulse Aircraft Responses.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2498
• Wing, L. D. 1972. A Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses. NASA-TM-X-69896. NASA. https://ntrs.nasa.gov/citations/19730017274
• Wing, L. D. 1973. “A Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730038400
• Wingrove, R. 1972. “Applications of a Technique for Estimating Aircraft States from Recorded Flight Test Data.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-965
• Winski, Courtney, Sarah Langston, Melissa Rivers, and Miranda Ertsgaard. n.d. “NASA 5.2%-Scale Semispan High Lift Common Research Model High Reynolds Number Wind Tunnel Test in the National Transonic Facility.” In AIAA AVIATION Forum. https://ntrs.nasa.gov/citations/20250006451
• Winski, Courtney S., Sarah Langston, Melissa B. Rivers, and Miranda Ertsgaard. 2025. “NASA 5.2%-Scale Semispan High Lift Common Research Model (CRM-HL) High Reynolds Number Wind Tunnel Test in the National Transonic Facility (NTF).” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3461. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3461
• Winston, Michael James. n.d. “Parameter Estimation of a 100 Seater Simulated Passenger Aircraft.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.13153
• Winston, M. M. 1969. Static Stability Characteristics of a 0.16- Scale Model of a Jet-Lift V/STOL Research Airplane in Cruise. NASA-TM-X-1835. NASA. https://ntrs.nasa.gov/citations/19690021255
• Winston, M. M. 1970. Induced Interference Effects on the Aerodynamic Characteristics of a 0.16-Scale Six-Jet V/STOL Model in Transition. NASA-TN-D-5727. NASA. https://ntrs.nasa.gov/citations/19700013328
• Wintzer, Mathias, and Raymond S. Castner. 2015. “Airframe-Nozzle-Plume Interactions in the Context of Low Sonic Boom Design.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1045
• Wintzer, Mathias, and Ilan Kroo. 2012. “Optimization and Adjoint-Based CFD for the Conceptual Design of Low Sonic Boom Aircraft.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-963
• Wintzer, Mathias, and Irian Ordaz. 2015. “Under-Track CFD-Based Shape Optimization for a Low-Boom Demonstrator Concept.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2260
• Wirth, F. A. 1972. “Flight Simulator Development in Parallel with Aircraft Flight Test: A Case Study of the American Airlines DC-10 Program.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/720858
• Wise, Kevin. 2003a. “First Flight of the X-45A Unmanned Combat Air Vehicle (UCAV).” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5320. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5320
• Wise, Kevin. 2003b. “X-45 Program Overview and Flight Test Status.” In 2nd AIAA “Unmanned Unlimited” Conf. and Workshop & Exhibit. AIAA 2003-6645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6645
• Wissler, J., F. Gilliam, M. Robinson, and J. Walker. 1987. “Visualization of Three-Dimensional Structures about a Pitching Forward Swept Wing.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1322. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1322
• Witcofski, R., W. Scallion, D. Carter Jr., and R. Courter. 1991. “An Advanced Hypervelocity Aerophysics Facility: A Ground-Based Flight-Test Range.” In 29th Aerospace Sciences Meeting. AIAA 1991-296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-296
• Withrow-Maser, Shannah, Carlos Malpica, and Keiko Nagami. 2020. “Multirotor Configuration Trades Informed by Handling Qualities for Urban Air Mobility Application.” In Proceedings of the Vertical Flight Society 76th Annual Forum. The Vertical Flight Society. https://doi.org/10.4050/f-0076-2020-16453
• Wittliff, C., A. O’Connor, and S. Sweet. 1992. “A Hypersonic Shock Tunnel Test of the Aeroassist Flight Experiment (AFE) Vehicle at High Altitude Test Conditions.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3906
• Wizsa, Uqwatul Alma. 2019. “Bayesian Approach to the d-Optimal for Mixture Experimental Design.” Jurnal Riset dan Aplikasi Matematika (JRAM) 3 (2): 109. https://doi.org/10.26740/jram.v3n2.p109-115
• Wizsa, Uqwatul Alma, Utami Dyah Syafitri, and Aji Hamim Wigena. 2020. “The Bayesian D-Optimal Design in Mixture Experimental Design.” In Proceedings of the Proceedings of the 1st International Conference on Statistics and Analytics, ICSA 2019, 2-3 August 2019, Bogor, Indonesia. EAI. https://doi.org/10.4108/eai.2-8-2019.2290470
• Woeste, Timothy. 1992. “Shuttle Entry Air Data System: An Experimental Investigation of Calibration for Ascent Flight.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-133
• Woike, Mark, and Brian Willis. 2000. “Mach 6 Integrated Systems Testing for the Hypersonic Tunnel Facility.” In 21st Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2000-2446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2446
• Woike, Mark R., and Brian P. Willis. 2001. The NASA Glen Research Center’s Hypersonic Tunnel Facility. NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20020023535
• Wolf, Jason, and David Bossert. 2001. “Design and Application of a Flight Test Instrumentation System for Education/research.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4313
• Wolf, H., M. Henry, and Paul Siemers III. 1988. “Shuttle Entry Air Data System (SEADS): Optimization of Preflight Algorithms Based on Flight Results.” In 15th Aerodynamic Testing Conference. AIAA 1988-2053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2053
• Wolf, J., and A. Sansone. 2002. “The U.S. Air Force Academy’s Flight Test Course: Preparing Tomorrow’s Flight Testers.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1048
• Wolfe, David Michael, and John A. Bakalyar. 2011. “NASA Dryden: Flight Loads Lab Capabilities and Mass Properties Testing.” In Spring 2011 AFDC Flutter Club. https://ntrs.nasa.gov/citations/20110014439
• Wolkovitch, J. 1984. “Joined-Wing Research Airplane Feasibility Study.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2471
• Wolles, B. A. 1997. “Computation of Transonic Flows Applying Shock Boundary Layer Interaction Control.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-90711-0_18
• Wolowicz, Chester H., and Herman A. Rediess. 1957. Effects of Jet Exhausts on Flight-Determined Longitudinal and Lateral Dynamic Stability Characteristics of the Douglas D-558-II Research Airplane. NACA-RM-H57G09. NASA. https://ntrs.nasa.gov/citations/19930089762
• Wolowicz, C. H., and R. B. Yancey. 1973. Comparisons of Predictions of the XB-70-1 Longitudinal Stability and Control Derivatives with Flight Results for Six Flight Conditions. NASA-TM-X-2881. NASA. https://ntrs.nasa.gov/citations/19730022208
• Wong, Thomas J., Glen Goodwin, and Robert E. Slye. 1960. Motion and Heating during Atmosphere Reentry of Space Vehicles. NASA-TN-D-334. NASA. https://ntrs.nasa.gov/citations/19980231044
• Wong, Jackie, Eric Nesbitt, Michael G. Jones, and Douglas M. Nark. 2019. “Flight Test Methodology for NASA Advanced Inlet Liner on 737MAX-7 Test Bed (Quiet Technology Demonstrator 3).” In 25th AIAA/CEAS Aeroacoustics Conference. AIAA 2019-2763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2763
• Wood, N. B. 1968. “Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Blunted Cones.” Aeronautical Quarterly 19 (4): 301–16. https://doi.org/10.1017/s0001925900004704
• Wood, J. 1983. “Comparison of Fixed-Base and in-Flight Simulation Results for Lateral High Order Systems.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2105
• Woodbury, Don. 2003. “DARPA/Army Unmanned Combat Armed Rotorcraft (UCAR) Program.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2617
• Woodbury, S., and R. Gorman. 1983. “Program Overview of Peacekeeper Flight Test Planning.” In 2nd Flight Testing Conference. AIAA 1983-2729. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2729
• Woodbury, G. E., and J. W. Wallace. 1974. Investigation of New Radar-Data-Reduction Techniques Used to Determine Drag Characteristics of a Free-Flight Vehicle. NASA-TN-D-7710. NASA. https://ntrs.nasa.gov/citations/19740027145
• Woodcock, G. R. 1988. “The National Aerospace Plane.” Science: 518–518. https://doi.org/10.1126/science.518-c
• Woodfield, A. A. 1970. “Thrust Measurement in Flight: The Requirements, Current Situation and Future Possibilities.” Aeronautical Journal 74 (712): 314–26. https://doi.org/10.1017/s0001924000047606
• Woodman, J. 1971. “L-1011 Flight Test Program.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-789. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-789
• Woodrow, Paul, Mark Tischler, Gonzalo Mendoza, Steven G. Hagerott, and Jeanine Hunter. 2013. “Low Cost Flight-Test Platform to Demonstrate Flight Dynamics Concepts Using Frequency-Domain System Identification Methods.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4739
• Woods, W. C., S. D. Holland, and M. DiFulvio. 2000a. Hyper-X Stage Separation Wind Tunnel Test Program. AIAA Paper 2000-4008. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000081743
• Woods, William C., Scott D. Holland, and Michael Difulvio. 2000b. Hyper-X Storage Separation Wind Tunnel Test Program. AIAA Paper 2000-4008. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20000099722
• Woodward, Richard P., and Irvin J. Loeffler. 1993. In-Flight near- and Far-Field Acoustic Data Measured on the Propfan Test Assessment (PTA) Testbed and with an Adjacent Aircraft. NASA-TM-103719. NASA. https://ntrs.nasa.gov/citations/19930017869
• Woodyard, Christopher. 2026. “System and Method for Active Environmental Modulation in Hypersonic Flight Regimes.” Preprint, . https://doi.org/10.2139/ssrn.6142029
• Woolf, Reagan. 2012a. “Applications of Statistically Defensible Test and Evaluation Methods to Aircraft Performance Flight Testing.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-2723. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2723
• Woolf, Reagan K. 2012b. Flight Test Validation of an Analytical Method for Predicting Trailing Cone System Drag Force and Droop Angle. Defense Technical Information Center. https://doi.org/10.21236/ada583117
• Work, Andrew, Jonathan Salem, Eric Baker, Ernestina Schirmer, Rebekah Douglass, and Richard Kreeger. 2019. “Measured Interfacial Residual Strains Produced by in-Flight Ice.” In International Conference on Icing of Aircraft, Engines, and Structures. https://ntrs.nasa.gov/citations/20190026544
• Wright, John B. 1948a. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Basic Longitudinal Stability of the D-558-1. NACA-RM-L7K24. NASA. https://ntrs.nasa.gov/citations/19930085814
• Wright, John B. 1948b. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Longitudinal Stability and Control of the D-558-1. NACA-RM-L8C23. NASA. https://ntrs.nasa.gov/citations/19930085349
• Wright, John B. 1948c. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane: D-558-1 Speed-Reduction Brake and Symmetrical-Profile Wing Characteristics. NACA-RM-L8B06. NASA. https://ntrs.nasa.gov/citations/19930085315
• Wright, Howard. 1989. “National Aero-Space Plane Technology Development Overview.” In National Aerospace Plane Conference. AIAA 1989-5003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-5003
• Wright, Michael R. 2011. “Flight Systems Integration and Test.” In Flight Systems Integration and Test. https://ntrs.nasa.gov/citations/20110022499
• Wright, M. J. 2019. “Introduction Course on Thermal Protection Systems for Atmospheric Entry.” In Pyrolysis, a key step in the thermochemical conversion of biomass. von Karman Institute for Fluid Dynamics. https://doi.org/10.35294/ls201901.wright
• Wright, Cody, and Onur Bilgen. 2019. “A Variable Camber Piezocomposite Trailing-Edge for Subsonic Aircraft: Multidisciplinary Design Optimization.” In ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers. https://doi.org/10.1115/smasis2019-5604
• Wright, Michael, Ioana Cozmuta, Bernard Laub, Yih-Kanq Chen, and William H. Wilcoxson. 2011. “Defining Ablative Thermal Protection System Margins for Planetary Entry Vehicles.” In 42nd AIAA Thermophysics Conference. AIAA 2011-3757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3757
• Wright, John D., and Donald L. Loving. 1953. High-Speed Wind-Tunnel Tests of a 1/16-Scale Model of the D-558 Research Airplane Lift and Drag Characteristics of the D-558-1 and Various Wing and Tail Configurations. NACA-RM-L6J09. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019302
• Wu, Jian-Hui. 2018. “Optimization Design of High Lift to Drag Ratio Waverider Vehicle Based on Viscosity Simulation.” DEStech Transactions on Engineering and Technology Research, no. pmsms. https://doi.org/10.12783/dtetr/pmsms2018/24866
• Wu, Keyi, Peng Chen, and Omar Ghattas. 2023b. “A Fast and Scalable Computational Framework for Large-Scale High-Dimensional Bayesian Optimal Experimental Design.” SIAM/ASA Journal on Uncertainty Quantification 11 (1): 235–61. https://doi.org/10.1137/21m1466499
• Wu, Keyi, Peng Chen, and Omar Ghattas. 2023d. “An Offline-Online Decomposition Method for Efficient Linear Bayesian Goal-Oriented Optimal Experimental Design: Application to Optimal Sensor Placement.” SIAM Journal on Scientific Computing 45 (1): B57-B77. https://doi.org/10.1137/21m1466542
• Wu, Zhigang, and Jonathan E. Cooper. 2016. “Active Flutter Suppression Combining the Receptance Method and Flutter Margin.” In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2016-1227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1227
• Wu, Yunpeng, and Yang Liu. 2021. “Research on Flight Technique and Hazard Control for Civil Airplane Crosswind Flight Test.” In 2021 International Symposium on Electrical, Electronics and Information Engineering. ACM. https://doi.org/10.1145/3459104.3459109
• Wu, Zaigui, and Yanbin Liu. 2022. “Integrated Optimization Design Using Improved Pigeon-Inspired Algorithm for a Hypersonic Vehicle Model.” International Journal of Aeronautical and Space Sciences 23 (5): 1033–42. https://doi.org/10.1007/s42405-022-00492-1
• Wu, Peng, Zhili Tang, and Jacques Periaux. 2018. “Multi-Disciplinary Design Optimization of Air-Breathing Hypersonic Vehicle Using Pareto Games and Evolutionary Algorithms.” In Computational Methods in Applied Sciences. Springer International Publishing. https://doi.org/10.1007/978-3-319-89988-6_19
• Wu, Peng, Zhili Tang, and Jianda Sheng. 2016. “Multi-Disciplinary Design Optimization of Hypersonic Air-Breathing Vehicle.” International Journal of Modern Physics: Conference Series 42: 1660169. https://doi.org/10.1142/s2010194516601691
• Wu, Cunli, and Fang Tong. 2017. “Active Flutter Suppression of Stochastic Airfoil with Uncertain Pitch Stiffness.” Journal of Aerospace Engineering and Mechanics 1 (2). https://doi.org/10.36959/422/431
• Wu, Dafang, Yuewu Wang, Shougen Zhao, Bing Pan, and Shuang Wu. 2014. “Experimental Research on Thermal Vibration Characteristics of Wing Structure for High-Speed Flight Vehicles in High-Temperature Environment.” In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2014-2511. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2511
• Wuestenhagen, Matthias, Thiemo Kier, Yasser M. Meddaikar, Manuel Pusch, Daniel Ossmann, and Andreas Hermanutz. 2018. “Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3150
• Wulff, G., and M. Zoellner. 1991. “DIVA/MIMO Flight Test Data Analysis for the X-31A Demonstrator.” In 18th Atmospheric Flight Mechanics Conference. AIAA 1991-2852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2852
• Wurster, K. 1981. “An Assessment of the Impact of Transition on Advanced Winged Entry Vehicle Thermal Protection System Mass.” In 16th Thermophysics Conference. AIAA 1981-1090. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1090
• Wyatt, Earl. 2003. “The DARPA/Air Force Unmanned Combat Air Vehicle (UCAV) Program.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2616. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2616
• Wyborny, W., and G. Requardt. 1974. “A New Aerodynamic Free Flight Testing System for Six-Component Measurements in Short Duration Wind Tunnels.” In 8th Aerodynamic Testing Conference. AIAA 1974-613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-613
• Wygle, B. 1981. “Two at a Time: Flight Test Plans for the New Boeing Airliners.” In 1st Flight Test Conference. AIAA 1981-2378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2378
• Wykes, J. H., and R. E. Lawrence. 1971. Estimated Performance and Stability and Control Data for Correlation with XB-70-1 Flight Test Data. NASA-CR-114335. NASA. https://ntrs.nasa.gov/citations/19710024525
• Wyrick, Donald R. 1965. Extension of the High-Speed Flight Envelope of the XH-51A Compound Helicopter. Defense Technical Information Center. https://doi.org/10.21236/ad0627372
• X-29: Research Aircraft. 1991. NASA-TM-109370. NASA. https://ntrs.nasa.gov/citations/19940014489
• “X-43A Research Vehicle Design and Construction.” 2011. In Eleven Seconds into the Unknown. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867774.0199.0219
• “X-48B Blended Wing Body Flight Tests Enter Second Phase.” 2008. Aircraft Engineering and Aerospace Technology 80 (5). https://doi.org/10.1108/aeat.2008.12780eaf.013
• Xia, Zhaoyang, Xingsi Han, Majie Zhao, Baolu Shi, and Xiao Hou. 2026. “Mode Transition and Combustion Characteristics of a Dual-Mode Scramjet Engine Using Flamelet Modeling.” Physics of Fluids 38 (7): 076126. https://doi.org/10.1063/5.0332049
• Xiang, Zhengchao, and Lifeng Wang. 2023. “Active Flutter Suppression for a T-Tail via Optimal Control.” Journal of Aerospace Engineering 36 (5): 04023034. https://doi.org/10.1061/jaeeez.aseng-4658
• Xianyu, Wu, Xu Lin, Jin Liang, et al. 2006. “The MDO Environment for Hypersonic Vehicle System Design and Optimization.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-5191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-5191
• Xiao, Q., H. M. Tsai, and F. Liu. 2004. “A Numerical Study of Transonic Buffet on a Supercritical Airfoil.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1056. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1056
• Xiao, Zhixiang, and Yijiang Yang. 2025. “Effect of Boundary Layer Transition on the Unsteady SWBLI past the Forebody and Intake at Hypersonic Speed.” Preprint, . https://doi.org/10.2139/ssrn.5902345
• Xie, Jinran. 2024. “The History of Modern Commercial Aircraft Focuses on Technical Developments, Sustainable Growth and Efficiency.” Highlights in Science, Engineering and Technology 120: 312–20. https://doi.org/10.54097/wqm0cw84
• Xie, Jiacheng, Yu Cai, Mengzhen Chen, and Dimitri N. Mavris. 2019. “Integrated Sizing and Optimization of Hybrid Wing Body Aircraft in Conceptual Design.” In AIAA Aviation 2019 Forum. AIAA 2019-2885. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2885
• Xie, Wei, Luyang Guan, Ming Bao, and Xiaodong Li. 2012. “Aircraft Flight Parameter Estimation via Multipath Delays Using Ground-Based Microphone Array.” Journal of the Acoustical Society of America 131 (4_Supplement): 3445–3445. https://doi.org/10.1121/1.4708964
• Xiong, Juntao, Robert E. Bartels, and Nhan T. Nguyen. 2021a. “Aerodynamic Optimization of Mach 0.745 Transonic Truss-BracedWing Aircraft with Variable-Camber Continuous Trailing-Edge Flap.” In AIAA Scitech 2021 Forum. AIAA 2021-0337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0337
• Xiong, Juntao, Robert E. Bartels, and Nhan T. Nguyen. 2021b. “Aeroelastic Trim Drag Optimization of Mach 0.745 Transonic Truss-BracedWing Aircraft with Variable-Camber Continuous Trailing-Edge Flap.” In AIAA Aviation 2021 Forum. AIAA 2021-2528. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2528
• Xiong, Juntao, Jason Fugate, and Nhan T. Nguyen. 2019. “Investigation of Truss-Braced Wing Aircraft Transonic Wing-Strut Interference Effects Using FUN3D.” In AIAA Aviation 2019 Forum. AIAA 2019-3026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3026
• Xiong, Juntao, Jason A. Fugate, and Nhan T. Nguyen. 2020. “Jig Twist Optimization of Mach 0.745 Transonic Truss Braced Wing Aircraft and High-Fidelity CFD Validation.” In AIAA Scitech 2020 Forum. AIAA 2020-0451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0451
• Xiong, Juntao, and Nhan T. Nguyen. 2022. “Steady and Unsteady Simulations of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis.” In AIAA AVIATION 2022 Forum. AIAA 2022-4151. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4151
• Xiong, Juntao, and Nhan T. Nguyen. 2023. “Simulations of Mach 0.8 Transonic Truss-Braced Wing Aircraft Aerodynamics at High Angles of Attack.” In AIAA AVIATION 2023 Forum. AIAA 2023-4528. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4528
• Xiong, Juntao, and Nhan T. Nguyen. 2024a. “Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis.” In AIAA SCITECH 2024 Forum. AIAA 2024-2668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2668
• Xiong, Juntao, and Nhan T. Nguyen. 2024b. “Transonic Buffet Simulation of Mach 0.8 Transonic Truss-Braced Wing Aeroelastic Model.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4056. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4056
• Xiong, Juntao, Nhan T. Nguyen, and Robert E. Bartels. 2022a. “Aerodynamic Optimization of Mach 0.8 Transonic Truss-Braced Wing Aircraft Using Variable Camber Continuous Trailing Edge Flap.” In AIAA SCITECH 2022 Forum. AIAA 2022-0016. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0016
• Xiong, Juntao, Nhan T. Nguyen, and Robert E. Bartels. 2022b. “Aeroelastic Analysis of Mach 0.8 Transonic Truss-Braced Wing Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-0300. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0300
• Xiong, Juntao, Nhan T. Nguyen, and Robert E. Bartels. 2022c. “Aeroelastic Trim Drag Optimization of Mach 0.8 Transonic Truss-Braced Wing Aircraft with Variable Camber Continuous Trailing Edge Flap.” In AIAA AVIATION 2022 Forum. AIAA 2022-4150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4150
• Xiong, Juntao, Nhan T. Nguyen, and Robert E. Bartels. 2023a. “Aeroelastic Trim Drag Optimization of Mach 0.8 Transonic Truss-Braced Wing Aircraft Using High-Lift Devices and Control Surfaces.” In AIAA SCITECH 2023 Forum. AIAA 2023-1575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1575
• Xiong, Juntao, Nhan T. Nguyen, and Robert E. Bartels. 2023b. “Jig Twist Optimization of Mach 0.8 Transonic Truss-Braced Wing Aircraft.” In AIAA SCITECH 2023 Forum. AIAA 2023-1573. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1573
• Xiong, Juntao, Nhan T. Nguyen, John Foster, and William E. Milholen. 2026. “Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall.” In AIAA SCITECH 2026 Forum. AIAA 2026-1111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1111
• Xiong, Juntao, Nhan T. Nguyen, and Jason Fugate. 2021c. “Study of Mach 0.8 Transonic Truss-Braced Wing Aircraft Wing-Strut Interference Effects.” In AIAA Scitech 2021 Forum. AIAA 2021-0336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0336
• Xiong, Gang, and Chao Yang. 2001. “Synthesis on Flutter Suppression Control Law for Active Aeroelastic Wing.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1463. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1463
• Xu, Lai Bin. 2012. “Longitudinal Dynamics Response of M-Wing Morphing Aircraft.” Advanced Materials Research 538-541: 2627–30. https://doi.org/10.4028/www.scientific.net/amr.538-541.2627
• Xu, Jihong, Yaqiang Fan, and Yu Xu. 2025b. “Fiber Optic Sensing System for Real-Time Inversion of Aircraft Wing Morphology Based on Photonic Integrated Chips.” Preprint, . https://doi.org/10.2139/ssrn.5498202
• Xu, Zhenming, Zhonghua Han, Zhen Zhu, and Wenping Song. 2019a. “On the Flow Mechanism of Forward Swept Natural-Laminar-Flow Wing for Crossflow Instability Suppression.” In AIAA Aviation 2019 Forum. AIAA 2019-3291. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3291
• Xu, Zhixiong, Guangwei Wen, Yixin Hu, Xu Chao, and Li Fan. 2026. “Trajectory Planning for Level Flight of Eagle of Taihu 10, a Canard-Configured Tail-Sitter Technology Demonstrator.” Preprint, . https://doi.org/10.2139/ssrn.6173519
• Xu, Danyang, Chi Yuan, and Youmin Zhang. 2019b. “Time-Domain System Identification for Long-EZ Fixed-Wing Aircraft Based on Flight Test Data.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-0474-7_83
• Xu, Xiao-wu, Wei Zhang, and Hao Zhan. 2018a. “Analysis of Asymmetric Control Efficiency for Folding Wing Morphing Aircraft.” DEStech Transactions on Computer Science and Engineering, no. mmsta. https://doi.org/10.12783/dtcse/mmsta2017/19666
• Xue, Fei, Han Qin, Yuchao Wang, Zenghui Jiang, Xin Jin, and Peng Bai. 2019b. “Free Flight Wind Tunnel Test Similarity Law Derivation for Light Store Separation from Aircraft.” Advances in Mechanical Engineering 11 (5): 1687814019853062. https://doi.org/10.1177/1687814019853062
• Yamada, Kento, Takahiro Uchiyama, and Makoto Ueno. 2023. “Flight-to-Wind-Tunnel Correlation Study Using JAXA’s Flying Test Bed “Hisho”.” Transactions of the Japan Society for Aeronautical and Space Sciences 66 (2): 17–25. https://doi.org/10.2322/tjsass.66.17
• Yamakawa, George M., James L. Webre, Richard S. Adler, and Ronald E. Ratcliff. 1984. Airworthiness and Flight Characteristics Test of the RC-12D Guardrail V. Defense Technical Information Center. https://doi.org/10.21236/ada148046
• Yamamoto, Yukimutsu, Takashi Kai, and Koichi Hozumi. 2001. “Numerical Rebuilding of Aerothermal Environments and CFD Analysis of Post Flight Wind Tunnel Tests for Hypersonic Flight Experiment HYFLEX.” In 35th AIAA Thermophysics Conference. AIAA 2001-2899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2899
• Yamamoto, Y., M. Ueno, M. Yanagihara, Y. Miyazawa, and R. Ito. 2002. “Pre-Flight CFD Analysis of High Speed Flight Demonstrator Phase II Vehicle and the Validation of HOPE-X Transonic Aerodynamics.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-685. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-685
• Yamanaka, Tatsuo. 2003. “Flight Performance of an Airbreathing Rocket Combuned Engine Powered Spaceplane.” In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. AIAA 2003-6996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6996
• Yamane, Takashi, and Peretz Friedmann. 1990. “Aeroelastic Tailoring Analysis for Preliminary Design of Advanced Turbo Propellers with Composite Blades.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-1160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1160
• Yamato, Hiroyuki, Noriaki Okada, and Toshio Bando. 1988. “Flight Test of the Japanese USB STOL Experimental Aircraft ASKA.” In 4th Flight Test Conference. AIAA 1988-2180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2180
• Yamauchi, G. K., and W. Johnson. 1983. Trends of Reynolds Number Effects on Two-Dimensional Airfoil Characteristics for Helicopter Rotor Analyses. NASA-TM-84363. NASA. https://ntrs.nasa.gov/citations/19830016201
• Yamazaki, Yuki, Kazuhide Mizobata, and Kazuyuki Higashino. 2019. “Drag Reduction on the Basis of the Area Rule of the Small-Scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 17 (2): 127–33. https://doi.org/10.2322/tastj.17.127
• Yan, Yuqing, and Jian Fu. 2026. “Fractional-Order Adaptive Optimal Control for Hypersonic Flight Vehicles.” Preprint, . https://doi.org/10.2139/ssrn.6248882
• Yan, Farui, Lu Han, Yongqi Yang, Xuedong Xie, and Baocheng Xie. 2025. “Current Status and Development Trends of Morphing Wing of Aircraft.” Recent Patents on Engineering 19 (8): e280524230392. https://doi.org/10.2174/0118722121302573240527051750
• Yancey, R. B. 1964. Flight Measurements of Stability and Control Derivatives of the x-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25 Deg. NASA-TN-D-2532. NASA. https://ntrs.nasa.gov/citations/19650001037
• Yang, Lung-Te. n.d. “Aircraft Flight Control System Design by Model Reference Adaptive Control.” PhD diss., Iowa State University. https://doi.org/10.31274/td-20260812-346
• Yang, Tingwu. 2021a. “Airborne Data Acquisition and Recording.” In Telemetry Theory and Methods in Flight Test. Springer Singapore. https://doi.org/10.1007/978-981-33-4737-3_4
• Yang, Tingwu. 2021b. “Basic Theory of Flight Test Telemetry.” In Telemetry Theory and Methods in Flight Test. Springer Singapore. https://doi.org/10.1007/978-981-33-4737-3_2
• Yang, Da Qing, and Shi Jun Guo. 2009. “Rolling Active Control for an Aircraft of Seamless Aeroelastic Wing.” In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2009-2197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2197
• Yang, T. Y., P. Guruswamy, and Alfred G. Striz. 1980. Flutter Analysis of a Two-Dimensional and Two-Degree-of-Freedom Supercritical Airfoil in Small-Disturbance Unsteady Transonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ada084172
• Yang, Qingchun, Jichao Hu, Juntao Chang, Youhai Zong, and Wen Bao. 2014a. “Experimental Study on Combustion Mode Transition Effects in a Strut-Based Scramjet Combustor.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 229 (4): 764–71. https://doi.org/10.1177/0954410014539288
• Yang, Yong, Defeng Hu, and Menglun Yu. 2006a. “Roadmap of Long-March Reusable Launch Vehicle.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-d2.4.03
• Yang, Zhigang, and Qiliang Li. 2008. “Effects of Reynolds Number on Wind Tunnel Corner Losses.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-374. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-374
• Yang, Shuchi, Shijun Luo, Feng Liu, and Her-Mann Tsai. 2006b. “Supercritical Flow over Unstalled Plunging Airfoil Computed by Euler Method.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-293
• Yang, H., and A. Przekwas. 1993. “Three-Dimensional Unsteady Separating Flows around an Oscillatory Forward-Swept Wing.” In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. AIAA 1993-2976. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2976
• Yang, Jian, Pia Sartor, Jonathan E. Cooper, and R. K. Nangia. 2015. “Morphing Wing Design for Fixed Wing Aircraft.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-0441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0441
• Yankui, Wang, Zhang Dongjun, and Deng Xueying. 2005. “The Design of Waverider Configuration with High Lift-Drag Ratio.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6040
• Yates, E. 1964. “Cost Analysis as an Aid to Aircraft Design.” In General Aviation Aircraft Design and Operations Meeting. AIAA 1964-178. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-178
• Yavuztürk, Vefa N., Eren Topbas, Ümit Kutluay, and Yigit Yazicioglu. 2017. “Flight Test Maneuver Design and Aerodynamic Parameter Estimation for Single Use Autonomous Gliding Air Vehicles.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-1865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1865
• Ye, Qingqing, Ferry Schrijer, and Fulvio Scarano. 2017. “Tomographic PIV Measurement of Hypersonic Boundary Layer Transition past a Micro-Ramp.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-4512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4512
• Yeager, W. T., Jr., and W. R. Mantay. 1976. Correlation of Full-Scale Helicopter Rotor Performance in Air with Model-Scale Freon Data. NASA-TN-D-8323. NASA. https://ntrs.nasa.gov/citations/19770005056
• Yechout, Thomas. 1988b. “Lessons Learned in Flight Test Education: The Air Force Academy Experience.” In 4th Flight Test Conference. AIAA 1988-2201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2201
• Yechout, T. R., and K. B. Braman. 1984. Development and Evaluation of a Performance Modeling Flight Test Approach Based on Quasi Steady-State Maneuvers. NASA-CR-170414. NASA. https://ntrs.nasa.gov/citations/19840019656
• Yechout, T., and D. Oelschlaeger. 1976. “Flight Evaluation of a Digital Multimode Flight Control System in anA-7D Aircraft.” In Guidance and Control Conference. AIAA 1976-1913. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1913
• Yechout, T., and W. Schweikhard. 1984. “In-Flight Measurement of Engine Power Effects on the Lift and Drag Characteristics of a High Performance Business Jet.” In 22nd Aerospace Sciences Meeting. AIAA 1984-563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-563
• Yee, Layton, Harry E. Bailey, and Henry T. Woodward. 1961. Ballistic Range Measurements of Stagnation-Point Heat Transfer in Air and in Carbon Dioxide at Velocities up to 18,000 Feet per Second. NASA-TN-D-777. NASA. https://ntrs.nasa.gov/citations/20040047120
• Yeh, Hsien-Yang. 1988a. Stress Concentration around Circular Hole in a Composite Material Specimen Representative of the X-29A Forward-Swept Wing Aircraft. NASA-CR-179435. NASA. https://ntrs.nasa.gov/citations/19880017310
• Yeh, Hsien-Yang. 1988b. Temperature Effect on Stress Concentration around Circular Hole in a Composite Material Specimen Representative of X-29A Forward-Swept Wing Aircraft. NASA-CR-179439. NASA. https://ntrs.nasa.gov/citations/19890005085
• Yeh, Hsien-Yang, and Hsien-Liang Yeh. 1989. “Stress Concentration of the Composite Material Used by the X-29A Forward-Swept Wing Aircraft under Various Temperature Levels.” In Composite Structures 5. Springer Netherlands. https://doi.org/10.1007/978-94-009-1125-3_30
• Yen, J. G., S. Viswanathan, and C. G. Matthys. 1976. “Flight Flutter Testing of Rotary Wing Aircraft Using a Control System Oscillation Technique.” In NASA. Langley Res. Center Flutter Testing Tech.. https://ntrs.nasa.gov/citations/19770014097
• Yentsch, Robert J., and Datta V. Gaitonde. 2013. “Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet Flowpath.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3753
• Yentsch, Robert J., and Datta V. Gaitonde. 2014. “Comparison of Mode-Transition Phenomena in Axisymmetric and Rectangular Scramjet Flowpaths.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0625. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0625
• Yeo, Yih Tang, and Hugh H. Liu. 2018. “Transition Control of a Tilt-Rotor VTOL UAV.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1848
• Yeo, Hyeonsoo, Thomas Norman, and Mark Potsdam. 2016. “Investigation of UH-60A Rotor Structural Loads from Flight and Wind Tunnel Tests.” In Proceedings of the Vertical Flight Society 72nd Annual Forum and Technology Display. The Vertical Flight Society. https://doi.org/10.4050/f-0072-2016-11430
• Yeo, Hyeonsoo, and Ethan A. Romander. 2012. Loads Correlation of a Full-Scale UH-60A Airloads Rotor in a Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ada566027
• Yergensen, Stephen, and Donald Rhea. 1988. “Configuration Management Issues and Objectives for a Real-Time Research Flight Test Support Facility.” In 4th Flight Test Conference. AIAA 1988-2200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2200
• Yetter, J., G. B. Evelyn, and C. Mercer. 1982. “Transonic Wind Tunnel Test of a Supersonic Nozzle Installation.” In 18th Joint Propulsion Conference. AIAA 1982-1045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1045
• Yin, Jianping. 2011. “Simulation of Tail Rotor Noise Reduction and Comparison with HeliNovi Wind Tunnel Test Data.” In Proceedings of the Vertical Flight Society 67th Annual Forum and Technology Display - Forum 67 - Virginia Beach, Virginia 2011. The Vertical Flight Society. https://doi.org/10.4050/vfs-f67-000045
• Yin, Xiaomeng, Yongji Wang, Lei Liu, and Xing Wei. 2017. “Particle Swarm Optimization for the Hypersonic Vehicle Robust Control System Design.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2229. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2229
• Yip, Long, Paul Vijgen, Jay Hardin, and C. Van Dam. 1992. “Subsonic High-Lift Flight Research on the NASA Transport System Research Vehicle (TSRV).” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4103. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4103
• Yoko, Matthew. 2024. “Optimal Experiment Design with Adjoint-Accelerated Bayesian Inference.” Preprint, . https://doi.org/10.52843/cassyni.by16mj
• Yokoyama, Yoshiya, and Daigo Fujiwara. 2021. “Reference Trajectory/Attitude Control System Design and Flight Tests of an Immelmann-Turn Maneuver of Unmanned Helicopters.” Proceedings of Mechanical Engineering Congress, Japan 2021 (0): J181-05. https://doi.org/10.1299/jsmemecj.2021.j181-05
• Yoler, Y. A. 1961. “Contributions of Dyna-Soar to Space Flight Technology.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/610355
• Yoo, Seung Y., Jeffrey A. Housman, Mark Smith, and Michael Frederick. n.d. “Computational Analysis of X-57 Rate Derivatives and Comparison to Wind Tunnel Data.” In Aviation 2024. https://ntrs.nasa.gov/citations/20240007397
• Yoo, Seung, Jeffrey A. Housman, Mark Smith, and Michael Frederick. 2024. “Computational Analysis of X-57 Rate Derivative and Comparison to Wind Tunnel Data.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3925
• Yoon, Jangho, Peter Attar, and Prakash Vedula. 2010. “Non-Intrusive Uncertainty Quantification for Hypersonic Flight Using Direct Quadrature.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8171
• Yoshida, Kenji. 2009. “Supersonic Drag Reduction Technology in the Scaled Supersonic Experimental Airplane Project by JAXA.” Progress in Aerospace Sciences 45 (4–5): 124–46. https://doi.org/10.1016/j.paerosci.2009.05.002
• Yoshida, Kenji, Makino Yoshikazu, and Yuichi Shimbo. 2002. “An Experimental Study on Unmanned Scaled Supersonic Experimental Airplane.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2842
• Yoshinaga, Takashi, Atsushi Tate, Mitsunori Watanabe, and Takayuki Shimoda. 1995. “Dynamic Test of the Orbital Reentry Vehicle (OREX) in a Transonic Wind Tunnel with Comparison to Flight Data.” In 13th Applied Aerodynamics Conference. AIAA 1995-1901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1901
• You, Yancheng, and Dewang Liang. 2009. “Numerical Research of Internal Waverider Hypersonic Inlet in Non-Design Statuses.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-4215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-4215
• You, Jin, Anyuan Yu, Jialing Le, Shunhua Yang, Xiangsen Rong, and Fangji Li. 2017. “Experimental Research on Restarting Characteristics of Supersonic Inlet Based of Injection Regulation.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2387. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2387
• Young, Tom. n.d. “What Is the Future of Telemetry at Armstrong Flight Research Center?” In Test Instrumentation Workshop (TIW) “Range of the Future”. https://ntrs.nasa.gov/citations/20220005991
• Young, J. C. 1982. “Aerodynamic Comparisons of STS-1 Space Shuttle Entry Vehicle.” In NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017328
• Young, T. M., and J. P. Fielding. 2001. “Flight Operational Assessment of Hybrid Laminar Flow Control (HLFC) Aircraft.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_12
• Yu, Ming Li. 2012. “Group Delay in Digital Filter Induced Instability of a Two-Dimensional Airfoil Active Flutter Suppression System.” Applied Mechanics and Materials 226-228: 64–69. https://doi.org/10.4028/www.scientific.net/amm.226-228.64
• Yu, N., H. Chen, and S. Samant. 1983. “Inviscid Drag Calculations for Transonic Flows.” In 6th Computational Fluid Dynamics Conference Danvers. AIAA 1983-1928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1928
• Yu, Fanglin, and Mirko Hornung. 2026. “Aeroelastic Evaluation of Dry Wing Effects for Hydrogen Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.7180118
• Yu, Pan, Liu Wei-Dong, and Wang Zhen-Guo. 2007. “Investigation on the Combustion Mode Translation of Thermal Choked Scramjet.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5387. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5387
• Yuan, Kuo, Peretz Friedman, and Comandur Venkatesan. 1994. “Aeroelastic Stability, Response and Loads of Swept Tip Composite Rotor Blades in Forward Flight.” In 35th Structures, Structural Dynamics, and Materials Conference. AIAA 1994-1309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1309
• Yuan, XianXu, BingBing Wan, JiuFen Chen, JianQiang Chen, and GuoHua Tu. 2019. “Investigation on Correlation between Wind Tunnel and Flight for Boundary Layer Stability and Transition of MF-1 Blunt Cone.” SCIENTIA SINICA Physica, Mechanica & Astronomica 49 (12): 124701. https://doi.org/10.1360/sspma-2019-0162
• Yue, Brian Y. 2026. “An Overview of Transonic Truss-Braced Wing Technology.” In AIAA AVIATION 2026 Forum. AIAA 2026-4344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4344
• Yue, Shuai, Hong Nie, Ming Zhang, Mingyang Huang, and Dafu Xu. 2018. “Optimization and Performance Analysis of Oleo-Honeycomb Damper Used in Vertical Landing Reusable Launch Vehicle.” Journal of Aerospace Engineering 31 (2): 04018002. https://doi.org/10.1061/(asce)as.1943-5525.0000825
• Yue, Ting, Lixin Wang, and Junqiang Ai. 2009. “Multibody Dynamic Modeling and Simulation of a Tailless Folding Wing Morphing Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-6155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6155
• Yue, Ting, Lixin Wang, and Junqiang Ai. 2017b. “Longitudinal Integrated Linear Parameter Varying Control for Morphing Aircraft in Large Flight Envelope.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-3396. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3396
• Yuldashev, Petr. 2021. “1pCA2: Modelling Statistics of Sonic Boom Parameters in Turbulent Media Using Nonlinear Parabolic Equation.” Preprint, . https://doi.org/10.26226/morressier.606f15dd30a2e980041f23aa
• Yun, Yongtae, Joungki Seo, Kiyun Park, Junyeong Jeong, Juwon Kim, and Sejin Kwon. 2019. “Flight Testing of Technology Demonstrator with Hydrogen Peroxide Hybrid Rocket.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4267
• Yungkurth, C., F. Dawson, S. Houck, S. Corda, and C. Trefny. 1991. The F/A-18 External Burning Flight Test. AIAA PAPER 91-5050. Johns Hopkins University. https://ntrs.nasa.gov/citations/19920061923
• Yurkovich, Rudolph. 2009. “An Analysis of the Integration of Active Aeroelastic Wing Technology into a Co-Planar Variable Geometry Morphing Wing.” In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2009-2514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2514
• Zafirov, Dimo. 2010. “Joined Wings Thrust Vectored UAV Flight Envelope.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7509
• Zahm, A. F. 1921. “Review of Experiments with the Rehabilitated Langley Aeroplane in 1914.” Aeronautical journal (London, England: 1897) 25 (132): 647–51. https://doi.org/10.1017/s2398187300137946
• Zahn, David, Gayle Patterson, Paul Sampson, et al. 2024. “Flight Test Evaluation of Automation-Induced Oscillations.” In Aviation 2024. https://ntrs.nasa.gov/citations/20240007468
• Zahn, David, Gayle Patterson, Ethan Williams, Sarah Eggum, and Tyler Fettrow. n.d. “Flight Test Evaluation of Autonomous Descending-Decelerating Precision Point-in-Space Approach to the Ground.” In 43rd Digital Avionics Systems Conference. https://ntrs.nasa.gov/citations/20240008754
• Zalesak, P., Sr. 1981. “Flight Testing the Nonmetallic Spline Coupling Technology at the Naval Air Test Center.” In 1st Flight Test Conference. AIAA 1981-2405. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2405
• Zammit, Steve, and Koos Zwaanenburg. 1989. “Real-Time Flight Simulation Support for the X-31 Aircraft Program.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1989-3283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3283
• Zammit Mangion, David, Evangelia Pontika, Rachel Zammit-Mangion, and pericles Pilidis. 2024. “Mission Definition and Flight Performance Analysis of a Hydrogen Technology C-130J Flying Demonstrator.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3663
• Zander, Fabian. 2025. “Remote Diagnostics of Aerospace Ground and Flight Testing.” In IAF Space Operations Symposium. International Astronautical Federation (IAF). https://doi.org/10.52202/083086-0011
• Zanette, Joao Vitor, and Fabio Almeida. 2015. “Lateral-Directional Aerodynamic Model Identification of a Single-Engine Propeller Aircraft Using Partial Orthogonal Least Squares.” In AIAA Flight Testing Conference. AIAA 2015-3227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3227
• Zaw Linn, Khin. 2019. “Design, Construction and Flight Performance on T-Tail Airplane.” International Journal of Research Publications 21 (1). https://doi.org/10.47119/ijrp10021112019496
• Zeisloft, Harry. 1983. “Autogas Flight Test in a Cessna 150 Airplane.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/830706
• Zelinski, Shannon, Carl Recine, Carlos Natividad, et al. 2025. “Assessing National Airspace System Impact of the Transonic Truss-Braced Wing Aircraft.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3101
• Zemplenyi, Michele, and Jeffrey W. Miller. 2023. “Bayesian Optimal Experimental Design for Inferring Causal Structure.” Bayesian Analysis 18 (3): 929–56. https://doi.org/10.1214/22-ba1335
• Zeng, Jie, Raymond de Callafon, and Martin Brenner. 2009. “Adaptive Feedback Control Algorithm for Flutter Boundary Expansion.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-6145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6145
• Zeng, Jie, P. C. Chen, and Sunil Kukreja. 2012. “Investigation of the Prediction Error Identification for Flutter Prediction.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4575
• Zeng, Jie, Pc Chen, Rick Lind, and Chuck Harris. 2010. “Parameter Varying Estimation Toolbox for Flutter Prediction.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8115
• Zeng, Jie, Wenmin Qian, and Chuanjun Liu. 2017. “Application of Shape Function for Aeroelastic Tailoring of the Composite Wing Structure.” In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2017-4146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4146
• Zettervall, Niklas, and Christer Fureby. 2018. “A Computational Study of Ramjet, Scramjet and Dual-Mode Ramjet Combustion in Combustor with a Cavity Flameholder.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1146
• Zha, Gecheng, Hongsik Im, and Daniel Espinal. 2010. “Toward Zero Sonic-Boom and High Efficiency Supersonic Flight, Part I: A Novel Concept of Supersonic Bi-Directional Flying Wing.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1013
• Zhang, Chao. n.d. “Cantilever Plate Flutter in Wind Tunnel Tests and Comparison with 2D Theory.” PhD diss., The University of Hong Kong. https://doi.org/10.5353/th_b5699944
• Zhang, J. 1988. “A Numerical Method for Unsteady Transonic Flow about Low-Aspect-Ratio Wings.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4362
• Zhang, Yan Lian. 2013. “Design of Flight Test System Based on 1553B-Bus Real-Time Processing System.” Advanced Materials Research 774-776: 1481–84. https://doi.org/10.4028/www.scientific.net/amr.774-776.1481
• Zhang, Kenan, and Wanchun Chen. 2011. “Reentry Vehicle Constrained Trajectory Optimization.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2231. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2231
• Zhang, Geng, Jim He, and Nickolas Vlahopoulos. 2010. “Multidisciplinary Design under Uncertainty for a Hypersonic Vehicle.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9189. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9189
• Zhang, Liang, Liang Jing, Liheng Ye, and Xing Gao. 2021. “Predefined-Time Control for a Horizontal Takeoff and Horizontal Landing Reusable Launch Vehicle.” Aircraft Engineering and Aerospace Technology 93 (6): 957–70. https://doi.org/10.1108/aeat-11-2020-0253
• Zhang, Haoran, Tang Jingfeng, Ji Li, and Daren Yu. 2025c. “Dynamic Response of Combustion Mode to Dual-Frequency Discharge Plasma in Scramjet Engine.” Preprint, . https://doi.org/10.2139/ssrn.5233781
• Zhang, Xiayang, Wei Li, Xin Wang, and Qijun Zhao. 2025a. “Aeroelastic Modeling and Analysis of the Wing–Rotor System in Forward Flight Considering Rotor–Wing Aerodynamic Interference.” International Journal of Aeronautical and Space Sciences 27 (1): 512–33. https://doi.org/10.1007/s42405-025-00955-1
• Zhang, Fan, and Dirk Soffker. n.d. “Active Flutter Suppression of a Nonlinear Aeroelastic System Using PI-Observer.” In Motion and Vibration Control. Springer Netherlands. https://doi.org/10.1007/978-1-4020-9438-5_36
• Zhang, Shen, Qing Wang, and Chaoyang Dong. 2017b. “A Novel Adaptive Dynamic Surface Control Scheme of Hypersonic Flight Vehicles with Thrust and Actuator Constraints.” Transactions of the Institute of Measurement and Control 40 (4): 1362–74. https://doi.org/10.1177/0142331217690223
• Zhang, Yu, Zhengyou Wen, Haonan Chen, Yuchen Zhang, and Liaoni Wu. 2025e. “Trajectory Planning and Guidance Design for the Automatic Landing Phase of Reusable Launch Vehicle.” Journal of Physics: Conference Series 2977 (1): 012006. https://doi.org/10.1088/1742-6596/2977/1/012006
• Zhang, Ming, Dafu Xu, Shuai Yue, and Haifeng Tao. 2018. “Design and Dynamic Analysis of Landing Gear System in Vertical Takeoff and Vertical Landing Reusable Launch Vehicle.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (10): 3700–3713. https://doi.org/10.1177/0954410018804093
• Zhang, Jianye, and Peng Zhang. 2016. “Design and Implementation of Flight Data Mining System.” In Time Series Analysis Methods and Applications for Flight Data. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-53430-4_6
• Zhao, Xuejun. 2015. “Compressible Boundary Layer Transition Measurements on the Flat Plate.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3631
• Zhao, Min. 2021a. “Development of Hypersonic Aerothermodynamic Technologies.” In Springer Aerospace Technology. Springer Singapore. https://doi.org/10.1007/978-981-33-6526-1_1
• Zhao, Min. 2021b. “An Overview of Ground-Flying Calibration Technologies for Hypersonic Vehicle.” In Springer Aerospace Technology. Springer Singapore. https://doi.org/10.1007/978-981-33-6526-1_2
• Zhao, Qinghe. 2023. “Drag Reduction Design of Transonic Airfoil Based on Particle Swarm Optimization Algorithm.” Journal of Physics: Conference Series 2442 (1): 012038. https://doi.org/10.1088/1742-6596/2442/1/012038
• Zhao, Jingchao. 2026. “Flight Test Analysis Method for Aerodynamic Characteristics of Helicopter Rotor in Level Flight.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2026-99-1821
• Zhao, Huan, Zhenghong Gao, and Yuan Gao. 2017. “Design Optimization of Natural-Laminar-Flow Airfoil for Complicated Flight Conditions.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3060. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3060
• Zhao, Xi You, and Jun Hu. 2013. “Research on Aerodynamic Characteristics of Morphing Aircraft with a Telescopic Wing.” Advanced Materials Research 709: 257–61. https://doi.org/10.4028/www.scientific.net/amr.709.257
• Zhao, Rui, Guohua Tu, Jun Liang, and Chihyung Wen. 2025a. “Hypersonic Boundary-Layer Stabilization.” In Stabilization of Hypersonic Boundary-Layer: Acoustic Metasurfaces. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-8623-7_2
• Zhao, Libei, Zhixun Xia, Likun Ma, et al. 2022. “Study of Combustion Mode Identification Method on Dual-Mode Solid Rocket Scramjet.” Journal of Physics: Conference Series 2364 (1): 012066. https://doi.org/10.1088/1742-6596/2364/1/012066
• Zhao, Yatian, Xianda Zeng, Jian Luo, Fanzhi Zeng, Ze Pang, and Hongkang Liu. 2026. “Curvature-Controlled Instability Coupling in Hypersonic Three-Dimensional Boundary-Layer Transition.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9826495/v1
• Zhao, Qingfeng, Yawen Zhang, Rui Wang, and Zhou Zhou. 2025b. “Modeling and Control of Hover Flight for a Distributed Electric Propulsion VTOL.” Preprint, . https://doi.org/10.20944/preprints202508.2060.v1
• Zheng, Yiyu, Hutao Cui, and Yang Tian. 2015. “Improvements to Entry Terminal Point Controller for Mars Atmospheric Entry.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2398
• Zheng, Qiu Ya, Jian Hu Feng, and Zun Huan Shen. 2012. “Transonic Drag Prediction on a DLR-F6 Transport Configuration.” Advanced Materials Research 566: 676–79. https://doi.org/10.4028/www.scientific.net/amr.566.676
• Zheng, X., J. Wu, H. Sun, and C. Su. 2023. “Optimization Design of Hypersonic Vehicle Propulsion System Based on ISIGHT and MATLAB.” IET Conference Proceedings 2022 (21): 1215–26. https://doi.org/10.1049/icp.2022.3035
• Zhong, Xiaolin. 2000. “DNS of Boundary-Layer Receptivity to Freestream Sound for Hypersonic Flows over Blunt Elliptical Cones.” In Laminar-Turbulent Transition. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-03997-7_67
• Zhong, Xiaolin. 2009. Numerical Simulation of Hypersonic Boundary Layer Receptivity, Transient Growth and Transition with Surface Roughness. Defense Technical Information Center. https://doi.org/10.21236/ada517055
• Zhong, Shijie, Wanggang Shen, Tommie Catanach, and Xun Huan. 2026. “Goal-Oriented Bayesian Optimal Experimental Design for Nonlinear Models Using Markov Chain Monte Carlo.” SIAM/ASA Journal on Uncertainty Quantification 14 (1): 19–47. https://doi.org/10.1137/24m1649344
• Zhou, H. C. 2023. “Design of Hypersonic Vehicle Time-Delay Compensation Controller Based on Dynamic Surface Control.” International Journal of Vehicle Structures and Systems 15 (2). https://doi.org/10.4273/ijvss.15.2.22
• Zhou, Yan, Yihan Mei, Shanfei Su, Xiaowen Shan, and Hao Wang. 2023a. “Aerodynamics and Flight Performance of a UAV in Ground Effect Based on Flight Simulation.” In AIAA SCITECH 2023 Forum. AIAA 2023-2104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2104
• Zhou, Ling, Chao Yan, Zi Hui Hao, and Wei Xuan Kong. 2015b. “A “Laminar + Transition Criteria” Model for Hypersonic Three-Dimensional Boundary Layer Transition Prediction.” Applied Mechanics and Materials 798: 627–31. https://doi.org/10.4028/www.scientific.net/amm.798.627
• Zhu, Yuanhang, and Kenneth Breuer. 2022. “Aeroelastic Instability Boundaries of Pitching Swept Wings.” In AIAA SCITECH 2022 Forum. AIAA 2022-2328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2328
• Zhu, Li Feng, Kai Wang, Lei Wang, Wei Wei, Bo Guo, and Zheng Yu Lu. 2014. “A Horizontal Projection-Based Research on Cross Matching Method in Flight Trajectory of Airplane Model.” Applied Mechanics and Materials 602-605: 345–48. https://doi.org/10.4028/www.scientific.net/amm.602-605.345
• Zhuang, Weiliang, Zhenghong Li, Jiao Liu, and Zhenzong He. 2025. “Research on Multi-Objective Optimization of Aircraft NACA Inlet Air Characteristics Based on Neural Network.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-9771-4_39
• Zientek, Thomas A. 2001. “Expanding the Flight Envelope with a Segmented Rotor.” In Proceedings of the Vertical Flight Society Forum 57 - Washington, D.C. 2001. The Vertical Flight Society. https://doi.org/10.4050/vfs-f57-00067
• Zimpfer, Douglas. 1999. “Onorbit Flight Control Design for the Kistler K-1 Reusable Launch Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4210
• Zingg, David, Laslo Diosady, and Laura Billing. 2006. “Adaptive Airfoils for Drag Reduction at Transonic Speeds.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3656. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3656
• Zink, P. Scott, Dimitri N. Mavris, Peter M. Flick, and Michael H. Love. 1999. “Development of Wing Structural Weight Equation for Active Aeroelastic Wing Technology.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/1999-01-5640
• Zink, P., Dimitri Mavris, Michael Love, and Mordechay Karpel. 1998. “Robust Design for Aeroelastically Tailored/active Aeroelastic Wing.” In 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 1998-4781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4781
• Zink, P., Dimitri Mavris, and Daniella Raveh. 2000a. “Integrated Structural/trim Optimization for Active Aeroelastic Wing Technology.” In 8th Symposium on Multidisciplinary Analysis and Optimization. AIAA 2000-4827. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4827
• Zink, P., Daniella Raveh, and Dimitri Mavris. 2000b. “Robust Structural Design for Active Aeroelastic Wing with Aerodynamic Uncertainties.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1439
• Zink, P., Daniella Raveh, and Dimitri Mavris. 2001. “An Integrated Trim and Structural Design Process for Active Aeroelastic Wing Technology.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1427
• Zink, Paul, Daniella Raveh, and Dimitri Mavris. 2002. “Robust Structural Design of an Active Aeroelastic Wing with Maneuver Load Uncertainty.” In 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 2002-5603. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5603
• Zohuri, Bahman. 2015. “Similitude Theory and Applications.” In Dimensional Analysis and Self-Similarity Methods for Engineers and Scientists. Springer International Publishing. https://doi.org/10.1007/978-3-319-13476-5_2
• Zou, Zihao, and Xiaolin Zhong. 2026. “Receptivity and Biorthogonal Decomposition of Hypersonic Boundary Layer.” In Turbulence and Transition in Supersonic and Hypersonic Flows. Elsevier. https://doi.org/10.1016/b978-0-44-318785-8.00011-0
• Zuber, Matthew, and John Bertin. 1998. “Hypersonic Aerodynamic Research at the USAF Academy.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1633. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1633
• Zubrin, Robert, and Mitchell Clapp. 1996. “The Pioneer Pathfinder: A Low-Cost Solution for a near-Term Reusable Launch Vehicle.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4605
• Zumwalt, Carlie H., Juan R. Cruz, Donald F. Keller, and Clara O’Farrell. 2016. “Wind Tunnel Test of Subscale Ringsail and Disk-Gap-Band Parachutes.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160010106
• Zumwalt, G., and A. Mueller. 1984. “Flight and Wind Tunnel Tests of an Electro-Impulse De-Icing System.” In General Aviation Technology Conference. AIAA 1984-2234. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2234
• Zurer, Pamela S. 1995. “NASA Cultivating Basic Technology for Supersonic Passenger Aircraft: Top Priority Aeronautics Research Program Seeks to Clear Environmental and Cost Barriers to a New Generation of Supersonic Planes.” Chemical & Engineering News Archive 73 (17): 10–16. https://doi.org/10.1021/cen-v073n017.p010
• Zweber, Jeffrey, Hanee Kabis, William Follett, and Narayan Ramabadran. 2002. “Towards an Integrated Design Environment for Hypersonic Vehicle Design and Synthesis.” In AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2002-5172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5172
• Zyluk, Andrzej, and Krzysztof Sibilski. 2015. “The Gust Resistant MAV: Aerodynamic Measurements, Performance Analysis, and Flight Tests.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-1684. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1684
• Αργύρης, Κωνσταντίνος. n.d. “Bayesian Uncertainty Quantification and Optimal Experimental Design in Data Driven Simulations of Engineering Systems.” PhD diss., Πανεπιστήμιο Θεσσαλίας, Σχολή Πολυτεχνική, Τμήμα Μηχανολόγων Μηχανικών, Εργαστήριο Δυναμικής Συστημάτων. https://doi.org/10.12681/eadd/41258
• Ερτζάν, Τουλάι. n.d. “Bayesian Optimal Experimental Design Tools: -.” PhD diss., Πανεπιστήμιο Θεσσαλίας, Σχολή Πολυτεχνική, Τμήμα Μηχανολόγων Μηχανικών, Εργαστήριο Δυναμικής Συστημάτων. https://doi.org/10.12681/eadd/51842
• Казак, В. Н. 2000. “Flight Control of an Airplane Damaged in Flight.” Proceedings of the National Aviation University 7 (3–4). https://doi.org/10.18372/2306-1472.7.11270
• 신경은 and 엄정식. 2017. “The Study for the United States Air Force’s Dyna-Soar Project Approved by the Eisenhower Administration That Pursued the Peaceful Use Policy of Space.” military history null (102): 37–62. https://doi.org/10.29212/mh.2017..102.37

Secondary Sources

• American Institute of Aeronautics and Astronautics, ed. 2021. Recommended Practice: When Flight Modelling Is Used to Reduce Flight Testing Supporting Aircraft Certification (AIAA R-154-2021). American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.106231
• Amping Airpower—Electric Vertical Takeoff and Landing for the U.S. Air Force: Military Utility, Market Dynamics, and Warfighter Adoption. 2024. RAND Corporation. https://doi.org/10.7249/rra1524-2
• Anderson, John. 1997. A History of Aerodynamics and Its Impact on Flying Machines. Cambridge University Press. https://openlibrary.org/works/OL1993322W
• Anderson, John. 2001. Fundamentals of Aerodynamics. McGraw-Hill Science/Engineering/Math. https://openlibrary.org/works/OL3232211W
• Anderson, John. 2002a. The Airplane: A History of Its Technology. AIAA (American Institute of Aeronautics & Ast. https://openlibrary.org/works/OL3232201W
• Anderson, John. 2002b. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Science/Engineering/Math. https://openlibrary.org/works/OL1993329W
• Anderson, John. 2006. Hypersonic and High-Temperature Gas Dynamics. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL1993330W
• Anderson, John. 2012. Introduction to Flight. McGraw-Hill. https://openlibrary.org/works/OL1993331W
• Anderson, John, Aircraft performance, and design. 1999. Aircraft Performance and Design. WCB/McGraw-Hill. https://openlibrary.org/works/OL1993317W
• Ashley, marten landahl holt, and Landahl. 1965. Aerodynamics of Wings and Bodies. addison-wesley publishing company, inc. https://openlibrary.org/works/OL42971075W
• Asselin, Mario. 2021. Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.105920
• Atkinson, A. C., and Donev. 1992. Optimum Experimental Designs. Clarendon Press. https://openlibrary.org/works/OL4280715W
• Atmospheric Re-Entry Vehicle Mechanics. 2007. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-73647-9
• Baals, William Corliss Donald, and Corliss. 1981. Wind Tunnels of NASA. NATIONAL AERONAUTICS & SPACE. https://openlibrary.org/works/OL31504107W
• Barlow, Jewel B., Rae, and Pope. 1999. Low-Speed Wind Tunnel Testing. Wiley. https://openlibrary.org/works/OL1921571W
• Barnwell, R. W., and M. Y. Hussaini, eds. 1992. Natural Laminar Flow and Laminar Flow Control. Springer New York. https://doi.org/10.1007/978-1-4612-2872-1
• Bertin, John J. 1994. Hypersonic Aerothermodynamics. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL3287053W
• Bertin, John J., and Russell M. Cummings. 2013. Aerodynamics for Engineers. Pearson Education, Limited. https://openlibrary.org/works/OL21437883W
• Bevington, Philip R., and D. Keith Robinson. 2002. Data Reduction and Error Analysis for the Physical Sciences. McGraw-Hill. https://openlibrary.org/works/OL44935135W
• Bilstein, Roger E. 1989a. Orders of Magnitude: A History of the NACA and NASA, 1915-1990. United States Govt Printing Office. https://openlibrary.org/works/OL18823771W
• Bilstein, Roger E. 2001. Flight in America: From the Wrights to the Astronauts. Johns Hopkins University Press. https://openlibrary.org/works/OL2856898W
• Bisplinghoff, Raymond L., Ashley, Halfman, and Aeroelasticity. 1955. Aeroelasticity. Addison-Wesley Pub. Co. https://openlibrary.org/works/OL3240762W
• Box, George E. P., J. Stuart Hunter, and William G. Hunter. 2005. Statistics for Experimenters: Design, Innovation, and Discovery. Wiley & Sons, Incorporated, John. https://openlibrary.org/works/OL28985605W
• Boyd, Stephen, and Lieven Vandenberghe. 2004. Convex Optimization. Cambridge University Press. https://openlibrary.org/works/OL25692727W
• Braslow, Albert L. 1999a. A History of Suction-Type Laminar Flow Control with Emphasis on Flight Research. NASA Headquarters. https://ntrs.nasa.gov/citations/19990058717
• Bruhn, E. F. 1973. Analysis and Design of Flight Vehicle Structures. Jacobs Pub. https://openlibrary.org/works/OL8796483W
• Chambers, Joseph R. 2000a. Partners in Freedom Contributions of the Langley Research Center to U. S. Military Aircraft of the 1990’s [the NASA History Series]. National Aeronautics and Space Administration. https://openlibrary.org/works/OL33867704W
• Chambers, Joseph. 2005. Innovation in Flight: Research of the NASA Langley Research Center on Revolutionary Advanced Concepts for Aeronautics: NASA History Series. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL40097313W
• Chambers, Joseph R., and Joseph R. Chambers. 2008. Radical Wings & Wind Tunnels: Advanced Concepts Tested at NASA Langley. Specialty Press. https://openlibrary.org/works/OL5834577W
• A Comparison of Cost Models for Fighter Aircraft. 1977. RAND Corporation. https://doi.org/10.7249/p6011
• Constant, Edward W. 1980. The Origins of the Turbojet Revolution. Johns Hopkins University Press. https://openlibrary.org/works/OL6325070W
• Cost-Estimating Relationships for Aircraft Airframes. 1972. RAND Corporation. https://doi.org/10.7249/r0761
• Cover, Thomas M., and Joy A. Thomas. 2006. Elements of Information Theory. Wiley & Sons Canada, Limited, John. https://openlibrary.org/works/OL21500808W
• Crossfield, Albert Scott, and Clay Blair. 1960. Always Another Dawn: The Story of a Rocket Test Pilot. Independently Published. https://openlibrary.org/works/OL29040763W
• Curran, E. T., and S. N. B. Murthy, eds. 1991. High-Speed Flight Propulsion Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866104
• Curran, E. T., and S. N. B. Murthy. 2000. Scramjet Propulsion. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL23791670W
• de Syon, Guillaume. 2000. Allen, Edmund Turney (1896-1943), Test Pilot. Oxford University Press. https://doi.org/10.1093/anb/9780198606697.article.2001637
• Dickinson, William B., Jr. 1964. Supersonic Transport Race. CQ Press. https://doi.org/10.4135/cqresrre1964031800
• Dowell, Earl H., and A modern course in aeroelasticity. 2014. A Modern Course in Aeroelasticity: Fifth Revised and Enlarged Edition. Springer. https://openlibrary.org/works/OL20677670W
• Etkin, Bernard, Lloyd Duff Reid, and Dynamics of flight. 1959. Dynamics of Flight: Stability and Control. John Wiley & Sons/ Chapman & Hall. https://openlibrary.org/works/OL19844466W
• Ferguson, Eugene S. 1992. Engineering and the Mind’s Eye. MIT Press. https://openlibrary.org/works/OL4119982W
• Fletcher, Leroy S., ed. 1978. Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.865336
• Flight Test Instrumentation. 1965. Elsevier. https://doi.org/10.1016/c2013-0-01867-1
• Functional Approach to Optimal Experimental Design. 2006. Springer-Verlag. https://doi.org/10.1007/0-387-31610-8
• Fung, Y. C. 1955. An Introduction to the Theory of Aeroelasticity. Wiley. https://openlibrary.org/works/OL2655267W
• Gelman, Andrew, John B. Carlin, Hal S. Stern, Donald B. Rubin, David B. Dunson, and Aki Vehtari. 2013. Bayesian Data Analysis. Taylor & Francis Group. https://openlibrary.org/works/OL12630389W
• Godwin, Robert. 2000. X-15: The NASA Mission Reports (Apogee Books Space Series). Apogee Books. https://openlibrary.org/works/OL2881994W
• Gorn, Michael H. 1992. The Universal Man: Theodore Von Kármán’s Life in Aeronautics. Smithsonian Institution Press. https://openlibrary.org/works/OL4400575W
• Gorn, Michael H. 2001a. Expanding the Envelope: Flight Research at NACA and NASA. University Press of Kentucky. https://openlibrary.org/works/OL4400572W
• Gorn, Michael H. 2001b. Expanding the Envelope: Flight Research at NACA and NASA. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20010071533
• Gunston, Bill. 1992. Faster than Sound: The Story of Supersonic Flight. Haynes Pubns. https://openlibrary.org/works/OL774338W
• Hallion, Richard. 1972. Supersonic Flight. Macmillan. https://openlibrary.org/works/OL2688456W
• Hallion, Richard. 1981. Test Pilots: The Frontiersmen of Flight. Doubleday. https://openlibrary.org/works/OL2688457W
• Hallion, Richard P., and Curtis E. Peebles. 2014. Probing the Sky: Selected NACA Research Airplanes and Their Contributions to Flight. NASA. https://ntrs.nasa.gov/citations/20150008346
• Hansen, James R. 1987. Engineer in Charge: A History of Langley Aeronautical Laboratory, 1917-1958. United States Government Printing Office. https://openlibrary.org/works/OL37594565W
• Hansen, James R. 2004. The Bird Is on the Wing: Aerodynamics and the Progress of the American Airplane (Centennial of Flight Series, No. 6). Texas A&M University Press. https://openlibrary.org/works/OL3492401W
• Heiser, William H., and Pratt. 1994. Hypersonic Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL3932490W
• Heppenheimer, T. 2007. Facing the Heat Barrier: A History of Hypersonics: NASA History Series. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL39929219W
• Hill, Philip G., and Peterson. 1991. Mechanics and Thermodynamics of Propulsion [by] Philip G. Hill [and] Carl R. Peterson. https://openlibrary.org/works/OL8229940W
• Hodges, Dewey H., and Pierce. 2011. Introduction to Structural Dynamics and Aeroelasticity. Cambridge University Press. https://openlibrary.org/works/OL16972710W
• Houchin. 2006b. US Hypersonic Research and Development: The Rise and Fall of ‘Dyna-Soar’, 1944-1963. Taylor & Francis Group. https://openlibrary.org/works/OL21244606W
• Houchin, Roy F., II. 2006a. US Hypersonic Research and Development. Routledge. https://doi.org/10.4324/9780203012994
• Hurt, Hugh H. 1960. Aerodynamics for Naval Aviators. Office of the Chief of Naval Operations, Aviation Training Division, U.S. Navy. https://openlibrary.org/works/OL4297319W
• Huzel, Dieter K., and David H. Huang. 1992. Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL27313820W
• Hypersonic Flow Research. 1962. Elsevier. https://doi.org/10.1016/b978-0-12-395595-1.x5001-6
• Improving Acquisition and Sustainment Outcomes for Military Commercial Derived Aircraft: The KC-46A Pegasus Experience. 2023. RAND Corporation. https://doi.org/10.7249/rra1676-1
• Jaynes, E. T. 2003. Probability Theory: The Logic of Science. https://openlibrary.org/works/OL5911565W
• Jenkins, Dennis R. 2000a. Hypersonics before the Shuttle: A Concise History of the X-15 Research Airplane. https://openlibrary.org/works/OL813290W
• Jenkins, Dennis R. 2000b. Hypersonics before the Shuttle: A Concise History of the X-15 Research Airplane. NASA. https://ntrs.nasa.gov/citations/20000068530
• Jenkins, Dennis R. 2001. Space Shuttle: The History of the National Space Transportation System: The First 100 Missions. D.R. Jenkins. https://openlibrary.org/works/OL813312W
• Jenkins, Dennis R. 2007. X-15: Extending the Frontiers of Flight. NASA. https://ntrs.nasa.gov/citations/20080008340
• Jenkins, Dennis R., and Tony R. Landis. 2003. Hypersonic: The Story of the North American X-15. Specialty Press. https://openlibrary.org/works/OL813289W
• Jenkins, Dennis R., Tony Landis, and Jay Miller. 2003. American X-Vehicles: An Inventory X-1 to X-50 Centennial of Flight Edition. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL20394726W
• Johnson, Clarence L., and Smith. 1985. Kelly: More than My Share of It All. Smithsonian Institution Press. https://openlibrary.org/works/OL5461367W
• Jones, Robert M. 1998. Mechanics of Composite Materials. Taylor & Francis. https://openlibrary.org/works/OL1876296W
• Kerber, L. V. 1927. Proposed Standard Procedure for Computing Flight-Test Data. University of Michigan Press. https://doi.org/10.3998/mpub.12945728
• Kimberlin, Ralph D. 2003. Flight Testing of Fixed-Wing Aircraft (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast. https://openlibrary.org/works/OL8874080W
• Küchemann, Dietrich. 1978. The Aerodynamic Design of Aircraft. Published by the American Institute of Aeronautics and Astronautics, Inc. https://openlibrary.org/works/OL22640504W
• Kuethe, Arnold M. 1950. Foundations of Aerodynamics. Wiley. https://openlibrary.org/works/OL2661785W
• Larsson, Roger. 2019. Flight Test System Identification. Linköping University Electronic Press. https://doi.org/10.3384/diss.diva-156694
• Launius, Roger, and Dennis Jenkins. 2012. Coming Home: Reentry and Recovery from Space. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL39998199W
• Leary, William M. 2002. “We Freeze to Please”: A History of NASA’s Icing Research Tunnel and the Quest for Flight Safety. NASA. https://ntrs.nasa.gov/citations/20020066162
• Liepmann, Hans Wolfgang, and Roshko. 1957. Elements of Gasdynamics, by H.W. Liepmann [and] a. Roshko. Wiley. https://openlibrary.org/works/OL13214987W
• Loh, W. H. T. 1963. Dynamics and Thermodynamics of Planetary Entry. Prentice-Hall. https://openlibrary.org/works/OL7075585W
• Low Cost Cargo Aircraft: Turboprop or Turbofan?. 1960. RAND Corporation. https://doi.org/10.7249/p2049
• Lukasiewicz, J. 1973. Experimental Methods of Hypersonics. M. Dekker. https://openlibrary.org/works/OL6954489W
• MacKay, David J. C. 2003. Information Theory, Inference & Learning Algorithms. CAMBRIDGE UNIV PRESS. https://openlibrary.org/works/OL8325677W
• Maisel, Martin D., Demo J. Giulianetti, and Daniel C. Dugan. 2000. The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight. NASA. https://ntrs.nasa.gov/citations/20000027499
• Mattingly, Jack D. 2006. Elements of Propulsion: Gas Turbines and Rockets (AIAA Education) (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast. https://openlibrary.org/works/OL3739227W
• McRuer, Duane, Irving Ashkenas, and Dunstan Graham. 1990. Aircraft Dynamics and Automatic Control. Princeton Univ Pr. https://openlibrary.org/works/OL13424815W
• Megson, T. H. G., and Aircraft structures for engineering students. n.d. Aircraft Structures for Engineering Students. https://openlibrary.org/works/OL4809615W
• Merlin, Peter W. 2009. From Archangel to Senior Crown: Design and Development of the Blackbird. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL11706498W
• Miller, Jay. 2001. The X-Planes: X-1 to X-45: 3rd Edition. Midland. https://openlibrary.org/works/OL7006680W
• Mohamed, Majeed, and Vikalp Dongare. 2021a. Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0
• Morphing Wing Technologies. 2018. Elsevier. https://doi.org/10.1016/c2015-0-01317-x
• Nelson, Robert C. 1998. Flight Stability and Automatic Control. Mcgraw. https://openlibrary.org/works/OL11288560W
• Nicolai, Leland M., Carichner, Fundamentals of aircraft, and airship design. 2010a. Fundamentals of Aircraft and Airship Design: Aircraft Design. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL15909375W
• Niu, Chunyun. 1992. Composite Airframe Structures: Practical Design Information and Data. Conmilit Press. https://openlibrary.org/works/OL32576700W
• Niu, Michael Chun-Yung, and Mike Niu. 1988. Airframe Structural Design: Practical Design Information and Data on Aircraft Structures. Adaso Adastra Engineering Center. https://openlibrary.org/works/OL19561185W
• Nocedal, Jorge, and Stephen Wright. 2006. Numerical Optimization. Springer London, Limited. https://openlibrary.org/works/OL16972382W
• Olstad, Walter B., ed. 1980. Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.865435
• Osburg, Jan, Philip Anton, Frank Camm, et al. 2016. Expanding Flight Research: Capabilities, Needs, and Management Options for NASA’s Aeronautics Research Mission Directorate. RAND Corporation. https://doi.org/10.7249/rr1361
• Parameter Estimation Techniques and Application in Aircraft Flight Testing. 1974. NASA. https://ntrs.nasa.gov/citations/19740017456
• Parametric Flyaway Cost Estimating Relationships for Manned and Remotely Piloted Military Aircraft. 2024. RAND Corporation. https://doi.org/10.7249/rr1618.1
• Peebles, Curtis. 2007. The X-43A Flight Research Program: Lessons Learned on the Road to Mach 10. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070021686
• Peebles, Curtis. 2008a. Road to Mach 10: Lessons Learned from the X-43A Flight Research Program. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL2653134W
• Peebles, Curtis. 2008b. Road to Mach 10: Lessons Learned from the X-43A Flight Research Program. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.479328
• Peebles, Curtis. 2014. Probing the Sky: Selected NACA/NASA Research Airplanes and Their Contributions to Flight. National Aeronautics and Space Administration. https://openlibrary.org/works/OL23215820W
• Perrow, Charles. 1984. Normal Accidents: Living with High-Risk Technologies. Basic Books. https://openlibrary.org/works/OL4468929W
• Petroski, Henry. 1985. To Engineer Is Human: The Role of Failure in Successful Design. Macmillan. https://openlibrary.org/works/OL112186W
• Phillips, W. Hewitt. 1998. Journey in Aeronautical Research: A Career at NASA Langley Research Center: Monographs in Aerospace History: No. 12. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19990021535
• Pisano, Dominick A., van der Linden, and Frank H. Winter. 2006. Chuck Yeager and the Bell X-1: Breaking the Sound Barrier. “Harry N. Abrams, Inc.”. https://openlibrary.org/works/OL4301215W
• Pope, Alan, and Goin. 1965. High-Speed Wind Tunnel Testing [by] Alan Pope [and] Kennith L. Goin. Wiley. https://openlibrary.org/works/OL3791131W
• Portree, David S. F. 1998. NASA’s Origins and the Dawn of the Space Age: Monographs in Aerospace History: No. 10. NASA Headquarters. https://ntrs.nasa.gov/citations/19980236048
• Rafajłowicz, Ewaryst. 2022. Optimal Input Signals for Parameter Estimation: In Linear Systems with Spatio-Temporal Dynamics. De Gruyter. https://doi.org/10.1515/9783110351040
• Rand, Lisa Ruth. 2014. Cooper, L. Gordon, Jr. (1927-2004), Test Pilot and Astronaut. Oxford University Press. https://doi.org/10.1093/anb/9780198606697.article.2091933
• Raymer, Daniel P., Aircraft design, and a conceptual approach. 2012. Aircraft Design: A Conceptual Approach. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL17855977W
• Recapturing NASA’s Aeronautics Flight Research Capabilities. 2012. National Academies Press. https://doi.org/10.17226/13384
• Reed, R. Dale, and Darlene Lister. 1997. Wingless Flight: The Lifting Body Story. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL20339072W
• Regan, Frank J., and Anandakrishnan. 1993. Dynamics of Atmospheric Re-Entry. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL4305679W
• Remple, Robert K., and Mark B. Tischler. 2006. Aircraft and Rotorcraft System Identification: Engineering Methods with Flight-Test Examples. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.861352
• Report on Human Response to the Sonic Boom. 1968. National Academies Press. https://doi.org/10.17226/18775
• Report on Physical Effects of the Sonic Boom. 1968. National Academies Press. https://doi.org/10.17226/18702
• Reusable Launch Vehicle: Technology Development and Test Program. 1995. National Academies Press. https://doi.org/10.17226/5115
• Rich, Ben R., Leo Janos, and Skunk Works. 1994. Skunk Works: A Personal Memoir of My Years at Lockheed. Hachette Book Group. https://openlibrary.org/works/OL3466236W
• Rom, Josef. 1992. High Angle of Attack Aerodynamics: Subsonic, Transonic, and Supersonic Flows. Springer New York. https://doi.org/10.1007/978-1-4612-2824-0
• Roskam, Jan. 1985. Airplane Design. Roskam Aviation and Engineering Corp. https://openlibrary.org/works/OL6612019W
• Rotundo, Louis C. 1994. Into the Unknown: The X-1 Story. Smithsonian Institution Press. https://openlibrary.org/works/OL3920129W
• Sagan, Scott Douglas. 1993. The Limits of Safety: Organizations, Accidents, and Nuclear Weapons. Princeton University Press. https://openlibrary.org/works/OL3492159W
• Schlichting, Hermann, and Klaus Gersten. 2017. Boundary-Layer Theory. Springer London, Limited. https://openlibrary.org/works/OL20524688W
• Schultz, James. 2003. Crafting Flight: Aircraft Pioneers and the Contributions of the Men and Women of NASA Langley Research Center. NASA. https://ntrs.nasa.gov/citations/20040010394
• Scramjet Combustion. 2022. Elsevier. https://doi.org/10.1016/c2021-0-02204-5
• Sensitivity and Value of Information in Decision Trees. 2023. SAGE Publications, Ltd. https://doi.org/10.4135/9781529668896
• Shapiro, Ascher H. 1953. The Dynamics and Thermodynamics of Compressible Fluid Flow. Ronald Press Co. https://openlibrary.org/works/OL5908243W
• Simon, Daniel. 2014. Model Predictive Control in Flight Control Design: Stability and Reference Tracking. Linköping University Electronic Press. https://doi.org/10.3384/lic.diva-103742
• Sobron, Alejandro. 2018. On Subscale Flight Testing: Applications in Aircraft Conceptual Design. Linköping University Electronic Press. https://doi.org/10.3384/lic.diva-152488
• Sobrón Rueda, Alejandro. 2021. On Subscale Flight Testing: Cost-Effective Techniques for Research and Development. Linköping University Electronic Press. https://doi.org/10.3384/diss.diva-175520
• Srinathkumar, S. 2011. Eigenstructure Control Algorithms: Applications to Aircraft/rotorcraft Handling Qualities Design. Institution of Engineering and Technology. https://doi.org/10.1049/pbce074e
• Stengel, Robert F., and Flight dynamics. 2004. Flight Dynamics. Princeton University Press. https://openlibrary.org/works/OL3486012W
• Stevens, Brian L., Frank L. Lewis, and Eric N. Johnson. 2015. Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems. Wiley & Sons, Limited, John. https://openlibrary.org/works/OL21570717W
• Stinton, Darrol. 2001. The Design of the Aeroplane: Which Describes Common-Sense Mechanics of Design as They Affect the Flying Qualities of Aeroplanes Needing Only One Pilot. Blackwell Science. https://openlibrary.org/works/OL1911152W
• Stratford, Alan H. 1973a. Air Transport Economics in the Supersonic Era. Palgrave Macmillan UK. https://doi.org/10.1007/978-1-349-01549-8
• Sutton, George P., and Oscar Biblarz. 2016. Rocket Propulsion Elements. Wiley & Sons, Incorporated, John. https://openlibrary.org/works/OL21470530W
• Taylor, John R. 1997. An Introduction to Error Analysis: The Study of Uncertainties in Physical Measurements. University Science Books. https://openlibrary.org/works/OL3232610W
• Test Techniques for Flight Control Systems of Large Transport Aircraft. 2021. Elsevier. https://doi.org/10.1016/c2018-0-00829-4
• Thompson, Milton O. 1992. At the Edge of Space: The X-15 Flight Program. Smithsonian Books. https://openlibrary.org/works/OL1994111W
• Thompson, Milton O., J. D. Hunley, and Roger Launius. 2000. Flight Research: Problems Encountered and What They Should Teach Us. NASA. https://ntrs.nasa.gov/citations/20010072026
• Thornton, Earl A., ed. 1992. Thermal Structures and Materials for High-Speed Flight. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866128
• Tischler, Mark B., and Robert K. Remple. 2012. Aircraft and Rotorcraft System Identification: Engineering Methods with Flight Test Examples, Second Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.868207
• Torenbeek, Egbert. 2020. Essentials of Supersonic Commercial Aircraft Conceptual Design. Wiley. https://doi.org/10.1002/9781119667063
• Torenbeek, E., and Synthesis of subsonic airplane design. 1979. Synthesis of Subsonic Airplane Design: An Introduction to the Preliminary Design of Subsonic General Aviation and Transport Aircraft, with Emphasis on … Design, Propulsion and Performance. Springer. https://openlibrary.org/works/OL9096469W
• Truitt, Robert Wesley. 1960. Fundamentals of Aerodynamic Heating. Ronald Press. https://openlibrary.org/works/OL178473W
• Tsai, Stephen W., and Hahn. 1980. Introduction to Composite Materials. Technomic Pub. https://openlibrary.org/works/OL6341234W
• U.S. Supersonic Commercial Aircraft: Assessing NASA’s High Speed Research Program. 1997. National Academies Press. https://doi.org/10.17226/5848
• Vaughan, Diane. 1996. The Challenger Launch Decision: Risky Technology, Culture, and Deviance at NASA. University of Chicago Press. https://openlibrary.org/works/OL2962391W
• Vehicle Estimates for Target Designation RPVs. 1971. RAND Corporation. https://doi.org/10.7249/hda1607-1
• Viladegut, Alan. 2018. Assessment of Gas-Surface Interaction Modelling for Lifting Body Re-Entry Flight Design. von Karman Institute for Fluid Dynamics. https://doi.org/10.35294/phdt201804
• Vincenti, Walter G. 1990. What Engineers Know and How They Know It: Analytical Studies from Aeronautical History. Johns Hopkins University Press. https://openlibrary.org/works/OL4805206W
• Vinh, Nguyen X., Busemann, and Culp. 1980. Hypersonic and Planetary Entry Flight Mechanics. University of Michigan Press. https://openlibrary.org/works/OL4092275W
• Viskanta, Raymond, ed. 1979. Outer Planet Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.865381
• Volkov, Konstantin, ed. 2023. Hypersonic and Supersonic Flight: Advances in Aerodynamics, Materials, and Vehicle Design. IntechOpen. https://doi.org/10.5772/intechopen.104045
• Von Kármán, Theodore, and Edson. 1967. The Wind and Beyond: Theodore Von Kármán, Pioneer in Aviation and Pathfinder in Space. Little, Brown. https://openlibrary.org/works/OL7117470W
• Ward, Strganac, and Niewoehner. 2006. Introduction to Flight Test Engineering. Kendall Hunt Pub Co. https://openlibrary.org/works/OL19810630W
• Weiland, Claus, and Ernst Hirschel. 2009. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.479908
• White, Frank M. 2006. Viscous Fluid Flow. McGraw-Hill Higher Education. https://openlibrary.org/works/OL1911849W
• Whitford, Ray. 1987. Design for Air Combat. Jane’s. https://openlibrary.org/works/OL5054670W
• Wills, Colin. 2015a. Unmanned Combat Air Systems in Future Warfare. Palgrave Macmillan UK. https://doi.org/10.1057/9781137498496
• Winchester, Jim. 2005. X Planes Prototypes/Experimental Aircraf. Grange Books. https://openlibrary.org/works/OL8492617W
• Wolfe, Tom. 1979. The Right Stuff. https://openlibrary.org/works/OL1925474W
• Wooldridge, E. T. 2003. Engen, Donald Davenport (1924-1999), Naval Officer, Test Pilot, Public Servant. Oxford University Press. https://doi.org/10.1093/anb/9780198606697.article.0700779
• Wright, Jan Robert, Jonathan Edward Cooper, Introduction to aircraft aeroelasticity, and loads. 2007. Introduction to Aircraft Aeroelasticity and Loads. John Wiley & Sons. https://openlibrary.org/works/OL12439109W
• Yang, Tingwu. 2021c. Telemetry Theory and Methods in Flight Test. Springer Singapore. https://doi.org/10.1007/978-981-33-4737-3
• Yeager, Chuck, and Janos. 1985. Yeager, an Autobiography. Bantam Books. https://openlibrary.org/works/OL4628050W
• Younossi, Obaid, Michael Kennedy, and John Graser. 2001. New Processes for the Estimation of Military Airframe Costs. RAND Corporation. https://doi.org/10.7249/rb79

Commercial Sources

• “Armstrong Flight Research Center.” n.d. NASA. Accessed October 25, 2026. https://www.nasa.gov/centers-and-facilities/armstrong/
• Banke, Jim. 2016. “NASA Aeronautics Budget Proposes Return of X-Planes.” National Aeronautics and Space Administration, February 18. https://www.nasa.gov/centers-and-facilities/ames/nasa-aeronautics-budget-proposes-return-of-x-planes/
• “Bell X-1 Glamorous Glennis.” n.d. Smithsonian National Air and Space Museum. Accessed October 24, 2026. https://airandspace.si.edu/collection-objects/bell-x-1-glamorous-glennis/nasm_A19510007000
• Benson, Tom. n.d. “Viscosity.” Beginner’s Guide to Hypersonics. Accessed October 24, 2026. https://www.grc.nasa.gov/www/BGH/viscosity.html
• “DARPA Official Site.” n.d. Accessed October 24, 2026. https://www.darpa.mil/
• Defense Advanced Research Projects Agency. 2026. “DARPA’s New X-76: The Speed of a Jet, the Freedom of a Helicopter: SPRINT X-76 Enters Build Phase to Demonstrate Runway-Independent, High-Speed Flight.” Defense Advanced Research Projects Agency, March 9. https://www.darpa.mil/news/2026/darpa-new-x-76-speed-of-jet-freedom-of-helicopter
• “NASA History Office.” n.d. Accessed October 24, 2026. https://www.nasa.gov/history/

General Sources

• “Kordes and Noll Flight Loads Measurements on the X-15.” n.d. Accessed October 24, 2026. https://ntrs.nasa.gov/search?q=flight%20loads%20measurements%20X-15%20airplane
• Krone. 1975. “Divergence Elimination with Advanced Composites.” https://ntrs.nasa.gov/search?q=Krone%20divergence%20elimination%20with%20advanced%20composites%20forward%20swept%20wing
• McClinton. 2006. “X-43 Scramjet Power Breaks the Hypersonic Barrier.” https://ntrs.nasa.gov/search?q=X-43%20scramjet%20power%20breaks%20the%20hypersonic%20barrier%20Dryden%20lectureship
• “NASA Technical Reports Server.” n.d. Accessed October 25, 2026. https://ntrs.nasa.gov/
• Riddell, Frederick R., Martin Summerfield, and R. E. Street. 1962. “Hypersonic Flow Research.” Physics Today 15 (11): 76–78. https://doi.org/10.1063/1.3057873

Tertiary Sources

• “Ablation.” 2026. Wikipedia. Last modified July 26, at 20:27 (UTC). https://en.wikipedia.org/w/index.php?title=Ablation&oldid=1366193010
• “Adolf Busemann.” 2026. Wikipedia. Last modified June 12, at 13:46 (UTC). https://en.wikipedia.org/w/index.php?title=Adolf_Busemann&oldid=1359013165
• “Aerobee.” 2026. Wikipedia. Last modified June 23, at 14:34 (UTC). https://en.wikipedia.org/w/index.php?title=Aerobee&oldid=1360775001
• “Aerodynamic Center.” 2026. Wikipedia. Last modified April 5, at 16:04 (UTC). https://en.wikipedia.org/w/index.php?title=Aerodynamic_center&oldid=1347249608
• “Aeroelasticity.” 2026. Wikipedia. Last modified August 1, at 15:32 (UTC). https://en.wikipedia.org/w/index.php?title=Aeroelasticity&oldid=1367186470
• “Air Force Research Laboratory.” 2026. Wikipedia. Last modified June 18, at 03:13 (UTC). https://en.wikipedia.org/w/index.php?title=Air_Force_Research_Laboratory&oldid=1359928127
• “Aircraft Flight Dynamics.” 2026. Wikipedia. Last modified June 27, at 22:00 (UTC). https://en.wikipedia.org/w/index.php?title=Aircraft_flight_dynamics&oldid=1361433043
• “Area Rule.” 2026. Wikipedia. Last modified July 3, at 19:54 (UTC). https://en.wikipedia.org/w/index.php?title=Area_rule&oldid=1362409745
• “Armstrong Flight Research Center.” 2026. Wikipedia. Last modified May 30, at 07:50 (UTC). https://en.wikipedia.org/w/index.php?title=Armstrong_Flight_Research_Center&oldid=1356860896
• “Aspect Ratio (Aeronautics).” 2026. Wikipedia. Last modified May 21, at 13:38 (UTC). https://en.wikipedia.org/w/index.php?title=Aspect_ratio_(aeronautics)&oldid=1355374989
• “Atmospheric Entry.” 2026. Wikipedia. Last modified July 26, at 21:22 (UTC). https://en.wikipedia.org/w/index.php?title=Atmospheric_entry&oldid=1366205102
• “Aurora X-65 CRANE.” 2026. Wikipedia. Last modified July 4, at 06:57 (UTC). https://en.wikipedia.org/w/index.php?title=Aurora_X-65_CRANE&oldid=1362484399
• “Ballistic Coefficient.” 2026. Wikipedia. Last modified July 16, at 23:46 (UTC). https://en.wikipedia.org/w/index.php?title=Ballistic_coefficient&oldid=1364505283
• “Bayesian Experimental Design.” 2026. Wikipedia. Last modified May 31, at 21:27 (UTC). https://en.wikipedia.org/w/index.php?title=Bayesian_experimental_design&oldid=1357119619
• “Bell X-1.” 2026. Wikipedia. Last modified June 1, at 08:33 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-1&oldid=1357198470
• “Bell X-14.” 2026. Wikipedia. Last modified May 14, at 16:44 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-14&oldid=1354149621
• “Bell X-16.” 2025. Wikipedia. Last modified April 21, at 21:51 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-16&oldid=1286771591
• “Bell X-2.” 2026. Wikipedia. Last modified June 5, at 01:41 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-2&oldid=1357851079
• “Bell X-22.” 2026. Wikipedia. Last modified May 21, at 14:56 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-22&oldid=1355384594
• “Bell X-5.” 2026. Wikipedia. Last modified June 16, at 18:23 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-5&oldid=1359700610
• “Bell X-9 Shrike.” 2024. Wikipedia. Last modified February 27, at 13:16 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-9_Shrike&oldid=1210610675
• “Bensen B-8.” 2026. Wikipedia. Last modified March 13, at 07:34 (UTC). https://en.wikipedia.org/w/index.php?title=Bensen_B-8&oldid=1343264109
• “Binomial Distribution.” 2026. Wikipedia. Last modified June 13, at 20:20 (UTC). https://en.wikipedia.org/w/index.php?title=Binomial_distribution&oldid=1359203125
• “Boeing B-52 Stratofortress.” 2026. Wikipedia. Last modified August 4, at 14:02 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_B-52_Stratofortress&oldid=1367674817
• “Boeing X-20 Dyna-Soar.” 2026. Wikipedia. Last modified July 24, at 19:51 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-20_Dyna-Soar&oldid=1365845652
• “Boeing X-32.” 2026. Wikipedia. Last modified August 4, at 18:22 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-32&oldid=1367709153
• “Boeing X-37.” 2026. Wikipedia. Last modified July 7, at 03:41 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-37&oldid=1362950749
• “Boeing X-40.” 2025. Wikipedia. Last modified August 3, at 16:56 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-40&oldid=1304047722
• “Boeing X-45.” 2026. Wikipedia. Last modified May 22, at 03:22 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-45&oldid=1355484000
• “Boeing X-46.” 2025. Wikipedia. Last modified October 31, at 22:02 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-46&oldid=1319792815
• “Boeing X-48.” 2025. Wikipedia. Last modified November 11, at 14:49 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-48&oldid=1321603411
• “Boeing X-50 Dragonfly.” 2026. Wikipedia. Last modified February 11, at 17:37 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-50_Dragonfly&oldid=1337826686
• “Boeing X-51 Waverider.” 2026. Wikipedia. Last modified June 18, at 20:55 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-51_Waverider&oldid=1360036635
• “Boeing X-53 Active Aeroelastic Wing.” 2026. Wikipedia. Last modified May 15, at 01:16 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-53_Active_Aeroelastic_Wing&oldid=1354217149
• “Boeing X-66.” 2026. Wikipedia. Last modified July 25, at 20:33 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_X-66&oldid=1366020754
• “Boundary Layer.” 2026. Wikipedia. Last modified April 24, at 16:14 (UTC). https://en.wikipedia.org/w/index.php?title=Boundary_layer&oldid=1350882651
• “Buckingham Pi Theorem.” 2026. Wikipedia. Last modified February 20, at 11:37 (UTC). https://en.wikipedia.org/w/index.php?title=Buckingham_pi_theorem&oldid=1339414059
• “Chuck Yeager.” 2026. Wikipedia. Last modified July 26, at 17:04 (UTC). https://en.wikipedia.org/w/index.php?title=Chuck_Yeager&oldid=1366159580
• “Convair X-6.” 2026. Wikipedia. Last modified June 5, at 11:35 (UTC). https://en.wikipedia.org/w/index.php?title=Convair_X-6&oldid=1357908013
• “Critical Mach Number.” 2026. Wikipedia. Last modified March 24, at 22:36 (UTC). https://en.wikipedia.org/w/index.php?title=Critical_Mach_number&oldid=1345208821
• “Curtiss-Wright X-19.” 2026. Wikipedia. Last modified April 5, at 06:27 (UTC). https://en.wikipedia.org/w/index.php?title=Curtiss-Wright_X-19&oldid=1347190617
• “Damköhler Numbers.” 2026. Wikipedia. Last modified June 23, at 16:11 (UTC). https://en.wikipedia.org/w/index.php?title=Damk%C3%B6hler_numbers&oldid=1360787322
• “DARPA.” 2026. Wikipedia. Last modified August 3, at 23:50 (UTC). https://en.wikipedia.org/w/index.php?title=DARPA&oldid=1367582302
• “DARPA Falcon Project.” 2025. Wikipedia. Last modified December 8, at 12:08 (UTC). https://en.wikipedia.org/w/index.php?title=DARPA_Falcon_Project&oldid=1326336442
• “Delta Wing.” 2026. Wikipedia. Last modified March 22, at 12:46 (UTC). https://en.wikipedia.org/w/index.php?title=Delta_wing&oldid=1344770205
• “Douglas X-3 Stiletto.” 2025. Wikipedia. Last modified November 8, at 15:35 (UTC). https://en.wikipedia.org/w/index.php?title=Douglas_X-3_Stiletto&oldid=1321081857
• “Drag Coefficient.” 2026. Wikipedia. Last modified April 10, at 13:33 (UTC). https://en.wikipedia.org/w/index.php?title=Drag_coefficient&oldid=1348064431
• “Drag Curve.” 2026. Wikipedia. Last modified May 13, at 22:40 (UTC). https://en.wikipedia.org/w/index.php?title=Drag_curve&oldid=1354034912
• “Drag-Divergence Mach Number.” 2026. Wikipedia. Last modified February 11, at 00:16 (UTC). https://en.wikipedia.org/w/index.php?title=Drag-divergence_Mach_number&oldid=1337700758
• “Dutch Roll.” 2026. Wikipedia. Last modified April 27, at 03:28 (UTC). https://en.wikipedia.org/w/index.php?title=Dutch_roll&oldid=1351296518
• “Dynamic Pressure.” 2025. Wikipedia. Last modified November 20, at 06:58 (UTC). https://en.wikipedia.org/w/index.php?title=Dynamic_pressure&oldid=1323192083
• “Dynetics X-61 Gremlins.” 2025. Wikipedia. Last modified January 11, at 18:17 (UTC). https://en.wikipedia.org/w/index.php?title=Dynetics_X-61_Gremlins&oldid=1268816378
• “Edwards Air Force Base.” 2026. Wikipedia. Last modified August 5, at 00:51 (UTC). https://en.wikipedia.org/w/index.php?title=Edwards_Air_Force_Base&oldid=1367754618
• “Energy–maneuverability Theory.” 2026. Wikipedia. Last modified February 10, at 13:02 (UTC). https://en.wikipedia.org/w/index.php?title=Energy%E2%80%93maneuverability_theory&oldid=1337603045
• “Experimental Aircraft.” 2026. Wikipedia. Last modified June 7, at 06:23 (UTC). https://en.wikipedia.org/w/index.php?title=Experimental_aircraft&oldid=1358202387
• “Flight Envelope.” 2025. Wikipedia. Last modified June 9, at 19:25 (UTC). https://en.wikipedia.org/w/index.php?title=Flight_envelope&oldid=1294779750
• “Flight Test.” 2025. Wikipedia. Last modified November 23, at 11:07 (UTC). https://en.wikipedia.org/w/index.php?title=Flight_test&oldid=1323721398
• “Forward-Swept Wing.” 2026. Wikipedia. Last modified July 15, at 02:18 (UTC). https://en.wikipedia.org/w/index.php?title=Forward-swept_wing&oldid=1364193418
• “Future Aircraft Technology Enhancements.” 2026. Wikipedia. Last modified July 25, at 23:11 (UTC). https://en.wikipedia.org/w/index.php?title=Future_Aircraft_Technology_Enhancements&oldid=1366042278
• “General Atomics XQ-67A.” 2026. Wikipedia. Last modified January 12, at 03:56 (UTC). https://en.wikipedia.org/w/index.php?title=General_Atomics_XQ-67A&oldid=1332491931
• “General Dynamics X-62 VISTA.” 2026. Wikipedia. Last modified May 14, at 16:38 (UTC). https://en.wikipedia.org/w/index.php?title=General_Dynamics_X-62_VISTA&oldid=1354148860
• “Generation Orbit X-60.” 2026. Wikipedia. Last modified July 16, at 02:31 (UTC). https://en.wikipedia.org/w/index.php?title=Generation_Orbit_X-60&oldid=1364359079
• “Grumman X-29.” 2026. Wikipedia. Last modified March 26, at 09:53 (UTC). https://en.wikipedia.org/w/index.php?title=Grumman_X-29&oldid=1345488135
• “Gulfstream X-54.” 2026. Wikipedia. Last modified July 31, at 06:28 (UTC). https://en.wikipedia.org/w/index.php?title=Gulfstream_X-54&oldid=1366984615
• “Heat Flux.” 2026. Wikipedia. Last modified February 4, at 19:37 (UTC). https://en.wikipedia.org/w/index.php?title=Heat_flux&oldid=1336610285
• “Hiller X-18.” 2026. Wikipedia. Last modified April 5, at 06:10 (UTC). https://en.wikipedia.org/w/index.php?title=Hiller_X-18&oldid=1347189032
• “Hypersonic Flight.” 2026. Wikipedia. Last modified July 16, at 04:32 (UTC). https://en.wikipedia.org/w/index.php?title=Hypersonic_flight&oldid=1364374853
• “Hypersonic Wind Tunnel.” 2026. Wikipedia. Last modified January 21, at 05:44 (UTC). https://en.wikipedia.org/w/index.php?title=Hypersonic_wind_tunnel&oldid=1334046877
• “Inconel.” 2026. Wikipedia. Last modified June 24, at 15:06 (UTC). https://en.wikipedia.org/w/index.php?title=Inconel&oldid=1360930983
• “Inertia Coupling.” 2025. Wikipedia. Last modified December 8, at 22:28 (UTC). https://en.wikipedia.org/w/index.php?title=Inertia_coupling&oldid=1326422870
• “International Standard Atmosphere.” 2026. Wikipedia. Last modified July 14, at 16:39 (UTC). https://en.wikipedia.org/w/index.php?title=International_Standard_Atmosphere&oldid=1364119487
• “Junkers Ju 287.” 2026. Wikipedia. Last modified July 22, at 16:43 (UTC). https://en.wikipedia.org/w/index.php?title=Junkers_Ju_287&oldid=1365468091
• “Kármán Line.” 2026. Wikipedia. Last modified July 15, at 21:18 (UTC). https://en.wikipedia.org/w/index.php?title=K%C3%A1rm%C3%A1n_line&oldid=1364312719
• “Karush–Kuhn–Tucker Conditions.” 2026. Wikipedia. Last modified June 8, at 21:37 (UTC). https://en.wikipedia.org/w/index.php?title=Karush%E2%80%93Kuhn%E2%80%93Tucker_conditions&oldid=1358466796
• “Knudsen Number.” 2026. Wikipedia. Last modified June 22, at 02:49 (UTC). https://en.wikipedia.org/w/index.php?title=Knudsen_number&oldid=1360535957
• “Kratos XQ-58 Valkyrie.” 2026. Wikipedia. Last modified August 3, at 22:24 (UTC). https://en.wikipedia.org/w/index.php?title=Kratos_XQ-58_Valkyrie&oldid=1367572946
• “Kullback–Leibler Divergence.” 2026. Wikipedia. Last modified July 15, at 12:25 (UTC). https://en.wikipedia.org/w/index.php?title=Kullback%E2%80%93Leibler_divergence&oldid=1364249363
• “Lagrange Multiplier.” 2026. Wikipedia. Last modified July 8, at 18:40 (UTC). https://en.wikipedia.org/w/index.php?title=Lagrange_multiplier&oldid=1363206730
• “Laminar Flow.” 2025. Wikipedia. Last modified July 21, at 22:31 (UTC). https://en.wikipedia.org/w/index.php?title=Laminar_flow&oldid=1301823620
• “Lift Coefficient.” 2026. Wikipedia. Last modified March 24, at 18:00 (UTC). https://en.wikipedia.org/w/index.php?title=Lift_coefficient&oldid=1345170854
• “Lift-to-Drag Ratio.” 2026. Wikipedia. Last modified May 16, at 13:54 (UTC). https://en.wikipedia.org/w/index.php?title=Lift-to-drag_ratio&oldid=1354447709
• “List of Experimental Aircraft.” 2026. Wikipedia. Last modified June 16, at 18:42 (UTC). https://en.wikipedia.org/w/index.php?title=List_of_experimental_aircraft&oldid=1359703466
• “List of United States Tri-Service Aircraft Designations.” 2026. Wikipedia. Last modified July 31, at 05:28 (UTC). https://en.wikipedia.org/w/index.php?title=List_of_United_States_Tri-Service_aircraft_designations&oldid=1366979010
• “List of X-Planes.” 2026. Wikipedia. Last modified June 16, at 19:44 (UTC). https://en.wikipedia.org/w/index.php?title=List_of_X-planes&oldid=1359712029
• “Lockheed CL-1200 Lancer.” 2025. Wikipedia. Last modified November 29, at 16:34 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_CL-1200_Lancer&oldid=1324793114
• “Lockheed F-104 Starfighter.” 2026. Wikipedia. Last modified July 26, at 20:49 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_F-104_Starfighter&oldid=1366197980
• “Lockheed Martin X-33.” 2026. Wikipedia. Last modified June 19, at 23:02 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-33&oldid=1360208553
• “Lockheed Martin X-35.” 2026. Wikipedia. Last modified July 25, at 06:18 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-35&oldid=1365924511
• “Lockheed Martin X-44 MANTA.” 2026. Wikipedia. Last modified May 1, at 09:16 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-44_MANTA&oldid=1351984359
• “Lockheed Martin X-55.” 2025. Wikipedia. Last modified December 18, at 21:52 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-55&oldid=1328271237
• “Lockheed Martin X-56.” 2026. Wikipedia. Last modified January 21, at 20:49 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-56&oldid=1334146801
• “Lockheed Martin X-59 Quesst.” 2026. Wikipedia. Last modified July 21, at 19:32 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_Martin_X-59_Quesst&oldid=1365334981
• “Lockheed U-2.” 2026. Wikipedia. Last modified August 4, at 13:30 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_U-2&oldid=1367671066
• “Lockheed X-17.” 2024. Wikipedia. Last modified August 18, at 10:49 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_X-17&oldid=1240936671
• “Lockheed X-7.” 2026. Wikipedia. Last modified May 31, at 14:29 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_X-7&oldid=1357058663
• “Longitudinal Stability.” 2026. Wikipedia. Last modified March 13, at 01:57 (UTC). https://en.wikipedia.org/w/index.php?title=Longitudinal_stability&oldid=1343225347
• “Ludwig Prandtl.” 2026. Wikipedia. Last modified June 30, at 09:25 (UTC). https://en.wikipedia.org/w/index.php?title=Ludwig_Prandtl&oldid=1361826498
• “Mach Number.” 2026. Wikipedia. Last modified July 21, at 19:50 (UTC). https://en.wikipedia.org/w/index.php?title=Mach_number&oldid=1365337650
• “Martin Marietta X-24.” 2026. Wikipedia. Last modified July 2, at 03:37 (UTC). https://en.wikipedia.org/w/index.php?title=Martin_Marietta_X-24&oldid=1362134430
• “Martin X-23 PRIME.” 2026. Wikipedia. Last modified April 18, at 23:11 (UTC). https://en.wikipedia.org/w/index.php?title=Martin_X-23_PRIME&oldid=1349788802
• “McDonnell Douglas X-36.” 2026. Wikipedia. Last modified June 9, at 15:39 (UTC). https://en.wikipedia.org/w/index.php?title=McDonnell_Douglas_X-36&oldid=1358573088
• “Measurement Uncertainty.” 2026. Wikipedia. Last modified August 2, at 18:11 (UTC). https://en.wikipedia.org/w/index.php?title=Measurement_uncertainty&oldid=1367370535
• “NASA.” 2026. Wikipedia. Last modified July 30, at 01:25 (UTC). https://en.wikipedia.org/w/index.php?title=NASA&oldid=1366759859
• “NASA X-38.” 2026. Wikipedia. Last modified April 18, at 23:28 (UTC). https://en.wikipedia.org/w/index.php?title=NASA_X-38&oldid=1349791068
• “NASA X-43.” 2026. Wikipedia. Last modified August 1, at 11:52 (UTC). https://en.wikipedia.org/w/index.php?title=NASA_X-43&oldid=1367164912
• “NASA X-57 Maxwell.” 2026. Wikipedia. Last modified May 5, at 20:02 (UTC). https://en.wikipedia.org/w/index.php?title=NASA_X-57_Maxwell&oldid=1352706947
• “National Advisory Committee for Aeronautics.” 2026. Wikipedia. Last modified June 10, at 22:19 (UTC). https://en.wikipedia.org/w/index.php?title=National_Advisory_Committee_for_Aeronautics&oldid=1358779367
• “North American X-10.” 2024. Wikipedia. Last modified November 13, at 05:15 (UTC). https://en.wikipedia.org/w/index.php?title=North_American_X-10&oldid=1257092074
• “North American X-15.” 2026. Wikipedia. Last modified July 8, at 22:01 (UTC). https://en.wikipedia.org/w/index.php?title=North_American_X-15&oldid=1363232706
• “Northrop Grumman X-47B.” 2026. Wikipedia. Last modified April 20, at 01:08 (UTC). https://en.wikipedia.org/w/index.php?title=Northrop_Grumman_X-47B&oldid=1350044624
• “Northrop X-21.” 2026. Wikipedia. Last modified July 25, at 13:11 (UTC). https://en.wikipedia.org/w/index.php?title=Northrop_X-21&oldid=1365965891
• “Northrop X-4 Bantam.” 2025. Wikipedia. Last modified September 13, at 11:16 (UTC). https://en.wikipedia.org/w/index.php?title=Northrop_X-4_Bantam&oldid=1311101016
• “Nyquist–Shannon Sampling Theorem.” 2026. Wikipedia. Last modified August 1, at 16:45 (UTC). https://en.wikipedia.org/w/index.php?title=Nyquist%E2%80%93Shannon_sampling_theorem&oldid=1367195325
• “Orbital Sciences X-34.” 2026. Wikipedia. Last modified June 13, at 22:49 (UTC). https://en.wikipedia.org/w/index.php?title=Orbital_Sciences_X-34&oldid=1359221653
• “Osprey Osprey I.” 2025. Wikipedia. Last modified December 22, at 10:29 (UTC). https://en.wikipedia.org/w/index.php?title=Osprey_Osprey_I&oldid=1328887479
• “Oswald Efficiency Number.” 2026. Wikipedia. Last modified February 21, at 03:03 (UTC). https://en.wikipedia.org/w/index.php?title=Oswald_efficiency_number&oldid=1339548943
• Parsch, Andreas. 2002a. “DOD 4120.15-L: Addendum: MDS Designators Allocated after 19 August 1998 (until November 2025).” Designations of U.S. Military Aircraft. https://www.designation-systems.net/usmilav/412015-L(addendum).html
• Parsch, Andreas. 2002b. ““Missing” USAF/DOD Aircraft Designations.” Designation-Systems.Net. https://www.designation-systems.net/usmilav/missing-mds.html
• Parsch, Andreas. 2006. “Orbital Sciences USFE (X-42).” Directory of U.S. Military Rockets and Missiles. https://www.designation-systems.net/dusrm/app4/x-42.html
• “Phugoid.” 2026. Wikipedia. Last modified March 25, at 19:48 (UTC). https://en.wikipedia.org/w/index.php?title=Phugoid&oldid=1345375911
• “Piasecki X-49 SpeedHawk.” 2025. Wikipedia. Last modified October 28, at 17:10 (UTC). https://en.wikipedia.org/w/index.php?title=Piasecki_X-49_SpeedHawk&oldid=1319244222
• “Prandtl Number.” 2026. Wikipedia. Last modified June 3, at 23:53 (UTC). https://en.wikipedia.org/w/index.php?title=Prandtl_number&oldid=1357669388
• “Prandtl–Glauert Singularity.” 2025. Wikipedia. Last modified June 18, at 18:11 (UTC). https://en.wikipedia.org/w/index.php?title=Prandtl%E2%80%93Glauert_singularity&oldid=1296229963
• “Prandtl–Glauert Transformation.” 2025. Wikipedia. Last modified July 28, at 14:03 (UTC). https://en.wikipedia.org/w/index.php?title=Prandtl%E2%80%93Glauert_transformation&oldid=1302988225
• “Propagation of Uncertainty.” 2026. Wikipedia. Last modified January 10, at 08:21 (UTC). https://en.wikipedia.org/w/index.php?title=Propagation_of_uncertainty&oldid=1332173257
• “Pulse-Code Modulation.” 2026. Wikipedia. Last modified March 9, at 03:48 (UTC). https://en.wikipedia.org/w/index.php?title=Pulse-code_modulation&oldid=1342473067
• “Ramjet.” 2026. Wikipedia. Last modified May 10, at 15:40 (UTC). https://en.wikipedia.org/w/index.php?title=Ramjet&oldid=1353487326
• “Range (Aeronautics).” 2026. Wikipedia. Last modified June 9, at 20:54 (UTC). https://en.wikipedia.org/w/index.php?title=Range_(aeronautics)&oldid=1358612677
• “Reaction Control System.” 2026. Wikipedia. Last modified June 23, at 07:00 (UTC). https://en.wikipedia.org/w/index.php?title=Reaction_control_system&oldid=1360731507
• “Reaction Motors XLR11.” 2026. Wikipedia. Last modified January 8, at 20:56 (UTC). https://en.wikipedia.org/w/index.php?title=Reaction_Motors_XLR11&oldid=1331905169
• “Reaction Motors XLR99.” 2026. Wikipedia. Last modified March 16, at 00:22 (UTC). https://en.wikipedia.org/w/index.php?title=Reaction_Motors_XLR99&oldid=1343720775
• “Reynolds Number.” 2026. Wikipedia. Last modified July 2, at 12:53 (UTC). https://en.wikipedia.org/w/index.php?title=Reynolds_number&oldid=1362194896
• “Richard T. Whitcomb.” 2026. Wikipedia. Last modified July 31, at 02:23 (UTC). https://en.wikipedia.org/w/index.php?title=Richard_T._Whitcomb&oldid=1366961254
• “Robert Thomas Jones (Engineer).” 2026. Wikipedia. Last modified July 31, at 02:30 (UTC). https://en.wikipedia.org/w/index.php?title=Robert_Thomas_Jones_(engineer)&oldid=1366962040
• “Rockwell X-30.” 2026. Wikipedia. Last modified April 18, at 23:30 (UTC). https://en.wikipedia.org/w/index.php?title=Rockwell_X-30&oldid=1349791405
• “Rockwell-MBB X-31.” 2026. Wikipedia. Last modified January 12, at 09:05 (UTC). https://en.wikipedia.org/w/index.php?title=Rockwell-MBB_X-31&oldid=1332528370
• “Ryan X-13 Vertijet.” 2026. Wikipedia. Last modified May 14, at 16:39 (UTC). https://en.wikipedia.org/w/index.php?title=Ryan_X-13_Vertijet&oldid=1354149090
• “Schweizer X-26 Frigate.” 2025. Wikipedia. Last modified October 29, at 08:05 (UTC). https://en.wikipedia.org/w/index.php?title=Schweizer_X-26_Frigate&oldid=1319352446
• “Scramjet.” 2026. Wikipedia. Last modified June 23, at 07:36 (UTC). https://en.wikipedia.org/w/index.php?title=Scramjet&oldid=1360734823
• “Sears–Haack Body.” 2026. Wikipedia. Last modified January 18, at 20:44 (UTC). https://en.wikipedia.org/w/index.php?title=Sears%E2%80%93Haack_body&oldid=1333615860
• “Similitude.” 2026. Wikipedia. Last modified April 8, at 23:21 (UTC). https://en.wikipedia.org/w/index.php?title=Similitude&oldid=1347810321
• “SM-65 Atlas.” 2026. Wikipedia. Last modified July 4, at 11:55 (UTC). https://en.wikipedia.org/w/index.php?title=SM-65_Atlas&oldid=1362506481
• “Sound Barrier.” 2026. Wikipedia. Last modified July 20, at 18:39 (UTC). https://en.wikipedia.org/w/index.php?title=Sound_barrier&oldid=1365170399
• “Specific Impulse.” 2026. Wikipedia. Last modified June 29, at 04:42 (UTC). https://en.wikipedia.org/w/index.php?title=Specific_impulse&oldid=1361633653
• “Speed of Sound.” 2026. Wikipedia. Last modified June 23, at 08:19 (UTC). https://en.wikipedia.org/w/index.php?title=Speed_of_sound&oldid=1360738426
• “Stagnation Temperature.” 2025. Wikipedia. Last modified March 15, at 22:24 (UTC). https://en.wikipedia.org/w/index.php?title=Stagnation_temperature&oldid=1280690173
• “Stall (Fluid Dynamics).” 2026. Wikipedia. Last modified July 4, at 14:56 (UTC). https://en.wikipedia.org/w/index.php?title=Stall_(fluid_dynamics)&oldid=1362523428
• “Stefan–Boltzmann Law.” 2026. Wikipedia. Last modified July 26, at 01:51 (UTC). https://en.wikipedia.org/w/index.php?title=Stefan%E2%80%93Boltzmann_law&oldid=1366061882
• “Supersonic Speed.” 2026. Wikipedia. Last modified June 7, at 02:54 (UTC). https://en.wikipedia.org/w/index.php?title=Supersonic_speed&oldid=1358181368
• “Swept Wing.” 2026. Wikipedia. Last modified May 21, at 17:56 (UTC). https://en.wikipedia.org/w/index.php?title=Swept_wing&oldid=1355410696
• “Telemetry.” 2026. Wikipedia. Last modified July 14, at 15:08 (UTC). https://en.wikipedia.org/w/index.php?title=Telemetry&oldid=1364108053
• “Theodore Von Kármán.” 2026. Wikipedia. Last modified July 31, at 02:56 (UTC). https://en.wikipedia.org/w/index.php?title=Theodore_von_K%C3%A1rm%C3%A1n&oldid=1366965968
• “Thrust-Specific Fuel Consumption.” 2025. Wikipedia. Last modified December 16, at 03:32 (UTC). https://en.wikipedia.org/w/index.php?title=Thrust-specific_fuel_consumption&oldid=1327790465
• “Transonic.” 2026. Wikipedia. Last modified March 19, at 15:25 (UTC). https://en.wikipedia.org/w/index.php?title=Transonic&oldid=1344296529
• “Tsiolkovsky Rocket Equation.” 2026. Wikipedia. Last modified June 4, at 05:39 (UTC). https://en.wikipedia.org/w/index.php?title=Tsiolkovsky_rocket_equation&oldid=1357709322
• “Turbojet.” 2026. Wikipedia. Last modified June 20, at 03:53 (UTC). https://en.wikipedia.org/w/index.php?title=Turbojet&oldid=1360241019
• “U.S. Standard Atmosphere.” 2026. Wikipedia. Last modified March 20, at 18:40 (UTC). https://en.wikipedia.org/w/index.php?title=U.S._Standard_Atmosphere&oldid=1344480951
• “Viscosity.” 2026. Wikipedia. Last modified July 9, at 01:52 (UTC). https://en.wikipedia.org/w/index.php?title=Viscosity&oldid=1363261473
• “Wave Drag.” 2025. Wikipedia. Last modified November 22, at 19:16 (UTC). https://en.wikipedia.org/w/index.php?title=Wave_drag&oldid=1323602563
• “Wind Tunnel.” 2026. Wikipedia. Last modified July 28, at 11:26 (UTC). https://en.wikipedia.org/w/index.php?title=Wind_tunnel&oldid=1366503596
• “Wing Loading.” 2026. Wikipedia. Last modified April 22, at 17:34 (UTC). https://en.wikipedia.org/w/index.php?title=Wing_loading&oldid=1350568065
• “X-41 Common Aero Vehicle.” 2026. Wikipedia. Last modified April 23, at 07:09 (UTC). https://en.wikipedia.org/w/index.php?title=X-41_Common_Aero_Vehicle&oldid=1350667634

Related Posts

• Sechter, Brendan. 2026. “Rocket Propellant Chemistry, A Design-Tradeoff Space.” Brendan A R Sechter’s Development Blog, February 1. https://sgeos.github.io/aerospace/propulsion/chemistry/2026/02/01/rocket_propellant_chemistry_a_design_tradeoff_space.html
• Sechter, Brendan. 2026. “Introduction to Space Studies.” Brendan A R Sechter’s Development Blog, February 21. https://sgeos.github.io/space/math/2026/02/21/introduction_to_space_studies.html
• Sechter, Brendan. 2026. “Cryptotelemeritocracy for Space Exploitation.” Brendan A R Sechter’s Development Blog, February 23. https://sgeos.github.io/space/management/philosophy/2026/02/23/cryptotelemeritocracy_for_space_exploitation.html
• Sechter, Brendan. 2026. “History of Rocketplanes.” Brendan A R Sechter’s Development Blog, February 27. https://sgeos.github.io/space/history/2026/02/27/history_of_rocketplanes.html
• Sechter, Brendan. 2026. “What Does the United States Space Force Do?” Brendan A R Sechter’s Development Blog, February 28. https://sgeos.github.io/space/military/2026/02/28/what_does_united_states_space_force_do.html
• Sechter, Brendan. 2026. “Two-Stage Flying Delta Wing Vehicles for Civil and National Security Applications.” Brendan A R Sechter’s Development Blog, March 12. https://sgeos.github.io/aerospace/engineering/2026/03/12/two_stage_flying_delta_wing_vehicles_for_civil_and_national_security_applications.html
• Sechter, Brendan. 2026. “Propulsion and Power Sizing for Small Fixed-Wing UAVs.” Brendan A R Sechter’s Development Blog, June 2. https://sgeos.github.io/aerospace/engineering/uav/2026/06/02/propulsion_and_power_sizing_for_fixed_wing_uavs.html
• Sechter, Brendan. 2026. “Staged and Boosted Propulsion for Small Fixed-Wing UAVs.” Brendan A R Sechter’s Development Blog, June 3. https://sgeos.github.io/aerospace/engineering/uav/2026/06/03/staged_and_boosted_propulsion_for_fixed_wing_uavs.html
• Sechter, Brendan. 2026. “Stability, Control, and Configuration for Fixed-Wing UAVs.” Brendan A R Sechter’s Development Blog, June 5. https://sgeos.github.io/aerospace/engineering/uav/2026/06/05/stability_control_and_configuration_for_fixed_wing_uavs.html
• Sechter, Brendan. 2026. “Dynamic Stability and Control for Fixed-Wing UAVs.” Brendan A R Sechter’s Development Blog, June 6. https://sgeos.github.io/aerospace/engineering/uav/2026/06/06/dynamic_stability_and_control_for_fixed_wing_uavs.html
• Sechter, Brendan. 2026. “Structures and the Flight Envelope for Fixed-Wing UAVs.” Brendan A R Sechter’s Development Blog, June 10. https://sgeos.github.io/aerospace/engineering/uav/2026/06/10/structures_and_the_flight_envelope_for_fixed_wing_uavs.html
• Sechter, Brendan. 2026. “Aerospace, Programming Languages, and Information Technology Co-Development: Framing and the Co-Development Mechanism.” Brendan A R Sechter’s Development Blog, July 13. https://sgeos.github.io/history/technology/aerospace/2026/07/13/framing_and_the_co_development_mechanism.html
• Sechter, Brendan. 2026. “Aerospace, Programming Languages, and Information Technology Co-Development: Aerospace Simulation and Real-Time Systems.” Brendan A R Sechter’s Development Blog, July 17. https://sgeos.github.io/history/technology/aerospace/2026/07/17/aerospace_simulation_and_real_time_systems.html
• Sechter, Brendan. 2026. “Aerospace, Programming Languages, and Information Technology Co-Development: Space Shuttle Software as Engineering Landmark.” Brendan A R Sechter’s Development Blog, July 20. https://sgeos.github.io/history/technology/aerospace/2026/07/20/space_shuttle_software_as_engineering_landmark.html
• Sechter, Brendan. 2026. “Aerospace, Programming Languages, and Information Technology Co-Development: Software-Defined Aerospace and Autonomy.” Brendan A R Sechter’s Development Blog, July 23. https://sgeos.github.io/history/technology/aerospace/2026/07/23/software_defined_aerospace_and_autonomy.html
• Sechter, Brendan. 2026. “History of SpaceX: Series Framing and the Seven-Plus-Three Forcing-Function Framework.” Brendan A R Sechter’s Development Blog, July 25. https://sgeos.github.io/history/business/aerospace/2026/07/25/spacex_history_framing.html
• Sechter, Brendan. 2026. “History of SpaceX: The Category-Dominating Commercial Spinoff and the Internalization of Anchor Demand.” Brendan A R Sechter’s Development Blog, August 4. https://sgeos.github.io/history/business/aerospace/2026/08/04/spacex_history_category_dominating_spinoff.html