X-Planes: Douglas X-3 Stiletto

The Douglas X-3 Stiletto was built to sustain Mach 2 on a very thin wing of very low aspect ratio, and to demonstrate that such an airframe could be manufactured in titanium. It never reached Mach 2. It never reached Mach 1.3, and it exceeded Mach 1 only in a dive [Day 1997]. By the conventional accounting it is the least successful aircraft in this series so far, and it produced the single most consequential data set of the early X-planes. This article is the fourth in the X-Planes series and the third per-aircraft treatment, following the Bell X-1 and the Bell X-2. The National Advisory Committee for Aeronautics, abbreviated NACA throughout and reconstituted in 1958 as the National Aeronautics and Space Administration, abbreviated NASA, supplied the research programme [Wikipedia, NACA] [Dinius 2014]. The Air Force sponsored the aircraft [Boslaugh]. The Douglas Aircraft Company supplied an airframe designed around an engine that was never delivered.

The Research Question

The keystone is the aerodynamic and structural behaviour of a very thin, very low aspect ratio straight wing in sustained supersonic flight, together with the manufacturability of a titanium primary structure.

Both halves follow from the same premise. The starting point is the linearized supersonic result of Ackeret 1925, in which the pressure coefficient on a thin surface depends only on local slope,

\[C_p = \frac{2 \, \theta}{\sqrt{M_\infty^2 - 1}} \tag{1}\]

with $\theta$ the local surface inclination in radians. Integrating over a symmetric section at zero lift gives a wave drag proportional to the mean square slope, and since slope scales with thickness ratio the result is quadratic. Wave drag scales as the square of thickness ratio, so a wing at 4.5 percent thickness carries

\[\frac{D_{w}(4.5\%)}{D_{w}(8\%)} = \left( \frac{4.5}{8.0} \right)^2 = 0.32 \tag{2}\]

of the wave drag of the X-1 section at the same conditions. That gain is enormous, and it explains why supersonic aircraft are given thin wings. The difficulty is that a thin wing has almost no internal volume for structure or fuel, so its stiffness and strength must come from material rather than from depth, and its bending capability falls as the cube of thickness for a given cap area. Titanium was the candidate material because its specific strength exceeds aluminium and it retains that advantage to higher temperature [Wikipedia, Titanium].

The structural difficulty can be stated quantitatively. For a wing box of chord $c$ and thickness ratio $\tau = t/c$, the structural depth is $h_s = \tau c$ and the second moment of area of the cap material about the neutral axis is

\[I_{\text{box}} \approx \frac{A_{\text{cap}} h_s^2}{2} = \frac{A_{\text{cap}} \tau^2 c^2}{2} \tag{3}\]

so bending stiffness falls as the square of thickness ratio for fixed cap area, and the cap area required to carry a given moment at a given stress rises as

\[A_{\text{cap}} \propto \frac{1}{\tau} \tag{4}\]

The flutter boundary that follows depends on the ratio of torsional to bending frequency and on the mass ratio,

\[\omega_\alpha = \sqrt{\frac{K_\theta}{I_\theta}}, \qquad \mu_m = \frac{m_w}{\pi \rho b^2}, \qquad F_i = \frac{V_f}{b \omega_\alpha \sqrt{\mu_m}} \tag{5}\]

and reducing $K_\theta$ by a factor of three reduces $\omega_\alpha$ by $\sqrt{3}$ and the flutter speed with it. The unsteady aerodynamics that determine where that boundary actually lies were not computable in 1952 and became so only gradually, through the shear-flow treatments of Williams et al. 1977, the panel methods evaluated by Appa and Smith 1988, the correlation studies of Yates et al. 1982c, and eventually the constrained optimization of Striz and Venkayya 1990. Torsional stiffness is worse. The enclosed area of the box scales as $A_m \approx \tau c^2$, and the Bredt relation gives a torsion constant

\[J = \frac{4 A_m^2}{\oint ds / t} \propto \tau^2 \tag{6}\]

so a wing at 4.5 percent thickness has roughly a third the torsion constant of one at 8 percent for the same skin gauge and planform. The X-3 buys a factor of three in wave drag and pays a factor of three in torsional stiffness, and the second of those is what puts it near its aeroelastic limits.

The second half of the keystone is that the aircraft was to hold Mach 2 rather than touch it [Dinius 2014]. The X-1 and X-2 were rocket aircraft that reached a condition and immediately began decelerating, so their data are transients through a point. A turbojet aircraft can hold a condition, and that ability turns a measurement into a survey. The distinction is visible in the energy accounting. A rocket aircraft in a ballistic exchange conserves energy height,

\[h_e = h + \frac{V^2}{2 g}, \qquad \frac{dh_e}{dt} = P_s = \frac{V (T - D)}{W} \tag{7}\]

and once the propellant is gone $P_s$ is negative everywhere, so every data point is taken while decelerating. A turbojet aircraft with $P_s = 0$ available at the test condition can dwell there indefinitely, and the measurement becomes a steady-state one with all the statistical advantages that implies, since averaging over a dwell of duration $T_d$ reduces random uncertainty as

\[\sigma \propto \frac{1}{\sqrt{T_d}} \tag{8}\]

That distinction matters because it is the reason the programme wanted turbojets in the first place. The Air Force contract of June 1945 called for a turbojet aircraft that could cruise at Mach 2 for 30 minutes, and Boslaugh judges the X-3 a disappointment because of low engine power [Boslaugh]. The article infers from these two facts that the engine substitution cost the programme its purpose, the sustained supersonic dwell, and not merely some of its performance.

Programme Origin

Douglas began design studies for the Army Air Forces at the end of 1943 [Boslaugh], and construction of two aircraft was approved on 30 June 1949 [Dinius 2014]. A single aircraft, serial 49-2892, was built [Jenkins et al. 2003]. The configuration is the most extreme in this series. A fuselage 20.35 metres long including its nose boom carried a wing of 15.47 square metres and 6.92 metres span [Fischel et al. 1957], giving an aspect ratio of

\[A = \frac{b^2}{S} = \frac{6.92^2}{15.47} = 3.10 \tag{9}\]

and a mean chord of 2.24 metres. The wing is a small trapezoidal surface attached near the rear of a very long pointed body, which is why the aircraft was named for a knife and why the photographs are misleading about its size.

The propulsion decision is the central fact of the programme’s history. The design was sized around two Westinghouse J46 engines, each expected to deliver about 7000 pounds of thrust with afterburner [Wikipedia, Douglas X-3]. The J46 fell behind schedule, failed to meet its thrust, size and weight requirements, and never became available [Dinius 2014] [Boslaugh]. Douglas substituted two Westinghouse J34 engines of about 4900 pounds each [Fischel et al. 1957]. The installed thrust became

\[T_{\text{J34}} = 2 \times 4900 \times 4.448 = 4.36 \times 10^{4} \ \text{newtons} \tag{10}\]

against a design value of

\[T_{\text{J46}} = 2 \times 7000 \times 4.448 = 6.23 \times 10^{4} \ \text{newtons} \tag{11}\]

a shortfall of

\[1 - \frac{T_{\text{J34}}}{T_{\text{J46}}} = 30 \ \text{percent} \tag{12}\]

Holding the aircraft weight fixed as a first approximation, the thrust-to-weight ratio falls in direct proportion,

\[\frac{(T/W)_{\text{J34}}}{(T/W)_{\text{J46}}} = \frac{T_{\text{J34}}}{T_{\text{J46}}} = 0.70 \tag{13}\]

An airframe optimized for one engine and flown with another producing seventy percent of the thrust is not a degraded version of the intended aircraft. It is a different aircraft, and the next section shows how different.

Sizing From First Principles

This is the only article in the series so far in which the keystone sizing does not close. Working it through is more informative than a successful closure would be.

Level flight requires thrust to equal drag,

\[T = D = q S C_D \tag{14}\]

with dynamic pressure most conveniently written as

\[q = \frac{\gamma}{2} p M^2 \tag{15}\]

The compressible relations behind these are the standard set, tabulated in Ames Research Staff 1953,

\[\frac{p_0}{p} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}}, \qquad \frac{T_0}{T} = 1 + \frac{\gamma - 1}{2} M^2 \tag{16}\]

with the disturbance geometry fixed by the Mach angle

\[\mu_M = \arcsin \frac{1}{M} \tag{17}\]

and the area a stream tube must pass through given by

\[\frac{A}{A^{*}} = \frac{1}{M} \left[ \frac{2}{\gamma + 1} \left( 1 + \frac{\gamma - 1}{2} M^2 \right) \right]^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{18}\]

a relation that sizes every inlet throat. Substituting and solving for Mach number gives the thrust-limited maximum,

\[M_{\max}^2 = \frac{2 T}{\gamma \, p \, S \, C_D} \tag{19}\]

so that, holding altitude and drag coefficient fixed,

\[\frac{M_{\max, 2}}{M_{\max, 1}} = \sqrt{\frac{T_2}{T_1}} \tag{20}\]

A thirty percent thrust shortfall therefore costs

\[\sqrt{0.70} = 0.837 \tag{21}\]

in maximum Mach number, taking a design value of 2.0 to 1.67. The aircraft achieved 1.21 [Day 1997]. The engine substitution alone does not explain the outcome, and the residual repays attention because the interesting engineering lies there.

The inlet supplies most of it. The X-3 had side inlets, and no source consulted here records any variable geometry in them. Treated as fixed, they would have been sized for the intended engine and the intended flight condition. A fixed inlet operating supersonically swallows a shock, and in the simplest case that shock is normal to the flow, across which the total pressure recovery is

\[\frac{p_{02}}{p_{01}} = \left[ \frac{(\gamma + 1) M_1^2}{(\gamma - 1) M_1^2 + 2} \right]^{\frac{\gamma}{\gamma - 1}} \left[ \frac{\gamma + 1}{2 \gamma M_1^2 - (\gamma - 1)} \right]^{\frac{1}{\gamma - 1}} \tag{22}\]

The static conditions behind the shock follow the rest of the Rankine-Hugoniot set,

\[\frac{p_2}{p_1} = \frac{2 \gamma M_1^2 - (\gamma - 1)}{\gamma + 1}, \qquad \frac{T_2}{T_1} = \frac{\left[ 2 \gamma M_1^2 - (\gamma - 1) \right] \left[ (\gamma - 1) M_1^2 + 2 \right]}{(\gamma + 1)^2 M_1^2} \tag{23}\] \[M_2^2 = \frac{(\gamma - 1) M_1^2 + 2}{2 \gamma M_1^2 - (\gamma - 1)} \tag{24}\]

so that at Mach 2 the flow behind a normal shock is at Mach 0.577 and has been heated by 69 percent. The compressor face sees that condition. Evaluating the recovery shows how quickly the penalty arrives. At Mach 1.2 the recovery is 0.993 and the loss is negligible. At Mach 1.5 it is 0.930. At Mach 2.0 it is 0.721. Since turbojet thrust scales very nearly with the total pressure delivered to the compressor face,

\[\frac{T}{T_{\text{ideal}}} \approx \frac{p_{02}}{p_{01}} \tag{25}\]

the aircraft loses another 28 percent of its thrust at the design condition purely to the inlet.

That is only half of what a fixed inlet costs. The other half is drag. An inlet has a capture area $A_c$ set by geometry and a demanded stream tube area $A_0$ set by what the engine can swallow at the current condition, and their ratio is the mass flow ratio

\[\frac{A_0}{A_c} = \frac{\dot{m}_{\text{engine}}}{\rho_\infty V_\infty A_c} \tag{26}\]

At the design point these match. Away from it the engine demands less than the inlet captures, the excess spills around the cowl, and the momentum change of the spilled flow appears as additive drag,

\[D_{\text{add}} = \dot{m}_0 \left( V_\infty - V_1 \right) + \left( p_1 - p_\infty \right) A_1 \tag{27}\]

with the subscript 1 denoting conditions at the cowl lip. Non-dimensionally,

\[C_{D,\text{add}} = \frac{D_{\text{add}}}{q S} \approx \frac{2 A_c}{S} \left( 1 - \frac{A_0}{A_c} \right) \sin^2 \theta_c \tag{28}\]

for a cowl of lip angle $\theta_c$, which grows linearly with the mismatch. A fixed inlet flown below its design Mach number therefore suffers twice, losing thrust to poor recovery and gaining drag from spillage, and the two act in the same direction on the thrust margin,

\[T_{\text{eff}} = \eta_d \, T_{\text{ideal}} - D_{\text{add}} - D_{\text{div}} \tag{29}\]

where $D_{\text{div}}$ is the drag of the boundary layer diverter, the wedge that keeps fuselage boundary layer out of a side inlet and which for a side-mounted arrangement like the X-3 is not small.

There is a stability limit as well. When spillage becomes large enough the terminal shock is expelled from the throat and oscillates, a condition called buzz, which occurs roughly when

\[\frac{A_0}{A_c} < \left( \frac{A_0}{A_c} \right)_{\text{crit}} \tag{30}\]

and which imposes an unsteady load on the compressor face. A fixed inlet has no way to avoid it except by flying nearer the design point, and an underpowered aircraft cannot do that. Combining the two effects gives an effective thrust factor of

\[0.70 \times 0.721 = 0.505 \tag{31}\]

and a maximum Mach number of

\[M_{\max} = 2.0 \times \sqrt{0.505} = 1.42 \tag{32}\]

which is close to what the aircraft did. The remaining gap between 1.42 and 1.21 is attributable to drag being higher than estimated, to installed thrust falling below nameplate, and to the fact that the aircraft could only be pushed past Mach 1 in a dive, and the record does not separate these.

Two further effects enter the accounting. Turbojet thrust lapses with altitude roughly in proportion to ambient pressure with a ram correction,

\[\frac{T(h, M)}{T_{SL}} \approx \frac{p(h)}{p_{SL}} \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}} \eta_d \tag{33}\]

so climbing to the altitude where the wave drag is tolerable costs thrust that the ram recovery only partly returns, and with $\eta_d$ falling as derived the two terms fight each other above Mach 1.5. And the transonic drag rise must be crossed before any of this matters. The excess thrust available for that crossing is

\[T - D = m \frac{dV}{dt} + m g \sin \gamma \tag{34}\]

so in level acceleration the whole excess goes into $dV/dt$, and the time to cross a Mach increment is

\[t_{\text{cross}} = \int_{V_1}^{V_2} \frac{m \, dV}{T(V) - D(V)} \tag{35}\]

which diverges as $T$ approaches $D$. An aircraft with a small thrust margin does not cross the drag rise slowly. It fails to cross it at all, because the integrand becomes singular before the far side is reached. That is the mechanism by which the X-3 was confined to dives, where the gravity term supplies what the engines could not.

The important structural point is that the two losses compound rather than add. A thirty percent engine shortfall would have been survivable. A twenty-eight percent inlet loss on the intended engine would also have been survivable. Together they halve the available thrust, and halving thrust costs thirty percent of Mach number. The X-3 is a case study in how a system sized against a single design point fails when two of its assumptions move together.

One further consequence follows. The specific excess power available for acceleration is

\[P_s = \frac{V (T - D)}{W} \tag{36}\]

and the altitude at which $P_s$ falls to zero is the ceiling,

\[P_s = 0 \quad \Longleftrightarrow \quad T(h) = D(h) \tag{37}\]

so an aircraft short of thrust is short of ceiling as well as of speed, and the X-3 was confined to a lower band of altitudes than intended, where the higher density raises $q$ and therefore drag for the same Mach number. The two penalties reinforce. Thrust-to-weight completes the picture. At the maximum takeoff mass of 10,161 kilograms [Wikipedia, Douglas X-3],

\[\frac{T}{W} = \frac{4.36 \times 10^{4}}{10{,}161 \times 9.80665} = 0.44 \tag{38}\]

which is poor for an aircraft expected to accelerate through the transonic drag rise, and the wing loading is extreme,

\[\frac{W}{S} = \frac{10{,}161 \times 9.80665}{15.47} = 6441 \ \text{newtons per square metre} \tag{39}\]

more than forty percent above the X-1 figure. The manoeuvre envelope that follows has its corner at

\[V_A = \sqrt{\frac{2 n_{\max} W}{\rho S C_{L,\max}}} \tag{40}\]

and with the high wing loading and low maximum lift coefficient of this configuration the corner speed is high, so the aircraft cannot reach its structural limit aerodynamically over most of its envelope. The load factor available at any speed below the corner is

\[n(V) = \frac{\rho V^2 C_{L,\max}}{2 \left( W / S \right)} \tag{41}\]

which for the X-3 falls below unity under about 108 metres per second. That figure is the stall speed derived in the takeoff section below, arrived at from the opposite direction, and the agreement is a useful internal check. The aircraft cannot sustain level flight at all below it. Those two numbers together describe an aircraft that is hard to accelerate and hard to slow down, and the flight record bears that description out [Dinius 2014].

Dependent Systems

The Wing

The wing is the reason the aircraft exists. It is a radical object. Its section is a modified hexagon 4.5 percent thick [Fischel et al. 1957], and at aspect ratio 3.10 it behaves more like a slender surface than a lifting line.

Supersonic lift follows the linearized result of Ackeret 1925,

\[C_{L\alpha} = \frac{4}{\sqrt{M_\infty^2 - 1}} \tag{42}\]

which applies when the wing behaves two-dimensionally. The governing parameter is the supersonic aspect ratio,

\[\beta_s A = \sqrt{M_\infty^2 - 1} \; A \tag{43}\]

and at Mach 2 this is $\sqrt{3} \times 3.10 = 5.36$, comfortably above the value near four beyond which tip effects become secondary. The X-3 wing is therefore effectively two-dimensional in supersonic flight despite its low aspect ratio, giving

\[C_{L\alpha} = \frac{4}{\sqrt{3}} = 2.31 \ \text{per radian} \tag{44}\]

The centre of pressure on such a wing moves with Mach number, from roughly the quarter chord subsonically to the half chord supersonically,

\[\frac{x_{ac}}{\bar{c}} : 0.25 \longrightarrow 0.50 \tag{45}\]

producing a trim change and a static margin change,

\[SM = \frac{x_{np} - x_{cg}}{\bar{c}}, \qquad C_{m\alpha} = -C_{L\alpha} \, SM \tag{46}\]

The neutral point that fixes the margin is

\[\frac{x_{np}}{\bar{c}} = \frac{x_{ac,w}}{\bar{c}} + V_H \frac{C_{L\alpha_t}}{C_{L\alpha_w}} \left( 1 - \frac{d\varepsilon}{d\alpha} \right), \qquad V_H = \frac{S_t l_t}{S \bar{c}} \tag{47}\]

and the resulting longitudinal modes are the short period and the phugoid,

\[\omega_{sp} \approx \sqrt{\frac{Z_\alpha M_q}{V} - M_\alpha}, \qquad \zeta_{sp} \approx -\frac{M_q + M_{\dot\alpha} + Z_\alpha / V}{2 \omega_{sp}} \tag{48}\]

with the lateral counterpart the Dutch roll,

\[\omega_{dr} \approx \sqrt{\frac{q S b \, C_{n\beta}}{I_z}} \tag{49}\]

whose frequency for the X-3 is low because $I_z$ is large, so the aircraft is slow to correct a yaw disturbance and quick to roll. That combination feeds the coupling. The horizontal tail must absorb the trim change, and its loads were measured and reported for this aircraft in Stephenson 1956. Subsonically the same aspect ratio is a severe penalty, since the lift-curve slope falls toward the slender-wing limit

\[C_{L\alpha} \to \frac{\pi A}{2} = 4.87 \ \text{per radian} \tag{50}\]

and induced drag rises as

\[C_{D,i} = \frac{C_L^2}{\pi A e} \tag{51}\]

with $A = 3.10$ giving an induced drag more than twice that of an aspect ratio seven wing at the same lift coefficient. A wing optimized for Mach 2 is a poor wing at Mach 0.3, and the takeoff and landing consequences below follow directly.

The supersonic drag of such a wing decomposes into three terms,

\[C_D = C_{D,f} + C_{D,w} + \frac{C_L^2}{\pi A e} \tag{52}\]

with friction, wave, and induced contributions. The Reynolds number that sets it is

\[Re_L = \frac{\rho_\infty V_\infty L}{\mu} \tag{53}\]

with the viscosity from Sutherland’s relation,

\[\mu = \mu_{\text{ref}} \left( \frac{T}{T_{\text{ref}}} \right)^{3/2} \frac{T_{\text{ref}} + S}{T + S} \tag{54}\]

taking $\mu_{\text{ref}} = 1.716 \times 10^{-5}$ pascal seconds at 273.15 kelvin and $S = 110.4$ kelvin. Friction follows the turbulent flat-plate relation referred to wetted area,

\[C_{D,f} = \frac{0.074}{Re_L^{1/5}} \cdot \frac{S_{\text{wet}}}{S} \tag{55}\]

and wave drag due to thickness for a thin two-dimensional section at zero lift follows the Ackeret form

\[C_{D,w} = \frac{4 \, \overline{(dy/dx)^2}}{\sqrt{M_\infty^2 - 1}} \tag{56}\]

where the overbar denotes a chordwise mean of the squared surface slope, which is proportional to $\tau^2$ and recovers the thickness-squared scaling quoted above. Wave drag due to lift adds

\[C_{D,w,L} = \frac{4 \alpha^2}{\sqrt{M_\infty^2 - 1}} = \frac{C_L^2 \sqrt{M_\infty^2 - 1}}{4} \tag{57}\]

which at Mach 2 and a cruise lift coefficient near 0.1 contributes only 0.004, so the X-3 at its design point would have been dominated by friction and thickness wave drag rather than by lift-dependent terms. This balance is the aerodynamic justification for the configuration, and it was never tested [Dinius 2014].

The structural consequence of thinness is severe. For a spar of structural depth $h_s$ proportional to thickness ratio, the cap area required to carry a root bending moment is

\[A_{\text{cap}} = \frac{M_{\text{root}}}{\sigma_{\text{allow}} h_s}, \qquad M_{\text{root}} = \frac{n W b}{3 \pi} \tag{58}\]

so halving the thickness ratio doubles the required cap area for the same moment, and the structural mass penalty is direct. Torsional stiffness suffers worse, since for a closed box the Bredt relation gives

\[K_\theta = \frac{G J}{\ell_w}, \qquad J = \frac{4 A_m^2}{\oint \frac{ds}{t}} \tag{59}\]

and the enclosed area $A_m$ scales with thickness, so $J$ scales as thickness squared. A wing half as thick has a quarter the torsional stiffness for the same skin gauge, which drives the aeroelastic boundaries down,

\[q_D = \frac{K_\theta}{e S C_{L\alpha}}, \qquad q_R = \frac{K_\theta \, C_{L\delta}}{S \bar{c} \, C_{L\alpha} \left| C_{m\delta} \right|} \tag{60}\]

for divergence and control reversal respectively. The thin wing is not merely harder to build. It is closer to every aeroelastic limit at once, and for that reason the surviving reports on this configuration are weighted heavily toward loads and flutter.

Titanium and the Manufacturing Problem

The X-3 is among the first aircraft to use titanium extensively in primary structure [Dinius 2014], and the difficulty was manufacturing rather than design, since Douglas had to develop pioneering procedures for machining, forming and cutting the metal [Boslaugh].

The material case is straightforward. Specific strength at temperature is the figure of merit,

\[\left. \frac{\sigma_{\text{allow}}(T)}{\rho_m} \right|_{T = T_w} \tag{61}\]

and a titanium alloy at about 4500 kilograms per cubic metre [Wikipedia, Ti-6Al-4V] withstands moderately high temperatures without creeping [Wikipedia, Titanium], whereas aluminium alloy at 2780 kilograms per cubic metre [Wikipedia, 2024 Aluminium] is limited to about 400 kelvin, the limit of 127 degrees Celsius that held the aluminium Concorde to Mach 2.02 [Wikipedia, Concorde]. At the recovery temperature the X-3 would have seen at Mach 2,

\[T_r = T_\infty \left( 1 + r \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{62}\]

with $r = 0.89$ and $T_\infty = 218.6$ kelvin, the surface reaches 374 kelvin, which aluminium survives. Titanium was therefore not required for the X-3’s own envelope. It was adopted to save weight, after the structure was found in July 1949 to be running unacceptably heavy [Boslaugh], and its large-scale use was itself one of the things the aircraft was built to test [Dinius 2014].

The manufacturing problem is that titanium galls against tooling, reacts with oxygen and nitrogen at elevated temperature [Wikipedia, Titanium], and has a springback that makes formed parts dimensionally unpredictable. Sheet forming is governed by the ratio of yield to modulus,

\[\frac{\sigma_y}{E} \tag{63}\]

which for Ti-6Al-4V, at a yield stress near 900 megapascals and a modulus near 110 gigapascals [Wikipedia, Ti-6Al-4V], is roughly twice the value for 2024 aluminium at about 270 megapascals and 73 gigapascals [Wikipedia, 2024 Aluminium]. The springback of a sheet bent to radius $R_i$ and released follows

\[\frac{R_i}{R_f} = 1 - 3 \frac{\sigma_y R_i}{E t_s} + 4 \left( \frac{\sigma_y R_i}{E t_s} \right)^3 \tag{64}\]

with $t_s$ the sheet thickness and $R_f$ the radius after release, so the recovery scales with the group $\sigma_y R_i / E t_s$ and doubling the yield-to-modulus ratio roughly doubles the correction required. It follows that elastic recovery after forming is roughly twice as large as for aluminium, and tooling must be overbent to compensate. The property data behind the material decision were being generated at the same time, and Barrett 1950 supplies compressive properties of titanium sheet at elevated temperature, the loading relevant to an upper wing surface and the condition relevant to a supersonic aircraft. Long-term exposure changes the properties again, and Ellis 2012 measures what sustained heating does to titanium elevated-temperature strength, a question of service life as distinct from strength. Later alloy and fabrication development runs through Kaneko et al. 1982 and Hinkley et al. 1999, with the composite alternatives that eventually displaced some of it described by Turner and Grande 1978. Contemporary work on the same problems appears in Saidi et al. 2021, Kim et al. 2022, and Shu et al. 2025, and its volume is a measure of how far from solved the problem remains. The later supersonic cruise programmes inherited the same difficulties, documented in Lunde 1977, Guess et al. 1981, Bales et al. 1990, and the joining problem in Scott 1972.

Propulsion and the Inlet

The turbojet cycle sets what the engines could deliver. Thermal and propulsive efficiency decompose as

\[\eta_{th} = 1 - \frac{1}{\pi_c^{\frac{\gamma - 1}{\gamma}}}, \qquad \eta_p = \frac{2}{1 + u_e / u_\infty}, \qquad \eta_0 = \eta_{th} \eta_p \tag{65}\]

with $\pi_c$ the compressor pressure ratio, and the afterburner raises thrust by adding heat downstream of the turbine at the cost of specific fuel consumption,

\[\frac{T_{AB}}{T_{\text{dry}}} \approx \sqrt{\frac{T_{07}}{T_{05}}} \tag{66}\]

with the subscripts denoting nozzle and turbine exit total temperatures. The J34 with afterburner produced roughly 4900 pounds against 3370 dry, a ratio near 1.45 consistent with that relation [Fischel et al. 1957]. The engine was characterized directly in an altitude chamber in Reller and Dowman 1949. That measurement concerns the actual powerplant this aircraft flew with, and it establishes that the altitude performance was known before the substitution, not discovered afterward. Afterburner behaviour at altitude was a sustained research subject in its own right, pursued for other engines of the period by Useller and Russey 1955 and Groesbeck and Peters 1958 and continuing much later through Johnsen and Cullom 1977 and Hanloser and Cullom 1979, with the nozzle and cooling arrangement that surrounds it characterized by Wallner and Jansen 1951. Installed performance degrades further from causes the test cell does not see, as Stromberg 1981 documents, and the eventual answer to the whole class of problem is to control engine and airframe together, which Burcham et al. 1995 takes up. Compressor behaviour away from the design point, the regime a fixed inlet forces, is examined by Biesiadny 1974, with the flow characteristics that govern it compared by Evans et al. 1974.

Separating thrust from drag in flight is itself a discipline, since only their difference is measurable from the trajectory,

\[T - D = m \frac{dV}{dt} + m g \sin \gamma \tag{67}\]

and assigning the two requires an independent thrust model. The bookkeeping conventions that make such an assignment reproducible are set out by Arnaiz 1975, and the consequence for the X-3 is that the published thrust shortfall and the inferred drag excess are not independently measured quantities but a single measured difference apportioned by assumption.

Installed thrust is a different quantity from uninstalled thrust, and the difference is the inlet. Ram compression is what makes a turbojet work at supersonic speed, since the total pressure available at the compressor face is

\[p_{02} = p_\infty \left( 1 + \frac{\gamma - 1}{2} M_\infty^2 \right)^{\frac{\gamma}{\gamma - 1}} \cdot \eta_d \tag{68}\]

with $\eta_d$ the inlet pressure recovery. A fixed normal-shock inlet has $\eta_d$ falling as derived above. The oblique shock relation makes the remedy quantitative. For a wedge of turn angle $\theta$ the shock angle $\beta_o$ satisfies

\[\tan \theta = 2 \cot \beta_o \frac{M_1^2 \sin^2 \beta_o - 1}{M_1^2 \left( \gamma + \cos 2 \beta_o \right) + 2} \tag{69}\]

and the normal Mach number ahead of the shock is $M_{1n} = M_1 \sin \beta_o$, so the total pressure loss is that of a normal shock at $M_{1n}$ rather than at $M_1$. Because the loss grows steeply with normal Mach number, splitting one strong shock into several weak ones recovers most of the total pressure. A two-shock system at Mach 2 recovers roughly 0.90 against 0.72 for a single normal shock, and a three-shock system approaches 0.95. Thrust scales with that recovery directly, so the difference between a fixed and a variable inlet at Mach 2 is roughly a quarter of the installed thrust. The remedy known at the time was a variable geometry inlet using oblique shocks, since a sequence of $n$ oblique shocks followed by a weak normal shock recovers far more total pressure than a single strong normal shock. The NACA was investigating this remedy while the X-3 was being built, through Ferri and Nucci 1946, Goelzer and Cortright 1951, Dryer and Beke 1952, Allen and Beke 1953, Beke and Allen 1953, and later with throat bleed by Mitchell and Campbell 1957 and active control by Anderson and Bowditch 1958. Side-inlet placement, the X-3 arrangement, was studied by Hasel et al. 1953. No source consulted here records that the X-3 received any of it. The problem did not go away, and improved compression surfaces are still being designed and flight tested, as Bulman et al. 1997, Fernandez et al. 2001, and St. John and Frederick 2013 show, the last of these confronting off-design behaviour, the failure mode of the X-3. Lee and Choi 2021 and Yang et al. 2024a treat the loss mechanism in modern terms, with off-design behaviour in Nikolaidis et al. 2022 and airframe integration in Su et al. 2025a.

Inertia Distribution and the Coupling Problem

This subsystem made the aircraft valuable. It follows directly from the configuration and is not an incidental property.

Mass in the X-3 is concentrated along a 20.35 metre fuselage. The wings are small, short, and carry little [Dinius 2014]. The moments of inertia that result are extremely asymmetric. Taking the mass properties tabulated by Day 1997, a weight of 21,900 pounds with moments of inertia of 4100, 61,200 and 65,100 slug square feet in roll, pitch and yaw, and converting,

\[I_x = 5.56 \times 10^{3}, \qquad I_y = 8.30 \times 10^{4}, \qquad I_z = 8.83 \times 10^{4} \ \text{kilogram square metres} \tag{70}\]

so that $I_z \approx I_x + I_y$ holds within one percent and the asymmetry ratio is

\[\frac{I_y}{I_x} = 14.9 \tag{71}\]

against 5.1 for the X-2 in the same tabulation. The X-3 is about three times more inertially asymmetric than the aircraft that inertia coupling destroyed.

The consequence follows from the analysis derived in the X-2 article. Divergence in a rolling manoeuvre occurs when the roll rate approaches the lower of the two aerodynamic natural frequencies,

\[\omega_\alpha = \sqrt{\frac{q S \bar{c} \left| C_{m\alpha} \right|}{I_y}}, \qquad \omega_\beta = \sqrt{\frac{q S b \, C_{n\beta}}{I_z}}, \qquad p_{\text{crit}} \approx \min \left( \omega_\alpha, \omega_\beta \right) \tag{72}\]

Evaluate at the condition of the first roll of October 1954, Mach 0.92 at 9144 metres [Day 1997], where the static pressure is 30,089 pascals and

\[q = \frac{\gamma}{2} p M^2 = 0.7 \times 30{,}089 \times 0.846 = 1.78 \times 10^{4} \ \text{pascals} \tag{73}\]

With representative stiffness coefficients of 0.3 and 0.1 per radian,

\[\omega_\alpha = 1.49 \ \text{radians per second}, \qquad \omega_\beta = 1.47 \ \text{radians per second} \tag{74}\] \[p_{\text{crit}} \approx 1.47 \ \text{radians per second} = 84 \ \text{degrees per second} \tag{75}\]

Eighty-four degrees per second is not an aggressive roll rate. It is a moderate one, well inside the peak roll rates the X-3 reached in flight test, and about a third of the 255 degrees per second that the same method gives for the X-2 at Mach 3.2. Fischel et al. 1957 found that those peak rates exceeded the calculated resonant frequencies and that the coupled regime was avoided only because the average rate over a full roll stayed low.

Roll damping is what would ordinarily limit the rate reached for a given input, and for a thin low aspect ratio wing it is weak. The steady roll rate from an aileron deflection is

\[p_{ss} = -\frac{C_{l \delta_a} \delta_a}{C_{l p}} \cdot \frac{2 V}{b} \tag{76}\]

and the damping derivative $C_{lp}$ for such a planform at supersonic speed had been calculated and measured extensively in the period immediately before the X-3 flew, in Brown and Adams 1948a, Tucker and Piland 1950, Malvestuto et al. 1950, Walker and Ballantyne 1950, and Ribner 1951, with rolling effectiveness measured in free flight in Sandahl 1948. For a thin wing at supersonic speed the damping derivative itself carries the Prandtl-Glauert falloff,

\[C_{lp} \approx -\frac{\pi A}{8 \sqrt{M_\infty^2 - 1}} \quad \text{for } \beta_s A \gtrsim 4 \tag{77}\]

so it weakens with Mach number exactly as the stiffness derivatives do. The roll mode time constant that results is

\[\tau_r = -\frac{2 I_x V}{q S b^2 C_{lp}} \tag{78}\]

and the small $I_x$ that defines the X-3’s inertia distribution makes that time constant short. The aircraft therefore reaches its steady roll rate quickly, which leaves the pilot even less time between input and threshold. The approach to steady state is first order,

\[p(t) = p_{ss} \left( 1 - e^{-t / \tau_r} \right) \tag{79}\]

so the critical rate is crossed at

\[t_{\text{crit}} = -\tau_r \ln \left( 1 - \frac{p_{\text{crit}}}{p_{ss}} \right) \tag{80}\]

A small span appears twice in the steady-rate expression, once directly and once through the damping, so the X-3 reaches a high roll rate for a modest input and has little to arrest it.

The loads a rolling manoeuvre imposes were also understood, and Pearson and Aiken 1946 analyses wing and aileron loads in rolling pull-outs, the manoeuvre class that produced the departure. The analytical and experimental groundwork for predicting what happened to the X-3 was therefore substantially complete before the aircraft flew, with the supporting flight measurement technique established by Talmage and Reeder 1947 and further damping data supplied by Brown and Adams 1948b. What was missing was its application to this configuration.

The phenomenon did not stop with the X-3. Uncommanded lateral-directional motions at transonic conditions recurred across the fleet for decades, and Chambers and Hall 2003 reviews that history directly. The review places the X-3 events in their full sequence and does not treat them as an isolated incident. Reynolds number proves to matter for the derivatives involved, as Owens et al. 2002 shows for a supersonic transport, and control-surface effectiveness on the low aspect ratio planforms that provoke the problem is characterized by Bennett 2000.

The growth rate past the threshold follows as before,

\[\lambda = \sqrt{p^2 - \omega_\alpha^2}, \qquad \tau_{\text{div}} = \frac{1}{\lambda} \tag{81}\]

so a roll at 2.5 radians per second, or 143 degrees per second, gives $\lambda = 2.00$ per second and an e-folding time of 0.50 seconds. The X-3 thus diverges more readily than the X-2 but somewhat more slowly once it does, because its aerodynamic frequencies and its achievable roll rates are both lower. The coupled equations themselves are those derived for the X-2,

\[I_y \dot{q} = M + \left( I_z - I_x \right) p r, \qquad I_z \dot{r} = N + \left( I_x - I_y \right) p q \tag{82}\]

and linearizing about a steady roll rate gives the pair

\[\ddot{\alpha} + \left( \omega_\alpha^2 - p^2 \right) \alpha = \left( \frac{I_z - I_x}{I_y} \right) p \, \dot{\beta} \tag{83}\] \[\ddot{\beta} + \left( \omega_\beta^2 - p^2 \right) \beta = \left( \frac{I_x - I_y}{I_z} \right) p \, \dot{\alpha} \tag{84}\]

in which the effective stiffness in each axis is reduced by $p^2$. The inertia ratios multiplying the cross terms,

\[\mu_1 = \frac{I_z - I_x}{I_y} = 1.00, \qquad \mu_2 = \frac{I_x - I_y}{I_z} = -0.88 \tag{85}\]

are both near unity in magnitude for this configuration. Unity is the maximum the geometry permits, and the values confirm that the X-3 sits at the worst corner of the coupling problem and does not merely fall inside it.

The excursions that follow produce loads. An angle of attack increment $\Delta \alpha$ gives a normal load factor increment

\[\Delta n = \frac{q S C_{L\alpha} \Delta \alpha}{W} \tag{86}\]

and at the flight condition with $q = 1.78 \times 10^{4}$ pascals, a lift-curve slope near 3.5 per radian subsonically, and a weight of 97.4 kilonewtons, a twenty degree excursion gives $\Delta n = 3.5$. Sideslip produces a lateral increment through $C_{Y\beta}$ of comparable size. Those are survivable numbers, unlike the X-2 figures, because of the lower dynamic pressure at which the X-3 met the phenomenon. The margin was narrow. In the second roll, at higher dynamic pressure, the normal load factor swung from $-6.7$ to $+7.0$ and the design acceleration loads were reached [Day 1997] [Saltzman and Ayers 1995].

Takeoff, Landing, and the Cost of the Wing

Unlike the X-1 and X-2, the X-3 took off under its own power [Jenkins et al. 2003], and its wing made that difficult.

The takeoff speed follows from the wing loading and the maximum lift coefficient,

\[V_{TO} = \sqrt{\frac{2 W}{\rho S C_{L,\max}}} \tag{87}\]

and with a thin low aspect ratio wing carrying only plain leading-edge flaps and split trailing-edge flaps [Fischel et al. 1957], $C_{L,\max}$ near 0.9 is optimistic. At sea level this gives

\[V_{TO} = \sqrt{\frac{2 \times 99{,}646}{1.225 \times 15.47 \times 0.9}} = 108 \ \text{metres per second} \tag{88}\]

or 242 miles per hour, close to the takeoff speed of 260 miles per hour recorded for the aircraft [Jenkins et al. 2003]. The ground roll follows from the available acceleration,

\[s_{TO} = \frac{V_{TO}^2}{2 a}, \qquad a \approx \frac{T - D - \mu \left( W - L \right)}{m} \tag{89}\]

with $\mu$ the rolling friction coefficient. Retaining the drag and friction terms gives the more honest form

\[s_{TO} = \int_0^{V_{TO}} \frac{m V \, dV}{T - \frac{1}{2} \rho V^2 S \left( C_D - \mu C_L \right) - \mu m g} \tag{90}\]

and taking the thrust-dominated approximation $a \approx T/m = 4.29$ metres per second squared gives 1362 metres before rotation, with the real figure substantially longer. The lift-off condition is a balance,

\[\frac{1}{2} \rho V_{TO}^2 S C_{L,TO} = W \tag{91}\]

and a wing that cannot generate a high $C_{L,TO}$ forces $V_{TO}$ up as the square root, which is why the aircraft that most needs a short field is the one least able to have one. The climb gradient immediately after lift-off follows the same thrust margin,

\[\sin \gamma_{\text{climb}} = \frac{T}{W} - \frac{1}{L / D} \tag{92}\]

and with a thrust-to-weight of 0.44 and a subsonic lift-to-drag near 8 at climb lift coefficient, the available gradient is

\[0.44 - 0.125 = 0.315 \tag{93}\]

which is healthy, so the X-3 climbed acceptably once airborne. Its difficulty was reaching flying speed, not leaving the ground. The aircraft needed the lake bed not for safety but for length.

Landing inherits the same penalty. The recorded landing speed of 200 miles per hour, or 89 metres per second [Jenkins et al. 2003], lies below the clean stall speed derived above, which points to a lighter landing weight and deflected flaps, but it is still high, and the landing gear absorbs correspondingly higher energy,

\[E_{\text{gear}} = \frac{1}{2} m w_s^2 \tag{94}\]

with $w_s$ the sink rate. The landing distance from the same relations is

\[s_L = \frac{V_{TD}^2}{2 \bar{a}_{\text{brake}}} \tag{95}\]

and the energy the brakes must absorb scales as the square of touchdown speed, so an aircraft landing at 89 metres per second dissipates roughly twice the energy of one landing at 63. Stated directly, the brake energy is

\[E_{\text{brake}} = \frac{1}{2} m V_{TD}^2 - \int_0^{s_L} D \, ds \tag{96}\]

and the tire has an independent limit, since its structural speed rating is a ground speed rather than an airspeed,

\[V_{\text{ground}} = V_{TD} - V_{\text{wind}} \le V_{\text{tire}} \tag{97}\]

and the X-3 pressed that limit hard enough that it was common for its tires to come apart [Jenkins et al. 2003]. The gear stroke required to hold the load factor at touchdown to a chosen value $n_g$ is

\[s_{\text{stroke}} = \frac{w_s^2}{2 g \left( n_g - 1 \right)} \tag{98}\]

so a three metre per second sink at a two g limit needs 0.46 metres of stroke, and every increment of sink rate costs stroke quadratically. The oleo strut that provides that stroke is a velocity-dependent damper, and its behaviour under impact depends on orifice sizing and fluid properties, characterized in drop testing as in Kranz 1954. Active control of the same load path became possible much later, as McGehee and Carden 1976 and Howell et al. 1990 describe. High-lift devices more powerful than the plain and split flaps the X-3 carried, which would have relieved the takeoff and landing problem at its source, are surveyed by Rudolph 1996. The loads that result were measured and reported in Marcy 1958.

Instrumentation

The X-3 carried a conventional NACA installation of the period, and the measurements that matter for this article are the loads and the rates [Fischel et al. 1957].

Structural loads came from calibrated strain gauge bridges, whose calibration on a thin low aspect ratio wing is a documented difficulty in Peele and Eckstrom 1975. External strain-gauge installation, used where an internal fit is impossible on a thin structure, is described by Eckstrom 1976. The lifting pressure distributions that such a wing produces were measured in flight much later in Byrdsong 1977 and compared against tunnel and computation in Lawing et al. 1991.

Angle of attack and sideslip on a research aircraft come from a nose boom carrying vanes, whose indicated values require correction for the aircraft’s rotation,

\[\alpha_{\text{true}} = \alpha_{\text{vane}} - \frac{\ell_b \, q}{V}, \qquad \beta_{\text{true}} = \beta_{\text{vane}} + \frac{\ell_b \, r}{V} \tag{99}\]

with $\ell_b$ the boom length ahead of the centre of gravity. During a coupled departure $q$ and $r$ are large, so the correction is large, and an uncorrected record overstates the excursions. That correction is why the rate gyros matter as much as the vanes. Rate measurement is what the coupling investigation depended on, and the requirement is severe. Uncertainty in any derived quantity propagates as

\[u_c^2(y) = \sum_i \left( \frac{\partial y}{\partial x_i} \right)^2 u^2(x_i) \tag{100}\]

and resolving a divergence with an e-folding time near 0.5 seconds requires a sample rate satisfying

\[f_s > 2 f_{\max} \tag{101}\]

with practical rates several times higher, giving a recorded bit budget of

\[B = N_c f_s b \tag{102}\]

for $N_c$ channels of $b$ bits, and the amplitude resolution follows from the converter word length,

\[\Delta = \frac{FS}{2^b}, \qquad \sigma_q = \frac{\Delta}{\sqrt{12}} \tag{103}\]

with $FS$ the full-scale range. A rate gyro recorded to eight bits over a range of two radians per second resolves 0.008 radians per second, which is adequate for the rates of a departure and marginal for the small perturbations that precede one. Moments of inertia, which the analysis above depends on entirely, are not measured in flight at all. They are established by ground swing tests or by mass accounting, the values used for the X-3 being the manufacturer’s estimates [Fischel et al. 1957], and their uncertainty propagates directly into any coupling prediction through

\[\frac{u(p_{\text{crit}})}{p_{\text{crit}}} = \frac{1}{2} \frac{u(I)}{I} \tag{104}\]

so a ten percent inertia error gives a five percent error in the predicted threshold. The swing test that establishes inertia measures a pendulum period,

\[T_{\text{swing}} = 2 \pi \sqrt{\frac{I_p}{m g \ell_p}}, \qquad I = I_p - m \ell_p^2 \tag{105}\]

with $\ell_p$ the distance from pivot to centre of gravity, so the inertia is a difference of two comparable quantities and the uncertainty amplification familiar from drag measurement reappears,

\[\frac{u(I)}{I} \approx \frac{I_p}{I} \sqrt{ \left( 2 \frac{u(T_{\text{swing}})}{T_{\text{swing}}} \right)^2 + \left( \frac{u(\ell_p)}{\ell_p} \right)^2 } \tag{106}\]

Differencing is the recurring structural feature of flight-test measurement and it appears here in the one quantity the coupling analysis cannot do without. Dehghan Manshadi and Saghafi 2021 and Mwenegoha et al. 2019 take up the estimation problem with current methods. The swing test has since been superseded by a dynamic method that excites the structure and infers the inertia tensor from the measured response, validated in Chin et al. 2015, which removes the differencing amplification described above by measuring the quantity directly rather than as a residual. Air data calibration has undergone the same modernization, with a satellite-referenced method replacing the tower fly-by in Martos et al. 2011.

The Flight Test Record

The aircraft first flew on 20 October 1952 with Douglas pilot Bill Bridgeman at the controls, having made an inadvertent short hop during a high-speed taxi test five days earlier [Dinius 2014]. It flew 51 times in total across Douglas, Air Force, and NACA phases [Jenkins et al. 2003].

The dive can be quantified. In a descent at flight path angle $\gamma$ the gravity component supplies

\[\Delta T_{\text{effective}} = W \sin \gamma \tag{107}\]

so a thirty degree dive at a weight of 99.6 kilonewtons adds 49.8 kilonewtons, which slightly exceeds the entire installed thrust of 43.6 kilonewtons. Gravity was the larger engine. Its maximum speed was Mach 1.208, achieved on 28 July 1953 in a dive [Dinius 2014]. It never exceeded Mach 1 in level flight [Day 1997]. Contractor demonstration results are reported in Day and Fischel 1955, horizontal tail loads in Stephenson 1956, buffet and maximum normal force in Baker et al. 1957, and landing loads in Marcy 1958.

The flight that matters took place on 27 October 1954. NACA pilot Joe Walker performed an abrupt left roll at Mach 0.92 and about 9100 metres. The aircraft departed immediately into a violent coupled motion in all three axes, pitching up 20 degrees and yawing 16 degrees and gyrating for five seconds before Walker recovered [Dinius 2014]. He repeated the manoeuvre later in the same flight, at Mach 1.05 in the account of Day 1997 and at Mach 1.154 in that of Dinius 2014, and the response was worse. The aircraft was not lost and Walker was not injured, which distinguishes this event from the X-2 accident two years later and is the reason the X-3 data set exists at all.

The transonic handling qualities investigation that resulted is Fischel et al. 1957, and it is the single most cited document the programme produced. An aircraft built to study thin wings at Mach 2 is remembered for what it did at Mach 0.92 with the wing incidental.

The programme can be scored on the information accounting used throughout this series. With a prior uncertainty $\sigma_0$, a per-flight uncertainty $\sigma_m$, and a target $\sigma_T$,

\[n^{*} = \left\lceil \sigma_m^2 \left( \frac{1}{\sigma_T^2} - \frac{1}{\sigma_0^2} \right) \right\rceil, \qquad I_n = \frac{1}{2} \ln \frac{\sigma_0^2}{\sigma_n^2} \tag{108}\]

following Lindley 1956 and Chaloner and Verdinelli 1995. Fifty-one flights is a large campaign by the standards of this series, comparable to the X-1 and far exceeding the X-2. The single airframe is the anomaly. The attrition condition

\[\sum_{i=0}^{n_a - 1} \binom{n}{i} p^i (1-p)^{n-i} \ge 1 - \alpha \tag{109}\]

at fifty-one flights and even a one percent per-flight loss probability returns three airframes for ninety-five percent confidence, and the X-3 flew with one. That it survived is fortunate rather than planned, and the coupling data exist because of that fortune.

The X-3 was retired in 1956 after 51 flights and is preserved at the National Museum of the United States Air Force [Dinius 2014] [Wikipedia, Douglas X-3].

Comparison With Ground Prediction

The X-3 offers an unusually clean test of ground prediction because the coupling behaviour was, in this case, partly anticipated [Saltzman and Ayers 1995].

A dynamically scaled model of the aircraft had been tested in the Langley free-spinning tunnel, reported in Hultz 1951, three years before the flight events. A spin tunnel model is ballasted to represent the full-scale inertia distribution, so unlike the static force models discussed in the X-2 article it does satisfy the mass and inertia similarity groups,

\[\mu_m = \frac{m}{\rho S b}, \qquad \hat{I}_x = \frac{I_x}{\rho S b^3}, \qquad \hat{I}_y = \frac{I_y}{\rho S \bar{c}^3} \tag{110}\]

The instrument capable of finding the problem was therefore applied to this aircraft, which is the opposite of the X-2 situation. Dynamic similarity additionally requires the reduced frequency to match,

\[k = \frac{\omega b}{2 V} \tag{111}\]

so that the ratio of motion timescale to flow timescale is preserved. Scaling the inertias to a model of geometric ratio $1/k_g$ requires

\[I_m = \frac{I_f}{k_g^5} \cdot \frac{\rho_m}{\rho_f} \tag{112}\]

whose fifth-power dependence makes ballasting exacting but not impossible. What a spin tunnel investigates, however, is developed spin and recovery rather than the entry into a coupled divergence from a rolling manoeuvre at high speed, so the test asked a different question of the right model.

The theoretical prediction existed as well. Phillips 1948 had published the analysis six years before Walker’s flights, and the programme history in Day 1997 traces how slowly that prediction propagated into practice. The gap here was not instrumental and not theoretical. It was that nobody connected an available analysis and an available facility to a specific aircraft until an aircraft did it for them.

The comparison between tunnel and flight for stability and control had been studied as a methodological question in Kayten and Koven 1945, and rocket-boosted free-flight models supplied an independent route to low-lift drag and directional stability, reported for a Douglas configuration by Mitcham et al. 1952. Low-speed lateral characteristics of comparable models come from Sleeman and Morrison 1953. Low aspect ratio and thin wing behaviour had been characterized in Ribner 1947, Walker and Berggren 1948, and Margolis 1947, with flow characteristics measured later by Taillon 1959 and thickness effects on zero-lift drag quantified by Shrout 1965. Planform details that matter at these thicknesses, such as trailing-edge truncation, were quantified by Bartlett and Harris 1974, and the interference at wing-body junctions that a thin wing on a large fuselage aggravates in Milholen and Chokani 1992. The eventual answer to transonic wing design, which the X-3 predates entirely, is the supercritical section, flight-measured in Pyle and Steers 1975 and Montoya and Banner 1977. The contemporary fighter against which the X-3 configuration should be judged is characterized by Blanchard 1953, and an all-wing alternative that took the low aspect ratio argument further appears as Brewer 1946. The comparative summary of research airplane lift and drag in Bellman 1959 places the X-3 alongside its contemporaries.

What the Data Changed

Three consequences are traceable and they are unequal in importance.

The coupling data are the first. Walker’s flight produced an instrumented record of an inertia-coupled departure and a recovery from one, in an aircraft that survived to fly again [Dinius 2014]. The F-100A supplied the only comparable record of 1954, and the NACA reported the two together [Day 1997]. The X-3 record arrived while the F-100 fleet was experiencing the same phenomenon in service and two years before it killed Mel Apt in the X-2, and it fed directly into the operating restrictions, the artificial damping requirements, and the vertical tail sizing described in the previous article. The historical account in Day 1997 treats the X-3 as a principal source. The wider stability and control envelope across the supersonic and hypersonic range is surveyed in Compton et al. 1983, transonic stability characteristics continued to be flight-evaluated, as Matheny and Gatlin 1978 records, and the departure and spin research that grew out of the same concerns is summarized by Patton et al. 1979. The research aircraft that inherited the resulting understanding include the F-15 programme summarized by Burcham et al. 1986 and the oblique-wing vehicles whose deliberate asymmetry makes coupling a design variable rather than a hazard, explored by Alag et al. 1986b and Kempel et al. 1988b.

The information the flights returned can be quantified against what a purpose-built campaign would have needed. Two departures at two Mach numbers is a sample of two, so the posterior uncertainty in any coupling parameter after those flights is

\[\sigma_n = \frac{\sigma_m}{\sqrt{n}} = \frac{\sigma_m}{\sqrt{2}} \tag{113}\]

against a prior that was effectively unbounded because no instrumented departure existed. The information gain from the first such record is therefore very large and the second adds a factor of $\sqrt{2}$. That asymmetry is the mathematical statement of why an unplanned event in a surviving aircraft was worth more than a planned campaign in an aircraft that could not have survived it.

The wing is the second. The thin low aspect ratio planform the X-3 demonstrated was used on the Lockheed F-104 Starfighter [Dinius 2014], which first flew in 1954 and became the first combat aircraft capable of sustained Mach 2 flight [Wikipedia, F-104]. The X-3 also contributed to tire technology, since its very high takeoff and landing speeds required better tires and several tire manufacturers used its data [Jenkins et al. 2003]. The scale of that inheritance can be put in terms of the wing loading and touchdown energy relations derived above, since the F-104 carried a comparable wing loading [Wikipedia, F-104] and therefore a comparable

\[E_{\text{gear}} = \frac{1}{2} m w_s^2, \qquad V_{TD} \propto \sqrt{\frac{W/S}{C_{L,\max}}} \tag{114}\]

and tire data gathered against those numbers is a substantial transfer. An aircraft that failed to reach its design speed nonetheless supplied a wing planform to the aircraft that did, and tire data to the aircraft that followed.

The supersonic cruise programmes that followed inherited both the structural and the propulsion problems, as Kirkham et al. 1975 and Arnaiz 1977 record for the large flexible high-speed aircraft that the X-3 configuration anticipated at small scale, with the structural design problem taken up by Hoy 1976 and the successor research vehicle studies by Combs 1977. Propulsion integration at the extreme end of the same lineage occupies Andrews and Mackley 1976. The titanium experience is the third and is the hardest to trace. The manufacturing lessons were real, since Douglas developed pioneering procedures for machining, forming and cutting titanium [Boslaugh], but the sources consulted here record no published account of them. The X-3 is better described as an early datum than as a cause.

A fourth consequence is a negative one. The X-3 illustrated that an inlet without variable geometry is a severe handicap on a supersonic aircraft intended to hold a condition, and demonstrated that engine and airframe cannot be procured on independent schedules. Both lessons were available in principle beforehand. The programme made them expensive enough to be learned.

The Contemporary Literature

Cluster	Records
Titanium and the manufacture of the airframe	702
The thin, low aspect ratio wing at supersonic speed	695
Supersonic inlets, pressure recovery and unstart	599
Aeroelasticity, flutter and divergence	492
Roll damping, lateral-directional stability and handling qualities	484
Flight test measurement, system identification and mass properties	460
Turbojets, afterburning and installed thrust	337
Inertia coupling, departure and loss of control	337
Takeoff, landing and the landing gear	339
Compressible flow, heating and the boundary layer	296
Flight loads, buffet and structural response	175
Research airplane programmes and their record	145
Wind tunnels, models and the prediction of flight	145
Aircraft performance, flight mechanics and design method	113
Wings, airfoils and low-speed aerodynamics	46
Information, experimental design and cost	6
Total	5,371

The threads the X-3 opened are live, and two of them have become substantially better understood.

Inlet performance is now a design discipline rather than a compromise. Total pressure loss mechanisms are analysed directly in Lee and Choi 2021 and Yang et al. 2024a, with off-design behaviour in Nikolaidis et al. 2022 and the shock structures that govern it in Wang et al. 2023b. Airframe and propulsion integration is treated as a single problem in Su et al. 2025a and Fu et al. 2024, and turbojet performance in subsonic flight is modelled in Derbel and Beneda 2025.

Low aspect ratio and thin wing behaviour continues to be studied, with dynamic characteristics in Zeng et al. 2022, transonic static aeroelastic behaviour in Wang 2019, and thermal wall effects in Lin et al. 2021. The transonic flutter boundary that a thin wing approaches so closely is measured, with the shock movement that accompanies it, in Stubblefield et al. 2025.

Coupled rotational dynamics has become a nonlinear dynamical systems subject, with the coupling ratio itself parameterized in Shen et al. 2019b, chaotic regimes in Xu et al. 2019b, departure and spin prediction in Tu et al. 2024, and bifurcation analysis in Nguyen et al. 2021. Prevention is a control problem in Altunkaya et al. 2025 and Moreira et al. 2022, and the institutional continuation is the loss of control research programme documented in Belcastro 2014 and Belcastro et al. 2014.

The inlet is where the contemporary literature has moved furthest, and it has moved onto the same failure the X-3 suffered. Unstart, the violent expulsion of the terminal shock that follows from operating outside the swallowing condition, is now studied as a controllable boundary rather than an accident. Chen et al. 2019a present an external-compression design intended to be free of it, Jin et al. 2023b broaden the unstart and restart boundary deliberately, Wang et al. 2023e characterize the effect of backpressure on both, and Jin et al. 2023a measure the hysteresis between them. Because of that hysteresis, recovering from an unstart is harder than avoiding one. Multi-objective optimization of the whole inlet appears in Wang et al. 2023g, separation control on the swept interaction in Kim and Park 2026, bleed plenum design in Türkkahraman et al. 2024, and oscillation suppression in Luo et al. 2020. Configuration-level computation is treated by Ezzeldin and Wu 2025.

The accounting problem the X-3 exposed has also been formalized. Thrust and drag cannot be separated by measurement alone, and Goulos et al. 2021 set out the bookkeeping conventions that make an installed-performance claim reproducible. Those conventions now answer the question this article had to leave open about where the X-3’s missing performance went. Propulsion and airframe are now designed together as in Li and Geiselhart 2024 and Hutchinson et al. 2021, with supersonic transport configuration optimization in Habibniarami et al. 2026.

Coupled rotational motion is now something to be suppressed by control rather than avoided by limitation. The X-3 lacked that capability entirely, and for this reason its critical roll rate was a hard boundary, not a soft one. Parameter identification, which is how a modern programme would have found that boundary before flying into it, is treated by Metodiev 2024, Wang et al. 2022a, and Singh and Ghosh 2023.

Thin and slender wing aeroelasticity has become computable. Miyaji and Takegawa 2022 predict transonic wing flutter directly, Yuan et al. 2024 apply resolvent analysis to the flutter boundary, and high aspect ratio cases are treated by Yang and Li 2022 and Ghalandari et al. 2022. The X-3’s designers had none of this and sized against margins instead.

Titanium forming remains difficult enough to sustain an active literature, and the springback that this article derives is now predicted rather than compensated by trial, as Pham et al. 2019 and Wu et al. 2020 show, with machine learning applied to dimensional accuracy by Huang et al. 2024. The forming problems themselves persist, and Saidi et al. 2021, Kim et al. 2022, and Shu et al. 2025 report them. Mass properties estimation, which the coupling analysis depends on, is treated in Dehghan Manshadi and Saghafi 2021 and Mwenegoha et al. 2019. Machine learning has entered the modelling of all of it, as Brunton et al. 2020 survey, and dynamically scaled flight testing continues as described in Kong et al. 2023.

Titanium and the manufacture of the airframe

The second half of the keystone. Titanium alloys, their elevated-temperature properties, forming, machining, joining and the fabrication of titanium airframe structure. Of the 274 titles in the survey that name springback, 13 also name titanium, so the literature that predicts the springback this article derives treats sheet metal in general far more often than titanium, and it is kept because the relation is the same.

702 records. [IOM3 2024] [Abele and Hölscher 2013] [Abu-Farha and Curtis 2011] [Adzman and Zakaria 2014] [Aircraft Construction 2008] [Akula et al. 2023] [Albertson et al. 1997] [Alimov et al. 2019] [Allazadeh and Zuelli 2017] [Anggono et al. 2011] [Ankėnas and Barauskas 2006] [Ao et al. 2018] [Appiah 2004] [Applications of Titanium 2005] [Arcella and Froes 2000] [Arcella et al. 2000] [arfa and Hassine 2023] [Artificial Neural Networks Model 2020] [Arvin et al. 1981] [Astarita et al. 2014] [Balckburn 1987] [Bales and Cain 1971] [Bambach et al. 2020] [Banerjee et al. 2022] [Barrau et al. 2016] [Batista dos Santos] [Batista Ponce et al. 2019] [Baucom 1969] [Beal et al. 2006] [Beck 1966] [Beck 2003] [Belhassen et al. 2016] [Ben Said et al. 2025] [Bernhart et al. 2011] [Berryman et al. 1976] [Berryman et al. 1977] [Bertram et al. 2007] [Bharathi et al. 2021] [Bhatt 1985] [Bhatt et al. 1990] [Billah and Acar 2026] [Bosetti and Bruschi 2011] [Bottomley 1995] [Bouhamed et al. 2026] [Boyer and Finden 1972] [Braski and Royster 1966] [Braski and Royster 1967] [Briesenick et al. 2021] [Brindley et al. 2005] [Brown and Shannon 1963] [Brown et al. 1961a] [Bruschi and Ghiotti 2018] [Bui] [Burchitz] [Burkhart and Hefti 2020] [Bylya et al. 2016] [Byrer and Boulger 1970] [Băilă and Tonoiu 2019] [Calamaz et al. 2010] [Campbell 1991] [Cardoso et al. 2026] [Carrino et al. 2012] [Carter 1960] [Carter 1970] [Chalal et al. 2012a] [Chalal et al. 2012b] [Chandra 1987] [Chandrappa et al. 2020] [Chang 1970] [Chang 1984] [Chang 2007] [Chang 2024] [Charit and Mishra 2007] [Chen 2005] [Chen 2010] [Chen 2011b] [Chen 2011a] [Chen and Ko 2011] [Chen and Wang 2008] [Chen et al. 2006b] [Chen et al. 2010] [Chen et al. 2019b] [Chen et al. 2021b] [Chen et al. 2022] [Chen et al. 2025b] [Chirita and Brabie 2007] [Chongthairungruang et al. 2013] [Christiana 1963] [Chun et al. 2001] [Churi et al. 2006] [Comley 2007] [Cotton et al. 2015] [Cox and Erbin 1965] [Craddock 1973] [Crossley and Barice 1983] [D’Acquisto and Fratini 2000] [D’Urso et al. 2007] [Dan and Zhang 2012] [Dang et al. 2017] [Davis et al. 1987] [Davis et al. 1990] [de Souza and Rolfe 2010] [Del Prete et al. 2007] [Delannay 2004] [Demeri et al. 2000] [Deng et al. 2014] [Deng et al. 2017] [Deokar et al. 2019] [Han 2008] [DeSisto 1973] [Dilan et al. 2016] [Dilan et al. 2017] [Ding et al. 2023] [Ding et al. 2025] [Ding et al. 2026] [Dobson and Whiffen 1984] [Dodds and Davies 1954] [DongGyu et al. 2025] [Du et al. 1994] [Du et al. 2022] [Du et al. 2024] [Duncan and Hubbard 1973] [君 2024] [Díaz et al. 2021] [Edwards and Dickason 1966] [El-Megharbel et al. 1990] [Elsayed et al. 2017] [Erbin 1963] [Estman et al. 2013] [Lee 2004] [Experimental Study of Diffusion 2018] [Kim 2007] [Fabrication and Properties 2003] [Fan et al. 2018] [Fan et al. 2023] [Fann et al. 2025] [Fanta et al. 2000] [Feng et al. 2023] [Feng et al. 2025] [Filice et al. 2009] [Firat et al. 2008] [Fisher and Vollmer 1970] [Fitzpatrick et al. 1964] [Forming of Titanium Plate 2015] [Fretting Fatigue Strength 1958] [Friedman and Luckey 2011] [Frisby 1960] [Fu 2010] [Fu 2011] [Fu 2023] [Fu and Liu 2011] [Fu and Mo 2010] [Fu et al. 2009] [Fu et al. 2016] [Fu et al. 2022] [Fukuoka et al. 2014] [Functional-Purpose Titanium Alloys 2005] [Gao et al. 2025] [García-Barrachina and Gámez 2021] [Gardner and Royster 1970] [Garrett 1956] [Gau and Kinzel 2005] [Gau et al. 2006] [Gau et al. 2007] [Gershon and Eldror 2005] [Ghosh and Hamilton 1986] [Gibson 1932] [Gillig and Guarnieri 1956] [Giraudet et al. 2016] [Girton et al. 1956] [Gisario et al. 2011] [Gisario et al. 2016] [Giuliano 2011] [Gong et al. 2021] [Gould and Stotler 1991] [Gray 1969] [Grimm et al. 2016] [Grinberg et al. 1971] [Groche and Bäcker 2013] [Groneck and Harmon 2001] [Gu et al. 2017a] [Guo 2005] [Guo and Tang 2017] [Guo et al. 2002] [Gupta et al. 2020] [Göttmann et al. 2011] [Halilovič et al. 2007] [Hama et al. 2010] [Hama et al. 2017] [Hama et al. 2018] [Hamilton and Paton 1988] [Han et al. 2010b] [Han et al. 2010a] [Han et al. 2011] [Han et al. 2012] [Han et al. 2017] [Han et al. 2018] [Han et al. 2024] [Hardrath and Heimerl 1965] [Hardy 1996] [Hardy 1998] [Harmon et al. 1996] [Harper et al. 2026] [Hartmann et al. 2021] [Hatipoğlu and Alkaş 2016] [Hayashi 1996] [Hefti 2010a] [Hefti 2010c] [Hefti 2010b] [Hefti 2012] [Hegazy and Mote 1985] [Heimerl et al. 1956] [High-Temperature Titanium Alloys 2005] [Hino et al. 2003] [Hoffmann et al. 1982] [Hoffmann et al. 1989] [Hong and Zhang 2023] [Hower et al. 1956] [Hu et al. 2021] [Hu et al. 2024] [Huang et al. 2024] [Hussain and Gao 2006] [Ibrahim 2026] [Illg and Imig 1969] [Illg and Imig 1971] [Imig 1967] [Islam et al. 2015] [Iwata et al. 2007] [Jackson 2011] [Jackson and Gordon 1957] [Jain Sudhir et al. 2021] [Jarosław et al. 2026] [Jenkins 1984] [Jia et al. 2013] [Jiang 2023] [Jiang 2026] [Jiang et al. 2000b] [Jin and Lu 2010] [Jone et al. 1961] [Ju Min and Lee 2015] [Jukes 1970] [Kadkhodayan 2004] [Kadkhodayan and Zafarparandeh 2008] [Kaganovich et al. 1982] [Kan and Hailing 2011] [Kaneko and Woods 1983] [Karafillis and Boyce 1992] [Karafillis and Boyce 1996] [Kazan et al. 2009] [Kenger and Leavy 1955] [Keys et al. 1965] [Khademi et al. 2019] [Khan 2006] [Khanna and Agrawal 2019] [Khanna and Davim 2015] [Khleif et al. 2020] [Khudadad et al. 2025] [Kim and Kang 2011] [Kim and Kim 2018] [Kim and Koç 2008] [Kim et al. 2022] [Kim et al. 2025] [King 1962] [Kishawy and Hosseini 2018] [Kobryn 1996] [Kolom 1969] [Kondetimmanahalli] [Koppenhofer et al. 1961] [Korner and Ou 2025] [Krasovskyy et al. 2006] [Kremer et al. 1973] [Kukuryk 2025] [Kumar et al. 2008] [Kumar et al. 2021] [Kumar Sharma et al. 2022] [Kut et al. 2021] [Kędzierski and Popławski 2019] [Lal et al. 2016] [Lal et al. 2018] [Lan et al. 2006b] [Lange et al. 2024] [Lavrinenko and Ринатович 2019] [Lawanwomg et al. 2014] [Lawanwong et al. 2019] [Lazoglu et al. 2014] [Leach and McDonough 1978] [Leacock et al. 2015] [Lebon et al. 2013a] [Lebon et al. 2013b] [Lee 2017] [Lee and Kim 2012] [Lee and Yang 1998] [Lee et al. 2014] [Lee et al. 2019] [Leen 2011] [Leen and Stoyanov 2009] [Leen et al. 2008] [Leen et al. 2010] [Lenning and Heil 1973] [Lerch and Arnold 2014] [Lesuer 2001] [Li 2023e] [Li 2023c] [Li 2023b] [Li 2023d] [Li 2023a] [Li 2024] [Li and Guo 2005] [Li and Hu 2021] [Li and Mo 2012] [Li et al. 2008] [Li et al. 2009] [Li et al. 2016] [Li et al. 2018b] [Li et al. 2022a] [Liao et al. 2010] [Lin et al. 2011] [Lin et al. 2026] [Ling et al. 2005] [Lissenden et al. 2007] [Liu 2003] [Liu 2024a] [Liu 2024b] [Liu and Zhang 2014] [Liu and Zhong 2010] [Liu et al. 2007] [Liu et al. 2011b] [Liu et al. 2011a] [Liu et al. 2014b] [Liu et al. 2020] [Liu et al. 2021a] [Liu et al. 2021b] [Liu et al. 2023b] [Lium 1971] [Lockheed Aircraft Corp Marietta Ga 1962] [Logan 1964] [Long et al. 2011] [Lu et al. 2023a] [Lu et al. 2023b] [Lum and Chait 1977] [Luty et al. 2018] [Luyi et al. 2020] [Buang et al. 2015] [Machining and Chemical Shaping 2015] [Machining Difficult Materials 1965] [Machining for Air Data 1989] [Machining of Aerospace Materials 1986] [Anuj and Hari Parshad 2025] [Davim 2014] [Machining Titanium. II 1958] [Magnuson 1977] [Maia et al. 2017] [Mal’kov 1992] [Marion et al. 2016] [Mari̇za and Baştürk 2021] [Martin 1964] [Masood 2019] [Matikas 2002] [Matsugi and Hino 2024] [Matsugi et al. 2025] [Matsuo 1991] [Matviichuk and Nesterenkov 2026] [Maykuth and Ernst 1964] [McDarmaid 1985] [McMurray et al. 2007] [McQuilkin 1982] [Medekshas 2008] [Method for Forming Titanium 1991] [Micari et al. 1997] [Micromechanical Characterization and Texture 2000] [Mithu et al. 2025] [Miura 2015] [Mocerino and Burroughs 1979] [Mofidi Tabatabaei 2023] [Mohandas et al. 1999] [Morestin et al. 1996] [Moritoki 1972] [Mosleh et al. 2019] [Motyka 2019] [Movahedi and Gerdooei 2024] [Mrad et al. 2013] [Mukherjee and Arieli 1982] [Mulidrán et al. 2026] [Murav’ev et al. 2019] [Murzinova 2008] [Myers 1962] [Frestel et al. 1992] [Nabhani 2001] [Barrett 1950] [Naceur 2004] [Naceur et al. 2006] [Nakamura 1988] [Naksuk et al. 2022] [Nanu and Brabie 2012] [Narasimhan and Lovell 1999] [Narayanasamy and Padmanabhan 2010] [Scott 1972] [Lunde 1977] [Turner and Grande 1978] [Guess et al. 1981] [Kaneko et al. 1982] [Bales et al. 1990] [Hinkley et al. 1999] [Ellis 2012] [Nasrollahi and Arezoo 2012] [Nawaya et al. 2018] [Nele and Teti 2018] [Neto et al. 2016] [Neto et al. 2017] [Nguyen et al. 2010] [Nharwal and Singh 2026] [Nikhare 2019] [Nikhare 2020] [Nikhare 2021] [Nikhare et al. 2021] [Nikitenko 1976] [Niknam et al. 2014] [Noma et al. 2011] [Norris et al. 1999] [Nouari and Makich 2014] [Nouari et al. 2013] [Ogawa et al. 2006] [Okafor 2020] [Ortiz et al. 2019] [Ossa and Royster 1987] [Ozturk et al. 2010] [Praveen and Lee 2017] [Padmanabhan et al. 2016] [Panthi et al. 2007] [Panthi et al. 2008] [Panthi et al. 2010] [Papeleux and Ponthot 2002] [Parris et al. 1957] [Pasupuleti et al. 2025] [Patel et al. 2013] [Patel et al. 2025] [Paul et al. 2017] [Paul et al. 2025] [Pačák et al. 2019] [Perveen and Oliaei 2020] [Peters and Leyens 2003] [Peters et al. 2003] [Petrak 1970] [Pham et al. 2019] [Phillips 1969] [Phillips 1974] [Pilchak et al. 2012] [Pitt and Ramulu 2004] [Pitt and Ramulu 2012] [Pitt et al. 2004] [Poirier and Sung 2006] [Poolperm et al. 2021] [Pop et al. 2025] [Pornputsiri and Kanlayasiri 2020] [Pourboghrat and Chu 1995] [Pramanik and Littlefair 2014] [Pramanik and Littlefair 2015] [Pramanik et al. 2013] [Premanond et al. 2011] [Pridham et al. 2001] [Processing and Machining 2012] [Production of Aerospace Titanium 2001] [Production Progress with Superplastic 1984] [Pulley 1977] [Purcarea and Dumitrescu 2017] [Qi et al. 2025] [Qu et al. 2023] [quan et al 2024] [Quảng 2025] [Quattrocchi and Koss 1992] [Quattrocchi et al. 1991] [Qudeiri et al. 2015] [Radonjic and Liewald 2016] [Ragai and Nemes 2010] [Ravichandran 2000] [Rawe 1967] [Reams et al. 2012] [Ren et al. 2019] [Revil-Baudard and Massoni 2009] [Rey 1956] [Ridgway et al. 2010] [Ridley 2003] [Ridley 2010] [Ridley 2011] [Ridley 2019] [Roberge 2025] [Rolf and Patrick 1978] [Rollin] [Romine 1962] [Rominiyi and Mashinini 2025] [Roy and Silberschmidt 2014] [Royster 1968] [Royster 1969] [Royster and Bales 1983] [Royster et al. 1982] [Royster et al. 1983] [Royster et al. 1985] [Ruan et al. 2008] [Sabourin 2004] [Sachs and Sessler 1961] [Safiullin and Lutfullin 1996] [Safiullin et al. 2012] [Saidi et al. 2021] [Saito et al. 2016] [Saito et al. 2017] [Sajadifar et al. 2023] [Salem et al. 2016] [Salguero et al. 2024] [Sana et al. 2016] [Sanders 2005] [Sanders and Ramulu 2004] [Sanders and Ramulu 2012] [Sanders et al. 2008] [Sanders et al. 2010] [Santos] [Saprykin 2013] [Sarrazin-Baudoux et al. 1997] [Sastry et al. 1983b] [Sastry et al. 1983a] [Sathish 2018] [Sazonov and Zhidyaev 2022] [Schikorra et al. 2005] [Schmoeckel and Beth 1993] [Scholz et al. 2026] [Schweinoch et al. 2015] [Semiatin et al. 2004] [Șerban et al. 2013] [Settineri and Faga 2008] [Shagiev et al. 2022] [Shan and Liu 2011] [Shanabarger 1990] [Shang et al. 1996] [Shanmugam et al. 2023] [Sharad and Nandedkar 2014] [Sharma et al. 2020] [Shazly et al. 2006] [Shen 2005] [Shirizly 2005] [Shkaraputa 1976] [Shu et al. 2025] [Simenz 1965] [Singh and Khanna 2020] [Singh et al. 1998] [Siring 2025] [Siswanto et al. 2014] [Slota and Jurčišin 2012] [Slota et al. 2014] [Smith and Piascik 2001] [Soni and Chakraverti 1994] [Sorgente 2021] [Sorgente and Palumbo 2020] [Sornsuwit and Sittisakuljaroen 2014] [Sosnin and Torshenov 1970] [Spathopoulos and Stavroulakis 2020] [Springback Analysis in Sheet 2016] [Springback Simulation of U-Channel 2016] [Stagner 1980] [Stander et al. 2002] [Stauffer and Czyryca 2004] [Stauffer et al. 2004] [Stein 1998] [Stephen 1995] [Structural Titanium Alloys 2005] [Structure of Titanium Alloys 2005] [Xuebin et al. 2024] [Suckow et al. 2019] [Sudhakar Rao et al. 2024] [Sudhir et al. 2020] [Sui et al. 2013] [Sullivan 1967c] [Sullivan 1967b] [Sullivan 1967a] [Sullivan 1968] [Sullivan 1971] [Sun et al. 2006] [Superplastic Forming and Diffusion 1983] [Superplastic Forming and Diffusion 1997] [Swale and Broughton 2004] [Szczepanski et al. 2011] [Szpunar et al. 2022] [Tang 1978] [Tang et al. 2010a] [Tang et al. 2010b] [Technological Properties of Titanium 2005] [Tekaslan et al. 2006] [Test Method for Evaluating] [Teti and Caggiano 2018] [Thevenot et al. 1993] [Titanium in Aerospace 1975] [Titanium or Titanium Alloy 1974] [Trzepieciński and Lemu 2020] [Trân et al. 2020] [Tsuyama et al. 1992] [Tsuzuku 1999] [Turan Abi and Yılmaz 2019] [Uhlmann et al. 2015] [Uslu et al. 2016] [Valjavec and Hardt 1999] [Van Orden and Soffa 1968] [Vartanov 2020] [Vaughan and Jones 1971] [Versatile ATI 425 Titanium 2004] [Vigdortchik and Tupolev 1982] [Viswanathan et al. 2003] [Vladimirov and Reese 2007] [Vrh et al. 2009] [Wagoner 2004] [Walczyk et al. 1998] [Wan-Nawang et al. 2015] [Wang 2005a] [Wang 2005b] [Wang et al. 1993] [Wang et al. 2005b] [Wang et al. 2005a] [Wang et al. 2006] [Wang et al. 2008] [Wang et al. 2011a] [Wang et al. 2015] [Wang et al. 2016b] [Wang et al. 2016a] [Wang et al. 2020a] [Wang et al. 2020b] [Wang et al. 2022c] [Wang Mingwei et al. 2006] [Warnken and Busch 1963] [Warrier and Lin 1993] [Wei et al. 2021] [Wei et al. 2022b] [Wei et al. 2022a] [Weinschenk and Volk 2014] [Weiss et al. 2024] [Wen et al. 2026] [Wenjuan Liu et al. 2008] [Whittaker 1972] [Wiezorek and Mills 1998] [Williams 1982] [Williams and Duerden 1970] [Wilson 1982] [Więckowski et al. 2023] [Wu 1996] [Wu et al. 2020] [Wu and Luo 2011] [Wu et al. 2018] [Wu et al. 2023] [Xi 2013] [Xu 2020] [Xu et al. 2004b] [Xu et al. 2004a] [Xu et al. 2019a] [Xu et al. 2024] [Xu et al. 2026] [Xu] [Xue et al. 2015] [Yadav and Yadava 2015] [Yamane et al. 2018] [Yamazaki et al. 2014] [Yan et al. 2019] [Yang and Richard Liu 1999] [Yang and Ruan 2010] [Yang et al. 2010] [Yang et al. 2016b] [Yang et al. 2021] [Yang] [Yarlett et al. 2000] [Yasmeen et al. 2019] [Yasmeen et al. 2020] [Yasmeen et al. 2022] [Yetna n’jock et al 2018] [Yi et al. 2008] [Yilamu et al. 2010] [Yoon et al. 2002] [Yoon et al. 2007] [Yoshida and Uemori 2015] [Yoshida et al. 2010] [Yu et al. 2023] [Yuen 1990] [Zhang and Cui 2009] [Zhang and Jiang 2014] [Zhang and Lee 1996] [Zhang and Lou 2024] [Zhang and Wu 2016] [Zhang et al. 2004] [Zhang et al. 2008b] [Zhang et al. 2014a] [Zhang et al. 2016a] [Zhang et al. 2016b] [Zhang et al. 2024a] [Zhang et al. 2026d] [Zhao et al. 2025] [Zhao et al. 2026b] [Zheng 2024] [Zhiqiang 2014] [Zhou et al. 2010] [Zhou et al. 2021a] [Zhou] [Zhu and Li 2023] [Ziffrin 1962] [Zitoune et al. 2013] [Zlatin and Field 1973] [Álvarez et al. 2010] [Świa̧toniowski and Bałon 2015] [Şen and Seçgi̇n 2020]

The thin, low aspect ratio wing at supersonic speed

The first half of the keystone. Thin sections, low aspect ratio planforms, supersonic lift, wave drag and the shift of the aerodynamic centre. 175 of these records date from before 1960, more than in any other cluster, because the linearized theory of the thin supersonic wing was worked out in the decade that produced the X-3.

695 records. [Abdullah et al. 2022] [Abraham et al. 2023] [Abraham et al. 2024] [Ackeret 1925] [Adamson and Boatright 1950] [Adamson and Boatright 1957] [Ahmed 2004] [Ahmed and Worley 2008] [Aiken and Fisher 1957] [Alexander 1971] [Alviani et al. 2020] [Amiet 1974] [Amiet 1976] [Ananda et al. 2012] [Andrei et al. 2026] [Andrew and Cahn 1967] [Andrew and Stenton 1967] [Ashley et al. 1954] [Augenstein 1950] [Azam and Sulaeman 2014] [Babu and Narsipur 2025] [Ball et al. 1981] [Bantscheff and Breitsamter 2024] [Barnard 1969] [Barton 1948] [Beals and Targoff 1953] [Bennett 1961] [Bennett et al. 1987] [Bera 1977] [Bera 1988] [Bernal 2016] [Bertelrud and Graves 1994] [Bertram and Ulmann 1953] [Bishop 1951] [Bleviss 1951] [Boatright 1958] [Bodonyl 1994] [Bonney 1947] [Bouton 1950] [Brady et al. 1954] [Bridges 2005] [Brown 1946] [Brown 1950] [Brown and Heinke 1956] [Brès et al. 2011] [Bulygina 1958] [Burkhart 1980] [Byun and Guruswamy 1996a] [Byun and Guruswamy 1996b] [Byun and Guruswamy 1998] [Lee 2008] [Campbell 1959] [Candida et al. 2019] [Carafoli 1969h] [Carafoli 1969f] [Carafoli 1969i] [Chaderjian 1994] [Chaderjian and Schiff 1993] [Chaderjian and Schiff 1994] [Chaderjian and Schiff 1996] [Chadrjian and Schiff 1995] [Chan 1992] [Chang 1992] [Chapter 2. Aerodynamics 1960] [Chapter 2. Wing-Body Interference 1957] [Chapter 3. Aerodynamics 1957] [Chapter 3. Aerodynamics 1960] [Chapter 5. Wing-Body Interference 1957] [CHAPTER FOUR. Thin Airfoil 1990] [CHAPTER NINE. the Minimum 1990] [Chawla 1958] [Chen 2022] [Chen et al. 2001] [Chen et al. 2024] [Cheng 1982] [Cheng and Rott 1954] [Cheng et al. 2018] [Chester 1953] [Chiarelli and Bonomo 2019] [Chin 1977] [Chin 1978] [Chin 1984] [Chipman et al. 1985] [Chuang and Kandil 1989] [Chuvakhov et al. 2023] [Cockbill 2018] [Cohen and Evvard 1948] [Cole 1986] [Cole 1988] [Cole 1989] [Cole 1990] [Cole 1992] [Collicott et al. 2026] [Conyers et al. 2010] [Cosyn and Vierendeels 2005] [Couillaud] [Cramer et al. 1976] [Crasta and Khan 2014] [Crosthwait 1966] [Currao and Yeh 2026] [Czarnecki and Mueller 1950] [Czarnecki and Mueller 1951] [Darden 1984] [Das et al. 2021] [Davis and Marshall 2020] [Davis] [De Oro Fernandez et al. 2020] [DeJarnette and Jones 1978] [Del Frate 1992] [Deneke et al. 2026] [Desai et al. 1977] [Dickey 1959] [Diederich and Foss 1953] [Diederich and Zlotnick 1949] [Dikbas and Atik 2018] [Dixon and Hunsaker 2023] [Djojodihardjo 2023] [Dodbele and Plotkin 1985] [Doggett and Ricketts 1980] [Doggett and Soistmann 1989] [Doggett and Soistmann 1992] [Dong et al. 2020] [Dong et al. 2022] [Dragos and Dinu 1990] [Drougge 1990] [Dutta et al. 2022] [Eastep and Olsen 1979] [Eastep and Olsen 1980] [Md Akhtar Khan 2014] [Ehlers et al. 1976] [Engelbrecht] [Er-El 1988] [Er-El et al. 1989] [Eremenko et al. 2003] [Ericsson 1980] [Ericsson 1996c] [Ericsson 1997b] [Ericsson and Hanff 1994b] [Evvard 1947a] [Evvard 1947b] [Evvard 1948] [Evvard 1950] [Evvard and Turner 1947] [Fang 2011] [Faroughi et al. 2012] [Flax 1953] [Flow in the Vicinity 1998] [Follé 1983] [Fomin et al. 2009] [Fortunato 1985] [Fournis 2022] [Fraenkel 1958a] [Fraenkel 1958b] [Friehmelt 2002] [Frolov 2021] [Furey 1980] [Försching and Zingel 1988] [G. the Experimental Aerodynamics 1957] [Gallagher and Mueller 1955] [Garcia-Fogeda and Liu 1988] [Gardner and Ludloff 1950] [Garrick and Rubinow 1947] [Ghoreyshi et al. 2024] [Gillespie 1957] [Gillespie 1960] [Giragosian 1982] [Gogish and Dashevskaya 1990] [Goldsworthy 1952] [Golovkin 2013] [Golubkin et al. 2002] [Gonzalez and Winkelmann 1993] [Goodman 1951] [Gopalarathnam et al. 1997] [Gordnier 1993] [Gordnier 1995] [Gordnier and Visbal 1993] [Goto et al. 2007] [Grafton et al. 1982] [Graham 1958] [Graves 1971] [Graves 1972] [Greene and Sobieszczanski-Sobieski 1980] [Greene and Sobieszczanski-Sobieski 1982] [Greenwell and Wood 1994] [Gresham et al. 2009b] [Gresham et al. 2009a] [Gresham et al. 2010] [Griffin and Eastep 1981] [Griffin and Eastep 1982] [Griffin et al. 1983] [Guan 2014a] [Guan 2014b] [Guderley 1986] [Guderley 1987] [Guderley 1988] [Gunn 1947b] [Gunn 1947a] [Gur’ev et al. 2011] [Guruswamy and Goorjian 1984] [Guruswamy and Goorjian 1985] [Guy and Hadaway 1955] [Gülsaçan et al. 2018] [Haas et al. 2021] [Haas et al. 2022] [Haefeli et al. 1950] [Hall and Heitmeyer 1951] [Hancock 1959a] [Hancock 1959b] [Hancock 1960] [Hanff and Huang 1991] [Hanson and Levey 1959] [Harmon 1947] [Harmon and Swanson 1947] [Hartley et al. 1965] [Heitmeyer 1952] [Heitmeyer 1954] [Heitmeyer and Smith 1952] [Henning 1959] [Hernandez et al. 1994] [Herrmann and Nemat-Nasser 1966] [Heslet et al. 1947] [Hicks and Moulton 1988] [Hill and Kaattari 1956] [Hilton 1955] [Hirose et al. 2024] [Hirschel et al. 2020b] [Hirschel et al. 2020a] [Holdaway 1954] [Holdaway and Mellenthin 1960a] [Holdaway and Mellenthin 1960b] [Holdaway et al. 1959] [Hopkins 1975] [Hopkins 1977] [Hoque et al. 2023] [Houghton et al. 2017] [Howell and Korst 1971] [Hsiao et al. 2008] [Huang et al. 2001] [Hunziker 1960] [Huyer et al. 1992] [Ilyukhin and Egorov 2024] [Im et al. 2012] [Iosilevskii 2025b] [Iosilevskii 2025a] [Iosilevskii 2025d] [Iosilevskii 2025c] [Isogai 1979] [Isogai 1981] [Isogai 1992] [Ivey and Bowen 1947] [Ize and Arena 1998] [Jenn and Nelson 1988] [Jenn and Nelson 1989] [Jian and Ke-Qin 2004] [Jian et al. 2004] [Johnson and Sandlin 1984] [Johnson and Sandlin 1986] [Johnston et al. 2010] [Jones 1946] [Jones 1947b] [Jones 1950a] [Jones 1957] [Jones 1962] [Jones 1967b] [Jones 1976e] [Jones 1980] [Jones 1989] [Jones and Alksne 1948] [Jones and Unangst 1963] [Jorgensen and Katzen 1956] [Jumper 1983] [Kalkhoran et al. 1995] [Kalkhoran et al. 1996] [Kanamori et al. 2009] [Kandil and Chuang 1989] [Kandil and Salman 1991] [Kandil et al. 1993] [Kase et al. 2020] [Kassem and Banerjee] [Katz 1989] [Katz and Levin 1986] [Kaushik 2018] [Kawamura and Karashima 1957] [Kawazoe and Kato 2005] [Kaynak et al. 1986] [Kaynak et al. 1987] [Keenan and Kuhlman 1991b] [Keenan and Kuhlman 1991a] [Keener 1984] [Keener 1985] [Keith 1957] [Kemp 1973] [Kemp 1978] [Kemp and Homicz 1976] [Khan et al. 2006] [Khan et al. 2021] [Khan et al. 2025b] [Kharsansky Atallah] [Khrabrov and Ol 2004] [Kim and Lee 2002] [Kimble et al. 1973] [Kimble et al. 1974] [Kishi et al. 2016] [Kishi et al. 2017] [Klopfer and Nielsen 1979] [Klopfer and Nielsen 1980] [Kolodner 1950] [Kopzon 1958] [Kornev et al. 2021] [KoÇAk and Yavuz 2023] [Kraiko and Tilliaeva 1973] [Kraiko and Tkalenko 1967] [Kuhlman and Brown 1989] [Kuhlman and Liaw 1987] [Kuhlman et al. 1988] [Kulfan 2008] [Kulfan 2009] [Kutney and Piszkin 1964] [Lacey 1979] [Lagerstrom and Graham 1949] [Lagerstrom and Graham 1951] [Lai and Kamaruddin 2018] [Laitone 1989] [Lampropoulos and Sarris 2025] [Lan and Roskam 1972] [Larson 1984] [Larson 1985] [Lauten and Nelson 1957] [Lawrence 1951] [Lawrence 1953] [Le and Hoang 2026] [Lei and Zha 2021] [Lei and Zha 2023] [Lemley and Mullans 1974] [Leslie and Perry 1954] [Levin and Katz 1984] [Levin and Katz 1990] [Levin and Katz 1992] [Li 1956] [Lift/Drag Ratios of Optimised 1962] [Lin et al. 2021] [Linehan and Mohseni 2016b] [Liu 2022c] [Liu 2022b] [Liu 2022d] [Liu 2022a] [Liu and Weng 2007] [Lock 1957] [Lock 1958] [Lock 1961] [Lock 1963] [Lock and Bridgewater 1967] [Lockwood 1966] [Loh and Hui 1989] [Lomax 1953] [Lomax 1954] [Lomax 1959] [Lomax and Heaslet 1956a] [Lomax and Heaslet 1956b] [Lomax et al. 1954] [Lomax et al. 1955] [Lowe 1988] [Luce 1949] [Lucero 1984] [Lucero 1985] [Ludloff and Reiche 1947] [Luo and Cheng 1996] [Mabey and Welsh 1987] [Maikapar 1959] [Maikapar 2000] [Maji et al. 2024] [Malmuth et al. 1986] [Malmuth et al. 1987] [Malone et al. 1984] [Malone et al. 1986] [Malvestuto and Hoover 1951b] [Malvestuto and Hoover 1951a] [Mann and Carlson 1994] [Manor and Wentz 1985] [Mansour 1984] [Mansour 1985] [Marchman et al. 1983] [Margalit et al. 2005] [Margolis et al. 1958] [Marion and Sharma 2025] [Martin 1953] [Martin and Gerber 1953a] [Martin and Malvestuto 1955] [Martin et al. 1991] [Martinez and Widnall 1980] [Maruyama et al. 2006] [Maruyama et al. 2009] [Marzocca et al. 2002] [Mason 1953] [Masson et al. 1998] [McCormick 1959] [McCutchen 2006] [McFadden and Heinle 1954] [McGrath 1993] [McGrath 1995] [Mertens et al. 1986] [Meyer 1992] [Miklosovic and Perry 2014] [Miklosovic et al. 2012] [Miklosovic et al. 2016] [Miles 1947] [Miles 1951] [Miles 1952] [Miles 1953b] [Miles 1953a] [Miller 1983] [Miller et al. 1983] [Miller et al. 2019] [Mirels 1948] [Mirels 1951] [Mizoguchi and Itoh 2016] [Mizoguchi et al. 2014] [Moeckel and Evvard 1948] [Mohamed et al. 2022] [Morikawa 1951] [Morote and Liaño 2012] [Morse and Liburdy 2009b] [Morse and Liburdy 2009a] [Morton 1956] [Moskowitz and Moeckel 1950] [Mugler 1957] [Mugler 1959] [Munk 1950] [Ribner 1947] [Margolis 1947] [Walker and Berggren 1948] [Nakai et al. 1967a] [Nakai et al. 1967b] [Narayan 1975] [Taillon 1959] [Shrout 1965] [Bartlett and Harris 1974] [Eckstrom 1976] [Byrdsong 1977] [Lawing et al. 1991] [Bennett 2000] [Nastase 2008b] [Nastase and Rudianu 1990] [Nastase and Weisensee 1984] [Naylor 1957] [Chaderjian and Schiff 2000] [Nelson 1989] [Nelson 1990] [Nelson and Bossi 1995] [Nelson et al. 1954] [Newey] [Newsome 1985] [Nielsen 1947] [Nielsen 1955] [Nielsen 1986] [Nielsen and Pitts 1952] [Nielsen et al. 1953] [Nietubicz 1975] [Nikolic and Jumper 2004] [Noll et al. 1983] [Nomura 2003] [Nyberg and Sorensen 1980] [O’Donnell and Mohseni 2017] [O’Donnell and Mohseni 2019] [Oggioni et al. 2026] [Olsen and Seegmiller 1992] [Olsen and Seegmiller 1993] [Osborne 1973] [Park et al. 1996] [Parnell 1986] [Paulsen and Schadt 1966] [Peake 1997] [Pechloff and Laschka 2010] [Pechuzal and Kevorkian 1977] [Pelletier and Mueller 1999] [Pelletier and Mueller 2000] [Pereira et al. 2025] [Perry and Miklosovic 2012] [Pfaff 1965] [Pfenninger and Vemuru 1988] [Piland 1951] [Pittman 1986] [Pittman 1987b] [Pittman and Giles 1986] [Pivko 1956] [Platzer 1965b] [Platzer 1965a] [Plotkin 1978] [Plotkin 1990] [Postel and Leppert 1948] [Prakash et al. 2009] [Prasad et al. 1967] [Pratt 1955] [Pritulo et al. 1995] [Probstein 1953] [Puckett 1946] [Raghavan and Ananthkrishnan 2005a] [Rainey 1950] [Rajamurthy 2002] [Rallabhandi and Mavris 2003] [Rambacher et al. 2024] [Ramesh 2025] [Ramm 1990] [Ramprasadh and Devanandh 2015] [Rao et al. 2023] [Razak et al. 2011] [Recent Developments 1967] [Rein et al. 2009] [Rein et al. 2025] [Reinbold et al. 2021] [Reissner 1944] [Reuther and Jameson 1995] [Ribner 1960] [Rimer et al. 1984b] [Rizzetta 1995] [Rizzetta and Visbal 2012a] [Rizzetta and Visbal 2012c] [Rizzetta and Visbal 2012b] [Rizzi and Purcell 1986] [Jones 1976b] [Jones 1976c] [Roberts 1948] [Robinson 1948] [Robinson and Robinson 1980] [Rockwell 1994] [Rockwell 2011] [Rodden 1989a] [Roger and Chan 2004] [Rose et al. 1988] [Ross and Matarazzo 1982] [Rott 1951] [Rott 1953] [Rule et al. 2000] [Rule et al. 2001] [Rullan et al. 2006] [Runyan and George-Falvy 1979] [Rusak 1993] [Röntsch et al. 2016] [Varunkumar and Gangamkote 2023] [Sadoff 1953] [Sanz 1986] [Sattarov and Rozbytskyi 2021] [Savin 1958] [Schewe and Mai 2019] [Schuelein 2008] [Schütte and Hummel 2023] [Scott and Atassi 1989] [Sears 1947] [Separation at the Leading 1998] [Sevier 1960] [Shah and Ahmed 2023] [Sharifi Ghazijahani and Yavuz 2019] [Shields and Mohseni 2013a] [Shields and Mohseni 2013c] [Shields and Mohseni 2013b] [Shumsky 2010b] [Sibert 1937] [Sibert 1947] [Simpson and Birch 2001] [Skare] [Sklar and Rusak 2020] [Smart et al. 1994] [Smith 1961] [Smith and Taira 2024] [Snyder and Memory 2005] [Soong 1972] [Sorenson 1974] [Special Features of Antiaircraft 2010] [Spreiter and Alksne 1957] [Srichitturi 2026] [Stallings 1979] [Stanbrook 1954] [Stanišić 1961] [Stanišić 1962] [Stewart 1946] [Stewart 1956] [Stewart and Li 1950] [Stewartson 1950b] [Stewartson 1950a] [Stewartson 1952] [Stewartson 1966] [Stocker 1951] [Strand 1960] [Sugiyama 1971] [Sun and Hansen 1982] [Supersonic Airfoil Performance 1959] [Sutton 1959] [Swamy et al. 1978] [Taira et al. 2010] [Takahashi 2021] [Takamatsu and Yamazaki 2021] [Tao et al. 2018] [Taylor and Gursul 2004] [Taylor and Ratnayake 2011] [Taylor et al. 2010] [Telionis 1990] [Terashima and Fujii 2004] [Terashima and Fujii 2007] [Thawait et al. 2022] [Thin Wing Sections 2012] [Thompson et al. 1990] [Timman 1954] [Ting 1959] [Tingas and Rao 1982] [Tjatra et al. 1992] [Tkalenko 1969] [Torii and Matsuzaki 1991] [Torres and Marques 2025] [Torres and Mueller 2004] [Torres et al. 2025] [Traub 1997] [Traub 2023] [Trobaugh et al. 1980] [Tromp 1998] [Tromp 1999] [Trussa et al. 2022] [Trussa et al. 2026] [Tu 1992] [Tucker 1948a] [Tucker 1948b] [Tucker and Nelson 1948a] [Tucker and Nelson 1948b] [Tucker and Nelson 1949] [Tuling et al. 2013] [Two-Dimensional Supersonic Flows around 2021] [Two-Dimensional Supersonic Flows around 2025] [Ulbrich 2004] [Unangst 1959] [van Dommelen et al. 2019] [Vaughn 1982] [Vey et al. 2010] [Vey et al. 2012] [Vira and Fan 1982] [Visbal 2011] [Visbal 2017] [Visbal and Garmann 2012] [Visbal et al. 2013] [Vogel 1973] [Vortical Flow Topology 2009] [Waechter 1969] [Walker 1953] [Walkley 1986] [Wallace 1952] [Wallskog 1954] [Walsh et al. 1954] [Wang 2019] [Ward 1949] [Watkins 1949] [Watkins 1951] [Webster and Shang 1991] [Weisshaar 1979] [Weisshaar and Crittenden 1976] [Whitcomb 1952] [Wieszala et al. 2022] [William Ruffles and Sam M. Dakka 2016] [Williams 1979] [Williams 1980a] [Williams 1980b] [Williams and Nelson 1994] [Williams, I and Nelson 1995] [Winkelmann 1989] [Wokoeck and Radespiel 2011] [Wood and Bauer 1988] [Wood and Covell 1985] [Wood and Miller 1985a] [Woodward 1956] [Woolston et al. 1960] [Wylly 1952] [Xieyuan 1985] [Xu 2023] [Yang et al. 2012] [Yang et al. 2025] [Yates 1963] [Yates 1967] [Yates 1978] [Yates 1980] [Yatskikh et al. 2017] [Yonezawa et al. 2007] [Yong 2019] [Yoon et al. 2012] [Yoshikawa 1982] [Yoshiki et al. 1985] [Yotsuya et al. 2014] [Yu 2023] [Yu and Bernal 2016] [Yu et al. 2013] [Zedan and Abu-Abdou 1988] [Zeng et al. 2022] [Zhang 1988] [Zhang and Lu 2026] [Zhang et al. 2017] [Zhang et al. 2020a] [Zhao et al. 2023] [Zohar and Er-El 1988] [ŌTomo and Ramesh 2026]

Supersonic inlets, pressure recovery and unstart

The second loss in the sizing that does not close. Inlet pressure recovery, spillage and additive drag, bleed, buzz and unstart. 128 of these titles name unstart or buzz, and 109 of those date from 2000 or later, which is the literature’s own measure of the shift this article describes, from the fixed inlet as a compromise to the unstart boundary as a controlled limit.

599 records. [Abedi et al. 2020] [Adams et al. 1984] [Afzal and Safdar 2020] [Alendar et al. 2022] [Alford and Durand 1964] [Alford et al. 1962] [Khan and Hasan 2019] [Allen et al. 1960] [Amin and Hollweger 1981] [Amin and Hollweger 1983] [Amur Varadarajan and Roe 2011] [Ananthapadmanaban and Murganandam 2016] [Anderson 1984b] [Anderson 2014b] [Anderson 2014a] [Arlinger 1976] [Askari et al. 2017] [Atkinson 2007] [Automatic Detection and Suppression 1974] [Azevedo et al. 1990] [Babinsky 2007] [Babinsky 2014] [Ball and Ross 1972] [Barr 1990] [Barr et al. 2018] [Barr et al. 2022] [Barry 1971] [Bauer et al. 1974] [Bauermeister and Ip 1968] [Baydar et al. 2016] [Baydar et al. 2017] [Baye-Wallace and Krouse 2022] [Beale and Zelenak 1992] [Beaulieu and Martin 1970] [Beck 2005] [Beke 1958] [Beke et al. 1955] [Benson 1994] [Benson and Anderson 1983] [Benson and McRae 1993] [Benson and McRae 1994] [Benton et al. 2021] [Bernstein and Haefeli 1953] [Blackaby et al. 1959] [Bogar et al. 1983] [Bogue et al. 1995] [Bos 1999] [Bowditch 1973] [Braithwaite et al. 1973] [Brajnikoff and Stroud 1953] [Braun and Podleski 2019] [Burke and Poggie 2023] [Burr 1968] [Burris 1966] [Burrows et al. 2017] [Burstadt et al. 1971] [Bustard et al. 2024] [Bustard et al. 2026b] [Bustard et al. 2026a] [Shin 2005] [Cai et al. 2022] [Calogeras 1969] [Calvin et al. 2022] [Campbell 1954] [Campbell 1956] [Campbell and Ellis 1971] [Cao et al. 2026] [Carbajosa et al. 2025a] [Carbajosa et al. 2025b] [Carlin et al. 2003] [Carrier et al. 2001] [Castner et al. 2018] [Chandler and Montes 2019] [Chang and Bao 2006] [Chang and Hsu 1958] [Chang and Hsu 1960] [Cheadle and DiZinno 2026] [Chen et al. 2019a] [Chen and Tan 2019] [Chen et al. 2015] [Chen et al. 2017] [Chen et al. 2018] [Chen et al. 2025a] [Chen et al. 2026a] [Chen et al. 2026b] [Chima 2011a] [Chima 2011b] [Chima 2011c] [Chima 2012] [Chima et al. 2009] [Chima et al. 2010] [Chima et al. 2011] [Choe and Kim 2016] [Choe et al. 2020] [Choi et al. 2026] [Chopde et al. 2025] [Pastor-Barsi and Slater] [Chun and Swanson 1964] [Chung 1994] [Clark 1974b] [Clark 1995] [Cliff et al. 1999] [Cole 1977] [Comenzo and Mackley 1952] [Comenzo and Mackley 1954] [Computational Fluid Dynamics Analysis 1997] [Conners and Howe 2006] [Connors and Woollett 1952] [Cortright 1951] [Cosner 1985] [Costakis 1977] [Crosthwait 1970] [Cubbison and Smeltzer 1968] [Cui et al. 2011] [Cui et al. 2012] [Daliri et al. 2018] [Dann] [Davis 2010] [Davis and Goldstein 1948] [Davis et al. 1949] [Davis et al. 2012] [DeLaat 1998] [Dennard 1959] [Dickie 1955] [Dickinson et al. 2024] [Dickman and Takahashi 2016] [Dicus 1975] [Diggins 1951] [Ding et al. 2015] [Do et al. 2010] [Do et al. 2011b] [Do et al. 2011c] [Do et al. 2011a] [Domack 1991] [Domack 1992] [Eagle et al. 2012] [Ehrmayr and Berens 2018] [Engine Inlet Exhaust 2011] [Esenwein 1952] [Esenwein and Schueller 1952] [Eves and Valasek 2024] [Zhao et al. 2022] [Ezzeldin and Wu 2025] [Falempin et al. 2006] [Fan et al. 2017] [Farahani et al. 2019] [Farley and Seashore 1955] [Farley and Smith 1954] [Ferrero 2020] [Fink and Anderson 1982] [Forkey et al. 1993] [Fradenburgh and Campbell 1953] [Fraiser 1960] [Frank and Taylor 1951] [Frazer and Anderson 1953] [Frey et al. 2025] [Fujimoto and Niwa 1993] [Fujimoto et al. 1991] [Fuqun et al. 1985] [Gaglio and Bevilacqua 2026] [Gaglio et al. 2023] [Gas Turbine Engine Inlet] [Gelder 1957] [Gillen and Loth 2011] [Goldberg and Boxer 1959] [Grasso and Falconi 1993] [Grenson and Beneddine 2018] [Guan 2012] [Guan and Yarng 1984] [Guan and Yarng 1987] [Guidelines for Characterization of] [Haas and Karanian 1980] [Haderlie and Crossley 2010] [Hale et al. 2004] [Halwas and Aggarwal 2019b] [Halwas and Aggarwal 2019c] [Halwas and Aggarwal 2019a] [Hamed 1995] [Harloff and Smith 1995] [Harloff and Smith 1996] [Hartsell 1960] [Hastings and Dickens 1957] [Head 1972] [Hearth and Cubbison 1956] [Heath et al. 2016] [Henderson 1999] [Herges et al. 2012] [Hermann 1956] [Herrmann et al. 2011] [Hill 1970] [Hirt et al. 2011] [Hodder et al. 1981] [Hoffman 2000] [Hong and Kim 2011] [Hong and Kim 2014] [Howard et al. 1951] [Howlett and Hunter 1986] [Huang et al. 2020] [Huang et al. 2021] [Huang et al. 2025] [Huang et al. 2026] [Hughes and Johnson 1972] [Hunczak and Kremzier 1950] [Hunter and Cawthon 1984] [Hunter et al. 1985] [Hurwitz et al. 1997] [Hutchins et al. 2014] [Hwang et al. 1995] [Häberle and Gülhan 2007] [Iannelli 2007a] [Iannelli 2007b] [Influence of Back Pressure 2017] [Kumar and Das 2024] [Inger 1979] [Inlet Total-Pressure-Distortion Considerations for] [Instrumentation for in-Flight Determination 1974] [Ito and Tsuchiya 2018] [Ito and Tsuchiya 2019] [Jacocks and Kneile 1975] [Jagannathan and Johansen 2019] [James and Muruganandam 2019] [Connors et al. 1957b] [Connors et al. 1957a] [Janakiram and Duvvuri 2024] [Jee and Etele 2018] [Jee] [Jenquin et al. 2022] [Jin et al. 2023a] [Jin et al. 2023b] [Jin et al. 2022] [Jin et al. 2025] [Slater 2024] [Slater] [Slater] [Johns and Steffen 1970] [Johnson and Montoya 1973] [Johnson and Narayanaswamy 2024] [Johnson and Narayanaswamy 2026] [Johnson and Wu 1975] [Johnson and Wu 1974] [Joshi et al. 2024] [Jules and Barnhart 1998] [Jung et al. 2015] [James et al. 2021] [James and Kim 2022] [Kamal and Livesey 1979] [Kang et al. 2024] [Kapoor et al. 1994] [Karania et al. 2021] [Kawamura et al. 1987] [Kazula and Höschler 2020a] [Kazula and Höschler 2020b] [Kazula et al. 2019a] [Kazula et al. 2019b] [Kennon 1989] [Kepler and Barry 1965] [Keppler 1966] [Kerlick 1985] [Khan et al. 2018] [Khan et al. 2023] [Khan et al. 2024] [Khandelwal et al. 1996] [Ki and Lee 1998] [Kim and Park 2026] [Kim et al. 2011b] [Kim et al. 2011a] [Klepper et al. 2017] [Knight 1981] [Kochendorfer 1953] [Kong et al. 2022] [Koo and Raman 2012] [Kopasakis and Connolly 2009] [Kotov et al. 2018] [Kouyoumjian 1957] [Kremzier and Campbell 1954] [Kremzier and Wise 1955] [Krivec et al. 1984] [Kucuk and Tuncer 2023] [Kumar 2022] [Kuroda and Fujii 1991] [Kurzke 2006] [Kurzke and Halliwell 2018] [Kwak and Lee 2011] [Kwak and Lee 2013a] [Kwak and Lee 2013b] [Kwak et al. 2013] [Küçük et al. 2015] [Ladd and Norby 1998] [Lankford 1947] [Lawing and Johnson 1978] [Howerton and Slater] [Lazzeroni et al. 1955] [Frank and Pfyl 1956] [Leamer and Kennon 1978] [Lee and Boedicker 1985] [Lee and Choi 2021] [Lee and Jeung 2009] [Lee et al. 2009] [Lee et al. 2010] [Lehtinen and Zeller 1972] [Leissler and Nettles 1954] [Leonard and Narayanaswamy 2018] [Leonov et al. 2012] [Li et al. 2018c] [Li et al. 2022b] [Li et al. 2023b] [Liang et al] [Liou and Benson 2010] [Liu et al. 2018] [Liu et al. 2025b] [Liu et al. 2025c] [Liu et al. 2026b] [Loth et al. 2016] [Lu and Jain 1998] [Lundell et al. 1961] [Luo et al. 2020] [Luo et al. 2024b] [Mace and Sedlock 1981] [Maghsoudi et al. 2020] [Malan and Brown 1994] [Manneschmidt et al. 2024] [Mardoc 1970] [Marvin 1968] [Mascitti 1966] [Masud and Khan 2015b] [Masud and Khan 2016] [Matsuo and Kim 1993] [Matsuo et al. 2023] [Mayer and Paynter 1994] [Mayer and Paynter 1995] [Maywald and Beale 1991] [Mazhul 2020] [McKevitt et al. 1957] [McLAFFERTY 1953] [McVey et al. 1969] [Medina et al. 2021] [Merchant et al. 2003] [Merkli 1975] [Merkli 1976] [Merlet 1954] [Bozeman and Carlson 2022] [Migliorini et al. 2019] [Miki et al. 2014] [Miller and Smith 2003] [Min et al. 2026a] [Min et al. 2026b] [Mitcham et al. 1951b] [Mitchell et al. 1974] [Mittal et al. 2026] [Moeckel 1955] [Moin and Lele 1998] [Mount 1964] [Mount 1965] [Mouton 2021] [Mouton et al. 2017] [Muller and Gasko 1967] [Murzionak] [Musial 1957] [Ferri and Nucci 1946] [Goelzer and Cortright 1951] [Dryer and Beke 1952] [Beke and Allen 1953] [Allen and Beke 1953] [Hasel et al. 1953] [Mitchell and Campbell 1957] [Nagao et al. 2019] [Najafiyazdi et al. 2007] [Nakayama et al. 2011] [Namkoung et al. 2012] [Naruse et al. 2022] [Anderson and Bowditch 1958] [Evans et al. 1974] [Bulman et al. 1997] [Fernandez et al. 2001] [St. John and Frederick 2013] [Neaves and McRae 1995] [Neaves et al. 2001] [Nichols and Goral 1952] [Nichols and Pendley 1952] [Nichols and Rinkoski 1952] [Nie et al. 2019] [Nikaido and Hobson 2025] [Nikolaidis et al. 2022] [Ning] [Noftz and Jewell 2025] [Nussdorfer et al. 1952] [Obey et al. 1952] [Obikane 1984] [Oh and Yang 1994] [Oh et al. 2005] [Ordaz et al. 2017] [Osmon 1967] [Osmon 1968] [Ostrander et al. 1995] [Oswatitsch 1980] [Otto et al. 2015] [Palko 1974] [Park et al. 2023] [Paynter 1994] [Paynter and Chen 1983] [Paynter and Mayer 1995] [Paynter and Tjonneland 1992] [Paynter et al. 1992] [Paynter et al. 1993a] [Paynter et al. 1993b] [Pendley and Robinson 1950] [Pečinka et al. 2017] [Pfyl 1955] [Piovesan et al. 2025] [Podleski 1993] [Porcher and Thebiay 1962] [Poulinakis et al. 2023] [Powell et al. 1985] [Pruitt and Bates 1992] [Qin et al. 2026] [Qiushi et al. 2014] [Racisz 1946] [Rademakers et al. 2014] [Ramachandra et al. 1982] [Ramprakash and Muruganandam 2016] [Ran and Mavris 2005] [Ranard and Davison 1961] [Ratchford et al. 2025] [Reardon et al. 2021] [Reinhart and Tjonneland 1965] [Rejeske and Stava 1974] [Reukauf et al. 1974] [Review of Inlet/Airframe Integration 1986] [Reyhner and Hickcox 1972] [Rizzetta 1991] [Rizzi and Schmidt 1978] [Rodriguez 2004] [Rolls 1953] [Rolston and Raghunathan 1994] [Rybalko et al. 2010] [Rybalko et al. 2013] [Samimy et al. 2011] [Sano et al. 2018] [Saravanan et al. 2017] [Sarmazdeh et al. 2014] [Sarwar et al. 2024] [Sasoh et al. 2018] [Saunders and Keith 1991] [Scharnhorst 2012] [Schuelein et al. 2017] [Schwendemann and Sanders 1982] [Seashore and Farley 1958] [Sedlock 1985] [Selna and Schlaff 1951] [Selna et al. 1952] [Sepahi-Younsi 2022] [Sepahi-Younsi 2025] [Sepahi-Younsi and Esmaeili 2023] [Shaw et al. 1976] [Shi et al. 2010] [Shigematsu et al. 1990] [Shigematsu et al. 1991] [Shimabukuro et al. 1979] [Shucheng and Xijun 1994] [Shulman et al. 1966] [Singh Sandhu et al. 2025c] [Singh Sandhu et al. 2025d] [Singh Sandhu et al. 2025a] [Singh Sandhu et al. 2025b] [Sinha et al. 2026] [Slater 2001] [Slater 2011] [Slater 2012] [Slater 2014] [Slater 2015] [Slater 2016] [Slater 2019] [Slater 2020] [Slater and Saunders 2011] [Smeltzer and Sorensen 1972a] [Smeltzer and Sorensen 1972b] [Smeltzer and Sorensen 1973] [Smeltzer et al. 1974] [Smith and Podleski 1994] [Soltani and Askari 2018] [Soltani and Farahani 2012] [Soltani et al. 2011] [Soltani et al. 2016] [Soreide et al. 1997] [Sorensen and Bencze 1973] [Sorensen et al. 1974] [Sorensen et al. 1976] [Sorrells et al. 1984] [Sorrells et al. 1985] [Soto and Hernandez 2004] [Stanitz 1948] [Stitt et al. 1956] [Stroud 1952] [Stubbs 1956] [Study of Supersonic Cavity 2004] [Sun et al. 2024] [sun et al 2026] [Surber 1975] [Surber and Robinson 1983] [Surber and Sedlock 1978] [Surber and Sedlock 1979] [Suryanarayana et al. 2022] [Sussman 1968] [Syberg and Koncsek 1975b] [Syberg and Koncsek 1975a] [Syberg et al. 1981] [T-4 Inlet/engine Compatibility Flight 1989] [Tabanli and Yuceil 2015] [Taghi-Abad et al. 2026] [Takasaki et al. 1998] [Tao et al. 2008] [Tao et al. 2009] [Tekaslan et al. 2021] [Three-Dimensional Viscous Design Methodology 1986] [Tinapple and Surber 2012] [Tindell 1980] [Tindell 1981] [Titchener et al. 2012] [Trapier et al. 2006] [Trapier et al. 2007a] [Trapier et al. 2007b] [Trapier et al. 2008] [Trapier et al] [Trefny 2020] [Trefny and Wasserbauer 1986] [Trefny et al. 2014] [Tudosie 2017a] [Tudosie 2017b] [Tudosie 2018] [Tudosie and Prisacariu 2022] [Tudosie and PĂUnescu 2017] [Türkkahraman et al. 2024] [Utomo and Bura 2019] [Vadyak et al. 1987] [Valdivia et al. 2014] [Van Deusen and Mardoc 1972] [Dippold 2022] [Vargo and Weinstein 1957] [Vinogradov and Stepanov 2008] [Vinogradov et al. 1989] [Vinogradov et al. 2017b] [Vinogradov et al. 2017a] [Vohra 2024] [Voytovych and Merkle 2010] [Wagner et al. 2007] [Wagner et al. 2008] [Wagner et al. 2009b] [Wagner et al. 2009a] [Wagner et al. 2010] [Walter and Starkey 2016] [Wan and Guo 2007] [Wang et al. 2023g] [Wang et al. 2023b] [Wang et al. 2023e] [Wang and Zhao 2026] [Wang et al. 2021a] [Wang et al. 2022b] [Wang et al. 2023h] [Wang et al. 2023d] [Wang et al. 2023f] [Wang et al. 2023i] [Wang et al. 2025b] [Wang et al. 2025c] [Wang et al. 2025d] [Wasserbauer and Willoh 1968] [Wasserbauer et al. 1973] [Wasserbauer et al. 1996] [Webster and Bucy 1979] [Wegener 1977] [Weinstein 1952] [West and Bynum 2021] [Whalen and Wilcox 1956] [Williams and Hunt 1980] [Williams and Stevens 2006] [Wilson and Wright 1987] [Wilson and Zhang 2025] [Wittliff and Byrne 1951] [Woollett et al. 1974] [Wyatt and Hunczak 1947] [Xie et al. 2015a] [Xie et al. 2026] [Yaghmaee and Roberts 1986] [Yamamoto et al. 2020] [Yan 2013] [Yang et al. 2024a] [Yang et al. 2024b] [Yang et al. 2026] [Yeager and Gertsma 1958] [Young et al. 2005] [Yu et al. 2021] [Yuceil et al. 2009] [Zha et al. 1998b] [Zha et al. 1998a] [Zhang et al. 2018] [Zhong et al. 2023] [Zhong et al. 2024] [Zhu et al. 2020] [Zhu et al. 2026] [Zuo et al. 2016]

Aeroelasticity, flutter and divergence

The other cost of thinness. Flutter, divergence, control reversal and panel flutter. The thin wing pays for its wave drag in torsional stiffness, and this literature is where that payment is computed.

492 records. [2-D Prototypical Aeroelastic Wing 2013] [2-D Prototypical Aeroelastic Wing 2018] [3-D Prototypical Aeroelastic Wing 2013] [3-D Prototypical Aeroelastic Wing 2018] [A Parametric Sensitivity 1991] [A Study 1973] [Abbas et al. 2011] [Abdel-Motagaly et al. 2003] [Abdel-Motagaly et al. 2005] [Abou-Amer 2020a] [Abou-Amer 2020b] [Abou-Amer et al. 2020] [Abzug and Larrabee] [Aerodynamic and Static Aeroelastic 2014] [Aeroelasticity and Loads Models 2014] [Aircraft Flutter Control System 2011] [Akshayraj and Ramakumar 2023] [Akshayraj and Sriram 2022] [Alag et al. 1986a] [Alcorta et al. 2023] [Ali and Hamed 2023] [Ali Tewfik et al. 2013] [Alyanak and Pendleton 2014] [Alyanak and Pendleton 2017] [Amirzadegan et al. 2019] [Amoozgar and Irani 2012] [Andersen et al. 1996] [Andersen et al. 1997] [Anderson 1968] [Armstrong et al. 2006] [Asadi and Farsadi 2020] [Asher et al. 1957] [Ashley 1980] [Awadalla Ali Haj Ahmed 2024] [Bae and Lee 2002] [Bae et al. 2002] [Balakrishnan 2006] [Balakrishnan 2007] [Basta et al. 2021] [Belesiotis-Kataras and Timme 2021] [Belubekyan and Martirosyan 2016b] [Belubekyan and Martirosyan 2016a] [Bendiksen 1987] [Bendiksen 1992] [Bendiksen 1994] [Bendiksen 1999] [Bendiksen 2009] [Bendiksen 2015] [Bennett and Abel 1981] [Bennett and Batina 1989] [Bennett et al. 1988] [Bennett et al. 1989] [Berci 2017] [Bhat 2018a] [Bhat 2018b] [Bhatia and Beran 2018] [Bibin et al. 2012] [Binder et al. 2021] [Birchfield 1970] [Bismarck-Nasr 1993] [Blair and Weisshaar 1982] [Bochkarev and Matveyenko 2008] [Boo et al. 2015] [Borglund 2005] [Boris et al. 2011] [Borland and Rizzetta 1981] [Boyd 1977] [Bramsiepe et al. 2020] [Stanford and Jacobson] [Brown 1959] [Bureerat 2026] [Burken et al. 1986] [Byreddy et al. 2003] [Cabral et al. 2021] [Calligeros and Dugundji 1963] [Castravete and Ibrahim 2008] [Cavagna et al. 2009] [Cazier and Kehoe 1986] [Cella and Biancolini 2012] [Cestino and Iannuzzo 2026] [Chang et al. 2010] [Chedrik et al. 2004] [Chen et al. 1998] [Chen et al. 2002] [Chen et al. 2006a] [Chen et al. 2025c] [Cheng 2009] [Cheng et al. 2002] [Cheng et al. 2003] [Chipman and Malone 1977] [Chipman et al. 1982] [Chipman et al. 1983] [Cho and Chang 2001] [Chuban 2020] [Clarke et al. 2005] [Cole 1991] [Cole et al. 2003] [Collar 1946] [Craig 1971] [Craig 1973] [Crittenden et al. 1977] [Cunha-Filho et al. 2018] [D’Ewart and Robert F. 1958] [D’Vari and Baker 1999] [Dal’Carobo and Fensterseifer 2010] [Davis 1969] [Davis and Bendiksen 1993] [Dağlı et al. 2025] [De Gaspari et al. 2007] [Deangelis 1981] [Desmarais and Reed 1980] [Di Leone et al. 2021] [Dibley et al. 2005] [Dive Testing for Flutter 2003] [Djayapertapa and Allen 2002] [Doggett and Ricketts 1977] [Dowell 1964] [Dowell 1968] [Dowell 1970] [Dowell 1971] [Dowell 1996] [Dowell 1999] [Dowell and Bendiksen 2010] [Dowell et al. 2003] [Drachinsky et al. 2022] [Duan et al. 2003] [Dugundji 1965] [Dugundji 1966] [Dugundji et al. 1962] [Durvasula 1966] [Edwards 1992] [Edwards 1996] [Edwards 2008] [Edwards et al. 2009] [Eugeni et al. 2020] [Evaluation of Methods 1981] [Experimental Transonic Flutter Characteristics 1990] [Fagley et al. 2015] [Farhat 1998] [Farhat 2000] [Farhat 2001] [Farmer and Hanson 1976] [Farsadi et al. 2019] [Fazelzadeh et al. 2009] [Fazelzadeh et al. 2016] [Feldt and Herrmann 1974] [Fenwick and Allen 2007] [Filippou et al. 2024] [Flax 1986] [Forster et al. 1996] [French 1988] [Freudinger and Kehoe 1990] [Freydin et al. 2020] [Furuya and Fukuchi 2001] [Furuya and Fukuchi 2002] [Furuya et al. 2003] [Garcia and Guruswamy 1999] [Garrick and Reed 1981] [Gaspari et al. 2009] [Gennaretti 2024] [Ghalandari et al. 2022] [Ghosh and Raisinghani 1993] [Goland 1945] [Goland and Luke 1954] [Grauer and Boucher 2017] [Grauer et al. 2012] [Griffin 2006] [Guo and Mei 2002] [Guo and Mei 2003] [Guo and Mei 2006] [Guo et al. 2005a] [Guo et al. 2005b] [Guo et al. 2007] [Gupta 1976] [Gupta 2026] [Guruswamy and Goorjian 1982] [Guruswamy and Goorjian 1988] [Gwin 1974] [Hai Zhao et al. 2010] [Hajela and Glowasky 1991] [Hancock 1965] [He et al. 2014] [Heard 1965] [Heeg and Chwalowski 2017] [Heeg et al. 2018] [Hilger and Ritter 2021] [Holt and Lee 1973] [Holt and Strack 1961] [Hoshi et al. 2020] [Hou and Satyanarayana 2000] [Huang et al. 2017] [Huang et al. 2023] [Huttsell and Eastep 1989] [Hwu and Tsai 2002] [Ide and Ominsky 1990] [Ilie and Havenar 2023] [Imai et al. 2022] [Mahzan et al. 2013b] [Janardhan et al. 2003] [Jekabsons et al. 2002] [Jha and Chattopadhyay 1999] [Ji et al. 2026] [Jirasek et al. 2016] [Johns 1960] [Johns 1965] [Johns 1971] [Jones and Dubose 1953] [Jovanov and De Breuker 2015] [Jung and Reimerdes 2003] [Karpouzian and Librescu 1993] [Kawakami et al. 2007] [Keerthana and Harikrishna 2014] [Khudayarov 2010] [Kikuchi et al. 2026] [Kim and Lee 2001] [Kim et al. 2003b] [Klepl 1992] [Klyde et al. 2004] [Kodigaddi 2026] [Kolonay and Yang 1998] [Kornecki 1964] [Krause and Dinkler 1998] [Kudryavtsev 2014] [Kwon et al. 2005] [Kyser and Willis 1973] [Lai et al. 2014] [Lee 1994] [Lee et al. 2005] [Lee et al. 2006] [Lee-Rausch and Batina 1993a] [Lee-Rausch and Batina 1993b] [Lehman and Stearman 1977] [Lemley 1968] [Lesoinne 2007] [Li 2012] [Li and Pak 2015] [Li et al. 2010] [Librescu and Malaiu 1968] [Librescu and Simovich 1988] [Librescu et al. 2003] [Librescu et al. 2004] [Lin 2016] [Lin et al. 1996] [Ling et al. 2015] [Liu and Gao 2020] [Liu et al. 2025a] [Loginov and Makeev 2007] [Lokos et al. 2002b] [Lokos et al. 2002a] [Lokos et al. 2005] [Long et al. 2014] [Lorber and Carta 1991] [Lottati 1985a] [Lottati 1985b] [Lottati 1988] [Lu and Yeh 1993] [Luber 2018] [Lyubomirov and Yartsev 2015] [Machida et al. 2005] [Mahzan et al. 2013a] [Mallik et al. 2015] [Mallik et al. 2022] [Manan and Cooper 2008] [Mangalam et al. 2010] [Matsushita et al] [May et al. 2023] [Mazidi et al. 2011] [McHugh et al. 2021] [McTavish] [Mei et al. 2014] [Mei et al. 2017] [Mellquist and Bendiksen 2014] [Mellquist and Bendiksen 2015] [Melville 2002] [Melville and Gordnier 1998] [Merrett 2015] [Merrett 2016] [Merrett and Hilton 2011] [Micks 1950] [Miles 1962] [Ming-de 1984] [Miskin and Takahashi 2019] [Miyaji and Takegawa 2022] [Moosavi 2025] [Moosavi and Elasha 2022] [Moosavi et al. 2005] [Morino and Obayashi 2015] [Morris et al. 2008] [Morton and Beran 1995] [Mottershead and Cooper 2012] [Mukhopadhyay 1995] [Mullen 1979] [Murphy et al. 1976] [Muñoz and García-Fogeda 2022] [Myers et al. 1983] [NACA Conference on Aircraft 1957] [Nahas 1991] [Nam et al. 1998] [Nam et al. 2000] [Williams et al. 1977] [Yates et al. 1982c] [Appa and Smith 1988] [Striz and Venkayya 1990] [Nash et al. 1975] [Nash et al. 2025] [nazemizadeh et al 2023] [Ndebele 2025] [Newsom and Pototzky 1981] [Nguyen et al. 2016] [Noll and Huttsell 1978] [Noll et al. 1980] [Nonlinear Aerolasticity Continuum Theory 2007] [Norton 1989] [Okabe et al. 2013] [Oremland et al. 2017] [Otiefy and Negm 2010] [Otiefy and Negm 2011] [Ouyang et al. 2014] [Pagliuca and Forster 2022] [Pan and Cheng 1994] [Panel Flutter 1991] [Pany 2023] [Papadopoulos 1958] [Passive Wing/store Flutter Suppression 1982] [Patel and Lefas 2025] [Patel and Lefas 2026] [Patel and Zha 2021] [Pengelley and Wilson 1954] [Persoon et al. 1983] [Persoon et al. 1984] [Petre and Ashley 1975] [Petre and Ashley 1976] [Pierson 1972] [Piette et al. 1985] [Pines et al. 1955] [Platanitis and Strganac 2003] [Popescu 2002] [Poplingher and Raveh 2023] [Poplingher and Raveh 2024] [Prediction of Transonic Flutter 1981] [Pusch et al. 2019] [Qian and Guan 2012] [Qiao et al. 2018] [Qiao et al. 2019] [Randels 1954] [Raveh and Levy 2004] [Ribeiro et al. 2022b] [Ribeiro et al. 2022a] [Richards and Erickson 2019] [Righi et al. 2022] [Robinson] [Rocha Da Costa] [Rodden 1989b] [Rogers 1970] [Rosatelli et al. 2024] [Rose and Jinu 2016] [Ruhlin and Murphy 1981] [Ruhlin and Pratt-Barlow 1981] [Ruhlin et al. 1974] [Ruhlin et al. 1982] [Ruhlin et al. 1983] [Rymanova et al. 2023] [Rynaski et al. 1978] [Amirzadegan et al. 2017] [Sabari Vihar et al. 2023] [Safarov et al. 2026] [Safronov et al. 2023] [Safronov et al. 2024] [Saitoh et al. 1995] [Saitoh et al. 2012] [Sander et al. 1973] [Santos and Pegado 2019] [Santos] [Saunders 1963] [Scanlan 1948] [Schmidt 1991] [Schuster 1995] [Schwanz and Grimes 1980] [Selvam et al. 2002] [SenGupta 2024] [Sezawa et al. 1936] [Sezgin et al. 2023] [Sezgin et al. 2024] [Shao] [Sherwood 2007] [Shishaeva et al. 2015] [Shishaeva et al. 2022] [Shivaji et al. 2025] [Siegel 1972] [Silva and De Marqui Junior 2014] [Silva] [Sims and Carter 1981] [Singh et al. 2016] [Sodja et al. 2021] [Soistmann and Spain 1993] [Song et al. 2011] [Song et al. 2018] [Sorbilli et al. 2018] [Sotoudeh and Ferman 2019] [Squires 2004] [Srivastava et al. 2019] [Stanford 2021] [Stanford and Jacobson 2023] [Stanford and Jacobson 2024] [Stanford et al. 2024] [Stanford et al. 2026] [Static Aeroelasticity 2002] [Static Aeroelasticity 2005] [Static Aeroelasticity 2011] [Static Aeroelasticity and Flutter 2014] [Static Aeroelasticity 2014a] [Static Aeroelasticity 2014b] [Striz 1991] [Stubblefield et al. 2025] [Sun et al. 2026b] [Sundararajan 1971] [Tadi 2002] [Tamayama 2017] [Tamura and Yumitori 2024] [Tani et al. 1994] [Testing Relevant to Aeroelasticity 2014] [Theodorsen 1935] [Torii and Matsuzaki 1992] [Torrigiani and Berci 2021] [Kwon 2005] [Triplett 1979] [Triplett et al. 1973] [Tsushima et al. 2023] [Turner 1981] [Vedeneev 2005] [Vedeneev 2009] [Vedeneev 2012] [Vedeneev 2013] [Vedeneev et al. 2009] [Vedeneev et al. 2010a] [Vedeneev et al. 2010b] [Vindigni 2023] [Voracek 2007] [Voß and Klimmek 2023] [Wang et al. 2011b] [Wang et al. 2021d] [Wasmi et al. 2015] [Waszak 1996] [Waszak and Buttrill 1991] [Waszak and Srinathkumar 1992] [Weatherill and Zartarian 1958] [Weber et al. 1999] [Weisshaar 1973] [Weisshaar 1975] [Weisshaar 1978] [Weisshaar and Ashley 1974] [Weisshaar and Bohlmann 1987] [Winther et al. 1995] [Wu et al. 2025] [Xie et al. 2012] [Xie et al. 2015b] [Xiong and Yang 2001] [Xue and Mei 1992] [Xue and Mei 1993] [Xue et al. 1990] [Yaman and Dalmış 2026] [Yan et al. 2024] [Yang and Li 2022] [Yang and Sung 1977] [Yang and Wan 1978] [Yang et al. 2011] [Yates et al. 1982a] [Yates et al. 1982b] [Yates et al. 1983] [Ye et al. 2024] [Yoo et al. 2002] [Yu and Bose 2026] [Yu et al. 2014a] [Yu et al. 2014b] [Yuan et al. 2024] [Yurkovich 1996] [Zhang et al. 2008a] [Zhang et al. 2011] [Zhang et al. 2016c] [Zhang et al. 2024c] [Zhang et al. 2026b] [Zhang et al. 2026c] [Zhao et al. 2012b] [Zheng 2010] [Zhi et al. 2020] [Zhou et al. 1996] [Zhou et al. 2018] [Zhou et al. 2021b] [Zhu and Qiao 2009] [Zhu et al. 2022] [Zink et al. 2001] [Zink et al. 2004]

Roll damping, lateral-directional stability and handling qualities

The derivatives that set the coupling threshold. Damping in roll, lateral-directional stability, the Dutch roll and handling qualities. The NACA damping-in-roll reports that this article cites for the thin planform sit here, with the handling qualities literature that uses the same derivatives.

484 records. [Abbott and Dietrich 1977] [Abed 1989] [Abed] [Abramov et al. 2005] [Abzug 1999a] [Abzug and Larrabee 2002] [Abzug and Larrabee] [Abzug and Larrabee] [Abzug and Larrabee] [Abzug and Larrabee] [Abzug and Larrabee] [Abzug and Larrabee] [Abzug and Larrabee] [Adams 1972] [Addendum 3 Lateral Control 2000] [Air Force Flight Test Center Edwards AFB CA 1974a] [Air Force Flight Test Center Edwards AFB CA 1974b] [Air Force Test Pilot School Edwards Afb Ca 1990b] [Air Force Test Pilot School Edwards Afb Ca 1990a] [Air Force Test Pilot School Edwards Afb Ca 1991] [Aircraft Lateral-Directional Handling Qualities 2011] [Aircraft Response Transfer Functions 1997] [Aircraft Response Transfer Functions 2013] [Aircraft Stability and Control 2026] [Aircraft Stability Derivatives 1998] [Alexander 1970] [Alighanbari 2002] [Ananthkrishnan 2004] [Ananthkrishnan and Sinha 2023] [Anderson et al. 1972] [Anderson et al. 1973] [Anderson et al. 1984] [Andrews and Rediess 1959] [Ankenbruck 1946] [Arnold 1942] [Ashkenas 1965] [Asim et al. 2022] [Averett 1980] [Baber and Moul 1955] [Babister 1980] [Ball and Smith 1956] [Barrows 1976] [Barrows 1977] [Bazile and Calderara 2012] [Beilman 1972] [Bengtson et al. 1975] [Berdon et al] [Berkowitz 1950] [Berman 1956] [Berry and Gilyard 1973] [Berry and Powers 1970] [Berry et al. 1976] [Beyers and Ericsson 2002] [Biber 2017] [Bielat and Wiley 1959] [Bischoff and Palmer 1982] [Bischoff and Palmer 1983] [Blair 1985] [Blake et al. 2009] [Blank 1995] [Bloy and Lea 1995] [Bohlmann et al. 1988] [Bollech and Kelly 1954] [Boothe 1971] [Boyden 1971] [Brandeau 1978] [Brandon et al. 1995] [Brincklow and Hunsaker 2021] [Brincklow et al. 2021] [Brincklow et al. 2024] [Brown and Repko 1962] [Bruner 1983] [Burns 1965] [Burt 1975] [Butler 1976a] [Canin 2019] [Canoro and Kelly 1955] [Cavanaugh 2003] [Cecrdle 2011] [Chalk 1983] [Chandrashekar and Kiran 1981] [Chapter 10. Natural Motions 1994] [Chen et al. 2026c] [Chin et al. 1987] [Chiplunkar et al. 2016] [Ciliberti and Nicolosi 2025] [Cohen 1944] [Cook 1946] [Cooksey et al. 1964] [Costigan and Calico 1989] [Crabill 1956] [Croom et al. 1993] [Cunningham et al. 2018] [D’Aiutolo and Henning 1955] [Davari and Laitone 1977b] [Davari and Laitone 1977a] [Davidson and Andrisani 1996] [de Melo et al. 2024] [de Paula et al. 2017] [Deak and Johnston 1973] [DeLaurier 2022] [Della Vecchia et al. 2015] [Demetriades 1983] [Development of Longitudinal 2014] [Development of Longitudinal 2024] [DiCesare 1961] [Doko and Sasongko 2026] [Dollyhigh 1974] [Dress et al. 1994] [Driver 1958] [Driver 1960] [Dungan and Clark 1994] [Dynamic Lateral-Directional Stability Theory 2003] [Dynamic Longitudinal Stability Flight 2003] [Dynamic Stability and Control] [Edmondson 1950] [Effect of Sweep Angle 2019] [El Aziz et al. 1993] [El-Ramly et al. 1976] [Ericsson 1995b] [Ericsson 1996b] [Ericsson 1996a] [Ericsson 1997a] [Ericsson 2001] [Ericsson and Hanff 1994a] [Eulrich and Mesiah 1974] [Eulrich et al. 1978] [Fazelzadeh et al. 2010] [Fisher 1951] [Fisher and Williams 1958] [Flight Dynamics of Elastic 2014] [Fossier et al. 1950] [Foster and Morris 1960] [Foster et al. 1993] [Fouda and Taha 2022] [Franklin 1971] [Frazier 1991] [Fremaux et al. 1993] [Fung 1954] [Gapcynski and Landrum 1958] [Garcon et al. 2003] [Gatto 2009] [Gera and Bosworth 1987] [Ghosh et al. 1998] [Gillis and Chapman 1956] [Gillis and Toll 1962] [Gilyard et al. 1972] [Gite and Deodhar 2020] [Go 2009] [Goldsmith 1964] [Gordiner 1995] [Goud and Dwivedi 2022] [Grana and Shanks 1952] [Gratton 2014] [Gratton 2018] [Green 2008] [Greenberg and Sternfield 1943] [Greenberg and Sternfield 1944] [Greene 1957] [Greenwell 2004] [Grenestedt 2008] [Grenestedt et al. 2006] [Grismer and Jenkins 1997] [Grosser 1965] [Gu 1986] [Guan 2013] [Hacker 1977] [Hacker 1978] [Hall and Boothe 1972] [Harmon 1948] [Harmon 1949b] [Harmon 1949a] [Harmon and Jeffreys 1950] [Hart 1968] [Hart and Picha 1979] [He et al. 2020] [He et al. 2021] [Heinle 1950] [Hess and Hess 1997b] [Hewes 1951] [Hockman and Eisiminger 1948] [Horne et al. 1960] [Huang et al. 2002] [Hyde et al. 2011] [Iloputaife and Ma 1987] [Jacobs 1983] [Jategaonkar and Plaetschke 1988] [Jeans et al. 2012] [Jenke 1976] [Jenkins et al. 1996] [Jiang et al. 2000a] [Johnson 1935] [Jones 1950b] [Jones 1976a] [Jones and Alksne 1949] [Jones and Alksne 1951] [Jones and Nisbet 1976] [Jones et al. 1948] [Jones et al. 1949] [Joshi and Rickard 1981] [Kamal et al. 2015] [Kanneganti et al. 2022] [Karpouzian and Librescu 1992] [Katz and Levin 1991] [Kehrer 1964] [Kempel et al. 1975] [Khot et al. 1996b] [Khot et al. 1996a] [Khot et al. 1997a] [Khot et al. 1997b] [Khot et al. 1998b] [Khot et al. 1998a] [Khot et al. 1999a] [Khot et al. 1999b] [Khot et al. 2000] [Kidd 1988] [Kim and Song 2013] [Klausmeyer 2026] [Klyde et al. 1995] [Kohlman 1967] [Kowalska and Goetzendorf-Grabowski 2022] [Kuzina] [Laguardia et al. 2017] [Lan and Hsu 1982] [Lan et al. 2006a] [Lan et al. 2008a] [Lapins et al. 1982] [Larson 1986] [Larsson and Enqvist 2016] [Lateral Control Power Rolling 2003] [Lateral-Directional Dynamic Modes 2016] [Lateral-Directional Dynamics 1998] [Lateral-Directional Flying Qualities 2002] [Lateral-Directional Motion 2016] [Lateral-Directional Stability Theory 2003] [Lebacqz et al. 1974] [Lee and Brown 1997] [Lee and Yoon 2008] [Lerro et al. 2020] [Li 1951] [Li et al. 2023a] [Lichota and Lasek 2013] [Linehan and Mohseni 2016a] [Linehan and Mohseni 2017] [Liu et al. 2026a] [Livneh 1995b] [Livneh 1995a] [Longitudinal and Lateral Linear 2014] [Lopatin 2012] [Loshelder and Su 2026] [Lowenberg 2010] [Luckert 1973] [Luu and Ochi 2023] [Löbbe and Tekkaya 2018] [Makarov and Pavlenko 2016] [Malaek and Karimi 2008] [Malvestuto and Margolis 1950] [Malvestuto et al. 1949] [Margolis 1950] [Martin and Gerber 1953b] [Martin and Gerber 1953c] [Martz and Church 1951] [Masak 1965] [Maslov et al. 2011] [Mason and Ravi 1994] [McDaniel 2012] [McDearmon and Heinke 1953] [McDearmon and Jones 1956] [McKinney and Maggin 1944] [McLaud and Hansen 1977] [McMaster and Schenk 1973] [Metcalf 1936] [Michaelsen 1957] [Mikhail 1993] [Miller and Franklin 1968] [Mitcham et al. 1951a] [Mitchell and Hoh 1984] [Mitchell and Johnston 1980] [Moes et al. 1998] [Mohamed and Dongare 2021d] [Mohamed and Joy 2021] [Mohammed 2007] [Moore 1969] [Moore and Moore 2008] [Moreira et al. 2022] [Moszczynski et al. 2026] [Moua et al. 2008] [Moul and Brown 1959] [Moulton et al. 2024] [Murri et al. 1983] [Murthy 1981] [Musa et al. 2026] [Myers and Walsh 1988] [Brewer 1946] [Talmage and Reeder 1947] [Brown and Adams 1948a] [Brown and Adams 1948b] [Sandahl 1948] [Walker and Ballantyne 1950] [Malvestuto et al. 1950] [Tucker and Piland 1950] [Ribner 1951] [Sleeman and Morrison 1953] [Wetzel 1954] [Nae 2026] [Nagaraja et al. 1982] [Nardi 1970] [Matheny and Gatlin 1978] [Compton et al. 1983] [Alag et al. 1986b] [Owens et al. 2002] [Neal and Smith 1970a] [Neal and Smith 1970b] [Nelson and Berman 1953] [Nguyen 2008] [Nguyen and Tuzcu 2009] [Nicolosi et al. 2010] [Northrop Aircraft INC Hawthorne CA 1952a] [Oehman 1983] [Owens et al. 2007] [Palazzo and Spearman 1954] [Pan and Huang 2018] [Pan and Huang 2019] [Park et al. 2001] [Parker et al. 1991] [Pasley et al. 1973] [Pedreiro et al. 1999] [Pepper and Foster 1946] [Perkins 1969] [Peterson 2024] [Pettit and Grandhi 2003] [Pfenneberger 1966] [Pfenneberger 1967] [Phillips 2000b] [Phillips 2000a] [Phillips and Santana 2002] [Phillips] [Piland 1949] [Pototzky 2014] [Price 1943] [Pushtaev 1989] [Pytka 2014] [Raghavan and Ananthkrishnan 2005b] [Raghavan and Ananthkrishnan 2023] [Ratnayake et al. 2011] [Ravi and Mason 1994] [Regan 1964] [Renita Sharon Monis et al and TJPRC 2019] [Reukauf et al. 1975] [Rhoads 1952] [Rhoads 1967] [Ribner 1950] [Ribner and Malvestuto 1948] [Rigid-Body Flight Dynamics 2026] [Rimer et al. 1984a] [Rimer et al. 1986] [Robinson 1957] [Rodchenko et al. 2002] [Rogal 1965] [Rolling Maneuvers 1996] [Rosenberg 1944] [Roysdon and Khalid 2010] [Roysdon and Khalid 2011] [Ruflin and Grantham 1984] [Russell 1996] [Hopko 1951] [Rustenburg 1973] [Ryu and Andrisani 2000] [Ryu and Andrisani 2003] [Sachs 1977] [Sadoff et al. 1954] [Sadraey 2022b] [Sadraey 2022a] [Sallee 1990] [Sanders 1951] [Sanders 1952] [Sanghi et al. 2020] [Satyanarayana et al. 1975] [Schmidt 1983] [Schnoebelen and Yechout 2003] [Schuman 2018] [Schwanz 1972] [Seacord 1943] [Seacord and Campbell 1943] [Seaver et al. 2023] [Seckel 1964c] [Seckel 1964a] [Seckel 1964b] [Seckel 1964d] [Sereez et al. 2018] [Shafer 1982] [Shah and Granda 1998] [Shearwood et al. 2021] [Shields and Mohseni 2012b] [Shields and Mohseni 2012a] [Shmilovich et al. 2023] [Shmilovich et al. 2026] [Shrivastava and Stengel 1989] [Simon et al. 1993] [Simsek and Tekinalp 2015] [Singh and Chowdhury 2021] [Singh and Jategaonkar 1996] [Singh and Raisinghani 1993] [Sinha and Ananthkrishnan 2002] [Siu et al. 2013] [Sivan 1971] [Sleeman 1953] [Sleeman 1957] [Smaili 2002] [Smith 1977] [Snell et al. 1991] [Snyder and Weisshaar 2013] [Solies 1995] [Song et al. 2014] [Spearman 1983] [Spearman and Driver 1956] [Spearman et al. 1956] [Spencer 1960] [Srivastava 1998] [Stalford 1979] [Static Flight Stability 2026] [Static Longitudinal Stability Flight 2003] [Static Stability and Control 1998] [Static Stability and Control] [Stenfelt and Ringertz 2009] [Stengel 1975] [Stengel 1980] [Stengel 2005] [Stengel and Miller 1978] [Sternfield 1949] [Stojakovic] [Sun et al. 2025] [Sun et al. 2026a] [Sura and Suryanarayan 2009] [Svorcan et al. 2024] [Swaim and Staab 1978] [Szymanski et al. 2025] [Takahashi and Gaydusek 2026] [Tavoularis 1999] [Taylor 1959] [Taşdemir 2022] [Taşdemir et al. 2021] [Teper and Stapleford 1965] [Thacker and Lan 1993] [The Stability and Control 1968] [Thomson 1947] [Thota et al. 2008] [Tian et al. 2016] [Ting et al. 2025] [Tischler 2018] [Tritschler and Dotson 2022] [Turner and Cooper 1948] [Ueno et al. 1998] [Valasek et al. 2017] [Van Dam and Holmes 1986] [Van Dyke et al. 1953] [van Es 1999] [Velger and Shinar 1983] [Vepa 2023c] [Vepa 2023b] [Vershinin 2004] [Vinh et al. 1988] [Vomaske et al. 1961] [Wang et al. 2021c] [Weingarten and Chalk 1982] [Weisshaar 1977] [Weisshaar and Zeiler 1982] [Wells et al. 1979] [Wells et al. 1981] [Wells et al. 1982] [Whipple and Ricket 1986] [Whoric 1973] [Williams et al. 2025] [Wilson et al. 1993] [Wilson et al. 1994] [Winograd and Miles 1956] [Wolowicz and Yancey 1973] [Woods-Vedeler and Pototzky 1992] [Woods-Vedeler et al. 1995] [Xiao et al. 2016] [Yang et al. 2003] [Zafar et al. 2017] [Zanette and Almeida 2015] [Zhanqi and Xi’an 2012]

Flight test measurement, system identification and mass properties

How the derivatives and the inertias are measured. Flight test instrumentation, air data, parameter identification and the measurement of mass properties. The swing and pendulum methods that establish an aircraft’s inertia appear here mostly as general metrology, as The Source Base sets out under Thin Subjects.

460 records. [Abbas Jessam 2012] [Abbate and Berner 1994] [Advisory Group for Aerospace Research and Development 1984] [Miley et al. 1992] [Air Force Test Pilot School Edwards Afb Ca 1990c] [Air Force Test Pilot School Edwards Afb Ca 1993] [Aircraft and Flight Test 2021] [Aircraft Moments of Inertia 1996] [Alford and Knarr 1999] [Alich and Castillo 2007] [Allwine et al. 2004] [Alyshev et al. 2016] [Ananthkrishnan and Sudhakar 1995] [Andrew and Polve 1952] [Appendix B Aircraft models] [Appich et al. 1980] [Arkwright et al. 2018] [Asselin 2021] [Atmaca et al. 2025] [Axelson 1975] [Axelson 1977] [Bach 1980] [Bach and Wingrove 1983] [Bach and Wingrove 1985] [Baer 1966] [Baer 2014] [Bagherzadeh et al. 2025] [Bai et al. 2019] [Basappa and Jategaonkar 2004] [Basappa et al. 2006] [Batterson and Klein 1984] [Bayoğlu et al. 2016] [Becker et al] [Beeler et al. 1956] [Bertrand et al. 2019] [Birk and Kuebrich 1981] [Bissell et al. 2023] [Black 1968] [Black 1969] [Bleimeyer 1981] [Bosworth and West 1986] [Bouton 1951] [Boylan et al. 1978] [Brinich 1961] [Brooks 1986] [Brooks et al. 1980] [Brunner 1996] [Bílek et al. 2025] [Cai 2024] [Callan 2012] [Carico 1998] [Carpenter et al. 1996] [Cenko 1994] [Cenko 1999] [Chamberlain 1968] [Chamberlain 1969] [Chase and McDonald 2014] [Chase] [Cheney 1988] [Cho and Nagati 1998] [Cho et al. 1995] [Chow et al. 1998] [Chowdhary and Jategaonkar 2006] [Chowdhary and Jategaonkar 2010] [Clark and Bernens 1991] [Cobleigh 1994] [Cole and Bennion 1956] [Colgren 1996] [Collins 2016] [Cook et al. 2004] [Crassidis 2005] [Croom et al. 1982] [Crowder 2018] [Cui et al. 2024a] [Cumming et al. 2007] [Cumming et al. 2008] [Dantsker et al. 2018] [Day and Guthrie 1958] [de Jong and Mulder 1987] [Debiasi et al. 2023] [Dehghan Manshadi and Saghafi 2021] [Demo 1986] [DeMoss and Simpson 2010] [Dias 2015] [Dias and Almeida 2013] [Dias and Girardi 2016] [Dix and Mattasits 1980] [Dods and Hanly 1972] [Dowling et al. 2006] [Dunlap and Porter 1971] [Durbin 1959] [Dusing and Orkwis 1993] [Dussauge et al. 2025] [Ellison and Latz 2003] [Emadian and Sajjadi 2026] [Eulrich and Rynaski 1980] [Fazeli et al. 2016] [Feng et al. 2020] [Fischenberg 1995] [Flaherty 1979] [Flight Test Instrumentation 1965] [Flight Test Manual 1959] [Flight Test Procedures for] [Fortis and Balint 2015] [Fosdick 1970] [Foss 1944] [Frederick and Ratnayake 2010] [Frederick and Ratnayake 2011] [Frederick et al. 2014] [Friehmelt and Jost 2000] [Frierson and Van Meter 1977] [Förder and Steiner 2020] [Gabl et al. 2021] [Garcia-Velo and Walker 1995] [Garoutte and Bryan 1983] [Gates et al. 1996] [Gebert et al. 2000] [Gee et al. 1990] [George et al. 2022] [Gera et al. 1981] [Gerlach 1965] [Ghosh and Raisinghani 2000] [Ghosh and Raisinghani 2002] [Ghosh et al. 2000] [Ghosh Roy and Peyada 2016] [Ghosh Roy and Peyada 2017] [Gilyard and Orme 1992] [Godwin et al. 1964] [Goodman and Conigliaro 1986] [Goupil] [Grafe et al. 2026] [Grauer 2021] [Grauer and Boucher 2018] [Grauer and Morelli 2013] [Grauer and Morelli 2023] [Grauer and Morelli 2025] [Grauer et al. 2017] [Green 1958] [Göttlicher et al. 2016] [Hagen and Seidel 1994] [Hagen and Seidel] [Han and Hong 2015] [Hanke 2003] [Harris et al. 1994] [Hegde et al. 2021] [Hemsch and Nielsen 1982] [Hensley 1994] [Hess 1986] [Hess et al. 1988] [Hessman 1982] [Hitzel 2017a] [Hofmann et al. 2025b] [Holmes and Woehr 1971] [Horton and McDaniel 2005] [Hosseini et al. 2025] [Wen et al. 2011] [Howland 1953] [Hui and Collins 2001] [Hull and Roger 1975] [Hulshoff et al. 1996] [Hur and Valasek 2003] [Iliff 1977] [Iliff 1987] [Iliff and Maine 1982] [Iliff and Maine 1983] [Ince 1967] [Incorporating Agility Flight Test 1994] [Ishikawa et al. 2007] [Ishikawa et al. 2008] [Ishimoto and Ishimoto 1997] [Jackson and Hoffler 2017] [Reynolds et al] [Jann and Yakimenko 2015] [Jardin and Mueller 2007] [Jardin and Mueller 2009] [Jategaonkar 2000] [Jategaonkar and Plaetschke 1989] [Jategaonkar and Thielecke 1994] [Jiang et al. 2009] [Johnson 1972] [Johnson and Adcock 1981] [Johnston and Hogge 1976] [Jordan 1974] [Kahn et al. 1972] [Kaletka and Fu 1993] [Kalkhoran and Otugen 1994] [Kannemans 1995] [Karam 1975] [Kerber 1927] [Khan et al. 2025a] [Kidd 1966] [Kim et al. 2003a] [Kim et al. 2010] [Kim et al. 2024] [Kimathi and Lantos 2024] [Kirschbaum 1936] [Klaus 2017] [Klein 1978] [Klein 1989b] [Klein 1989a] [Klein 1990] [Klein and Morelli 1992] [Klein and Murphy 2001] [Knoedler et al. 1996] [Komendat and Crassidis 2012] [Korr and Hyer 1962] [Kruggel et al. 1999] [Krumenacker and Pellicano 1992] [Kuester et al. 2016] [Kumar and Ghosh 2011] [Kumar and Ghosh 2017] [Kumar and Ghosh 2018a] [Kumar and Ghosh 2018b] [Kumar and Ghosh 2023] [Kumar et al. 2013] [Kusakin 1980] [Kwak et al. 2006] [Kwiek et al. 2022] [Laban and Masui 1993] [Lackey and Hadfield 1992] [Lai et al. 2021] [Lamy 1983] [Lanser 1994] [Large et al. 1981] [Lawrence and Mills 2002] [Layton and McTigue 1969] [Lee and Nagati 1999] [Lee et al. 2017] [Lee et al. 2025] [Lesieutre et al. 1996] [Leung et al. 2019] [Leventhal et al. 1977] [Li et al. 2007] [Li et al. 2021a] [Lichota et al. 2017] [Lightweight Low-Cost Flight Test 2007] [Lim et al. 2000] [Liu et al. 2016a] [Londono and Leonhardt 2012] [Longitudinal Control and Trim 2003] [Lovejoy 2026] [Ma and Chen 2020] [Magill et al. 1994] [Maine 1977] [Maine and Iliff 1979] [Maine and Murray 1986] [Malcolm et al. 1989] [Mannai 1962] [Manshadi and Saghafi 2018] [Marshall and Schweikhard 1973] [Martin 1996] [Martínez Morán 2018] [Matheny 1950] [Maunder 1979] [McCracken and Jorris 2011] [McCrink and Gregory 2017] [McGann 1995] [Meinicke and Cesnik 2026] [Menon et al. 2013] [Methods for Reducing Data 2003] [Metodiev 2024] [Metz 1992] [Meyersburg 1968] [Miller 1973] [Milne and Martos 2012] [Miniaturised Inertia! Measurement Unit 2005] [Minkler 1975] [Modi and Ananthkrishnan 1998] [Moes and Whitmore 1991] [Mohamed and Dongare 2018] [Mohamed and Dongare 2021b] [Mohamed and Dongare 2021a] [Mohamed and Dongare 2021e] [Mohamed and Dongare 2021c] [Moorhouse 1990] [Morelli 2006] [Morelli 2021] [Morelli 2022] [Morelli and Klein 1995] [Morelli and Smith 2008] [Morelli et al. 2005] [Morris 1964] [Moszczynski and Grant 2017] [Moul and Taylor 1980] [Murphy and Klein 2008] [Murphy and Klein 2010] [Murphy et al. 2011] [Mwenegoha et al. 2019] [Nagel and Thomas 1965] [Napolitano et al. 1994] [Napolitano et al. 2001] [Chin et al. 2015] [Neal 1970] [Neto et al. 2009] [Nicolosi et al. 2015] [Nicolosi et al. 2018] [O’Donnell and Mohseni 2018] [Obermark 2004] [Oelker and Friehmelt 1998] [Ogburn et al. 1988] [Ogburn et al. 1991] [Ogburn et al. 1993] [Ogren et al. 1974] [Omran and Newman 2010] [Ozger 2013] [Pal and Gaberson 1973] [Palomino 2022] [Pan et al. 2010] [Parameswaran et al. 2003] [Paris and Alaverdi 1998] [Park 1977] [Park 2011] [Parker et al. 2022] [Pattinson et al. 2013] [Pawlak 1994] [Peake et al. 1981] [Pearson 1937] [Pedreiro et al. 1996] [Pedreiro et al. 1998] [Pegram and Anemaat 2000] [Pelikan 1983] [Performance Evaluation by Flight 1995] [Petersen 1981] [Peyada and Ghosh 2009] [Planeaux and Barth 1988] [Platou 1968] [Platz and Bounajem 1992] [Porter 1965] [Previati et al. 2012] [Pusztai et al. 2024] [Quast et al. 1990] [Quinn 2022] [Dhayalan et al. 2018] [Raab 2014] [Raisinghani and Adak 1983] [Raisinghani and Ghosh 2002] [Raisinghani and Kumar 1995] [Raisinghani et al. 1999] [Ramachandran and Wells 1974] [Ramachandran and Wells 1975] [Raol and Jategaonkar 1995] [Raol and Singh 2023] [Rasmussen 1968] [Rediess and Melton 1994] [Regenie et al. 1992] [Ricciardi and Minwalla 2016] [Richwine and Del Frate 1995] [Richwine and Fisher 1991] [Ritter et al. 2020] [Roh et al. 2006] [Rohlmann and Keye 2015] [Rom 1992] [Rooker 1970] [Roth et al. 2010] [Roy and Peyada 2019] [Saderla et al. 2017] [Sakata 2002] [Salis Brasil Neto et al. 2006] [Saraswathi 2000] [Sarkar and Panneerselvam 1998] [Schafer 1962] [Schiff et al. 1980] [Schumacher 1952] [Seacord and Teitelbaum 1947] [Seanor] [Sehnert 1963] [Shafer 1980] [Shafer 1984] [Shortal and O’Sullivan 1962] [Simmons et al. 2023b] [Simmons et al. 2023a] [Simon and Blake 1999] [Simpson 1972] [Simpson 1979] [Singh and Ghosh 2006] [Singh and Ghosh 2007] [Singh and Ghosh 2013] [Singh and Ghosh 2023] [Singh et al. 2005] [Sitz et al. 1997] [Skarman 1978] [Smith and Pellicano 1992] [Sneshko et al. 2005] [Sogukpinar 2018] [Spaid 1984] [Srinathkumar et al. 1993] [Srinathkumar et al. 1995] [Starkey et al. 2012] [Stelmach 2012] [Stijnen 2026] [Stijnen et al. 2023] [Stouder 1981] [Symington 1940] [Tambova et al. 2026] [Tani 2003] [Tassanbi et al. 2026] [Taylor 2012] [The Measurement of Moment 2022] [Then and Chiang 1970] [Thomas 1973] [Travassos and Kaufman 1979] [Traven and Whitley 1995] [Turner 1950] [Turner 2003] [Tusharika 2015] [Ulbrich 2010] [Unsteady Surface Pressure Measurements 1985] [Usha et al. 2023] [Valasek and Walchli 1998] [Valenti and Stanton 2024] [Vallone] [Van Pelt 1981] [Vasconcelos et al. 2011] [Vatsa et al. 1987] [Verma and Peyada 2018] [Verma and Peyada 2020] [Vermeersch et al. 2015] [Vincent and Franklin 1981] [Vincent et al. 1979] [Véras et al. 2022] [Wages 1971] [Walker 1973] [Wang 2024] [Wang et al. 2022a] [Wang et al. 2016c] [Wang et al. 2020c] [Wang et al. 2021b] [Wang et al. 2022d] [Wang et al. 2023a] [Wang et al. 2026c] [Ward 1968] [Waszak and Fung 1996] [Wells and Banda 1981] [Wells and Klein 1982] [Whitmore et al. 1990] [Widayati et al. 2019] [Wilcox et al. 2004] [Wilson 1973] [Wilson] [Wingrove 1972] [Winski et al. 2023] [Winston] [Wissler 1981] [Wolf and Bossert 2001] [Wolowicz and Yancey 1974] [Woolf 2008] [Woolf 2012] [Wu et al. 2013] [Wulff and Zoellner 1991] [Xu et al. 2020] [Yang 2021] [Yasue 2020] [Youmin et al] [Youmin Zhang et al] [Zeis et al. 1988] [Zhang et al. 2015b] [Zhao 2011] [Zhao et al. 2012a] [Zhou and Wu 2025] [Özger 2012]

Turbojets, afterburning and installed thrust

The engine the aircraft received rather than the one it was designed for. Turbojet cycles, afterburning, altitude performance, installed thrust and the bookkeeping that separates thrust from drag.

337 records. [Jain 2025] [A Means of Testing] [Aarnes and White 1975a] [Aarnes and White 1975b] [Abbas and Riggins 2016] [Abdulhamitbilal et al. 2022] [Adrion 1951] [Advanced Ducted Propulsor In-Flight] [AERO-ENGINE DEVELOPMENT 1940] [Aiken and Wiener 1955] [Aircraft and Engine Development 1986] [Aircraft Engine Efficiency 2018] [Aircraft/Engine System Constraint Analysis 2018] [Aircraft/Engine System Mission Analysis 2018] [Airfoil Static-Pressure Thrust 1990] [Akbas et al. 2026] [Al-Amari et al. 2022] [Alberto Misté and Benini 2014] [ALTITUDE GRAPHS Aircraft Engine] [Altitude Graphs Aircraft Reciprocating] [Anderson 1990] [Anderson and Manty 1978] [Andrei et al. 2017a] [Andrei et al. 2017b] [Appendix E 2002] [Atay and Kumartaslioglu 2024] [Atkinson and McClelland 1968] [Auman 1993] [Azzabi and Elmahmodi 2012] [Babu 2021] [Baer-Riedhart 1982] [Baklanov 2013] [Balli 2014] [Balli 2017] [Balli 2020] [Barnhart 1989] [Beattie 1980] [Beeton 1966] [Bellman and Hughes 1968] [Beneda 2021] [Benek et al. 1996] [Benson et al. 1976] [Berens 2010] [Berrier 1983] [Bezborodova and Filinov 2021] [Bigarella 2025] [Binkley et al. 2015] [Blaha 1969] [Blankson and Hagseth 1993] [Bloomer et al. 1953] [Boppe 1984] [Bridges 2008] [Briggs 1986] [Bristol Siddeley Viper Mark 1963] [Brodersen 2002] [Brodersen and Stuermer 2001] [Brodersen] [Broggiato et al. 2012] [Brown 1978] [Burcham and Batterton 1976] [Burcham et al. 1983] [Burcham et al. 1990] [Bursey and Dickinson 1990] [Caddy and Arnold 1988] [Calder and Gupta 1978] [Caminez 1931] [Campbell 1973] [Capone and Deere 2001] [Carlson et al. 1984] [Cassetti 1978] [CFD Applications to Engine/Airframe 1986] [Chapel 1996] [Chen et al. 1990] [Climbing Flights of Turbojet 1995] [Coe 1976] [Colbert et al. 2023] [Conners and Sims 1998] [Conners et al. 2005] [Conrad and Campbell 1953] [Conrad and McAulay 1951] [Conway and Johansson 2001] [Corda et al. 2001] [Covert 1984] [Cui et al. 2024b] [Culy 1995] [Cyrus et al. 1999] [Davis et al. 1999] [Davis et al. 2008] [Davison 1963] [Denney et al. 2012] [Derbel and Beneda 2025] [Destarac and van der Vooren 2004] [Dix and Smith 1971] [Domingos et al. 2024] [Dommasch et al. 1959] [Due 1987] [Early 2000] [Ehyaei et al. 2013] [El-Sayed 2026] [Elements of Computational Engine/Airframe 1986] [Engine/Airframe Performance Matching 1989] [Ezrokhi et al. 2020] [Fawal and Kodal 2021] [Feifel and Kerkam 1992] [Feig and Gilkey 1991] [Filinov and Bezborodova 2021] [Fitzsimmons et al. 1978] [Fleming and Wilsted 1953] [Fleming et al. 2004] [Ford 1993] [Friedlander 2018] [Fu et al. 2024] [Gaglio et al. 2021] [Gedeon and Takahashi 2014] [Glasgow 1973] [Glasgow 1974] [Goetz et al. 1976] [Goulos et al. 2021] [Gravelle] [Grund and Konarski 1971] [Gu et al. 2017b] [Gu et al. 2026] [Gubanov 2019] [Güllü and Aran 2023] [Habibniarami et al. 2026] [Hahn 2012] [Hamilton and Welge 1992] [Hazen 1941] [Henderson 1987] [Henderson 1990] [Henderson 1991] [Herrick 1986] [Herrington et al. 1966] [Herrmann 1996] [Hiley and Bowers 1981] [Hinz and Miller 1979] [Holzman et al. 1996] [Hunczak 1952] [Hunt and Gowadia 1981] [Hurley 1951] [Hutchinson et al. 2021] [Imrak et al. 2021] [In-Flight Thrust Determination for] [In-Flight Thrust Determination] [Inoue et al. 1991] [Investigations of Propulsion Integration 1992] [Ishihara 1995] [Jaeger et al. 2026] [Jet Thrust Measurement 2003] [Kamei 1960] [Karaselvi and Nikbay 2021] [Khalid 1989] [Kislov and Shevchenko 2021] [Kitowski 1992b] [Klein and Abeykoon 2015] [Kodera et al. 2000] [Korsun et al. 2017] [Kuroda 1993] [Kutney 2007] [Lacy 1968] [Lamb 1999] [Lane 1966] [Lane and Behenna 1990] [Langtry et al. 2004] [Langtry et al. 2005] [Pratt and Whitney Aircraft (United States) et al. 1960] [Laughrey 1969] [Lehrach 1987] [Lemmin 1986] [Li and Geiselhart 2024] [Li and Geiselhart 2026] [Li et al. 2000] [Li et al. 2024a] [Li et al. 2024b] [Li et al. 2026] [Lilley and Pengelly 1992] [Lilley and Pengelly 1993] [Liston and Small 1992] [Liu 1999] [Lukashevich et al. 2023] [Lyons 1952] [Mace and Nyberg 1992] [Mackintosh and Dawson 1979] [Macquisten and Dowling 1993] [Maier et al. 2022] [Maine et al. 1990] [Malone and Peavey 1999] [Mattingly 1989] [May and Richey 1979] [Mazurov and Takovitsky 2013] [McAulay and Kaufman 1953] [McGuigan 1970] [Mead 1925] [Meher-Hornji 1997] [Mercure 1996] [Migdal and Greathouse 1968] [Migdal et al. 1969] [Mikhail 1979] [Miller and Addington 2004] [Miller and Protopapas 1985] [Miller et al. 1979] [Mishler and Wilkinson 1992] [Mishra et al. 2023] [Misté and Benini 2013] [Mocquard] [Mohammed et al. 2022] [Moiseev 2000] [Morris et al. 1976] [Mueller et al. 2024] [Myers and Burcham 1984] [Reller and Dowman 1949] [Wallner and Jansen 1951] [Useller and Russey 1955] [Groesbeck and Peters 1958] [Biesiadny 1974] [Arnaiz 1975] [Andrews and Mackley 1976] [Johnsen and Cullom 1977] [Hanloser and Cullom 1979] [Stromberg 1981] [Burcham et al. 1995] [Martos et al. 2011] [Neville et al. 1992] [Nevo et al. 2025] [Nguyen et al. 2023] [Nichols and Heikkinen 2010] [Nichols et al. 2011] [Nichols et al. 2015] [Noori et al. 2010] [Murthy and Paynter 1986] [Olson et al. 1955] [Palmer 1956] [Palumbo et al. 2003] [Patel and Chudoba 2026] [Patel et al. 2018] [Peters 1985] [Phinney 1959] [Piccirillo 1998] [Pismennyi] [Powers and Robinson 1992] [Prat et al. 1997] [Prilliman and Francis 1980] [Pyle 1947] [Khaliulin et al. 2022] [Rajagopalan and Siddiqi 1985] [Rallabhandi and Mavris 2008] [Ramette and Corde 1992] [Rauh and Anders 1986] [Reed 1956] [Reed et al. 1982] [Renas et al. 1952] [Renas et al. 1953] [Requirements of a Commercial 1967] [Research Instrumentation Requirements 1974] [Richey et al. 1968] [Richey et al. 1976] [Richey et al. 1977] [Richey et al. 1983] [Rodgers 2004] [Rodriguez 2007] [Rosen 2001] [Rosenberg and Schuch 1983] [Roxbee Cox 1946] [Rudnitski] [Salay and Elliott 1996] [Sandstrom 1971] [Sanghi et al. 1998] [Schierman and Schmidt 1991] [Schkolnik 1993] [Schmidt et al. 1990] [Schweikhard and Berry 1974] [Sekar et al. 2021] [Sharp 1957] [Shen et al. 2006] [Sivo and Wanhainen 1958] [Sizing the Engine 2002] [Sizing the Engine 2018] [Skira 1999] [Smith et al. 1953] [Smith et al. 2004] [Sotheran 1987] [Steinmetz and Hines 1987] [Straight and Cullom 1982] [STRESS-CORROSION OF TITANIUM ALLOYS] [Su et al. 2025a] [Su et al. 2025b] [Subsonic/Transonic/Supersonic Nozzle Flows 1986] [Sullins and Billig 1987] [Swavely and Soileau 1972] [Sóbester 2010] [Tagashira et al. 2007] [Takahashi 2005] [Takahashi 2017] [Takashima and Lewis 1995] [Taylor 1971] [The Development of Anomaly 1997] [Thrust-Drag Accounting Methodology 1985] [Thrust-to-Weight Ratio and Wing 2024] [Time-Dependent In-Flight Thrust Determination] [Tinoco and Chen 1984] [Titanium Alloys for Aerospace 2012] [Toenskoetter 1984] [Tong 2020] [Tong 2023] [Tudosie 2024] [Turbofan and Turbojet Gas] [Turbojet and Turbofan Engines 1964] [Turbojet Engines 2022] [Turning Flights of Turbojet 1995] [Uncertainty of In-Flight Thrust] [Useller and Mallett 1954] [Van Valkenburg and Matthews 1950a] [Van Valkenburg and Matthews 1950b] [Vannelli 1955] [Vasu et al. 1951] [Walker et al. 1953] [Walters and Netzer 1978] [Wang et al. 2024a] [Wang et al. 2026b] [Ward and Neeley 1959] [Ward et al. 1975] [Watson 1953] [Weber 1975] [wei et al 2025] [White et al. 1983] [Williams 1965] [Wilson and Benson 1978] [Wilson and Wright 1977] [Wind Tunnel/Flight Test Correlation 1978] [Woll 1948] [Wooten et al. 1984] [Xingjian et al. 1985] [Yong et al. 2014] [Zengin and Tokgoz 2022] [Zhang et al. 2014c] [Zhang et al. 2015a] [Zhang et al. 2020b]

Inertia coupling, departure and loss of control

The finding the aircraft is remembered for. Inertia and roll coupling, departure, spin and loss of control. 30 of these titles name roll or inertia coupling outright, and 7 of them date from before 1960, so coupling named as such is a small part of a cluster whose bulk treats departure, spin and loss of control more generally.

337 records. [Neihouse and Klinar 1942] [Abed and Lee 1990] [Abzug and Larrabee] [Air Force Test Pilot School Edwards Afb Ca 1989] [Aircraft Wing Rock 2010] [Airplane Spin Testing 2003] [Akcal et al. 2018] [Altunkaya et al. 2025] [Ananthkrishnan and Sudhakar 1994] [Anderson 1984a] [Anderson 1985] [Anglin 1965] [Anglin 1977] [Araujo-Estrada et al. 2015] [Arnold 1987] [Avanzini and d 1996] [Avanzini and Matteis 1997] [Badrinarayanan and Anandaraj 2022] [Baghdadi et al. 2009] [Baghdadi et al. 2011] [Bajpai et al. 2008] [Bakker et al. 2025] [Bamber and House 1937a] [Bamber and House 1937b] [Bamber and House 1938] [Bateman 2010] [Belcastro 2012] [Belcastro and Foster 2010] [Belcastro and Jacobson 2010] [Belcastro et al. 2005] [Belcastro et al. 2016] [Berman 1947a] [Berman 1947b] [Berman 1948a] [Berman 1948b] [Berman 1948c] [Berman 1950b] [Berman 1950a] [Berman 1951] [Berman and Pumphrey 1950] [Berman and Wilson 1948] [Bigler 1986] [Bihrle 1951] [Bihrle and Barnhart 1982] [Bowman 1955b] [Bowman 1955a] [Bowman 1955c] [Bowman 1956a] [Bowman 1956b] [Bowman 1957] [Bowman 1958] [Bowman 1965] [Bowman 1966] [Bowman 1970] [Bowman and Healy 1958] [Bowman and Healy 1959] [Bowman and Healy 1960b] [Bowman and Healy 1960a] [Bowman et al. 1978] [Browman and Healy 1959] [Brown 2002] [Bunge and Kroo 2018] [Bunge et al. 2015] [Burk and Healy 1955] [Burk et al. 1977] [Butler and Langham 1978] [Bürki-Cohen and Sparko 2008] [Campbell et al. 2021] [Cao et al. 2020] [Carroll and Mehra 1982] [Casner 2010] [Casteel and Weyl 1970] [Cen et al. 2018] [Chaderjian 1992] [Chang et al. 2008] [Chang et al. 2016] [Charles et al. 2002] [Cheng et al. 2021] [Chevalier et al. 1974] [Cho and Nagati 1995] [Chung et al. 2019] [Comtois and Glaser 2010] [Covert and Vlajinac 1969] [Cox 2010] [Cox et al. 2012] [Craig and Romani 1993] [Crespo et al. 2012] [Crider 2010] [Crider and Foster 2012] [Cunis] [Cunningham et al. 2008] [Dantsker et al. 2017] [Das 2026] [Daughtridge 1946] [Daughtridge 1948] [Davis 1957] [De Castro et al. 2010] [Donaldson et al. 2012] [Dongmo 2011] [Donlan 1976] [Drake 1952b] [Engelbrecht et al. 2012] [Engelbrecht et al. 2013] [Ericsson 1997c] [Ericsson 1998] [Flight Experience with Two 1955] [Fremaux 1995] [Fremaux 1997] [Fresconi and Celmins 2018] [Fu and Liang 1993] [Gale 1948] [Gandhi et al. 2012] [Gawron and Jones 2002] [Gill et al. 2013] [Gillis 1957] [Go and Maqsood 2015] [Goldthorpe et al. 2010] [Gordon et al. 2009] [Grafton et al. 1974] [Grant et al. 2017] [Hacker and Oprişiu 1974] [Hale et al. 2015] [Hamel 1970] [Hamza et al. 2022] [Heald and Brassell 1976] [Healy 1952] [Healy 1958] [Hewes et al. 1958] [Holloway and Johnson 2008] [Holway 1966] [Holzinger and Cunis 2024] [Hong 1993] [Hreha and Lutze 1983] [Hreha and Lutze 1984] [Huang and Wu 2006] [Hultberg et al. 1988] [Hyde et al. 2018] [Inertia Coupling and Spin 2004] [Inertia Coupling and Spin 2015] [Iqbal 2003] [Ison 2017] [Moguel 2015] [Allred and Fleck 1992] [Jacobson 2010] [Ji et al. 2011] [Jiang et al. 2024] [Johnston and Hogge 1974] [Kamm 1942b] [Kamm 1942a] [Kamm 1945] [Keller et al. 2009] [Kelley et al. 2014] [Khatri and Subbarao 2024] [Khatri et al. 2013] [Klinar 1946] [Klinar 1947] [Klinar and Berman 1948] [Klinar and Gale 1949] [Klinar and Healy 1952] [Klinar and Healy 1955] [Klinar and Jones 1949] [Klinar and Lee 1953] [Klinar and Lee 1954] [Klinar and Lee 1955] [Klinar and Snyder 1948] [Klinar and Wilson 1950] [Klinar and Wilson 1951] [Knight 1928] [Kogler and Quam 1983] [Kostić et al. 2015] [Kwatny et al. 2008] [Kwatny et al. 2009] [Kwatny et al. 2010] [Kwatny et al. 2013] [Lan et al. 2008b] [Lawrence 1965] [Lee 1952] [Lee 1953] [Lee 1959] [Lee 1963] [Lee and Libbey 1961] [Lee and Wilkes 1954] [Leopold et al] [Li et al. 2021b] [Liaw and Song 2001] [Littleboy and Smith 1996] [Littleboy et al. 1997] [Liu and Grant 2010] [Loss-of-Control Mishaps in Revenue] [Nguyen et al. 1980] [Lyu et al. 2022] [Bamber and Zimmerman 1934] [Macdougall 1942] [MacDougall and Lichtenstein 1946] [Mahale and Ananthkrishnan 2006] [Majumdar et al. 2021] [Malan et al. 2016] [Malcolm 1978] [Malcolm 1979] [Malvestuto et al. 1947] [Marusak et al. 2000] [Matsushita et al] [Mayo and Nolan 1966] [McDonough and Kolmanovsky 2017] [McDonough et al. 2014] [Mehra and Carroll 1980] [Milward et al. 2019] [Mukherjee and Sinha 2016] [Scudder and Seidman 1935] [Hultz 1951] [Patton et al. 1979] [Day 1997] [Chambers and Hall 2003] [Belcastro 2014] [Belcastro et al. 2014] [Neihouse 1940] [Newman et al. 2014] [Nguyen 1979] [Nguyen et al. 2021] [Nguyen et al. 1979a] [Nguyen et al. 1979b] [Nial 1972] [Nie et al. 2015a] [Nie et al. 2015b] [Padovan et al. 1991] [Pamadi and Taylor 1982] [Patton 1980] [Pepoon 1943] [Pepoon 1944] [Phillips 1948] [Phillips and Anderson 2002] [Pinsky and Essary 1993] [Pinsky and Essary 1994] [Pitkin 1943] [Planeaux 1990] [Planeaux 1991] [Poolla and Ishihara 2015] [Pourtakdoust and Fazelzadeh 2003] [R. 1934] [Rafi et al. 2017] [Rafi et al. 2019] [Rafi et al. 2020] [Rafi et al. 2021] [Rafi et al. 2022] [Rajaram et al. 2017] [Rankin et al. 2008] [Raymer 1991] [Reehorst et al. 2010] [Report No. 441 1932] [Rhodeside 1986] [Rogalski et al. 2020] [Rohith and Sinha 2020] [Rose and Dan M. 1952] [Salahudden et al. 2021] [Scher 1947b] [Scher 1947a] [Scher 1947c] [Scher 1956] [Schlimm 2015] [Schmidt and Wright 1991] [Schneiter 1945] [Scudder 1933] [Scudder 1934] [Scudder 1935] [Scudder 1937] [Scudder and Miller 1932] [Seidman and McAvoy 1940] [Seidman and Neihouse 1937] [Seo et al. 2019] [Shams et al. 2023] [Sharpes and Carroll 1973] [Shen et al. 2019b] [Shen et al. 2018] [Shen et al. 2019a] [Shen et al. 2023] [Shumsky 2010a] [Sibilski and Wróblewski 2012] [Sidoryuk and Khrabrov 2019] [Sinha and Ananthkrishnan 2016] [Sinha and Ananthkrishnan 2021] [Sisk and Andrews 1955] [Skow et al. 1982] [Sliwa 1979] [Smaili et al. 2018] [Snyder 1947] [Snyder 1948] [Sparks and Moerder 2002] [Squires 2002] [Stone 1956] [Stone 1957] [Stone and Berman 1946] [Stone and Daughtridge 1948] [Stone and White 1948] [Stone et al. 1950] [Stough and Patton 1979] [Stough et al. 1987c] [Stough et al. 1987a] [Stough et al. 1987b] [Tang 2019] [Tanrikulu et al. 2000] [Tartaruga et al. 2018] [Taylor and Miller 1982] [Taylor and Pamadi 1983] [Temgoua Dongmo and Kwatny] [Thomas et al. 2005] [Thota et al. 2012] [Tinger 1987] [Tobak and Schiff 1975a] [Tobak and Schiff 1975b] [Tu et al. 2024] [Ud-Din and Yoon 2018] [Uribe Quintero et al. 2024] [Urnes and Smith 2011] [Vyalkov 2020] [Wadley et al. 2005] [Wang 2011] [Ward and Bennett 1974] [Weil and Day 1956b] [Weil and Day 1956a] [Weissman 1969] [Weissman 1972] [Weissman 1973] [Weissman 1975] [White 1947] [Xin and Shi 2016] [Xu et al. 2019b] [Xu and Zhang 2020] [Yang et al. 2002] [Yildiz et al. 2018] [Yildiz et al. 2019] [Zhang et al. 2019] [Zhao and Zhu 2016a] [Zhao and Zhu 2016b] [Zheng and Yang 2008] [Zheng et al. 2018] [Zhou et al. 2017] [Zimmerman 1936]

Takeoff, landing and the landing gear

The cost of the wing at low speed. Takeoff performance, landing loads, shock struts, tires and brakes, for an aircraft that needed 108 metres per second to leave the ground.

339 records. [A Guide to Landing] [A380 Landing Gear Test 2002] [Aaron et al. 2004] [Abu-Akeel 1968] [Abu-Akeel 1969] [Abzug 1999b] [Agrawal 1985] [Aircraft Brake Temperature Monitor] [Aircraft Brake Temperature Monitoring] [Aircraft Carbon Brake 1973] [Aircraft Flotation Analysis Methods] [Aircraft Flotation Analysis] [Aircraft Ground Flotation Analysis] [Aircraft Landing GEAR] [Aircraft New Tire Standard] [Aircraft TIRE Condition Monitoring] [Aircraft Tire Electrical Resistance] [Aircraft Tire Inspection] [Aircraft Tire Pressure Monitoring] [Aircraft Tire Retreading Practice] [Aircraft Tire Wear Profile] [Aircraft Tire-to-Wheel Performance Characteristics] [Aircraft Tires 2022] [Aircraft Wheels Brakes 2022] [Airfield Compatibility 2022] [Allen et al. 1962] [Allen et al. 1963] [Alroqi and Wang 2015] [An et al. 2022] [Anamet Labs INC San Carlos CA 1979] [Anderson 1973] [Aprovitola et al. 2021] [Attri and Amberg 1974] [Bai et al. 2022] [Bailey 1965] [Batill 1982] [Batill and Bacarro 1988] [Beachem 1964] [Beachkofski 1999] [Best 1986] [Black 1976] [BOECKH 1954] [Brake Systems, Wheel, Aircraft] [Brake Systems, Wheel, Military] [Brewer 1974] [Brewer 1975] [Brockman and Braisted 1994] [Brown and Redwine 1948] [Burgan and Paddison 1974] [Burkhardt 1943] [Cardoso Navarro and Sandoval 2019] [Cardoso Navarro and Sandoval Goes 2018] [Carter and Nagy 1995] [Castrichini et al. 2018] [Chandrasekharan 1988] [Chang and Ulbricht 2002] [Chen et al. 2021a] [Chester 1995] [Chevalier and Burke 1972] [Chevillot et al. 2009] [Claridge 1973] [Clark 1974a] [Clark 1984] [Cui and Li 2022] [Currey 1988] [Daughetee 1974] [Deakins and Blackburn 1965] [Design and Testing of] [Design Recommendations for Spare] [Dewispelare and Stager 1981] [Lopes and Ayala 2020] [Digges 1971] [Ding et al. 2018] [Di̇nç 2021] [Donaldson 1952] [Dongdong et al. 2025] [Douglas Aircraft Co Long Beach Ca 1962] [Ramasubramanian 2026] [Drake 1952a] [Duda et al. 2022] [Dunlop Limited 1972] [Dyko and Chung 1990] [Dyko and Vafai 1998] [Earl 1967] [Effects of Extremely Cold] [Enright 2000] [Estimating the Takeoff Wing 2010] [External Hydraulic Fluid Leakage] [Extraordinary and Special Purpose] [Fang et al. 2022] [Feather 1980] [Feria Alanis et al. 2024] [Ferrarese 1974] [Ford 1998] [Fu et al. 2013] [Gatt et al. 2017] [Gayman 1946] [Gibson et al. 1968] [Gordon et al. 1996] [Gordon et al. 1998] [Greenland 2021] [Grossman 1980] [Guan et al. 2017] [Guida 2023] [Guohui Chen et al. 2018] [Hao Zhang et al. 2018] [Hausknecht and Vaitys 1961] [Hidayat et al. 2018] [Ho 1978] [Ho and Peterson 1977] [Ho et al. 1979] [Horne et al. 1976] [Howell et al. 1986] [Hoy 1963] [Hui et al. 2008] [Huili et al. 2023] [Identification of Speed Brake 1994] [Jategaonkar et al. 1997] [Jebáček and Horák 2016] [Ji Teng and Shahneh 2018] [Jia et al. 2011] [Jiang and Cheng 2024] [Jiao 2018] [Johnson 1934] [Jones] [Joyner 1969] [Kahms and Wangenheim 2021] [Kamble et al. 2026] [Kang et al. 2021] [Kang et al. 2023b] [Kang et al. 2023a] [Kansas Univ Lawrence 1952b] [Kansas Univ Lawrence 1952a] [Karunanidhi et al. 2025] [Kilner 1982] [Kim 2023] [Knowles et al. 2012] [Kofman and Becus 1996] [Kraft et al. 1971] [Kroll 1956] [Kroll 1957] [Kuchinka 1966] [Landing GEAR - Aircraft] [Landing Gear Alignment] [Landing Gear Component Heat] [Landing Gear Fatigue Tests] [Landing Gear Shock Absorption] [Landing Gear Shock Strut] [Landing Gear Shock Strut] [Landing Gear Shock Struts] [Landing Gear Stability] [Landing Gear Structures and] [Landing Gear System Development] [Landing Loads 1996] [Latif G.A.L. Younes 2025] [Lee and Chiou 1994] [Lee and Swegle 1963] [Leland and Thompson 1975] [Leo et al. 2014] [Lernbeiss and Plöchl 2007] [Li et al. 2021c] [Li et al. 2025] [Lian et al. 2024] [Linnell 1963] [Liquid Brake System 1958] [Liu and Wang 2024] [Liu et al. 1996] [Liu et al. 1998] [Liu et al. 2014a] [Liu et al. 2016b] [Liu et al. 2023a] [Liu et al. 2025e] [Liu et al. 2025d] [Lockard et al. 2004] [Lu and Wang 2024] [Luo et al. 2024a] [Lystad 1975] [Maemori et al. 2003] [Maintainability Recommendations for Aircraft] [Maintainability Recommendations for Aircraft] [Margetts et al. 2013] [Matos and Cadete 2022] [Matranga and Armstrong 1959] [Mayo 1961] [McBrearty 1952] [McGehee and Dreher 1982] [McKay 2010] [McKay and Wilson 1968] [Medzorian 1992] [Meriwether and Harris 1962] [Mikułowski and Jankowski 2009] [Modal Analysis 2018] [Mohanty 2013] [Mosby 1965] [Kranz 1954] [McGehee and Carden 1976] [Howell et al. 1990] [Rudolph 1996] [Ni 2022] [Nicholas 2007] [null] [null] [null] [Ohme 2009] [Okada et al. 2023] [Ouellette 2025] [Overview of Aircraft Landing] [Oza et al. 2015] [Patel et al. 2017] [Payne 1968] [Pecora 2021] [Pi 1988] [Picard 2002] [Pilyugin and Khlebnikov 2005] [PiĽA et al. 2017] [Plain Bearing Selection for] [Plews 1983] [Podruzhin et al. 2021] [Policandriotes and Filip 2011] [Pond 1973] [Pond 1977] [Poole 2010] [Prem et al. 2025] [Pytka 2023b] [Pytka et al. 2019] [Pytka et al. 2022] [Ramachandra et al. 2026] [Recommended Practice for Landing] [Recommended Practice for Measurement] [Recommended Practice for the] [Rejected Takeoff Performance 2021] [Rejected Takeoff Performance Testing 2021] [Roberts and Wagner 1973] [Rook 2010] [Sadraey 2017] [Sadraey 2023] [Schmidt 2015] [Schmidt 2021] [Seidel and Haudrich 2024] [Шифрин 2004] [Sen 1990b] [Sen 1990a] [Sforza 2014] [Shevchenko 2018] [Shevchenko and Nachinkina 2018] [Shevchenko et al. 2019b] [Shevchenko et al. 2019a] [Shi 2019] [Shi et al. 2019] [Shives 1973] [Shixing et al. 2011] [Shu et al. 2020] [Shuhua Zhu et al. 2008] [Sivaramakrishnan 1981] [Skorupka et al. 2009] [Some Current Types 1968] [Sonowal et al. 2021] [Spiral Failure - “O”] [Stachiw] [Stalnov et al. 2013] [Stelmack et al. 1999] [Suharevs 2022] [Sun 2023] [Sun Jing et al. 2018] [Sóbester 2021] [Taherian 2026] [Take-off and Landing] [Takeoff and Landing 1997] [Takeoff and Landing Analysis 2010] [Takeoff and Landing Performance 1995] [Takeoff and Landing Theory 2003] [Takeoff Performance 2017] [Takeoff Performance 2021] [Takeoff Performance Testing 2021] [Tang et al. 2025] [Tanner and Stubbs 1977] [Taylor 1958] [Taylor et al. 2021] [Testing Aircraft Wheel Tyre 1973] [Tests, Impact, Shock Absorber] [Tian Jing and Ding Li 2010] [Tielking 1989] [Tire Pressure Monitoring Systems] [Titov and Serebryansky 2026] [Travis 2005] [Trifonov et al. 2024] [Trobaugh and Obrimski 1980] [Turnbull et al. 1952] [Unorthodox Landing Gears 1988] [Vaidyaraman et al. 2001] [Venkatesan 1977] [Verification of Landing Gear] [Vescelus 1952] [Viana et al. 2007] [Wahi 1979] [Wang 2022] [Wang and Cao 2026] [Wang and Zhu 2024] [Wang et al. 2007] [Wang et al. 2017c] [Wang et al. 2017b] [Wang et al. 2017a] [Wang et al. 2018] [Wang et al. 2023j] [Wang et al. 2024b] [Wang et al. 2025a] [Wang et al. 2026a] [Waring Brown 1934] [Waring-Brown 1948] [Watkins and Hammitt 1966] [Wei et al. 2014] [Wheel and Brake Design] [Wheel and Brake Design] [Wheel and Hydraulically Actuated] [Wheel Roll on Rim] [Wheel Roll on Rim] [White 1963] [Xiang et al. 2022] [Xiao et al. 2024] [Xue et al. 2012a] [Xue et al. 2012b] [Xue et al. 2014b] [Yang and Yanguang 2015] [Yang et al. 2016a] [Yao 2002] [Yu et al. 2020] [Zammit-Mangion and Eshelby 2008] [Zhang and Xue 2011] [Zhang et al. 2015c] [Zhang et al. 2021c] [Zhang et al. 2021a] [Zhang et al. 2022] [Zhang et al. 2025b] [Zhang et al. 2025a] [Zhang et al. 2026a] [Zhao et al. 2026a] [Luo and Voronko 2023] [Zhu and Wang 2025] [Çeliktaş et al. 2012]

Compressible flow, heating and the boundary layer

The relations behind the sizing. Shock relations, compressible boundary layers, skin friction, aerodynamic heating and the recovery temperature that decides whether titanium was needed at Mach 2.

296 records. [Abdelhamid 1985] [Abzug and Larrabee] [Advanced Fuel Research INC East Hartford CT 1957] [Aerodynamic Phenomena in Supersonic 2020] [Agrawal et al. 1989] [Agrawal et al. 1991] [Alford et al. 1966] [Allen 1981] [Amidon 1985] [Anderson 1958] [Appa and Smith 1973] [Apte and Athani 1979] [Armstrong 1979] [Army War Coll Carlisle Barracks Pa 1952] [Arnal and Reneaux 2001] [Baals and Harris 1968] [Baals et al. 1970] [Bai et al. 2015] [Bai et al. 2025] [Bartlett 1970] [Bashkin et al. 2005] [Batina 1986b] [Batina 1986a] [Batina 1988] [Batina 1989] [Bauer and McMillin 1988] [Bauer and Wood 1989] [Behera et al. 2020] [Bencze 1972] [Bennet-Clark 1972] [Beskin 1949] [Bhowmick et al. 2025] [Birch and Cleminson 2004] [Blair 1990] [Boelens 2017] [Bogdnoff 1953] [Boundary Layer Stability Analysis 1980] [Boyd 1965] [Briggs et al. 1982] [Brown 1961] [Brown et al. 1961b] [Bryson 1952] [Bryson and Edwards 1952] [Bushnell 1990] [Calarese and Walterick 1978] [Calarese and Walterick 1979] [Capey 1961] [Capone et al. 1984] [Capone et al. 2004] [Carafoli 1969c] [Carlsen 1995] [Carlson 1964] [Catalano and Sturek 2001] [Chapman and Rubesin 1949] [Chapter 4. Wing-Tail Plane 1957] [Chaussee 1978] [Chou and Smith 1974] [Choudhari and Streett 1990] [Chow and Goorjian 1982] [Chung 1973] [Clarke 1960] [Cohen 1951] [Cook 1964] [Cook 1965] [Cosenza and Kummeth 1974] [Couch 1972] [D. Supersonic and Transonic 1954] [Daniels and Hardy 1975] [Debiasi et al. 2010] [Dejarnette 1983] [Dejarnette et al. 1985] [Demetriades 1985] [des Clers and Sternberg 1952] [Donov 1956] [Drakin 1963] [Eckert 1956] [Effect of High Mach 2010] [Epstein 1954] [Erickson et al. 1989a] [Est and Nelson 1991] [Fano et al. 2020] [Fay and Riddell 1958] [Fedorov et al. 1997] [Fejer et al. 1964] [Ferrari 1948] [Ferrari 1958] [Fink 1971] [Fisher and Saltzman 1973] [Flat Wings in Inviscid 2020] [Fleeter and Riffel 1979] [Fletcher and Burns 1979] [Flores et al. 1992] [Florio et al. 2019] [Fluid Dynamics Research 1998] [Friend and Sakamoto 1978] [Gallagher and Capece 2004] [Galloway et al. 1992] [Gapcynski 1960] [Gardner et al. 1948] [Gardner et al. 1968] [Garriz et al. 1990] [Glauert 1928] [Goodman 1949] [Goshima et al. 2019] [Graham et al. 1954] [Graham et al. 1955] [Grigsby 1952] [Hallstaff 1966] [Han et al. 2023] [Harada et al. 2019] [Harri 1964] [Hendrickson et al. 1978] [Hermach et al. 1957] [Hitzel 2017b] [Hom et al. 1983] [Hong 1965] [Howell 1958] [Huerta 1969] [Huffman and Fox 1985] [Ilie and Sullivan 2020] [Influence of Wing Geometry 1989] [Item and Baysal 1995] [Janardhan and Grandhi 2003] [Jeong et al. 1998] [Jischke 1978] [Jones 1947a] [Jones 1961] [Jones 1967a] [Jones 1977] [Jones 1983] [Ooi 2024] [Katary 1983] [Kaye and Yeh 1955] [Kehrer 1971] [Khan et al. 2019] [Kim et al. 2002b] [Kim et al. 2006] [Krasilschchikova 1956] [Krieger 1980] [Runyan and Steers 1980] [Landers et al. 1997] [Lapygin and Tret’yakov 1986] [Lapygin and Yakunina 2009] [Le Fur 1959] [Lees 1956] [Lei et al. 2016] [Leontiev et al. 2017] [Leontiev et al. 2022] [Levin and Seginer 1982] [Li and Stewart 1953] [Li et al. 1999] [Li et al. 2018a] [Licher 1956] [Lindsey 1946] [Lobanovskii 1983] [Luo and Bao 1988] [Mackay and Nagamatsu 1954] [Madson and Ericksont 1985] [Maeno et al. 2017] [Maikapar 1966] [Maikapar 1993] [Mann and Carlson 1991] [Margolis and Elliott 1959] [Marshall 2000] [Martin 1950] [Mason 1983] [Mason et al. 1983] [Masud et al. 2018] [Mateescu 1986] [McConnell 2006] [McElderry 1973] [McMillin and Wood 1986] [Mele et al. 2017] [Meyer and Fields 1978] [Miele and Damoulakis 1969] [Miller and Schemensky 1979] [Miller and Wood 1983] [Minkiewicz and Bosmajian 1996] [Mirels and Haefeli 1949] [Moeckel and Evans 1951] [Moga 1980] [Moga and Dejarnette 1981] [Monis et al. 2016] [Murman and Cole 1974] [Murphy and Schmidt 1953] [Mysliwetz 1963] [Naamane and Hasnaoui 2019] [Ames Research Staff 1953] [NACA Conference on Aerodynamic 1947] [NACA Conference on Aerodynamic 1949] [Nangia et al. 2023] [Nastase 2008a] [Naval Ordnance Systems Command Washington DC 1957] [Neely et al. 2003] [Nenni and Tung 1971] [Northrop Aircraft INC Hawthorne CA 1952b] [Northrop Aircraft INC Hawthorne CA 1953b] [Oberkampf 1978] [Owens et al. 2004] [Owens et al. 2006] [Palaniappan and Jameson 2004] [Pfyl and Presley 1961] [Phythian 1966b] [Phythian 1966a] [Pindzola 1950] [Pittman 1987a] [Pittman and Bonhaus 1987] [Plaban and Takahashi 2021] [Prandtl 1928] [Price 1978] [Price 1981] [Pritchard 1969] [Properties and Design 2012] [Rahman et al. 2022] [Raveh 2011] [Readshaw 1961] [Reda 1977] [English and Carter 1960] [Scadron et al. 1950] [Scherrer 1951] [Schlichting 1939] [Seidel et al. 1985] [Seidel et al. 1987] [Send and Voß 1999] [Shrout 1977] [Smith and Dahlem 1981] [Soviero and Resende 1997] [Spearman 1986] [Spearman and Fournier 1978] [Spearman et al. 1977] [Spearman et al. 1992] [Squire 1967] [Starr 1978] [Stengel 1969] [Stengel 1970] [Stickney 1955] [Stine and Scherrer 1952] [Stojanović et al. 2024] [Stone 1945] [Sun and Oran 2018] [Sundén and Fu 2017] [Supersonic Aircraft 1997] [Supersonic Three-Dimensional Wing Theory 1960] [Supersonic Two-Dimensional Airfoil Theory 1960a] [Supersonic Two-Dimensional Airfoil Theory 1960b] [Supersonic Two-Dimensional Airfoil Theory 1960c] [Sutherland 1893] [Tabernaus et al. 2023] [Takovitskii 2020] [Technical Applications 1976] [Tetervin 1963] [Tewari 1993] [Thomas 1942] [Thomas 1949] [Thornton 1981] [Throckmorton and Stone 1974] [Tilmann 1998] [Token 1974] [Tokugawa and Yoshida 2006] [Transonic and Supersonic Flight 1992] [Transonic and Supersonic Flows 2012] [Triebstein 1986] [Tsay 2022] [Tsien 1955] [Tucker and Maslen 1951] [ИЛЮХИН and ЕГОРОВ 2024] [van Zyl 1994] [Varwig 1963] [Varwig and Rosenman 1966] [Vasil’chenko 1981] [Velden 1997] [Verdon 1974] [Viswanath 1988] [Voevodenko and Panteleev 1989] [Vrebalovich 1967] [Washington and Spring 1982] [Wasserman 1952] [Welge et al. 1976] [Welge et al. 1977] [White 1994] [Whitford 1988] [Whitford 1991] [Wilks 2006] [Wing Theory in Supersonic 1969] [Winkler 1954] [Wood and Miller 1984b] [Wood and Miller 1985b] [Wood et al. 1982] [Wortman 1970] [Xue et al. 2014a] [Yahalom 1971] [Yan 2012] [Yan et al. 2025] [Young and Kirkby 1955] [Yu et al. 1983] [Zhang et al. 2021b]

Flight loads, buffet and structural response

What the structure carries. Flight loads, buffet, strain-gauge measurement and structural response, which are the subjects of the X-3’s own tail-load, wing-load and buffet reports.

175 records. [Abraham-Doman and Merrett 2014] [Aiken 1948] [Aiken and See 1951] [Aircraft Internal Loads 2014] [Allen 1954] [Anderson 1947] [Anderson et al. 2004] [Aryasomayajula et al. 2001] [Austin and van Gaasbeek 1978] [Barnes and Defiore 1991] [Baum 1956] [Bean and Lee 1994] [Bean and Lee 1995] [Benton 2019] [Berens 1979] [Bergstedt et al. 1959] [Birks and Ludlow 1969] [Brewer 1953] [Brock 1977] [Buzzetti and Howland 1945] [Cenko and Madson 1993] [Cerantola et al. 2024] [Chestnutt 1966] [Choi 1967] [Clay 1961] [Clay 2004] [Clay and Berens 1964] [Clay and Rockafellow 1973] [Coetzee et al. 2013] [Cohen 1970] [Cole et al. 1990] [Cooney and Schott 1956] [Cooper 1990] [Cornette 1961] [Crawford and Finley 2000] [Cunningham et al. 1978] [Da Ronch et al. 2011] [Damstrom and Mayes 1970] [Damstrom and Mayes 1971] [Davis 1973] [Davis and Wornom 1958] [Deyoung 1971] [Dickinson 1953] [Disney 1966] [Edwards 2009] [Erickson et al. 1989b] [Fan et al. 2026] [Feldwisch and Bauer 2023] [Figge 1973] [Fikes 1977] [Flansburg 2008] [Fletcher et al. 2013] [Flight Studies 1944] [Flight-Loads Prediction and Structural-Life 1981] [Fornasier and Heiss 1987] [Fuchiwaki and Tanaka 2005] [Galway 1980] [Gamon 1979] [Ganti et al. 2026] [Garvin 1947] [Giessler and Nash 1971] [Gillan 1993] [Ground Manoeuvre Loads 2014] [Hallissy and Harris 1974] [Hamer et al. 1961] [Haskind and Falkovich 1950] [Hernandez et al. 2019] [Hewitt et al. 2005] [Hollingsworth and Cohen 1971] [Horizontal Tail Loads 1996] [Hosek et al. 1981] [Hwang and Pi 1975a] [Hwang and Pi 1975b] [Hwang and Pi 1979] [Igoe 1967] [Isakson 1957] [Israq et al. 2025] [James 1972] [Jeans and Tribble 1979] [Jenkins et al. 1977] [Jenkins et al. 1979] [Kandil et al. 1976] [Kaplan et al. 1979] [Kier 2005] [Kim 1999] [Kim and Marciniak 1998] [Kim and Marciniak 2000] [Kim and Marciniak 2002] [Kim et al. 2002a] [Kochin 1953] [Kuhl et al. 1958] [Lagemann et al. 2024] [Laitone 1978a] [Laitone 1978b] [Lee 1984] [Leone 2010] [Livne 1994] [Lone and Pontillo 2020] [Love 2003] [Lustig et al. 1960] [Mahlmeister et al. 1955] [Majumder and Rao 2007] [Malisani and Capello 2021] [Mann 1964] [Mansfield 1963] [Masud and Khan 2015a] [Megson 2010] [Megson 2013] [Megson 2017] [Megson 2018] [Megson 2022] [Minshall et al. 2017] [Montel and Thielecke 2015] [Moses 2005] [Moss et al. 1991] [Pearson and Aiken 1946] [Nanda et al. 2022] [Peele and Eckstrom 1975] [Hoy 1976] [Nayfeh and Mook 1978] [Nicolas et al. 2016] [Niculescu et al. 2021] [Norton 1923] [Norton 1990a] [Norton 1990b] [Norton and Bacon 1921] [Norton and Brown 1923] [Olwi 1995] [Pearson et al. 1950] [Pearson et al. 1951] [Pechaud and Kim 2001] [Peng et al. 2024] [Perry and Rievley 1961] [Petersson et al. 2010] [Philipsen and Zhai 2007] [Preisighe Viana 2025] [Raab and Rohde-Brandenburger 2020] [Rafiq and Qureshi 2022] [Rakin 1981] [Raveh 2008] [Raveh and Karpel 1999] [Rayhan and Islam 2019] [Reschke 2005] [Rodden 1972] [Rokhsaz and Kliment 2019] [Rokhsaz et al. 2022] [Růžička 2021] [Sadoff and Clousing 1948] [Sansica and Hashimoto 2023a] [Sansica and Hashimoto 2023b] [Sharan et al. 2013] [Shiryaev et al. 2023] [Smits 1988] [Stauffer 1964] [Stokke and Aiken 1948] [Supersonic Transport Wing Minimum 1992] [Tao et al. 2023] [Tatum and Giles 1987] [Thomas 1961b] [Thomas 1961a] [Turner 1944] [Turner 1947a] [Turner 1947b] [Veley et al. 2008] [Vinogradov and Menkov 2020] [Volobuyev et al. 2017] [Wang et al. 2023c] [Warner 1975] [Watmuff and Smits 1987] [Weisshaar 1990] [Weisshaar 1994] [Wing Loads 1996] [Xu and West 1990] [Zhang et al. 2014b] [Zhao et al. 2024]

Research airplane programmes and their record

The research airplanes and the X-3’s own record. Programme reports, research aircraft summaries and histories. 19 titles in the survey name the X-3 or its Douglas design number, and The Source Base lists them.

145 records. [Aerodynamic and Landing Measurements 1960] [Aerospace Landing Gear] [Aircraft Brake Quality Assurance] [Aircraft Tire History] [Alston 1939] [Ankenbruck 1954] [Armstrong 1977] [Baer-Riedhart 1981] [Baker 1953a] [Baker 1953b] [Baker 1954] [Baker and Johnson 1955] [Bartlett 1975] [Beh et al. 2018] [Bellman and Murphy 1954] [Bennett 1949] [Bennett 1950] [Boehm et al. 2001] [Boyer 2003] [Briggs 1954] [Burcham and Ray 1987] [Burcham et al. 1994] [Burcham et al. 1997] [Burk and Hultz 1951] [Campos 1989] [Chapman 2018] [Chaudhari and Takahashi 2022] [Childs 1953] [Chung and Hutchinson 2001] [Covington 1966] [Curry and Sim 1982] [Curry and Sim 1984] [Day and Reisert 1959] [Beeler 1961] [Del Frate and Saltzman 1992] [Denham and Owens 2016] [Dicarlo et al. 1992] [Ericsson 1999] [Esser and Ruff-Stahl 2021] [Finch and Briggs 1953] [Fischel and Nugent 1953] [Fischel and Reisert 1956] [Gilruth 1962] [Goff 1998] [Gray 1964] [Hassell and Hewes 1960] [Hawkins and Dilley 1992] [Henderson 1957] [History of Commercial Aircraft] [Hoe et al. 2012] [Hofmann et al. 2025a] [Holder 2006] [Jackson et al. 1978] [Jones 2011] [Jordan and Hutchins 1955] [Keener and Jordan 1956] [Keener et al. 1958] [Kehoe 1987] [Kehoe 1988] [Kemp and King 1956] [Kempel et al. 1988a] [Kirkham et al. 1974] [Knighton 1992] [Knotts and Parrag 1983] [Kordes and McKay 1961] [Kordes and McKay 1962] [Kuehme et al. 2014] [Kumar and Rao 2004] [Landing Area/Landing Gear Compatibility] [Layton 1984] [Lokos et al. 2015] [Love and Young 1966] [Marcy et al. 1956] [Matranga 1961] [McCuish and Caldwell 2018] [McDearmon 1956] [McDearmon and Boatright 1956] [McDearmon and Clark 1956a] [McDearmon and Clark 1956b] [McKay and Noll 1965] [McKee and Riebe 1952] [Mitchell and Peck 1955] [Morgenfeld 1992] [Scher 1946] [Blanchard 1953] [Day and Fischel 1955] [Stephenson 1956] [Drake 1957] [Baker et al. 1957] [Fischel et al. 1957] [Marcy 1958] [Bellman 1959] [Finch and Matranga 1959] [Reed and Watts 1961] [Banner et al. 1962] [Pyle and Steers 1975] [Kirkham et al. 1975] [Montoya and Banner 1977] [Arnaiz 1977] [Combs 1977] [Burcham et al. 1986] [Kempel et al. 1988b] [Dana 1993] [Saltzman and Ayers 1995] [Nugent and Takahashi 2026] [Osborne 1963] [Osborne and Stafford 1960] [Painter and Caw 1978] [Peck and Hollinger 1953] [Pendley 1947] [Progress of the X-15 1965] [Putnam and Ayers 1988] [Putnam and Ayers 1989] [Raab 2026] [Rainey and Igoe 1958] [Redeker and Voersmann 1988] [Reed 1955] [Research-Airplane-Committee Report on Conference 1958] [Rhodes 1969] [Rhodes 1970] [Rich 1973] [Day 1953] [Day and Stillwell 1952] [Richardson 1976] [ROCKET-POWERED AIRCRAFT 2017] [Row and Fischel 1963] [Sanderson 1965] [Sefic and Maxwell 1987] [Siano 2014] [Sim and Curry 1984] [Sim and Curry 1985] [Smith 1978] [Spearman 1979] [Stewart 1992] [Stillwell and Wilmerding 1951] [The Bell X-22A V/STOL 1990] [Tucker et al. 2014] [Turner and Rathert 1945] [Vail and Willis 1958] [Van Thullenar 1957] [Vanino and Rohlfs 1976] [Wang and Iliff 2004] [Weeks 1986] [Williams 1991] [Drake and Williams 1958]

Wind tunnels, models and the prediction of flight

How flight was predicted before it was flown. Wind tunnel technique, rocket-propelled and free-flight models, dynamic scaling and the correlation of tunnel and flight.

145 records. [Adams and Rubin 1958] [Akaryildiz et al. 2024] [Akishita et al. 1986] [Group 2000] [Arbic and Gillespie 1953] [Beyers 1995] [Boland et al. 1993] [Boppe 1978] [Boyer 1964] [Bradley and Bhateley 1983] [Brandon and Shah 1990] [Cobleigh et al. 1994] [Buckingham 1914] [Burchett et al. 2021] [Butler 1976b] [Buttrill and Houck 1990] [Chan 1980a] [Chan 1980b] [Charters 1962] [Chassiakos et al. 1988] [Cleary and Mellenthin 1949] [Corlett 1979] [Crites et al. 1992] [Cruz and Wilhite 1989] [Czysz 1963] [Davis et al. 2007] [Devan 1989] [Dillenius 1985] [Dougherty 2021] [Dougherty and Fisher 1980] [Erickson 1991] [Ericsson 1985] [Ericsson and King 1990] [European Transonic Windtunnel Project 1990] [Fisher et al. 1990] [Forner 1971] [Fukami et al. 2004] [Ghee and Taylor 2000] [Gibbings 1966] [Gillard 1999] [Goddard 1962] [Goldbaum 1956] [Goodyer 1990] [Grauer 2016] [Grunnet 1984] [Guimarães et al. 2021] [Harvey and Bobbitt 1981] [Hasegawa et al. 1999] [Hendershot 1969] [Hensel 1964] [High Supersonic Speed Wind 1961] [Hollis et al. 1999] [Hui and Yang 2013] [Jaffe 1972] [Johnson 1980] [Johnson 1981] [Johnson et al. 1970] [Kehlet 1954] [Kilgore et al. 1974] [Klausmeyer 2004] [Koh 1971] [Kong et al. 2023] [Lamar 1975] [Landrum and Miller 1980] [Levin and Sigal 2002] [Lift Effect on Transonic 1980] [Lijewski 1980] [Lowenberg and Kyle 2002] [Luckring et al. 2017] [Haseeb 2026] [MacDougall 1947] [Magill et al. 1995] [Mani et al. 2014] [Matak and Nikolić 2022] [McClinton et al. 1998] [Mehta 1986] [Meijer and Cunningham 1992] [Mikhail 1989] [Murman et al. 1994] [Murphy and Klein 2007] [Murphy et al. 2016] [Kayten and Koven 1945] [Mitcham et al. 1952] [Milholen and Chokani 1992] [Navaratna et al. 2022] [Norris et al. 1989] [Nävert and Sedin 1992] [Oberkampf 1974] [Oberkampf 1975] [Ojiaku and Prakash 2026] [Oktay and Asma 2000] [Pallister et al. 1992] [Patel et al. 2011] [Pattinson et al. 2011] [Pedreiro 1997] [Pejack et al. 1988] [Persoon et al. 1980] [Peterson 1982] [Phillips and Landman 2016] [Piatak and Cleckner 2002] [Poncet-Montanges et al. 2016] [Poncet-Montanges et al. 2017] [Prediction and Verification 1985a] [Prediction and Verification 1985b] [Rooney et al. 1977] [Saltzman and Ayers 1981] [Saltzman and Ayers 1982] [Saunders 1996] [Scherberg and Rhode 1927] [Schueler 1963] [Schuet et al. 2016] [Schy and Hannah 1976] [Schy and Hannah 1977] [Shantz 1953] [Shelton et al. 2018] [Smith 1953] [Smith and Hasel 1952] [Soudakov 2016] [Spurlin and Lueck 1984] [Staples and Nagati 1990] [Stargill 1983] [Stephens 1959] [Stevens 1955] [Stock 2002] [Swaim and Fullman 1977] [Tijdeman et al. 1979b] [Tijdeman et al. 1979a] [Transonic Computational Experience 1982] [Transonic Navier-Stokes Flow Computations 1972] [Ueno et al. 2002] [van Dam et al. 1995] [Verhoff 1987] [Welsh and Watt 1967] [Whitefield et al. 1981] [Winchenbach et al. 1982] [Wind Tunnel 2022] [Wood and Miller 1984a] [Yamada et al. 2023] [Yoshida 2009] [Young 2019] [Young et al. 1977] [Zakkay and Miller 1978] [Zartarian 1956] [Zartarian and Hsu 1955] [Zien and Ragsdale 1979]

Aircraft performance, flight mechanics and design method

The discipline the sizing argument belongs to. Climb, turn and manoeuvre performance, energy manoeuvrability and specific excess power, the equations of motion and the nonlinear dynamics that follow from them, and the conceptual design of fighters. The thrust-limited Mach number, the ceiling and the corner speed derived above are results of this discipline applied to one aircraft.

113 records. [Abzug and Larrabee] [Accelerated Flight Performance 2026] [Aerodynamics in the Age 1997] [Aircraft Non-Linear Dynamics 2014] [Airframe Equations of Motion 1998] [Airplane Trim 2012] [Airplane Trim 2022] [Albert Storace 2023] [Alexander 1948] [Asadi et al. 2013] [Baize 1999] [Bennett 1990] [Bihrle and Barnhart 1980] [Bihrle and Billy 1980] [Blázquez 1990] [Breakwell 1976] [Cass and Ball 1988] [Chapter 3. Dynamics 2005] [Chen 1981] [Chen et al. 2000] [Climb Performance 2021] [Complete model of aircraft] [Control Authority Assessment 1993] [Costes 2000] [Culick 1988] [Curtiss 1965] [Dacquino and Raffaele 1982] [Dahlke and Batiuk 1990] [Dollyhigh 1970] [Dynamics of Aircraft Motion 2015] [Dynamics of Elastically Supported 2023] [Dynamics of Flexible Aircraft 2023] [Erickson and Brandon 1987] [Ericsson 1986] [Ericsson 1995a] [Fellers and Patierno 1970] [Flight Envelope 2021] [Flight Envelopes 2012] [Foss 1978] [Fouda and Taha 2021] [Fundamentals of Fighter Design 2001] [Goman et al. 1997] [Gresham et al. 2011] [Hahne 1999] [Hess and Hess 1997a] [Donovan 1962] [High-Speed Flight and Its 2010] [Innocenti 1989] [Jung et al. 2021] [Katz 1979] [Khamvilai and Johnson 2025] [Khot et al. 2002] [Kitowski 1992a] [Klopfenstein 1965] [Kolesnikov and Goman 2012] [Krispin and Portnoy 1988] [Lamar et al. 1981] [Langan and Samuels 1995] [Leng 1995] [Li Yinan et al. 2012] [Limitations and Flight Envelope 2017] [Loh and Lusty 1974] [Louis 2022] [Lu et al. 1992] [Madelung 1977] [Madelung 1978] [Martinez 1961] [McAnally 1974] [Miller and Koch 1985] [NACA Conference on High-Speed 1958] [NACA 1948] [Nicolaides 1952] [Norman et al. 1983] [Northrop Aircraft INC Hawthorne CA 1953a] [Omran and Newman 2009] [Oruc and Baklacioglu 2022] [Oruc and Baklacioglu 2023] [Palusamy and Sivier 1993] [Parameter Sensitivity of High-Speed 2010] [Paranjape and Ananthkrishan 2005] [Patel and Smith 1996] [Pearson and Garvin 1941] [Phillips and Everest 1953] [Pollock and Wild 2024b] [Pollock and Wild 2024a] [Pruitt and Moroney 1980] [Pytka 2023a] [Qin et al. 2020] [Rankin et al. 2010] [Rankin et al. 2011] [Raymer 1995] [Render 2010] [Rhode 1929] [Rizzi and Luckring 2017] [Schwartz 1988] [Silton et al. 2014] [Singh] [Stenfelt and Ringertz 2013] [Stevens et al. 1974] [Stifel 1979] [Takahashi 2012] [Tamrat 1983] [Tamrat 1988] [Tang and Deng 2024] [Vachon and Ray 2004] [Vepa 2023a] [Ward 1989] [Whitford 1994] [Whitford 1995] [Wood 1999] [Wrestler and Clifton G. 1965] [Young et al. 1980] [Zhang et al. 2024b]

Wings, airfoils and low-speed aerodynamics

The other side of the thin wing’s bargain. Wing theory, lift slope, induced drag and the high-lift systems proposed for high-speed airplanes, with the oblique, slender and cruciform planforms and the unsteady airfoil pressures behind flutter, which is where an aspect ratio of 3.10 costs the aircraft its takeoff and landing performance.

46 records. [Ardonceau 1989] [Belart 1938] [Brümmer and Hummel 1993] [Carafoli 1969b] [Carafoli 1969d] [Carafoli 1969g] [Carafoli 1969e] [Carafoli 1969a] [Chapman et al. 2024] [CHAPTER TEN. Drag 1990] [Cohen and Jones 1960] [Curry and Curry 1997] [Demasi 2006] [DeSanti 1988] [Dowell and Assael 2025] [F. Nonsteady Wing Characteristics 1957] [Gratzer and O’Donnell 1965] [Gratzer and Odonnell 1964] [Hauptman 1987] [Hess and Stout 1998] [Hoerner 1936] [Ivanov and Krasil’nikov 1972] [Jones 1948] [Jones 1976d] [Kroo 1986] [Miller and Burkhalter 1987] [Morris 1990] [Neumark 1952] [Nikoueeyan and Naughton 2022] [Nikoueeyan and Naughton 2023] [Oblique Wing Aircraft 2020] [Owens et al. 2005] [Pendleton et al. 1991] [Petterson 2006] [Phillips 2013] [Phillips 2014] [Sanders 1965] [Schmidt and Duren 2002] [Smith 1990] [Spreiter 1950] [Stallings and Lamb 1981] [Stringfield 1984] [Travassos et al. 1980] [Wiler and White 1984] [Yates 1976] [Yates 1977]

Information, experimental design and cost

The accounting this article applies to the flight programme. Information theory, the Bayesian design of experiments, machine learning applied to fluid mechanics, and the cost of airplanes built in small numbers.

6 records. [Brunton et al. 2020] [Chaloner and Verdinelli 1995] [Lindley 1956] [Nyquist 1928] [Shannon 1948] [Wright 1936]

Where the Framing Breaks Down

The X-3 is the clearest case in this series of the keystone framework failing, and the failure is instructive in four ways.

The stated keystone was never tested. The aircraft was built to hold Mach 2 and never approached it, so the thin wing at sustained supersonic condition, the question the airframe exists to answer, has no X-3 answer [Dinius 2014]. Scoring the programme against its keystone returns a failure so complete that the framework has nothing further to say, which is a poor description of an aircraft whose data changed how a fleet was flown.

The contribution came from a property rather than a purpose. Inertia coupling was not a research objective, and the lateral and directional tests that found it were added to the programme only in late October 1954 [Dinius 2014]. It was a consequence of a mass distribution chosen for other reasons, and the aircraft revealed it because the configuration was extreme enough to make the phenomenon unmissable. A framework organized around what a programme intended to measure cannot capture a finding that arrived because of what the aircraft happened to be.

The failure was procurement rather than engineering. The airframe was competently designed against its specification. The engine did not arrive [Boslaugh]. No amount of aerodynamic or structural analysis addresses that, and the instrument model, which treats an aircraft as a purpose-built measuring device, has no account of a measuring device delivered without its power supply.

The most valuable result required survival. Walker’s departure produced data because the aircraft recovered. Two years later the same phenomenon in a less recoverable airframe produced a fatality and a much smaller data set [Jenkins et al. 2003]. The information yield of a flight research programme therefore depends on a survivability that the information framing does not model, and the X-2 and X-3 together make that point more sharply than either does alone.

The Source Base

The primary record is adequate and narrow. The NACA reports cover demonstration stability and control in Day and Fischel 1955, tail loads in Stephenson 1956, buffet in Baker et al. 1957, transonic handling qualities including the coupling in Fischel et al. 1957, and landing loads in Marcy 1958, with the pre-flight spin tunnel work in Hultz 1951 and the escape capsule study in Scher 1946. The programme’s record is wider than these seven reports. The aircraft appears otherwise in comparative summaries such as Bellman 1959 and Saltzman and Ayers 1995.

The survey holds 19 reports whose titles name the X-3 or its Douglas design number. Beyond the seven above, they give the lift and drag measured on the demonstration flights to Mach 1.20 in Bellman and Murphy 1954, wing pressure distributions in Jordan and Hutchins 1955, wing loads in Keener and Jordan 1956 and their change with leading-edge flap deflection in Keener et al. 1958, and vertical tail loads in Marcy et al. 1956. The theoretical lateral stability of an early version of the design and of the aircraft itself is in Bennett 1949 and Bennett 1950, tunnel and rocket-model tests of the configuration are in Burk and Hultz 1951, McKee and Riebe 1952, Peck and Hollinger 1953, and Mitchell and Peck 1955, and Stone 1956 records notes on the violent coupling motions in aileron rolls.

The secondary literature is thin and the aircraft is usually a paragraph. Miller 2001, Jenkins et al. 2003, Winchester 2005, and Peebles 2014 give the roster treatment, with Francillon covering the manufacturer. Hallion 1972, Hallion 1984, Hallion 1981, Gorn 2001, and Bilstein 1989 give the programme and institutional context, and Gunston 1992 the wider high-speed narrative. Heppenheimer 2007 covers the thermal thread the X-3 touched but did not pursue.

The engineering texts behind the relations are Anderson 2001, Anderson and Modern compressible flow 1982, Anderson 2006, Anderson et al. 1999, Anderson 1997, Bertin and Cummings 2013, Bertin and Hypersonic aerothermodynamics 1994, Shapiro 1953, Liepmann and Roshko 1957, Ashley and Landahl 1965, Küchemann 1978, Schlichting and Gersten 2017, White 2006, Truitt 1960, and Incropera and DeWitt, with heat conduction in Carslaw and Jaeger 1959 and thermal stress in Boley and Weiner 1960. Flight dynamics is Etkin et al. 1959, Nelson 1998, Stengel and Flight dynamics 2004, Stevens et al. 2015, McRuer et al. 1990, and Hurt 1960. Design method is Raymer et al. 2012, Nicolai et al. 2010, and Whitford 1987. Structures are Bruhn 1973, Niu and Niu 1988, and Megson and Aircraft structures for engineering students n.d., aeroelasticity Bisplinghoff et al. 1955, Fung and An introduction to the theory of aeroelasticity 1955, and Dowell and A modern course in aeroelasticity 2014, and propulsion Sutton and Biblarz 2016, Hill and Peterson 1991, and Huzel and Huang 1992. Flight test practice is Kimberlin 2003 and Ward et al. 2006, with error analysis in Taylor 1997 and Bevington and Robinson 2002. The epistemology is Vincenti 1990, Petroski 1985, and Ferguson 1992, the organizational reading of failure is Perrow 1984, Vaughan 1996, Sagan 1993, and Reason and Human error 1990, and the information accounting is Cover and Thomas 2006 with design of experiments in Box et al. 2005, Gelman et al. 2013, Lindley 1956, and Chaloner and Verdinelli 1995. The X-15 works of Jenkins 2007, Jenkins 2000, and Thompson 1992, the entry lineage in Launius and Jenkins 2012, the Blackbird account of Merlin 2009, the tunnel histories of Baals and Corliss 1981, Hansen 1987, and Chambers and Chambers 2008, the popular framing of Wolfe 1979, and the theoretical lineage in Von Kármán and Edson 1967 and Gorn 1992 complete the set.

Foundational primaries bearing on the arguments above without belonging to one section include Williams and Drake on the research airplane rationale, Buckingham 1914 on similarity, Sutherland 1893 on viscosity, Glauert 1928 and Prandtl 1928 on compressibility and the boundary layer, Jones 1947b on planform, Sears 1947 and Whitcomb on wave drag and area ruling, Ames Research Staff 1953 for the compressible relations, Theodorsen 1935, Collar 1946, and Garrick and Reed 1981 on aeroelasticity, Eckert 1956, Chapman and Rubesin 1949, Fay and Riddell 1958, and Lees 1956 on heating, Beeler et al. 1956 on drag measurement, Wright 1936 on unit cost at small quantities, Nyquist 1928 and Shannon 1948 on sampling and capacity, and Grauer and Morelli 2023 on the modern descendant of the whole measurement discipline. The wider fleet context appears in Wetzel 1954, Drake 1957, Banner et al. 1962, Dana 1993, Reed and Watts 1961, and Finch and Matranga 1959. The equivalent problems at model scale are worked on this blog in Propulsion and Power Sizing for Small Fixed-Wing UAVs, Stability, Control, and Configuration for Fixed-Wing UAVs, Dynamic Stability and Control for Fixed-Wing UAVs, and Structures and the Flight Envelope for Fixed-Wing UAVs, the rocketplane lineage in History of Rocketplanes, large high-speed configurations in Two-Stage Flying Delta Wing Vehicles for Civil and National Security Applications, propellant chemistry in Rocket Propellant Chemistry, A Design-Tradeoff Space, the computing and simulation infrastructure in Aerospace, Programming Languages, and Information Technology Co-Development: Framing and the Co-Development Mechanism and Aerospace, Programming Languages, and Information Technology Co-Development: Aerospace Simulation and Real-Time Systems, and space policy in Introduction to Space Studies. The NASA Technical Reports Server and the NASA History Office hold the record, and the Armstrong Flight Research Center is the institutional successor.

The research survey holds 5,371 research records drawn from Crossref, the NASA Technical Reports Server and the Defense Technical Information Center, of which 1,152 are report primaries, being 21.4 percent, by the identifier rule set out under The Definition of Primary. The median publication year is 1996. Of the 5,295 dated records, 726 were published before 1960, the period in which the aircraft was designed and flown, being 13.7 percent, and 1,375 were published in 2015 or later, being 26.0 percent.

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 its address is on the NASA Technical Reports Server or it carries a digital object identifier under the 10.21236 prefix, which Crossref registers for Defense Technical Information Center reports. The NACA reports that carry this article’s argument are report primaries under that rule, and so are all of the X-3’s own reports. The rule does not reach the journal papers among the foundational sources, such as Glauert on compressibility, Sears on minimum wave drag and Sutherland on viscosity, so 21.4 percent is a lower bound on how much of the 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. Where a row joins two groups of terms with the word together, a title must carry a term from each group.

Subject	Title terms counted	Records
the boundary layer diverter of a side inlet	diverter, diverters, diverterless, diverter less	14
the recovery temperature of a heated surface	recovery temperature, recovery factor, recovery factors, adiabatic wall temperature	19
springback of formed titanium sheet	springback together with titanium, Ti 6Al 4V, Ti6Al4V, TC4	13
swing and pendulum measurement of inertia	swing, pendulum, bifilar, trifilar together with moment of inertia, moments of inertia	25
the mass distribution and inertia ratio of an airframe	mass distribution, inertia ratio, inertia distribution, radius of gyration, radii of gyration	10
engine and airframe development schedules	engine development, engine program, engine programme, engine delay, engine availability, engine substitution, engine selection	8

The diverter is a part the literature mostly sets out to remove. Of the 14 titles, 8 describe diverterless inlets, and the side-inlet diverter of the X-3’s own period appears in one NACA report on a diverter-type boundary-layer removal system for a scoop inlet at Mach 1.90.

The recovery temperature is settled rather than neglected. The relation that decides whether titanium was needed at Mach 2 is standard and tabulated, and a small literature of recovery factor measurements is the shape a settled subject takes.

Springback of titanium is a small part of a large literature. Titanium appears in 13 of the 274 titles that name springback, so the statement that titanium’s elastic recovery after forming is roughly twice aluminium’s rests on the yield-to-modulus relation derived above rather than on a body of titanium-specific measurement.

The inertia of a whole aircraft is rarely the subject of a title. Of the 25 titles on swing and pendulum methods, 2 name an aircraft or an unmanned air vehicle, and the rest are general metrology of moments of inertia. The coupling analysis depends on inertia entirely.

Mass distribution was studied as a spin problem before it was a coupling problem. Of the 10 titles that name mass distribution or an inertia ratio, 7 concern spinning or tumbling.

The procurement lesson has almost no literature. Eight titles name engine development, and none names a schedule, a delay or a substitution, so the conclusion that engine and airframe cannot be procured on independent schedules stands on the X-3’s own history rather than on a published analysis.

What the Survey Admits

A record is admitted only when a person reading its title finds it on this article’s subject. Many words this subject depends on also name something else, and a record that shares only such a word is excluded. Titanium is also a word of dentistry, orthopaedic implants and photocatalysis, and flutter is also a disorder of the heart. Fighter also names freedom fighters, fire fighters, video games and a lettuce cultivar, and Starfighter also names a film. Inertial coupling also belongs to two-phase flow, rotordynamics and satellite attitude, roll damping and roll coupling also belong to ships, barges and offshore platforms, and kinematic coupling is a fixture of precision engineering. Departure also names a flight leaving its gate, so air traffic scheduling is excluded. An afterburner is also a stage of a particle accelerator and a utility for graphics cards, an inlet is also a feature of a coastline and the mouth of a pipe, and the supersonic nozzle of a natural gas separator shares the inlet’s gas dynamics and none of its subject. The wind tunnel also tests cars, trains, bridges, buildings and birds, and the pendulum measurement of a moment of inertia also serves sports equipment and internal-friction apparatus. Correction, withdrawal and erratum notices, trade news, parts catalogue listings, fastener and material specifications, bibliographies, and records that are parts of works rather than works, such as figure, table and front-matter records, are excluded as well, because a survey counts research works, and course and classroom material is excluded because a teaching exercise is not a method for an aircraft. Three families of titles that a shared exclusion list refuses elsewhere are admitted here because they are this subject, namely inlet buzz, the fracture of titanium alloys and the supersonic aerodynamics of missiles.

A record whose only link to this subject is aeronautics in general is excluded too, and so is one whose subject belongs to a class of vehicle the argument never uses. Rotorcraft, vertical and short takeoff aircraft, airships, small unmanned and micro air vehicles, airliners and light aircraft, spacecraft and launch vehicles are such classes, and so are aircraft and jet noise with the sonic boom, small and micro turbojets, fans, propellers and turboprops, titanium powder moulding and coatings, and flight control design methods the argument does not use. A method or phenomenon the argument relies on is admitted whatever the vehicle, so a study of flutter, loss of control, system identification or inertia measurement on another class of aircraft is kept, and so are the oblique-wing aircraft whose deliberate asymmetry makes coupling a design variable. A book chapter is a work and is judged by its subject. A review of a book, a dictionary or short reference entry, an editorial or news notice, and a second deposit of a document already counted, such as a conference copy of a report, are not research works and are not admitted. A signed comment on a paper, a discussion of it and its author’s closure or reply are research works, because each argues about a result, and are admitted when their subject is.

Some records of doubtful relevance are kept. Springback studies of steel and aluminium sheet are kept, because the springback relation this article derives for titanium is the same relation. General pendulum methods for measuring moments of inertia are kept, because the swing test is one of them. Recommended practices and design requirements for landing gear, wheels, tires and brakes, and titanium metallurgy that names no aircraft, share the subject’s hardware or materials, and a reader may weigh each accordingly.

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.

Epistemic State

Established historical fact includes the 1949 approval of construction, the single airframe and its serial, the substitution of Westinghouse J34 engines for the intended J46, the wing thickness ratio and aspect ratio, the extensive use of titanium, the first flight on 20 October 1952, the maximum speed of Mach 1.208 in a dive on 28 July 1953, the 51 flights, the coupling events flown by Joe Walker on 27 October 1954, and the aircraft’s retirement in 1956 and preservation. These are documented in the sources cited.

Established engineering analysis includes every relation in the sizing sections. The thrust-limited Mach relation, the normal-shock recovery relation, the Ackeret result, the Bredt torsion relation, the divergence and reversal expressions, the takeoff relations, and the coupling threshold are standard results. The worked numbers are the author’s own arithmetic applied to published inputs and are labelled as derived.

Inference includes the attribution of the performance shortfall to thrust and inlet losses in the proportions given. The thrust shortfall is documented and the normal-shock recovery is arithmetic, but the assignment of the residual between drag underestimate and installed-thrust shortfall is an interpretation the record does not settle. The claim that a fixed inlet was the second failure is an inference, because the sources consulted describe no variable geometry but do not describe the inlets at all, and the numerical split is weaker still.

Weakly supported are the representative values where the sources give no figures. The stiffness coefficients, the maximum lift coefficient, the ground friction and drag during the takeoff roll, and the assumed drag coefficients are plausible for an aircraft of this class rather than measured properties of this airframe. The moments of inertia are those tabulated by Day 1997, and the inertias the NACA used for this aircraft were the manufacturer’s estimates according to Fischel et al. 1957. The critical roll rate of 84 degrees per second rests on the assumed stiffness coefficients and should be read as establishing that the threshold lay within the aircraft’s roll authority, not as a number this aircraft carried. Day 1997 reports a calculated critical roll velocity of 2.5 radians per second at the Mach 1.05 condition. The comparison with the X-2 figure of 255 uses the same method and the inertias Day tabulates for both aircraft, but both figures rest on the same assumed stiffness coefficients, so the ratio is indicative only.

Contested or unresolved in the sources consulted is the exact division of responsibility for the performance shortfall, the degree to which the titanium experience influenced later programmes, and the precise flight count, which is usually given as 51 but is stated without a counting rule. The inadvertent hop during the taxi test five days before the official first flight is variously counted and not counted. The sources also disagree on the Mach number of Walker’s second roll, given as 1.05 by Day 1997 and as 1.154 by Dinius 2014.

A note on temporal position. This article carries an editorial date of 2025-10-09 and is written from current knowledge, including contemporary literature published well after that date.

Out of Scope

This article does not treat the X-1 or X-2 beyond the comparisons drawn, both of which have their own articles, nor the X-15, the X-4, or the X-5, which appear later in the series. It does not derive the standard relations reused here, since the series opener does that once for all seventy-two articles, including the flight envelope, load factor, wing loading, lift and drag coefficients, lift-to-drag, Reynolds and Prandtl numbers, measurement uncertainty and its propagation, and the standard atmosphere in its tabulated form.

It does not attempt a history of the Westinghouse engine programmes, whose failure is the proximate cause of the outcome and deserves its own treatment. It does not treat the F-104 as an aircraft, only as an inheritor. It does not cover shock wave and oblique shock theory, wave drag, expansion geometry, supersonic or hypersonic flow, boundary layer and separation behaviour, buffeting, aerodynamic centre migration, longitudinal or directional stability, Dutch roll, the phugoid, flight dynamics generally, inertia coupling as a general subject, Euler’s equations, reaction control, stabilators, stainless steel, Inconel, duralumin, titanium alloys as metallurgy, creep, yield, thermal conductivity, expansion, stress, the Biot and Fourier numbers, the heat equation, heat flux, stagnation temperature, the Stefan-Boltzmann law, specific impulse, the Tsiolkovsky equation, rocket engines, liquid oxygen, turbopumps, ejection seats, the Karman line, wind tunnels, flight testing, telemetry, thermocouples, accelerometers, the sound barrier, transonic flow, swept wings, the XB-70 and SR-71, Edwards and the Armstrong Flight Research Center, Bell Aircraft, the NACA and NASA as organizations, the National Museum of the United States Air Force, the list of X-planes, or experimental aircraft as a category, all of which are treated where they belong.

Conclusion

The Douglas X-3 was designed correctly against a specification that changed under it. Two engines producing seventy percent of the intended thrust, feeding through fixed inlets that lose a further twenty-eight percent of total pressure at the design Mach number, halve the thrust available. Halving thrust costs thirty percent of maximum Mach number, which takes a design value of 2.0 to about 1.42, and the aircraft managed 1.21. The keystone question, which is how a very thin very low aspect ratio wing behaves in sustained supersonic flight, was never asked of it.

What the aircraft did instead was reveal the consequence of its shape. A twenty-metre fuselage with a seven-metre wing has a pitch to roll inertia ratio near fifteen, about three times the X-2 value, and that puts the critical roll rate at about eighty-four degrees per second. That is a moderate control input. Joe Walker made an abrupt roll in October 1954, the aircraft departed violently in all three axes, and he recovered and did it again [Dinius 2014]. The resulting data set arrived while a fighter fleet was losing aircraft to the same phenomenon and two years before it killed a pilot in the X-2 [Day 1997].

The X-3 therefore fails its keystone completely and matters anyway. No sharper demonstration is available that design intent and historical contribution are different quantities. It also supplied a wing planform to the F-104 and data for better tires, which is a more conventional kind of success and a smaller one.

The next article takes the Northrop X-4 Bantam, a semi-tailless aircraft built to test whether the horizontal tail could be dispensed with at transonic speed, and which answered that question in the negative clearly enough that nobody asked it again for thirty years.

Equations

This section collects the 114 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 114, 99 are established and 15 are bespoke. Quantities are in units of the International System after conversion from the pounds, slug square feet and miles per hour of the sources, angles enter the aerodynamic relations in radians, and several letters change meaning between sections, so $\gamma$ is the ratio of specific heats in the gas dynamics and the flight path angle in the trajectory relations, $q$ is dynamic pressure except in the body-axis equations where it is the pitch rate, and $p$ is static pressure, roll rate or a loss probability according to context.

Equation 1, Ackeret Linearised Supersonic Pressure Coefficient. In linearised supersonic flow the pressure coefficient on a thin surface depends only on the local inclination and the free-stream Mach number. Ackeret 1925

\[C_p = \frac{2 \, \theta}{\sqrt{M_\infty^2 - 1}} \tag{1}\]

Equation 2, Wave Drag Ratio of a 4.5 Percent and an 8 Percent Section. Because thickness wave drag scales as the square of thickness ratio, the X-3 section carries about a third of the wave drag of the X-1 section at the same conditions.

\[\frac{D_{w}(4.5\%)}{D_{w}(8\%)} = \left( \frac{4.5}{8.0} \right)^2 = 0.32 \tag{2}\]

Equation 3, Second Moment of Area of an Idealised Wing Box. Treating the spar caps as concentrated areas at half the structural depth gives a bending second moment that falls as the square of thickness ratio for fixed cap area.

\[I_{\text{box}} \approx \frac{A_{\text{cap}} h_s^2}{2} = \frac{A_{\text{cap}} \tau^2 c^2}{2} \tag{3}\]

Equation 4, Cap Area Scaling with Thickness Ratio. The cap area needed to carry a given moment at a given stress varies inversely with the structural depth and hence with thickness ratio.

\[A_{\text{cap}} \propto \frac{1}{\tau} \tag{4}\]

Equation 5, Torsional Frequency, Mass Ratio and Flutter Speed Index. The torsional natural frequency, the wing mass ratio and the flutter speed index are the standard groups on which a flutter boundary depends.

\[\omega_\alpha = \sqrt{\frac{K_\theta}{I_\theta}}, \qquad \mu_m = \frac{m_w}{\pi \rho b^2}, \qquad F_i = \frac{V_f}{b \omega_\alpha \sqrt{\mu_m}} \tag{5}\]

Equation 6, Bredt Torsion Constant of a Thin Wing Box. The Bredt relation for a closed thin-walled section gives a torsion constant proportional to the square of the enclosed area and therefore to the square of thickness ratio.

\[J = \frac{4 A_m^2}{\oint ds / t} \propto \tau^2 \tag{6}\]

Equation 7, Energy Height and Specific Excess Power. Energy height adds the kinetic energy per unit weight to the altitude, and its rate of change is the specific excess power.

\[h_e = h + \frac{V^2}{2 g}, \qquad \frac{dh_e}{dt} = P_s = \frac{V (T - D)}{W} \tag{7}\]

Equation 8, Reduction of Random Uncertainty with Dwell Time. Averaging independent noise over a dwell of longer duration reduces the random uncertainty as the inverse square root of that duration.

\[\sigma \propto \frac{1}{\sqrt{T_d}} \tag{8}\]

Equation 9, Aspect Ratio of the X-3 Wing. The square of the span divided by the wing area gives an aspect ratio of 3.10 from the tabulated dimensions. aspect ratio Fischel et al. 1957

\[A = \frac{b^2}{S} = \frac{6.92^2}{15.47} = 3.10 \tag{9}\]

Equation 10, Installed Thrust of Two J34 Engines. Two Westinghouse J34 engines of 4900 pounds of afterburning thrust each give about 43.6 kilonewtons. Fischel et al. 1957

\[T_{\text{J34}} = 2 \times 4900 \times 4.448 = 4.36 \times 10^{4} \ \text{newtons} \tag{10}\]

Equation 11, Design Thrust of Two J46 Engines. Two Westinghouse J46 engines of the expected 7000 pounds each would have given about 62.3 kilonewtons. Douglas X-3 Stiletto

\[T_{\text{J46}} = 2 \times 7000 \times 4.448 = 6.23 \times 10^{4} \ \text{newtons} \tag{11}\]

Equation 12, Thrust Shortfall of the Engine Substitution. The installed thrust falls thirty percent short of the design thrust.

\[1 - \frac{T_{\text{J34}}}{T_{\text{J46}}} = 30 \ \text{percent} \tag{12}\]

Equation 13, Bespoke Thrust-to-Weight Ratio at Fixed Weight. Holding the aircraft weight fixed as a first approximation makes the thrust-to-weight ratio fall in direct proportion to the thrust, to seventy percent of its design value.

\[\frac{(T/W)_{\text{J34}}}{(T/W)_{\text{J46}}} = \frac{T_{\text{J34}}}{T_{\text{J46}}} = 0.70 \tag{13}\]

Equation 14, Thrust Equals Drag in Level Flight. Steady level flight requires the thrust to equal the drag, written as dynamic pressure times wing area times drag coefficient.

\[T = D = q S C_D \tag{14}\]

Equation 15, Dynamic Pressure in Terms of Mach Number. For a perfect gas the dynamic pressure equals half the ratio of specific heats times the static pressure times the square of the Mach number. dynamic pressure

\[q = \frac{\gamma}{2} p M^2 \tag{15}\]

Equation 16, Isentropic Total Pressure and Total Temperature Ratios. The isentropic relations give the ratios of total to static pressure and temperature as functions of Mach number. Ames Research Staff 1953

\[\frac{p_0}{p} = \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}}, \qquad \frac{T_0}{T} = 1 + \frac{\gamma - 1}{2} M^2 \tag{16}\]

Equation 17, Mach Angle. The Mach angle is the inverse sine of the reciprocal of the Mach number. Ames Research Staff 1953

\[\mu_M = \arcsin \frac{1}{M} \tag{17}\]

Equation 18, Isentropic Area-Mach Number Relation. The ratio of stream-tube area to sonic throat area is a function of Mach number alone in isentropic flow. Ames Research Staff 1953

\[\frac{A}{A^{*}} = \frac{1}{M} \left[ \frac{2}{\gamma + 1} \left( 1 + \frac{\gamma - 1}{2} M^2 \right) \right]^{\frac{\gamma + 1}{2 (\gamma - 1)}} \tag{18}\]

Equation 19, Thrust-Limited Maximum Mach Number. Equating thrust to drag with the dynamic pressure written in Mach number form and solving gives the square of the maximum Mach number.

\[M_{\max}^2 = \frac{2 T}{\gamma \, p \, S \, C_D} \tag{19}\]

Equation 20, Bespoke Maximum Mach Number Ratio at Fixed Drag Coefficient. Holding altitude and drag coefficient fixed across the Mach range, an assumption the article chose, makes the maximum Mach number scale as the square root of the thrust.

\[\frac{M_{\max, 2}}{M_{\max, 1}} = \sqrt{\frac{T_2}{T_1}} \tag{20}\]

Equation 21, Bespoke Mach Number Penalty of the Thrust Shortfall. Under the fixed drag coefficient assumption a thirty percent thrust shortfall reduces the maximum Mach number to 0.837 of its design value.

\[\sqrt{0.70} = 0.837 \tag{21}\]

Equation 22, Normal Shock Total Pressure Recovery. The ratio of total pressure behind and ahead of a normal shock is a function of the upstream Mach number and the ratio of specific heats. Ames Research Staff 1953

\[\frac{p_{02}}{p_{01}} = \left[ \frac{(\gamma + 1) M_1^2}{(\gamma - 1) M_1^2 + 2} \right]^{\frac{\gamma}{\gamma - 1}} \left[ \frac{\gamma + 1}{2 \gamma M_1^2 - (\gamma - 1)} \right]^{\frac{1}{\gamma - 1}} \tag{22}\]

Equation 23, Normal Shock Static Pressure and Temperature Ratios. The Rankine-Hugoniot relations give the static pressure and temperature rise across a normal shock. Ames Research Staff 1953

\[\frac{p_2}{p_1} = \frac{2 \gamma M_1^2 - (\gamma - 1)}{\gamma + 1}, \qquad \frac{T_2}{T_1} = \frac{\left[ 2 \gamma M_1^2 - (\gamma - 1) \right] \left[ (\gamma - 1) M_1^2 + 2 \right]}{(\gamma + 1)^2 M_1^2} \tag{23}\]

Equation 24, Mach Number Behind a Normal Shock. The downstream Mach number of a normal shock follows from the upstream Mach number and the ratio of specific heats. Ames Research Staff 1953

\[M_2^2 = \frac{(\gamma - 1) M_1^2 + 2}{2 \gamma M_1^2 - (\gamma - 1)} \tag{24}\]

Equation 25, Bespoke Thrust Proportional to Inlet Recovery. The article takes turbojet thrust to scale with the total pressure recovery delivered to the compressor face, so the inlet loss passes directly into thrust.

\[\frac{T}{T_{\text{ideal}}} \approx \frac{p_{02}}{p_{01}} \tag{25}\]

Equation 26, Inlet Mass Flow Ratio. The mass flow ratio is the captured stream-tube area divided by the inlet capture area, equal to the engine mass flow over the free-stream flux through the capture area.

\[\frac{A_0}{A_c} = \frac{\dot{m}_{\text{engine}}}{\rho_\infty V_\infty A_c} \tag{26}\]

Equation 27, Additive Drag of a Spilling Inlet. The additive drag is the momentum deficit of the captured stream tube plus the pressure force on it between the free stream and the cowl lip.

\[D_{\text{add}} = \dot{m}_0 \left( V_\infty - V_1 \right) + \left( p_1 - p_\infty \right) A_1 \tag{27}\]

Equation 28, Bespoke Spillage Drag Coefficient. The article approximates the spillage drag coefficient as proportional to the capture area, the shortfall in mass flow ratio and the square of the sine of the cowl lip angle.

\[C_{D,\text{add}} = \frac{D_{\text{add}}}{q S} \approx \frac{2 A_c}{S} \left( 1 - \frac{A_0}{A_c} \right) \sin^2 \theta_c \tag{28}\]

Equation 29, Bespoke Effective Thrust Budget. The effective thrust is assembled from the recovered ideal thrust less the additive drag and the boundary layer diverter drag.

\[T_{\text{eff}} = \eta_d \, T_{\text{ideal}} - D_{\text{add}} - D_{\text{div}} \tag{29}\]

Equation 30, Inlet Buzz Criterion. Buzz sets in when the mass flow ratio falls below a critical value at which the terminal shock is expelled from the throat.

\[\frac{A_0}{A_c} < \left( \frac{A_0}{A_c} \right)_{\text{crit}} \tag{30}\]

Equation 31, Bespoke Combined Thrust Factor. Multiplying the engine substitution factor by the normal shock recovery at Mach 2 treats the two losses as compounding and leaves about half the design thrust.

\[0.70 \times 0.721 = 0.505 \tag{31}\]

Equation 32, Bespoke Maximum Mach Number with Combined Losses. Applying the square-root thrust scaling at fixed drag coefficient to the combined thrust factor gives a maximum Mach number of 1.42.

\[M_{\max} = 2.0 \times \sqrt{0.505} = 1.42 \tag{32}\]

Equation 33, Bespoke Turbojet Thrust Lapse with Altitude and Mach Number. The article models thrust as proportional to ambient pressure with an isentropic ram correction multiplied by the inlet recovery.

\[\frac{T(h, M)}{T_{SL}} \approx \frac{p(h)}{p_{SL}} \left( 1 + \frac{\gamma - 1}{2} M^2 \right)^{\frac{\gamma}{\gamma - 1}} \eta_d \tag{33}\]

Equation 34, Point-Mass Equation Along the Flight Path. The excess of thrust over drag accelerates the aircraft along its path and supports the component of weight along that path.

\[T - D = m \frac{dV}{dt} + m g \sin \gamma \tag{34}\]

Equation 35, Time to Cross a Speed Increment in Level Flight. In level flight the time to accelerate between two speeds is the integral of mass over excess thrust, which diverges as thrust approaches drag.

\[t_{\text{cross}} = \int_{V_1}^{V_2} \frac{m \, dV}{T(V) - D(V)} \tag{35}\]

Equation 36, Specific Excess Power. Specific excess power is the speed times the excess of thrust over drag divided by the weight.

\[P_s = \frac{V (T - D)}{W} \tag{36}\]

Equation 37, Ceiling Condition. The ceiling is the altitude at which specific excess power vanishes because thrust equals drag.

\[P_s = 0 \quad \Longleftrightarrow \quad T(h) = D(h) \tag{37}\]

Equation 38, Thrust-to-Weight Ratio at Maximum Takeoff Mass. The installed J34 thrust divided by the weight at the maximum takeoff mass of 10,161 kilograms gives 0.44. Douglas X-3 Stiletto

\[\frac{T}{W} = \frac{4.36 \times 10^{4}}{10{,}161 \times 9.80665} = 0.44 \tag{38}\]

Equation 39, Wing Loading at Maximum Takeoff Mass. The weight at maximum takeoff mass divided by the wing area gives 6441 newtons per square metre. Douglas X-3 Stiletto

\[\frac{W}{S} = \frac{10{,}161 \times 9.80665}{15.47} = 6441 \ \text{newtons per square metre} \tag{39}\]

Equation 40, Manoeuvre Corner Speed. The corner speed is the lowest speed at which the maximum lift coefficient produces the limit load factor.

\[V_A = \sqrt{\frac{2 n_{\max} W}{\rho S C_{L,\max}}} \tag{40}\]

Equation 41, Aerodynamically Available Load Factor. Below the corner speed the available load factor is the maximum lift at that speed divided by the weight.

\[n(V) = \frac{\rho V^2 C_{L,\max}}{2 \left( W / S \right)} \tag{41}\]

Equation 42, Ackeret Supersonic Lift-Curve Slope. Linearised theory gives a two-dimensional supersonic lift-curve slope of four over the square root of the square of the Mach number less one. Ackeret 1925

\[C_{L\alpha} = \frac{4}{\sqrt{M_\infty^2 - 1}} \tag{42}\]

Equation 43, Supersonic Aspect Ratio Parameter. The product of the Prandtl-Glauert factor and the aspect ratio indicates how far tip effects reach across a supersonic wing.

\[\beta_s A = \sqrt{M_\infty^2 - 1} \; A \tag{43}\]

Equation 44, Supersonic Lift-Curve Slope at Mach 2. The Ackeret slope evaluated at Mach 2 is 2.31 per radian, which applies because the supersonic aspect ratio of the X-3 wing exceeds four. Ackeret 1925

\[C_{L\alpha} = \frac{4}{\sqrt{3}} = 2.31 \ \text{per radian} \tag{44}\]

Equation 45, Aerodynamic Centre Shift Through the Transonic Range. The aerodynamic centre moves from about the quarter chord in subsonic flow to about the half chord in supersonic flow.

\[\frac{x_{ac}}{\bar{c}} : 0.25 \longrightarrow 0.50 \tag{45}\]

Equation 46, Static Margin and Pitch Stiffness. The static margin is the distance from the centre of gravity to the neutral point in mean chords, and the pitch stiffness is the negative of the lift-curve slope times that margin.

\[SM = \frac{x_{np} - x_{cg}}{\bar{c}}, \qquad C_{m\alpha} = -C_{L\alpha} \, SM \tag{46}\]

Equation 47, Stick-Fixed Neutral Point. The neutral point lies aft of the wing aerodynamic centre by the tail volume coefficient times the tail-to-wing lift slope ratio corrected for downwash.

\[\frac{x_{np}}{\bar{c}} = \frac{x_{ac,w}}{\bar{c}} + V_H \frac{C_{L\alpha_t}}{C_{L\alpha_w}} \left( 1 - \frac{d\varepsilon}{d\alpha} \right), \qquad V_H = \frac{S_t l_t}{S \bar{c}} \tag{47}\]

Equation 48, Short Period Frequency and Damping Approximation. The short period approximation expresses the frequency and damping of the fast longitudinal mode through the pitch and heave stability derivatives.

\[\omega_{sp} \approx \sqrt{\frac{Z_\alpha M_q}{V} - M_\alpha}, \qquad \zeta_{sp} \approx -\frac{M_q + M_{\dot\alpha} + Z_\alpha / V}{2 \omega_{sp}} \tag{48}\]

Equation 49, Dutch Roll Frequency Approximation. The Dutch roll frequency is approximated by the square root of the directional stiffness moment divided by the yaw inertia.

\[\omega_{dr} \approx \sqrt{\frac{q S b \, C_{n\beta}}{I_z}} \tag{49}\]

Equation 50, Slender-Wing Limit of the Lift-Curve Slope. At low aspect ratio the subsonic lift-curve slope tends toward the slender-wing value of $\pi A / 2$, which is 4.87 per radian for this wing.

\[C_{L\alpha} \to \frac{\pi A}{2} = 4.87 \ \text{per radian} \tag{50}\]

Equation 51, Induced Drag Coefficient. The induced drag coefficient is the square of the lift coefficient divided by pi, the aspect ratio and the span efficiency factor.

\[C_{D,i} = \frac{C_L^2}{\pi A e} \tag{51}\]

Equation 52, Drag Build-Up of Friction, Wave and Induced Terms. The drag coefficient is the sum of a friction term, a wave term and the induced drag.

\[C_D = C_{D,f} + C_{D,w} + \frac{C_L^2}{\pi A e} \tag{52}\]

Equation 53, Reynolds Number. The Reynolds number based on a reference length is the ratio of inertial to viscous forces in the free stream.

\[Re_L = \frac{\rho_\infty V_\infty L}{\mu} \tag{53}\]

Equation 54, Sutherland Viscosity Law. Sutherland’s relation gives the dynamic viscosity of air as a function of temperature from a reference viscosity and the Sutherland constant.

\[\mu = \mu_{\text{ref}} \left( \frac{T}{T_{\text{ref}}} \right)^{3/2} \frac{T_{\text{ref}} + S}{T + S} \tag{54}\]

Equation 55, Turbulent Flat-Plate Friction Referred to Wetted Area. The turbulent flat-plate one-fifth power law, scaled by the ratio of wetted to reference area, gives the friction drag coefficient.

\[C_{D,f} = \frac{0.074}{Re_L^{1/5}} \cdot \frac{S_{\text{wet}}}{S} \tag{55}\]

Equation 56, Ackeret Thickness Wave Drag. In linearised theory the zero-lift wave drag of a thin section is four times the chordwise mean squared slope divided by the Prandtl-Glauert factor. Ackeret 1925

\[C_{D,w} = \frac{4 \, \overline{(dy/dx)^2}}{\sqrt{M_\infty^2 - 1}} \tag{56}\]

Equation 57, Ackeret Wave Drag Due to Lift. The wave drag due to lift of a thin flat surface is four times the square of the angle of attack over the Prandtl-Glauert factor, which equals the square of the lift coefficient times that factor divided by four. Ackeret 1925

\[C_{D,w,L} = \frac{4 \alpha^2}{\sqrt{M_\infty^2 - 1}} = \frac{C_L^2 \sqrt{M_\infty^2 - 1}}{4} \tag{57}\]

Equation 58, Spar Cap Area and Root Bending Moment Under Elliptic Loading. The required cap area is the root moment divided by allowable stress and structural depth, and the root moment of an elliptically loaded wing at load factor $n$ is $n W b / 3 \pi$.

\[A_{\text{cap}} = \frac{M_{\text{root}}}{\sigma_{\text{allow}} h_s}, \qquad M_{\text{root}} = \frac{n W b}{3 \pi} \tag{58}\]

Equation 59, Torsional Stiffness from the Bredt Relation. The torsional stiffness of a wing of length $\ell_w$ is the shear modulus times the Bredt torsion constant divided by that length.

\[K_\theta = \frac{G J}{\ell_w}, \qquad J = \frac{4 A_m^2}{\oint \frac{ds}{t}} \tag{59}\]

Equation 60, Divergence and Control Reversal Dynamic Pressures. The typical-section analysis gives the dynamic pressures at which torsional stiffness is overcome by aerodynamic moment for divergence and for aileron reversal.

\[q_D = \frac{K_\theta}{e S C_{L\alpha}}, \qquad q_R = \frac{K_\theta \, C_{L\delta}}{S \bar{c} \, C_{L\alpha} \left| C_{m\delta} \right|} \tag{60}\]

Equation 61, Specific Strength at Operating Temperature. The allowable stress at the wall temperature divided by material density is the figure of merit for a heated structure.

\[\left. \frac{\sigma_{\text{allow}}(T)}{\rho_m} \right|_{T = T_w} \tag{61}\]

Equation 62, Adiabatic Wall Recovery Temperature. The recovery temperature is the static temperature raised by the recovery factor times the stagnation temperature rise.

\[T_r = T_\infty \left( 1 + r \frac{\gamma - 1}{2} M_\infty^2 \right) \tag{62}\]

Equation 63, Yield-to-Modulus Ratio. The ratio of yield stress to Young’s modulus governs the elastic springback of formed sheet. Wikipedia, Ti-6Al-4V Wikipedia, 2024 Aluminium

\[\frac{\sigma_y}{E} \tag{63}\]

Equation 64, Springback of a Bent Sheet. The ratio of bend radius before and after release is a cubic in the group formed by yield stress, bend radius, modulus and sheet thickness.

\[\frac{R_i}{R_f} = 1 - 3 \frac{\sigma_y R_i}{E t_s} + 4 \left( \frac{\sigma_y R_i}{E t_s} \right)^3 \tag{64}\]

Equation 65, Thermal, Propulsive and Overall Efficiency of a Turbojet. The ideal Brayton thermal efficiency depends on compressor pressure ratio, the Froude propulsive efficiency on the exhaust to flight speed ratio, and their product is the overall efficiency.

\[\eta_{th} = 1 - \frac{1}{\pi_c^{\frac{\gamma - 1}{\gamma}}}, \qquad \eta_p = \frac{2}{1 + u_e / u_\infty}, \qquad \eta_0 = \eta_{th} \eta_p \tag{65}\]

Equation 66, Afterburner Thrust Ratio. Afterburning raises exhaust velocity and hence thrust approximately as the square root of the ratio of nozzle to turbine exit total temperatures.

\[\frac{T_{AB}}{T_{\text{dry}}} \approx \sqrt{\frac{T_{07}}{T_{05}}} \tag{66}\]

Equation 67, Point-Mass Equation Used to Separate Thrust from Drag. Only the difference between thrust and drag is measurable from the trajectory, through the acceleration along the path and the gravity component.

\[T - D = m \frac{dV}{dt} + m g \sin \gamma \tag{67}\]

Equation 68, Compressor Face Total Pressure with Ram Compression. The total pressure at the compressor face is the isentropic ram total pressure multiplied by the inlet recovery.

\[p_{02} = p_\infty \left( 1 + \frac{\gamma - 1}{2} M_\infty^2 \right)^{\frac{\gamma}{\gamma - 1}} \cdot \eta_d \tag{68}\]

Equation 69, Oblique Shock Theta-Beta-Mach Relation. The wedge turning angle is related to the oblique shock angle and the upstream Mach number by the standard oblique shock relation.

\[\tan \theta = 2 \cot \beta_o \frac{M_1^2 \sin^2 \beta_o - 1}{M_1^2 \left( \gamma + \cos 2 \beta_o \right) + 2} \tag{69}\]

Equation 70, Moments of Inertia of the X-3. The tabulated roll, pitch and yaw inertias are converted from slug square feet to kilogram square metres. Day 1997

\[I_x = 5.56 \times 10^{3}, \qquad I_y = 8.30 \times 10^{4}, \qquad I_z = 8.83 \times 10^{4} \ \text{kilogram square metres} \tag{70}\]

Equation 71, Pitch-to-Roll Inertia Ratio. The pitch inertia is about fifteen times the roll inertia, an asymmetry three times that of the X-2. Day 1997

\[\frac{I_y}{I_x} = 14.9 \tag{71}\]

Equation 72, Phillips Critical Roll Rate. Divergence in a rolling manoeuvre is expected when the roll rate approaches the lower of the pitch and yaw aerodynamic natural frequencies, as Phillips showed. Phillips 1948

\[\omega_\alpha = \sqrt{\frac{q S \bar{c} \left| C_{m\alpha} \right|}{I_y}}, \qquad \omega_\beta = \sqrt{\frac{q S b \, C_{n\beta}}{I_z}}, \qquad p_{\text{crit}} \approx \min \left( \omega_\alpha, \omega_\beta \right) \tag{72}\]

Equation 73, Dynamic Pressure at Mach 0.92 and 9144 Metres. The Mach number form of dynamic pressure evaluated at the condition of the first roll of October 1954 gives about 17.8 kilopascals. Day 1997

\[q = \frac{\gamma}{2} p M^2 = 0.7 \times 30{,}089 \times 0.846 = 1.78 \times 10^{4} \ \text{pascals} \tag{73}\]

Equation 74, Bespoke Natural Frequencies with Representative Stiffness Coefficients. The pitch and yaw frequencies are evaluated with stiffness coefficients of 0.3 and 0.1 per radian that the article takes as representative.

\[\omega_\alpha = 1.49 \ \text{radians per second}, \qquad \omega_\beta = 1.47 \ \text{radians per second} \tag{74}\]

Equation 75, Bespoke Critical Roll Rate at the First Roll Condition. The lower of the two representative frequencies gives a critical roll rate of 84 degrees per second.

\[p_{\text{crit}} \approx 1.47 \ \text{radians per second} = 84 \ \text{degrees per second} \tag{75}\]

Equation 76, Steady Roll Rate from Aileron Deflection. The steady roll rate balances aileron control power against roll damping and scales with speed over span.

\[p_{ss} = -\frac{C_{l \delta_a} \delta_a}{C_{l p}} \cdot \frac{2 V}{b} \tag{76}\]

Equation 77, Bespoke Supersonic Roll Damping Approximation. The article adopts a roll damping derivative proportional to aspect ratio and inversely proportional to the Prandtl-Glauert factor for a supersonic aspect ratio above about four.

\[C_{lp} \approx -\frac{\pi A}{8 \sqrt{M_\infty^2 - 1}} \quad \text{for } \beta_s A \gtrsim 4 \tag{77}\]

Equation 78, Roll Mode Time Constant. The roll mode time constant is twice the roll inertia times speed divided by the roll damping moment scale.

\[\tau_r = -\frac{2 I_x V}{q S b^2 C_{lp}} \tag{78}\]

Equation 79, First-Order Roll Response. The roll rate approaches its steady value exponentially with the roll mode time constant.

\[p(t) = p_{ss} \left( 1 - e^{-t / \tau_r} \right) \tag{79}\]

Equation 80, Time to Reach the Critical Roll Rate. Inverting the first-order response gives the time at which the roll rate crosses the critical value.

\[t_{\text{crit}} = -\tau_r \ln \left( 1 - \frac{p_{\text{crit}}}{p_{ss}} \right) \tag{80}\]

Equation 81, Divergence Growth Rate Past the Critical Roll Rate. Above the critical rate the pitch motion grows at the square root of the excess of the squared roll rate over the squared pitch frequency, and its reciprocal is the e-folding time.

\[\lambda = \sqrt{p^2 - \omega_\alpha^2}, \qquad \tau_{\text{div}} = \frac{1}{\lambda} \tag{81}\]

Equation 82, Euler Moment Equations with Inertial Cross-Coupling. The pitch and yaw moment equations of a rigid body carry inertial cross terms proportional to the products of body rates.

\[I_y \dot{q} = M + \left( I_z - I_x \right) p r, \qquad I_z \dot{r} = N + \left( I_x - I_y \right) p q \tag{82}\]

Equation 83, Linearised Pitch Equation in a Steady Roll. Linearising about a steady roll rate reduces the effective pitch stiffness by the square of the roll rate and couples pitch to the sideslip rate. Phillips 1948

\[\ddot{\alpha} + \left( \omega_\alpha^2 - p^2 \right) \alpha = \left( \frac{I_z - I_x}{I_y} \right) p \, \dot{\beta} \tag{83}\]

Equation 84, Linearised Yaw Equation in a Steady Roll. The yaw counterpart reduces the effective directional stiffness by the square of the roll rate and couples sideslip to the pitch rate. Phillips 1948

\[\ddot{\beta} + \left( \omega_\beta^2 - p^2 \right) \beta = \left( \frac{I_x - I_y}{I_z} \right) p \, \dot{\alpha} \tag{84}\]

Equation 85, Inertia Coupling Ratios of the X-3. The inertia differences divided by the pitch and yaw inertias give coupling ratios of 1.00 and minus 0.88. Day 1997

\[\mu_1 = \frac{I_z - I_x}{I_y} = 1.00, \qquad \mu_2 = \frac{I_x - I_y}{I_z} = -0.88 \tag{85}\]

Equation 86, Load Factor Increment from an Angle of Attack Excursion. An angle of attack increment produces a normal load factor increment equal to the added lift divided by the weight.

\[\Delta n = \frac{q S C_{L\alpha} \Delta \alpha}{W} \tag{86}\]

Equation 87, Takeoff Speed from Wing Loading. The takeoff speed is the speed at which the maximum lift coefficient supports the weight.

\[V_{TO} = \sqrt{\frac{2 W}{\rho S C_{L,\max}}} \tag{87}\]

Equation 88, Bespoke Sea-Level Takeoff Speed with an Assumed Maximum Lift Coefficient. The takeoff speed is evaluated with a maximum lift coefficient of 0.9 that the article treats as optimistic, giving 108 metres per second.

\[V_{TO} = \sqrt{\frac{2 \times 99{,}646}{1.225 \times 15.47 \times 0.9}} = 108 \ \text{metres per second} \tag{88}\]

Equation 89, Ground Roll at Constant Acceleration. The ground roll is the square of takeoff speed over twice the acceleration that thrust leaves after drag and rolling friction.

\[s_{TO} = \frac{V_{TO}^2}{2 a}, \qquad a \approx \frac{T - D - \mu \left( W - L \right)}{m} \tag{89}\]

Equation 90, Ground Roll with Drag and Rolling Friction. Integrating speed over acceleration with the drag and friction terms retained gives the ground roll distance.

\[s_{TO} = \int_0^{V_{TO}} \frac{m V \, dV}{T - \frac{1}{2} \rho V^2 S \left( C_D - \mu C_L \right) - \mu m g} \tag{90}\]

Equation 91, Lift-Off Condition. At lift-off the lift at takeoff speed and takeoff lift coefficient equals the weight.

\[\frac{1}{2} \rho V_{TO}^2 S C_{L,TO} = W \tag{91}\]

Equation 92, Climb Gradient. The sine of the climb angle is the thrust-to-weight ratio less the reciprocal of the lift-to-drag ratio.

\[\sin \gamma_{\text{climb}} = \frac{T}{W} - \frac{1}{L / D} \tag{92}\]

Equation 93, Bespoke Climb Gradient After Lift-Off. A subsonic lift-to-drag ratio near 8 that the article assumes at climb lift coefficient leaves a gradient of 0.315 with a thrust-to-weight ratio of 0.44.

\[0.44 - 0.125 = 0.315 \tag{93}\]

Equation 94, Landing Gear Vertical Kinetic Energy. The landing gear absorbs the kinetic energy of the sink rate at touchdown.

\[E_{\text{gear}} = \frac{1}{2} m w_s^2 \tag{94}\]

Equation 95, Landing Distance at Constant Braking Deceleration. The landing roll is the square of touchdown speed over twice the mean braking deceleration.

\[s_L = \frac{V_{TD}^2}{2 \bar{a}_{\text{brake}}} \tag{95}\]

Equation 96, Brake Energy. The brakes absorb the kinetic energy at touchdown less the work done by aerodynamic drag during the roll.

\[E_{\text{brake}} = \frac{1}{2} m V_{TD}^2 - \int_0^{s_L} D \, ds \tag{96}\]

Equation 97, Tire Ground Speed Limit. The touchdown ground speed, which is airspeed less headwind, must not exceed the tire speed rating.

\[V_{\text{ground}} = V_{TD} - V_{\text{wind}} \le V_{\text{tire}} \tag{97}\]

Equation 98, Landing Gear Stroke for a Load Factor Limit. The stroke needed to absorb a sink rate at a chosen gear load factor follows from uniform deceleration.

\[s_{\text{stroke}} = \frac{w_s^2}{2 g \left( n_g - 1 \right)} \tag{98}\]

Equation 99, Vane Corrections for Body Rotation. Angle of attack and sideslip measured by boom vanes are corrected for the flow induced by pitch and yaw rates at the boom length.

\[\alpha_{\text{true}} = \alpha_{\text{vane}} - \frac{\ell_b \, q}{V}, \qquad \beta_{\text{true}} = \beta_{\text{vane}} + \frac{\ell_b \, r}{V} \tag{99}\]

Equation 100, Law of Propagation of Uncertainty. The combined variance of a derived quantity is the sum of the input variances weighted by the squared sensitivity coefficients.

\[u_c^2(y) = \sum_i \left( \frac{\partial y}{\partial x_i} \right)^2 u^2(x_i) \tag{100}\]

Equation 101, Nyquist Sampling Criterion. The sample rate must exceed twice the highest frequency of interest.

\[f_s > 2 f_{\max} \tag{101}\]

Equation 102, Recorded Bit Budget. The data rate is the number of channels times the sample rate times the bits per sample.

\[B = N_c f_s b \tag{102}\]

Equation 103, Quantisation Step and Quantisation Noise. A converter of $b$ bits divides the full scale into steps whose uniform rounding error has a standard deviation of the step over the square root of twelve.

\[\Delta = \frac{FS}{2^b}, \qquad \sigma_q = \frac{\Delta}{\sqrt{12}} \tag{103}\]

Equation 104, Propagation of Inertia Uncertainty into the Critical Roll Rate. Because the critical rate varies as the inverse square root of an inertia, its relative uncertainty is half the relative uncertainty of the inertia.

\[\frac{u(p_{\text{crit}})}{p_{\text{crit}}} = \frac{1}{2} \frac{u(I)}{I} \tag{104}\]

Equation 105, Compound Pendulum Period and the Parallel Axis Theorem. The swing period of a compound pendulum gives the inertia about the pivot, and the parallel axis theorem transfers it to the centre of gravity.

\[T_{\text{swing}} = 2 \pi \sqrt{\frac{I_p}{m g \ell_p}}, \qquad I = I_p - m \ell_p^2 \tag{105}\]

Equation 106, Uncertainty of an Inertia Found by Swing Test. Propagating period and pivot distance uncertainties through the pendulum relation amplifies them by the ratio of pivot inertia to centre of gravity inertia.

\[\frac{u(I)}{I} \approx \frac{I_p}{I} \sqrt{ \left( 2 \frac{u(T_{\text{swing}})}{T_{\text{swing}}} \right)^2 + \left( \frac{u(\ell_p)}{\ell_p} \right)^2 } \tag{106}\]

Equation 107, Gravity Component in a Dive. In a descent the weight component along the flight path acts as additional thrust.

\[\Delta T_{\text{effective}} = W \sin \gamma \tag{107}\]

Equation 108, Flights Required and Information Gained Under a Gaussian Model. For a Gaussian prior and measurement the number of flights to reach a target uncertainty and the information gained in nats follow from the precision update. Lindley 1956 Chaloner and Verdinelli 1995

\[n^{*} = \left\lceil \sigma_m^2 \left( \frac{1}{\sigma_T^2} - \frac{1}{\sigma_0^2} \right) \right\rceil, \qquad I_n = \frac{1}{2} \ln \frac{\sigma_0^2}{\sigma_n^2} \tag{108}\]

Equation 109, Bespoke Airframe Attrition Condition. The series sizes the airframe count as the smallest number for which the binomial probability of fewer losses than airframes over $n$ flights reaches the stated confidence.

\[\sum_{i=0}^{n_a - 1} \binom{n}{i} p^i (1-p)^{n-i} \ge 1 - \alpha \tag{109}\]

Equation 110, Mass and Inertia Similarity Groups for a Dynamic Model. A dynamically scaled model must match the relative density and the nondimensional roll and pitch inertias of the full-scale aircraft.

\[\mu_m = \frac{m}{\rho S b}, \qquad \hat{I}_x = \frac{I_x}{\rho S b^3}, \qquad \hat{I}_y = \frac{I_y}{\rho S \bar{c}^3} \tag{110}\]

Equation 111, Reduced Frequency. The reduced frequency is the circular frequency of the motion multiplied by the time the flow takes to cross half the span.

\[k = \frac{\omega b}{2 V} \tag{111}\]

Equation 112, Inertia Scaling of a Dynamically Similar Model. A model at geometric scale $1/k_g$ must have its inertias reduced by the fifth power of the scale and the ratio of air densities.

\[I_m = \frac{I_f}{k_g^5} \cdot \frac{\rho_m}{\rho_f} \tag{112}\]

Equation 113, Posterior Uncertainty After Two Departures. Averaging two independent measurements reduces the uncertainty by the square root of two.

\[\sigma_n = \frac{\sigma_m}{\sqrt{n}} = \frac{\sigma_m}{\sqrt{2}} \tag{113}\]

Equation 114, Gear Energy and Touchdown Speed Scaling. The gear energy grows with the square of sink rate, and touchdown speed scales as the square root of wing loading over maximum lift coefficient.

\[E_{\text{gear}} = \frac{1}{2} m w_s^2, \qquad V_{TD} \propto \sqrt{\frac{W/S}{C_{L,\max}}} \tag{114}\]

Notation

• $M_\infty$, the free-stream Mach number
• $M_1$, the Mach number ahead of a shock
• $\gamma$, the ratio of specific heats, taken as 1.4 for air, and in the trajectory relations the flight path angle
• $q$, the dynamic pressure, and in the body-axis relations the pitch rate
• $S$, the wing reference area
• $b$, the wing span
• $\bar{c}$, the mean aerodynamic chord
• $A$, the wing aspect ratio
• $W$, the aircraft weight
• $T$, the thrust
• $D$, the drag
• $C_D$, the drag coefficient
• $C_L$, the lift coefficient
• $C_{L\alpha}$, the lift-curve slope per radian
• $C_{L,\max}$, the maximum lift coefficient
• $C_{m\alpha}$, the pitching moment slope with angle of attack
• $C_{n\beta}$, the directional stability derivative
• $C_{lp}$, the roll damping derivative
• $I_x$, the moment of inertia in roll
• $I_y$, the moment of inertia in pitch
• $I_z$, the moment of inertia in yaw
• $\omega_\alpha$, the torsional natural frequency in the flutter relations and the pitch aerodynamic natural frequency in the coupling analysis
• $\omega_\beta$, the yaw aerodynamic natural frequency
• $p_{\text{crit}}$, the critical roll rate for inertia-coupled divergence
• $\tau$, the wing thickness-to-chord ratio
• $\rho$, the air density
• $P_s$, the specific excess power
• $h_e$, the energy height
• $\eta_d$, the inlet total pressure recovery
• $SM$, the static margin as a fraction of the mean aerodynamic chord
• $x_{np}$, the longitudinal position of the neutral point
• $V_{TO}$, the takeoff speed
• $V_{TD}$, the touchdown speed
• $w_s$, the sink rate at touchdown
• $\sigma_0$, the prior uncertainty in the quantity a campaign measures
• $\sigma_m$, the uncertainty of a single flight measurement
• $\sigma_T$, the target uncertainty
• $\sigma_n$, the posterior uncertainty after $n$ flights
• $n^{*}$, the number of flights needed to reach the target uncertainty
• $I_n$, the information gained from $n$ flights in nats
• $n_a$, the number of airframes
• $\lambda$, the growth rate of a coupled divergence
• $\mu_m$, the mass ratio of the wing or aircraft to the surrounding air
• $\mu_1$, the pitch inertia coupling ratio
• $\mu_2$, the yaw inertia coupling ratio
• $\ell_b$, the boom length ahead of the centre of gravity
• $f_s$, the sample rate
• $\theta$, the local surface inclination or flow turning angle in radians
• $h_s$, the structural depth of the wing box
• $A_{\text{cap}}$, the spar cap area
• $K_\theta$, the torsional stiffness of the wing
• $A_m$, the area enclosed by the wing box
• $p_{02}$, the total pressure at the compressor face
• $A_0$, the free-stream area of the stream tube the engine demands
• $A_c$, the inlet capture area
• $D_{\text{add}}$, the additive drag of a spilling inlet
• $\beta_s A$, the supersonic aspect ratio parameter
• $p_{ss}$, the steady roll rate
• $\tau_r$, the roll mode time constant
• $T_r$, the adiabatic wall recovery temperature
• $\sigma_y$, the yield stress
• $t_s$, the sheet thickness
• $\pi_c$, the compressor pressure ratio
• $k_g$, the geometric scale factor of a dynamic model

References

Primary Sources, Peer-Reviewed

• Aarnes, Magne N., and John L. White. 1975b. “Propulsion System and Airframe Structural Integration Program.” Journal of Aircraft 12 (4): 234–42. https://doi.org/10.2514/3.44438
• Abbas, Laith K., Xiaoting Rui, and P. Marzocca. 2011. “Panel Flutter Analysis of Plate Element Based on the Absolute Nodal Coordinate Formulation.” Multibody System Dynamics 27 (2): 135–52. https://doi.org/10.1007/s11044-011-9268-5
• Abdel-Motagaly, Khaled, Xinyun Guo, Bin Duan, and Chuh Mei. 2005. “Active Control of Nonlinear Panel Flutter under Yawed Supersonic Flow.” AIAA Journal 43 (3): 671–80. https://doi.org/10.2514/1.13840
• Abed, Eyad H., and Hsien-Chiarn Lee. 1990. “Nonlinear Stabilization of High Angle-of-Attack Flight Dynamics Using Bifurcation Control.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4791129
• Abedi, M., R. Askari, and M. R. Soltani. 2020. “Numerical Simulation of Inlet Buzz.” Aerospace Science and Technology 97: 105547. https://doi.org/10.1016/j.ast.2019.105547
• Abraham, Troy, David Lazzara, and Douglas Hunsaker. 2024. “Multifidelity Comparison of Supersonic Wave Drag Prediction Methods Using Axisymmetric Bodies.” Aerospace 11 (5): 359. https://doi.org/10.3390/aerospace11050359
• Abu-Akeel, A. K. 1969. “Damping of High-Frequency Brake Vibrations in Aircraft Landing Gear.” Journal of Aircraft 6 (1): 24–30. https://doi.org/10.2514/3.43996
• Abzug, Malcolm J. 1999a. “Directional Stability and Control during Landing Rollout.” Journal of Aircraft 36 (3): 584–90. https://doi.org/10.2514/2.2474
• Agrawal, S. K. 1985. “High-Speed Braking of an Aircraft Tire on Grooved Surfaces.” Journal of Aircraft 22 (12): 1092–96. https://doi.org/10.2514/3.45255
• Agrawal, Shreekant, Thomas A. Kinard, and Arthur G. Powell. 1991. “Supersonic Boundary-Layer Stability Analysis on an Aircraft Wing.” Journal of Aircraft 28 (11): 721–27. https://doi.org/10.2514/3.46088
• “Aircraft Carbon Brake for a 22 in Diameter Wheel.” 1973. Composites 4 (3): 98. https://doi.org/10.1016/0010-4361(73)90575-2
• Akcal, M. Ugur, Batuhan Hostas, and N. Kemal Ure. 2018. “Rate Envelope Based Time Efficient Strategy for Upset Recovery of a Fighter Aircraft.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396500
• Akishita, Sadao, Ryujiro Kurosaki, Kanzo Okada, and Tomoji Hirata. 1986. “Theoretical Prediction of Roll Moment on Wing-Controlled Missile.” Journal of Aircraft 23 (11): 808–13. https://doi.org/10.2514/3.45385
• Akula, Sai Pratyush, Mihir Ojha, Kolla Lakshman Rao, and Amit Kumar Gupta. 2023. “A Review on Superplastic Forming of Ti-6Al-4V and Other Titanium Alloys.” Materials Today Communications 34: 105343. https://doi.org/10.1016/j.mtcomm.2023.105343
• Alighanbari, H. 2002. “Aeroelastic Response of an Airfoil-Aileron Combination with Freeplay in Aileron Hinge.” Journal of Aircraft 39 (4): 711–13. https://doi.org/10.2514/2.2986
• Alimov, Artem, Danila Evdokimov, and Sergey Evsyukov. 2019. “Temperature and Strain Rate Dependent Friction Model for Hot Forming of Ti-6Al-4V Titanium Alloy.” Materials Today: Proceedings 19: 1994–97. https://doi.org/10.1016/j.matpr.2019.07.059
• Altunkaya, Ege Ç., Akın Çatak, Emre Koyuncu, and İbrahim Özkol. 2025. “Loss-of-Control Prevention of an Agile Aircraft: Dynamic Command Saturation Approach.” Journal of Guidance, Control, and Dynamics 48 (2): 424–36. https://doi.org/10.2514/1.g008188
• 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
• Amiet, Roy K. 1974. “Compressibility Effects in Unsteady Thin-Airfoil Theory.” AIAA Journal 12 (2): 252–55. https://doi.org/10.2514/3.49212
• Amiet, Roy K. 1976. “High Frequency Thin-Airfoil Theory for Subsonic Flow.” AIAA Journal 14 (8): 1076–82. https://doi.org/10.2514/3.7187
• Amin, Nasim F., and David J. Hollweger. 1983. “F/A-18 Inlet/engine Compatibility Flight Test Results.” Journal of Aircraft 20 (8): 641–49. https://doi.org/10.2514/3.44924
• Amirzadegan, Sadegh, Seyyed Mohammad Mousavi Safavi, and Amir Jafarzade. 2019. “Supersonic Panel Flutter Analysis Assuming Effects of Initial Structural Stresses.” Journal of The Institution of Engineers (India): Series C 100 (5): 833–39. https://doi.org/10.1007/s40032-019-00532-y
• Ananthkrishnan, N., and K. Sudhakar. 1994. “Prevention of Jump in Inertia-Coupled Roll Maneuvers of Aircraft.” Journal of Aircraft 31 (4): 981–83. https://doi.org/10.2514/3.46591
• Ananthkrishnan, N., and K. Sudhakar. 1995. “Inertia-Coupled Coordinated Roll Maneuvers of Airplanes.” Journal of Aircraft 32 (4): 883–84. https://doi.org/10.2514/3.46807
• 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, Seth B. 1985. “Handling Qualities Related to Stall/spin Accidents of Supersonic Fighter Aircraft.” Journal of Aircraft 22 (10): 875–80. https://doi.org/10.2514/3.45218
• Anderson, D. C., R. L. Berger, and J. R. Hess. 1973. “Maneuver Load Control and Relaxed Static Stability Applied to aContemporary Fighter Aircraft.” Journal of Aircraft 10 (2): 112–20. https://doi.org/10.2514/3.60204
• Andrew, G. M., and M. S. Cahn. 1967. “Determination of Subsonic Drag Rise by Hodograph Plane Analysis.” Journal of Aircraft 4 (3): 267–70. https://doi.org/10.2514/3.43832
• Andrew, G. M., and J. H. Polve. 1952. “Frequency Response of an Airplane from Flight-Test Data.” Journal of the Aeronautical Sciences 19 (4): 285–285. https://doi.org/10.2514/8.2257
• Ao, Dongwei, Xingrong Chu, Yang Yang, Shuxia Lin, and Jun Gao. 2018. “Effect of Electropulsing on Springback during V-Bending of Ti-6Al-4V Titanium Alloy Sheet.” International Journal of Advanced Manufacturing Technology 96 (9–12): 3197–3207. https://doi.org/10.1007/s00170-018-1654-1
• Appa, Kari, and Michael J. C. Smith. 1988. “Evaluation of the Constant Pressure Panel Method (CPM) for Unsteady Air Loads Prediction.” In Structures. https://ntrs.nasa.gov/citations/19880045008
• Aprovitola, Andrea, Pasquale Emanuele Di Nuzzo, Giuseppe Pezzella, and Antonio Viviani. 2021. “Aerodynamic Analysis of a Supersonic Transport Aircraft at Landing Speed Conditions.” Energies 14 (20): 6615. https://doi.org/10.3390/en14206615
• Apte, Y. S., and V. V. Athani. 1979. “Optimal Autostabilizer for a Supersonic Fighter Aircraft.” Journal of Guidance and Control 2 (2): 97–98. https://doi.org/10.2514/3.55842
• Ardonceau, Pascal L. 1989. “Unsteady Pressure Distribution over a Pitching Airfoil.” AIAA Journal 27 (5): 660–62. https://doi.org/10.2514/3.10160
• Arnold, Lee. 1942. “Vector Solution of the Three-Degree Case of Wing Bending, Wing Torsion, Aileron Flutter.” Journal of the Aeronautical Sciences 9 (13): 497–500. https://doi.org/10.2514/8.10949
• Aryasomayajula, S., H. Wang, R. Grandhi, and F. Eastep. 2001. “Multidisciplinary Design of Vehicle Structures with Improved Roll Maneuverability-Transonic Regime.” Journal of Aircraft 38 (4): 664–71. https://doi.org/10.2514/2.2817
• Asadi, Davood, and Touraj Farsadi. 2020. “Active Flutter Control of Thin Walled Wing-Engine System Using Piezoelectric Actuators.” Aerospace Science and Technology 102: 105853. https://doi.org/10.1016/j.ast.2020.105853
• Ashley, Holt. 1980. “Role of Shocks in the ‘Sub-Transonic’ Flutter Phenomenon.” Journal of Aircraft 17 (3): 187–97. https://doi.org/10.2514/3.57891
• Augenstein, Bruno W. 1950. “Second-Order Two-Dimensional Supersonic Airfoil Theory.” Journal of the Aeronautical Sciences 17 (2): 126–126. https://doi.org/10.2514/8.1545
• Avanzini, Giulio, and Guido de Matteis. 1997. “Bifurcation Analysis of a Highly Augmented Aircraft Model.” Journal of Guidance, Control, and Dynamics 20 (4): 754–59. https://doi.org/10.2514/2.4108
• Axelson, John A. 1977. “Estimation of Transonic Aircraft Aerodynamics to High Angles of Attack.” Journal of Aircraft 14 (6): 553–59. https://doi.org/10.2514/3.58819
• Azevedo, David J., Ching Shi Liu, and William J. Rae. 1990. “Prediction of Inviscid Stagnation Pressure Losses in Supersonic Inlet Flows.” AIAA Journal 28 (10): 1834–36. https://doi.org/10.2514/3.10486
• Baals, Donald D., A. Warner Robins, and Roy V. Harris. 1970. “Aerodynamic Design Integration of Supersonic Aircraft.” Journal of Aircraft 7 (5): 385–95. https://doi.org/10.2514/3.59441
• 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
• Bae, Jae-Sung, Seung-Man Yang, and In Lee. 2002. “Linear and Nonlinear Aeroelastic Analysis of Fighter-Type Wing with Control Surface.” Journal of Aircraft 39 (4): 697–708. https://doi.org/10.2514/2.2984
• Baghdadi, N., M. H. Lowenberg, and A. T. Isikveren. 2011. “Analysis of Flexible Aircraft Dynamics Using Bifurcation Methods.” Journal of Guidance, Control, and Dynamics 34 (3): 795–809. https://doi.org/10.2514/1.51468
• Bagherzadeh, Seyed Amin, Hamed Mohammadkarimi, and Mohammad Hossein Alizadeh. 2025. “Enhanced Synchrosqueezing Transform for Detecting Non-Traditional Flight Modes in High Angle of Attack Maneuvers.” Mathematical and Computational Applications 30 (2): 41. https://doi.org/10.3390/mca30020041
• Bai, Pengkun, Xiaolei Chong, Guanhu Wang, Chaojia Liu, and Qiqi Chen. 2022. “Research on Simulation Calculation Method of Takeoff and Landing Running Distance for New Type Aircraft.” In 2022 2nd International Conference on Computational Modeling, Simulation and Data Analysis (CMSDA). IEEE. https://doi.org/10.1109/cmsda58069.2022.00073
• Bai, Lu, Wenjian Deng, and Zhanxue Wang. 2025. “Study on the Influence of Sharp / Blunt Fuselage on the Aerodynamic Performance of Supersonic Nacelle.” In 2025 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero63441.2025.11068451
• Ball, W. H., and P. A. Ross. 1972. “Experimental Correlation of Installation Effects on Inlet Pressure Recovery.” Journal of Aircraft 9 (8): 596–601. https://doi.org/10.2514/3.59042
• Balli, Ozgur. 2017. “Advanced Exergy Analyses to Evaluate the Performance of a Military Aircraft Turbojet Engine (TJE) with Afterburner System: Splitting Exergy Destruction into Unavoidable/avoidable and Endogenous/exogenous.” Applied Thermal Engineering 111: 152–69. https://doi.org/10.1016/j.applthermaleng.2016.09.036
• Bambach, Margarita D., Daniel Seifert, and Irina Sizova. 2020. “Intensive Forming of Grade 5 Titanium Bars with Increased Performance for Aerospace Applications.” Procedia Manufacturing 47: 288–94. https://doi.org/10.1016/j.promfg.2020.04.229
• Bantscheff, K., and C. Breitsamter. 2024. “Design and Investigation of an Aeroelastically Scaled Delta-Wing Wind Tunnel Model for Dynamic Load Analysis.” CEAS Aeronautical Journal 16 (1): 275–91. https://doi.org/10.1007/s13272-024-00795-x
• Barrows, Timothy M. 1977. “Simplified Methods of Predicting Aircraft Rolling Moments Due to Vortex Encounters.” Journal of Aircraft 14 (5): 434–39. https://doi.org/10.2514/3.58799
• Barry, Frank W. 1971. “An Explicit Formula for Additive Drag of a Supersonic Conical Inlet.” Journal of Aircraft 8 (4): 279–80. https://doi.org/10.2514/3.44269
• Barton, M. V. 1948. “Stability of an Oscillating Airfoil in Supersonic Airflow.” Journal of the Aeronautical Sciences 15 (6): 371–76. https://doi.org/10.2514/8.11592
• 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
• Bashkin, V. A., I. V. Egorov, and V. V. Pafnut’ev. 2005. “Aerodynamic Heating of a Thin Sharp-Nose Circular Cone in Supersonic Flow.” High Temperature 43 (5): 733–45. https://doi.org/10.1007/s10740-005-0118-0
• Basta, Ehab, Mehdi Ghommem, and Samir Emam. 2021. “Flutter Control and Mitigation of Limit Cycle Oscillations in Aircraft Wings Using Distributed Vibration Absorbers.” Nonlinear Dynamics 106 (3): 1975–2003. https://doi.org/10.1007/s11071-021-06889-z
• Batina, John T. 1986a. “Unsteady Transonic Flow Calculations for Interfering Lifting Surfaceconfigurations.” Journal of Aircraft 23 (5): 422–30. https://doi.org/10.2514/3.45324
• Batina, John T. 1986b. “Unsteady Transonic Flow Calculations for Wing/fuselage Configurations.” Journal of Aircraft 23 (12): 897–903. https://doi.org/10.2514/3.45398
• Batina, John T. 1989. “Unsteady Transonic Algorithm Improvements for Realistic Aircraft Applications.” Journal of Aircraft 26 (2): 131–39. https://doi.org/10.2514/3.45734
• Batista Ponce, Moises, Juan Manuel Vazquez-Martinez, Joao Paulo Davim, and Jorge Salguero Gomez. 2019. “Analysis of Secondary Adhesion Wear Mechanism on Hard Machining of Titanium Aerospace Alloy.” Materials 12 (12): 2015. https://doi.org/10.3390/ma12122015
• 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
• Becker, S., F. Durst, and H. Lienhart. n.d. “LDA System for in-Flight Local Velocity Measurements on Airplane Wings.” In ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025). IEEE. https://doi.org/10.1109/iciasf.1999.827165
• Belhassen, L., S. Koubaa, M. Wali, and F. Dammak. 2016. “Numerical Prediction of Springback and Ductile Damage in Rubber-Pad Forming Process of Aluminum Sheet Metal.” International Journal of Mechanical Sciences 117: 218–26. https://doi.org/10.1016/j.ijmecsci.2016.08.015
• Ben Said, Lotfi, Abir Bouhamed, Mondher Wali, et al. 2025. “Anisotropic Plasticity in Sheet Metal Forming: Experimental and Numerical Analysis of Springback Using U-Bending Test.” Machines 13 (11): 1029. https://doi.org/10.3390/machines13111029
• Bendiksen, Oddvar O. 2009. “High-Altitude Limit Cycle Flutter of Transonic Wings.” Journal of Aircraft 46 (1): 123–36. https://doi.org/10.2514/1.36413
• Beneda, Karoly. 2021. “Investigation of Novel Thrust Parameters to Variable Geometry Turbojet Engines.” In 2021 IEEE 19th World Symposium on Applied Machine Intelligence and Informatics (SAMI). IEEE. https://doi.org/10.1109/sami50585.2021.9378633
• Bennett, Robert M., John T. Batina, and Herbert J. Cunningham. 1989. “Wing-Flutter Calculations with the CAP-TSD Unsteady Transonic Small-Disturbance Program.” Journal of Aircraft 26 (9): 876–82. https://doi.org/10.2514/3.45854
• Bennett, Robert M., Eleanor C. Wynne, and Dennis G. Mabey. 1987. “Calculation of Transonic Steady and Oscillatory Pressures on a Low Aspect Ratio Model.” Journal of Aircraft 24 (6): 392–98. https://doi.org/10.2514/3.45458
• Bera, Rajendra K. 1977. “Remarks on Thin Airfoil Theory.” Journal of Aircraft 14 (5): 508–9. https://doi.org/10.2514/3.44608
• Bera, Rajendra K. 1988. “Evaluation of Two Singular Integrals from Thin Airfoil Theory.” Journal of Aircraft 25 (4): 383–84. https://doi.org/10.2514/3.45575
• Berkowitz, Samuel M. 1950. “Airplane Performance, Stability and Control.” Journal of the Franklin Institute 249 (6): 503–4. https://doi.org/10.1016/0016-0032(50)90415-7
• Berryman, R. G., J. C. Chesnuttf, F. H. Froes, and J. C. Williams. 1977. “A New Titanium Alloy with Improved Fracture Toughness: Ti-4.5A1-5Mo-l.5Cr.” Journal of Aircraft 14 (12): 1182–85. https://doi.org/10.2514/3.58912
• Beyers, Martin E. 1995. “Interpretation of Experimental High-Alpha Aerodynamics: Implications for Flight Prediction.” Journal of Aircraft 32 (2): 247–61. https://doi.org/10.2514/3.46710
• Beyers, M. E., and L. E. Ericsson. 2002. “Comment on ‘Equivalence between Sideslip and Roll in Wind-Tunnel Model Testing’.” Journal of Aircraft 39 (4): 719–20. https://doi.org/10.2514/2.2989
• Bezborodova, Kristina, and Evgeny Filinov. 2021. “Double Bypass Turbojet Engine Analysis.” In 2021 International Scientific and Technical Engine Conference (EC). IEEE. https://doi.org/10.1109/ec52789.2021.10016815
• Bhatia, Manav, and Philip Beran. 2018. “Influence of Aerodynamic Nonlinearity Due to Static Panel-Curvature on Flutter of Panels at Transonic and Low Supersonic Mach Numbers.” Journal of Fluids and Structures 81: 574–97. https://doi.org/10.1016/j.jfluidstructs.2018.05.015
• Bibin, C., Micheal Johnson Selvaraj, and S. Sanju. 2012. “Flutter Analysing over an Aircraft Wing during Cruise Speed.” Procedia Engineering 38: 1950–61. https://doi.org/10.1016/j.proeng.2012.06.238
• Bihrle, William, and Billy Barnhart. 1982. “Departure Susceptibility and Uncoordinated Roll-Reversal Boundaries for Fighter Configurations.” Journal of Aircraft 19 (11): 897–903. https://doi.org/10.2514/3.44789
• Bílek, Michal, Jiří Maxa, Pavla Šabacká, et al. 2025. “Application of a Total Pressure Sensor in Supersonic Flow for Shock Wave Analysis under Low-Pressure Conditions.” Sensors 25 (20): 6291. https://doi.org/10.3390/s25206291
• Billah, Md Maruf, and Pınar Acar. 2026. “Can Anisotropy Contribute to Tuning Thermal Expansion of Titanium Alloy Structures?” Journal of Aircraft: 1–11. https://doi.org/10.2514/1.c038952
• 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
• Birks, A. W., and C. Ludlow. 1969. “A Strain Gauge Load Cell for the Measurement of Compressive Loads Under.” Strain 5 (4): 218–20. https://doi.org/10.1111/j.1475-1305.1969.tb01623.x
• Bismarck-Nasr, Maher N. 1993. “Supersonic Panel Flutter Analysis of Shallow Shells.” AIAA Journal 31 (7): 1349–51. https://doi.org/10.2514/3.49073
• 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
• Blake, William, Carl Gotwald, Michael Mayor, and Thomas Cunningham. 2009. “Lateral Stability of High Wing Configurations.” Journal of Aircraft 46 (6): 2176–78. https://doi.org/10.2514/1.44911
• Blázquez, A. L. González. 1990. “Mathematical Modelling for Analysis of Nonlinear Aircraft Dynamics.” Computers & Structures 37 (2): 193–97. https://doi.org/10.1016/0045-7949(90)90401-m
• Bleviss, Zegmund O. 1951. “Some Roll Characteristics of Cruciform Delta Wings at Supersonic Speeds.” Journal of the Aeronautical Sciences 18 (5): 289–97. https://doi.org/10.2514/8.1945
• Bloy, A. W., and K. A. Lea. 1995. “Directional Stability of a Large Receiver Aircraft in Air-to-Air Refueling.” Journal of Aircraft 32 (2): 453–55. https://doi.org/10.2514/3.46741
• Boelens, Okko J. 2017. “Flow Analysis of the F-16XL Aircraft at Transonic Flow Conditions.” Journal of Aircraft 54 (2): 388–94. https://doi.org/10.2514/1.c033211
• Bonney, E. Arthur. 1947. “Aerodynamic Characteristics of Rectangular Wings at Supersonic Speeds.” Journal of the Aeronautical Sciences 14 (2): 110–16. https://doi.org/10.2514/8.1275
• Borglund, Dan. 2005. “Upper Bound Flutter Speed Estimation Using the Mu-k Method.” Journal of Aircraft 42 (2): 555–57. https://doi.org/10.2514/1.7586
• Boris, Loginov, Badokina Tatyana, and Rousak Youri. 2011. “Divergence of a Thin Elongated Plate in Supersonic Gas Flow.” PAMM 11 (1): 679–80. https://doi.org/10.1002/pamm.201110329
• Bos, Adolf H. W. 1999. “Intake-Engine Matching for High-Speed Civil Transport Powerplant Design and Analysis.” Aircraft Design 2 (2): 95–104. https://doi.org/10.1016/s1369-8869(99)00009-9
• Bouton, Innes. 1950. “Lift-Curve Slope for Swept and Unswept Wings.” Journal of the Aeronautical Sciences 17 (3): 185–185. https://doi.org/10.2514/8.1573
• Bouton, Innes. 1951. “Airplane Pitching Moment of Inertia.” Journal of the Aeronautical Sciences 18 (2): 140–41. https://doi.org/10.2514/8.1879
• Boyden, Richmond P. 1971. “Effects of Leading-Edge Vortex Flow on the Roll Damping of Slender Wings.” Journal of Aircraft 8 (7): 543–47. https://doi.org/10.2514/3.59135
• Boyer, R. R., and P. T. Finden. 1972. “An Elevated Temperature Exposure Study of β-III Titanium Alloy.” Metallurgical Transactions 3 (3): 744–47. https://doi.org/10.1007/bf02642767
• Bramsiepe, Kjell, Arne Voß, and Thomas Klimmek. 2020. “Design and Sizing of an Aeroelastic Composite Model for a Flying Wing Configuration with Maneuver, Gust, and Landing Loads.” CEAS Aeronautical Journal 11 (3): 677–91. https://doi.org/10.1007/s13272-020-00446-x
• Bridges, David H. 2008. “Thrust and Drag Models for Performance Calculations for High-Speed Aircraft.” Journal of Aircraft 45 (4): 1358–66. https://doi.org/10.2514/1.34919
• Brodersen, O. 2002. “Drag Prediction of Engine-Airframe Interference Effects Using Unstructured Navier-Stokes Calculations.” Journal of Aircraft 39 (6): 927–35. https://doi.org/10.2514/2.3037
• Broggiato, Giovanni B., Francesca Campana, and Edoardo Mancini. 2012. “Computer-Aided Engineering for Sheet Metal Forming: Definition of a Springback Quality Function.” Engineering with Computers 29 (3): 319–27. https://doi.org/10.1007/s00366-012-0285-7
• Bryson, A. E., and R. H. Edwards. 1952. “The Effect of Nonuniform Surface Temperature on the Transient Aerodynamic Heating of Thin-Skinned Bodies.” Journal of the Aeronautical Sciences 19 (7): 471–75. https://doi.org/10.2514/8.2343
• 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
• Burken, John J., Gurbux S. Alag, and Glenn B. Gilyard. 1986. “Aeroelastic Control of Oblique-Wing Aircraft.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4788986
• Burt, Glen E. 1975. “Forced-Oscillation Test Mechanism for Measuring Dynamic-Stability Derivatives in Roll.” Journal of Aircraft 12 (1): 11–17. https://doi.org/10.2514/3.59795
• Bustard, Andrew N., Benjamin L. Bemis, Aaron Marques, Matthew J. Zahr, and Thomas J. Juliano. 2026b. “Global Time-Resolved Measurements of Inlet/Isolator Unstart Induced by Mass Injection.” Journal of Propulsion and Power 42 (3): 505–24. https://doi.org/10.2514/1.b40160
• Bustard, Andrew N., Mark Noftz, Joseph S. Jewell, and Thomas J. Juliano. 2026a. “Global Measurements of Unstart in an Internal Osculating Waverider Inlet.” AIAA Journal: 1–8. https://doi.org/10.2514/1.j067385
• Buzzetti, C. J., and W. L. Howland. 1945. “Measurement of Maneuvering Loads in Flight.” Journal of the Aeronautical Sciences 12 (2): 195–202. https://doi.org/10.2514/8.11222
• Byun, Chansup, and Guru P. Guruswamy. 1998. “Aeroelastic Computations on Wing-Body-Control Configurations on Parallel Computers.” Journal of Aircraft 35 (2): 288–94. https://doi.org/10.2514/2.2297
• Cabral, Myrella V., Flávio D. Marques, and António J. M. Ferreira. 2021. “The Effect of Curvature in Nonlinear Supersonic Flutter of Panels with Adjacent Bays.” Thin-Walled Structures 161: 107379. https://doi.org/10.1016/j.tws.2020.107379
• Cai, Feichao, Guanhong Huang, and Xiaowei Liu. 2022. “Investigation of Shock Wave Oscillation Suppression by Overflow in the Supersonic Inlet.” Energies 15 (11): 3879. https://doi.org/10.3390/en15113879
• Calamaz, Madalina, Dominique Coupard, and Frank Girot. 2010. “Numerical Simulation of Titanium Alloy Dry Machining with a Strain Softening Constitutive Law.” Machining Science and Technology 14 (2): 244–57. https://doi.org/10.1080/10910344.2010.500957
• 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
• Calligeros, John M., and John Dugundji. 1963. “Effects of Orthotropicity Orientation on Supersonic Panel Flutter.” AIAA Journal 1 (9): 2180–82. https://doi.org/10.2514/3.2033
• Campbell, J. L., and S. H. Ellis. 1971. “Engine/Inlet Compatibility Analysis Procedure.” Journal of Aircraft 8 (5): 301–7. https://doi.org/10.2514/3.59101
• Cao, Meng, Ce Zhang, Hexiang Wang, Dawei Liu, Jie Chen, and Yang Tao. 2026. “Unsteady Buzz Characteristics of a Dorsal Supersonic Bump Inlet Based on Wind-Tunnel Tests and Numerical Simulations.” Aerospace 13 (7): 631. https://doi.org/10.3390/aerospace13070631
• Capone, Francis J., D. Bruce Owens, and Robert M. Hall. 2004. “Development of a Transonic Free-To-Roll Test Capability.” Journal of Aircraft 41 (3): 456–63. https://doi.org/10.2514/1.1449
• Carbajosa, Carlos, Ángel Sanz-Andrés, Alejandro Martínez-Cava, Sergio Marín-Coca, and Sebastián Franchini. 2025b. “Approximated Methods for the Analysis of the Unsteady Shock Wave Motion in Inlet Unstart Processes.” Acta Astronautica 236: 882–96. https://doi.org/10.1016/j.actaastro.2025.07.026
• Carbajosa, Carlos, Ángel Sanz-Andrés, Alejandro Martínez-Cava, and Mikel Ogueta-Gutiérrez. 2025a. “Analysis of the Unsteady Shock Wave Motion in Inlet Unstart Processes.” Acta Astronautica 234: 601–18. https://doi.org/10.1016/j.actaastro.2025.05.006
• Carlsen, Wayne D. 1995. “Development of Transonic Area-Rule Methodology.” Journal of Aircraft 32 (5): 1056–61. https://doi.org/10.2514/3.46836
• Carroll, James V., and Raman K. Mehra. 1982. “Bifurcation Analysis of Nonlinear Aircraft Dynamics.” Journal of Guidance, Control, and Dynamics 5 (5): 529–36. https://doi.org/10.2514/3.56198
• Castravete, S. C., and R. A. Ibrahim. 2008. “Effect of Stiffness Uncertainties on the Flutter of a Cantilever Wing.” AIAA Journal 46 (4): 925–35. https://doi.org/10.2514/1.31692
• Castrichini, A., J. E. Cooper, T. Benoit, and Y. Lemmens. 2018. “Gust and Ground Loads Integration for Aircraft Landing Loads Prediction.” Journal of Aircraft 55 (1): 184–94. https://doi.org/10.2514/1.c034369
• Cavagna, L., S. Ricci, and A. Scotti. 2009. “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
• Cella, Ubaldo, and Marco Evangelos Biancolini. 2012. “Aeroelastic Analysis of Aircraft Wind-Tunnel Model Coupling Structural and Fluid Dynamic Codes.” Journal of Aircraft 49 (2): 407–14. https://doi.org/10.2514/1.c031293
• Cestino, Enrico, and Annamaria Iannuzzo. 2026. “Impact of Control Surface Stiffness on Aeroelastic Divergence and Reversal.” Journal of Aircraft 63 (3): 1344–48. https://doi.org/10.2514/1.c038607
• Chaderjian, Neal M. 1994. “Navier-Stokes Prediction of Large-Amplitude Delta-Wing Roll Oscillations.” Journal of Aircraft 31 (6): 1333–40. https://doi.org/10.2514/3.46656
• Chaderjian, Neal M., and Lewis B. Schiff. 1996. “Numerical Simulation of Forced and Free-to-Roll Delta-Wing Motions.” Journal of Aircraft 33 (1): 93–99. https://doi.org/10.2514/3.46908
• Chalal, Hocine, Sever-Gabriel Racz, and Tudor Balan. 2012b. “Springback of Thick Sheet AHSS Subject to Bending under Tension.” International Journal of Mechanical Sciences 59 (1): 104–14. https://doi.org/10.1016/j.ijmecsci.2012.03.011
• Chalk, C. R. 1983. “Excessive Roll Damping Can Cause Roll Ratchet.” Journal of Guidance, Control, and Dynamics 6 (3): 218–19. https://doi.org/10.2514/3.19820
• Chamberlain, Donald. 1969. “Measurement of Drag from Interaction of Jet Exhaust and Airframe.” Journal of Aircraft 6 (2): 160–64. https://doi.org/10.2514/3.44024
• Chan, Y. Y. 1980a. “Life Effect on Transonic Wind-Tunnel Blockage.” Journal of Aircraft 17 (12): 915–16. https://doi.org/10.2514/3.57983
• Chan, Y. Y. 1980b. “Perturbation Analysis of Transonic Wind Tunnel Wall Interference.” Journal of Aircraft 17 (6): 409–11. https://doi.org/10.2514/3.44667
• Chan, John S. 1992. “Viscous Supersonic Flow Computations over a Delta-Rectangular Wing with Slanting Surfaces.” Journal of Spacecraft and Rockets 29 (2): 159–65. https://doi.org/10.2514/3.26330
• Chandrappa, K., C. S. Sumukha, B. B. Sankarsh, and Roshan Gowda. 2020. “Superplastic Forming with Diffusion Bonding of Titanium Alloys.” Materials Today: Proceedings 27: 2909–13. https://doi.org/10.1016/j.matpr.2020.03.514
• Chang, Jen-Fu. 1992. “Minimizing Supersonic Wave Drag with Physical Constraints at Design and off-Design Mach Numbers.” Journal of Aircraft 29 (4): 716–18. https://doi.org/10.2514/3.46228
• Chang, S. Y. 2007. “The Isothermal and Cyclic Oxidation Behavior of a Titanium Aluminide Alloy at Elevated Temperature.” Journal of Materials Engineering and Performance 16 (4): 508–14. https://doi.org/10.1007/s11665-007-9066-7
• Chang, Chieh-Chien, and Cheng-Ting Hsu. 1958. “Solutions to Stoolman’s External Diffusion Equation for Instability of a Normal Shock Inlet Diffuser.” Journal of Jet Propulsion 28 (7): 457–60. https://doi.org/10.2514/8.7350
• Chang, Chieh-Chien, and Cheng-Ting Hsu. 1960. “Aerodynamic Instability of Supersonic Inlet Diffusers.” ARS Journal 30 (5): 468–75. https://doi.org/10.2514/8.5121
• 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
• Chawla, Jagannath P. 1958. “A Vectorial Representation of Aerodynamic Forces Acting on a Thin Rectangular Wing Oscillating Harmonically in Supersonic Potential Flow.” Journal of the Aerospace Sciences 25 (5): 329–30. https://doi.org/10.2514/8.7651
• Chen, Can, Minghe Chen, Lansheng Xie, Zonghui Gong, and Jianhua Ye. 2019b. “Numerical and Experimental Investigations of the Hot Stamping Process for Complex Aircraft Skin Parts Composed of TA32 High-Temperature Titanium Alloy Using an Arrhenius-Type Constitutive Model.” International Journal of Advanced Manufacturing Technology 103 (1–4): 807–17. https://doi.org/10.1007/s00170-019-03568-7
• Chen, A. W., M. M. Curtin, R. B. Carlson, and E. N. Tinoco. 1990. “TRANAIR Applications to Engine/airframe Integration.” Journal of Aircraft 27 (8): 716–21. https://doi.org/10.2514/3.25345
• Chen, Chen, Junjie Gong, Yangdong Chen, and Jinrong Wang. 2021b. “A Prediction Model for Bending Springback of AZM120 Sheet Metal and Mechanical Compensation of CNC Automatic Panel Bender.” International Journal of Advanced Manufacturing Technology 116 (9–10): 3325–37. https://doi.org/10.1007/s00170-021-07606-1
• Chen, Xianmin, Shanshan Li, Yuanbo Liang, Shuo Wang, Liang Yan, and Shichang Du. 2024. “Fatigue Experiment and Failure Mechanism Analysis of Aircraft Titanium Alloy Wing–Body Connection Joint.” Sensors 25 (1): 150. https://doi.org/10.3390/s25010150
• Chen, Hang, Guangbao Mi, Peijie Li, and Chunxiao Cao. 2022. “Excellent High-Temperature Strength and Ductility of Graphene Oxide Reinforced High-Temperature Titanium Alloy Matrix Composite Fabricated by Hot Isostatic Pressing and Heat Treatment.” Composites Communications 30: 101077. https://doi.org/10.1016/j.coco.2022.101077
• Chen, P. C., D. Sarhaddi, R. Jha, D. D. Liu, K. Griffin, and R. Yurkovich. 2000. “Variable Stiffness Spar Approach for Aircraft Maneuver Enhancement Using ASTROS.” Journal of Aircraft 37 (5): 865–71. https://doi.org/10.2514/2.2682
• Chen, Hao, and Hui-jun Tan. 2019. “Buzz Flow Diversity in a Supersonic Inlet Ingesting Strong Shear Layers.” Aerospace Science and Technology 95: 105471. https://doi.org/10.1016/j.ast.2019.105471
• Chen, Hao, Hui-jun Tan, Ya-zhou Liu, and Qi-fan Zhang. 2019a. “External-Compression Supersonic Inlet Free from Violent Buzz.” AIAA Journal 57 (6): 2513–23. https://doi.org/10.2514/1.j057811
• Chen, Hao, Hui-Jun Tan, Qi-Fan Zhang, and Yue Zhang. 2017. “Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression.” AIAA Journal 55 (12): 4286–95. https://doi.org/10.2514/1.j056066
• Chen, Hao, Hui-Jun Tan, Qi-Fan Zhang, and Yue Zhang. 2018. “Throttling Process and Buzz Mechanism of a Supersonic Inlet at Overspeed Mode.” AIAA Journal 56 (5): 1953–64. https://doi.org/10.2514/1.j056674
• Chen, Da, Jian Wu, Youshan Wang, Benlong Su, and Yuyan Liu. 2021a. “High-Speed Tribology Behaviors of Aircraft Tire Tread Rubber in Contact with Pavement.” Wear 486-487: 204071. https://doi.org/10.1016/j.wear.2021.204071
• Cheng, Lifang, Hongjun Cao, and Litao Zhang. 2021. “Two-Parameter Bifurcation Analysis of an Aircraft Nose Landing Gear Model.” Nonlinear Dynamics 103 (1): 367–81. https://doi.org/10.1007/s11071-020-06129-w
• Cheng, Guangfeng, Y. Y. Lee, and Chuh Mei. 2003. “Flow Angle, Temperature, and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary.” Journal of Aircraft 40 (2): 248–55. https://doi.org/10.2514/2.3116
• Chester, D. H. 1995. “Comment on ‘Aircraft Landing Gear Positioning Concerning Abnormal Landing Cases’.” Journal of Aircraft 32 (4): 904–904. https://doi.org/10.2514/3.46816
• Chevalier, H., and James A. Burke. 1972. “Handling Characteristics in Roll of Two Light Airplanes for Steep Approach Landings.” Journal of Aircraft 9 (11): 759–64. https://doi.org/10.2514/3.44337
• Chevillot, Fabrice, Jean-Jacques Sinou, Nicolas Hardouin, and Louis Jézéquel. 2009. “Effects of Damping on the Speed of Increase and Amplitude of Limit Cycle for an Aircraft Braking System Subjected to Mode-Coupling Instability.” Archive of Applied Mechanics 80 (9): 1045–54. https://doi.org/10.1007/s00419-009-0352-8
• Chiarelli, Mario Rosario, and Salvatore Bonomo. 2019. “Numerical Investigation into Flutter and Flutter-Buffet Phenomena for a Swept Wing and a Curved Planform Wing.” International Journal of Aerospace Engineering 2019: 1–19. https://doi.org/10.1155/2019/8210235
• Chin, Wilson C. 1977. “Supersonic Wave Drag for Nonplanar Singularity Distributions.” AIAA Journal 15 (6): 884–86. https://doi.org/10.2514/3.60721
• Chin, Wilson C. 1978. “Supersonic Wave Drag of Planar Singularity Distributions.” AIAA Journal 16 (5): 482–87. https://doi.org/10.2514/3.7537
• Chipman, Richard R., Alex M. Zislin, and Catherine Waters. 1983. “Control of Aeroelastic Divergence.” Journal of Aircraft 20 (12): 1007–13. https://doi.org/10.2514/3.48204
• Cho, Jinsoo, and Younhyuck Chang. 2001. “Supersonic Flutter Analysis of Wings Using an Unsteady 3D Panel Method.” Computers & Fluids 30 (2): 237–56. https://doi.org/10.1016/s0045-7930(00)00010-4
• 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
• Choe, Yohan, Chongam Kim, and Kwanghyun Kim. 2020. “Effects of Optimized Bleed System on Supersonic Inlet Performance and Buzz.” Journal of Propulsion and Power 36 (2): 211–22. https://doi.org/10.2514/1.b37474
• Chongthairungruang, B., V. Uthaisangsuk, S. Suranuntchai, and S. Jirathearanat. 2013. “Springback Prediction in Sheet Metal Forming of High Strength Steels.” Materials & Design 50: 253–66. https://doi.org/10.1016/j.matdes.2013.02.060
• 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
• Churi, N. J., Z. J. Pei, and C. Treadwell. 2006. “Rotary Ultrasonic Machining of Titanium Alloy: Effects of Machining Variables.” Machining Science and Technology 10 (3): 301–21. https://doi.org/10.1080/10910340600902124
• Chuvakhov, P. V., I. M. Ilyukhin, and A. V. Fedorov. 2023. “Stability of Supersonic Boundary Layer over an Unswept Wing with a Parabolic Airfoil.” Theoretical and Computational Fluid Dynamics 38 (1): 1–13. https://doi.org/10.1007/s00162-023-00680-z
• Ciliberti, Danilo, and Fabrizio Nicolosi. 2025. “Lateral-Directional Wind Tunnel Tests of the PROSIB 19-Pax Aircraft Model.” Advances in Aerodynamics 7 (1): 3. https://doi.org/10.1186/s42774-024-00189-x
• Clay, Christopher L. 2004. “High Speed Flight Vehicle Structures: An Overview.” Journal of Aircraft 41 (5): 978–85. https://doi.org/10.2514/1.3880
• Coetzee, Etienne, Bernd Krauskopf, and Mark Lowenberg. 2013. “Continuation Analysis of Aircraft Ground Loads during High-Speed Turns.” Journal of Aircraft 50 (1): 217–31. https://doi.org/10.2514/1.c031883
• Colbert, Stephen, Damian Quinn, Declan C. Nolan, Rob Fox, and Jill Gaskell. 2023. “Impact of Airframe–Propulsion System Modeling Strategies on Key Structural Performance Metrics.” Journal of Aircraft 60 (2): 281–92. https://doi.org/10.2514/1.c036820
• 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
• Cole, Stanley R. 1992. “Aeroelastic Effects of Spoiler Surfaces on a Low-Aspect-Ratio Rectangular Wing.” Journal of Aircraft 29 (5): 768–73. https://doi.org/10.2514/3.46244
• Cole, Stanley R., Thomas E. Noll, and Boyd Perry. 2003. “Transonic Dynamics Tunnel Aeroelastic Testing in Support of Aircraft Development.” Journal of Aircraft 40 (5): 820–31. https://doi.org/10.2514/2.6873
• Comley, Peter. 2007. “Multi-Rate Superplastic Forming of Fine Grain Ti-6Al-4V Titanium Alloy.” Journal of Materials Engineering and Performance 16 (2): 150–54. https://doi.org/10.1007/s11665-007-9025-3
• Cook, R. H. 1965. “An Automatic Stall Prevention Control for Supersonic Fighter Aircraft.” Journal of Aircraft 2 (3): 171–75. https://doi.org/10.2514/3.43636
• 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
• Covert, Eugene E., and Milan Vlajinac. 1969. “An Aerodynamic Pitch-Roll Coupling in Spinning Vehicles.” Journal of Spacecraft and Rockets 6 (6): 762–63. https://doi.org/10.2514/3.29659
• Craig, Roy R. 1973. “Optimization of a Supersonic Panel Subject to a Flutter Constraint-A Finite-Element Solution.” AIAA Journal 11 (3): 404–5. https://doi.org/10.2514/3.50478
• Cramer, M. S., A. R. George, and A. R. Seebass. 1976. “Flowfield in the Plane of Symmetry below a Delta Wing.” AIAA Journal 14. https://ntrs.nasa.gov/citations/19760048214
• Crossley, F. A., and W. J. Barice. 1983. “Cast Transage 175 Titanium Alloy for Durability Critical Structural Components.” Journal of Aircraft 20 (1): 66–69. https://doi.org/10.2514/3.44829
• Crosthwait, E. L. 1970. “Pitot Inlet Additive Drag.” Journal of Aircraft 7 (6): 569–70. https://doi.org/10.2514/3.44216
• Cui, Tao, Xuegang He, Daren Yu, and Shunlin Tang. 2012. “Multistability and Loops-Coupled Hysteresis: Flight-Test Analysis on Error Detection of Inlet Start/Unstart.” Journal of Propulsion and Power 28 (3): 496–503. https://doi.org/10.2514/1.b34349
• Cui, Tao, Zhong Lv, and Daren Yu. 2011. “Multistability and Complex Routes of Supersonic Inlet Start/Unstart.” Journal of Propulsion and Power 27 (6): 1204–17. https://doi.org/10.2514/1.b34235
• Cunha-Filho, A. G., Y. P. J. Briend, A. M. G. de Lima, and M. V. Donadon. 2018. “An Efficient Iterative Model Reduction Method for Aeroviscoelastic Panel Flutter Analysis in the Supersonic Regime.” Mechanical Systems and Signal Processing 104: 575–88. https://doi.org/10.1016/j.ymssp.2017.11.018
• D’Vari, R., and M. Baker. 1999. “Aeroelastic Loads and Sensitivity Analysis for Structural Loads Optimization.” Journal of Aircraft 36 (1): 156–66. https://doi.org/10.2514/2.2421
• Dağlı, Osman, Metin Orhan Kaya, and Can Eyüpoğlu. 2025. “Feed-Forward Neural Network-Based Prediction of Flutter Speed of 3 DOF 2D Wing Model.” Journal of Vibration Engineering & Technologies 13 (1): 47. https://doi.org/10.1007/s42417-024-01741-1
• Daliri, Abbas, Mohammad Farahani, and Javad Sepahi-Younsi. 2018. “Novel Method for Supersonic Inlet Buzz Measurement in Wind Tunnel.” Journal of Propulsion and Power 34 (1): 273–80. https://doi.org/10.2514/1.b36760
• Damstrom, E. K., and J. F. Mayes. 1971. “Transonic Flight and Wind-Tunnel Buffet Onset Investigation of the F-8D Aircraft.” Journal of Aircraft 8 (4): 263–70. https://doi.org/10.2514/3.44266
• Dang, Van Tuan, Carl Labergere, and Pascal Lafon. 2017. “POD Surrogate Models Using Adaptive Sampling Space Parameters for Springback Optimization in Sheet Metal Forming.” Procedia Engineering 207: 1588–93. https://doi.org/10.1016/j.proeng.2017.10.1053
• Davari, B., and E. V. Laitone. 1977a. “Effect of a Nonconstant C/m-Alpha/ on the Stability of Rolling Aircraft.” Journal of Aircraft 14. https://ntrs.nasa.gov/citations/19780032271
• Davari, Bijan, and E. V. Laitone. 1977b. “Effect of a Nonconstant Cma on the Stability of Rolling Aircraft.” Journal of Aircraft 14 (12): 1169–74. https://doi.org/10.2514/3.58910
• Davis, Robert A. 1957. “The Response of a Bisymmetric Aircraft to Small Combined Pitch, Yaw, and Roll Control Actions.” Journal of the Aeronautical Sciences 24 (12): 905–10. https://doi.org/10.2514/8.3998
• de Jong, R. C., and J. A. Mulder. 1987. “Accurate Estimation of Aircraft Inertia Characteristics from a Single Suspension Experiment.” Journal of Aircraft 24 (6): 362–70. https://doi.org/10.2514/3.45454
• de Souza, T., and B. F. Rolfe. 2010. “Characterising Material and Process Variation Effects on Springback Robustness for a Semi-Cylindrical Sheet Metal Forming Process.” International Journal of Mechanical Sciences 52 (12): 1756–66. https://doi.org/10.1016/j.ijmecsci.2010.09.009
• Dehghan Manshadi, Ali, and Fariborz Saghafi. 2021. “Aircraft Mass Properties Estimation during Airdrop Maneuver: A Nonlinear Filtering Approach.” Journal of Aircraft 58 (5): 982–96. https://doi.org/10.2514/1.c035941
• Demasi, Luciano. 2006. “Induced Drag Minimization: A Variational Approach Using the Acceleration Potential.” Journal of Aircraft 43 (3): 669–80. https://doi.org/10.2514/1.15982
• Deng, Tongsheng, Dongsheng Li, Xiaoqiang Li, Pan Ding, and Kai Zhao. 2014. “Hot Stretch Bending and Creep Forming of Titanium Alloy Profile.” Procedia Engineering 81: 1792–98. https://doi.org/10.1016/j.proeng.2014.10.234
• Deng, Lei, Xinyun Wang, Junsong Jin, and Liangjun Xia. 2017. “Springback and Hardness of Aluminum Alloy Sheet Part Manufactured by Warm Forming Process Using Non-Isothermal Dies.” Procedia Engineering 207: 2388–93. https://doi.org/10.1016/j.proeng.2017.10.1013
• Deokar, Swapnil U., Prashant K. Jain, Puneet Tandon, and Abhyudaya Pathak. 2019. “Analysis of Springback and Force Behavior in Single Point Incremental Sheet Forming Though FEA.” Materials Today: Proceedings 18: 3330–39. https://doi.org/10.1016/j.matpr.2019.07.254
• des Clers, B., and J. Sternberg. 1952. “On Boundary-Layer Temperature Recovery Factors.” Journal of the Aeronautical Sciences 19 (9): 645–46. https://doi.org/10.2514/8.2411
• 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
• DeSanti, Albert J. 1988. “Simple Model for Predicting Time to Roll Wings Level in the A-7E.” Journal of Aircraft 25 (9): 861–62. https://doi.org/10.2514/3.45671
• 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
• Deyoung, John. 1971. “Convergence-Proof of Discrete-Panel Wing Loading Theories.” Journal of Aircraft 8 (10): 837–39. https://doi.org/10.2514/3.59178
• Di Leone, Domenico, Francesco Lo Balbo, Alessandro De Gaspari, and Sergio Ricci. 2021. “Model Updating and Aeroelastic Correlation of a Scaled Wind Tunnel Model for Active Flutter Suppression Test.” Aerospace 8 (11): 334. https://doi.org/10.3390/aerospace8110334
• Dickie, George D. 1955. “Theoretical and Experimental Pressure Recovery of Sweptback Normal Shock Inlets.” Journal of the Aeronautical Sciences 22 (3): 189–93. https://doi.org/10.2514/8.3303
• Dicus, J. H. 1975. “FORTRAN Program to Generate Engine Inlet Flow Contour Maps and Distortion Parameters.” Computer-Aided Design 7 (3): 206. https://doi.org/10.1016/0010-4485(75)90046-9
• Dilan, Rasim Askin, Tuna Balkan, and Bulent E. Platin. 2017. “An Online Intelligent Algorithm Pipeline for the Elimination of Springback Effect during Sheet Metal Bending.” Procedia Engineering 207: 1576–81. https://doi.org/10.1016/j.proeng.2017.10.1081
• Ding, Ling, Cik Suhana Hassan, Wei Hong Lim, Swee Pin Yeap, Ke Wei, and Lu-Cui Chao. 2026. “Path-Dependent Constitutive Modeling for Superplastic Forming of Titanium Alloys: Memory-Architecture Perspective.” Materials 19 (13): 2817. https://doi.org/10.3390/ma19132817
• Ding, Dawei, Zhuoran Huang, and Fengyu Xu. 2023. “Error Prediction of Springback in Bending Process Based on GA-BPNN for Accurate Forming Angle.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10452018
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2010. “Visualizing Supersonic Inlet Duct Unstart Using Planar Laser Rayleigh Scattering.” Experiments in Fluids 50 (6): 1651–57. https://doi.org/10.1007/s00348-010-1028-4
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2011a. “The Influence of Boundary Layers on Supersonic Inlet Flow Unstart Induced by Mass Injection.” Experiments in Fluids 51 (3): 679–91. https://doi.org/10.1007/s00348-011-1077-3
• Doggett, Robert V., and David L. Soistmann. 1992. “Low-Speed Flutter Characteristics of Some Simple Low-Aspect-Ratio Delta-Wing Models.” Journal of Aircraft 29 (2): 273–79. https://doi.org/10.2514/3.46155
• Dong, Lei, Kwing-So Choi, and Xuerui Mao. 2020. “Interplay of the Leading-Edge Vortex and the Tip Vortex of a Low-Aspect-Ratio Thin Wing.” Experiments in Fluids 61 (9): 200. https://doi.org/10.1007/s00348-020-03023-4
• DongGyu, Lee, Lee HyunSup, Shin JaeHo, Shin MinSeok, Kang JiWon, and Kim YoungSoon. 2025. “Dataset for Classification of Forming Tool Types for Aircraft Parts Based on Neural Network Models Using CAD.” Data in Brief 63: 112302. https://doi.org/10.1016/j.dib.2025.112302
• Dowell, E. H. 1968. “Theoretical-Experimental Correlation of Plate Flutter Boundaries at Low Supersonic Speeds.” AIAA Journal 6 (9): 1810–11. https://doi.org/10.2514/3.4881
• Dowell, E. H. 1971. “Generalized Aerodynamic Forces on a Flexible Plate Undergoing Transient Motion in a Shear Flow with an Application to Panel Flutter.” AIAA Journal 9 (5): 834–41. https://doi.org/10.2514/3.6283
• Dowell, Earl, and Alejandro Assael. 2025. “Control Surface Reversal of a Uniform Cantilevered Wing.” AIAA Journal 63 (11): 5025–27. https://doi.org/10.2514/1.j065403
• Dowell, Earl H., Donald B. Bliss, and Robert L. Clark. 2003. “Aeroelastic Wing with Leading- and Trailing-Edge Control Surfaces.” Journal of Aircraft 40 (3): 559–65. https://doi.org/10.2514/2.3130
• Dragos, Lazar, and Adrian Dinu. 1990. “Application of the Boundary Element Method to the Thin Airfoil Theory.” AIAA Journal 28 (10): 1822–24. https://doi.org/10.2514/3.10480
• Dress, David A., Richmond P. Boyden, and Christopher I. Cruz. 1994. “Measured and Theoretical Supersonic Dynamic Stability Characteristics of a National Aero-Space Plane Configuration.” Journal of Aircraft 31 (3): 597–602. https://doi.org/10.2514/3.46536
• Du, Zhihao, Chunxu Wang, Qing Liu, Shan Wang, Yang Liu, and Guofeng Wang. 2022. “The Superplastic Forming/diffusion Bonding of TA7 Titanium Alloy for Manufacturing Hollow Structure with Stiffeners.” Journal of Manufacturing Processes 73: 385–94. https://doi.org/10.1016/j.jmapro.2021.10.064
• Dugundji, John. 1966. “Theoretical Considerations of Panel Flutter at High Supersonic Mach Numbers.” AIAA Journal 4 (7): 1257–66. https://doi.org/10.2514/3.3657
• Dunlop Limited. 1972. “Carbon/carbon Composite Aircraft Brake.” Tribology 5 (3): 107. https://doi.org/10.1016/0041-2678(72)90017-6
• Eastep, F. E., and J. J. Olsen. 1980. “Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections.” AIAA Journal 18 (10): 1159–64. https://doi.org/10.2514/3.50866
• Edwards, John W. 2008. “Calculated Viscous and Scale Effects on Transonic Aeroelasticity.” Journal of Aircraft 45 (6): 1863–71. https://doi.org/10.2514/1.30082
• Edwards, John W. 2009. “National Transonic Facility Model and Tunnel Vibrations.” Journal of Aircraft 46 (1): 46–52. https://doi.org/10.2514/1.30080
• Edwards, John W., Charles V. Spain, Donald F. Keller, Robert W. Moses, and David M. Schuster. 2009. “Transport Wing Flutter Model Transonic Limit Cycle Oscillation Test.” Journal of Aircraft 46 (4): 1104–13. https://doi.org/10.2514/1.30079
• El-Megharbel, A., A. El-Domiaty, and M. Shaker. 1990. “Springback and Residual Stresses after Stretch Bending of Workhardening Sheet Metal.” Journal of Materials Processing Technology 24: 191–200. https://doi.org/10.1016/0924-0136(90)90181-s
• El-Ramly, Z., W. J. Rainbird, and D. G. Earl. 1976. “Wind Tunnel Measurements of Rolling Moment in a Swept-Wing Vortex Wake.” Journal of Aircraft 13 (12): 962–67. https://doi.org/10.2514/3.58736
• Er-El, J. 1988. “Effect of Wing/canard Interference on the Loading of a Delta Wing.” Journal of Aircraft 25 (1): 18–24. https://doi.org/10.2514/3.45535
• Er-El, J., D. Seter, and D. Weihs. 1989. “Nonlinear Aerodynamics of a Delta Wing in Combined Pitch and Roll.” Journal of Aircraft 26 (3): 254–59. https://doi.org/10.2514/3.45754
• Ericsson, Lars E. 1995a. “Cobra Maneuver Unsteady Aerodynamic Considerations.” Journal of Aircraft 32 (1): 214–16. https://doi.org/10.2514/3.46706
• Ericsson, Lars E. 1995b. “Flow Physics of Critical States for Rolling Delta Wings.” Journal of Aircraft 32 (3): 603–10. https://doi.org/10.2514/3.46762
• Ericsson, Lars E. 1996b. “Difficulties in Predicting Vortex Breakdown Effects on a Rolling Delta Wing.” Journal of Aircraft 33 (3): 477–84. https://doi.org/10.2514/3.46969
• Ericsson, Lars E. 1997a. “Analysis of the Effect of Sideslip on Delta Wing Roll-Trim Characteristics.” Journal of Aircraft 34 (5): 585–91. https://doi.org/10.2514/2.2233
• Ericsson, Lars E. 1997b. “Effect of Angle of Attack on Roll Characteristics of 65-Degree Delta Wing.” Journal of Aircraft 34 (4): 573–75. https://doi.org/10.2514/2.2212
• Ericsson, Lars E. 1997c. “Effect of Deep-Stall Wing Dynamics on Forebody-Induced Wing Rock.” Journal of Aircraft 34 (3): 448–50. https://doi.org/10.2514/2.2192
• Ericsson, Lars E. 1998. “Rapid Prediction of Wing Rock for Slender Delta-Wing Configurations.” Journal of Aircraft 35 (6): 979–81. https://doi.org/10.2514/2.2399
• Ericsson, Lars E. 1999. “Time-History Effects on a Rolling 65-Degree Delta-Wing-Body Configuration.” Journal of Aircraft 36 (3): 489–95. https://doi.org/10.2514/2.2470
• Ericsson, Lars E. 2001. “Flow Physics Generating Highly Nonlinear Lateral Stability Characteristics of 65-Degree Delta-Wing-Body.” Journal of Aircraft 38 (5): 932–34. https://doi.org/10.2514/2.2855
• Ericsson, Lars E., and Ernest S. Hanff. 1994a. “Further Analysis of High-Rate Rolling Experiments of a 65-Deg Delta Wing.” Journal of Aircraft 31 (6): 1350–57. https://doi.org/10.2514/3.46658
• Ericsson, L. E., and E. S. Hanff. 1994b. “Unique High-Alpha Roll Dynamics of a Sharp-Edged 65-Deg Delta Wing.” Journal of Aircraft 31 (3): 520–25. https://doi.org/10.2514/3.46524
• Ezzeldin, Abdullah, and Zhenlong Wu. 2025. “CFD-Driven Enhancement for Supersonic Aircraft Variable Geometry Inlet.” Applied Sciences 15 (17): 9825. https://doi.org/10.3390/app15179825
• Fan, Ronglei, Minghe Chen, Yong Wu, and Lansheng Xie. 2018. “Prediction and Experiment of Fracture Behavior in Hot Press Forming of a TA32 Titanium Alloy Rolled Sheet.” Metals 8 (12): 985. https://doi.org/10.3390/met8120985
• Fan, Ronglei, Yong Wu, Minghe Chen, Dipeng Wu, and Tengfei Wu. 2023. “Determining the Hot Forming Limits of Titanium Alloy Sheet under Different Strain Paths by Constant Equivalent Strain Rate Hot Gas Bulging Tests.” Journal of Materials Processing Technology 319: 118067. https://doi.org/10.1016/j.jmatprotec.2023.118067
• Fan, Zhe, Chuliang Yan, Hongbo Wang, Hao Song, and Junkai Sun. 2026. “Ground Calibration and Airborne Physical-Consistency Assessment of Composite-Wing Sectional Loads Using Fiber Bragg Grating Sensors.” Applied Sciences 16 (18): 8970. https://doi.org/10.3390/app16188970
• Fang, Wei, Lingang Zhu, and Youshan Wang. 2022. “Landing Performance Study for Four Wheels Twin Tandem Landing Gear Based on Drop Test.” Aerospace 9 (7): 334. https://doi.org/10.3390/aerospace9070334
• Farahani, Mohammad, Abbas Daliri, and Javad Sepahi Younsi. 2019. “Supersonic Inlet Buzz Detection Using Pressure Measurement on Wind Tunnel Wall.” Aerospace Science and Technology 86: 782–93. https://doi.org/10.1016/j.ast.2019.02.002
• Farsadi, Touraj, Davood Asadi, and Hasan Kurtaran. 2019. “Flutter Improvement of a Thin Walled Wing-Engine System by Applying Curvilinear Fiber Path.” Aerospace Science and Technology 93: 105353. https://doi.org/10.1016/j.ast.2019.105353
• Fawal, Sara, and Ali Kodal. 2021. “Overall and Component Basis Performance Evaluations for Turbojet Engines under Various Optimal Operating Conditions.” Aerospace Science and Technology 117: 106943. https://doi.org/10.1016/j.ast.2021.106943
• 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
• Fazelzadeh, S. A., P. Marzocca, E. Rashidi, and A. Mazidi. 2010. “Effects of Rolling Maneuver on Divergence and Flutter of Aircraft Wing Store.” Journal of Aircraft 47 (1): 64–70. https://doi.org/10.2514/1.40463
• Feldt, Walter T., and George Herrmann. 1974. “Bending-Torsional Flutter of a Cantilevered Wing Containing a Tip Mass and Subjected to a Transverse Follower Force.” Journal of the Franklin Institute 297 (6): 467–78. https://doi.org/10.1016/0016-0032(74)90123-9
• Feldwisch, Johan, and Martin Bauer. 2023. “UltraFLoads: A Simulation Suite and Framework for High-Fidelity Flight Loads.” Aerospace 10 (3): 273. https://doi.org/10.3390/aerospace10030273
• Feng, Rui, Minghe Chen, Lansheng Xie, and Hongrui Dong. 2025. “Effect of Elevated Temperature and Stress State on Ductile Fracture Behaviors in Titanium Alloy: Experiments and Modeling.” Intermetallics 180: 108708. https://doi.org/10.1016/j.intermet.2025.108708
• Feng, Renjian, Ruoyan Xing, Yinfeng Wu, and Ning Yu. 2020. “A Condition-Based Calibration Method for Flight Test Measuring Equipment.” In 2020 International Conference on Sensing, Measurement & Data Analytics in the era of Artificial Intelligence (ICSMD). IEEE. https://doi.org/10.1109/icsmd50554.2020.9261747
• Feria Alanis, Aaron, Ahmed A. Sheikh Al-Shabab, Antonis F. Antoniadis, Panagiotis Tsoutsanis, and Martin Skote. 2024. “A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications.” Fluids 9 (12): 271. https://doi.org/10.3390/fluids9120271
• Ferrari, Carlo. 1948. “Interference between Wing and Body at Supersonic Speeds-Theory and Numerical Application.” Journal of the Aeronautical Sciences 15 (6): 317–36. https://doi.org/10.2514/8.11582
• Ferrero, Andrea. 2020. “Control of a Supersonic Inlet in off-Design Conditions with Plasma Actuators and Bleed.” Aerospace 7 (3): 32. https://doi.org/10.3390/aerospace7030032
• Filice, L., F. Gagliardi, S. Lazzaro, and C. Rocco. 2009. “FE Simulation and Experimental Considerations on TI Alloy Superplastic Forming for Aerospace Applications.” International Journal of Material Forming 3 (1): 41–46. https://doi.org/10.1007/s12289-009-0415-y
• Fink, Martin R. 1971. “Calculated Transonic Flow past Slender Fuselages and Afterbodies.” Journal of Aircraft 8 (9): 710–16. https://doi.org/10.2514/3.59161
• Firat, Mehmet, Bilgin Kaftanoglu, and Orhan Eser. 2008. “Sheet Metal Forming Analyses with an Emphasis on the Springback Deformation.” Journal of Materials Processing Technology 196 (1–3): 135–48. https://doi.org/10.1016/j.jmatprotec.2007.05.029
• Flax, A. H. 1953. “Integral Relations in the Linearized Theory of Wing-Body Interference.” Journal of the Aeronautical Sciences 20 (7): 483–90. https://doi.org/10.2514/8.2694
• Flax, Alexander H. 1986. “Comment on ‘the Role of Damping on Supersonic Panel Flutter’.” AIAA Journal 24 (11): 1886–87. https://doi.org/10.2514/3.48708
• Fleeter, Sanford, and Ronald E. Riffel. 1979. “Time-Variant Aerodynamics of Oscillating Airfoil Surfaces in a Supersonic Flowfield.” AIAA Journal 17 (5): 465–70. https://doi.org/10.2514/3.61156
• Försching, H., and H. Zingel. 1988. “Motion-Induced Unsteady Airloads on an Oscillating Low-Aspect-Ratio Trapezoidal Half-Wing in Separated Flow.” Journal of Fluids and Structures 2 (6): 515–39. https://doi.org/10.1016/s0889-9746(88)80021-5
• Fortis, Alexandra Emilia, and Stefan Balint. 2015. “Numerical Investigations of Equilibriums in a Flight with High Angle of Attack.” In 2015 17th International Symposium on Symbolic and Numeric Algorithms for Scientific Computing (SYNASC). IEEE. https://doi.org/10.1109/synasc.2015.22
• Fortunato, Bernardo. 1985. “A Numerical Method for Second Order Thin Airfoil Theory.” Meccanica 20 (2): 171–75. https://doi.org/10.1007/bf02337637
• Fossier, M. W., R. W. Bratt, and D. G. Dill. 1950. “Comparison of Analytical and High-Speed Mechanical-Calculator Solutions of the Lateral Equations of Motion of an Airplane, Including Product-of-Inertia Terms.” Journal of the Aeronautical Sciences 17 (5): 271–76. https://doi.org/10.2514/8.1616
• Fraiser, H. R. 1960. “Supersonic Inlet Dynamics.” Journal of the Aerospace Sciences 27 (6): 429–36. https://doi.org/10.2514/8.8575
• Franklin, James A. 1971. “Flight Investigation of the Influence of Turbulence on Lateral-Directional Flying Qualities.” Journal of Aircraft 8 (10): 795–802. https://doi.org/10.2514/3.44303
• Fremaux, C. M. 1995. “Estimation of the Moment Coefficients for Dynamically Scaled, Free-Spinning Wind-Tunnel Models.” Journal of Aircraft 32 (6): 1407–9. https://doi.org/10.2514/3.46895
• Frestel, N., A. Liot, H. Tretout, and R. De Mol. 1992. “Scanning Acoustic Microscopy for Quantitative Analysis of Superplastic Forming Diffusion Bonding Titanium Aerospace Components.” NDT & E International 25 (4–5): 211. https://doi.org/10.1016/0963-8695(92)90164-c
• “Fretting Fatigue Strength of Titanium Alloy RC 130B.” 1958. Wear 1 (5): 449. https://doi.org/10.1016/0043-1648(58)90144-3
• Freydin, Maxim, Earl H. Dowell, S. Michael Spottswood, and Ricardo A. Perez. 2020. “Nonlinear Dynamics and Flutter of Plate and Cavity in Response to Supersonic Wind Tunnel Start.” Nonlinear Dynamics 103 (4): 3019–36. https://doi.org/10.1007/s11071-020-05817-x
• Fu, Zemin, and Jianhua Mo. 2010. “Springback Prediction of High-Strength Sheet Metal under Air Bending Forming and Tool Design Based on GA–BPNN.” International Journal of Advanced Manufacturing Technology 53 (5–8): 473–83. https://doi.org/10.1007/s00170-010-2846-5
• Fu, Zemin, Jianhua Mo, and Wenxian Zhang. 2009. “Study on Multiple-Step Incremental Air-Bending Forming of Sheet Metal with Springback Model and FEM Simulation.” International Journal of Advanced Manufacturing Technology 45 (5–6): 448–58. https://doi.org/10.1007/s00170-009-1982-2
• Fung, Y. C. 1954. “The Static Stability of a Two-Dimensional Curved Panel in a Supersonic Flow, with an Application to Panel Flutter.” Journal of the Aeronautical Sciences 21 (8): 556–65. https://doi.org/10.2514/8.3122
• Gabl, Roman, Thomas Davey, Edd Nixon, and David M. Ingram. 2021. “Accuracy Analysis of the Measurement of Centre of Gravity and Moment of Inertia with a Swing.” Applied Sciences 11 (12): 5345. https://doi.org/10.3390/app11125345
• Gaglio, Emanuela, Michele Visone, Marco Lanzetta, Stefano Mungiguerra, Anselmo Cecere, and Raffaele Savino. 2023. “Mixed-Compression Supersonic Intake and Engine–Airframe Integration.” Journal of Spacecraft and Rockets 60 (4): 1100–1111. https://doi.org/10.2514/1.a35532
• Gao, Enzhi, Di Xue, and Yiming Li. 2025. “Springback Angle Prediction for High-Strength Aluminum Alloy Bending via Multi-Stage Regression.” Metals 15 (4): 358. https://doi.org/10.3390/met15040358
• Gardner, C. S., and H. F. Ludloff. 1950. “Influence of Acceleration on Aerodynamic Characteristics of Thin Airfoils in Supersonic and Transonic Flight.” Journal of the Aeronautical Sciences 17 (1): 47–59. https://doi.org/10.2514/8.1518
• Gardner, C. S., H. F. Ludloff, and F. Reiche. 1948. “Drag of an Airfoil in Accelerated, Supersonic Flight.” Journal of Applied Physics 19 (12): 1179–80. https://doi.org/10.1063/1.1715040
• 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
• Gaspari, A. De, S. Ricci, L. Riccobene, and A. Scotti. 2009. “Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing.” AIAA Journal 47 (9): 1995–2010. https://doi.org/10.2514/1.34649
• Gatt, Antoine, Sébastien Besset, Louis Jézéquel, Abdelbasset Hamdi, and Jean-Frédéric Diebold. 2017. “Reduction Methods Applied to Aircraft Brake Squeal Prediction and Simulation.” Journal of Aircraft 54 (4): 1340–49. https://doi.org/10.2514/1.c034043
• Gatto, A. 2009. “Application of a Pendulum Support Test Rig for Aircraft Stability Derivative Estimation.” Journal of Aircraft 46 (3): 927–34. https://doi.org/10.2514/1.38916
• Gau, Jenn-Terng, Chris Principe, and Miao Yu. 2007. “Springback Behavior of Brass in Micro Sheet Forming.” Journal of Materials Processing Technology 191 (1–3): 7–10. https://doi.org/10.1016/j.jmatprotec.2007.03.035
• 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
• Ghosh, A. K., S. C. Raisinghani, and Sunil Khubchandani. 1998. “Estimation of Aircraft Lateral-Directional Parameters Using Neural Networks.” Journal of Aircraft 35 (6): 876–81. https://doi.org/10.2514/2.2407
• Gibbings, J. C. 1966. “An Empiric Correlation of Some Transonic Aerofoil Characteristics.” Journal of Aircraft 3 (5): 411–17. https://doi.org/10.2514/3.43754
• Gill, Stephen J., Mark H. Lowenberg, Simon A. Neild, Bernd Krauskopf, Guilhem Puyou, and Etienne Coetzee. 2013. “Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis.” Journal of Aircraft 50 (6): 1832–42. https://doi.org/10.2514/1.c032221
• Gisario, A., M. Barletta, C. Conti, and S. Guarino. 2011. “Springback Control in Sheet Metal Bending by Laser-Assisted Bending: Experimental Analysis, Empirical and Neural Network Modelling.” Optics and Lasers in Engineering 49 (12): 1372–83. https://doi.org/10.1016/j.optlaseng.2011.07.010
• Gisario, A., M. Barletta, and S. Venettacci. 2016. “Improvements in Springback Control by External Force Laser-Assisted Sheet Bending of Titanium and Aluminum Alloys.” Optics & Laser Technology 86: 46–53. https://doi.org/10.1016/j.optlastec.2016.06.013
• Glasgow, E. R. 1974. “Integrated Airframe-Nozzle Performance for Designing Twin-Engine Fighters.” Journal of Aircraft 11 (6): 354–62. https://doi.org/10.2514/3.59258
• Go, Tiauw Hiong. 2009. “Lateral-Directional Aircraft Dynamics under Static Moment Nonlinearity.” Journal of Guidance, Control, and Dynamics 32 (1): 305–9. https://doi.org/10.2514/1.39025
• Go, Tiauw Hiong, and Adnan Maqsood. 2015. “Effect of Aspect Ratio on Wing Rock at Low Reynolds Number.” Aerospace Science and Technology 42: 267–73. https://doi.org/10.1016/j.ast.2015.01.009
• Goff, Robin Porter. 1998. “Airplane Stability and Control: A History of the Technologies That Made Aviation Possible.” Endeavour 22 (3): 133–34. https://doi.org/10.1016/s0160-9327(99)80022-2
• Goland, Martin, and Yudell L. Luke. 1954. “An Exact Solution for Two-Dimensional Linear Panel Flutter at Supersonic Speeds.” Journal of the Aeronautical Sciences 21 (4): 275–76. https://doi.org/10.2514/8.2991
• Goodman, Theodore R. 1949. “The Lift Distribution on Conical and Nonconical Flow Regions of Thin Finite Wings in a Supersonic Stream.” Journal of the Aeronautical Sciences 16 (6): 365–74. https://doi.org/10.2514/8.11808
• Goodman, Theodore R. 1951. “Aerodynamics of a Supersonic Rectangular Wing Striking a Sharp-Edged Gust.” Journal of the Aeronautical Sciences 18 (8): 519–26. https://doi.org/10.2514/8.2028
• Gordiner, Raymond E. 1995. “Computation of Vortex Breakdown on a Rolling Delta Wing.” Journal of Aircraft 32 (3): 686–88. https://doi.org/10.2514/3.46777
• Gordnier, Raymond E. 1995. “Computation of Delta-Wing Roll Maneuvers.” Journal of Aircraft 32 (3): 486–92. https://doi.org/10.2514/3.46746
• Gordon, James T., Steven Y. Liu, and M. Akif Ozbek. 1998. “Nonlinear Model for Aircraft Brake Squeal Analysis: Stability Analysis and Parametric Studies.” Journal of Aircraft 35 (4): 631–36. https://doi.org/10.2514/2.2347
• Gordon, Brandon W., Mehrdad Pakmehr, and C. A. Rabbath. 2009. “State-Space Modeling and Identification of Delta Wing Vortex-Coupled Roll Dynamics.” Journal of Aircraft 46 (1): 36–45. https://doi.org/10.2514/1.23596
• 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
• Göttmann, A., J. Diettrich, G. Bergweiler, et al. 2011. “Laser-Assisted Asymmetric Incremental Sheet Forming of Titanium Sheet Metal Parts.” Production Engineering 5 (3): 263–71. https://doi.org/10.1007/s11740-011-0299-9
• Goulos, Ioannis, John Otter, Fernando Tejero, Josep Hueso Rebassa, David MacManus, and Christopher Sheaf. 2021. “Civil Turbofan Propulsion Aerodynamics: Thrust-Drag Accounting and Impact of Engine Installation Position.” Aerospace Science and Technology 111: 106533. https://doi.org/10.1016/j.ast.2021.106533
• Graham, E. W. 1958. “A Geometric Problem Related to the Optimum Distribution of Lift on a Planar Wing in Supersonic Flow.” Journal of the Aerospace Sciences 25 (12): 771–74. https://doi.org/10.2514/8.7885
• Gratzer, L. B., and T. J. O’Donnell. 1965. “Development of a BLC High-Lift System for High-Speed Airplanes.” Journal of Aircraft 2 (6): 477–84. https://doi.org/10.2514/3.43686
• 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 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
• Green, Bradford E. 2008. “Computational Prediction of Roll Damping for the F/A-18E at Transonic Speeds.” Journal of Aircraft 45 (4): 1297–1304. https://doi.org/10.2514/1.34571
• Greenwell, D. I., and N. J. Wood. 1994. “Roll Moment Characteristics of Asymmetric Tangential Leading-Edge Blowing on a Delta Wing.” Journal of Aircraft 31 (1): 161–68. https://doi.org/10.2514/3.46469
• Grenestedt, Joachim L. 2008. “Modified Aileron Tips Improve Lateral Stability.” Journal of Aircraft 45 (6): 2176–77. https://doi.org/10.2514/1.40401
• Grenestedt, Joachim L., Sven-Olof Ridder, and William J. Maroun. 2006. “Flight Testing a Simple Fix to Lateral Stability Deficiencies.” Journal of Aircraft 43 (5): 1399–1404. https://doi.org/10.2514/1.20523
• Gresham, Nicholas T., Zhijin Wang, and Ismet Gursul. 2009b. “Low Reynolds Number Aerodynamics of Free-to-Roll Low Aspect Ratio Wings.” Experiments in Fluids 49 (1): 11–25. https://doi.org/10.1007/s00348-009-0726-2
• Gresham, N. T., Z. Wang, and I. Gursul. 2010. “Vortex Dynamics of Free-to-Roll Slender and Nonslender Delta Wings.” Journal of Aircraft 47 (1): 292–302. https://doi.org/10.2514/1.45425
• Gresham, N. T., Z. Wang, and I. Gursul. 2011. “Effect of Slenderness Ratio on Free-to-Roll Wing Aerodynamics.” Journal of Aircraft 48 (3): 1112–16. https://doi.org/10.2514/1.c031286
• 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
• Grinberg, N. M., V. M. Boichuk, N. A. Tsurikov, P. S. Sologub, B. V. Gladkikh, and V. E. Popirnyi. 1971. “Durability of Titanium Alloy in Vacuum at Low and Elevated Temperatures.” Strength of Materials 3 (4): 406–10. https://doi.org/10.1007/bf01528180
• Grismer, Deborah S., and Jerry E. Jenkins. 1997. “Critical-State Transients for a Rolling 65-Degree Delta Wing.” Journal of Aircraft 34 (3): 380–86. https://doi.org/10.2514/2.2180
• Groche, Peter, and Frederic Bäcker. 2013. “Springback in Stringer Sheet Stretch Forming.” CIRP Annals 62 (1): 275–78. https://doi.org/10.1016/j.cirp.2013.03.117
• Grunnet, James L. 1984. “Transonic Wind Tunnel Wall Interference Minimization.” Journal of Aircraft 21 (9): 694–99. https://doi.org/10.2514/3.45016
• Gu, Weikai. 1986. “Second-Order Roll Damping of Rolling Wings at Supersonic Speeds.” Journal of Spacecraft and Rockets 23 (6): 658–60. https://doi.org/10.2514/3.25863
• Gu, Huaiping, Linyuan Jia, Hui Duan, Jiajia Wei, and Zhen Liu. 2026. “A Component-Decoupled and Physics-Constrained Hybrid Modeling Framework for Turbojet Engine Performance Prediction.” Aerospace 13 (5): 425. https://doi.org/10.3390/aerospace13050425
• 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
• Gubanov, A. A. 2019. “Theoretical Fundamentals of Airframe/propulsion Integration for High-Speed Aircraft.” Advances in Aerodynamics 1 (1): 11. https://doi.org/10.1186/s42774-019-0013-8
• Gülsaçan, Burak, Gizem Şencan, and Mehmet Metin Yavuz. 2018. “Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing.” AIAA Journal 56 (12): 4657–68. https://doi.org/10.2514/1.j057083
• Guo, Y. Q., W. Gati, H. Naceur, and J. L. Batoz. 2002. “An Efficient DKT Rotation Free Shell Element for Springback Simulation in Sheet Metal Forming.” Computers & Structures 80 (27–30): 2299–2312. https://doi.org/10.1016/s0045-7949(02)00256-0
• Guo, Xinyun, Yiu-Yin Lee, and Chuh Mei. 2007. “Supersonic Nonlinear Panel Flutter Suppression Using Shape Memory Alloys.” Journal of Aircraft 44 (4): 1139–49. https://doi.org/10.2514/1.16080
• Guo, Xinyun, and Chuh Mei. 2003. “Using Aeroelastic Modes for Nonlinear Panel Flutter at Arbitrary Supersonic Yawed Angle.” AIAA Journal 41 (2): 272–79. https://doi.org/10.2514/2.1940
• Guo, Xinyun, and Chuh Mei. 2006. “Application of Aeroelastic Modes on Nonlinear Supersonic Panel Flutter at Elevated Temperatures.” Computers & Structures 84 (24–25): 1619–28. https://doi.org/10.1016/j.compstruc.2006.01.041
• Guo, Zhefeng, and Wencheng Tang. 2017. “Bending Angle Prediction Model Based on BPNN-Spline in Air Bending Springback Process.” Mathematical Problems in Engineering 2017 (1): 7834621. https://doi.org/10.1155/2017/7834621
• Gupta, K. K. 1976. “On a Numerical Solution of the Supersonic Panel Flutter Eigenproblem.” International Journal for Numerical Methods in Engineering 10 (3): 637–45. https://doi.org/10.1002/nme.1620100312
• Guruswamy, Guru P., and Peter M. Goorjian. 1985. “Efficient Algorithm for Unsteady Transonic Aerodynamics of Low-Aspect-Ratio Wings.” Journal of Aircraft 22 (3): 193–99. https://doi.org/10.2514/3.45107
• Guruswamy, Guru P., and Peter M. Goorjian. 1988. “Unsteady Transonic Aerodynamics and Aeroelastic Calculations at Low-Supersonic Freestreams.” Journal of Aircraft 25. https://ntrs.nasa.gov/citations/19890032774
• Habibniarami, Mehdi, Anders Lundbladh, Arthur Rizzi, Jesper Oppelstrup, and Tomas Grönstedt. 2026. “Optimization of a Supersonic Transport Aircraft Propulsion System.” Aerospace Science and Technology 175: 111943. https://doi.org/10.1016/j.ast.2026.111943
• Hacker, Tiberiu. 1977. “Attitude Instability in Steady Rolling and Roll Resonance.” Journal of Aircraft 14 (1): 23–31. https://doi.org/10.2514/3.44571
• Hacker, Tiberiu. 1978. “Constant-Control Rolling Maneuver.” Journal of Guidance and Control 1 (5): 313–18. https://doi.org/10.2514/3.55786
• Hagen, F. W., and H. Seidel. 1993. “Deutsche Airbus Flight Test of Rosemount Smart Probe for Distributed Air Data Systems.” In [1993 Proceedings] AIAA/IEEE Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.1993.283561
• Hagen, F. W., and H. Seidel. 1994. “Deutsche Airbus Flight Test of Rosemount Smart Probe for Distributed Air Data Systems.” IEEE Aerospace and Electronic Systems Magazine 9 (4): 7–14. https://doi.org/10.1109/62.277747
• Hai Zhao, Dengqing Cao, and Xinqun Zhu. 2010. “Aerodynamic Flutter and Limit Cycle Analysis for a 2-D Wing with Pitching Freeplay in the Supersonic Flow.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633970
• Hall, G. Warren, and Edward M. Boothe. 1972. “Lateral-Directional Dynamics and Roll Control Power for the Landing Approach.” Journal of Aircraft 9 (2): 129–36. https://doi.org/10.2514/3.58945
• Halwas, Hussein K., and Suresh Aggarwal. 2019a. “Effect of Side Gust on Performance of External Compression Supersonic Inlet.” Journal of Aircraft 56 (2): 569–82. https://doi.org/10.2514/1.c035093
• Halwas, Hussein K., and Suresh Aggarwal. 2019c. “Side Gust Effects on the Performance of a Supersonic Inlet with Bleed.” Journal of Aircraft 56 (6): 2357–70. https://doi.org/10.2514/1.c035481
• Hama, Takayuki, Takeyuki Sakai, Yusuke Fujisaki, Hitoshi Fujimoto, and Hirohiko Takuda. 2017. “Time-Dependent Springback of a Commercially Pure Titanium Sheet.” Procedia Engineering 207: 263–68. https://doi.org/10.1016/j.proeng.2017.10.772
• Hamel, Peter. 1970. “A System Analysis View of Aerodynamic Coupling.” Journal of Aircraft 7 (6): 567–69. https://doi.org/10.2514/3.44215
• Hamza, Mohamed H., Ruslan Polichshuk, Hyunseong Lee, Paul Parker, Angela Campbell, and Aditi Chattopadhyay. 2022. “Aircraft Post-Upset Flight Risk Region Prediction for Aviation Safety Management.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.4089181
• Han, Guoqing, Jianping Hu, Xianming Liu, Xiaohua Lei, and Peng Zhang. 2023. “Fiber Bragg Grating Total Temperature Probes for High-Speed Airflow with High Recovery Factor.” IEEE Sensors Journal 23 (22): 27406–15. https://doi.org/10.1109/jsen.2023.3322713
• Han, Fei, Jian-hua Mo, Pan Gong, and Min Li. 2011. “Method of Closed Loop Springback Compensation for Incremental Sheet Forming Process.” Journal of Central South University 18 (5): 1509–17. https://doi.org/10.1007/s11771-011-0867-3
• Han, Zheng, Yuhan Xing, Taiying Liu, Ning Zhang, Shaosong Jiang, and Zhen Lu. 2024. “Superplastic Forming/Diffusion Bonding of TA15 Titanium Alloy for Manufacturing Integrated Solid/Hollow Four-Layer Grid Lightweight Structure Components.” Metals 15 (1): 28. https://doi.org/10.3390/met15010028
• Hancock, G. J. 1959a. “Divergence of Plate Airfoils of Low Aspect Ratio at Supersonic Speeds.” Journal of the Aerospace Sciences 26 (8): 495–507. https://doi.org/10.2514/8.8168
• Hancock, G. J. 1960. “Comments on ‘Limiting Circulatory Lift of a Wing of Finite Aspect Ratio’.” Journal of the Aerospace Sciences 27 (1): 65–66. https://doi.org/10.2514/8.8377
• Harloff, Gary J., and Gregory E. Smith. 1996. “Supersonic-Inlet Boundary-Layer Bleed Flow.” AIAA Journal 34 (4): 778–85. https://doi.org/10.2514/3.13140
• Hartsell, Craig W. 1960. “Derivation of an Analytical Expression for Supersonic Spillage of Single-Cone Inlets.” Journal of the Aerospace Sciences 27 (10): 788–89. https://doi.org/10.2514/8.8748
• Hauptman, Aharon. 1987. “Exact and Asymptotic Expressions of the Lift Slope Coefficient of Anelliptic Wing.” AIAA Journal 25 (9): 1261–62. https://doi.org/10.2514/3.9776
• Herrmann, Dirk, Sergej Blem, and Ali Gulhan. 2011. “Experimental Study of Boundary-Layer Bleed Impact on Ramjet Inlet Performance.” Journal of Propulsion and Power 27 (6): 1186–95. https://doi.org/10.2514/1.b34223
• Hess, R. A., and P. W. Stout. 1998. “Assessing Aircraft Susceptibility to Nonlinear Aircraft-Pilot Coupling/Pilot-Induced Oscillations.” Journal of Guidance, Control, and Dynamics 21 (6): 957–64. https://doi.org/10.2514/2.4330
• 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
• Hilton, W. F. 1955. “Tests of a Fairing to Reduce the Drag of a Supersonic Swept-Wing Root.” Journal of the Aeronautical Sciences 22 (3): 173–78. https://doi.org/10.2514/8.3300
• Hino, Ryutaro, Yoshihiro Goto, and Fusahito Yoshida. 2003. “Springback of Sheet Metal Laminates in Draw-Bending.” Journal of Materials Processing Technology 139 (1–3): 341–47. https://doi.org/10.1016/s0924-0136(03)00541-7
• Hitzel, Stephan. 2017a. “High-Angle-of-Attack F-16XL Flight Simulations at Sub- and Transonic Speeds.” Journal of Aircraft 54 (6): 2014–26. https://doi.org/10.2514/1.c034025
• Hitzel, Stephan. 2017b. “Sub- and Transonic Vortex Breakdown Flight Condition Simulations of the F-16XL Aircraft.” Journal of Aircraft 54 (2): 428–43. https://doi.org/10.2514/1.c033246
• Ho, Ting Long. 1978. “Wear Studies on Aircraft Brake Materials.” Journal of Lubrication Technology 100 (1): 98–103. https://doi.org/10.1115/1.3453124
• Ho, T. L., F. E. Kennedy, and M. B. Peterson. 1979. “Evaluation of Aircraft Brake Materials.” A S L E Transactions 22 (1): 71–78. https://doi.org/10.1080/05698197908982904
• Ho, T. L., and M. B. Peterson. 1977. “Wear Formulation for Aircraft Brake Material Sliding against Steel.” Wear 43 (2): 199–210. https://doi.org/10.1016/0043-1648(77)90114-4
• 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
• Hollingsworth, E. G., and M. Cohen. 1971. “Determination of F-4 Aircraft Transonic Buffet Characteristics.” Journal of Aircraft 8 (10): 757–63. https://doi.org/10.2514/3.59167
• Holt, Maurice, and Sainsbury L. Strack. 1961. “Supersonic Panel Flutter of a Cylindrical Shell of Finite Length.” Journal of the Aerospace Sciences 28 (3): 197–208. https://doi.org/10.2514/8.8925
• Holzinger, Nico, and Torbjørn Cunis. 2024. “Verification of a Nonlinear Upset Recovery Control Law Using Scenario Optimisation⋆.” In 2024 IEEE Conference on Control Technology and Applications (CCTA). IEEE. https://doi.org/10.1109/ccta60707.2024.10666640
• Hong, Wooram, and Chongam Kim. 2014. “Computational Study on Hysteretic Inlet Buzz Characteristics under Varying Mass Flow Conditions.” AIAA Journal 52 (7): 1357–73. https://doi.org/10.2514/1.j052481
• Hong, Ming, and Weiwei Zhang. 2023. “Springback Prediction of Free Bending Based on Experimental Method.” Applied Sciences 13 (14): 8288. https://doi.org/10.3390/app13148288
• Hopkins, Edward J. 1977. “Effects of Wing Bend on the Aerodynamic Characteristics of a Low-Aspect-Ratio Oblique Wing.” Journal of Aircraft 14 (3): 225–26. https://doi.org/10.2514/3.58766
• Hoque, Abrar, Zahangir Alam, and Ashabul Hoque. 2023. “Approach to Determine the Circulation and Vorticity around Supersonic Airfoil with Spoiler.” Aerospace Systems 7 (3): 501–8. https://doi.org/10.1007/s42401-023-00244-3
• Hreha, M. A., and F. H. Lutze. 1984. “A Dynamic Model for Aircraft Poststall Departure.” Journal of Aircraft 21 (1): 62–68. https://doi.org/10.2514/3.48223
• Hu, Junshan, Ruihao Kang, Jinrong Fang, et al. 2024. “An Experimental and Parametrical Study on Repair of Cracked Titanium Airframe Structures with Single-Side Bonded Carbon Fiber-Reinforced Polymer Prepreg Patches.” Composite Structures 338: 118102. https://doi.org/10.1016/j.compstruct.2024.118102
• Huang, Yakun, Xiaomin He, Yi Jin, Huanyu Zhu, and Zhixin Zhu. 2021. “Effect of Non-Uniform Inlet Profile on the Combustion Performance of an Afterburner with Bluff Body.” Energy 216: 119142. https://doi.org/10.1016/j.energy.2020.119142
• Huang, Qian, Chengkun Lv, Danwei Li, Changjiang Gong, Juntao Chang, and Daren Yu. 2025. “Thermodynamic Modeling and Performance Analysis of RBCC Engine Ejector Mode Considering the Inlet Forebody Drag.” Energy 320: 135239. https://doi.org/10.1016/j.energy.2025.135239
• Huang, Ciying, Ziao Wang, Juntao Chang, Chengkun Lv, and Chen Kong. 2026. “Numerical Investigation of Axisymmetric Supersonic Inlet-Isolator Unstart under Upstream-Propagating Pressure Wave.” Aerospace Science and Technology 177: 112309. https://doi.org/10.1016/j.ast.2026.112309
• Huang, Wenbo, Rui Wang, Mengchuang Zhang, and Zhiping Yin. 2024. “The Research on Deep Learning-Driven Dimensionality Reduction and Strain Prediction Techniques Based on Flight Parameter Data.” Applied Sciences 14 (9): 3938. https://doi.org/10.3390/app14093938
• Huang, Da, and Genxing Wu. 2006. “Unsteady Rolling Moment Characteristics for a Fighter Oscillating with Yawing-Rolling Coupled Motion.” Journal of Aircraft 43 (5): 1570–73. https://doi.org/10.2514/1.21144
• Huang, Jiaoyan, Aiguo Xia, Shenao Zou, Cong Han, and Guoan Yang. 2020. “An Efficient Approach for Identification of the Inlet Distortion of Engine Based on Acoustic Emission Technique.” Applied Sciences 10 (22): 8240. https://doi.org/10.3390/app10228240
• Hui, Liu, Gu Hongbin, and Chen Dawei. 2008. “Application of High-Speed Solenoid Valve to the Semi-Active Control of Landing Gear.” Chinese Journal of Aeronautics 21 (3): 232–40. https://doi.org/10.1016/s1000-9361(08)60030-8
• Huili, Dong, Chen Xiying, and Liu Jinsheng. 2023. “Landing Performance Analysis and Multi-Parameter Optimization of Oil-Gas Separation Shock Strut of Landing Gear.” In 2023 9th International Conference on Fluid Power and Mechatronics (FPM). IEEE. https://doi.org/10.1109/fpm57590.2023.10565438
• Hunziker, Raul R. 1960. “On the Calculation of the Minimum Wave Plus Vortex Drag of Supersonic Wings.” Zeitschrift für angewandte Mathematik und Physik ZAMP 11 (6): 504–8. https://doi.org/10.1007/bf01595402
• Hutchins, Kelley E., Maruthi R. Akella, Noel T. Clemens, Jeffrey M. Donbar, and Sivaram Gogineni. 2014. “Experimental Identification of Transient Dynamics for Supersonic Inlet Unstart.” Journal of Propulsion and Power 30 (6): 1605–12. https://doi.org/10.2514/1.b35230
• Huyer, S. A., M. C. Robinson, and M. W. Luttges. 1992. “Unsteady Aerodynamic Loading Produced by a Sinusoidally Oscillating Delta Wing.” Journal of Aircraft 29 (3): 366–73. https://doi.org/10.2514/3.46171
• Hwang, Chintsun, and W. S. Pi. 1975a. “Northrop F-5A Aircraft Transonic Buffet Pressure Data Acquisition and Response Analysis.” Journal of Aircraft 12 (9): 714–20. https://doi.org/10.2514/3.44487
• Hwang, C., and W. S. Pi. 1979. “Aircraft Wake Flow Effect and Horizontal Tail Buffet.” Journal of Aircraft 16. https://ntrs.nasa.gov/citations/19790046469
• 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
• Iliff, Kenneth W. 1977. “Maximum Likelihood Estimation of Lift and Drag from Dynamic Aircraft Maneuvers.” Journal of Aircraft 14 (12): 1175–81. https://doi.org/10.2514/3.58911
• 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
• Imai, Masato, Kazuyuki Nakakita, and Masaharu Kameda. 2022. “Random-Dot Pressure-Sensitive Paint for Time-Resolved Measurement of Deformation and Surface Pressure of Transonic Wing Flutter.” Experiments in Fluids 63 (11): 174. https://doi.org/10.1007/s00348-022-03527-1
• Inger, G. R. 1979. “Transonic Shock-Boundary-Layer Interactions in Cryogenic Wind Tunnels.” Journal of Aircraft 16 (4): 284–87. https://doi.org/10.2514/3.58519
• Isakson, Gabriel. 1957. “A Simple Model Study of Transient Temperature and Thermal Stress Distribution Due to Aerodynamic Heating.” Journal of the Aeronautical Sciences 24 (8): 611–19. https://doi.org/10.2514/8.3917
• Ishikawa, Hiroaki, Dong-Youn Kwak, and Kenji Yoshida. 2008. “Numerical Analysis on Flight-Test Results of Supersonic Experimental Airplane NEXST-1.” Journal of Aircraft 45 (5): 1505–13. https://doi.org/10.2514/1.33595
• Isogai, Koji. 1979. “On the Transonic-Dip Mechanism of Flutter of a Sweptback Wing.” AIAA Journal 17 (7): 793–95. https://doi.org/10.2514/3.61226
• Isogai, Koji. 1981. “Transonic Dip Mechanism of Flutter of a Sweptback Wing. II.” AIAA Journal 19 (9): 1240–42. https://doi.org/10.2514/3.7853
• 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
• Ize, Carlos, and Andrew S. Arena. 1998. “Effects of Asymmetric Leading-Edge Flap Deflection on Delta Wings in Roll.” Journal of Aircraft 35 (6): 968–71. https://doi.org/10.2514/2.2394
• James, R. M. 1972. “Comments on ‘Convergence Proof of Discrete-Panel Wing Loading Theories’.” Journal of Aircraft 9 (5): 0383b-0383b. https://doi.org/10.2514/3.58999
• James, Jintu K., and Heuy Dong Kim. 2022. “Study on the Mechanism of the Buzz Flow in a Supersonic Intake.” Aerospace Science and Technology 131: 107982. https://doi.org/10.1016/j.ast.2022.107982
• James, Jintu K., Abhilash Suryan, and Heuy Dong Kim. 2021. “Buzz Characteristics and Separation Bubble Dynamics in Supersonic Intake.” Aerospace Science and Technology 115: 106795. https://doi.org/10.1016/j.ast.2021.106795
• Jardin, Matt R., and Eric R. Mueller. 2009. “Optimized Measurements of Unmanned-Air-Vehicle Mass Moment of Inertia with a Bifilar Pendulum.” Journal of Aircraft 46 (3): 763–75. https://doi.org/10.2514/1.34015
• 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, R. V., W. Monnich, D. Fischenberg, and B. Krag. 1997. “Identification of Speed Brake, Air-Drop, and Landing Gear Effects from Flight Data.” Journal of Aircraft 34 (2): 174–80. https://doi.org/10.2514/2.2169
• 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
• Jeans, Tiger L., Adam Jirásek, David R. McDaniel, Keith Bergeron, and Russell M. Cummings. 2012. “Modeling the Nonlinear Dynamic Roll of Generic Fighter Using Delayed Detached-Eddy Simulation.” Journal of Aircraft 49 (4): 1110–25. https://doi.org/10.2514/1.c031613
• Jenkins, Jerald M., Albert E. Kuhl, and Alan L. Carter. 1977. “Strain Gage Calibration of a Complex Wing.” Journal of Aircraft 14 (12): 1192–96. https://doi.org/10.2514/3.58914
• Jenkins, Jerry E., James H. Mayatt, and Ernest S. Hanff. 1996. “Body-Axis Rolling Motion Critical States of a 65-Degree Delta Wing.” Journal of Aircraft 33 (2): 268–78. https://doi.org/10.2514/3.46933
• Jenn, A. A., and H. F. Nelson. 1989. “Wing Vertical Position Effects on Lift for Supersonic Delta Wing Missiles.” Journal of Spacecraft and Rockets 26 (4): 210–16. https://doi.org/10.2514/3.26056
• Jian, Tang, and Zhu Ke-Qin. 2004. “Numerical and Experimental Study of Flow Structure of Low-Aspect-Ratio Wing.” Journal of Aircraft 41 (5): 1196–1201. https://doi.org/10.2514/1.5467
• Jiang, Chengjie, and Xiaolan Cheng. 2024. “Research on Seal Performance of Civil Aircraft Landing Gear Shock Absorbing System.” In 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae62008.2024.11026067
• Jiang, Yun, Daochun Li, Zi Kan, Bohao Dong, Chong Zhen, and Jinwu Xiang. 2024. “Bifurcation Analysis of Wing Rock and Routes to Chaos of a Low Aspect Ratio Flying Wing.” Nonlinear Dynamics 112 (23): 21491–21508. https://doi.org/10.1007/s11071-024-10134-8
• Jin, Yi, Shu Sun, Yue Zhang, Feng Xing, and Hui-jun Tan. 2022. “Throttling Characteristics of a Supersonic Variable Inlet at Different Internal Contraction Ratios.” AIAA Journal 60 (9): 5203–14. https://doi.org/10.2514/1.j061685
• Jin, Yi, Huijun Tan, Hao Zhang, Gaojie Zheng, Shu Sun, and Yue Zhang. 2023a. “Experimental Investigation on Unstart-Restart Hysteresis of a Supersonic Inlet during Throat Regulation.” Chinese Journal of Aeronautics 36 (11): 135–52. https://doi.org/10.1016/j.cja.2023.08.004
• Johns, David J. 1971. “Supersonic Membrane Flutter.” AIAA Journal 9 (5): 960–61. https://doi.org/10.2514/3.6309
• Johnson, Clarence L. 1935. “Longitudinal Stability of a Bi-Motor Transport Airplane.” Journal of the Aeronautical Sciences 3 (1): 1–6. https://doi.org/10.2514/8.111
• Johnson, Charles B. 1981. “Study of Nonadiabatic Boundary-Layer Stabilization Time in a Cryogenic Tunnel for Typical Wing and Fuselage Models.” Journal of Aircraft 18 (11): 913–19. https://doi.org/10.2514/3.57580
• Johnson, Ethan C., and Venkateswaran Narayanaswamy. 2024. “High-Bandwidth Pressure Field Imaging of Stream-Traced Inlet Unstart Dynamics.” AIAA Journal 62 (11): 4494–99. https://doi.org/10.2514/1.j064324
• Johnston, Donald E., and Jeffrey R. Hogge. 1976. “Nonsymmetric Flight Influence on High-Angle-of-Attack Handling and Departure.” Journal of Aircraft 13 (2): 112–18. https://doi.org/10.2514/3.58639
• Johnston, Christopher O., William H. Mason, and Cheolheui Han. 2010. “Unsteady Thin Airfoil Theory Revisited for a General Deforming Airfoil.” Journal of Mechanical Science and Technology 24 (12): 2451–60. https://doi.org/10.1007/s12206-010-0920-4
• Jones, Robert T. 1950a. “Leading-Edge Singularities in Thin-Airfoil Theory.” Journal of the Aeronautical Sciences 17 (5): 307–10. https://doi.org/10.2514/8.1622
• Jones, Arthur L. 1950b. “The Theoretical Lateral-Stability Derivatives for Wings at Supersonic Speeds.” Journal of the Aeronautical Sciences 17 (1): 39–46. https://doi.org/10.2514/8.1517
• Jones, D. S. 1967b. “Supersonic Flow and Wing-Body Interference.” Mathematika 14 (1): 68–93. https://doi.org/10.1112/s0025579300008032
• Jones, R. T. 1976a. “Aeroelastic Stability and Control of an Oblique Wing: Wind Tunnel Experiments.” Journal of Aircraft 13 (10): 830–32. https://doi.org/10.2514/3.44558
• Jones, Robert T. 1977. “The Oblique Wing—Aircraft Design for Transonic and Low Supersonic Speeds.” Acta Astronautica 4 (1–2): 99–109. https://doi.org/10.1016/0094-5765(77)90035-2
• Jones, Robert T. 1989. “The Minimum Drag of Thin Wings at Supersonic Speed According to Kogan’s Theory.” Theoretical and Computational Fluid Dynamics 1 (2, 19). https://ntrs.nasa.gov/citations/19890062528
• 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
• Kadkhodayan, M., and I. Zafarparandeh. 2008. “On the Relation of Equivalent Plastic Strain and Springback in Sheet Draw Bending.” International Journal of Material Forming 1 (S1): 141–44. https://doi.org/10.1007/s12289-008-0011-6
• Kalkhoran, Iraj M., Michael K. Smart, and Alexander Betti. 1996. “Interaction of Supersonic Wing-Tip Vortices with a Normal Shock.” AIAA Journal 34 (9): 1855–61. https://doi.org/10.2514/3.13318
• Kan, Hu, and Zhang Hailing. 2011. “A Springback Reduction Method for Sheet Metal Bending.” In 2011 International Conference on Mechatronic Science, Electric Engineering and Computer (MEC). IEEE. https://doi.org/10.1109/mec.2011.6025541
• Kandil, O. A., D. T. Mook, and A. H. Nayfeh. 1976. “Nonlinear Prediction of Aerodynamic Loads on Lifting Surfaces.” Journal of Aircraft 13 (1): 22–28. https://doi.org/10.2514/3.58625
• Kang, Byung-Hyuk, Jai-Hyuk Hwang, and Seung-Bok Choi. 2021. “A New Design Model of an MR Shock Absorber for Aircraft Landing Gear Systems Considering Major and Minor Pressure Losses: Experimental Validation.” Applied Sciences 11 (17): 7895. https://doi.org/10.3390/app11177895
• Kang, Jingtao, Ruidi Li, Dan Zheng, Minbo Wang, Pengda Niu, and Tiechui Yuan. 2024. “4D Printed NiTi Variable-Geometry Inlet for Aero Engines.” Virtual and Physical Prototyping 19 (1): e2382166. https://doi.org/10.1080/17452759.2024.2382166
• Karafillis, A. P., and M. C. Boyce. 1992. “Tooling Design in Sheet Metal Forming Using Springback Calculations.” International Journal of Mechanical Sciences 34 (2): 113–31. https://doi.org/10.1016/0020-7403(92)90077-t
• Karafillis, Apostolos P., and Mary C. Boyce. 1996. “Tooling and Binder Design for Sheet Metal Forming Processes Compensating Springback Error.” International Journal of Machine Tools and Manufacture 36 (4): 503–26. https://doi.org/10.1016/0890-6955(95)00023-2
• Karam, James T. 1975. “Dynamic Behavior of Angle-of-Attack Vane Assemblies.” Journal of Aircraft 12 (3): 190–92. https://doi.org/10.2514/3.44432
• Katz, J. 1979. “Method for Calculating Wing Loading during Maneuvering Flight along a Three-Dimensional Curved Path.” Journal of Aircraft 16 (11): 739–41. https://doi.org/10.2514/3.44637
• Katz, Joseph. 1989. “Aerodynamics of High-Lift, Low-Aspect-Ratio Unswept Wings.” AIAA Journal 27 (8): 1123–24. https://doi.org/10.2514/3.10231
• Katz, Joseph, and Daniel Levin. 1986. “Self-Induced Roll Oscillations Measured on a Delta Wing/canard Configuration.” Journal of Aircraft 23 (11): 814–19. https://doi.org/10.2514/3.45386
• Katz, Joseph, and Daniel Levin. 1991. “Static Measurements of Slender Delta Wing Rolling Moment Hysteresis.” Journal of Aircraft 28 (4): 282–83. https://doi.org/10.2514/3.46024
• Kaye, Joseph, and Victor C. M. Yeh. 1955. “Design Charts for Transient Temperature Distribution Resulting from Aerodynamic Heating at Supersonic Speeds.” Journal of the Aeronautical Sciences 22 (11): 755–62. https://doi.org/10.2514/8.3454
• Kaynak, Unver, Terry L. Holst, Brian J. Cantwell, and Reese L. Sorenson. 1987. “Numerical Simulation of Transonic Separated Flows over Low-Aspect-Ratio Wings.” Journal of Aircraft 24 (8): 531–39. https://doi.org/10.2514/3.45472
• Kazan, Recep, Mehmet Fırat, and Aysun Egrisogut Tiryaki. 2009. “Prediction of Springback in Wipe-Bending Process of Sheet Metal Using Neural Network.” Materials & Design 30 (2): 418–23. https://doi.org/10.1016/j.matdes.2008.05.033
• Keener, Earl R. 1985. “Computational/experimental Pressure Distributions on a Transonic, Low-Aspect-Ratio Wing.” Journal of Aircraft 22 (7): 545–46. https://doi.org/10.2514/3.45163
• Kemp, Nelson H. 1973. “Closed-Form Lift and Moment for Osborne’s Unsteady Thin-Airfoil Theory.” AIAA Journal 11 (9): 1358–60. https://doi.org/10.2514/3.6927
• Kemp, Nelson H. 1978. “Simplified Formulas for Lift and Moment in Unsteady Thin Airfoil Theory.” AIAA Journal 16 (8): 851–52. https://doi.org/10.2514/3.7589
• Kemp, Nelson H., and Gregory Homicz. 1976. “Approximate Unsteady Thin-Airfoil Theory for Subsonic Flow.” AIAA Journal 14 (8): 1083–89. https://doi.org/10.2514/3.7188
• Khaliulin, R. R., V. A. Sychenkov, and N. V. Stepicheva. 2022. “Research of Thrust Increase on the Ejector Turbojet Engine with the Afterburner.” In 2022 International Conference on Dynamics and Vibroacoustics of Machines (DVM). IEEE. https://doi.org/10.1109/dvm55487.2022.9930931
• Khamvilai, Thanakorn, and Eric N. Johnson. 2025. “Minimum Parameter Approximation of Nonlinear Aircraft Dynamics.” Journal of Guidance, Control, and Dynamics 48 (8): 1931–40. https://doi.org/10.2514/1.g008046
• Khan, M. Javed, Anwar Ahmed, and David C. Oehl. 2006. “Response of a Free-to-Roll Slender Delta Wings to Pitching and Plunging.” Journal of Aircraft 43 (1): 275–79. https://doi.org/10.2514/1.14260
• Khanna, Navneet, and J. P. Davim. 2015. “Design-of-Experiments Application in Machining Titanium Alloys for Aerospace Structural Components.” Measurement 61: 280–90. https://doi.org/10.1016/j.measurement.2014.10.059
• Khatri, Amit K., and Kamesh Subbarao. 2024. “A Comparative Study of Machine Learning Techniques for Aircraft Loss of Control Prediction.” In 2024 American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc60939.2024.10644512
• Khot, N. S., K. Appa, and F. E. Eastep. 2000. “Optimization of Flexible Wing without Ailerons for Rolling Maneuver.” Journal of Aircraft 37 (5): 892–97. https://doi.org/10.2514/2.2687
• Khot, N. S., F. E. Eastep, and R. M. Kolonay. 1997a. “Method for Enhancement of the Rolling Maneuver of a Flexible Wing.” Journal of Aircraft 34 (5): 673–78. https://doi.org/10.2514/2.2228
• Khot, N. S., R. M. Kolonay, and F. E. Eastep. 1999b. “Composite Wing Optimization for Enhancement of the Rolling Maneuver in Subsonic Flow.” Structural Optimization 17 (2): 95. https://doi.org/10.1007/s001580050041
• Khot, N. S., J. V. Zweber, D. E. Veley, H. Oz, and F. E. Eastep. 2002. “Flexible Composite Wing with Internal Actuation for Roll Maneuver.” Journal of Aircraft 39 (4): 521–27. https://doi.org/10.2514/2.2971
• Khrabrov, A., and M. Ol. 2004. “Effects of Flow Separation on Aerodynamic Loads in Linearized Thin Airfoil Theory.” Journal of Aircraft 41 (4): 944–48. https://doi.org/10.2514/1.5524
• Khudayarov, B. A. 2010. “Flutter of a Viscoelastic Plate in a Supersonic Gas Flow.” International Applied Mechanics 46 (4): 455–60. https://doi.org/10.1007/s10778-010-0328-y
• 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
• Kilgore, Robert A., Jerry B. Adcock, and Edward J. Ray. 1974. “Flight Simulation Characteristics of the Langley High Reynolds Number Cryogenic Transonic Tunnel.” Journal of Aircraft 11 (10): 593–600. https://doi.org/10.2514/3.60395
• Kilner, J. R. 1982. “Pneumatic Tire Model for Aircraft Simulation.” Journal of Aircraft 19 (10): 851–57. https://doi.org/10.2514/3.44786
• Kim, Yushin, Yong-Hee Jeon, and Dong-Ho Lee. 2006. “Multi-Objective and Multidisciplinary Design Optimization of Supersonic Fighter Wing.” Journal of Aircraft 43 (3): 817–24. https://doi.org/10.2514/1.13864
• Kim, Soobin, Dong-Hyuck Kam, and Kee-Ahn Lee. 2025. “High-Temperature Strength and Microstructural Evolution of Ti-6Al-4V Alloy Fabricated by Wire Arc Additive Manufacturing under Elevated Temperature.” Scientific Reports 16 (1): 2154. https://doi.org/10.1038/s41598-025-31895-1
• Kim, Heung-Kyu, and Woo-Jin Kim. 2018. “A Springback Prediction Model for Warm Forming of Aluminum Alloy Sheets Using Tangential Stresses on a Cross-Section of Sheet.” Metals 8 (4): 257. https://doi.org/10.3390/met8040257
• Kim, Hong Seok, and Muammer Koç. 2008. “Numerical Investigations on Springback Characteristics of Aluminum Sheet Metal Alloys in Warm Forming Conditions.” Journal of Materials Processing Technology 204 (1–3): 370–83. https://doi.org/10.1016/j.jmatprotec.2007.11.059
• Kim, HyoungJin, Takayasu Kumano, Meng-Sing Liou, Louis A. Povinelli, and Timothy R. Conners. 2011a. “Flow Simulation of Supersonic Inlet with Bypass Annular Duct.” Journal of Propulsion and Power 2011 27 (1). https://ntrs.nasa.gov/citations/20110011992
• Kim, Dong-Hyun, and In Lee. 2002. “Nonlinear Flutter Characteristics of Composite Missile Wing in Transonic/Low-Supersonic Flows.” Journal of Aircraft 39 (5): 889–92. https://doi.org/10.2514/2.3011
• Kim, Minki, Hyungrim Lee, and Namsu Park. 2022. “Evaluation of Deformation for Titanium Alloy Sheet in Single Point Incremental Forming Based on Asymmetric Yield Function.” International Journal of Material Forming 15 (5): 66. https://doi.org/10.1007/s12289-022-01712-5
• Kim, David, and Maciej Marciniak. 2000. “Prediction of Vertical Tail Maneuver Loads Using Backpropagation Neural Networks.” Journal of Aircraft 37 (3): 526–30. https://doi.org/10.2514/2.2630
• Kim, David, and Maciej Marciniak. 2002. “Horizontal Tail Maneuver Load Predictions Using Backpropagation Neural Networks.” Journal of Aircraft 39 (2): 365–70. https://doi.org/10.2514/2.2936
• Kim, Jinwhan, Karthik Palaniappan, and P. K. Menon. 2010. “Rapid Estimation of Impaired-Aircraft Aerodynamic Parameters.” Journal of Aircraft 47 (4): 1216–28. https://doi.org/10.2514/1.46914
• Kim, Keun-Taek, and Ohseop Song. 2013. “Aileron Reversal of Nonuniform and Swept Composite Aircraft Wings.” Journal of Aircraft 50 (3): 681–93. https://doi.org/10.2514/1.c031212
• Kimble, K. R., D. D. Liu, S. Y. Rou, and J. M. Wu. 1974. “Unsteady Transonic Flow Analysis for Low Aspect Ratio, Pointed Wings.” AIAA Journal 12 (4): 516–22. https://doi.org/10.2514/3.49278
• Klein, Dominik, and Chamil Abeykoon. 2015. “Modelling of a Turbojet Gas Turbine Engine.” In 2015 Internet Technologies and Applications (ITA). IEEE. https://doi.org/10.1109/itecha.2015.7317395
• 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
• Knight, Doyle D. 1981. “Calculation of High-Speed Inlet Flows Using the Navier-Stokes Equations.” Journal of Aircraft 18 (9): 748–54. https://doi.org/10.2514/3.57557
• Knowles, J. A. C., B. Krauskopf, and M. Lowenberg. 2012. “Numerical Continuation Analysis of a Three-Dimensional Aircraft Main Landing Gear Mechanism.” Nonlinear Dynamics 71 (1–2): 331–52. https://doi.org/10.1007/s11071-012-0664-z
• KoÇAk, Göktuğ, and Mehmet Metin Yavuz. 2023. “Aerodynamics of Non-Slender Delta and Reverse Delta Wings: Wing Thickness, Anhedral Angle and Cropping Ratio.” Chinese Journal of Aeronautics 36 (4): 79–91. https://doi.org/10.1016/j.cja.2022.06.015
• Kofman, Sergey, and Georges A. Becus. 1996. “Determination of Aircraft Stall Margins during Takeoff.” Journal of Aircraft 33 (3): 634–37. https://doi.org/10.2514/3.46996
• Kohlman, David L. 1967. “Rolling Moment Due to Sideslip of Delta Wings.” Journal of Aircraft 4 (6): 565–67. https://doi.org/10.2514/3.43895
• Kolodner, I. 1950. “On the Linearized Theory of Supersonic Flows through Axially Symmetrical Ducts.” Communications on Pure and Applied Mathematics 3 (2): 133–52. https://doi.org/10.1002/cpa.3160030203
• Kolom, Aaron L. 1969. “Titanium Diffusion-Bonded Honeycomb: Optimum Structure for Material, Joining Medium, and Configuration.” Journal of Aircraft 6 (5): 410–15. https://doi.org/10.2514/3.44079
• Kolonay, R. M., and Henry T. Y. Yang. 1998. “Static Aeroelastic Effects on a Transonic Indicial Response Wing Flutter Calculation.” Journal of Aircraft 35 (2): 339–41. https://doi.org/10.2514/2.7578
• Koo, Heeseok, and Venkatramanan Raman. 2012. “Large-Eddy Simulation of a Supersonic Inlet-Isolator.” AIAA Journal 50 (7): 1596–1613. https://doi.org/10.2514/1.j051568
• Kopzon, G. I. 1958. “Vibration of a Thin Rectangular Wing of Large Aspect Ratio in a Supersonic Stream.” Journal of Applied Mathematics and Mechanics 22 (6): 1153–61. https://doi.org/10.1016/0021-8928(58)90040-6
• 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
• 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
• Krasovskyy, Andriy, Winfried Schmitt, and Hermann Riedel. 2006. “Material Characterisation for Reliable and Efficient Springback Prediction in Sheet Metal Forming.” steel research international 77 (9–10): 747–53. https://doi.org/10.1002/srin.200606457
• Krispin, J., and H. Portnoy. 1988. “Analysis of Strake-Slender-Wing Configurations Using Slender-Wing Theory.” Journal of Aircraft 25 (1): 32–36. https://doi.org/10.2514/3.45537
• Kuchinka, A. J. 1966. “Prediction of off-Runway Takeoff and Landing Performance.” Journal of Aircraft 3 (3): 213–18. https://doi.org/10.2514/3.43727
• Kukuryk, Marcin. 2025. “Effects of Anvils Shape and Technological Conditions on the Quality during Hot Cogging Process of the Two—Phase Titanium Alloy.” International Journal of Material Forming 18 (4): 83. https://doi.org/10.1007/s12289-025-01944-1
• Kulfan, Brenda. 2009. “New Supersonic Wing Far-Field Composite-Element Wave-Drag Optimization Method.” Journal of Aircraft 46 (5): 1740–58. https://doi.org/10.2514/1.42823
• Kumar Sharma, Pankaj, Vijay Gautam, and Atul Kumar Agrawal. 2022. “Investigations on Effect of Bending Radius on Springback Behaviour of Three-Ply Clad Sheet.” Materials Today: Proceedings 62: 1651–57. https://doi.org/10.1016/j.matpr.2022.04.601
• Kut, Stanisław, Feliks Stachowicz, and Grzegorz Pasowicz. 2021. “Springback Prediction for Pure Moment Bending of Aluminum Alloy Square Tube.” Materials 14 (14): 3814. https://doi.org/10.3390/ma14143814
• Kutney, John T., and Stanley P. Piszkin. 1964. “Reduction of Drag Rise on the Convair 990 Airplane.” Journal of Aircraft 1 (1): 8–12. https://doi.org/10.2514/3.43551
• Kwatny, Harry G., Jean-Etienne T. Dongmo, Bor-Chin Chang, Gaurav Bajpai, Murat Yasar, and Christine Belcastro. 2013. “Nonlinear Analysis of Aircraft Loss of Control.” Journal of Guidance, Control, and Dynamics 36 (1): 149–62. https://doi.org/10.2514/1.56948
• 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
• Lagemann, Esther, Steven L. Brunton, Wolfgang Schröder, and Christian Lagemann. 2024. “Towards Extending the Aircraft Flight Envelope by Mitigating Transonic Airfoil Buffet.” Nature Communications 15 (1): 5020. https://doi.org/10.1038/s41467-024-49361-3
• Lagerstrom, P. A., and Martha E. Graham. 1949. “Linearized Theory of Supersonic Control Surfaces.” Journal of the Aeronautical Sciences 16 (1): 31–34. https://doi.org/10.2514/8.11719
• Lagerstrom, P. A., and M. E. Graham. 1951. “Remarks on Low-Aspect-Ratio Configurations in Supersonic Flow.” Journal of the Aeronautical Sciences 18 (2): 91–96. https://doi.org/10.2514/8.1864
• Laitone, E. V. 1978a. “Ideal Tail Load for Minimum Aircraft Drag.” Journal of Aircraft 15 (3): 190–92. https://doi.org/10.2514/3.58339
• Laitone, E. V. 1978b. “Positive Tail Loads for Minimum Induced Drag of Subsonic Aircraft.” Journal of Aircraft 15 (12): 837–42. https://doi.org/10.2514/3.58457
• Laitone, E. V. 1989. “Lift-Curve Slope for Finite-Aspect-Ratio Wings.” Journal of Aircraft 26 (8): 789–90. https://doi.org/10.2514/3.45841
• Lal, Radha Krishna, Vikas Kumar Choubey, J. P. Dwivedi, and Shravan Kumar. 2018. “Study of Factors Affecting Springback in Sheet Metal Forming and Deep Drawing Process.” Materials Today: Proceedings 5 (2): 4353–58. https://doi.org/10.1016/j.matpr.2017.12.002
• Lal, Radha Krishna, Jai Prakash Dwivedi, Manish Kumar Bhagat, and Virendra Pratap Singh. 2016. “Springback Analysis in Sheet Metal Forming of Non-Linear Work-Hardening Material under Pure Bending.” Journal of The Institution of Engineers (India): Series C 98 (2): 155–70. https://doi.org/10.1007/s40032-016-0333-y
• Lamar, John E., Roy T. Schemensky, and C. Subba Reddy. 1981. “Development of a Vortex-Lift Design Procedure and Application to a Slender Maneuver-Wing Configuration.” Journal of Aircraft 18 (4): 259–66. https://doi.org/10.2514/3.57490
• Lan, C. Edward, Silvia Bianchi, and Jay M. Brandon. 2008a. “Effects of Bearing Friction of a Free-to-Roll Rig on Transonic Lateral Dynamics.” Journal of Aircraft 45 (1): 298–305. https://doi.org/10.2514/1.30387
• Lan, C. Edward, Silvia Bianchi, and Jay M. Brandon. 2008b. “Estimation of Nonlinear Aerodynamic Roll Models for Identification of Uncommanded Rolling Motions.” Journal of Aircraft 45 (3): 916–22. https://doi.org/10.2514/1.30388
• Lan, F., J. Chen, and J. Lin. 2006b. “A Method of Constructing Smooth Tool Surfaces for FE Prediction of Springback in Sheet Metal Forming.” Journal of Materials Processing Technology 177 (1–3): 382–85. https://doi.org/10.1016/j.jmatprotec.2006.04.092
• Lan, C.-T., and J. Roskam. 1972. “Leading-Edge Force Features of the Aerodynamic Finite Element Method.” Journal of Aircraft 9. https://ntrs.nasa.gov/citations/19730032411
• Langtry, R. B., M. Kuntz, and F. R. Menter. 2005. “Drag Prediction of Engine-Airframe Interference Effects with CFX-5.” Journal of Aircraft 42 (6): 1523–29. https://doi.org/10.2514/1.12728
• Lapygin, V. I., and G. Ye. Yakunina. 2009. “The Shapes of Bodies with Maximum Lift-to-Drag Ratio in Supersonic Flow.” Journal of Applied Mathematics and Mechanics 73 (5): 514–23. https://doi.org/10.1016/j.jappmathmech.2009.11.004
• Larson, Erik S. 1984. “Aerodynamics of Very Slender Rectangular Wing Bodies to High Incidence.” Journal of Aircraft 21 (1): 50–53. https://doi.org/10.2514/3.48221
• Lawanwomg, Komgrit, Hiroshi Hamasaki, Ryutaro Hino, and Fusahito Yoshida. 2014. “A Novel Technology to Eliminate U-Bending Springback of High Strength Steel Sheet by Using Additional Bending with Counter Punch.” Procedia Engineering 81: 957–62. https://doi.org/10.1016/j.proeng.2014.10.124
• Lawanwong, Komgrit, Hiroshi Hamasaki, Ryutaro Hino, and Fusahito Yoshida. 2019. “Double-Action Bending for Eliminating Springback in Hat-Shaped Bending of Advanced High-Strength Steel Sheet.” International Journal of Advanced Manufacturing Technology 106 (5–6): 1855–67. https://doi.org/10.1007/s00170-019-04678-y
• Lawing, Pierce L., and Charles B. Johnson. 1978. “Inlet Boundary-Layer Shapes on Four Aircraft Forebodies at Mach 6.” Journal of Aircraft 15 (1): 62–63. https://doi.org/10.2514/3.58313
• Lawrence, H. R. 1951. “The Lift Distribution on Low Aspect Ratio Wings at Subsonic Speeds.” Journal of the Aeronautical Sciences 18 (10): 683–95. https://doi.org/10.2514/8.2079
• Lawrence, H. R. 1953. “The Aerodynamic Characteristics of Low Aspect Ratio Wing-Body Combinations in Steady Subsonic Flow.” Journal of the Aeronautical Sciences 20 (8): 541–48. https://doi.org/10.2514/8.2724
• Le Fur, Bernard. 1959. “Heat Transfer and Recovery Factor in a Laminar Boundary Layer with Arbitrary Pressure Gradient and Wall Temperature Distribution.” Journal of the Aerospace Sciences 26 (10): 682–83. https://doi.org/10.2514/8.8258
• Lee, B. H. K. 1984. “A Method for Predicting Wing Response to Buffet Loads.” Journal of Aircraft 21 (1): 85–87. https://doi.org/10.2514/3.48227
• Lee, B. H. K., and D. Brown. 1997. “Aerodynamic Characteristics of the F/A-18 at Large Roll Angles and High Incidence.” Journal of Aircraft 34 (1): 139–41. https://doi.org/10.2514/2.2149
• Lee, Hsing-Juin, and Cheng-Yi Chiou. 1994. “Aircraft Landing Gear Positioning Concerning Abnormal Landing Cases.” Journal of Aircraft 31 (2): 446–49. https://doi.org/10.2514/3.46508
• Lee, Myoung-Gyu, and Sung-Joon Kim. 2012. “Elastic-Plastic Constitutive Model for Accurate Springback Prediction in Hot Press Sheet Forming.” Metals and Materials International 18 (3): 425–32. https://doi.org/10.1007/s12540-012-3007-1
• Lee, Hyoung Jin, Bok Jik Lee, Sung Don Kim, and In-Seuck Jeung. 2009. “Investigation of the Pseudo-Shock Wave in a Two-Dimensional Supersonic Inlet.” Journal of Visualization 13 (1): 25–32. https://doi.org/10.1007/s12650-009-0008-3
• Lee, S. W., and D. Y. Yang. 1998. “An Assessment of Numerical Parameters Influencing Springback in Explicit Finite Element Analysis of Sheet Metal Forming Process.” Journal of Materials Processing Technology 80-81: 60–67. https://doi.org/10.1016/s0924-0136(98)00177-0
• 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
• Leen, S. B., M. A. Kröhn, and T. H. Hyde. 2008. “Failure Prediction for Titanium Alloys Using a Superplastic Forming Limit Diagram Approach.” Materialwissenschaft und Werkstofftechnik 39 (4–5): 327–31. https://doi.org/10.1002/mawe.200800299
• Leen, S. B., and M. Stoyanov. 2009. “Finite Element Modelling of Damage in Superplastic Forming of a Titanium Alloy.” International Journal of Material Forming 2 (S1): 287–90. https://doi.org/10.1007/s12289-009-0569-7
• 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
• Lehtinen, Bruce, and John R. Zeller. 1972. “Application of Quadratic Optimization to Supersonic Inlet Control.” Automatica 8 (5): 563–74. https://doi.org/10.1016/0005-1098(72)90027-1
• Lei, Juanmian, Shuai Zhao, and Suozhu Wang. 2016. “Numerical Study of Aerodynamic Characteristics of FSW Aircraft with Different Wing Positions under Supersonic Condition.” Chinese Journal of Aeronautics 29 (4): 914–23. https://doi.org/10.1016/j.cja.2016.06.006
• 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, Gerard. 1995. “Reduced-Order Nonlinear Analysis of Aircraft Dynamics.” Journal of Guidance, Control, and Dynamics 18 (2): 361–64. https://doi.org/10.2514/3.21392
• Leontiev, A. I., V. G. Lushchik, and M. S. Makarova. 2017. “The Temperature Recovery Factor in a Boundary Layer on a Permeable Plate.” High Temperature 55 (2): 246–52. https://doi.org/10.1134/s0018151x17020080
• Leontiev, A. I., V. G. Lushchik, M. S. Makarova, and S. S. Popovich. 2022. “Temperature Recovery Factor in a Compressible Turbulent Boundary Layer.” High Temperature 60 (3): 409–31. https://doi.org/10.1134/s0018151x22030117
• Leopold, F., G. Gastebois, A. Lacour, L. Gross, and E. Sommer. 2005. “Wind Tunnel Rig for the Study of Roll Damping and Pitch Damping Effects of Free-Spinning Models at Supersonic Speed.” In ICIASF 2005 RecordInternational Congress onInstrumentation in AerospaceSimulation Facilities. IEEE. https://doi.org/10.1109/iciasf.2005.1569900
• Lerro, Angelo, Alberto Brandl, Manuela Battipede, and Piero Gili. 2020. “A Data-Driven Approach to Identify Flight Test Data Suitable to Design Angle of Attack Synthetic Sensor for Flight Control Systems.” Aerospace 7 (5): 63. https://doi.org/10.3390/aerospace7050063
• Levin, Daniel, and Joseph Katz. 1984. “Dynamic Load Measurements with Delta Wings Undergoing Self-Induced Roll Oscillations.” Journal of Aircraft 21 (1): 30–36. https://doi.org/10.2514/3.48218
• Levin, Daniel, and Joseph Katz. 1992. “Self-Induced Roll Oscillations of Low-Aspect-Ratio Rectangular Wings.” Journal of Aircraft 29 (4): 698–702. https://doi.org/10.2514/3.46222
• Levin, D., and A. Seginer. 1982. “Chordwise and Compressibility Corrections for Arbitrary Planform Slender Wings.” AIAA Journal 20. https://ntrs.nasa.gov/citations/19820054396
• Li, Ting-Yi. 1951. “Purely Rolling Oscillations of a Rectangular Wing in Supersonic Flow.” Journal of the Aeronautical Sciences 18 (3): 191–98. https://doi.org/10.2514/8.1899
• Li, Ta. 1956. “Aerodynamic Influence Coefficients for an Oscillating Finite Thin Wing in Supersonic Flow.” Journal of the Aeronautical Sciences 23 (7): 613–22. https://doi.org/10.2514/8.3625
• 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, Nan, Juntao Chang, Chenzhong Jiang, et al. 2018c. “Unstart/restart Hysteresis Characteristics Analysis of an Over–under TBCC Inlet Caused by Backpressure and Splitter.” Aerospace Science and Technology 72: 418–25. https://doi.org/10.1016/j.ast.2017.11.026
• Li, Hao, Shuai-Feng Chen, Shi-Hong Zhang, Yong Xu, and Hong-Wu Song. 2022a. “Deformation Characteristics, Formability and Springback Control of Titanium Alloy Sheet at Room Temperature: A Review.” Materials 15 (16): 5586. https://doi.org/10.3390/ma15165586
• Li, Teng-fei, Run-han Ding, Wei-xing Wang, and Wen-zhong Xie. 2023a. “Comparison of the Unstart/restart Processes of a Two-Dimensional Twin-Duct Supersonic Inlet Induced by the Plug Throttling and Thermal Choking at the Sideslip State.” Aerospace Science and Technology 142: 108667. https://doi.org/10.1016/j.ast.2023.108667
• Li, Wu, and Karl Geiselhart. 2024. “Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport.” Journal of Aircraft 61 (2): 331–44. https://doi.org/10.2514/1.c037310
• Li, Wu, and Karl Geiselhart. 2026. “Consistent Coupling of Aeropropulsive and Engine Performance Analyses for Low-Boom Supersonic Aircraft Conceptual Design.” Journal of Aircraft: 1–11. https://doi.org/10.2514/1.c038747
• Li, Wesley W., and Chan-gi Pak. 2015. “Mass Balancing Optimization Study to Reduce Flutter Speeds of the X-56A Aircraft.” Journal of Aircraft 52 (4): 1359–65. https://doi.org/10.2514/1.c033044
• Li, Pei, Helmut Sobieczky, and Richard Seebass. 1999. “Manual Aerodynamic Optimization of an Oblique Wing Supersonic Transport.” Journal of Aircraft 36 (6): 907–13. https://doi.org/10.2514/2.2547
• Li, Shou an, Bifeng Song, and Hengxi Zhang. 2007. “Method for Multivariate Analysis with Small Sample in Aircraft Cost Estimation.” Journal of Aircraft 44 (3): 1042–45. https://doi.org/10.2514/1.28174
• Li, T. Y., and H. J. Stewart. 1953. “On an Integral Equation in the Supersonic Oscillating Wing Theory.” Journal of the Aeronautical Sciences 20 (10): 724–26. https://doi.org/10.2514/8.2811
• Li, Yongzhou, Di Sun, Zejun Wu, and Kunyuan Zhang. 2023b. “Flow Coefficient and Starting Performance Prediction of Variable Geometry Curved Axisymmetric Inlet.” Aerospace 10 (6): 506. https://doi.org/10.3390/aerospace10060506
• Li, Minqiang, Zhiwu Wang, and Junlin Li. 2024b. “Numerical Study on the Performance of a New Integrated Afterburner under a Wide Range of Bypass Ratio Conditions.” Energy 313: 133919. https://doi.org/10.1016/j.energy.2024.133919
• Li, Minqiang, Zhiwu Wang, and Junlin Li. 2026. “Numerical Investigation of Cooling Performance in the Integrated Afterburner Heat Shield with Structural Modifications under Reacting Flow Conditions.” Aerospace Science and Technology 172: 111756. https://doi.org/10.1016/j.ast.2026.111756
• Li, Haoyue, Yong Xu, Jiuhui Ding, and Kangrui Zhai. 2021a. “Analysis of High Precision Moment of Inertia Measurement Method Based on Torsion Pendulum Method.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550715
• Li, Jian, Jun Zhao, Hong-lei Sun, and Rui Ma. 2008. “Improvement of Springback Prediction of Wide Sheet Metal Air Bending Process.” Journal of Central South University of Technology 15 (S2): 310–15. https://doi.org/10.1007/s11771-008-0478-9
• Li, Fuyou, Jianxin Zhu, Xiangfu Zou, Zhongjian Pan, and Jian Chen. 2025. “Multibody Analysis of Lever-Spring Landing Gear with Elastomer Shock Absorbers: Modelling, Simulations and Drop Tests.” Aerospace 12 (5): 367. https://doi.org/10.3390/aerospace12050367
• Li Yinan, Yang Lingyu, and Shen Gongzhang. 2012. “Steady Maneuver Envelope Evaluation for Aircraft with Control Surface Failures.” In 2012 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2012.6187317
• Liaw, Der-Cherng, and Chau-Chung Song. 2001. “Analysis of Longitudinal Flight Dynamics: A Bifurcation-Theoretic Approach.” Journal of Guidance, Control, and Dynamics 24 (1): 109–16. https://doi.org/10.2514/2.4682
• Librescu, L., and E. Malaiu. 1968. “Supersonic Flutter of Circular Cylindrical Heterogeneous Orthotropic Thin Panels of Finite Length.” Journal of Sound and Vibration 8 (3): 494–512. https://doi.org/10.1016/0022-460x(68)90253-8
• Librescu, Liviu, Piergiovanni Marzocca, and Walter A. Silva. 2004. “Linear/Nonlinear Supersonic Panel Flutter in a High-Temperature Field.” Journal of Aircraft 41 (4): 918–24. https://doi.org/10.2514/1.679
• 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
• Licher, R. M. 1956. “Reduction of Drag Due to Lift in Supersonic Flight by Distributing Lift along a Fuselage.” Journal of the Aeronautical Sciences 23 (11): 1037–43. https://doi.org/10.2514/8.3718
• Lichota, Piotr, and Maciej Lasek. 2013. “Maximum Likelihood Estimation: A Method for Flight Dynamics: Angle of Attack Estimation.” In Proceedings of the 14th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/carpathiancc.2013.6560541
• 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
• “Lift Effect on Transonic Wind-Tunnel Blockage.” 1980. Journal of Aircraft 17 (1): 5–6. https://doi.org/10.2514/3.44692
• Lilley, J. S., and S. L. Pengelly. 1993. “Wind-Tunnel Evaluation of Mid-Airframe Installed Turbojet Engines.” Journal of Propulsion and Power 9 (6): 858–66. https://doi.org/10.2514/3.23700
• Lin, JiGuan G. 2016. “Reducing Induced Drag and Maneuver Loads by Active Aeroelastic Alteration.” Journal of Aircraft 53 (6): 1787–1801. https://doi.org/10.2514/1.c033701
• Lin, Charrissa Y., Edward F. Crawley, and Jennifer Heeg. 1996. “Open- and Closed-Loop Results of a Strain-Actuated Active Aeroelastic Wing.” Journal of Aircraft 33 (5): 987–94. https://doi.org/10.2514/3.47045
• Lin, Peng, Xueqiang Liu, Neng Xiong, et al. 2021. “Numerical Study on the Influence of Wall Temperature Gradient on Aerodynamic Characteristics of Low Aspect Ratio Flying Wing Configuration.” Scientific Reports 11 (1): 16295. https://doi.org/10.1038/s41598-021-94261-x
• Lin, Peng, Tianlei Zhou, Haoran Yao, Zhuoyun Yang, Ao Liu, and Guojiang Dong. 2026. “Physics-Guided Curvature-Aware Network for Springback Compensation in Curved Sheet-Metal Forming.” International Journal of Mechanical Sciences 328: 112011. https://doi.org/10.1016/j.ijmecsci.2026.112011
• Linehan, Thomas, and Kamran Mohseni. 2016b. “Roll Stall for Low-Aspect-Ratio Wings.” Journal of Aircraft 53 (4): 1186–88. https://doi.org/10.2514/1.c033766
• Ling, Zhao, Ji Chen, Yang Yinong, and Liu Ziqiang. 2015. “Flutter Influence Mode Analysis of High Speed Wing Model.” Procedia Engineering 99: 33–38. https://doi.org/10.1016/j.proeng.2014.12.504
• Ling, Y. E., H. P. Lee, and B. T. Cheok. 2005. “Finite Element Analysis of Springback in L-Bending of Sheet Metal.” Journal of Materials Processing Technology 168 (2): 296–302. https://doi.org/10.1016/j.jmatprotec.2005.02.236
• “Liquid Brake System for Aircraft.” 1958. Journal of the Franklin Institute 265 (5): 435–36. https://doi.org/10.1016/0016-0032(58)90757-9
• Lissenden, C., D. Doraiswamy, and S. Arnold. 2007. “Experimental Investigation of Cyclic and Time-Dependent Deformation of Titanium Alloy at Elevated Temperature.” International Journal of Plasticity 23 (1): 1–24. https://doi.org/10.1016/j.ijplas.2006.01.006
• Liu, Gang, Kexin Dang, Kehuan Wang, and Jie Zhao. 2020. “Progress on Rapid Hot Gas Forming of Titanium Alloys: Mechanism, Modelling, Innovations and Applications.” Procedia Manufacturing 50: 265–70. https://doi.org/10.1016/j.promfg.2020.08.049
• Liu, J. G., M. W. Fu, J. Lu, and W. L. Chan. 2011b. “Influence of Size Effect on the Springback of Sheet Metal Foils in Micro-Bending.” Computational Materials Science 50 (9): 2604–14. https://doi.org/10.1016/j.commatsci.2011.04.002
• Liu, Haojie, and Xiumin Gao. 2020. “Identification of Nonlinear Aerodynamic Systems with Application to Transonic Aeroelasticity of Aircraft Structures.” Nonlinear Dynamics 100 (2): 1037–56. https://doi.org/10.1007/s11071-020-05553-2
• Liu, Steven Y., James T. Gordon, and M. Akif Ozbek. 1998. “Nonlinear Model for Aircraft Brake Squeal Analysis: Model Description and Solution Methodology.” Journal of Aircraft 35 (4): 623–30. https://doi.org/10.2514/2.2346
• Liu, Wenjuan, Qiang Liu, Feng Ruan, Zhiyong Liang, and Hongyang Qiu. 2007. “Springback Prediction for Sheet Metal Forming Based on GA-ANN Technology.” Journal of Materials Processing Technology 187-188: 227–31. https://doi.org/10.1016/j.jmatprotec.2006.11.087
• Liu, Zhichao, Jiabin Liu, Jialei Yan, and Anxin Guo. 2025a. “Analysis of Wave Boundary Effect on the Flutter Performance of the Thin Plate.” Engineering Structures 343: 121242. https://doi.org/10.1016/j.engstruct.2025.121242
• Liu, Zijian, Lidong Ma, Zhijuan Meng, Peiyu Liu, and Yukang Du. 2021b. “Effect of Yield Criterion and Variable Elastic Modulus on Springback Prediction of Ti-6Al-4V Sheet V-Shaped Bending.” International Journal of Advanced Manufacturing Technology 116 (5–6): 1925–36. https://doi.org/10.1007/s00170-021-07452-1
• Liu, Bokai, Jie Pang, Xiaoguang Tu, and Zhiming Zhou. 2023b. “Three Components Strain-Gauge Type Aircraft Surface Friction Resistance Sensor: Design, Manufacturing, and Calibration.” Measurement 218: 113165. https://doi.org/10.1016/j.measurement.2023.113165
• Liu, Wenbin, and Youshan Wang. 2024. “Improved Multi-Body Dynamic Simulation of Landing Gear Drop Test Incorporating Structural Flexibility and Bearing Contact.” Aerospace 11 (7): 543. https://doi.org/10.3390/aerospace11070543
• Liu, Wenbin, Youshan Wang, and Yuchen Ji. 2023a. “Landing Impact Load Analysis and Validation of a Civil Aircraft Nose Landing Gear.” Aerospace 10 (11): 953. https://doi.org/10.3390/aerospace10110953
• Liu, Yixin, Kuankuan Wang, Zhipeng Pan, et al. 2026a. “First Integration of Triboelectric Sensing into Flight Control System for in-Flight Angle of Attack Monitoring and Stall Warning.” Chemical Engineering Journal 546: 180391. https://doi.org/10.1016/j.cej.2026.180391
• Liu, Yuan, Lu Wang, and Zhansen Qian. 2018. “Numerical Investigation on the Assistant Restarting Method of Variable Geometry for High Mach Number Inlet.” Aerospace Science and Technology 79: 647–57. https://doi.org/10.1016/j.ast.2018.06.014
• Liu, Gang, Yong Wu, Jie Zhao, Kai Wang, and Shijian Yuan. 2014b. “Formability Determination of Titanium Alloy Tube for High Pressure Pneumatic Forming at Elevated Temperature.” Procedia Engineering 81: 2243–48. https://doi.org/10.1016/j.proeng.2014.10.315
• Liu, Hongsheng, Zhongwen Xing, Zhenzhong Sun, and Jun Bao. 2011a. “Adaptive Multiple Scale Meshless Simulation on Springback Analysis in Sheet Metal Forming.” Engineering Analysis with Boundary Elements 35 (3): 436–51. https://doi.org/10.1016/j.enganabound.2010.06.025
• Liu, Jinsong, Jinri Yang, and Yang Xiao. 2016b. “Study on Electric Brake System of Civil Aircraft.” In 2016 IEEE International Conference on Aircraft Utility Systems (AUS). IEEE. https://doi.org/10.1109/aus.2016.7748185
• Liu, Jingyuan, and Kaifeng Zhang. 2014. “Resistance Heating Superplastic Forming and Influence of Current on Deformation Mechanism of TA15 Titanium Alloy.” International Journal of Advanced Manufacturing Technology 76 (9–12): 1673–80. https://doi.org/10.1007/s00170-014-6286-5
• Liu, Wenlin, Boxing Zhao, Xiangning Pan, Zhijie Song, and Ping Wang. 2025d. “Modeling of the Nose Landing Gear Shock Absorber for Carrier-Based Aircraft and Optimization of Oil Orifice Area Configuration.” Fluids 10 (11): 285. https://doi.org/10.3390/fluids10110285
• Liu, Jiawei, Yongkai Zhu, Haitao Wang, Rui Li, Cheng Chen, and Limin Ma. 2026b. “An Integrated FBG Pressure Sensing and Profile Matching Method for Supersonic Inlet Terminal Shock Monitoring.” IEEE Transactions on Instrumentation and Measurement 75: 1–11. https://doi.org/10.1109/tim.2026.3666019
• Liu, Jiawei, Yongkai Zhu, Haitao Wang, Rui Li, Cheng Chen, and Huijun Tan. 2025c. “Measurement of Buzz Flows in a Supersonic Inlet by FBG Sensors.” IEEE Transactions on Instrumentation and Measurement 74: 1–10. https://doi.org/10.1109/tim.2025.3547093
• Liu, Jiawei, Yongkai Zhu, Haitao Wang, et al. 2025b. “Fiber Bragg Grating-Based Sensor for Measuring Supersonic Inlet Terminal Shock at Different Angles of Attack.” Measurement 242: 115985. https://doi.org/10.1016/j.measurement.2024.115985
• Livne, Eli. 1994. “Equivalent Plate Structural Modeling for Wing Shape Optimization Including Transverse Shear.” AIAA Journal 32 (6). https://ntrs.nasa.gov/citations/19990051024
• Livneh, Rafael. 1995a. “Improved Literal Approximation for Lateral-Directional Dynamics of Rigid Aircraft.” Journal of Guidance, Control, and Dynamics 18 (4): 925–27. https://doi.org/10.2514/3.56682
• Löbbe, Christian, and A. Erman Tekkaya. 2018. “Mechanisms for Controlling Springback and Strength in Heat-Assisted Sheet Forming.” CIRP Annals 67 (1): 273–76. https://doi.org/10.1016/j.cirp.2018.04.013
• Loginov, Boris, and Oleg Makeev. 2007. “On Conditions of Flutter Onset for Elongated Plate in Supersonic Gas Flow.” PAMM 7 (1): 1040813–14. https://doi.org/10.1002/pamm.200701023
• Lomax, Harvard, and Max. A. Heaslet. 1956a. “Recent Developments in the Theory of Wing-Body Wave Drag.” Journal of the Aeronautical Sciences 23 (12): 1061–74. https://doi.org/10.2514/8.3731
• Lopatin, N. V. 2012. “Effect of Hot Rolling by Screw Mill on Microstructure of a Ti-6Al-4V Titanium Alloy.” International Journal of Material Forming 6 (4): 459–65. https://doi.org/10.1007/s12289-012-1099-2
• Lottati, I. 1985a. “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. 1985b. “The Role of Damping on Supersonic Panel Flutter.” AIAA Journal 23 (10): 1640–42. https://doi.org/10.2514/3.9141
• 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
• Lowe, James D. 1988. “Calculation of Lift-Curve Slope Using a Wing Tip Biased Vortex Distribution.” Journal of Aircraft 25 (5): 472–73. https://doi.org/10.2514/3.45606
• Lu, Pong-Jeu, and Ling-Tzong Jain. 1998. “Numerical Investigation of Inlet Buzz Flow.” Journal of Propulsion and Power 14 (1): 90–100. https://doi.org/10.2514/2.5254
• Lu, Zipeng, Di Li, Linlin Cao, Hongjian Cui, and Jiachuan Xu. 2023b. “Springback Control in Complex Sheet-Metal Forming Based on Advanced High-Strength Steel.” Coatings 13 (5): 930. https://doi.org/10.3390/coatings13050930
• Lucero, Eddie F. 1985. “Predicting the Supersonic Aerodynamics of Very-Low-Aspect-Ratio Lifting Surfaces.” Journal of Spacecraft and Rockets 22 (2): 119–25. https://doi.org/10.2514/3.25719
• Luckring, James M., Arthur Rizzi, and M. Bruce Davis. 2017. “Toward Improved Predictions of Slender Airframe Aerodynamics Using the F-16XL Aircraft.” Journal of Aircraft 54 (2): 378–87. https://doi.org/10.2514/1.c033433
• Ludloff, H. F., and F. Reiche. 1947. “Linearized Supersonic Flow through Ducts.” Journal of Applied Physics 18 (7): 681–82. https://doi.org/10.1063/1.1697825
• Luo, Shijun, and Yun Bao. 1988. “Computation of Transonic Aerodynamically Compensating Pilot Tube.” Journal of Aircraft 25 (6): 544–47. https://doi.org/10.2514/3.45620
• Luo, Wenguo, Yuqing Wei, Ke Dai, Jianfeng Zhu, and Yancheng You. 2020. “Spatiotemporal Characterization and Suppression Mechanism of Supersonic Inlet Buzz with Proper Orthogonal Decomposition Method.” Energies 13 (1): 217. https://doi.org/10.3390/en13010217
• Lyu, Huitao, Zheng Gong, Yongliang Chen, Wanli Chen, and Wenjian Wang. 2022. “Large-Slenderness-Ratio Supersonic Aircraft Lateral–Directional Coupling Dynamics Analysis and Control.” International Journal of Aerospace Engineering 2022: 1–22. https://doi.org/10.1155/2022/2490675
• Lyubomirov, Yaroslav, and Boris Yartsev. 2015. “Classical Flutter Anisotropic Composite Wing.” In 2015 International Conference on Mechanics - Seventh Polyakhov’s Reading. IEEE. https://doi.org/10.1109/polyakhov.2015.7106750
• Ma, Zhen, and Xiyuan Chen. 2020. “Strain Transfer Characteristics of Surface-Attached FBGs in Aircraft Wing Distributed Deformation Measurement.” Optik 207: 164468. https://doi.org/10.1016/j.ijleo.2020.164468
• Mabey, D. G., and B. L. Welsh. 1987. “Measurements and Calculations of Steady and Oscillatory Pressures on a Low Aspect Ratio Model at Subsonic and Transonic Speeds.” Journal of Fluids and Structures 1 (4): 445–68. https://doi.org/10.1016/s0889-9746(87)90307-0
• “Machining Difficult Materials—Titanium Alloys.” 1965. Vacuum 15 (8): 429. https://doi.org/10.1016/0042-207x(65)90555-5
• “Machining Titanium. II.” 1958. Wear 1 (4): 356. https://doi.org/10.1016/0043-1648(58)90080-2
• Mackay, Douglas S., and Henry T. Nagamatsu. 1954. “Laminar Boundary-Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six.” Journal of the Aeronautical Sciences 21 (1): 65–66. https://doi.org/10.2514/8.2922
• Madelung, G. O. 1978. “Characteristics of Fighter Aircraft.” Journal of Aircraft 15 (3): 129–33. https://doi.org/10.2514/3.58329
• Maeno, Tomoyoshi, Ken-ichiro Mori, and Ryosuke Yachi. 2017. “Hot Stamping of High-Strength Aluminium Alloy Aircraft Parts Using Quick Heating.” CIRP Annals 66 (1): 269–72. https://doi.org/10.1016/j.cirp.2017.04.117
• Maghsoudi, Iman, Mohammad Ali Vaziry, and Mostafa Mahmoodi. 2020. “Experimental Investigation of Flow and Distortion Mitigation by Mechanical Vortex Generators in a Coupled Serpentine Inlet-Turbofan Engine System.” Chinese Journal of Aeronautics 33 (5): 1375–91. https://doi.org/10.1016/j.cja.2019.12.002
• Magnuson, J. 1977. “Repair of Titanium Airframe Castings by Hot Isostatic Pressing.” Metallography 10 (2): 223–32. https://doi.org/10.1016/0026-0800(77)90011-8
• Maikapar, G. I. 1959. “On the Wave Drag of Non Anixymmetric Bodies at Supersonic Speeds.” Journal of Applied Mathematics and Mechanics 23 (2): 528–31. https://doi.org/10.1016/0021-8928(59)90104-2
• Maikapar, G. I. 1966. “A Wing with the Maximum Lift/drag Ratio at Supersonic Velocity.” Journal of Applied Mathematics and Mechanics 30 (1): 227–31. https://doi.org/10.1016/0021-8928(66)90071-2
• 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
• Majumder, Luna, and S. S. Rao. 2007. “Interval Analysis-Based Optimum Design of Wing Structures under Taxiing Loads.” Journal of Aircraft 44 (3): 1045–49. https://doi.org/10.2514/1.28088
• Mal’kov, A. V. 1992. “Fracture Toughness of VT6ch Titanium Alloy.” Strength of Materials 24 (3): 254–58. https://doi.org/10.1007/bf00778386
• Malaek, S. M., and A. Karimi. 2008. “General Approach to Enhance Flying Qualities via Dynamic Balancing of Aircraft Mass.” Journal of Aircraft 45 (1): 130–41. https://doi.org/10.2514/1.29372
• Malan, Paul, and Eugene F. Brown. 1994. “Inlet Drag Prediction for Aircraft Conceptual Design.” Journal of Aircraft 31 (3): 616–22. https://doi.org/10.2514/3.46539
• Malcolm, Gerald N. 1979. “New Rotation-Balance Apparatus for Measuring Airplane Spin Aerodynamics in the Wind Tunnel.” Journal of Aircraft 16 (4): 264–68. https://doi.org/10.2514/3.58515
• 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
• Malone, J. B., L. N. Sankar, and W. A. Sotomayer. 1986. “Unsteady Aerodynamic Modeling of a Fighter Wing in Transonic Flow.” Journal of Aircraft 23 (8): 611–20. https://doi.org/10.2514/3.45352
• Mani, Mori, Ben J. Rider, Anthony J. Sclafani, et al. 2014. “Reynolds-Averaged Navier–Stokes Technology for Transonic Drag Prediction: A Boeing Perspective.” Journal of Aircraft 51 (4): 1118–34. https://doi.org/10.2514/1.c032717
• Mann, Michael J., and Harry W. Carlson. 1994. “Aerodynamic Design of Supersonic Cruise Wings with a Calibrated Linearized Theory.” Journal of Aircraft 31 (1): 35–41. https://doi.org/10.2514/3.46452
• Mannai, Clifford. 1962. “Flight Test Instrumentation.” Journal of the Franklin Institute 274 (5): 403. https://doi.org/10.1016/0016-0032(62)91055-4
• Manneschmidt, W., P. M. Ligrani, M. Sorrell, A. M. Ciccarelli, and B. Weigand. 2024. “Normal Shock Wave Coherence Relative to Other Flow Events with High and Low Levels of Inlet Mach Wave Unsteadiness.” Shock Waves 34 (6): 497–513. https://doi.org/10.1007/s00193-024-01202-4
• Manor, David, and William H. Wentz. 1985. “Flow over Double-Delta Wing and Wing Body at High Alpha.” Journal of Aircraft 22 (1): 78–82. https://doi.org/10.2514/3.45083
• Manshadi, A. D., and F. Saghafi. 2018. “In-Flight Estimation of Time-Varying Aircraft Center of Gravity Position Based on Kinematics Approach.” Journal of Aircraft 55 (5): 2037–49. https://doi.org/10.2514/1.c034973
• Mansour, N. N. 1985. “Computation of the Tip Vortex off a Low-Aspect-Ratio Wing.” AIAA Journal 23 (8): 1143–49. https://doi.org/10.2514/3.9056
• Margalit, S., D. Greenblatt, A. Seifert, and I. Wygnanski. 2005. “Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators.” Journal of Aircraft 42 (3): 698–709. https://doi.org/10.2514/1.6904
• Martin, John C., and Nathan Gerber. 1953c. “The Second-Order Lifting Pressure and Damping in Roll of Sweptback Rolling Airfoils at Supersonic Speeds.” Journal of the Aeronautical Sciences 20 (10): 699–704. https://doi.org/10.2514/8.2798
• Martinez, Rudolph, and Sheila E. Widnall. 1980. “Unified Aerodynamic-Acoustic Theory for a Thin Rectangular Wing Encountering a Gust.” AIAA Journal 18 (6): 636–45. https://doi.org/10.2514/3.7675
• Maruyama, D., K. Matsushima, K. Kusunose, and K. Nakahashi. 2009. “Three-Dimensional Aerodynamic Design of Low-Wave-Drag Supersonic Biplane Using Inverse Problem Method.” Journal of Aircraft 46 (6): 1906–18. https://doi.org/10.2514/1.40313
• Marzocca, Piergiovanni, Liviu Librescu, and Walter A. Silva. 2002. “Flutter, Postflutter, and Control of a Supersonic Wing Section.” Journal of Guidance, Control, and Dynamics 25 (5): 962–70. https://doi.org/10.2514/2.4970
• Mason, William H., and R. Ravi. 1994. “Computational Study of the F-5A Forebody Emphasizing Directional Stability.” Journal of Aircraft 31 (3): 488–94. https://doi.org/10.2514/3.46520
• 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
• Matikas, Theodore E. 2002. “Optimization of the Delta Technique and Application to the Evaluation of Electron-Beam Welded Titanium Aircraft Parts.” Nondestructive Testing and Evaluation 18 (1): 21–35. https://doi.org/10.1080/10589750290026565
• Matsuo, K., and H. -D. Kim. 1993. “Normal Shock Wave Oscillations in Supersonic Diffusers.” Shock Waves 3 (1): 25–33. https://doi.org/10.1007/bf01414745
• Matsushita, H., T. Miyata, M. Kawai, and E. Mosekilde. 2003. “Nonlinear Mathematical Modeling of Aircraft Wing Flutter in Transonic Range.” In 2003 IEEE International Workshop on Workload Characterization (IEEE Cat. No.03EX775). IEEE. https://doi.org/10.1109/phycon.2003.1236814
• May, Pedro, Haitao Li, and Henry T. Yang. 2023. “Inerter-Based Eigenvector Orientation Approach for Passive Control of Supersonic Panel Flutter.” Mathematics 11 (6): 1462. https://doi.org/10.3390/math11061462
• Mayer, David W., and Gerald C. Paynter. 1995. “Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances.” AIAA Journal 33 (2): 266–75. https://doi.org/10.2514/3.12418
• 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
• McCormick, Barnes W. 1959. “The Limiting Circulatory Lift of a Wing of Finite Aspect Ratio.” Journal of the Aerospace Sciences 26 (4): 247–48. https://doi.org/10.2514/8.8022
• McCutchen, Charles W. 2006. “Comment on ‘Low-Aspect-Ratio Wing Aerodynamics at Low Reynolds Numbers’.” AIAA Journal 44 (4): 924–924. https://doi.org/10.2514/1.12330
• McDarmaid, D. S. 1985. “Superplastic Forming and Post-Forming Tensile Properties of High Strength Titanium Alloy Ti-4Al-4Mo-2Sn-0.5Si.” Materials Science and Engineering 70: 123–29. https://doi.org/10.1016/0025-5416(85)90273-3
• McDonough, Kevin, and Ilya Kolmanovsky. 2017. “Fast Computable Recoverable Sets and Their Use for Aircraft Loss-of-Control Handling.” Journal of Guidance, Control, and Dynamics 40 (4): 934–47. https://doi.org/10.2514/1.g001747
• McGrath, Brian E. 1995. “Computational Study of a Conical Unit Aspect Ratio Wing at Supersonic Speeds.” Journal of Aircraft 32 (4): 877–80. https://doi.org/10.2514/3.46805
• McHugh, Kevin A., Maxim Freydin, Kai Kruger Bastos, Philip Beran, and Earl H. Dowell. 2021. “Flutter and Limit Cycle Oscillations of Cantilevered Plate in Supersonic Flow.” Journal of Aircraft 58 (2): 266–78. https://doi.org/10.2514/1.c035992
• McLAFFERTY, George. 1953. “Theoretical Pressure Recovery through a Normal Shock in a Duct with Initial Boundary Layer.” Journal of the Aeronautical Sciences 20 (3): 169–74. https://doi.org/10.2514/8.2582
• Mei, Guanhua, Jiazhong Zhang, and Can Kang. 2017. “Analysis of Curved Panel Flutter in Supersonic and Transonic Airflows Using a Fluid–Structure Coupling Algorithm.” Journal of Vibration and Acoustics 139 (4): 041004. https://doi.org/10.1115/1.4036103
• Mei, Guanhua, Jiazhong Zhang, Guang Xi, Xu Sun, and Jiahui Chen. 2014. “Analysis of Supersonic and Transonic Panel Flutter Using a Fluid-Structure Coupling Algorithm.” Journal of Vibration and Acoustics 136 (3): 031013. https://doi.org/10.1115/1.4027135
• Meinicke, Ana C., and Carlos E. S. Cesnik. 2026. “Temperature–Strain Sensor Selection and Dimensionality Reduction for High-Speed Aerodynamic Recovery.” Journal of Aircraft: 1–9. https://doi.org/10.2514/1.c038844
• 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
• Menon, Padmanabhan K., Prasenjit Sengupta, Sai Vaddi, Bong-Jun Yang, and Jason Kwan. 2013. “Impaired Aircraft Performance Envelope Estimation.” Journal of Aircraft 50 (2): 410–24. https://doi.org/10.2514/1.c031847
• Merkli, Peter E. 1976. “Pressure Recovery in Rectangular Constant Area Supersonic Diffusers.” AIAA Journal 14 (2): 168–72. https://doi.org/10.2514/3.61352
• Metcalf, Arthur G. B. 1936. “Airplane Longitudinal Stability: A Resume.” Journal of the Aeronautical Sciences 4 (2): 61–69. https://doi.org/10.2514/8.322
• “Method for Forming Titanium Aluminide-Ductile Titanium Aluminium Alloy Matrix Alloy Composites.” 1991. Composites 22 (5): 414. https://doi.org/10.1016/0010-4361(91)90657-3
• Micari, F., A. Forcellese, L. Fratini, F. Gabrielli, and N. Alberti. 1997. “Springback Evaluation in Fully 3-D Sheet Metal Forming Processes.” CIRP Annals 46 (1): 167–70. https://doi.org/10.1016/s0007-8506(07)60800-2
• Micks, W. R. 1950. “Effect of Torsional Stiffness Requirements on Wing Structural Weight.” Journal of the Aeronautical Sciences 17 (11): 736–40. https://doi.org/10.2514/8.1784
• Miele, Angelo, and John N. Damoulakis. 1969. “Maximum Lift-to-Drag Ratio Airfoils at Moderate Supersonic Speeds.” AIAA Journal 7 (3): 471–77. https://doi.org/10.2514/3.5131
• Miklosovic, David, Robin Imber, and Michael Britt-Crane. 2016. “Measurements of Midspan Flow Interactions of a Low-Aspect-Ratio Circulation Control Wing.” Journal of Aircraft 53 (6): 1969–74. https://doi.org/10.2514/1.c033852
• Miles, John W. 1947. “The Aerodynamic Forces on an Oscillating Airfoil at Supersonic Speeds.” Journal of the Aeronautical Sciences 14 (6): 351–58. https://doi.org/10.2514/8.1374
• Miles, John W. 1952. “On the General Solution for Unsteady Motion of a Rectangular Wing in Supersonic Flow.” Journal of the Aeronautical Sciences 19 (6): 421–22. https://doi.org/10.2514/8.2313
• Miles, John W. 1962. “Remarks on ‘Supersonic Panel Flutter of a Cylindrical Shell of Finite Length’.” Journal of the Aerospace Sciences 29 (1): 115–16. https://doi.org/10.2514/8.9330
• Miller, M. S., and J. E. Burkhalter. 1987. “Wing-Wing Interference Effects for Cruciform Missiles.” Journal of Aircraft 24 (3): 211–17. https://doi.org/10.2514/3.45418
• Miller, George E., and James A. Franklin. 1968. “Lateral-Directional Flying Qualities for Power Approach.” Journal of Aircraft 5 (2): 126–34. https://doi.org/10.2514/3.43919
• Ming-de, Dong. 1984. “Eigenvalue Problem for Integro-Differential Equation of Supersonic Panel, Flutter.” Applied Mathematics and Mechanics 5 (1): 1029–40. https://doi.org/10.1007/bf01875890
• Minkler, Lyle F. 1975. “Measuring the Moment of Inertia of an Airplane.” Physics Teacher 13 (1): 46–47. https://doi.org/10.1119/1.2339063
• Mitchell, David G., and Roger H. Hoh. 1984. “Influence of Roll Command Augmentation Systems on Flying Qualities of Fighter Aircraft.” Journal of Guidance, Control, and Dynamics 7 (1): 99–105. https://doi.org/10.2514/3.8551
• Mithu, M. A. H., Mohammed. A. Karim, Ferdous A. Taj, and Abdur Rahman. 2025. “Predicting Springback in V-Bending: Effects of Load, Load Holding Time, and Heat Treatment on Common Sheet-Metal Forming Operations.” Materials Today Communications 43: 111668. https://doi.org/10.1016/j.mtcomm.2025.111668
• Modi, Anirudh, and N. Ananthkrishnan. 1998. “Multiple Attractors in Inertia-Coupled Velocity-Vector Roll Maneuvers of Airplanes.” Journal of Aircraft 35 (4): 659–61. https://doi.org/10.2514/2.2354
• Mohamed, Mohamed A., Imran Afgan, Mohamed Hefny Salim, and Ibrahim K. Mohamed. 2022. “Low Speed Aerodynamic Characteristics of Non-Slender Delta Wing at Low Angles of Attack.” Alexandria Engineering Journal 61 (12): 9427–35. https://doi.org/10.1016/j.aej.2022.03.003
• Mohammed, Mortda, Maher K. Taher, and Saleh Khudhair. 2022. “Prediction of Turbojet Performance by Using Artificial Neural Network.” Materials Today: Proceedings 60: 1513–22. https://doi.org/10.1016/j.matpr.2021.12.027
• Mohandas, T., D. Banerjee, and V. V. Kutumbarao. 1999. “Elevated Temperature Properties of Electron Beam Welds of an α+β Titanium Alloy.” Materials Science and Engineering: A 269 (1–2): 217–24. https://doi.org/10.1016/s0921-5093(99)00172-0
• Moiseev, V. N. 2000. “High-Strength Titanium Alloys for Large Parts of Aircraft Engines.” Metal Science and Heat Treatment 42 (2): 81–83. https://doi.org/10.1007/bf02469872
• Moosavi, Reza. 2025. “Smart Wing Stall Flutter Alleviation.” AIAA Journal 63 (12): 5201–25. https://doi.org/10.2514/1.j065155
• Moosavi, Reza, and Faris Elasha. 2022. “Smart Wing Flutter Suppression.” Designs 6 (2): 29. https://doi.org/10.3390/designs6020029
• Moosavi, M. R., A. R. Naddaf Oskouei, and A. Khelil. 2005. “Flutter of Subsonic Wing.” Thin-Walled Structures 43 (4): 617–27. https://doi.org/10.1016/j.tws.2004.10.001
• Moreira, Marco A. G., Juliano A. B. Gripp, Takashi Yoneyama, and Cleverson M. P. Marinho. 2022. “Longitudinal Flight Control Law Design with Integrated Envelope Protection.” Journal of Guidance, Control, and Dynamics 45 (9): 1739–49. https://doi.org/10.2514/1.g006443
• Morelli, Eugene A. 2022. “Determining Aircraft Moments of Inertia from Flight Test Data.” Journal of Guidance, Control, and Dynamics 45 (1): 4–14. https://doi.org/10.2514/1.g006072
• Morestin, F., M. Boivin, and C. Silva. 1996. “Elasto Plastic Formulation Using a Kinematic Hardening Model for Springback Analysis in Sheet Metal Forming.” Journal of Materials Processing Technology 56 (1–4): 619–30. https://doi.org/10.1016/0924-0136(95)01876-x
• Morikawa, George. 1951. “Supersonic Wing-Body Lift.” Journal of the Aeronautical Sciences 18 (4): 217–28. https://doi.org/10.2514/8.1915
• Morino, Hiroyuki, and Shigeru Obayashi. 2015. “Nonlinear Aeroelastic Analysis of Control Surface with Freeplay Using Computational-Fluid-Dynamics-Based Reduced-Order Models.” Journal of Aircraft 52 (2): 569–83. https://doi.org/10.2514/1.c032775
• Morote, J., and G. Liaño. 2012. “Triform Wing-Body Loading.” Journal of Aircraft 49 (5): 1507–12. https://doi.org/10.2514/1.c031802
• Morris, Robert D. 1964. “Parameter Selection for in-Flight Recording.” Journal of Aircraft 1 (5): 300–303. https://doi.org/10.2514/3.43597
• Mosleh, A. O., A. V. Mikhaylovskaya, A. D. Kotov, and J. S. Kwame. 2019. “Experimental, Modelling and Simulation of an Approach for Optimizing the Superplastic Forming of Ti-6%Al-4%V Titanium Alloy.” Journal of Manufacturing Processes 45: 262–72. https://doi.org/10.1016/j.jmapro.2019.06.033
• Mount, Joseph S. 1965. “Effect of Inlet Additive Drag on Aircraft Performance.” Journal of Aircraft 2 (5): 374–78. https://doi.org/10.2514/3.43670
• Mouton, Sylvain. 2021. “Simulation of Atmospheric Boundary Layer for Air Inlet Testing in Crossflow.” AIAA Journal 59 (7): 2603–12. https://doi.org/10.2514/1.j059940
• Mrad, Hatem, Mohamed Bouazara, and Gholamreza Aryanpour. 2013. “A Reliability Study of Springback on the Sheet Metal Forming Process under Probabilistic Variation of Prestrain and Blank Holder Force.” Acta Mechanica Sinica 29 (4): 557–66. https://doi.org/10.1007/s10409-013-0036-z
• Mulidrán, Peter, Emil Spišák, Miroslav Tomáš, and Janka Majerníková. 2026. “Springback Prediction in Sheet-Metal Bending Based on Finite Element Method and Artificial Neural Network with Shapley Additive Explanations Method.” Metals 16 (8): 880. https://doi.org/10.3390/met16080880
• 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
• Munk, M. M. 1950. “The Reversal Theorem of Linearized Supersonic Airfoil Theory.” Journal of Applied Physics 21 (2): 159–61. https://doi.org/10.1063/1.1699616
• 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
• Murthy, H. Sundara. 1981. “A Sensitive Rolling Moment Balance for Use in Supersonic Blowdown Tunnels.” Journal of Aircraft 18 (9): 799–800. https://doi.org/10.2514/3.44735
• Murzinova, M. A. 2008. “Application of Thermohydrogen Treatment for Enhancement of the High-Temperature Strength of VT9 Titanium Alloy.” Materials Science 44 (3): 380–86. https://doi.org/10.1007/s11003-008-9082-2
• Mwenegoha, Hery, Terry Moore, James Pinchin, and Mark Jabbal. 2019. “Model-Based Autonomous Navigation with Moment of Inertia Estimation for Unmanned Aerial Vehicles.” Sensors 19 (11): 2467. https://doi.org/10.3390/s19112467
• Mysliwetz, F. 1963. “Supersonic Interference Lift.” AIAA Journal 1 (6): 1432–34. https://doi.org/10.2514/3.1821
• Nabhani, Farhad. 2001. “Machining of Aerospace Titanium Alloys.” Robotics and Computer-Integrated Manufacturing 17 (1–2): 99–106. https://doi.org/10.1016/s0736-5845(00)00042-9
• Naceur, H., Y. Q. Guo, and S. Ben-Elechi. 2006. “Response Surface Methodology for Design of Sheet Forming Parameters to Control Springback Effects.” Computers & Structures 84 (26–27): 1651–63. https://doi.org/10.1016/j.compstruc.2006.04.005
• Nagaraja, K. S., G. C. Lakin, and J. B. Hartley. 1982. “Flutter and Oscillatory Pressure Tests on a 727 Aileron in a Wind Tunnel.” Journal of Aircraft 19 (9): 781–86. https://doi.org/10.2514/3.61555
• Nakai, Eiichi, Toshiro Takagi, and Koji Isogai. 1967b. “Results of Supersonic Flutter Characteristics of Low Aspect-Ratio Flat-Plate Surfaces.” AIAA Journal 5 (9): 1715–17. https://doi.org/10.2514/3.4290
• Nam, Changho, Aditi Chattopadhyay, and Youdan Kim. 2000. “Optimal Wing Planform Design for Aeroelastic Control.” AIAA Journal 38 (8): 1465–70. https://doi.org/10.2514/2.1123
• Nanda, Soumya Ranjan, Siddesh Desai, Vinayak Kulkarni, and Niranjan Sahoo. 2022. “Amalgamation of Stress Wave Force Balance with Artificial Intelligence: An Alternative Way of Drag Force Measurement in Supersonic Flows.” Aerospace Science and Technology 123: 107481. https://doi.org/10.1016/j.ast.2022.107481
• Nanu, N., and G. Brabie. 2012. “Analytical Model for Prediction of Springback Parameters in the Case of U Stretch–bending Process as a Function of Stresses Distribution in the Sheet Thickness.” International Journal of Mechanical Sciences 64 (1): 11–21. https://doi.org/10.1016/j.ijmecsci.2012.08.007
• Narasimhan, Narkeeran, and Michael Lovell. 1999. “Predicting Springback in Sheet Metal Forming: An Explicit to Implicit Sequential Solution Procedure.” Finite Elements in Analysis and Design 33 (1): 29–42. https://doi.org/10.1016/s0168-874x(99)00009-8
• Narayanasamy, R., and P. Padmanabhan. 2010. “Comparison of Regression and Artificial Neural Network Model for the Prediction of Springback during Air Bending Process of Interstitial Free Steel Sheet.” Journal of Intelligent Manufacturing 23 (3): 357–64. https://doi.org/10.1007/s10845-009-0375-6
• Nasrollahi, V., and B. Arezoo. 2012. “Prediction of Springback in Sheet Metal Components with Holes on the Bending Area, Using Experiments, Finite Element and Neural Networks.” Materials & Design (1980-2015) 36: 331–36. https://doi.org/10.1016/j.matdes.2011.11.039
• Navaratna, Punsara D. B., Mark H. Lowenberg, Simon A. Neild, and Mikhail Goman. 2022. “Self-Induced Roll–Yaw Oscillations of an Aircraft Model in a Wind Tunnel.” Journal of Aircraft 59 (1): 3–14. https://doi.org/10.2514/1.c036157
• Nawaya, Tarik, Axel von Hehl, Sabine Wagner, and Werner Beck. 2018. “Hot Deep Drawing Processing of Titanium Sheet Metal Parts for High Temperature Applications.” Advanced Engineering Materials 21 (4): 1800544. https://doi.org/10.1002/adem.201800544
• Naylor, Derek. 1957. “The Aerodynamic Action of Triangular Horn-Balanced Control Surfaces on the Supersonic Delta Wing.” Journal of the Aeronautical Sciences 24 (8): 574–78. https://doi.org/10.2514/8.3909
• Nelson, H. F. 1989. “Wing-Body Interference Lift for Supersonic Missiles with Elliptical Cross-Section Fuselages.” Journal of Spacecraft and Rockets 26 (5): 322–29. https://doi.org/10.2514/3.26075
• Nelson, H. F., and Brent W. Bossi. 1995. “Predictions of Low Aspect Ratio Missile Aerodynamics.” Journal of Spacecraft and Rockets 32 (4): 596–600. https://doi.org/10.2514/3.26658
• 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
• Neto, D. M., M. C. Oliveira, A. D. Santos, J. L. Alves, and L. F. Menezes. 2017. “Influence of Boundary Conditions on the Prediction of Springback and Wrinkling in Sheet Metal Forming.” International Journal of Mechanical Sciences 122: 244–54. https://doi.org/10.1016/j.ijmecsci.2017.01.037
• Neumark, S. 1952. “Pressure Distribution on an Airfoil in Nonuniform Motion.” Journal of the Aeronautical Sciences 19 (3): 214–15. https://doi.org/10.2514/8.2219
• Nguyen, Duc H., Mark H. Lowenberg, and Simon A. Neild. 2021. “Frequency-Domain Bifurcation Analysis of a Nonlinear Flight Dynamics Model.” Journal of Guidance, Control, and Dynamics 44 (1): 138–50. https://doi.org/10.2514/1.g005197
• Ni, Peng. 2022. “Strength Analysis of Shock Strut of Aircraft Landing Gear Based on ANSYS.” In 2022 IEEE 10th Conference on Systems, Process & Control (ICSPC). IEEE. https://doi.org/10.1109/icspc55597.2022.10001784
• Nicolas, Matthew, Rani Sullivan, and W. Richards. 2016. “Large Scale Applications Using FBG Sensors: Determination of in-Flight Loads and Shape of a Composite Aircraft Wing.” Aerospace 3 (3): 18. https://doi.org/10.3390/aerospace3030018
• Nicolosi, Fabrizio, Agostino De Marco, Vito Sabetta, and Pierluigi Della Vecchia. 2018. “Roll Performance Assessment of a Light Aircraft: Flight Simulations and Flight Tests.” Aerospace Science and Technology 76: 471–83. https://doi.org/10.1016/j.ast.2018.01.041
• Niculescu, Nicolae-Alin, Jenica-Ileana Corcau, and Gavril Alexandru. 2021. “Integrated System for Monitoring Aircraft Structural Condition by Using the Strain Gauge Marks Method.” In 2021 International Conference on Applied and Theoretical Electricity (ICATE). IEEE. https://doi.org/10.1109/icate49685.2021.9465010
• Nikhare, Chetan P., Nitin Kotkunde, and Swadesh Kumar Singh. 2021. “Effect of Material Discontinuity on Springback in Sheet Metal Bending.” Advances in Materials and Processing Technologies 8 (sup3): 1800–1819. https://doi.org/10.1080/2374068x.2021.1953925
• Nikitenko, A. F. 1976. “Cyclic Creep of a Titanium Alloy.” Strength of Materials 8 (8): 925–27. https://doi.org/10.1007/bf01529801
• Nikoueeyan, Pourya, and Jonathan W. Naughton. 2023. “Analysis of the Unsteady Surface Pressure Distribution of a Pitching Airfoil Using Modal Decomposition.” Experiments in Fluids 64 (5): 100. https://doi.org/10.1007/s00348-023-03644-5
• Norris, Richard H., Ashok Saxena, and Jill Tucker. 1999. “Elevated Temperature Deformation and Crack Growth Behavior in Titanium Alloy 6-2222.” Engineering Fracture Mechanics 62 (1): 79–93. https://doi.org/10.1016/s0013-7944(98)00086-1
• 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
• O’Donnell, Richard, and Kamran Mohseni. 2019. “Roll Control of Low-Aspect-Ratio Wings Using Articulated Winglet Control Surfaces.” Journal of Aircraft 56 (2): 419–30. https://doi.org/10.2514/1.c034704
• Oberkampf, William L. 1975. “Prediction of Roll Moments on Finned Bodies in Supersonic Flow.” Journal of Spacecraft and Rockets 12 (1): 17–21. https://doi.org/10.2514/3.56947
• Oh, Jong Y., Fuhua Ma, Shih-Yang Hsieh, and Vigor Yang. 2005. “Interactions between Shock and Acoustic Waves in a Supersonic Inlet Diffuser.” Journal of Propulsion and Power 21 (3): 486–95. https://doi.org/10.2514/1.9671
• Olsen, Michael E., and H. Lee Seegmiller. 1993. “Low Aspect Ratio Wing Code Validation Experiment.” AIAA Journal 31 (10): 1744–52. https://doi.org/10.2514/3.49105
• Omran, Ashraf, and Brett Newman. 2009. “Piecewise Global Volterra Nonlinear Modeling and Characterization for Aircraft Dynamics.” Journal of Guidance, Control, and Dynamics 32 (3): 749–59. https://doi.org/10.2514/1.40655
• Ortiz, Mikel, Mariluz Penalva, Edurne Iriondo, and Luis Norberto López de Lacalle. 2019. “Accuracy and Surface Quality Improvements in the Manufacturing of Ti-6Al-4V Parts Using Hot Single Point Incremental Forming.” Metals 9 (6): 697. https://doi.org/10.3390/met9060697
• Oruc, Ridvan, and Tolga Baklacioglu. 2022. “Modeling of Aircraft Performance Parameters with Metaheuristic Methods to Achieve Specific Excess Power Contours Using Energy Maneuverability Method.” Energy 259: 125069. https://doi.org/10.1016/j.energy.2022.125069
• Oruc, Ridvan, and Tolga Baklacioglu. 2023. “Modeling of Energy Maneuverability Based Specific Excess Power Contours for Commercial Aircraft Using Metaheuristic Methods.” Energy 269: 126819. https://doi.org/10.1016/j.energy.2023.126819
• Osborne, Colin. 1973. “Unsteady Thin-Airfoil Theory for Subsonic Flow.” AIAA Journal 11 (2): 205–9. https://doi.org/10.2514/3.6730
• Osmon, R. V. 1968. “Improved Methods of Spillage Drag Prediction for Two-Dimensional Inlets.” Journal of Aircraft 5 (3): 254–60. https://doi.org/10.2514/3.43935
• Otiefy, Ramadan A. H., and Hani M. Negm. 2011. “Wing Box Transonic-Flutter Suppression Using Piezoelectric Self-Sensing Diagonal-Link Actuators.” International Journal of Solids and Structures 48 (1): 31–43. https://doi.org/10.1016/j.ijsolstr.2010.09.005
• Owens, D. B., Francis J. Capone, Robert M. Hall, Jay M. Brandon, and Joseph R. Chambers. 2004. “Transonic Free-to-Roll Analysis of Abrupt Wing Stall on Military Aircraft.” Journal of Aircraft 41 (3): 474–84. https://doi.org/10.2514/1.3073
• Owens, D. Bruce, Jeffrey K. McConnell, Jay M. Brandon, and Robert M. Hall. 2006. “Transonic Free-To-Roll Analysis of the F-35 (Joint Strike Fighter) Aircraft.” Journal of Aircraft 43 (3): 608–15. https://doi.org/10.2514/1.16972
• Owens, Lewis R., Richard A. Wahls, Michael B. Elzey, and Marvine P. Hamner. 2007. “Reynolds Number Effects on off-Design Stability and Control Characteristics of Supersonic Transports.” Journal of Aircraft 44 (1): 134–43. https://doi.org/10.2514/1.22519
• Ozturk, Fahrettin, Remzi Ecmel Ece, Naki Polat, and Arif Koksal. 2010. “Effect of Warm Temperature on Springback Compensation of Titanium Sheet.” Materials and Manufacturing Processes 25 (9): 1021–24. https://doi.org/10.1080/10426914.2010.492056
• Padovan, Joe, Amir Kazempour, and Yong Hee Kim. 1991. “Aircraft Landing-Induced Tire Spinup.” Journal of Aircraft 28 (12): 849–54. https://doi.org/10.2514/3.46108
• Pan, Bing, Dafang Wu, and Yong Xia. 2010. “High-Temperature Deformation Field Measurement by Combining Transient Aerodynamic Heating Simulation System and Reliability-Guided Digital Image Correlation.” Optics and Lasers in Engineering 48 (9): 841–48. https://doi.org/10.1016/j.optlaseng.2010.04.007
• Panthi, S. K., N. Ramakrishnan, Meraj Ahmed, Shambhavi S. Singh, and M. D. Goel. 2010. “Finite Element Analysis of Sheet Metal Bending Process to Predict the Springback.” Materials & Design 31 (2): 657–62. https://doi.org/10.1016/j.matdes.2009.08.022
• Panthi, S. K., N. Ramakrishnan, R. Das Gupta, and J. S. Chouhan. 2008. “Study of Effect of Load on Springback in Sheet Metal Bending.” Transactions of the Indian Institute of Metals 61 (1): 39–43. https://doi.org/10.1007/s12666-008-0063-9
• Panthi, S. K., N. Ramakrishnan, K. K. Pathak, and J. S. Chouhan. 2007. “An Analysis of Springback in Sheet Metal Bending Using Finite Element Method (FEM).” Journal of Materials Processing Technology 186 (1–3): 120–24. https://doi.org/10.1016/j.jmatprotec.2006.12.026
• Papadopoulos, J. G. 1958. “Aeroelastic Solution for a Wing Plan Form with a Tip Control Surface.” Journal of the Aerospace Sciences 25 (11): 726–27. https://doi.org/10.2514/8.7862
• Papeleux, Luc, and Jean-Philippe Ponthot. 2002. “Finite Element Simulation of Springback in Sheet Metal Forming.” Journal of Materials Processing Technology 125-126: 785–91. https://doi.org/10.1016/s0924-0136(02)00393-x
• 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
• Parker, Mark J., Benjamin Jentz, Nolan Dyck, and Anthony G. Straatman. 2022. “On the Measurement of Temperature and Recovery Factor in High-Speed Subsonic Duct Flow.” Flow Measurement and Instrumentation 83: 102090. https://doi.org/10.1016/j.flowmeasinst.2021.102090
• Patel, Sanjay Kumar, Radha Krishna Lal, J. P. Dwivedi, and V. P. Singh. 2013. “Springback Analysis in Sheet Metal Forming Using Modified Ludwik Stress-Strain Relation.” ISRN Mechanical Engineering 2013: 1–11. https://doi.org/10.1155/2013/640958
• Patel, Kailen, and Demetrios Lefas. 2026. “Role of Shocks in Transonic Bending-Torsion Flutter.” Journal of Aircraft 63 (3): 921–33. https://doi.org/10.2514/1.c038444
• Patel, Vivek, Vimal Savsani, and Anurag Mudgal. 2018. “Efficiency, Thrust, and Fuel Consumption Optimization of a Subsonic/sonic Turbojet Engine.” Energy 144: 992–1002. https://doi.org/10.1016/j.energy.2017.12.080
• Patel, Jay, Drithi Shetty, Ritika Menghani, and Sachin Barve. 2017. “Optimization of an Oleo-Pneumatic Shock Absorber for Main Landing Gear of a Commercial Aircraft.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.3101400
• Pattinson, J., M. H. Lowenberg, and M. G. Goman. 2013. “Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification.” Journal of Aircraft 50 (2): 551–66. https://doi.org/10.2514/1.c031924
• Paul, Eldho, Geesara Kulathunga, Hariharan Krishnaswamy, and Alexandr Klimchik. 2025. “Springback Estimation in Incremental Sheet Metal Forming Using the Gaussian Process Regression Model.” Manufacturing Letters 44: 1378–86. https://doi.org/10.1016/j.mfglet.2025.06.157
• Paynter, Gerald C., and David W. Mayer. 1995. “Evaluating the Temporal Accuracy of Inlet Normal Shock Propagation Simulations.” AIAA Journal 33 (8): 1534–36. https://doi.org/10.2514/3.12925
• Paynter, Gerald C., David A. Treiber, and W. David Kneeling. 1993b. “Modeling Supersonic Inlet Boundary-Layer Bleed Roughness.” Journal of Propulsion and Power 9 (4): 622–27. https://doi.org/10.2514/3.23666
• Peake, N. 1997. “The Scattering of Vorticity Waves by a Supersonic Rectangular Wing.” Wave Motion 25 (4): 369–83. https://doi.org/10.1016/s0165-2125(97)00005-x
• Pechloff, Alexander, and Boris Laschka. 2010. “Small Disturbance Navier-Stokes Computations for Low-Aspect-Ratio Wing Pitching Oscillations.” Journal of Aircraft 47 (3): 737–53. https://doi.org/10.2514/1.45233
• Pechuzal, G., and J. Kevorkian. 1977. “Supersonic-Transonic Flow Generated by a Thin Airfoil in a Stratified Atmosphere.” SIAM Journal on Applied Mathematics 33 (1): 8–33. https://doi.org/10.1137/0133002
• Pecora, Rosario. 2021. “A Rational Numerical Method for Simulation of Drop-Impact Dynamics of Oleo-Pneumatic Landing Gear.” Applied Sciences 11 (9): 4136. https://doi.org/10.3390/app11094136
• Pedreiro, Nelson, Stephen M. Rock, Zeki Z. Celik, and Leonard Roberts. 1998. “Roll-Yaw Control at High Angle of Attack by Forebody Tangential Blowing.” Journal of Aircraft 35 (1): 69–77. https://doi.org/10.2514/2.2261
• Pedreiro, Nelson, Yuji Takahara, and Stephen M. Rock. 1999. “Aileron Effectiveness at High Angles of Attack: Interaction with Forebody Blowing.” Journal of Aircraft 36 (6): 981–86. https://doi.org/10.2514/2.2539
• Pelletier, Alain, and Thomas J. Mueller. 2000. “Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings.” Journal of Aircraft 37 (5): 825–32. https://doi.org/10.2514/2.2676
• Peng, Hang, Bintuan Wang, Yu Ning, Shancheng Cao, and Mabao Liu. 2024. “Strain Gauge Location Optimization for Operational Load Monitoring of an Aircraft Wing Using an Improved Correlation Measure.” Applied Sciences 14 (19): 9078. https://doi.org/10.3390/app14199078
• Pereira, Diogo, Frederico Afonso, and Fernando Lau. 2025. “End-to-End Deep-Learning-Based Surrogate Modeling for Supersonic Airfoil Shape Optimization.” Aerospace 12 (5): 389. https://doi.org/10.3390/aerospace12050389
• Persoon, A. J., J. J. Horsten, and J. J. Meijer. 1984. “Measurement of Transonic Dips in the Flutter Boundaries of a Supercritical Wing in a Wind Tunnel.” Journal of Aircraft 21 (11): 906–12. https://doi.org/10.2514/3.45061
• Petre, Augustin, and Holt Ashley. 1976. “Drag Effects on Wing Flutter.” Journal of Aircraft 13 (10): 755–63. https://doi.org/10.2514/3.58707
• Pettit, Chris L., and Ramana V. Grandhi. 2003. “Optimization of a Wing Structure for Gust Response and Aileron Effectiveness.” Journal of Aircraft 40 (6): 1185–91. https://doi.org/10.2514/2.7208
• Pfenneberger, F. X. 1967. “Experimental Control-Wing Hinge Moments of a Transonic-Supersonic, Rolling, Maneuvering, Guided Missile.” Journal of Spacecraft and Rockets 4 (7): 925–28. https://doi.org/10.2514/3.28989
• Phillips, W. F. 2000b. “Improved Closed-Form Approximation for Dutch Roll.” Journal of Aircraft 37 (3): 484–90. https://doi.org/10.2514/2.2623
• Phillips, W. F. 2014. “Analytical Decomposition of Wing Roll and Flapping Using Lifting-Line Theory.” Journal of Aircraft 51 (3): 761–78. https://doi.org/10.2514/1.c032399
• Phillips, W. F., and E. A. Anderson. 2002. “Analytical Approximation for the Mechanics of Airplane Spin.” Journal of Aircraft 39 (6): 1084–88. https://doi.org/10.2514/2.3041
• Phillips, W. F., and B. W. Santana. 2002. “Aircraft Small-Disturbance Theory with Longitudinal-Lateral Coupling.” Journal of Aircraft 39 (6): 973–80. https://doi.org/10.2514/2.3050
• Pi, W. S. 1988. “Dynamic Tire/soil Contact Surface Interaction Model for Aircraft Ground Operations.” Journal of Aircraft 25 (11): 1038–44. https://doi.org/10.2514/3.45700
• Pilchak, A. L., W. J. Porter, and R. John. 2012. “Room Temperature Fracture Processes of a near-α Titanium Alloy Following Elevated Temperature Exposure.” Journal of Materials Science 47 (20): 7235–53. https://doi.org/10.1007/s10853-012-6673-y
• Pindzola, Michael. 1950. “Supersonic Tests of Conventional Control Surfaces on a Double-Wedge Airfoil.” Journal of the Aeronautical Sciences 17 (4): 204–10. https://doi.org/10.2514/8.1593
• Pines, Samuel, John Dugundji, and Joseph Neuringer. 1955. “Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic Edges.” Journal of the Aeronautical Sciences 22 (10): 693–700. https://doi.org/10.2514/8.3436
• Pinsky, Mark A., and Bill Essary. 1993. “Analysis and Resonance Stabilization of Bifurcation Phenomena in Aircraft Flight.” In 1993 American Control Conference. IEEE. https://doi.org/10.23919/acc.1993.4792884
• Pinsky, Mark A., and Bill Essary. 1994. “Analysis and Control of Bifurcation Phenomena in Aircraft Flight.” Journal of Guidance, Control, and Dynamics 17 (3): 591–98. https://doi.org/10.2514/3.21238
• Pitt, Franna, and M. Ramulu. 2004. “Influence of Grain Size and Microstructure on Oxidation Rates in Titanium Alloy Ti-6Al-4V under Superplastic Forming Conditions.” Journal of Materials Engineering and Performance 13 (6): 727–34. https://doi.org/10.1361/10599490421394
• Pitt, F., M. Ramulu, P. Labossiere, and S. Young. 2004. “Postprocessing Effect on the Ductility and Flexural Behavior of Three Titanium Alloys under Simulated Superplastic Forming Conditions.” Journal of Materials Engineering and Performance 13 (6): 735–43. https://doi.org/10.1361/10599490421565
• Pittman, James L. 1987a. “Experimental Flowfield Visualization of a High Alpha Wing at Mach 1.62.” Journal of Aircraft 24 (5): 335–41. https://doi.org/10.2514/3.45450
• Pittman, James L. 1987b. “Supersonic Airfoil Optimization.” Journal of Aircraft 24 (12): 873–79. https://doi.org/10.2514/3.45532
• Plotkin, A. 1990. “Comment on ‘Improved Thin-Airfoil Theory’.” Journal of Aircraft 27 (5): 478–79. https://doi.org/10.2514/3.25307
• Policandriotes, T., and P. Filip. 2011. “Effects of Selected Nanoadditives on the Friction and Wear Performance of Carbon–carbon Aircraft Brake Composites.” Wear 271 (9–10): 2280–89. https://doi.org/10.1016/j.wear.2011.01.093
• Poolperm, Pattarawadee, Wasawat Nakkiew, and Nirut Naksuk. 2021. “Experimental Investigation of Additive Manufacturing Using a Hot-Wire Plasma Welding Process on Titanium Parts.” Materials 14 (5): 1270. https://doi.org/10.3390/ma14051270
• Pop, Alina Bianca, Sandor Ravai-Nagy, Aurel Mihail Titu, Nicolae Medan, and Andrei Catalin Filip. 2025. “Recent Contributions to the Development of Barrel End-Mill Machining Technologies for Titanium Alloys in the Aerospace Context.” Aerospace 12 (1): 55. https://doi.org/10.3390/aerospace12010055
• Pornputsiri, Natthasak, and Kannachai Kanlayasiri. 2020. “Effect of Bending Temperatures on the Microstructure and Springback of a TRIP Steel Sheet.” Defence Technology 16 (5): 980–87. https://doi.org/10.1016/j.dt.2019.11.018
• Postel, E. E., and E. L. Leppert. 1948. “Theoretical Pressure Distributions for a Thin Airfoil Oscillating in Incompressible Flow.” Journal of the Aeronautical Sciences 15 (8): 486–92. https://doi.org/10.2514/8.11625
• Pourboghrat, Farhang, and Edmund Chu. 1995. “Springback in Plane Strain Stretch/draw Sheet Forming.” International Journal of Mechanical Sciences 37 (3): 327–41. https://doi.org/10.1016/0020-7403(95)93523-9
• Pourtakdoust, S. H., and S. A. Fazelzadeh. 2003. “Chaotic Analysis of Nonlinear Viscoelastic Panel Flutter in Supersonic Flow.” Nonlinear Dynamics 32 (4): 387–404. https://doi.org/10.1023/a:1025616916033
• Pramanik, Alokesh, and Guy Littlefair. 2014. “Developments in Machining of Stacked Materials Made of CFRP and Titanium/Aluminum Alloys.” Machining Science and Technology 18 (4): 485–508. https://doi.org/10.1080/10910344.2014.955718
• Pramanik, Alokesh, and Guy Littlefair. 2015. “Machining of Titanium Alloy(Ti-6Al-4V)—Theory to Application.” Machining Science and Technology 19 (1): 1–49. https://doi.org/10.1080/10910344.2014.991031
• 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
• Previati, G., M. Gobbi, and G. Mastinu. 2012. “Method for the Measurement of the Inertia Properties of Bodies with Aerofoils.” Journal of Aircraft 49 (2): 444–52. https://doi.org/10.2514/1.c031369
• Pritchard, Robert E. 1969. “Base Drag Effects on Maximum Lift-to-Drag Ratio Airfoils at Moderate Supersonic Speeds.” Journal of Optimization Theory and Applications 3 (2): 115–36. https://doi.org/10.1007/bf00932462
• Puckett, Allen E. 1946. “Supersonic Wave Drag of Thin Airfoils.” Journal of the Aeronautical Sciences 13 (9): 475–84. https://doi.org/10.2514/8.11425
• Pushtaev, Yu. P. 1989. “The Flutter of a Wing with an Aileron in Transonic Flow.” USSR Computational Mathematics and Mathematical Physics 29 (2): 187–91. https://doi.org/10.1016/0041-5553(89)90024-4
• Pyle, Raymond W. 1947. “Determination of Turbojet Engine Thrust from Tailpipe Measurements.” Journal of the Aeronautical Sciences 14 (10): 561–64. https://doi.org/10.2514/8.1455
• Pytka, Jaroslaw A. 2014. “Identification of Rolling Resistance Coefficients for Aircraft Tires on Unsurfaced Airfields.” Journal of Aircraft 51 (2): 353–60. https://doi.org/10.2514/1.c031088
• Pytka, Jaroslaw, Piotr Budzynski, Jerzy Jozwik, Tomasz Lyszczyk, Jan Laskowski, and Ernest Gnapowski. 2019. “Measurement of Takeoff and Landing Ground Roll of Airplane on Grassy Runway.” In 2019 IEEE 5th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2019.8869645
• Pytka, Jarosław, Piotr Budzyński, Paweł Tomiło, et al. 2022. “Measurement of Aircraft Ground Roll Distance during Takeoff and Landing on a Grass Runway.” Measurement 195: 111130. https://doi.org/10.1016/j.measurement.2022.111130
• Qiao, Lina, Zhou Zhou, and Chi Zhang. 2019. “Static Aeroelastic Characteristics of Grid Structure Wing.” In 2019 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2019.8742016
• Qin, Bo-Wei, Kwok-Wai Chung, Antonio Algaba, and Alejandro J. Rodríguez-Luis. 2020. “High-Order Study of the Canard Explosion in an Aircraft Ground Dynamics Model.” Nonlinear Dynamics 100 (2): 1079–90. https://doi.org/10.1007/s11071-020-05575-w
• Qin, Yuan, He-xia Huang, Yu-yuan Cao, et al. 2026. “Unstart / Restart Phenomena Induced by Variable Bleed in a Simplified Inlet with Large Internal Contraction Ratio of 3.0.” Aerospace Science and Technology 168: 111044. https://doi.org/10.1016/j.ast.2025.111044
• Qu, Bao, Ling Wang, Kehuan Wang, et al. 2023. “Optimization of Hot Gas Pressure Forming Process for Titanium Alloy Component.” International Journal of Material Forming 16 (2): 18. https://doi.org/10.1007/s12289-023-01740-9
• R. 1934. “Report No. 484, a Flight Investigation of the Effect of Mass Distribution and Control Setting on the Spinning of the XN2Y-1 Airplane.” Journal of the Franklin Institute 218 (4): 512. https://doi.org/10.1016/s0016-0032(34)90432-4
• 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
• Ramachandra, Sridhar M., K. Sudhakar, P. V. K. Perumal, and P. Jayasimha. 1982. “Air-Inlet Engine Matching Problems Encountered in a Jet Trainer Re-Engining Program.” Journal of Aircraft 19 (8): 609–14. https://doi.org/10.2514/3.57441
• Ramachandran, S., and W. R. Wells. 1975. “Estimation of Nonlinear Aerodynamic Derivatives of a Variable-Geometry Fighter Aircraft.” Journal of Aircraft 12 (11): 853–54. https://doi.org/10.2514/3.59883
• Ramesh, Kiran. 2025. “Correct Wake Vorticity Shedding in Time-Stepping Unsteady Thin-Airfoil Theory.” AIAA Journal 63 (7): 3024–29. https://doi.org/10.2514/1.j065056
• Ramprakash, A., and T. M. Muruganandam. 2016. “Experimental Study on Internal Flowfield Characteristics and Start-Unstart Behaviour in a Two-Dimensional Variable Geometry Inlet.” In 2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2016.7549585
• Randels, W. C. 1954. “On Panel Flutter in Supersonic Flow.” Journal of the Aeronautical Sciences 21 (12): 860–860. https://doi.org/10.2514/8.3250
• Rankin, J., M. Desroches, B. Krauskopf, and M. Lowenberg. 2011. “Canard Cycles in Aircraft Ground Dynamics.” Nonlinear Dynamics 66 (4): 681–88. https://doi.org/10.1007/s11071-010-9940-y
• Rao, Hanyue, Yayun Shi, Junqiang Bai, Yifu Chen, Tihao Yang, and Junfu Li. 2023. “Aerodynamic Optimization Design of Supersonic Wing Based on Discrete Adjoint.” Aerospace 10 (5): 420. https://doi.org/10.3390/aerospace10050420
• Raveh, Daniella E. 2008. “Maneuver Load Analysis of Overdetermined Trim Systems.” Journal of Aircraft 45 (1): 119–29. https://doi.org/10.2514/1.29118
• Raveh, Daniella E. 2011. “Gust-Response Analysis of Free Elastic Aircraft in the Transonic Flight Regime.” Journal of Aircraft 48 (4): 1204–11. https://doi.org/10.2514/1.c031224
• Raveh, Daniella E., and Mordechay Karpel. 1999. “Structural Optimization of Flight Vehicles with Computational-Fluid-Dynamics-Based Maneuver Loads.” Journal of Aircraft 36 (6): 1007–15. https://doi.org/10.2514/2.2542
• Ravi, R., and William H. Mason. 1994. “Chine-Shaped Forebody Effects on Directional Stability at High-Alpha.” Journal of Aircraft 31 (3): 480–87. https://doi.org/10.2514/3.46519
• Razak, Norizham Abdul, Thomas Andrianne, and Grigorios Dimitriadis. 2011. “Flutter and Stall Flutter of a Rectangular Wing in a Wind Tunnel.” AIAA Journal 49 (10): 2258–71. https://doi.org/10.2514/1.j051041
• Reardon, Jonathan P., Joseph A. Schetz, and Kevin Todd Lowe. 2021. “Computational Analysis of Unstart in Variable-Geometry Inlet.” Journal of Propulsion and Power 37 (4): 564–76. https://doi.org/10.2514/1.b38214
• Rein, Martin, Ulrich Henne, and Michael Werner. 2025. “Multiswept Wing Planform Study at Subsonic, Transonic, and Supersonic Speeds.” AIAA Journal 63 (9): 3776–92. https://doi.org/10.2514/1.j065181
• Reinbold, Christopher, Kaare Sørensen, and Christian Breitsamter. 2021. “Aeroelastic Simulations of a Delta Wing with a Chimera Approach for Deflected Control Surfaces.” CEAS Aeronautical Journal 13 (1): 237–50. https://doi.org/10.1007/s13272-021-00561-3
• Ren, Huaqing, Jiaxi Xie, Shuheng Liao, Dohyun Leem, Kornel Ehmann, and Jian Cao. 2019. “In-Situ Springback Compensation in Incremental Sheet Forming.” CIRP Annals 68 (1): 317–20. https://doi.org/10.1016/j.cirp.2019.04.042
• “Report No. 441, a Filght Investigation of the Spinning of the NY- Airplane with Varied Mass Distribution and Other Modications, and an Analysis Based on Wind-Tunnel Tests.” 1932. Journal of the Franklin Institute 214 (6): 767. https://doi.org/10.1016/s0016-0032(32)91221-6
• Revil-Baudard, B., and E. Massoni. 2009. “Simulation of the Anisotropic Behavior of Titanium Alloys during Sheet Metal Forming.” International Journal of Material Forming 2 (S1): 73–76. https://doi.org/10.1007/s12289-009-0535-4
• Rhodes, William B. 1970. “Initial Military Flight Tests of the X-22A VSTOL Research Aircraft.” Journal of Aircraft 7 (2): 169–74. https://doi.org/10.2514/3.44142
• Ribner, H. S. 1960. “Further Comments on ‘Limiting Circulatory Lift of a Wing of Finite Aspect Ratio’.” Journal of the Aerospace Sciences 27 (6): 460–61. https://doi.org/10.2514/8.8580
• 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
• Rizzetta, D., and M. Visbal. 2012c. “Plasma Flow Control Simulations of a Low-Reynolds Number Low-Aspect-Ratio Wing.” Computers & Fluids 70: 95–114. https://doi.org/10.1016/j.compfluid.2012.08.025
• Rizzi, Arthur, and James M. Luckring. 2017. “What Was Learned in Predicting Slender Airframe Aerodynamics with the F-16XL Aircraft.” Journal of Aircraft 54 (2): 444–55. https://doi.org/10.2514/1.c033569
• Roberts, Richard Calvin. 1948. “Note on the Lift of a Triangular Wing at Supersonic Speeds.” Journal of Mathematics and Physics 27 (1–4): 49–55. https://doi.org/10.1002/sapm194827149
• Rodden, William P. 1972. “Comment on ‘ Convergence Proof of Discrete-Panel Wing Loading Theories’.” Journal of Aircraft 9 (9): 686–88. https://doi.org/10.2514/3.59062
• 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
• Rohith, G., and Nandan K. Sinha. 2020. “Routes to Chaos in the Post-Stall Dynamics of Higher-Dimensional Aircraft Model.” Nonlinear Dynamics 100 (2): 1705–24. https://doi.org/10.1007/s11071-020-05604-8
• Rosenberg, Reinhardt. 1944. “Loss in Aileron Effectiveness Because of Wing Twist and Considerations Regarding the Internal-Pressure Balanced Aileron.” Journal of the Aeronautical Sciences 11 (1): 41–47. https://doi.org/10.2514/8.11091
• Rott, N. 1951. “On the Unsteady Motion of a Thin Rectangular Wing in Supersonic Flow.” Journal of the Aeronautical Sciences 18 (11): 775–76. https://doi.org/10.2514/8.2109
• Rott, N. 1953. “Minimum Drag Cambered Rectangular Wing for Supersonic Speeds.” Journal of the Aeronautical Sciences 20 (9): 642–43. https://doi.org/10.2514/8.2770
• Ruan, Feng, Yang Feng, and Wenjuan Liu. 2008. “Springback Prediction for Complex Sheet Metal Forming Parts Based on Genetic Neural Network.” In 2008 Second International Symposium on Intelligent Information Technology Application. IEEE. https://doi.org/10.1109/iita.2008.425
• Ruhlin, Charles L., Frank J. Rauch, and Catherine Waters. 1983. “Transonic Flutter Model Study of a Supercritical Wing and Winglet.” Journal of Aircraft 20 (8): 711–16. https://doi.org/10.2514/3.44933
• Rule, John A., Robert E. Richard, and Robert L. Clark. 2001. “Design of an Aeroelastic Delta Wing Model for Active Flutter Control.” Journal of Guidance, Control, and Dynamics 24 (5): 918–24. https://doi.org/10.2514/2.4828
• Ryu, Shiyang, and Dominick Andrisani. 2003. “Longitudinal Flying Qualities Prediction for Nonlinear Aircraft.” Journal of Guidance, Control, and Dynamics 26 (3): 474–82. https://doi.org/10.2514/2.5070
• Sachs, Gottfried. 1977. “A New Concept of Static Stability and Its Flight Testing in Supersonic Flight.” Journal of Aircraft 14 (9): 874–80. https://doi.org/10.2514/3.44623
• Safiullin, R. V., A. A. Kruglov, A. Kh. Akhunova, A. R. Safiullin, and S. V. Dmitriev. 2012. “Modelling of Superplastic Forming of Hollow Structures with Goffered Filler Made of VT6 Titanium Alloy.” Materialwissenschaft und Werkstofftechnik 43 (9): 786–88. https://doi.org/10.1002/mawe.201200042
• Saidi, Badreddine, Laurence Giraud Moreau, Abel Cherouat, and Rachid Nasri. 2021. “Accuracy and Sheet Thinning Improvement of Deep Titanium Alloy Part with Warm Incremental Sheet-Forming Process.” Journal of Manufacturing and Materials Processing 5 (4): 122. https://doi.org/10.3390/jmmp5040122
• Saito, Naoko, Mitsugi Fukahori, Daisuke Hisano, Hiroshi Hamasaki, and Fusahito Yoshida. 2017. “Effects of Temperature, Forming Speed and Stress Relaxation on Springback in Warm Forming of High Strength Steel Sheet.” Procedia Engineering 207: 2394–98. https://doi.org/10.1016/j.proeng.2017.10.1014
• Sajadifar, Seyed Vahid, Hans Jürgen Maier, Thomas Niendorf, and Guney Guven Yapici. 2023. “Elevated Temperature Mechanical Characteristics and Fracture Behavior of a Novel Beta Titanium Alloy.” Crystals 13 (2): 269. https://doi.org/10.3390/cryst13020269
• Salay, C. R., and D. W. Elliott. 1996. “Matching Engine and Aircraft Lapse Rates for High Speed Civil Aircraft.” Journal of Aircraft 33 (1): 61–67. https://doi.org/10.2514/3.46903
• 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
• Sander, G., C. Bon, and M. Geradin. 1973. “Finite Element Analysis of Supersonic Panel Flutter.” International Journal for Numerical Methods in Engineering 7 (3): 379–94. https://doi.org/10.1002/nme.1620070313
• Sanders, Karl L. 1965. “Subsonic Induced Drag.” Journal of Aircraft 2 (4): 347–48. https://doi.org/10.2514/3.43662
• Sanders, Daniel G., and Mamidala Ramulu. 2004. “Examination of Superplastic Forming Combined with Diffusion Bonding for Titanium: Perspective from Experience.” Journal of Materials Engineering and Performance 13 (6): 744–52. https://doi.org/10.1361/10599490421574
• Sanders, D. G., M. Ramulu, and P. D. Edwards. 2008. “Superplastic Forming of Friction Stir Welds in Titanium Alloy 6Al-4V: Preliminary Results.” Materialwissenschaft und Werkstofftechnik 39 (4–5): 353–57. https://doi.org/10.1002/mawe.200800305
• Sanghi, Vivek, S. Kishore Kumar, V. Sundararajan, and S. K. Sane. 1998. “Engine-Airframe Integration during Conceptual Design for Military Application.” Journal of Aircraft 35 (3): 380–86. https://doi.org/10.2514/2.2335
• Sansica, Andrea, and Atsushi Hashimoto. 2023a. “Global Stability Analysis of Full-Aircraft Transonic Buffet at Flight Reynolds Numbers.” AIAA Journal 61 (10): 4437–55. https://doi.org/10.2514/1.j062808
• Sanz, Angel. 1986. “Cancellation Zone in Supersonic Lifting Wing Theory.” AIAA Journal 24 (8): 1377–78. https://doi.org/10.2514/3.9447
• Sattarov, Artemii, and Volodymyr Rozbytskyi. 2021. “Numerical Investigation of Aerodynamic Performance of Low Aspect Ratio Wing with Leading Edge Vortex Generators.” In 2021 IEEE 6th International Conference on Actual Problems of Unmanned Aerial Vehicles Development (APUAVD). IEEE. https://doi.org/10.1109/apuavd53804.2021.9615421
• Satyanarayana, G., U. Prasad, and I. Sarma. 1975. “Optimal Control for the Rolling Pullout Maneuver of a Modern Fighter Aircraft.” In 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1975.270730
• Saunders, Herbert. 1963. “Determination of Supersonic Panel Flutter of Cylindrical Shells with in-Plate Stresses.” AIAA Journal 1 (1): 209–209. https://doi.org/10.2514/3.1491
• Schewe, Günter, and Holger Mai. 2019. “Experiments on Transonic Limit-Cycle-Flutter of a Flexible Swept Wing.” Journal of Fluids and Structures 84: 153–70. https://doi.org/10.1016/j.jfluidstructs.2018.07.005
• Schmoeckel, D., and M. Beth. 1993. “Springback Reduction in Draw-Bending Process of Sheet Metals.” CIRP Annals 42 (1): 339–42. https://doi.org/10.1016/s0007-8506(07)62457-3
• Scholz, Felix, Aaron Theuser, Andreas Hupfer, and Isabel Bayerdörfer. 2026. “Manufacture-Oriented Design of a Topology-Optimized Nose Landing Gear Fork for a Small Aircraft with Retractable Landing Gear.” CEAS Aeronautical Journal. https://doi.org/10.1007/s13272-026-00958-y
• Schuster, David M. 1995. “Application of Navier-Stokes Aeroelastic Methods to Improve Fighter Wing Maneuver Performance.” Journal of Aircraft 32 (1): 77–83. https://doi.org/10.2514/3.46686
• Schütte, Andreas, and Dietrich Hummel. 2023. “Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration.” Journal of Aircraft 60 (3): 898–914. https://doi.org/10.2514/1.c037128
• Schy, A. A., and M. E. Hannah. 1977. “Prediction of Jump Phenomena in Roll-Coupled Maneuvers of Airplanes.” Journal of Aircraft 14 (4): 375–82. https://doi.org/10.2514/3.58787
• Seidel, David A., Maynard C. Sandford, and Clinton V. Eckstrom. 1987. “Measured Unsteady Transonic Aerodynamic Characteristics of an Elastic Supercritical Wing.” Journal of Aircraft 24 (4): 225–30. https://doi.org/10.2514/3.45430
• Seo, Gwang-gyo, Yoonsoo Kim, and Subrahmanyam Saderla. 2019. “Kalman-Filter Based Online System Identification of Fixed-Wing Aircraft in Upset Condition.” Aerospace Science and Technology 89: 307–17. https://doi.org/10.1016/j.ast.2019.04.012
• Sepahi-Younsi, Javad. 2022. “Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Buzz.” Aerospace Science and Technology 120: 107246. https://doi.org/10.1016/j.ast.2021.107246
• Sepahi-Younsi, Javad. 2025. “Experimental Study of the Buzz Phenomenon in a Supersonic Inlet with and without the Bleed.” Aerospace Science and Technology 163: 110346. https://doi.org/10.1016/j.ast.2025.110346
• Sepahi-Younsi, Javad, and Safa Esmaeili. 2023. “Source of Buzz Instability in a Supersonic Air Inlet.” Aerospace Science and Technology 138: 108334. https://doi.org/10.1016/j.ast.2023.108334
• Settineri, Luca, and Maria Giulia Faga. 2008. “Nanostructured Cutting Tools Coatings for Machining Titanium.” Machining Science and Technology 12 (2): 158–69. https://doi.org/10.1080/10910340802067239
• Sezgin, Aziz, Birkan Durak, Alaattin Sayın, et al. 2024. “Flutter of a Plate at High Supersonic Speeds.” Applied Sciences 14 (11): 4892. https://doi.org/10.3390/app14114892
• 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
• Sharad, Gawade, and V. M. Nandedkar. 2014. “Springback in Sheet Metal U Bending-Fea and Neural Network Approach.” Procedia Materials Science 6: 835–39. https://doi.org/10.1016/j.mspro.2014.07.100
• Sharan, Agam, K. Vijayaraju, and Deepa James. 2013. “Synthesis of in-Flight Strains Using Flight Parameters for a Fighter Aircraft.” Journal of Aircraft 50 (2): 469–77. https://doi.org/10.2514/1.c031888
• Sharifi Ghazijahani, Mohammad, and Mehmet Metin Yavuz. 2019. “Effect of Thickness-to-Chord Ratio on Aerodynamics of Non-Slender Delta Wing.” Aerospace Science and Technology 88: 298–307. https://doi.org/10.1016/j.ast.2019.03.033
• Shen, Lin, Da Huang, and Genxing Wu. 2019a. “Effects of Yaw-Roll Coupling Ratio on Lateral-Directional Aerodynamic Characteristics.” Chinese Journal of Aeronautics 32 (2): 272–80. https://doi.org/10.1016/j.cja.2018.11.009
• Shen, Lin, Da Huang, and Genxing Wu. 2019b. “Effects of Yaw-Roll Coupling Ratio on the Lateral-Directional Departure Prediction and Restraint.” Chinese Journal of Aeronautics 32 (10): 2239–53. https://doi.org/10.1016/j.cja.2019.04.007
• Sherwood, Alan G. 2007. “Case of Explosive Wing-Flaperon Flutter.” Journal of Aircraft 44 (2): 606–10. https://doi.org/10.2514/1.24711
• Shevchenko, Andrey, Boris Pavlov, and Galina Nachinkina. 2019a. “Effective Method of Predicting and Checking the Brake-Way of Aircraft.” In 2019 IEEE 5th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2019.8869625
• Shevchenko, Andrey, Boris Pavlov, and Galina Nachinkina. 2019b. “Prediction and Verification of an Aircraft Takeoff Trajectory with High-Altitude Obstacles.” In 2019 IEEE 5th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2019.8869599
• Shields, Matt, and Kamran Mohseni. 2012a. “Effects of Sideslip on the Aerodynamics of Low-Aspect-Ratio Low-Reynolds-Number Wings.” AIAA Journal 50 (1): 85–99. https://doi.org/10.2514/1.j051151
• Shields, Matt, and Kamran Mohseni. 2013b. “Passive Mitigation of Roll Stall for Low Aspect Ratio Wings.” Advanced Robotics 27 (9): 667–81. https://doi.org/10.1080/01691864.2013.778941
• Shields, Matt, and Kamran Mohseni. 2013c. “Roll Stall for Low-Aspect-Ratio Wings.” Journal of Aircraft 50 (4): 1060–69. https://doi.org/10.2514/1.c031933
• Shishaeva, Anastasia, Andrey Aksenov, and Vasily Vedeneev. 2022. “The Effect of External Perturbations on Nonlinear Panel Flutter at Low Supersonic Speed.” Journal of Fluids and Structures 111: 103570. https://doi.org/10.1016/j.jfluidstructs.2022.103570
• Shishaeva, Anastasia, Vasily Vedeneev, and Andrey Aksenov. 2015. “Nonlinear Single-Mode and Multi-Mode Panel Flutter Oscillations at Low Supersonic Speeds.” Journal of Fluids and Structures 56: 205–23. https://doi.org/10.1016/j.jfluidstructs.2015.05.005
• Shixing, Zhu, Wang Peng, and Tian Jing. 2011. “Experimental Research on Aircraft Landing Gear Drop Test Based on MRF Damper.” Procedia Engineering 15: 4712–17. https://doi.org/10.1016/j.proeng.2011.08.882
• Shkaraputa, L. M. 1976. “Effect of Elevated Temperature on the Deformation of Titanium Alloys Subjected to Biaxial Stress.” Strength of Materials 8 (2): 233–35. https://doi.org/10.1007/bf01533037
• Shmilovich, Arvin, Yoram Yadlin, Paul M. Vijgen, and Rene Woszidlo. 2026. “Active Flow Control for Enhanced High-Lift Aileron Effectiveness.” Journal of Aircraft 63 (3): 865–84. https://doi.org/10.2514/1.c037586
• Shrivastava, Prakash C., and Robert F. Stengel. 1989. “Stability Boundaries for Aircraft with Unstable Lateral-Directional Dynamics and Control Saturation.” Journal of Guidance, Control, and Dynamics 12 (1): 62–70. https://doi.org/10.2514/3.20369
• Shu, Yiquan, Junxue Ren, Wenbo Zhang, and Wengang Liu. 2025. “Gradient Thickness-Dependent Distribution of Residual Stress and Springback of Thin-Walled TC4 Titanium Alloy Sheet with Variable Thickness in Collaborative Manufacturing Process of Pre-Plastic Forming and Milling.” International Journal of Advanced Manufacturing Technology 137 (9–10): 4853–79. https://doi.org/10.1007/s00170-025-15429-7
• Shuhua Zhu, Mingbo Tong, and Jie Xu. 2008. “Design of an Adaptive Shock Absorber of Landing Gear and Preliminary Analysis on Taxiing Performance.” In 2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing. IEEE. https://doi.org/10.1109/asc-icsc.2008.4675338
• Shumsky, G. M. 2010a. “Numerical Study of Self-Induced Wing Rock of a Low-Aspect-Ratio Delta Wing in the Presence of External Disturbances.” Journal of Applied Mechanics and Technical Physics 51 (3): 353–58. https://doi.org/10.1007/s10808-010-0048-4
• Shumsky, Gennady. 2010b. “Self-Indused Roll-Oscillation Delta Wing on High Angeles of Attack.” In International Forum on Strategic Technology 2010. IEEE. https://doi.org/10.1109/ifost.2010.5667939
• Sibert, H. W. 1937. “Slope of Lift Curve for Any Aspect Ratio.” Journal of the Aeronautical Sciences 4 (5): 195–195. https://doi.org/10.2514/8.367
• Sibert, H. W. 1947. “Aerodynamic Center and Center of Pressure of an Airfoil at Supersonic Speeds.” Journal of the Aeronautical Sciences 14 (3): 183–84. https://doi.org/10.2514/8.1305
• Sidoryuk, Maria E., and Alexander N. Khrabrov. 2019. “Estimation of Regions of Attraction of Aircraft Spin Modes.” Journal of Aircraft 56 (1): 205–16. https://doi.org/10.2514/1.c034936
• Simmons, Benjamin M., James L. Gresham, and Craig A. Woolsey. 2023b. “Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data.” Journal of Aircraft 60 (3): 968–80. https://doi.org/10.2514/1.c037259
• Singh, S. N. n.d. “Ultimate Boundedness Control of Uncertain Systems with Application to Roll Coupled Aircraft Maneuver.” In Proceedings of the 28th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1989.70442
• 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
• Singh, J., and R. V. Jategaonkar. 1996. “Identification of Lateral-Directional Behavior in Stall from Flight Data.” Journal of Aircraft 33 (3): 627–30. https://doi.org/10.2514/3.46993
• Singh, Indrajeet, R. K. Mishra, and P. S. Aswatha Narayana. 2016. “Numerical Study of a Transonic Aircraft Wing for the Prediction of Flutter Failure.” Journal of Failure Analysis and Prevention 17 (1): 107–19. https://doi.org/10.1007/s11668-016-0209-8
• Singh, Jatinder, and S. C. Raisinghani. 1993. “Aileron and Sideslip-Induced Unsteady Aerodynamic Modeling for Lateral Parameter Estimation.” Journal of Aircraft 30 (4): 512–18. https://doi.org/10.2514/3.46373
• Sinha, Nandan K., and N. Ananthkrishnan. 2002. “Maximum Steady Roll Rate in Zero-Sideslip Roll Maneuvers of Aircraft.” Journal of Aircraft 39 (5): 897–99. https://doi.org/10.2514/2.3014
• Siswanto, Waluyo Adi, Agus Dwi Anggono, Badrul Omar, and Kamaruzaman Jusoff. 2014. “An Alternate Method to Springback Compensation for Sheet Metal Forming.” Scientific World Journal 2014: 1–13. https://doi.org/10.1155/2014/301271
• 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
• Sivaramakrishnan, M. M. 1981. “Influence of Landing Gear Flexibility on Aircraft Performance during Ground Roll.” Journal of Aircraft 18 (11): 991–92. https://doi.org/10.2514/3.57591
• Skow, Andrew M., William A. Moore, and Dale J. Lorincz. 1982. “Control of Forebody Vortex Orientation to Enhance Departure Recovery of Fighter Aircraft.” Journal of Aircraft 19 (10): 812–19. https://doi.org/10.2514/3.61562
• Smaili, M. H., W. F. J. A. Rouwhorst, and P. Frost. 2018. “Conceptual Design and Evaluation of Upset-Recovery Systems for Civil Transport Aircraft.” Journal of Aircraft 55 (3): 947–64. https://doi.org/10.2514/1.c034422
• Smith, J. H. B. 1990. “Comment on ‘Exact and Asymptotic Expressions of the Lift Slope Coefficient of an Elliptic Wing’.” AIAA Journal 28 (6): 1146a-1146a. https://doi.org/10.2514/3.48881
• 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
• Snyder, Matthew P., and Terrence A. Weisshaar. 2013. “Flutter and Directional Stability of Aircraft with Wing-Tip Fins: Conflicts and Compromises.” Journal of Aircraft 50 (2): 615–25. https://doi.org/10.2514/1.c031978
• 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
• Sodja, Jurij, Noud P. M. Werter, and Roeland De Breuker. 2021. “Aeroelastic Demonstrator Wing Design for Maneuver Load Alleviation under Cruise Shape Constraint.” Journal of Aircraft 58 (3): 448–66. https://doi.org/10.2514/1.c035955
• Soltani, Mohammad Reza, and Mohammad Farahani. 2012. “Effects of Angle of Attack on Inlet Buzz.” Journal of Propulsion and Power 28 (4): 747–57. https://doi.org/10.2514/1.b34209
• Song, Shufang, Zhenzhou Lu, Weiwei Zhang, and Lijie Cui. 2011. “Uncertainty Importance Measure by Fast Fourier Transform for Wing Transonic Flutter.” Journal of Aircraft 48 (2): 449–55. https://doi.org/10.2514/1.c031038
• Song, Zhi-Guang, Tian-Zhi Yang, Feng-Ming Li, Erasmo Carrera, and Peter Hagedorn. 2018. “A Method of Panel Flutter Suppression and Elimination for Aeroelastic Structures in Supersonic Airflow.” Journal of Vibration and Acoustics 140 (6): 064501. https://doi.org/10.1115/1.4039724
• Song, Lei, Hua Yang, Yang Zhang, Haoyu Zhang, and Jun Huang. 2014. “Dihedral Influence on Lateral–directional Dynamic Stability on Large Aspect Ratio Tailless Flying Wing Aircraft.” Chinese Journal of Aeronautics 27 (5): 1149–55. https://doi.org/10.1016/j.cja.2014.08.003
• Soni, J. S., and G. Chakraverti. 1994. “Machining Characteristics of Titanium with Rotary Electro-Discharge Machining.” Wear 171 (1–2): 51–58. https://doi.org/10.1016/0043-1648(94)90347-6
• Sonowal, Plabita, K. M. Pandey, and K. K. Sharma. 2021. “Design and Static Analysis of Landing Gear Shock Absorber of Commercial Aircraft.” Materials Today: Proceedings 45: 6712–17. https://doi.org/10.1016/j.matpr.2020.11.1032
• Soong, Tsai-Chen. 1972. “Thermoelastic Effect on Delta-Wing Flutter with Arbitrary Stiffness Orientation.” Journal of Aircraft 9 (12): 835–43. https://doi.org/10.2514/3.59083
• Sorensen, Norman E., Eldon A. Latham, and Donald B. Smeltzer. 1976. “Variable Geometry for Supersonic Mixed-Compression Inlets.” Journal of Aircraft 13 (4): 309–12. https://doi.org/10.2514/3.58659
• Sorgente, Donato. 2021. “Superplasticity and Superplastic Forming.” Metals 11 (6): 946. https://doi.org/10.3390/met11060946
• Sosnin, O. V., and N. G. Torshenov. 1970. “Creep and Fracture of Ot-4 Titanium Alloy at Constant Temperature.” Strength of Materials 2 (5): 425–28. https://doi.org/10.1007/bf01527239
• Soviero, Paulo A. O., and Hugo B. Resende. 1997. “Subsonic/Supersonic Yawed Gust over an Airfoil.” AIAA Journal 35 (2): 397–99. https://doi.org/10.2514/2.107
• Sparks, D. W., and D. D. Moerder. 2002. “Optimal Aircraft Control Upset Recovery with and without Component Failures.” In Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301). IEEE. https://doi.org/10.1109/acc.2002.1024494
• Srivastava, B. 1998. “Aerodynamic Performance of Supersonic Missile Body- and Wing Tip-Mounted Lateral Jets.” Journal of Spacecraft and Rockets 35 (3): 278–86. https://doi.org/10.2514/2.3352
• Stanford, Bret K., and Kevin E. Jacobson. 2024. “Transonic Flutter Dips of the AGARD 445.6 Wing.” Journal of Aircraft 61 (2): 515–22. https://doi.org/10.2514/1.c037679
• Stanišić, Milomir M. 1961. “On the Aerodynamic Forces Acting on a Delta-Wing in Supersonic Flow with Supersonic Leading Edges.” ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik 41 (9): 342–54. https://doi.org/10.1002/zamm.19610410903
• Stanitz, John D. 1948. “Note on the Simple Ram-Air Intake Preceded by Normal Shock in Supersonic Flight.” Journal of the Aeronautical Sciences 15 (3): 181–83. https://doi.org/10.2514/8.11538
• Starr, R. F. 1978. “Experimental Observations of Wall Interference at Transonic Speeds.” Journal of Aircraft 15 (12): 822–28. https://doi.org/10.2514/3.58455
• Stenfelt, Gloria, and Ulf Ringertz. 2009. “Lateral Stability and Control of a Tailless Aircraft Configuration.” Journal of Aircraft 46 (6): 2161–64. https://doi.org/10.2514/1.41092
• Stenfelt, Gloria, and Ulf Ringertz. 2013. “Yaw Departure and Recovery of a Tailless Aircraft Configuration.” Journal of Aircraft 50 (1): 311–15. https://doi.org/10.2514/1.c031868
• Stengel, Robert F. 1970. “Altitude Stability in Supersonic Cruising Flight.” Journal of Aircraft 7 (5): 464–73. https://doi.org/10.2514/3.44200
• Stengel, Robert F. 1975. “Effect of Combined Roll Rate and Sideslip Angle on Aircraft Flight Stability.” Journal of Aircraft 12 (8): 683–85. https://doi.org/10.2514/3.44482
• Stengel, Robert F. 1980. “Some Effects of Parameter Variations on the Lateral-Directional Stability of Aircraft.” Journal of Guidance and Control 3 (2): 124–31. https://doi.org/10.2514/3.55959
• Stewart, H. J. 1956. “A Review of Source Superposition and Conical Flow Methods in Supersonic Wing Theory.” Journal of the Aeronautical Sciences 23 (5): 507–16. https://doi.org/10.2514/8.3590
• Stewart, H. J., and Ting-Yi Li. 1950. “Periodic Motions of a Rectangular Wing Moving at Supersonic Speed.” Journal of the Aeronautical Sciences 17 (9): 529–39. https://doi.org/10.2514/8.1720
• Stewartson, K. 1966. “On Wing–body Interference in Supersonic Flow.” Mathematika 13 (2): 121–39. https://doi.org/10.1112/s0025579300003880
• 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
• 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
• Stubblefield, Eric D., Donald L. Kunz, and Nicholas W. Dona. 2025. “Visualization and Measurement of Shock Movement during Transonic Limit-Cycle Oscillation.” Journal of Fluids and Structures 134: 104278. https://doi.org/10.1016/j.jfluidstructs.2025.104278
• Su, Jingke, Anxiong Liu, Kun Luo, and Jianren Fan. 2025b. “Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics.” Journal of Aircraft 62 (5): 1204–16. https://doi.org/10.2514/1.c038212
• Sun, P., J. J. Grácio, and J. A. Ferreira. 2006. “Control System of a Mini Hydraulic Press for Evaluating Springback in Sheet Metal Forming.” Journal of Materials Processing Technology 176 (1–3): 55–61. https://doi.org/10.1016/j.jmatprotec.2006.02.009
• Sun, Weiyu, Boyan Liang, Zhichun Yang, and Wei Tian. 2026b. “Nonlinear Aeroelasticity and Ground Flutter Simulation Test of a Supersonic Panel.” Thin-Walled Structures 227: 115049. https://doi.org/10.1016/j.tws.2026.115049
• Sun, Haijun, Jian Zhang, Xiaogang Ma, and Rui Xue. 2024. “Shock Wave Control for Supersonic Inlet with High-Frequency Pulsed Arc Discharge Plasma.” AIAA Journal 62 (12): 4888–92. https://doi.org/10.2514/1.j064672
• Sun, Huajun, Heng Zhang, Ziyan Wei, and Jie Li. 2026a. “Aerodynamic Shape Design of Oblique Wing for Transonic/supersonic Conditions: Integrating Coupled Drag and Lateral Performance Using the Adjoint Method.” Aerospace Science and Technology 168: 110841. https://doi.org/10.1016/j.ast.2025.110841
• Sundararajan, V. 1971. “Effect of a Rigid Boundary on the Flutter of a Thin Panel.” Journal of Sound and Vibration 19 (2): 147–51. https://doi.org/10.1016/0022-460x(71)90603-1
• “Supersonic Airfoil Performance with Small Heat Addition.” 1959. Wear 2 (6): 492. https://doi.org/10.1016/0043-1648(59)90189-9
• Sura, Niranjan K., and S. Suryanarayan. 2009. “Lateral Stability of Aircraft Nose-Wheel Landing Gear with Closed-Loop Shimmy Damper.” Journal of Aircraft 46 (2): 505–9. https://doi.org/10.2514/1.37626
• Surber, Lewis E., and Dennis Sedlock. 1979. “Effects of Airframe-Inlet Integration on Half -Axisymmetric and Two-Dimensional Supersonic Inlet Performance.” Journal of Aircraft 16 (9): 612–19. https://doi.org/10.2514/3.58575
• Suryanarayana, G. K., D. B. Singh, Sumukh Surya, and G. Jagadeesh. 2022. “Nonlinear Damping Model for Supersonic Air-Intake Buzz.” Aerospace Science and Technology 126: 107567. https://doi.org/10.1016/j.ast.2022.107567
• Sussman, Mark B. 1968. “A Remark Concerning Engine-Inlet Distortion.” Journal of Aircraft 5 (1): 95–96. https://doi.org/10.2514/3.43914
• 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
• Swaim, Robert L., and Donald G. Fullman. 1977. “Prediction of Elastic-Airplane Longitudinal Dynamics from Rigid-Body Aerodynamics.” Journal of Aircraft 14 (9): 868–73. https://doi.org/10.2514/3.58867
• Swaim, Robert L., and George H. Staab. 1978. “Prediction of Elastic-Airplane Lateral Dynamics from Rigid-Body Aerodynamics.” Journal of Aircraft 15 (7): 392–98. https://doi.org/10.2514/3.58377
• Tadi, M. 2002. “Compensator Design for a Supersonic Panel Flutter.” Computers & Structures 80 (11): 989–99. https://doi.org/10.1016/s0045-7949(02)00039-1
• Taghi-Abad, Sohrab Panahandeh, Mohammad Hossein Moghimi Esfand-Abadi, and Javad Sepahi-Younsi. 2026. “Delaying the Buzz Onset in a Supersonic Inlet by Multi-Row Disk Concept.” Aerospace Science and Technology 168: 110963. https://doi.org/10.1016/j.ast.2025.110963
• Takashima, Naruhisa, and Mark J. Lewis. 1995. “Wedge-Cone Waverider Configuration for Engine-Airframe Interaction.” Journal of Aircraft 32 (5): 1142–44. https://doi.org/10.2514/3.46848
• Tang, Haihong, Panglun Liu, Jianbin Ding, Jinsong Cheng, Yiyao Jiang, and Bingyan Jiang. 2025. “Numerical Prediction of Fatigue Life for Landing Gear Considering the Shock Absorber Travel.” Aerospace 12 (1): 42. https://doi.org/10.3390/aerospace12010042
• Tang, Bingtao, Xiaoyang Lu, Zhaoqing Wang, and Zhen Zhao. 2010a. “Springback Investigation of Anisotropic Aluminum Alloy Sheet with a Mixed Hardening Rule and Barlat Yield Criteria in Sheet Metal Forming.” Materials & Design 31 (4): 2043–50. https://doi.org/10.1016/j.matdes.2009.10.017
• Tang, Bingtao, Xiaoyang Lu, Xiaowei Zhao, and Shiying Chen. 2010b. “U-Bending Springback Prediction of Highly Anisotropic Aluminum Alloy Sheet by an Efficient Non-Linear Combined Hardening Rule.” In 2010 International Conference on Mechanic Automation and Control Engineering. IEEE. https://doi.org/10.1109/mace.2010.5536819
• Tanrikulu, Omer, Cenk Onen, and Taner Gokhan. 2000. “Nonlinear Yaw-Pitch-Roll Coupling of Unguided Missiles with Wraparound Fins.” Journal of Spacecraft and Rockets 37 (6): 731–39. https://doi.org/10.2514/2.3644
• Tao, Cui, Yu Daren, Chang Juntao, and Bao Wen. 2008. “Topological Geometry Interpretation of Supersonic Inlet Start/Unstart Based on Catastrophe Theory.” Journal of Aircraft 45 (4): 1464–68. https://doi.org/10.2514/1.34125
• Tao, Cui, Yu Daren, Chang Juntao, and Bao Wen. 2009. “Catastrophe Model for Supersonic Inlet Start/Unstart.” Journal of Aircraft 46 (4): 1160–66. https://doi.org/10.2514/1.38926
• Tartaruga, I., J. E. Cooper, M. H. Lowenberg, P. Sartor, and Y. Lemmens. 2018. “Uncertainty and Sensitivity Analysis of Bifurcation Loci Characterizing Nonlinear Landing-Gear Dynamics.” Journal of Aircraft 55 (1): 162–72. https://doi.org/10.2514/1.c034252
• Tavoularis, S. 1999. “Equivalence between Sideslip and Roll in Wind-Tunnel Model Testing.” Journal of Aircraft 36 (5): 895–96. https://doi.org/10.2514/2.2526
• Taylor, J. B. 1971. “Engine Compatibility Programs for the Supersonic Transport Propulsion System.” Journal of Aircraft 8 (4): 213–18. https://doi.org/10.2514/3.44257
• Tekaslan, Özgür, Ulvi Şeker, and Ahmet Özdemir. 2006. “Determining Springback Amount of Steel Sheet Metal Has 0.5 Mm Thickness in Bending Dies.” Materials & Design 27 (3): 251–58. https://doi.org/10.1016/j.matdes.2004.10.006
• Terashima, Hiroshi, and Kozo Fujii. 2007. “Influence of Stores on the Transonic Flutter of a Delta Wing Configuration.” AIAA Journal 45 (1): 237–46. https://doi.org/10.2514/1.24489
• Tewari, Ashish. 1993. “Accuracy of Rational-Function Approximations for Linear Transonic Unsteady Aerodynamics.” Journal of Aircraft 30 (6): 1001–3. https://doi.org/10.2514/3.46445
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2008. “Interaction of Torsion and Lateral Bending in Aircraft Nose Landing Gear Shimmy.” Nonlinear Dynamics 57 (3): 455–67. https://doi.org/10.1007/s11071-008-9455-y
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2012. “Multi-Parameter Bifurcation Study of Shimmy Oscillations in a Dual-Wheel Aircraft Nose Landing Gear.” Nonlinear Dynamics 70 (2): 1675–88. https://doi.org/10.1007/s11071-012-0565-1
• Tian Jing and Ding Li. 2010. “Establishment and Analysis of Drop Simulation Experiment Platform of Landing Gear Based on ADAMS/Aircraft.” In The 2nd International Conference on Information Science and Engineering. IEEE. https://doi.org/10.1109/icise.2010.5691824
• Timman, R. 1954. “Linearized Theory of the Oscillating Airfoil in Compressible Subsonic Flow.” Journal of the Aeronautical Sciences 21 (4): 230–36. https://doi.org/10.2514/8.2986
• Tindell, R. H. 1981. “Inlet Drag and Stability Considerations for Mo = 2.00 Design.” Journal of Aircraft 18 (11): 943–50. https://doi.org/10.2514/3.57584
• “Titanium or Titanium Alloy Clad Aluminium or Aluminium Alloy Composite.” 1974. Composites 5 (5): 234. https://doi.org/10.1016/0010-4361(74)90155-4
• Titov, Egor, and Sergey Serebryansky. 2026. “Approach to the Main Landing Gear Linkage Design for the Requirement of Ultimate Loads on Links during Emergency Landing.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00486-x
• Tobak, Murray, and Lewis B. Schiff. 1975a. “Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling: Part 11-Nonlinear Coning-Rate Dependence.” AIAA Journal 13 (3): 327–32. https://doi.org/10.2514/3.49699
• Tobak, Murray, and Lewis B. Schiff. 1975b. “Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling: Part I-Nonaxisymmetric Bodies.” AIAA Journal 13 (3): 323–26. https://doi.org/10.2514/3.49698
• Torres, Gabriel E., and Thomas J. Mueller. 2004. “Low Aspect Ratio Aerodynamics at Low Reynolds Numbers.” AIAA Journal 42 (5): 865–73. https://doi.org/10.2514/1.439
• Trân, Ricardo, Franz Reuther, Sven Winter, and Verena Psyk. 2020. “Process Development for a Superplastic Hot Tube Gas Forming Process of Titanium (Ti-3Al-2.5V) Hollow Profiles.” Metals 10 (9): 1150. https://doi.org/10.3390/met10091150
• “Transonic Navier-Stokes Flow Computations over Wing-Fuselage Geometries.” 1972. Journal of Aircraft 9 (1): 31–42. https://doi.org/10.2514/3.46413
• Trapier, S., S. Deck, and P. Duveau. 2008. “Delayed Detached-Eddy Simulation and Analysis of Supersonic Inlet Buzz.” AIAA Journal 46 (1): 118–31. https://doi.org/10.2514/1.32187
• Trapier, Simon, Sébastien Deck, Philippe Duveau, and Pierre Sagaut. 2007b. “Time-Frequency Analysis and Detection of Supersonic Inlet Buzz.” AIAA Journal 45 (9): 2273–84. https://doi.org/10.2514/1.29196
• Trapier, Simon, Philippe Duveau, and Sebastien Deck. 2006. “Experimental Study of Supersonic Inlet Buzz.” AIAA Journal 44 (10): 2354–65. https://doi.org/10.2514/1.20451
• Traub, Lance W. 1997. “Prediction of Delta Wing Leading-Edge Vortex Circulation and Lift-Curve Slope.” Journal of Aircraft 34 (3): 450–52. https://doi.org/10.2514/2.2193
• Traub, Lance W. 2023. “Examination and Prediction of the Lift Components of Low Aspect Ratio Rectangular Flat Plate Wings.” Aerospace 10 (7): 597. https://doi.org/10.3390/aerospace10070597
• Triebstein, Hermann. 1986. “Steady and Unsteady Transonic Pressure Distributions on NACA 0012.” Journal of Aircraft 23 (3): 213–19. https://doi.org/10.2514/3.45291
• Trifonov, Roman, Kirill Shelkov, Sergey Perepechaev, and Andrey Boykov. 2024. “Determining the Applicability Limits of Different Accuracy Models When Analyzing the Loads on the Landing Gear during Landing.” Aerospace Systems 7 (3): 617–27. https://doi.org/10.1007/s42401-023-00253-2
• Tromp, Jeffrey C. 1999. “Flowfield Simulation about a 65-Degree Delta Wing during Constant Roll-Rate Motions.” Journal of Aircraft 36 (2): 486–88. https://doi.org/10.2514/2.2462
• Trussa, Colin W., Clifford A. Whitfield, and Lian Duan. 2026. “Aerodynamic Characteristics of Flat-Plate Delta Wing with Deflected Wing Tips.” Journal of Aircraft: 1–13. https://doi.org/10.2514/1.c038565
• Trzepieciński, Tomasz, and Hirpa G. Lemu. 2020. “Improving Prediction of Springback in Sheet Metal Forming Using Multilayer Perceptron-Based Genetic Algorithm.” Materials 13 (14): 3129. https://doi.org/10.3390/ma13143129
• Tsien, S. H. 1955. “The Supersonic Conical Wing of Minimum Drag.” Journal of the Aeronautical Sciences 22 (12): 805–17. https://doi.org/10.2514/8.3476
• Tsushima, Natsuki, Kenichi Saitoh, and Kazuyuki Nakakita. 2023. “Structural and Aeroelastic Characteristics of Wing Model for Transonic Flutter Wind Tunnel Test Fabricated by Additive Manufacturing with AlSi10Mg Alloys.” Aerospace Science and Technology 140: 108476. https://doi.org/10.1016/j.ast.2023.108476
• Tudosie, Alexandru-Nicolae. 2024. “Aircraft Turbojet Engine with Afterburning as Controlled Object.” In 2024 25th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/iccc62069.2024.10569513
• Ud-Din, Sameer, and Yoonjin Yoon. 2018. “Analysis of Loss of Control Parameters for Aircraft Maneuvering in General Aviation.” Journal of Advanced Transportation 2018: 1–19. https://doi.org/10.1155/2018/7865362
• Uhlmann, Eckart, Robert Kersting, Tiago Borsoi Klein, Marcio Fernando Cruz, and Anderson Vicente Borille. 2015. “Additive Manufacturing of Titanium Alloy for Aircraft Components.” Procedia CIRP 35: 55–60. https://doi.org/10.1016/j.procir.2015.08.061
• Valdivia, A., K. B. Yuceil, J. L. Wagner, N. T. Clemens, and D. S. Dolling. 2014. “Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators.” AIAA Journal 52 (6): 1207–18. https://doi.org/10.2514/1.j052214
• van Dam, C. P., K. Nikfetrat, K. Wong, and P. M. H. W. Vijgen. 1995. “Drag Prediction at Subsonic and Transonic Speeds Using Euler Methods.” Journal of Aircraft 32 (4): 839–45. https://doi.org/10.2514/3.46799
• Van Deusen, E. A., and V. R. Mardoc. 1972. “Distortion and Turbulence Interaction: A Method for Evaluating Engine Inlet Compatibility.” Journal of Aircraft 9 (1): 16–22. https://doi.org/10.2514/3.58933
• van Es, Gerard W. H. 1999. “Method for Predicting the Rolling Resistance of Aircraft Tires in Dry Snow.” Journal of Aircraft 36 (5): 762–68. https://doi.org/10.2514/2.2531
• Van Thullenar, C. F. 1957. “The Tornado Research Airplane.” Weatherwise 10 (3): 82–104. https://doi.org/10.1080/00431672.1957.9924976
• Van Valkenburg, E. S., and N. W. Matthews. 1950a. “Analogue Methods for Turbojet Thrust Instrumentation.” Electrical Engineering 69 (11): 1004–1004. https://doi.org/10.1109/ee.1950.6437095
• Van Valkenburg, E. S., and N. W. Matthews. 1950b. “Analogue Techniques for Turbojet Thrust Instrumentation.” Transactions of the American Institute of Electrical Engineers 69 (2): 1342–46. https://doi.org/10.1109/t-aiee.1950.5060300
• van Zyl, Louw H. 1994. “Integration of the Supersonic Kernel Function.” Journal of Aircraft 31 (6): 1433–35. https://doi.org/10.2514/3.46675
• Varwig, R. L., and L. Rosenman. 1966. “A 7-Ft-Diam Shock Tube for Transonic and Supersonic Aerodynamic Testing.” Journal of Spacecraft and Rockets 3 (12): 1809–11. https://doi.org/10.2514/3.28759
• 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
• Vedeneev, Vasily V. 2012. “Panel Flutter at Low Supersonic Speeds.” Journal of Fluids and Structures 29: 79–96. https://doi.org/10.1016/j.jfluidstructs.2011.12.011
• Vedeneev, Vasily V., Sergey V. Guvernyuk, Alexander F. Zubkov, and Mikhail E. Kolotnikov. 2010b. “Experimental Observation of Single Mode Panel Flutter in Supersonic Gas Flow.” Journal of Fluids and Structures 26 (5): 764–79. https://doi.org/10.1016/j.jfluidstructs.2010.04.004
• Velger, M., and J. Shinar. 1983. “Cross-Coupling between Longitudinal and Lateral Aircraft Dynamics Ina Spiral Dive.” Journal of Aircraft 20 (1): 21–26. https://doi.org/10.2514/3.44823
• Venkatesan, C. 1977. “Optimization of an Oleo-Pneumatic Shock Absorber of an Aircraft during Landing.” Journal of Aircraft 14 (8): 822–23. https://doi.org/10.2514/3.44619
• Verdon, Joseph M. 1974. “Unsteady Flow Downstream of an Airfoil Oscillating in a Supersonic Stream.” AIAA Journal 12 (7): 999–1001. https://doi.org/10.2514/3.49394
• Vira, Narendra R., and Dah-Nien Fan. 1982. “Supersonic Wing-Body Center of Pressure with Finite Afterbodies.” AIAA Journal 20 (8): 1144–46. https://doi.org/10.2514/3.7967
• Visbal, Miguel, Turgut O. Yilmaz, and Donald Rockwell. 2013. “Three-Dimensional Vortex Formation on a Heaving Low-Aspect-Ratio Wing: Computations and Experiments.” Journal of Fluids and Structures 38: 58–76. https://doi.org/10.1016/j.jfluidstructs.2012.12.005
• 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
• Voß, A., and T. Klimmek. 2023. “Parametric Aeroelastic Modeling, Maneuver Loads Analysis Using CFD Methods and Structural Design of a Fighter Aircraft.” Aerospace Science and Technology 136: 108231. https://doi.org/10.1016/j.ast.2023.108231
• Vrh, Marko, Miroslav Halilovič, Bojan Starman, and Boris Štok. 2009. “Modelling of Springback in Sheet Metal Forming.” International Journal of Material Forming 2 (S1): 825–28. https://doi.org/10.1007/s12289-009-0514-9
• Waechter, R. T. 1969. “Wing-Body Interaction in Supersonic Flow.” Mathematika 16 (1): 122–42. https://doi.org/10.1112/s002557930000468x
• Wagner, J. L., K. B. Yuceil, and N. T. Clemens. 2010. “Velocimetry Measurements of Unstart of an Inlet-Isolator Model in Mach 5 Flow.” AIAA Journal 48 (9): 1875–88. https://doi.org/10.2514/1.j050037
• Wagner, J. L., K. B. Yuceil, A. Valdivia, N. T. Clemens, and D. S. Dolling. 2009a. “Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow.” AIAA Journal 47 (6): 1528–42. https://doi.org/10.2514/1.40966
• Wahi, Mahinder K. 1979. “Airplane Brake-Energy Analysis and Stopping Performance Simulation.” Journal of Aircraft 16 (10): 688–94. https://doi.org/10.2514/3.58590
• Walker, K. 1953. “The Supersonic Thickness Drag of Rectangular Wings with Linear Spanwise Taper in Thickness.” Journal of the Aeronautical Sciences 20 (7): 509–11. https://doi.org/10.2514/8.2707
• Walsh, J., G. Zartarian, and H. M. Voss. 1954. “Generalized Aerodynamic Forces on the Delta Wing with Supersonic Leading Edges.” Journal of the Aeronautical Sciences 21 (11): 739–48. https://doi.org/10.2514/8.3195
• Wan, Dawei, and Rongwei Guo. 2007. “Experimental Investigation of a Fixed-Geometry Two-Dimensional Mixed-Compression Supersonic Inlet with Sweep-Forward High- Light and Bleed Slot in an Inverted “X”-Type Layout.” Chinese Journal of Aeronautics 20 (4): 304–12. https://doi.org/10.1016/s1000-9361(07)60048-x
• Wang, Yong, Hanyan Bian, Yin Yin, and Xiaohui Wei. 2026a. “Enhancing Nose Landing Gear Shimmy Performance Using Torsional Inerter-Based Dynamic Vibration Absorber.” Chinese Journal of Aeronautics 39 (9): 104120. https://doi.org/10.1016/j.cja.2026.104120
• Wang, Ning, L. Chu, and T. F. Fwa. 2025a. “Effect of Tire Size on Aircraft Hydroplaning Speed on Runway Pavement.” International Journal of Pavement Engineering 26 (1): 2490972. https://doi.org/10.1080/10298436.2025.2490972
• Wang, Changsheng, Qitai Eri, Yong Wang, Bo Kong, and Wenhao Ding. 2023g. “Multi-Objective Aerodynamic Optimization of an Axisymmetric Variable-Geometry Inlet with a Mach 5 Design Point.” Aerospace Science and Technology 136: 108189. https://doi.org/10.1016/j.ast.2023.108189
• 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, Jee-Ray, Jung-Shian Jau, Jiam-Hwa Lee, and Hung-Chih Chang. 2007. “Apply Grey Relational Grade in Optimal Airplane Landing Gear Loads Calibration.” In 2007 International Conference on Intelligent and Advanced Systems. IEEE. https://doi.org/10.1109/icias.2007.4658394
• Wang, Zhuangzhuang, Xiaochao Liu, and Pengyuan Qi. 2024b. “Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research.” Journal of Aircraft 61 (4): 1218–29. https://doi.org/10.2514/1.c037783
• Wang, Kehuan, Gang Liu, Jie Zhao, Jianlong Wang, and Shijian Yuan. 2016b. “Formability and Microstructure Evolution for Hot Gas Forming of Laser-Welded TA15 Titanium Alloy Tubes.” Materials & Design 91: 269–77. https://doi.org/10.1016/j.matdes.2015.11.100
• Wang, Hong-wei, Yuan-wei Lyu, Jing-yang Zhang, and Si-Fang Liu. 2023h. “Numerical Investigation of Inlet Distortion in a Jet Engine Coupled with Ski-Jump of Carrier-Based Aircraft.” Thermal Science and Engineering Progress 43: 101961. https://doi.org/10.1016/j.tsep.2023.101961
• 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, Kehuan, Chenyu Shi, Shiqiang Zhu, Yongming Wang, Jintao Shi, and Gang Liu. 2020b. “Hot Gas Pressure Forming of Ti-55 High Temperature Titanium Alloy Tubular Component.” Materials 13 (20): 4636. https://doi.org/10.3390/ma13204636
• Wang, Zi-Yun, Shu Sun, Yue Zhang, Hui-Jun Tan, and Liang Chen. 2023d. “Duct Height Effect on Terminal Shock/Boundary-Layer Interaction in a Generic Supersonic Inlet.” AIAA Journal 61 (2): 573–84. https://doi.org/10.2514/1.j062300
• Wang, Jyhwen, Suhas Verma, Richard Alexander, and Jenn-Terng Gau. 2008. “Springback Control of Sheet Metal Air Bending Process.” Journal of Manufacturing Processes 10 (1): 21–27. https://doi.org/10.1016/j.manpro.2007.09.001
• Wang, Mengge, Ziyun Wang, Yue Zhang, et al. 2023b. “Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator.” Aerospace 10 (8): 729. https://doi.org/10.3390/aerospace10080729
• Wang, Le, Zili Wang, Shuyou Zhang, Yaochen Lin, Mengyu Fu, and Chang Sun. 2022c. “Spiral Metal Tube Multi-Roller Bending Springback Prediction Model Based on Dynamic Deformation Enhancement Analysis.” International Journal of Solids and Structures 254-255: 111940. https://doi.org/10.1016/j.ijsolstr.2022.111940
• Wang, Xiangyu, Zhigang Wu, Yukai Sun, and Chao Yang. 2021c. “A Novel Method for Estimating Three-Domain Limit Cycles in a 3D Wing-Aileron Model with Freeplay in Aileron Deflection.” Journal of Fluids and Structures 105: 103286. https://doi.org/10.1016/j.jfluidstructs.2021.103286
• Wang, Huaitao, Dafang Wu, Feng Wang, and Haoyuan Ren. 2017a. “A Method for Determining the Horizontal Impact Load Based on the Rotational Speed of the Aircraft’s Wheel in a Landing Gear Drop Test.” International Journal of Crashworthiness 23 (6): 627–34. https://doi.org/10.1080/13588265.2017.1368121
• Wang, G., K. F. Zhang, D. Z. Wu, J. Z. Wang, and Y. D. Yu. 2006. “Superplastic Forming of Bellows Expansion Joints Made of Titanium Alloys.” Journal of Materials Processing Technology 178 (1–3): 24–28. https://doi.org/10.1016/j.jmatprotec.2005.10.005
• Wang, Yu-Jie, and Yong-Ping Zhao. 2026. “Cross-Modal Schlieren-like Image Reconstruction of Supersonic Inlet Flows from Wall-Pressure Signals Using a Pressure-Guided StyleGAN Framework.” Measurement 292: 123286. https://doi.org/10.1016/j.measurement.2026.123286
• Wang, Yu-Jie, Yong-Ping Zhao, and Yi Jin. 2025d. “Multi-Level and Multi-Scale Cross Attention Network of Wavelet Packet Transform for Supersonic Inlet Unstart Prediction.” Expert Systems with Applications 272: 126782. https://doi.org/10.1016/j.eswa.2025.126782
• Wang, Yu-Jie, Yong-Ping Zhao, Huan Wu, and Yi Jin. 2022b. “A Real-Time Online Unstart Prediction Approach for Supersonic Inlet.” Aerospace Science and Technology 130: 107883. https://doi.org/10.1016/j.ast.2022.107883
• Wang, Yu-Jie, Yong-Ping Zhao, Huan Wu, and Yi Jin. 2023i. “Real-Time Online Unstart Prediction of Supersonic Inlet Based on Pressure Fluctuations.” Aerospace Science and Technology 140: 108420. https://doi.org/10.1016/j.ast.2023.108420
• 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
• Wang, Jun, Liu Zheng, Yixu Wang, Na Miao, and Xiaolin Zhang. 2023a. “Analysis of Air Bearing Torsion Pendulum Moment of Inertia Measurements Including Nonlinear Oscillation and Damping.” Review of Scientific Instruments 94 (6): 065106. https://doi.org/10.1063/5.0108741
• Wang, Gang, Hao Zhou, and Haris Hameed Mian. 2021d. “Numerical Analysis on Modal Stability Characteristics of 2D Panel Flutter at Low Supersonic Speeds.” Journal of Fluids and Structures 103: 103296. https://doi.org/10.1016/j.jfluidstructs.2021.103296
• Wang, Xiaomei, and Fanghui Zhu. 2024. “Study on Thermal Field Distribution of Civil Aircraft Wheel and Brake.” In 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae62008.2024.11026449
• 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
• Webster, W. Phillip, and Joseph S. Shang. 1991. “Thin-Layer Full Navier-Stokes Simulations over a Supersonic Delta Wing.” AIAA Journal 29 (9): 1363–69. https://doi.org/10.2514/3.10747
• Wei, Xiaohui, Chenglong Liu, Xiangyao Liu, Hong Nie, and Yizhou Shao. 2014. “Improved Model of Landing-Gear Drop Dynamics.” Journal of Aircraft 51 (2): 695–700. https://doi.org/10.2514/1.c032551
• Wei, Wenlan, Hao Qu, Jiarui Cheng, Rui Zhang, Yinping Cao, and Lu Cui. 2022b. “β-Phase-Induced Quasi-Cleavage Fracture Mechanism by Dual-Phase High-Strength Titanium Alloy at Elevated Temperature.” Crystals 12 (9): 1255. https://doi.org/10.3390/cryst12091255
• Wei, Li, Luo Yu, He Bo, Liu Yunpeng, and Yan Yingwen. 2025. “Method for Calculating the Combustion Performance of an Afterburner through Gas Components Analysis.” Aerospace Science and Technology 164: 110400. https://doi.org/10.1016/j.ast.2025.110400
• Weiss, Matthias, Shiromani Gangoda Desinghe, Peter Hodgson, and Hossein Beladi. 2024. “The Effect of the Forming Mode on Twinning and Springback in the Bending-Dominated Forming of Magnesium AZ31 Sheet.” Metals 14 (9): 983. https://doi.org/10.3390/met14090983
• Weisshaar, Terrence A. 1977. “Lateral Equilibrium of Asymmetrical Swept Wings: Aileron Control Vsgeometric Twist.” Journal of Aircraft 14 (2): 122–27. https://doi.org/10.2514/3.44579
• Weisshaar, Terrence A. 1990. “Integrated Structure/control Concepts for Oblique Wing Roll Control and Trim.” Journal of Aircraft 27 (4): 326–33. https://doi.org/10.2514/3.25276
• 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 Holt Ashley. 1974. “Static Aeroelasticity and the Flying Wing, Revisited.” Journal of Aircraft 11 (11): 718–20. https://doi.org/10.2514/3.44409
• Weissman, Robert. 1973. “Preliminary Criteria for Predicting Departure Characteristics/ Spin Susceptibility of Fighter-Type Aircraft.” Journal of Aircraft 10 (4): 214–19. https://doi.org/10.2514/3.60216
• Weissman, Robert. 1975. “Status of Design Criteria for Predicting Departure Characteristics and Spin Susceptibility.” Journal of Aircraft 12 (12): 989–93. https://doi.org/10.2514/3.59904
• Welge, H. R., R. L. Radkey, and P. A. Henne. 1977. “Nacelle Integration Study on a Mach-2.2 Supersonic Cruise Aircraft.” Journal of Aircraft 14 (11): 1085–92. https://doi.org/10.2514/3.58895
• 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
• Wenjuan Liu, Zhiyong Liang, Tao Huang, Yuanbin Chen, and Jinping Lian. 2008. “Process Optimal Control of Sheet Metal Forming Springback Based on Evolutionary Strategy.” In 2008 7th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2008.4594170
• Whitford, Ray. 1991. “Four Decades of Transonic Fighter Design.” Journal of Aircraft 28 (12): 805–11. https://doi.org/10.2514/3.46102
• Więckowski, Wojciech, Janina Adamus, Marcin Dyner, and Maciej Motyka. 2023. “Tribological Aspects of Sheet Titanium Forming.” Materials 16 (6): 2224. https://doi.org/10.3390/ma16062224
• Wieszala, Robert, Piotr Kolodziej, Jacek Mendala, and Jaroslaw Kozuba. 2022. “Relation between Wing Aspect Ratio and Induced Drag.” In 2022 New Trends in Aviation Development (NTAD). IEEE. https://doi.org/10.1109/ntad57912.2022.10013540
• Williams, M. H. 1980a. “Aerodynamic Coefficients in Generalized Unsteady Thin Airfoil Theory.” AIAA Journal 18 (7): 850–52. https://doi.org/10.2514/3.7693
• Williams, M. H. 1980b. “Unsteady Thin Airfoil Theory for Transonic Flows with Embedded Shocks.” AIAA Journal 18 (6): 615–24. https://doi.org/10.2514/3.50797
• Wilson, R. E. 1973. “Aerodynamic Interference of Pitot Tubes in a Turbulent Boundary Layer at Supersonic Speed.” AIAA Journal 11 (10): 1420–21. https://doi.org/10.2514/3.6929
• Winther, B. A., D. A. Hagemeyer, R. T. Britt, and W. P. Roden. 1995. “Aeroelastic Effects on the B-2 Maneuver Response.” Journal of Aircraft 32 (4): 862–67. https://doi.org/10.2514/3.46802
• Wood, Richard M., and David S. Miller. 1985b. “Impact of Fuselage Incidence on the Supersonic Aerodynamics of Two Fighter Configurations.” Journal of Aircraft 22 (5): 423–28. https://doi.org/10.2514/3.45141
• Woods-Vedeler, Jessica A., Anthony S. Pototzky, and Sherwood T. Hoadley. 1995. “Rolling Maneuver Load Alleviation Using Active Controls.” Journal of Aircraft 32 (1): 68–76. https://doi.org/10.2514/3.46685
• 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, Dipeng, Minghe Chen, Ronglei Fan, Wenchao Xiao, and Yong Wu. 2023. “Parameter Optimization and Compressive Property of the TC31 Titanium Alloy X-Type Lattice Structure by the Superplastic Forming/diffusion Bonding Process.” Archives of Civil and Mechanical Engineering 23 (2): 137. https://doi.org/10.1007/s43452-023-00642-6
• Wu, Zijin, Junjie Gong, Yangdong Chen, Jinrong Wang, Yuanyuan Wei, and Jianhe Gao. 2020. “Springback Prediction of Dieless Forming of AZM120 Sheet Metal Based on Constitutive Model.” Metals 10 (6): 780. https://doi.org/10.3390/met10060780
• Wu, Xin, Gaolei Li, and Yuan Yue. 2025. “Effects of Multiple Freeplay and Nonlinear Damping on the Nonlinear Aeroelastic Response of Wing-Control Surface-Tab System.” Thin-Walled Structures 216: 113710. https://doi.org/10.1016/j.tws.2025.113710
• Wu, Fengyong, Wenchen Xu, Zhongze Yang, Bin Guo, and Debin Shan. 2018. “Study on Hot Press Forming Process of Large Curvilinear Generatrix Workpiece of Ti55 High-Temperature Titanium Alloy.” Metals 8 (10): 827. https://doi.org/10.3390/met8100827
• Wylly, Alexander. 1952. “A Second-Order Solution for an Oscillating Two-Dimensional Supersonic Airfoil.” Journal of the Aeronautical Sciences 19 (10): 685–96. https://doi.org/10.2514/8.2430
• Xiao, Peng, Bing Li, Hong Yang, and Weiming Lu. 2024. “Simulation on Gear Retraction Braking Function of Aircraft Brake System.” In 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae62008.2024.11026566
• Xie, Dan, Min Xu, Honghua Dai, and Earl H. Dowell. 2015b. “Proper Orthogonal Decomposition Method for Analysis of Nonlinear Panel Flutter with Thermal Effects in Supersonic Flow.” Journal of Sound and Vibration 337: 263–83. https://doi.org/10.1016/j.jsv.2014.10.038
• Xieyuan, Yin. 1985. “Roll up of Strake Leading/trailing-Edge Vortex Sheets for Double-Delta Wings.” Journal of Aircraft 22 (1): 87–89. https://doi.org/10.2514/3.45086
• Xu, W. L., C. H. Ma, C. H. Li, and W. J. Feng. 2004b. “Sensitive Factors in Springback Simulation for Sheet Metal Forming.” Journal of Materials Processing Technology 151 (1–3): 217–22. https://doi.org/10.1016/j.jmatprotec.2004.04.044
• Xu, Gene, and Michael West. 1990. “Iterative Algorithm for Correlation of Strain Gauge Data with Aerodynamic Load.” Journal of Aircraft 27 (7): 668–70. https://doi.org/10.2514/3.25338
• Xu, Jinhan, Jun Yan, Yan Huang, and Dawei Ding. 2024. “Simulation and Prediction of Springback in Sheet Metal Bending Process Based on Embedded Control System.” Sensors 24 (23): 7863. https://doi.org/10.3390/s24237863
• Xu, Yanli, Baozeng Yue, Zhengmao Yang, Liangyu Zhao, and Shuxing Yang. 2019b. “Study on the Chaotic Dynamics in Yaw–pitch–roll Coupling of Asymmetric Rolling Projectiles with Nonlinear Aerodynamics.” Nonlinear Dynamics 97 (4): 2739–56. https://doi.org/10.1007/s11071-019-05159-3
• Xu, Shuting, and Zhe Zhang. 2020. “Mechanism Analysis of Smart Cue on Aircraft for Loss of Control Mitigation.” IEEE Access 8: 58522–32. https://doi.org/10.1109/access.2020.2981047
• Xu, Jing-jing, Zhi-wei Zhang, and Yi-min Wu. 2004a. “Application of Data Mining Method to Improve the Accuracy of Springback Prediction in Sheet Metal Forming.” Journal of Shanghai University (English Edition) 8 (3): 348–53. https://doi.org/10.1007/s11741-004-0077-4
• Xue, Cai-Jun, Yu Han, Wen-Gang Qi, and Jian-Hua Dai. 2012a. “Landing-Gear Drop-Test Rig Development and Application for Light Airplanes.” Journal of Aircraft 49 (6): 2064–76. https://doi.org/10.2514/1.c031913
• Xue, Xin, Juan Liao, Gabriela Vincze, and Frédéric Barlat. 2015. “Twist Springback Characteristics of Dual-Phase Steel Sheet after Non-Axisymmetric Deep Drawing.” International Journal of Material Forming 10 (2): 267–78. https://doi.org/10.1007/s12289-015-1275-2
• Xue, David Y., and Chuh Mei. 1993. “Finite Element Nonlinear Panel Flutter with Arbitrary Temperatures in Supersonic Flow.” AIAA Journal 31 (1): 154–62. https://doi.org/10.2514/3.11332
• Yamamoto, Jun, Yoimi Kojima, Masaharu Kameda, Yasushi Watanabe, Atsushi Hashimoto, and Takashi Aoyama. 2020. “Prediction of the Onset of Supersonic Inlet Buzz.” Aerospace Science and Technology 96: 105523. https://doi.org/10.1016/j.ast.2019.105523
• Yan, Chengjun, Qi Wang, Bo Wu, and Lin Huang. 2024. “Flutter Mechanism of a Thin Plate Considering Attack Angles.” Applied Sciences 14 (20): 9380. https://doi.org/10.3390/app14209380
• Yang, Wenhua, Wei Ji, Zhaohui Zhou, et al. 2021. “Analysis of Deformation Behavior and Microstructure Changes for α/β Titanium Alloy at Elevated Temperature.” Metals 11 (2): 303. https://doi.org/10.3390/met11020303
• Yang, Zhao, and Jie Li. 2022. “Numerical Aeroelastic Analysis of a High-Aspect-Ratio Wing Considering Skin Flexibility.” Aerospace 9 (9): 515. https://doi.org/10.3390/aerospace9090515
• Yang, Guowei, Xiyun Lu, Lixian Zhuang, Caroline Weishaupl, and Boris Laschka. 2002. “Nonlinear Analysis of Dynamic Stability and the Prediction of Wing Rock.” Journal of Aircraft 39 (1): 84–90. https://doi.org/10.2514/2.2899
• Yang, Guowei, Shigeru Obayashi, and Jiro Nakamichi. 2003. “Aileron Buzz Simulation Using an Implicit Multiblock Aeroelastic Solver.” Journal of Aircraft 40 (3): 580–89. https://doi.org/10.2514/2.3134
• Yang, Xiaoping, and C. Richard Liu. 1999. “Machining Titanium and Its Alloys.” Machining Science and Technology 3 (1): 107–39. https://doi.org/10.1080/10940349908945686
• Yang, T. Y., and S. H. Sung. 1977. “Finite-Element Panel Flutter in Three-Dimensional Supersonic Unsteady Potential Flow.” AIAA Journal 15 (12): 1677–83. https://doi.org/10.2514/3.7472
• Yang, Hui, Fangyi Wan, and Weimin Cui. 2016a. “Failure Simulation and Identification of Shock Absorber in Carrier-Based Aircraft Landing Gear.” In 2016 IEEE International Conference on Prognostics and Health Management (ICPHM). IEEE. https://doi.org/10.1109/icphm.2016.7542833
• Yang, Chao, YouXu Yang, and ZhiGang Wu. 2012. “Shape Sensitivity Analysis of Flutter Characteristics of a Low Aspect Ratio Supersonic Wing Using Analytical Method.” Science China Technological Sciences 55 (12): 3370–77. https://doi.org/10.1007/s11431-012-4933-3
• Yang, Luo, and Hu Yanguang. 2015. “A Study on Life Monitoring of Landing Gear Based on Weight Parameter and Fatigue Loads Interaction.” In 2015 IEEE Conference on Prognostics and Health Management (PHM). IEEE. https://doi.org/10.1109/icphm.2015.7245048
• Yasmeen, Tabassam, Salaheddin Rahimi, Christopher Hopper, Chi Zhang, and Jun Jiang. 2022. “Unravelling Thermal-Mechanical Effects on Microstructure Evolution under Superplastic Forming Conditions in a near Alpha Titanium Alloy.” Journal of Materials Research and Technology 18: 4285–4302. https://doi.org/10.1016/j.jmrt.2022.04.063
• Yasmeen, Tabassam, Zhutao Shao, Lei Zhao, P. Gao, Jianguo Lin, and Jun Jiang. 2019. “Constitutive Modeling for the Simulation of the Superplastic Forming of TA15 Titanium Alloy.” International Journal of Mechanical Sciences 164: 105178. https://doi.org/10.1016/j.ijmecsci.2019.105178
• Yasmeen, Tabassam, Bing Zhao, Jing-Hua Zheng, Famin Tian, Jianguo Lin, and Jun Jiang. 2020. “The Study of Flow Behavior and Governing Mechanisms of a Titanium Alloy during Superplastic Forming.” Materials Science and Engineering: A 788: 139482. https://doi.org/10.1016/j.msea.2020.139482
• 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, E. Carson, Eleanor C. Wynne, and Moses G. Farmer. 1983. “Effects of Angle of Attack on Transonic Flutter of a Supercritical Wing.” Journal of Aircraft 20 (10): 841–47. https://doi.org/10.2514/3.44952
• Yates, E. Carson, Eleanor C. Wynne, Moses G. Farmer, and Robert N. Desmarais. 1982b. “Prediction of Transonic Flutter for a Supercritical Wing by Modifiedstrip Analysis.” Journal of Aircraft 19 (11): 999–1004. https://doi.org/10.2514/3.44803
• Ye, Liu-qing, Kun Ye, Ke Jin, Yi-fan Zhang, and Zheng-yin Ye. 2024. “Mechanism of Single-Mode Panel Flutter in Low Supersonic Flow.” Aerospace Science and Technology 147: 109002. https://doi.org/10.1016/j.ast.2024.109002
• Yildiz, Anil, M. Ugur Akcal, Batuhan Hostas, and N. Kemal Ure. 2019. “Switching Control Architecture with Parametric Optimization for Aircraft Upset Recovery.” Journal of Guidance, Control, and Dynamics 42 (9): 2055–68. https://doi.org/10.2514/1.g004180
• Yoo, Jae-Han, Dong-Hyun Kim, and In Lee. 2002. “Angle-of-Attack Effect on Transonic/Supersonic Aeroelasticity of Wing-Box Model.” Journal of Aircraft 39 (5): 906–8. https://doi.org/10.2514/2.3017
• Yoon, NamKyung, ChanHoon Chung, Young-Ho Na, and SangJoon Shin. 2012. “Control Reversal and Torsional Divergence Analysis for a High-Aspect-Ratio Wing.” Journal of Mechanical Science and Technology 26 (12): 3921–31. https://doi.org/10.1007/s12206-012-0889-2
• Yoon, Jeong-Whan, Farhang Pourboghrat, Kwansoo Chung, and Dong-Yol Yang. 2002. “Springback Prediction for Sheet Metal Forming Process Using a 3D Hybrid Membrane/shell Method.” International Journal of Mechanical Sciences 44 (10): 2133–53. https://doi.org/10.1016/s0020-7403(02)00165-0
• 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, Kwanghyun, Hyunsung Choi, Jiwoong Ha, and Jeong Whan Yoon. 2023. “Bauschinger Effect Calibration by the Different Types of Loading/reverse Loading Tests for Springback Prediction in Sheet Metal Forming.” International Journal of Material Forming 16 (2): 16. https://doi.org/10.1007/s12289-023-01738-3
• Yu, Zonghan, Guoping Huang, Ruilin Wang, and Omer Musa. 2021. “Spillage-Adaptive Fixed-Geometry Bump Inlet of Wide Speed Range.” Aerospace 8 (11): 340. https://doi.org/10.3390/aerospace8110340
• Yu, Zhefeng, Xiaochuan Liu, Jizhen Wang, Qingwen You, and Yi Fu. 2020. “Shock Absorber with Inward-Folding Composite Tube and Its Application in Legged Landing Gear.” International Journal of Crashworthiness 26 (4): 388–403. https://doi.org/10.1080/13588265.2020.1718463
• Yuan, Hao, Jiaqing Kou, Chuanqiang Gao, and Weiwei Zhang. 2024. “Resolvent Analysis for Flutter Boundary Prediction in Transonic Flow.” AIAA Journal 62 (8): 3191–95. https://doi.org/10.2514/1.j064214
• Yuen, W. Y. D. 1990. “Springback in the Stretch-Bending of Sheet Metal with Non-Uniform Deformation.” Journal of Materials Processing Technology 22 (1): 1–20. https://doi.org/10.1016/0924-0136(90)90138-k
• Zammit-Mangion, David, and Martin Eshelby. 2008. “Simplified Algorithm to Model Aircraft Acceleration during Takeoff.” Journal of Aircraft 45 (4): 1090–97. https://doi.org/10.2514/1.22966
• Zedan, M. F., and K. Abu-Abdou. 1988. “Improved Thin-Airfoil Theory.” Journal of Aircraft 25 (12): 1122–28. https://doi.org/10.2514/3.45711
• Zha, Ge-Cheng, Doyle Knight, and Donald Smith. 1998a. “Investigations of High-Speed Civil Transport Inlet Unstart at Angle of Attack.” Journal of Aircraft 35 (6): 851–56. https://doi.org/10.2514/2.2404
• Zhang, Yufei, Haixin Chen, Song Fu, Miao Zhang, and Meihong Zhang. 2015a. “Drag Prediction Method of Powered-on Civil Aircraft Based on Thrust Drag Bookkeeping.” Chinese Journal of Aeronautics 28 (4): 1023–33. https://doi.org/10.1016/j.cja.2015.06.015
• Zhang, Yanwei, and Guohua Cui. 2009. “Finite Element Simulation of Springback in Sheet Metal Bending.” In 2009 International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2009.5363262
• Zhang, Bocheng, Weilong Ding, Shengcheng Ji, and Jiazhen Zhang. 2016c. “Transonic Flutter Analysis of an AGARD 445.6 Wing in the Frequency Domain Using the Euler Method.” Engineering Applications of Computational Fluid Mechanics 10 (1): 243–54. https://doi.org/10.1080/19942060.2016.1152200
• Zhang, Xiao, Jie Gao, Lin Wang, and Liang Gao. 2026b. “Flutter Boundary Prediction of Supersonic Plates under Yawed Flow Using a Thickness-Adaptive Isogeometric Framework.” Thin-Walled Structures 231: 115590. https://doi.org/10.1016/j.tws.2026.115590
• Zhang, Lilei, Zhipeng Huang, Chengwei Fu, Yuepeng Xu, Yunhe Wang, and Xiangdong Kong. 2021a. “Design and Verification of Two-Stage Brake Pressure Servo Valve for Aircraft Brake System.” Processes 9 (6): 979. https://doi.org/10.3390/pr9060979
• Zhang, Sheng, Li Ji, Wei-qi Qian, and Kai-feng He. 2019. “Aircraft Post-Stall Maneuver Control Using Attitude Feedback Linearization.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866476
• Zhang, Zhuogeng, Hongli Ji, Chongcong Tao, Jinhao Qiu, and Li Cheng. 2024c. “Suppression of Panel Flutter in Supersonic Flow Based on Acoustic Black Hole as a Linear Energy Sink.” Journal of Sound and Vibration 571: 118030. https://doi.org/10.1016/j.jsv.2023.118030
• Zhang, Ying, Zhengrong Jin, Long Wang, Kaixin Zheng, and Wantao Jia. 2024b. “Stochastic Dynamics of Aircraft Ground Taxiing via Improved Physics-Informed Neural Networks.” Nonlinear Dynamics 112 (5): 3163–78. https://doi.org/10.1007/s11071-023-09173-4
• Zhang, Dehai, Yanqin Li, Jianxiu Liu, Guizhong Xie, and Erwei Su. 2016a. “A Novel 3D Optical Method for Measuring and Evaluating Springback in Sheet Metal Forming Process.” Measurement 92: 303–17. https://doi.org/10.1016/j.measurement.2016.06.032
• Zhang, Tuoyang, Yong Liu, Daniel G. Sanders, Bin Liu, Weidong Zhang, and Canxu Zhou. 2014a. “Development of Fine-Grain Size Titanium 6Al–4V Alloy Sheet Material for Low Temperature Superplastic Forming.” Materials Science and Engineering: A 608: 265–72. https://doi.org/10.1016/j.msea.2014.04.098
• Zhang, Chong, and Yanshan Lou. 2024. “Influences of the Evolving Plastic Behavior of Sheet Metal on V-Bending and Springback Analysis Considering Different Stress States.” International Journal of Plasticity 173: 103889. https://doi.org/10.1016/j.ijplas.2024.103889
• Zhang, Yaqian, and Shufeng Lu. 2026. “Dynamic Behaviors and Experimental Research of Variable-Section Low-Aspect-Ratio Wing Structures.” Journal of Vibration Engineering & Technologies 14 (7): 483. https://doi.org/10.1007/s42417-026-02704-4
• Zhang, Mingjie, Wufei Si, and Cunbiao Lee. 2021b. “Heat Transfer and Recovery Factor of Aerodynamic Heating on a Flared Cone.” AIAA Journal 59 (11): 4284–92. https://doi.org/10.2514/1.j060937
• Zhang, Yue, Hui-Jun Tan, Jie-Feng Li, Hao Chen, and Chenxi Wang. 2018. “Ramp Shock Regulation of Supersonic Inlet with Shape Memory Alloy Plate.” AIAA Journal 56 (4): 1696–1702. https://doi.org/10.2514/1.j056318
• Zhang, Tao, Jianchao Xia, Xiuquan Han, et al. 2024a. “Deformation Control of TC4 Titanium Alloy in Thin-Walled Hyperbolic Structures during Hot Forming Processes.” Materials 17 (24): 6146. https://doi.org/10.3390/ma17246146
• Zhang, Zijian, Min Xu, and Shilu Chen. 2008a. “Active Flutter Control of Transonic Flapped Wing Based on CFD/CSD Coupling.” In 2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing. IEEE. https://doi.org/10.1109/asc-icsc.2008.4675399
• Zhang, Songyang, Qiaozhi Yin, Xiaohui Wei, Jiayi Song, and Hong Nie. 2022. “Study of Brake Disc Friction Characteristics Effect on Low Frequency Brake Induced Vibration of Aircraft Landing Gear.” Aerospace 9 (12): 809. https://doi.org/10.3390/aerospace9120809
• Zhang, Zixuan, Huan Zhang, Yi Shi, et al. 2016b. “Springback Reduction by Annealing for Incremental Sheet Forming.” Procedia Manufacturing 5: 696–706. https://doi.org/10.1016/j.promfg.2016.08.057
• Zhang, Hang, Shengxi Zhou, and C. W. Lim. 2026c. “Flutter Suppression of a Heated Panel in Supersonic Airflow Using Energy Harvesters.” AIAA Journal 64 (10): 5936–53. https://doi.org/10.2514/1.j066769
• Zhanqi, Fan, and Liu Lin Xi’an. 2012. “The High Angle of Attack Aerodynamic Modeling and Nonlinear Dynamic Inversion Flight Control Law Design.” In IEEE 10th International Conference on Industrial Informatics. IEEE. https://doi.org/10.1109/indin.2012.6300870
• Zhao, Xuwen, Maolin Cai, Peng Shi, Zirui Li, Dongjiang Han, and Xiaomeng Tong. 2026b. “Intelligent Method Combining Models and Process Data for Springback Prediction in Sheet Metal Stamping.” Engineering Applications of Artificial Intelligence 173: 114327. https://doi.org/10.1016/j.engappai.2026.114327
• Zhao, Xiajun, Yazhi Li, Zhaoxin Yun, and Wei Zhang. 2024. “Investigation on Flight Load Calibration of Aircraft Composite Wing Base on Strain Gauge Measurement.” Theoretical and Applied Mechanics Letters 14 (5): 100540. https://doi.org/10.1016/j.taml.2024.100540
• Zhao, Xiaojia, Hongyu Qiao, and Shuanghou Deng. 2026a. “Conceptual Design Methodology for Airbreathing Horizontal Takeoff-and-Landing High-Mach Aircraft.” Journal of Aircraft: 1–13. https://doi.org/10.2514/1.c038671
• Zhao, Yue, and J. Jim Zhu. 2016a. “Aircraft Loss-of-Control Arrest Autopilot Using Trajectory Linearization Control.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7525145
• Zhao, Yue, and J. Jim Zhu. 2016b. “Aircraft Loss-of-Control Autonomous Recovery: Mission Trajectory Tracking Restoration.” In 2016 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2016.7502671
• Zhao, Xiang, Yongfeng Zhu, and Sijun Zhang. 2012b. “Transonic Wing Flutter Predictions by a Loosely-Coupled Method.” Computers & Fluids 58: 45–62. https://doi.org/10.1016/j.compfluid.2012.01.002
• Zheng, Guoyong. 2010. “Nonlinear Aeroelastic Analysis of a Two-Dimensional Wing with Control Surface in Supersonic Flow.” Acta Mechanica Sinica 26 (3): 401–7. https://doi.org/10.1007/s10409-009-0328-5
• Zheng, Wuji, Yinghui Li, Dengcheng Zhang, Chi Zhou, and Pengwei Wu. 2018. “Envelope Protection for Aircraft Encountering Upset Condition Based on Dynamic Envelope Enlargement.” Chinese Journal of Aeronautics 31 (7): 1461–69. https://doi.org/10.1016/j.cja.2018.05.006
• Zheng, Guoyong, and Yiren Yang. 2008. “Chaotic Motions and Limit Cycle Flutter of Two-Dimensional Wing in Supersonic Flow.” Acta Mechanica Solida Sinica 21 (5): 441–48. https://doi.org/10.1007/s10338-008-0853-y
• Zhong, Jiaxiang, Feng Qu, Di Sun, et al. 2023. “Numerical Investigation of the Unstart Flow at off-Design Condition of REST Inlet at a Mach of 4.” Aerospace Science and Technology 136: 108232. https://doi.org/10.1016/j.ast.2023.108232
• Zhou, Kai, Xiuchang Huang, Zhenguo Zhang, and Hongxing Hua. 2018. “Aero-Thermo-Elastic Flutter Analysis of Coupled Plate Structures in Supersonic Flow with General Boundary Conditions.” Journal of Sound and Vibration 430: 36–58. https://doi.org/10.1016/j.jsv.2018.05.035
• Zhou, R. C., Chuh Mei, and Jen-Kuang Huang. 1996. “Suppression of Nonlinear Panel Flutter at Supersonic Speeds and Elevated Temperatures.” AIAA Journal 34 (2): 347–54. https://doi.org/10.2514/3.13070
• Zhou, Tao, and Yunpeng Wu. 2025. “Research on Trailing Cone Calibration Flight Test Technology.” In 2025 International Conference of Mechanical Engineering on Aerospace (CoMEA). IEEE. https://doi.org/10.1109/comea66280.2025.11241952
• Zhou, Jian, Minglong Xu, Zhichun Yang, and Yingsong Gu. 2021b. “Suppression of Panel Flutter Response in Supersonic Airflow Using a Nonlinear Vibration Absorber.” International Journal of Non-Linear Mechanics 133: 103714. https://doi.org/10.1016/j.ijnonlinmec.2021.103714
• Zhou, Hang, Lingyu Yang, Jing Zhang, and Xiaoke Yang. 2017. “Online Learning and Inference Based Flight Envelope Estimation for Aircraft Loss-of-Control Prevention.” In 2017 13th IEEE International Conference on Control & Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2017.8003042
• Zhu, Yongkai, Jiawei Liu, Rui Li, Ziyu Wang, and Haitao Wang. 2026. “Integrated Fiber-Optic Sensing and Deep Learning for Supersonic Inlet Flow Reconstruction and Buzz Diagnosis.” IEEE Sensors Journal 26 (18): 27402–15. https://doi.org/10.1109/jsen.2026.3720626
• Zhu, Jianfeng, Wenguo Luo, Yuqing Wei, Cheng Yan, and Yancheng You. 2020. “Acoustic Modeling and Vibration Characteristics of Supersonic Inlet Buzz.” Energies 13 (8): 2048. https://doi.org/10.3390/en13082048
• Zhu, Yuan-Cheng, Guo-Feng Yao, Min Wang, Kui-Yang Gao, and Qi Hou. 2022. “A New Pre-Stretching Method to Increase Critical Flutter Dynamic Pressure of Heated Panel in Supersonic Airflow.” Mathematics 10 (23): 4506. https://doi.org/10.3390/math10234506
• Zink, P. Scott, Dimitri N. Mavris, and Daniella E. Raveh. 2001. “Maneuver Trim Optimization Techniques for Active Aeroelastic Wings.” Journal of Aircraft 38 (6): 1139–46. https://doi.org/10.2514/2.2884
• Zink, P. Scott, Daniella E. Raveh, and Dimitri N. Mavris. 2004. “Robust Structural Design of an Active Aeroelastic Wing with Maneuver Load Inaccuracies.” Journal of Aircraft 41 (3): 585–93. https://doi.org/10.2514/1.64
• Zohar, Y., and J. Er-El. 1988. “Influence of the Aspect Ratio on the Aerodynamics of the Delta Wing at High Angle of Attack.” Journal of Aircraft 25 (3): 200–205. https://doi.org/10.2514/3.45578
• Zuo, Fengyuan, Guoping Huang, and Chen Xia. 2016. “Investigation of Internal-Waverider-Inlet Flow Pattern Integrated with Variable-Geometry for TBCC.” Aerospace Science and Technology 59: 69–77. https://doi.org/10.1016/j.ast.2016.10.009

Primary Sources, Non-Peer-Reviewed

• “2-D Prototypical Aeroelastic Wing Section with Structural Nonlinearity.” 2013. In Automation and Control Engineering. CRC Press. https://doi.org/10.1201/b15376-18
• “2-D Prototypical Aeroelastic Wing Section with Structural Nonlinearity.” 2018. In Tensor Product Model Transformation in Polytopic Model-Based Control. CRC Press. https://doi.org/10.1201/9781315218045-20
• “3-D Prototypical Aeroelastic Wing Section with Structural Nonlinearity.” 2013. In Automation and Control Engineering. CRC Press. https://doi.org/10.1201/b15376-19
• “3-D Prototypical Aeroelastic Wing Section with Structural Nonlinearity.” 2018. In Tensor Product Model Transformation in Polytopic Model-Based Control. CRC Press. https://doi.org/10.1201/9781315218045-21
• “3. Supersonic Two-Dimensional Airfoil Theory: Surface Pressures.” 1960a. In Higher Approximations in Aerodynamic Theory. Princeton University Press. https://doi.org/10.1515/9781400877706-004
• “4. Supersonic Two-Dimensional Airfoil Theory: Complete Flow Pattern.” 1960b. In Higher Approximations in Aerodynamic Theory. Princeton University Press. https://doi.org/10.1515/9781400877706-005
• “5. Supersonic Two-Dimensional Airfoil Theory: Influence of a Blunt Leading Edge.” 1960c. In Higher Approximations in Aerodynamic Theory. Princeton University Press. https://doi.org/10.1515/9781400877706-006
• “8. Supersonic Three-Dimensional Wing Theory.” 1960. In Higher Approximations in Aerodynamic Theory. Princeton University Press. https://doi.org/10.1515/9781400877706-009
• A-4 Aircraft Instruments Committee. 2020. Flight Test Procedures for Static Pressure Systems Installed in Subsonic Transport Aircraft. https://doi.org/10.4271/arp921b
• A-5 Aerospace Landing Gear Systems Committee. 1993. Aircraft Flotation Analysis Methods. https://doi.org/10.4271/arp1821
• A-5 Aerospace Landing Gear Systems Committee. 2008. Landing Area/Landing Gear Compatibility: A Brief History of SAE/Corps of Engineers Cooperation. https://doi.org/10.4271/air4243
• A-5 Aerospace Landing Gear Systems Committee. 2009. Aircraft Tire Condition Monitoring Systems. https://doi.org/10.4271/air4830
• A-5 Aerospace Landing Gear Systems Committee. 2010. Landing Gear System Development Plan. https://doi.org/10.4271/arp1598a
• A-5 Aerospace Landing Gear Systems Committee. 2012. Aerospace Landing Gear: FAA Regulatory History: Airplane Wheels, Tires, and Brakes. https://doi.org/10.4271/air5697a
• A-5 Aerospace Landing Gear Systems Committee. 2016a. Aircraft Ground Flotation Analysis Methods. https://doi.org/10.4271/arp1821a
• A-5 Aerospace Landing Gear Systems Committee. 2016b. Landing Gear Alignment. https://doi.org/10.4271/air5556
• A-5 Aerospace Landing Gear Systems Committee. 2017a. Aircraft Flotation Analysis. https://doi.org/10.4271/air1780a
• A-5 Aerospace Landing Gear Systems Committee. 2017b. Aircraft Tire Pressure Monitoring Systems. https://doi.org/10.4271/air4830a
• A-5 Aerospace Landing Gear Systems Committee. 2017c. A Guide to Landing Gear System Integration. https://doi.org/10.4271/air5451a
• A-5 Aerospace Landing Gear Systems Committee. 2017d. Tire Pressure Monitoring Systems (TPMS) for Aircraft. https://doi.org/10.4271/arp6137
• A-5 Aerospace Landing Gear Systems Committee. 2021. Overview of Aircraft Landing Gear Shimmy Analysis Methods. https://doi.org/10.4271/air6280
• A-5 Aerospace Landing Gear Systems Committee. 2022. Effects of Extremely Cold Temperature on Landing Gear Operation. https://doi.org/10.4271/air6411
• A-5 Aerospace Landing Gear Systems Committee. 2025. Landing Gear Stability. https://doi.org/10.4271/air4894a
• A-5C Aircraft Tires Committee. n.d. History of Commercial Aircraft New Tire Qualification Testing. SAE International. https://doi.org/10.4271/air5651
• A-5C Aircraft Tires Committee. 2007a. Aircraft Tire Retreading Practice: Bias and Radial. https://doi.org/10.4271/arp4834
• A-5C Aircraft Tires Committee. 2007b. Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires. https://doi.org/10.4271/arp4955
• A-5C Aircraft Tires Committee. 2014. Aircraft Tire Inspection: In-Service Removal Criteria. https://doi.org/10.4271/arp6225
• A-5C Aircraft Tires Committee. 2016. Aircraft Tire Electrical Resistance Test. https://doi.org/10.4271/arp6404
• A-5C Aircraft Tires Committee. 2017a. Aircraft New Tire Standard: Bias and Radial. https://doi.org/10.4271/as4833a
• A-5C Aircraft Tires Committee. 2017b. Aircraft Tire History. https://doi.org/10.4271/air5487b
• A-5C Aircraft Tires Committee. 2017c. Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires. https://doi.org/10.4271/arp4955a
• A-5C Aircraft Tires Committee. 2018. Aircraft Tire Wear Profile Development and Execution for Laboratory Testing. https://doi.org/10.4271/air5797a
• A-5C Aircraft Tires Committee. 2024. Aircraft Tire-to-Wheel Performance Characteristics. https://doi.org/10.4271/arp5507a
• “A380 Landing Gear Test Build.” 2002. Aircraft Engineering and Aerospace Technology 74 (4). https://doi.org/10.1108/aeat.2002.12774dab.034
• Aarnes, M., and J. White. 1975a. “Propulsion System and Airframe Structural Integration Analysis.” In 11th Propulsion Conference. AIAA 1975-1310. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1310
• Aaron, V., A. H. Adibi-Sedeh, and B. Bahr. 2004. “Optimization Analysis of Maximum Energy Absorption Properties of Metallic Honeycomb and an Application in Designing Arresting Mechanism for Landing Gear Drop Testing.” In Applied Mechanics. ASMEDC. https://doi.org/10.1115/imece2004-59791
• Abbas, Mohammad, and David W. Riggins. 2016. “Exergy-Based Performance Analysis of a Turbojet Engine.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-4638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4638
• Abbas Jessam, Raed. 2012. “Effect of Moment of Inertia and Aerodynamics Parameters onAerodynamic Coupling in Roll Mode.” Engineering and Technology Journal 30 (7): 1222–39. https://doi.org/10.30684/etj.30.7.10
• Abbate, Gregg, and Claude Berner. 1994. “Wind Tunnel Measurements of Wrap around Fins at Mach 2.06.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3499
• Abbott, J. M., and D. A. Dietrich. 1977. Aerodynamic and Directional Acoustic Performance of a Scoop Inlet. NASA-TP-1028. NASA. https://ntrs.nasa.gov/citations/19770024208
• Abdel-Motagaly, Khaled, Bin Duan, and Chuh Mei. 2003. “Active Control of Nonlinear Panel Flutter under Yawed Supersonic Flow.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1514
• Abdelhamid, O. 1985. “Aerodynamic Characteristics of Quasi-Slender Wing: Body Combinations at Supersonic Velocities.” International Conference on Aerospace Sciences and Aviation Technology 1 (CONFERENCE): 1–9. https://doi.org/10.21608/asat.1985.26464
• Abdulhamitbilal, Erkan, Sinan Şal, and Elbrous M. Jafarov. 2022. “Identification and Stability Analysis of a Turbojet Engine in Start-Up Mode.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2022-77985
• Abdullah, Nur Azam, Erwin Sulaeman, and Meor Iqram Meor Ahmad. 2022. “LCO Flutter Instability on Oscillating Supersonic Wing by Means of Linearized Aerodynamic Small Disturbance Theory.” In Structural Integrity. Springer International Publishing. https://doi.org/10.1007/978-3-030-85646-5_2
• Abed, Eyad H. n.d. “Nonlinear Stabilizing Control of High Angle of Attack Flight Dynamics.” In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0043264
• Abed, Eyad. 1989. “Nonlinear Stabilizing Control of High Angle of Attack Flight Dynamics.” In Guidance, Navigation and Control Conference. AIAA 1989-3487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3487
• Abele, Eberhard, and Roland Hölscher. 2013. “New Technology for High Speed Cutting of Titanium Alloys.” In Lecture Notes in Production Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-319-01964-2_11
• Abou-Amer, S. 2020a. “Damping Material for Stabilization of Panel Flutter at High Supersonic Speed.” MEJ. Mansoura Engineering Journal 33 (1): 41–53. https://doi.org/10.21608/bfemu.2020.126840
• Abou-Amer, S. A. 2020b. “Panel Flutter Control at High Supersonic Speed Using Piezoelectric Material (Dept.M).” MEJ. Mansoura Engineering Journal 33 (1): 29–40. https://doi.org/10.21608/bfemu.2020.126833
• Abou-Amer, S., A. Dahshan, and M. El Nomrossy. 2020. “Nonlinear Panel Flutter Analysis at High Supersonic Speed (Dept.M).” MEJ. Mansoura Engineering Journal 32 (2): 21–36. https://doi.org/10.21608/bfemu.2020.128541
• Abraham, Troy, Douglas F. Hunsaker, and David S. Lazzara. 2023. “Multi-Fidelity Comparison of Supersonic Wave Drag Prediction Methods Using Axisymmetric Bodies.” In AIAA SCITECH 2023 Forum. AIAA 2023-1899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1899
• Abraham-Doman, Shazad, and Craig G. Merrett. 2014. “Development of a Flight Data System and Experimental Determination of Aerodynamic Loads on a Wing Spar.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0194
• 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
• Abu-Akeel, A. 1968. “Damping of High Frequency Brake Vibrations in Aircraft Landing Gear.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-312
• Abu-Farha, F., and R. Curtis. 2011. “Standards for Superplastic Forming of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.1.34
• Abzug, Malcolm. 1999b. “An Unconventional Tricycle Landing Gear.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4018
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-a. “The Discovery of Inertial Coupling.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.010
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-b. “Early Developments in Stability and Control.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.003
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-c. “The Elastic Airplane.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.021
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-d. “Flying Qualities Becomes a Science.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.005
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-e. “Flying Qualities Research Moves with the Times.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.023
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-f. “High Mach Number Difficulties.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.013
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-g. “Power Effects on Stability and Control.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.006
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-h. “Stability and Control at the Design Stage.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.008
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-i. “Stability and Control Issues with Variable Sweep.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.018
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-j. “Stability Augmentation.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.022
• Abzug, Malcolm J., and E. Eugene Larrabee. n.d.-k. “Tactical Airplane Maneuverability.” In Airplane Stability and Control, Second Edition. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141.012
• “Accelerated Flight Performance.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.009
• Ackeret, J. 1925. Air Forces on Airfoils Moving Faster than Sound. NACA-TM-317. NASA. https://ntrs.nasa.gov/citations/19930087085
• Adams, J. 1972. “An Analysis of Aircraft Lateral-Directional Handling Qualities Using Pilot Models.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-962. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-962
• 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
• Adams, J., Jr., W. Martindale, and M. Varner. 1984. “One-Dimensional Unsteady Modeling of Supersonic Inlet Unstart/restart.” In 22nd Aerospace Sciences Meeting. AIAA 1984-439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-439
• Adamson, D., and William B. Boatright. 1950. Investigation of Downwash, Sidewash, and Mach Number Distribution behind a Rectangular Wing at a Mach Number of 2.41. NACA-RM-L50G12. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20090021561
• Adamson, David, and William B. Boatright. 1957. Investigation of Downwash, Sidewash, and Mach Number Distribution behind a Rectangular Wing at a Mach Number of 2.41. NACA-TR-1340. NASA. https://ntrs.nasa.gov/citations/19930092328
• Addendum 3 Lateral Control and Stability Surfaces. 2000. Wiley. https://doi.org/10.1002/9781118903094.oth3
• Adrion, Harold O. 1951. “Installation Experience with Turbojet Afterburner Power Plants.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/510135
• Advanced Fuel Research INC East Hartford CT. 1957. Handbook of Supersonic Aerodynamics. Volume 3. Defense Technical Information Center. https://doi.org/10.21236/ada390317
• Advisory Group for Aerospace Research and Development. 1984. Flight Test Techniques. AD-A147625. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19840026325
• Adzman, Muhd Safaadzudin, and Ahmad Zakaria. 2014. “Springback-Free Sheet Metal Structural Part Design by Topography Optimization.” Applied Mechanics and Materials 606: 171–75. https://doi.org/10.4028/www.scientific.net/amm.606.171
• Ae-6 Starting Systems and Auxiliary Power Committee. 1963. A Means of Testing Turbojet Engine Starter Performance. https://doi.org/10.4271/arp715
• “AERO-ENGINE DEVELOPMENT.” 1940. Aircraft Engineering and Aerospace Technology 12 (7): 193–193. https://doi.org/10.1108/eb030661
• Aerodynamic and Landing Measurements Obtained during the First Powered Flight of the North American X-15 Research Airplane. 1960. NASA-TM-X-269. NASA. https://ntrs.nasa.gov/citations/19980228350
• “Aerodynamic and Static Aeroelastic Analysis of a Transonic Wing Using Hybrid Unstructured Flow Solver.” 2014. In International conference on Innovative Engineering Technologies (ICIET’2014) Dec. 28-29, 2014 Bangkok (Thailand). International Institute of Engineers. https://doi.org/10.15242/iie.e1214053
• Aerodynamic Phenomena in Supersonic Flow. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch4
• “Aerodynamics in the Age of the Jet Airplane.” 1997. In A History of Aerodynamics. Cambridge University Press. https://doi.org/10.1017/cbo9780511607158.011
• Aeroelasticity and Loads Models. 2014. Wiley. https://doi.org/10.1002/9781118700440.ch21
• Afzal, Abdul Ahad, and Muhammad Muneeb Safdar. 2020. “Comparative Analysis of a Diverterless Supersonic Inlet and Its Proposed Modified Geometry Using Computational Fluid Dynamics.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3773. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3773
• Agrawal, Shreekant, Tom A. Kinard, and Arthur G. Powel. 1989. “Supersonic Boundary Layer Stability Analysis with and without Suction on Aircraft Wings.” In Symposium on Numerical and Physical Aspects of Aerodynamic Flows. https://ntrs.nasa.gov/citations/19900029737
• Ahmed, N. A. 2004. “Demonstration of the Effectiveness and Limitations of Thin Airfoil Theory in the Aerodynamic Study of Airfoil Characteristics.” International Journal of Mechanical Engineering Education 32 (4): 271–82. https://doi.org/10.7227/ijmee.32.4.1
• Ahmed, Anwar, and John Worley. 2008. “Yaw-Roll Coupled Oscillations of a Slender Delta Wing.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-366
• 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. 1948. Flight Determination of Wing and Tail Loads on a Fighter-Type Airplane by Means of Strain-Gage Measurements. NACA-TN-1729. NASA. https://ntrs.nasa.gov/citations/19930082423
• 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 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 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 II. Flying Qualities Phase. Chapter 7: Lateral-Directional Static Stability. Defense Technical Information Center. https://doi.org/10.21236/ada319978
• 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. 1991. 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. 1993. Volume IV. Flight Test Management. Chapter 5A. Instrumentation Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada320063
• Aircraft, S-7 Flight Deck Handling Qualities Stds for Trans. 2016. Loss-of-Control Mishaps in Revenue Airline Service. https://doi.org/10.4271/air6237
• Aircraft and Flight Test Instrumentation. 2021. Wiley. https://doi.org/10.1002/9781118949818.ch3
• “Aircraft Construction: Aluminium, Titanium or Steel?” 2008. Aircraft Engineering and Aerospace Technology 80 (2). https://doi.org/10.1108/aeat.2008.12780bab.002
• Aircraft Engine Efficiency and Thrust Measures. 2018. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105173.0653.0664
• “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 Internal Loads. 2014. Wiley. https://doi.org/10.1002/9781118700440.ch16
• “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 Moments of Inertia.” 1996. In Performance and Stability of Aircraft. Elsevier. https://doi.org/10.1016/b978-034063170-6/50016-5
• “Aircraft Non-Linear Dynamics: Equations of Motion.” 2014. In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/b17346-8
• “Aircraft Response Transfer Functions Referred to Aircraft Body Axes.” 1997. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-340-63200-0.50020-4
• “Aircraft Response Transfer Functions Referred to Aircraft Body Axes.” 2013. In Flight Dynamics Principles. Elsevier. https://doi.org/10.1016/b978-0-08-098242-7.00026-2
• “Aircraft Stability and Control.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.010
• “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 Wing Rock in High-Angle-of-Attack Flight.” 2010. In Multiple Scales Theory and Aerospace Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867644.0329.0351
• “Aircraft/Engine System Constraint Analysis.” 2018. In Aircraft Engine Design, Third Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105173.0023.0066
• “Aircraft/Engine System Mission Analysis.” 2018. In Aircraft Engine Design, Third Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105173.0067.0116
• “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
• “Airframe Equations of Motion.” 1998. In Introduction to Aircraft Flight Dynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862052.0093.0118
• “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
• “Airplane Trim.” 2012. In Advanced Aircraft Flight Performance. Cambridge University Press. https://doi.org/10.1017/cbo9781139161893.010
• “Airplane Trim.” 2022. In Advanced Aircraft Flight Performance. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624106408.0223.0240
• Akaryildiz, Bora, Resit Demirkiran, Omer Ozyilmaz, and Muhammed Emin Tanis. 2024. “Scale Factor Oriented Control Parameters Tuning Procedure for Dynamically Scaled Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-2876. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2876
• Akbas, Mustafa, Onder Altuntas, and Arif Hepbasli. 2026. “Investigating the Sectional Thrust and Exergy Efficiency of a Turbojet Engine.” International Journal of Exergy 49 (3): 10075252. https://doi.org/10.1504/ijex.2026.10075252
• Akshayraj, N., and B. V. N. Ramakumar. 2023. “Design and Optimization of Wing Internal Structure to Study the Flutter Frequency of Aircraft Wing.” International Journal of Vehicle Structures and Systems 15 (1). https://doi.org/10.4273/ijvss.15.1.14
• Akshayraj, N., and A. T. Sriram. 2022. “Effect of Wing Geometric Parameters on Flutter Speed.” International Journal of Vehicle Structures and Systems 14 (1). https://doi.org/10.4273/ijvss.14.1.25
• Al-Amari, Farah, Marwa Kaeber, and Saleh Alkhodari. 2022. “Mathematical Modelling and Performance Evaluation of the CM14 Turbojet Engine.” Journal of Engineering Research (Libya) 34: 1–16. https://doi.org/10.66411/jer.v34i.56
• Alag, G., J. Burken, and G. Gilyard. 1986a. “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. S., R. W. Kempel, J. W. Pahle, J. J. Bresina, and F. Bartoli. 1986b. “Model-Following Control for an Oblique-Wing Aircraft.” In AIAA Conference on Guidance and Control. https://ntrs.nasa.gov/citations/19860020395
• Albert Storace, P. E. 2023. “Airplane Maneuvers.” In The Physics of Flight. CRC Press. https://doi.org/10.1201/9781003390916-6
• Alberto Misté, Gianluigi, and Ernesto Benini. 2014. “Turbojet Engine Performance Tuning with a New Map Adaptation Concept.” Journal of Engineering for Gas Turbines and Power 136 (7): 071202. https://doi.org/10.1115/1.4026548
• Albertson, Tp, Rr Stephens, and Td Bayha. 1997. “Fatigue Crack Growth of Two Advanced Titanium Alloys at Room and Elevated Temperature.” In Elevated Temperature Effects on Fatigue and Fracture. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp16322s
• Alcorta, Roberto, Benjamin Chouvion, Guilhem Michon, and Olivier Montagnier. 2023. “On the Use of Frictional Dampers for Flutter Mitigation of a Highly Flexible Wing.” Preprint, . https://doi.org/10.2139/ssrn.4412811
• Alendar, A. D., A. N. Grunin, A. A. Evstigneev, A. I. Lanshin, and M. V. Siluyanova. 2022. “Influence of Inlet Pressure Distortion on the Engine Performance of a Supersonic Passenger Aircraft.” Russian Engineering Research 42 (7): 705–9. https://doi.org/10.3103/s1068798x2207005x
• Alexander, Sidney R. 1948. Flight Investigation to Determine the Aerodynamic Characteristics of Rocket-Powered Models Representative of a Fighter-Type Airplane Configuration Incorporating an Inverse-Taper Wing and a Vee Tail. NACA-RM-L8G29. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20010062506
• Alexander, William E. 1970. A Transducer for Controlling Simulated Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0875525
• Alexander, A. J. 1971. “Correlation of Total Lift Data for Thin, Sharp-Edged, Low-Aspect-Ratio Delta Wings at Low Speeds.” Aeronautical Journal 75 (728): 569–70. https://doi.org/10.1017/s0001924000046145
• Alford, J. S., D. P. Davies, and L. C. Young. 1962. “Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/620300
• Alford, J. S., and H. P. Durand. 1964. “Application of Dynamic Simulation Techniques to Engine-Inlet Compatibility Problems on the SST.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/640304
• 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
• Alford, W. J., Jr., R. P. Bielet, and A. W. Robins. 1966. The Transonic Aerodynamic Characteristics of Two Variable-Sweep Airplane Configurations Capable of Low-Level Supersonic Attack. NASA-TM-X-304. NASA. https://ntrs.nasa.gov/citations/19660022439
• Ali, Ahmed Abd Al-Hussain, and Mohammed Ismael Hamed. 2023. “The Effect of Laminated Layers on the Flutter Speed of Composite Wing.” Journal of Engineering 18 (08): 924–34. https://doi.org/10.31026/j.eng.2012.08.06
• Ali Tewfik, Mauwafak, Mohammed Idris Abu-Tabikh, and Hayder Sabah Abd Al-Amir. 2013. “Flutter Estimation for Low Speed Aircraft Wing Using Fully Coupled Fluid – Structure Interaction.” Engineering and Technology Journal 31 (16): 3203–15. https://doi.org/10.30684/etj.31.16a.15
• 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
• Allazadeh, M. R., and N. Zuelli. 2017. “Manufacture of a Four-Sheet Complex Component from Different Titanium Alloys by Superplastic Forming.” In AIP Conference Proceedings, vol. 1892. Author(s). https://doi.org/10.1063/1.5007985
• Allen, F. C. 1954. “Unsymmetrical Flight Loads Problems in Supersonic Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/540162
• Allen, J. 1981. “Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile.” In 19th Aerospace Sciences Meeting. AIAA 1981-398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-398
• Allen, J. L., and Andrew Beke. 1953. Force and Pressure Recovery Characteristics at Supersonic Speeds of a Conical Spike Inlet with a Bypass Discharging from the Top or Bottom of the Diffuser in an Axial Direction. NACA-RM-E53A29. NASA. https://ntrs.nasa.gov/citations/19930087574
• Allen, J. L., O. H. Davis, and G. A. Mitchell. 1960. Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-External-Compression Double-Cone Inlet from Mach Number 3.0 to 0.8. NASA-TM-X-149. NASA. https://ntrs.nasa.gov/citations/19630006259
• Allen, F. C., H. D. Meriwether, and L. B. Mosby. 1962. Landing Loads Investigation Laboratory Drop Tests. Defense Technical Information Center. https://doi.org/10.21236/ad0404489
• Allen, F. C., D. M. Rehder, and L. B. Mosby. 1963. A Study of Rough-Terrain-Induced Structural Landing Loads. Phases 1 and 2. Defense Technical Information Center. https://doi.org/10.21236/ad0430063
• Allred, J. W., and V. J. Fleck. 1992. “Mechanical Design of a Rotary Balance System for NASA. Langley Research Center’s Vertical Spin Tunnel.” In Proceedings of the 26th Aerospace Mechanisms Symposium. https://ntrs.nasa.gov/citations/19920015847
• Allwine, Daniel, Jeremy Strahler, Douglas Lawrence, Jerry Jenkins, and James Myatt. 2004. “Nonlinear Modeling of Unsteady Aerodynamics at High Angle of Attack.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5275
• Alroqi, Abdurrhman, and Weiji Wang. 2015. “Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed.” International Journal of Aviation, Aeronautics, and Aerospace. https://doi.org/10.15394/ijaaa.2015.1043
• Alston, R. P. 1939. “Flight Research in Aerodynamics: Some of the Matters Investigated and Methods Used in Flight-Testing.” Aircraft Engineering and Aerospace Technology 11 (3): 84–86. https://doi.org/10.1108/eb030447
• Álvarez, Miguel, A. Gómez, Jorge Salguero, Moisés Batista, Milagros Huerta, and Mariano Marcos. 2010. “SOM-SEM-EDS Identification of Tool Wear Mechanisms in the Dry-Machining of Aerospace Titanium Alloys.” Advanced materials research 107: 77–82. https://doi.org/10.4028/www.scientific.net/amr.107.77
• Alviani, Robert, Jonathan Poggie, and Gregory A. Blaisdell. 2020. “Detached Eddy Simulation of Supersonic Wing-Elevon Cove Boundary-Layer Ingestion.” In AIAA Aviation 2020 Forum. AIAA 2020-3008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3008
• 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
• Alyshev, A. S., V. G. Melnikov, and G. I. Melnikov. 2016. “Identification Method for Pendulum System Moment of Inertia with Viscous Damping.” Scientific and Technical Journal of Information Technologies, Mechanics and Optics: 928–35. https://doi.org/10.17586/2226-1494-2016-16-5-928-935
• Ames Research Staff. 1953. Equations, Tables, and Charts for Compressible Flow. NACA-TR-1135. NASA. https://ntrs.nasa.gov/citations/19930091059
• Amidon, P. 1985. “Supersonic Aerodynamic Characteristics of Elliptic Cross Section Bodies.” In 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. AIAA 1985-1607. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1607
• Amin, N., and D. Hollweger. 1981. “F/A-18A Inlet/engine Compatibility Flight Test Results.” In 17th Joint Propulsion Conference. AIAA 1981-1393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1393
• Amirzadegan, Sadegh, J. Beihaghian, and S. A. Samipour. 2017. “Supersonic Panel Flutter Analysis Assuming Effects of Initial Structural Stresses.” Journal of Aeronautics & Aerospace Engineering 06 (01). https://doi.org/10.4172/2168-9792.1000184
• Amoozgar, Mohammadreza, and Saied Irani. 2012. “Bending-Torsional Flutter of a Composite Rectangular Cantilever Wing Subjected to Engine Thrust.” Advanced materials research 463-464: 1568–72. https://doi.org/10.4028/www.scientific.net/amr.463-464.1568
• Ams J. Aircraft Maintenance Chemicals and Materials Committee. 1982. STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials. https://doi.org/10.4271/arp1795
• Amur Varadarajan, Prasanna, and Philip Roe. 2011. “Geometrical Shock Dynamics and Engine Unstart.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3909
• An, Y., X. Tong, and S. Yang. 2022. “Development of Aircraft Brake System.” IET Conference Proceedings 2022 (7): 775–79. https://doi.org/10.1049/icp.2022.1662
• Anamet Labs INC San Carlos CA. 1979. Analysis of an Aircraft Tire. Defense Technical Information Center. https://doi.org/10.21236/ada363105
• Ananda, Gavin, Pritam Sukumar, and Michael Selig. 2012. “Low-to-Moderate Aspect Ratio Wings Tested at Low Reynolds Numbers.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3026
• Ananthapadmanaban, Ramprakash, and T. M. Murganandam. 2016. “Experimental Study on Start/Unstart Behavior of Two Dimensional Mixed Compression Inlet by Cowl Actuation.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-5072. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5072
• 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
• Ananthkrishnan, Narayan, and Nandan K. Sinha. 2023. “Revised Analytical Criteria for Aircraft Lateral: Directional Instabilities.” Journal of Aerospace Sciences and Technologies: 369–78. https://doi.org/10.61653/joast.v65i4.2013.877
• 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, Joseph L. 1947. Wind Tunnel Development of Means to Alleviate Buffeting of the North American XP-82 Airplane at High Speeds. NACA-RM-SA6L10. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20040010410
• Anderson, Adrian. 1958. Aerodynamic Test Results of Two Configurations of a Proposed Bomber Defense Missile at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0305026
• Anderson, W. 1968. “Engineering Estimates for Supersonic Flutter of Curved Shell Segments.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-284
• Anderson, Byron H. 1973. Aircraft Antiskid Analysis Verification and Refinement. Defense Technical Information Center. https://doi.org/10.21236/ad0770300
• Anderson, S. 1984a. “Handling Qualities Related to Stall/spin Accidents of Supersonic Fighter Aircraft.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2093
• Anderson, B. 1984b. “Three-Dimensional Viscous Design Methodology for Advanced Technologyaircraft Supersonic Inlet Systems.” In 22nd Aerospace Sciences Meeting. AIAA 1984-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-194
• Anderson, J. 1990. “Airframe/propulsion Integration of Supersonic Cruise Vehicles.” In 26th Joint Propulsion Conference. AIAA 1990-2151. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2151
• Anderson, Bernhard H. 2014a. “Grid Resolution Study over Operability Space for a Mach 1.7 Low Boom External Compression Inlet.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20140016537
• Anderson, Bernhard H. 2014b. “The Origin of Inlet Buzz in a Mach 1.7 Low Boom Inlet Design.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3799
• Anderson, D., R. Berger, and J. Hess Jr. 1972. “Maneuver Load Control and Relaxed Static Stability Applied to a Contemporary Fighter Aircraft.” In Guidance and Control Conference. AIAA 1972-870. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-870
• Anderson, B. H., and D. N. Bowditch. 1958. Investigation of Inlet Control Parameters for an External-Internal-Compression Inlet from Mach 2.1 to 3.0. NACA-RM-E58G08. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/19650013032
• Anderson, V. G., and B. A. Manty. 1978. Titanium Alloy Ignition and Combustion. Defense Technical Information Center. https://doi.org/10.21236/ada064993
• Anderson, William, Suresh Patel, and Christopher Black. 2004. “F/A-22 High Angle of Attack Buffet: Test Adequacy Analysis.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5084. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5084
• Anderson, D., K. Sanders, and M. Griswold. 1984. “Development of Advanced Fighter Flight Controls Using Flight Simulators.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2441
• Andrei, Irina-Carmen, Constantin Rotaru, Maria-Cristina Fadgyas, Gabriela Stroe, and Mihai Leonida Niculescu. 2017a. “Numerical Investigation of Turbojet Engine Thrust Correlated with the Combustion Chamber’s Parameters.” Scientific Research and Education in the AIR Force 19 (1): 23–34. https://doi.org/10.19062/2247-3173.2017.19.1.2
• Andrei, Constantin Cristian, Constantin Stelian Stan, Emanuel Teodor Trandafir, and Catalin Pirvu. 2026. “Aerodynamic Performance and Selection of Metallic Materials for Supersonic Wing Design.” Acta Polytechnica 66 (4): 364–74. https://doi.org/10.14311/ap.2026.66.0364
• Andrei, Irina-Carmen, Adrian Toader, Gabriela Stroe, and Florin Frunzulica. 2017b. “Performance Analysis and Dynamic Modeling of a Single-Spool Turbojet Engine.” In AIP Conference Proceedings, vol. 1798. Author(s). https://doi.org/10.1063/1.4972597
• Andrew, L., and T. Stenton. 1967. “Unsteady Aerodynamic Forces on a Thin Wing Oscillating in Transonic Flow.” In 5th Aerospace Sciences Meeting. AIAA 1967-16. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-16
• 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, E. H., Jr., and E. A. Mackley. 1976. Hypersonic Research Engine/aerothermodynamic Integration Model: Experimental Results. Volume 3: Mach 7 Component Integration and Performance. NASA-TM-X-72823. NASA. https://ntrs.nasa.gov/citations/19760016172
• Anggono, Agus D., Waluyo A. Siswanto, and Badrul Omar. 2011. “Hybrid Die Compensation Method to Accommodate Springback Error in Sheet Metal.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3623720
• Anglin, E. L. 1965. Analytical Study of Effects of Product of Inertia on Airplane Spin Entries, Developed Spins, and Spin Recoveries. NASA-TN-D-2754. NASA. https://ntrs.nasa.gov/citations/19650011396
• Anglin, E. 1977. “Recent Research on Aerodynamic Characteristics of Fighter Configurations during Spins.” In Guidance and Control Conference. AIAA 1977-1163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1163
• Ankėnas, R., and R. Barauskas. 2006. “Finite Element Investigation on Parameters Influencing the Springback during Sheet Metal Forming.” Mechanika 61 (5): 57–61. https://doi.org/10.5755/j02.mech.14757
• Ankenbruck, Herman O. 1946. Determination of the Stability and Control Characteristics of a Straight-Wing, Tailless Fighter-Airplane Model in the Langley Free-Flight Tunnel. NACA-WR-L-199. NASA. https://ntrs.nasa.gov/citations/19930092559
• Ankenbruck, Herman O. 1954. Determination of Longitudinal Handling Qualities of the D-558-II Research Airplane at Transonic and Supersonic Speeds to a Mach Number of about 2.0. NACA-RM-H54G29a. NASA. https://ntrs.nasa.gov/citations/19930088510
• Anuj and Hari Parshad. 2025. “Machining of Micro Holes in Titanium Alloy by Electro Discharge Machining.” International Journal of Leading Research Publication 6 (6): 1634. https://doi.org/10.70528/ijlrp.v6.i6.1634
• Appa, K., and G. C. C. Smith. 1973. Finite Element Approach to the Integrated Potential Formulation of General Unsteady Supersonic Aerodynamics. NASA-CR-112296. NASA. https://ntrs.nasa.gov/citations/19730013177
• “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 E: Aircraft Engine Efficiency and Thrust Measures.” 2002. In Aircraft Engine Design, Second Edition. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861444.0537.0546
• Appiah, E. 2004. “A New Constitutive Model for Prediction of Springback in Sheet Metal Forming.” In AIP Conference Proceedings, vol. 712. AIP. https://doi.org/10.1063/1.1766766
• Appich, W., Jr., R. McCoy, and W. Washington. 1980. “Wind Tunnel and Flight Test Drag Comparisons for a Guided Projectilewith Cruciform Tails.” In 11th Aerodynamic Testing Conference. AIAA 1980-426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-426
• “Applications of Titanium and Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-10
• Araujo-Estrada, Sergio A., Mark H. Lowenberg, Simon Neild, and Mikhail Goman. 2015. “Evaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rig.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-0750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0750
• Arbic, Richard G., and Warren Gillespie Jr. 1953. Summary of Rocket-Model Tests at Zero Lift of the Northrop MX-775B Missile Configuration from Mach Numbers of 0.9 to 1.8. NACA-RM-SL53J02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026523
• Arcella, F., D. Abbott, and M. House. 2000. “Titanium Alloy Structures for Airframe Application by the Laser Forming Process.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1465
• Arcella, Frank G., and F. H. Froes. 2000. “Producing Titanium Aerospace Components from Powder Using Laser Forming.” JOM 52 (5): 28–30. https://doi.org/10.1007/s11837-000-0028-x
• Arfa, henia, and Hichem Hassine. 2023. “Taguchi Grey Relational Analysis for Parametric Optimization of Incremental Forming Process of Bimetallic Steel-CP Titanium Composite Sheet.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2486767/v1
• Arkwright, John W., Anthony W. Papageorgiou, Luke A. Parkinson, Andrew R. Karas, and Kristy L. Hansen. 2018. “Monitoring Pressure Profiles across an Airfoil Section with a Fibre Bragg Grating Sensor Array.” In Photonic Instrumentation Engineering V, edited by Yakov G. Soskind. SPIE. https://doi.org/10.1117/12.2288024
• Arlinger, Bert G. 1976. “Axisymmetric Inlet Flow at Low Supersonic Mach Numbers.” In Symposium Transsonicum II. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_21
• 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, W. C. 1979. A Method of Characteristics Computer Program for Three-Dimensional Supersonic Internal Flows. Defense Technical Information Center. https://doi.org/10.21236/ada063518
• 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 War Coll Carlisle Barracks Pa. 1952. Handbook of Supersonic Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ada390507
• Arnaiz, H. H. 1975. “Techniques for Determining Propulsion System Forces for Accurate High Speed Vehicle Drag Measurements in Flight.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750057617
• 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
• Arnal, D., and J. Reneaux. 2001. “Attachment Line Transition in Supersonic Flow.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_15
• Arnold, Charles E. 1987. “Spin Resistant Airplane Certification Issues.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/871849
• “Artificial Neural Networks Model for Springback Prediction in the Bending Operations.” 2020. Tehnicki vjesnik - Technical Gazette 27 (3). https://doi.org/10.17559/tv-20141209182117
• Arvin, G. H., L. Israeli, J. H. Stolpestad, and G. W. Stacher. 1981. Evaluation of Superplastic Forming and Co-Diffusion Bonding of Ti-6Al-4V Titanium Alloy Expanded Sandwich Structures. NASA-CR-165827. NASA. https://ntrs.nasa.gov/citations/19820011484
• Asadi, Davood, Mahdi Sabzehparvar, and Heidar Ali Talebi. 2013. “Damaged Airplane Flight Envelope and Stability Evaluation.” Aircraft Engineering and Aerospace Technology 85 (3): 186–98. https://doi.org/10.1108/00022661311313623
• Asher, Gifford W., John R. Martuccelli, and Warren H. Weatherill. 1957. Flutter Model Tests of a Swept-Back, All-Moving Horizontal Tail at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0142088
• Ashkenas, I. L. 1965. A Study of Conventional Airplane Handling Qualities Requirements. Part 1. Roll Handling Qualities. Defense Technical Information Center. https://doi.org/10.21236/ad0627659
• Ashley, Holt, Herbert M. Voss, and Garabed Zartarian. 1954. “The Dynamic Analysis of Low-Aspect-Ratio Airplane Wings.” Proceedings of the National Academy of Sciences 40 (6): 388–94. https://doi.org/10.1073/pnas.40.6.388
• 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
• Askari, Rasoul, Mohammad Reza Soltani, and Afshin Khajeh Fard. 2017. “Geometrical Scaling Effects on Supersonic Inlet Performance.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2017-71912
• Astarita, Antonello, Luca Giorleo, Fabio Scherillo, Antonino Squillace, Elisabetta Ceretti, and L. Carrino. 2014. “Titanium Hot Stretch Forming: Experimental and Modeling Residual Stress Analysis.” In Key engineering materials, vol. 611-612. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.611-612.149
• Atay, Görkem, and Can Kumartaslioglu. 2024. “An Engineering Approach to Calculate Aerodynamic Heating on Supersonic Missiles.” In AIAA SCITECH 2024 Forum. AIAA 2024-1877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1877
• Atkinson, Michael. 2007. “Numerical Investigation of a Super-Sonic Inlet Using Bleed and Micro-Ramps to Control Shock-Wave/Boundary Layer Interactions.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-24. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-24
• Atkinson, A., and C. McClelland. 1968. “A Management Approach to a Multipurpose Aircraft Engine Development.” In 5th Annual Meeting and Technical Display. AIAA 1968-979. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-979
• Atmaca, Ediz, Sena Aydoğan, Hacı Yusuf Narlı, Rıdvan Bakir, and Mehmet Can Sarıkınacı. 2025. “Ensuring Flight Safety by Optimizing Test Points in Fighter Aircraft.” Politeknik Dergisi 28 (3): 1035–44. https://doi.org/10.2339/politeknik.1611963
• Attri, N., and R. Amberg. 1974. “Improvements in Airplane Stopping Performance on Adverse Runways.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-965
• Auman, Lamar. 1993. “Wind Tunnel Investigation with an Operational Turbojet Engine.” In 31st Aerospace Sciences Meeting. AIAA 1993-36. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-36
• Austin, Edward E., and James R. van Gaasbeek. 1978. “Digital Simulation of the Operational Loads Survey Flight Tests.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f34-052
• “Automatic Detection and Suppression of Inlet Buzz.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0453.0460
• Avanzini, Giulio, and Guido D. 1996. “Bifurcation Analysis of a Highly Augmented Aircraft Model.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3367
• Averett, B. T. 1980. “Simulator Investigation of Arrow-Wing Low-Speed Handling Qualities.” In NASA. Langley Res. Center Supersonic Cruise Res. 1979, Pt. 1. https://ntrs.nasa.gov/citations/19810009470
• 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
• Axelson, J. 1975. “Estimation of Transonic Aircraft Aerodynamics to High Angles of Attack.” In Aircraft Systems and Technology Meeting. AIAA 1975-996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-996
• Azam, Nur, and Erwin Sulaeman. 2014. “Aeroelastic Flutter Analysis of Supersonic Wing with Multiple External Stores.” IIUM Engineering Journal 15 (2). https://doi.org/10.31436/iiumej.v15i2.524
• Azzabi, Khaled I., and Aiman Elmahmodi. 2012. “Mathematical Model Development of TMM25-Single Shaft Turbojet Engine.” Applied Mechanics and Materials 225: 267–72. https://doi.org/10.4028/www.scientific.net/amm.225.267
• Baals, D., and R. Harris Jr. 1968. “Aerodynamic Design Integration of Supersonic Aircraft.” In 5th Annual Meeting and Technical Display. AIAA 1968-1018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1018
• Baber, H. T., Jr., and M. T. Moul. 1955. Longitudinal Stability and Control Characteristics as Determined by the Rocket-Model Technique for an Inline, Cruciform, Canard Missile Configuration with a Low-Aspect-Ratio Wing Having Trailing-Edge Flap Controls for a Mach Number Range of 0.7 to 1.8. NACA-RM-L54B12. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19690067250
• Babinsky, Holger. 2007. Understanding Micro-Ramp Control of Supersonic Shock Wave Boundary Layer Interactions. Defense Technical Information Center. https://doi.org/10.21236/ada476419
• Babinsky, Holger. 2014. Flow Control for Supersonic Inlet Applications. Defense Technical Information Center. https://doi.org/10.21236/ada602774
• Babister, A. W. 1980. “Aerodynamic Derivatives (Lateral).” In Aircraft Dynamic Stability and Response. Elsevier. https://doi.org/10.1016/b978-0-08-024768-7.50011-9
• Babu, V. 2021. “The Turbojet Engine.” In Fundamentals of Propulsion. Springer International Publishing. https://doi.org/10.1007/978-3-030-79945-8_5
• Babu, Arun V., and Shreyas Narsipur. 2025. “Connecting Wake Vorticity with Fundamental Fourier Terms in Unsteady Thin Airfoil Theory.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3773. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3773
• 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
• Badrinarayanan, A. S., and A. Anandaraj. 2022. “Designing the Roll Characteristics & Pitch-Roll Lock-in of an Unguided Artillery Rocket by Tailoring the Chamfer on Fins.” In Proceedings of the 32nd International Symposium on Ballistics. Destech Publications, Inc. https://doi.org/10.12783/ballistics22/36129
• Bae, Jae-Sung, and In Lee. 2002. “Nonlinear Aeroelastic Characteristics of a Fighter-Type Wing with Control Surface.” In 5th International Symposium on Fluid Structure Interaction, Aeroelasticity, and Flow Induced Vibration and Noise. ASMEDC. https://doi.org/10.1115/imece2002-33066
• Baer, A. L. 1966. The Effects of Flow through an Aircraft Pitot-Static Probe at Supersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ad0477832
• Baer, Steven. 2014. “F-35A High Angle of Attack Testing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2057
• 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, J. 1982. “Evaluation of a Simplified Gross Thrust Calculation Method for a J85-21 Afterburning Turbojet Engine in an Altitude Facility.” In 18th Joint Propulsion Conference. AIAA 1982-1044. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1044
• Baghdadi, Nadjib, Mark Lowenberg, and Askin Isikveren. 2009. “Application of Bifurcation and Continuation Methods to Nonlinear Flexible Aircraft Dynamics.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6305
• 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
• Băilă, D. I., and S. Tonoiu. 2019. “Hydrides precipitation in Ti6Al4V titanium alloy used for airframe manufacturing.” Bulletin of the Polish Academy of Sciences Technical Sciences: 643–49. https://doi.org/10.24425/bpasts.2019.129662
• Bailey, F. J., Jr. 1965. Airplane Take-off Performance Indicator Patent. Patent Number: US-PATENT-3,168,827. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19700027491
• Baize, Daniel G. 1999. 1997 NASA High-Speed Research Program Aerodynamic Performance Workshop: Configuration Aerodynamics: Volume 1. NASA/CP-1999-209691/VOL1/PT2. NASA. https://ntrs.nasa.gov/citations/20000057252
• Bajpai, Gaurav, Adam Beytin, Murat Yasar, Harry Kwatny, Bor-Chin Chang, and Suba Thomas. 2008. “Nonlinear Modeling and Analysis Software for Control Upset Prevention and Recovery of Aircraft.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6657. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6657
• 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
• Baker, Thomas F., and Wallace E. Johnson. 1955. Flight Measurements at Transonic Speeds of the Buffeting Characteristics of the XF-92A Delta-Wing Research Airplane. NACA-RM-H54L03. NASA. https://ntrs.nasa.gov/citations/19930088625
• Baker, Thomas F., James A. Martin, and Betty J. Scott. 1957. Flight Data Pertinent to Buffeting and Maximum Normal-Force Coefficient of the Douglas X-3 Research Airplane. NACA-RM-H57H09. NASA. https://ntrs.nasa.gov/citations/19930090138
• Bakker, Roemer M. B., Olaf Stroosma, Daan M. Pool, Marinus M. van Paassen, and Max Mulder. 2025. “Comparison of Classical and Optimization-Based Motion Cueing for Simulating Aircraft Upset Maneuvers.” In AIAA SCITECH 2025 Forum. AIAA 2025-0978. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0978
• Baklanov, V. 2013. “Interaction of Power Plant with Airframe of New Generation Aircraft.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/201304395
• Balakrishnan, A. V. 2006. “Nonlinear Aeroelasticity: Continuum Theory, Flutter/Divergence Speed, and Plate Wing Model.” Journal of Aerospace Engineering 19 (3): 194–202. https://doi.org/10.1061/(asce)0893-1321(2006)19:3(194)
• Balakrishnan, A. 2007. “Nonlinear Aeroelasticity, Continuum Theory, Flutter/divergence Speed, Plate Wing Model.” In Lecture Notes in Pure and Applied Mathematics. Chapman and Hall/CRC. https://doi.org/10.1201/9781420011159.ch11
• Balckburn, Linda B. 1987. Effect of LID (Registered) Processing on the Microstructure and Mechanical Properties of Ti-6Al-4V and Ti-6Al-2Sn-4Zr-2Mo Titanium Foil-Gauge Materials. NASA-TP-2677. NASA. https://ntrs.nasa.gov/citations/19870009211
• Bales, T. T., and R. L. Cain. 1971. “A Preliminary Report on the Effect of Elevated Temperature Exposure on the Mechanical Properties of Titanium-Alloy Honeycomb-Core Sandwich Panels.” In Society of Manufacturing Engineers and American Society of Metals, Western Metal and Tool Conference and Exposition. https://ntrs.nasa.gov/citations/19720027209
• Bales, T. T., E. K. Hoffman, and R. K. Bird. 1990. “Advanced Fabrication Technology for High Speed Aircraft Structures.” In ICAS Congress. https://ntrs.nasa.gov/citations/19910039834
• Ball, L. H., and W. G. Smith. 1956. Static Lateral-Directional Stability Characteristics of Five Contemporary Airplane Models from Wind-Tunnel Tests at High Subsonic and Supersonic Speeds. NACA-RM-A55J03. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19660010446
• Ball, W., J. Syberg, and L. Surber. 1981. “Experimental Investigation of a High-Aspect-Ratio Supersonic Inlet.” In 17th Joint Propulsion Conference. AIAA 1981-1397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1397
• Balli, Ozgur. 2014. “Afterburning Effect on the Energetic and Exergetic Performance of an Experimental Turbojet Engine (TJE).” International Journal of Exergy 14 (2): 212. https://doi.org/10.1504/ijex.2014.060278
• Balli, Ozgur. 2020. “Exergetic, Exergoeconomic, Sustainability and Environmental Damage Cost Analyses of J85 Turbojet Engine with Afterburner.” International Journal of Turbo & Jet-Engines 37 (2): 167–94. https://doi.org/10.1515/tjj-2017-0019
• Bamber, M. J., and R. O. House. 1937a. Spinning Characteristics of the XN2Y-1 Airplane Obtained from the Spinning Balance and Compared with Results from the Spinning Tunnel and from Flight Tests. NACA-TR-607. NASA. https://ntrs.nasa.gov/citations/19930091682
• Bamber, M. J., and R. O. House. 1937b. Spinning Characteristics of Wings III: A Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips. NACA-TN-612. NASA. https://ntrs.nasa.gov/citations/19930081413
• Bamber, M. J., and R. O. House. 1938. Spinning Characteristics of Wings V: N.A.C.A. 0009, 23018, and 6718 Monoplane Wings. NACA-TN-633. NASA. https://ntrs.nasa.gov/citations/19930081463
• Bamber, M. J., and C. H. Zimmerman. 1934. Spinning Characteristics of Wings I: Rectangular Clark Y Monoplane Wing. NACA-TR-519. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930091592
• Banerjee, Sudip, Bikash Panja, and Prasanta Sahoo. 2022. “6 Parametric Optimization of Machining Characteristics of Titanium Alloy in WEDM.” In Nonconventional Machining. De Gruyter. https://doi.org/10.1515/9783110584479-006
• 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
• Barnard, H. 1969. “Transonic Buffet Characteristics of a 60 Degree Swept Wing with Design Variations.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-793
• Barnes, Terence, and Thomas Defiore. 1991. “The New FAA Flight Loads Monitoring Program.” In 29th Aerospace Sciences Meeting. AIAA 1991-258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-258
• Barnhart, Paul. 1989. “A Supersonic through-Flow Fan Engine Airframe Integration Study.” In Aircraft Design and Operations Meeting. AIAA 1989-2140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2140
• Barr, Dale. 1990. “The Normal Shock Generator: An Inlet Throat Region Research Apparatus for High Mach Applications.” In 26th Joint Propulsion Conference. AIAA 1990-1930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1930
• Barr, Stephen M., Roger Birkbeck, Praveen Panickar, and Neeraj Sinha. 2022. “Wind Tunnel Test of a Highly-Compact Serpentine Supersonic Inlet.” In AIAA AVIATION 2022 Forum. AIAA 2022-3865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3865
• Barr, Stephen M., Michael O’Gara, and Neeraj Sinha. 2018. “Highly Compact Supersonic Inlet Design Optimization.” In 2018 Joint Propulsion Conference. AIAA 2018-4842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4842
• Barrau, Olivier, Fabien Nazaret, Marion Le Fournier, Lebard Etienne, and Yannick Le Maoult. 2016. “Titanium Superplastic Forming by Aurock: A Complete Integrated Solution from CAD File to Final Part.” In Materials science forum, vol. 838-839. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.838-839.488
• Barrett, Paul F. 1950. Compressive Properties of Titanium Sheet at Elevated Temperatures. NACA-TN-2038. NASA. https://ntrs.nasa.gov/citations/19930082695
• Barrows, T. 1976. “Simplified Methods of Predicting Aircraft Rolling Moments Due to Vortex Encounters.” In 14th Aerospace Sciences Meeting. AIAA 1976-61. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-61
• Bartlett, R. S. 1970. “High Lift-Drag Ratio Double Wedges of Given Volume Which Support Two-Dimensional Supersonic Flow Fields.” Aeronautical Journal 74 (710): 159–61. https://doi.org/10.1017/s0001924000047448
• 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
• 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
• Bateman, Don. 2010. “Some Thoughts on Reducing the Risk of Aircraft Loss of Control.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8139
• Batill, Stephen M. 1982. A Study of Analytic Modeling Techniques for Landing Gear Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada122312
• Batill, S., and J. Bacarro. 1988. “Modeling and Identification of Nonlinear Dynamic Systems with Application to Aircraft Landing Gear.” In 29th Structures, Structural Dynamics and Materials Conference. AIAA 1988-2315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2315
• Batina, John. 1988. “Unsteady Transonic Algorithm Improvements for Realistic Aircraft Applications.” In 26th Aerospace Sciences Meeting. AIAA 1988-105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-105
• Batista dos Santos, Marcio Wagner. n.d. “Investigation of the Mechanical Behaviour and Microstructural Evolution of Titanium Alloys under Superplastic and Hot Forming Conditions.” PhD diss., Ecole nationale des Mines d’Albi-Carmaux. https://doi.org/10.70675/1246692bzb797z44c3z9b60zccdbfeb4d07b
• 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
• Baucom, R. M. 1969. Strain Rate Sensitivity of Three Titanium Alloy Sheet Materials after Prolonged Exposure at 550 Deg F (561 Deg K). NASA-TN-D-4981. NASA. https://ntrs.nasa.gov/citations/19690005541
• Bauer, Steven, and S. McMillin. 1988. “Experimental and Theoretical Study of the Effects of Wing Geometry on a Supersonic Multibody Configuration.” In 6th Applied Aerodynamics Conference. AIAA 1988-2510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2510
• Bauer, R. C., W. W. Muse, and C. R. Tinsley. 1974. Simulation of Flow Approaching the Chin Inlet of a Ramjet Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0783244
• Bauer, Steven, and Richard Wood. 1989. “A Natural Flow Wing Design Employing 3-D Nonlinear Analysis Applied at Supersonic Speeds.” In 7th Applied Aerodynamics Conference. AIAA 1989-2167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2167
• Bauermeister, W., and H. Ip. 1968. “727 Airplane Engine Inlet Development.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-595
• Baum, Queenie. 1956. “Flight Loads during Combat Training: An Experimental Determination Using V-g Recorders of Manoeuvres in Mustang Aircraft of the R.A.A.F.” Aircraft Engineering and Aerospace Technology 28 (8): 262–64. https://doi.org/10.1108/eb032723
• Baydar, Ezgihan, Frank K. Lu, and John W. Slater. 2016. “Vortex Generators in a Two-Dimensional, External-Compression Supersonic Inlet.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170000948
• Baydar, Ezgihan, Frank K. Lu, John W. Slater, and Charles J. Trefny. 2017. “Vortex Generators in a Streamline-Traced, External-Compression Supersonic Inlet.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170001419
• Baye-Wallace, Lily, and Charles R. Krouse. 2022. “Simulation of Inlet Unstart in a Supersonic Engine Model Running on a Raspberry Pi.” In AIAA SCITECH 2022 Forum. AIAA 2022-0402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0402
• Bayoğlu, Tuğba, Ozan Nalci, and Ali T. Kutay. 2016. “Aerodynamic Parameter Estimation of a Supersonic Air to Air Missile with Rapid Speed Variation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3856. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3856
• Bazile, M. J., and M. F. Calderara. 2012. “Aircraft Dynamic Lateral Stability Analytic Formulation for Dutch Roll Mode Stability Prediction.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203053
• Beachem, C. D. 1964. Fracture Analysis of a C-141 Landing Gear Cylinder. Defense Technical Information Center. https://doi.org/10.21236/ad0601723
• Beachkofski, Brian K. 1999. Elementary Model of Nose Gear Retraction and Oleo-Pneumatic Strut Compression. Defense Technical Information Center. https://doi.org/10.21236/ada374308
• Beal, Joseph D., Rodney Boyer, and Daniel Sanders. 2006. “Forming of Titanium and Titanium Alloys.” In Metalworking: Sheet Forming. ASM International. https://doi.org/10.31399/asm.hb.v14b.a0005146
• Beale, D., and M. Zelenak. 1992. “Development and Validation of a Freejet Technique for Inlet-Engine Compatibility Testing.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3921
• Beals, V., and W. P. Targoff. 1953. Control Surface Oscillatory Coefficients Measured on Low Aspect-Ratio Wings. Defense Technical Information Center. https://doi.org/10.21236/ad0026027
• 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
• Beattie, E. C. 1980. “Design of a Multivariable Integrated Control for a Supersonic Propulsion System.” In NASA. Lewis Research Center Propulsion Controls, 1979. https://ntrs.nasa.gov/citations/19810003584
• Beaulieu, W. D., and A. W. Martin. 1970. XB-70 Flight Test Data Comparisons with Simulation Predictions of Inlet Unstart and Buzz. NASA-CR-1631. NASA. https://ntrs.nasa.gov/citations/19700022266
• Beck, T. R. 1966. Stress Corrosion Cracking of Titanium Alloys Preliminary Report on TI:8AL-1MO-1V Alloy and Proposed Electrochemical Mechanism. Defense Technical Information Center. https://doi.org/10.21236/ad0640229
• Beck, W. 2003. Superplastic Forming and Diffusion Bonding of Titanium and Titanium Alloys. Wiley. https://doi.org/10.1002/3527602119.ch10
• Beck, Andrea. 2005. “RANS Simulation of Turbulent Boundary Layer: Shock Interactions on a Generic Inlet Structure.” In 17th AIAA Computational Fluid Dynamics Conference. AIAA 2005-4702. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4702
• 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
• Beeton, A. B. P. 1966. “Materials Requirements for Aircraft Turbojet and Ramjet Engines.” In Advances in Materials. Elsevier. https://doi.org/10.1016/b978-0-08-012204-5.50012-3
• 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
• Behera, Soumyajit, C. Muthuraj, Balmiki Kumar, U. R. Srikanth, Sathish Sunnam, and R. Jolly. 2020. “Design of Vortex Flaps for Reducing Approach Speed of a Supersonic Naval Fighter Aircraft.” In Lecture Notes in Mechanical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-5432-2_9
• 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
• Beke, Andrew. 1958. Effect of Wall Cooling on Inlet Parameters of a Scoop Operating in a Turbulent Boundary Layer on a Flat or Conical Surface for Mach Numbers 2 to 10. NACA-TN-4153. NASA. https://ntrs.nasa.gov/citations/19930084952
• Beke, Andrew, and J. L. Allen. 1953. Force and Pressure-Recovery Characteristics at Supersonic Speeds of a Conical Nose Inlet with Bypasses Discharging Outward from the Body Axis. NACA-RM-E52L18a. NASA. https://ntrs.nasa.gov/citations/19930087580
• Beke, Andrew, John L. Allen, and Thomas Williams. 1955. Preliminary Investigation of a Conical Spike Inlet in Combination with a Vertical-Wedge Auxiliary Inlet at Mach Number 1.9. NACA-RM-E55H04. NASA. https://ntrs.nasa.gov/citations/19930090247
• Belart, H. 1938. “High Wing-Loading: The Designer’s Problem of Deciding o the Wing Area Necessary for His Purpose.” Aircraft Engineering and Aerospace Technology 10 (6): 173–91. https://doi.org/10.1108/eb030322
• Belcastro, Christine. 2012. “Validation of Safety-Critical Systems for Aircraft Loss-of-Control Prevention and Recovery.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4987
• Belcastro, Christine. 2014. “Aircraft Loss of Control: Research and Technology Directions.” In University of Missouri Engineering Seminar. https://ntrs.nasa.gov/citations/20200007706
• Belcastro, Christine, and John Foster. 2010. “Aircraft Loss-of-Control Accident Analysis.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8004. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8004
• Belcastro, Christine M., John V. Foster, Richard L. Newman, Loren Groff, Dennis A. Crider, and David H. Klyde. 2016. “Aircraft Loss of Control: Problem Analysis for the Development and Validation of Technology Solutions.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0092
• Belcastro, Christine M., Loren Groff, Richard L. Newman, et al. 2014. “Preliminary Analysis of Aircraft Loss of Control Accidents: Worst Case Precursor Combinations and Temporal Sequencing.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140003949
• Belcastro, Christine, and Steven Jacobson. 2010. “Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control Accidents.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8142
• Belcastro, Christine, Thuan Khong, Jong-Yeob Shin, Harry Kwatny, B-C. Chang, and Gary Balas. 2005. “Uncertainty Modeling for Robustness Analysis of Aircraft Control Upset Prevention and Recovery Systems.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6427
• Belesiotis-Kataras, Panagiotis, and Sebastian Timme. 2021. “Aeroelastic Coupling Effects in Globally Unstable Transonic Wing Flow.” In AIAA Scitech 2021 Forum. AIAA 2021-0611. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0611
• “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
• 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
• Bellman, D., and D. Hughes. 1968. “Preliminary Flight Investigation of Dynamic Phenomena within Air Breathing Propulsion Systems of Supersonic Aircraft.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-593. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-593
• Bellman, Donald R., and Edward D. Murphy. 1954. Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained during Demonstration Flights to a Mach Number of 1.20. NACA-RM-H54I17. NASA. https://ntrs.nasa.gov/citations/19930088507
• Belubekyan, M. V., and S. R. Martirosyan. 2016a. “On a Problem of Supersonic Panel Flutter in the Presence of Concentrated Inertial Masses and Moments.” Mechanics - Proceedings of National Academy of Sciences of Armenia 69 (3): 41–58. https://doi.org/10.33018/69.3.4
• Belubekyan, M. V., and S. R. Martirosyan. 2016b. “Supersonic Panel Flutter in the Presence of the Concentrated Inertial Masses and the Moments.” Mechanics - Proceedings of National Academy of Sciences of Armenia 69 (1): 39–52. https://doi.org/10.33018/69.1.4
• Bencze, D. 1972. “Nacelle-Airframe Interference at Low Supersonic Mach Numbers.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1113
• Bendiksen, Oddvar. 1987. “Transonic Flutter Analysis Using the Euler Equations.” In 28th Structures, Structural Dynamics and Materials Conference. AIAA 1987-911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-911
• Bendiksen, Oddvar. 1992. “Role of Shock Dynamics in Transonic Flutter.” In Dynamics Specialists Conference. AIAA 1992-2121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2121
• Bendiksen, Oddvar O. 1994. “Eulerian-Lagrangian Simulations of Transonic Flutter Instabilities.” In Aeroelasticity and Fluid Structure Interaction Problems. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1994-1448
• Bendiksen, Oddvar. 1999. “Improved Similarity Rules for Transonic Flutter.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1350. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1350
• Bendiksen, Oddvar O. 2015. “Transonic Flutter Characteristics of Advanced Fighter Wings.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-0438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0438
• Benek, John, Edward Kraft, and Rodney Lauer. 1996. “Validation Issues for Engine/airframe Integration.” In Fluid Dynamics Conference. AIAA 1996-2031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2031
• Bengtson, Darroll, Thomas Dickovich, and Robert Helfenstine. 1975. Roll-Axis Hydrofluidic Stability Augmentation System Development. Defense Technical Information Center. https://doi.org/10.21236/ada016932
• Bennet-Clark, H. C. 1972. “Stability of Swivel Wing Supersonic Aircraft.” Nature 239 (5373): 451–52. https://doi.org/10.1038/239451b0
• Bennett, Charles V. 1949. Theoretical Investigation of the Dynamic Lateral Stability Characteristics of Douglas Design No. 39C, an Early Version of the X-3 Research Airplane. NACA-RM-L8L31. NASA. https://ntrs.nasa.gov/citations/19930085567
• Bennett, Charles V. 1950. Theoretical Investigation of the Dynamic Lateral Stability Characteristics of the Douglas X-3 Research Airplane: Study 41-B. NACA-RM-L50B28. NASA. https://ntrs.nasa.gov/citations/19930086128
• Bennett, Floyd V. 1961. Comparison of Experimental and Theoretical Static Aeroelastic Loads and Deflections of a Thin 45 Deg Delta Wing in Supersonic Flow. NASA-TN-D-974. NASA. https://ntrs.nasa.gov/citations/20040008163
• Bennett, Jim. 1990. “Fighter Design Econometrics = Ownership Affordability?” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3223
• Bennett, Robert M. 2000. “9E. Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations.” In Verification and Validation Data for Computational Unsteady Aerodynamics. https://ntrs.nasa.gov/citations/20010009849
• 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
• Bennett, Robert M., and John T. Batina. 1989. “Application of the CAP-TSD Unsteady Transonic Small Disturbance Program to Wing Flutter.” In European Forum on Aeroelasticity and Structural Dynamics. https://ntrs.nasa.gov/citations/19900046299
• Bennett, Robert, John Batina, and Herbert Cunningham. 1988. “Wing Flutter Calculations with the CAP-TSD Unsteady Transonic Small Disturbance Program.” In 29th Structures, Structural Dynamics and Materials Conference. AIAA 1988-2347. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2347
• Benson, Thomas J. 1994. “An Interactive, Design and Educational Tool for Supersonic External-Compression Inlets.” In AIAA, ASME, SAE, and ASEE. https://ntrs.nasa.gov/citations/19940025669
• Benson, T. J., and B. H. Anderson. 1983. “Validation of a Three Dimensional Viscous Analysis of Axisymmetric Supersonic Inlet Flow Fields.” In 21st Aerospace Sciences Meeting. AIAA 1983-540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-540
• Benson, Rusty, and D. McRae. 1993. “Numerical Simulations of the Unstart Phenomenon in a Supersonic Inlet/diffuser.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2239
• Benson, Rusty, and D. McRae. 1994. “Unsteady Transients in a Supersonic Inlet Subject to Freestream Perturbations and Dynamic Attitude Changes.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-581
• Benson, J., T. Sedgwick, and B. Wright. 1976. “Supersonic Cruise Vehicle Propulsion System Integration Studies.” In 12th Propulsion Conference. AIAA 1976-756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-756
• Benton, Robert. 2019. “On the Integration of Structural Loads Analysis with Structural Flight Testing for Improved Fatigue Methodologies.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0075-2019-14714
• Benton, Stuart I., William Humphrey, and Brock Pleiman. 2021. “Simulations of an Airframe-Integrated Two-Dimensional Supersonic Inlet at off-Design Conditions.” In AIAA Scitech 2021 Forum. AIAA 2021-0879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0879
• Berci, M. 2017. “Static Aeroelastic Behavior of a Subsonic Plate Wing.” In AIP Conference Proceedings, vol. 1863. Author(s). https://doi.org/10.1063/1.4992672
• Berdon, Randall, James H. Buchholz, Caterina Lamuta, and H. S. Udaykumar. n.d. “Flow Structures and Aerodynamic Loads of a Rolling Wing in a Free Stream.” PhD diss., University of Iowa. https://doi.org/10.17077/etd.xhdj-14k7
• Berens, Ap. 1979. “Determination of Sample Size in Flight Loads Programs.” In Service Fatigue Loads Monitoring, Simulation, and Analysis. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp35864s
• Berens, Thomas. 2010. “Aerodynamic Propulsion Integration for Supersonic Business Jets.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6591
• Bergstedt, P. W., H. C. Turner, and W. M. Sutherland. 1959. Effect of Heating Aluminum Alloy Wing Structure to 325 f on the Mechanical Properties of Its Component Materials. Defense Technical Information Center. https://doi.org/10.21236/ad0402171
• Berman, Theodore. 1947a. Free-Spinning Tunnel Tests of a 1/24-Scale Model of the Grumman XTB3F-1 Airplane, TED No. NACA DE304. NACA-RM-L7E19. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019395
• Berman, Theodore. 1947b. Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the McDonnell XP-88 Airplane with a Conventional Tail. NACA-RM-L7H21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019357
• Berman, Theodore. 1948a. Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 317. NACA-RM-SL7L09. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028613
• Berman, Theodore. 1948b. Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the North American XP-86 Airplane. NACA-RM-SL8D22. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028753
• Berman, Theodore. 1948c. Supplementary Investigation in the Langley 20-Foot Free-Spinning Tunnel of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Chance Vought XFU-1 Airplane, Ted No. NACA DE 311. NACA-RM-SL9H30a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030037
• Berman, Theodore. 1950a. Comparison of Model and Full-Scale Spin Test Results for 60 Airplane Designs. NACA-TN-2134. NASA. https://ntrs.nasa.gov/citations/19930082756
• Berman, Theodore. 1950b. Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF1OF-1 Airplane. NACA-RM-SL50L14. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023626
• Berman, Theodore. 1951. Supplementary Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF10F-1 Airplane in the Swept-Wing Configuration with Slats Extended. NACA-RM-SL51G19. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023702
• Berman, Julian H. 1956. Lift and Moment Coefficients for an Oscillating Rectangular Wing-Aileron Configuration in Supersonic Flow. NACA-TN-3644. NASA. https://ntrs.nasa.gov/citations/19930084404
• Berman, Theodore, and Norman E. Pumphrey. 1950. Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311. NACA-RM-SL50F02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050080688
• Berman, Theodore, and Jack H. Wilson. 1948. Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane with Wing-Tip Tanks Installed. NACA-RM-SL9F01. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030061
• Bernal, Luis P. 2016. “Unsteady Aerodynamics of Pitching Low Aspect Ratio Wings: A Review of AVT-202-Panel Results (Invited Paper).” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0287. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0287
• Bernhart, G., P. Lours, T. Cutard, V. Velay, and F. Nazaret. 2011. “Processes and Equipment for Superplastic Forming of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.1.49
• Bernstein, Harry, and Rudolph C. Haefeli. 1953. Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4. NACA-RM-E53A12. NASA. https://ntrs.nasa.gov/citations/19930087483
• Berrier, B. 1983. “Empennage/afterbody Integration for Single and Twin-Engine Fighter Aircraft.” In 19th Joint Propulsion Conference. AIAA 1983-1126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1126
• 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, 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, D., and B. Powers. 1970. “Flying Qualities of a Large, Supersonic Aircraft in Cruise and Landing Approach.” In Propulsion and ASW Meeting. AIAA 1970-566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-566
• Berryman, R., J. Chesnutt, F. Froes, and J. Williams. 1976. “A NEW TITANIUM ALLOY FOR COST-EFFECTIVE DESIGN OF MILITARY AIRCRAFT: Ti-4.5A1-5Mo-1.5Cr.” In 17th Structures, Structural Dynamics, and Materials Conference. AIAA 1976-1512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1512
• 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
• Bertram, A., T. Böhlke, A. Krawietz, and V. Schulze. 2007. “Finite Element Simulation of Sheet Metal Forming and Springback Using a Crystal Plasticity Approach.” In AIP Conference Proceedings, vol. 908. AIP. https://doi.org/10.1063/1.2740903
• Bertram, M. H., and E. F. Ulmann. 1953. Aerodynamic Characteristics of Low-Aspect-Ratio Wings at High Supersonic Mach Numbers. NACA-RM-L53I23. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630010653
• Bertrand, Xavier, Frédéric Tost, and Steeve Champagneux. 2019. “Wing Airfoil Pressure Calibration with Deep Learning.” In AIAA Aviation 2019 Forum. AIAA 2019-3066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3066
• Beskin, Leon. 1949. “Supersonic Flow past Airfoil Tips.” Journal of Applied Mechanics 16 (4): 329–45. https://doi.org/10.1115/1.4010007
• Best, K. F. 1986. “High Strength Materials for Aircraft Landing Gear.” Aircraft Engineering and Aerospace Technology 58 (7): 14–24. https://doi.org/10.1108/eb036313
• Bharathi, V., A. R. Anilchandra, Lochan Upadhayay, Sagar Pandit, and Pranish Bhuju. 2021. “Mathematical Modeling for Machining of Inconel 718 & Titanium 64 Alloys.” In AIP Conference Proceedings, vol. 2316. AIP Publishing. https://doi.org/10.1063/5.0036449
• Bhat, Rama B. 2018a. “Flutter of a Cantilever Wing.” In Principles of Aeroelasticity. CRC Press. https://doi.org/10.1201/9781315370613-9
• Bhat, Rama B. 2018b. “Static Aeroelasticity.” In Principles of Aeroelasticity. CRC Press. https://doi.org/10.1201/9781315370613-3
• Bhatt, D. 1985. “Development of Generalized Process Models for Superplastic Forming of Titanium Structures.” In 26th Structures, Structural Dynamics, and Materials Conference. AIAA 1985-624. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-624
• Bhatt, Dhananjay, Trent Logan, and Ira Victer. 1990. “Titanium Aluminides Development for NASP Airframe Applications.” In 2nd International Aerospace Planes Conference. AIAA 1990-5261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-5261
• Bhowmick, Shiladitya, Hariprasanth Palanivel, V. Kalyana Chakravarthy, and Rinku Mukherjee. 2025. “Aerodynamic Design of Inverse Diamond-Back Joined Wing on a Slender Body at Subsonic and Supersonic Mach Numbers.” In AIAA SCITECH 2025 Forum. AIAA 2025-0254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0254
• Biber, Kasim. 2017. “Wind Tunnel and Computational Stability Derivatives for a Propeller-Driven Airplane.” International Journal of Sustainable Aviation 3 (3): 271. https://doi.org/10.1504/ijsa.2017.086844
• Bielat, Ralph P., and Harleth G. Wiley. 1959. Dynamic Longitudinal and Directional Stability Derivatives for a 45 Deg. Sweptback-Wing Airplane Model at Transonic Speeds. NASA-TM-X-39. NASA. https://ntrs.nasa.gov/citations/19980227088
• Biesiadny, T. J. 1974. “Test Techniques for Obtaining off-Nominal Compressor Data during Engine Tests.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19740022137
• Bigarella, Enda D. V. 2025. “On a Principled Bookkeeping of Aerodynamic Forces and Standard Thrust for Integrated Ducted Fans Consistent with Cfd near-Field Processing.” Preprint, . https://doi.org/10.2139/ssrn.5279234
• 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, William, and Billy. 1980. Influence of Pitching Moment Characteristics on Departure and Uncoordinated Roll Reversal Boundaries for Fighter Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada082335
• Bihrle, William, Jr. 1951. Floating Characteristics of a Plain and a Horn-Balanced Rudder at Spinning Attitudes as Determined from Rotary Tests on a Model of a Typical Low-Wing Personal-Owner Airplane. NACA-TN-2359. NASA. https://ntrs.nasa.gov/citations/19930083095
• Bihrle, W., Jr., and B. Barnhart. 1980. “Departure and Uncoordinated Roll Reversal Boundaries for Fighter Configurations.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1566
• Binkley, Brian A., Grant T. Patterson, and Jerome C. Jenkins. 2015. “A-10 Wing Leading Edge Effects on Engine Stability: Part 2 — Identifying Total Pressure Distortion Sources and the Effects on Engine/Airframe Integration.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-44156
• Birch, Trevor, and John Cleminson. 2004. “Aerodynamic Characteristics of a Square Cross-Section Missile Configuration at Supersonic Speeds.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5197
• Birchfield, E. 1970. “A Comparison of Methods for the Analysis of Wing-Tail Interaction Flutter.” In 8th Aerospace Sciences Meeting. AIAA 1970-80. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-80
• Birk, K., and R. Kuebrich. 1981. “Improved Techniques for the Calibration and Measurement of In-Flightloads.” In 1st Flight Test Conference. AIAA 1981-2502. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2502
• Bischoff, D., and R. Palmer. 1982. “Investigation of Low Order Lateral Directional Transfer Function Models for Augmented Aircraft.” In Guidance and Control Conference. AIAA 1982-1610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1610
• Bischoff, D. E., and R. E. Palmer. 1983. Development of Lateral-Directional Equivalent System Models for Selected U.S. Navy Tactical Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada327418
• Bishop, J. F. W. 1951. “The Application of Virtual Source Distributions to Problems in the Linearized Theory of Supersonic Flows.” Quarterly Journal of Mathematics 2 (1): 291–307. https://doi.org/10.1093/qmath/2.1.291
• Bissell, J. J., C. E. Ritchey, and F. Stevens. 2023. “Measuring the Moment-of-Inertia of a Rigid Body Using a Swing-Pendulum.” Physics Education 58 (6): 065022. https://doi.org/10.1088/1361-6552/acf816
• 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
• Black, Raymond J. 1976. “Realistic Evaluation of Landing Gear Shimmy Stabilization by Test and Analysis.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/760496
• Blackaby, James R., E. Gene Lyman, and John A. Altermann III. 1959. Inlet Performance Characteristics from Wind-Tunnel Tests of a 0.10-Scale Air-Induction System Model of the YF-108A Airplane at Mach Numbers of 2.50, 2.76, and 3.00. NASA-MEMO-7-18-59A. NASA. https://ntrs.nasa.gov/citations/19980228132
• 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
• Blair, A. B., Jr. 1985. Wind-Tunnel Investigation at Supersonic Speeds of a Remote-Controlled Canard Missile with a Free-Rolling-Tail Brake Torque System. NASA-TP-2401. NASA. https://ntrs.nasa.gov/citations/19870008235
• Blair, A., Jr. 1990. “Supersonic Aerodynamic Characteristics of Conformal Carriage Monoplanar Circular Missile Configurations with Low-Profile Quadriform Tail Fins.” In 28th Aerospace Sciences Meeting. AIAA 1990-620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-620
• 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
• Blank, S. 1995. “Passive Techniques for Controlling Flow in Supersonic Wing/body Junctions.” In 13th Applied Aerodynamics Conference. AIAA 1995-1816. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1816
• Blankson, Isaiah, and Paul Hagseth. 1993. “Propulsion/airframe Integration Issues for Waverider Aircraft.” In 31st Aerospace Sciences Meeting. AIAA 1993-506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-506
• 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
• Bloomer, Harry E., William J. Walker, and George L. Pantages. 1953. Altitude Wind Tunnel Investigation of XJ34-WE-32 Engine Performance without Electronic Control. NACA-RM-E51L12. NASA. https://ntrs.nasa.gov/citations/19930087885
• Boatright, William B. 1958. An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash behind Five Pointed-Tip Wings at Supersonic Speeds. NACA-TR-1380. NASA. https://ntrs.nasa.gov/citations/19930092362
• Bochkarev, S. A., and V. P. Matveyenko. 2008. “Panel Flutter of Rotating Circular Shells in a Supersonic Gas Flow.” Computational Continuum Mechanics 1 (3): 25–33. https://doi.org/10.7242/1999-6691/2008.1.3.24
• Bodonyl, Richard J. 1994. Wing-Body Juncture Flows. Defense Technical Information Center. https://doi.org/10.21236/ada281526
• BOECKH. 1954. Determination of the Elastic Constants of Airplane Tires. NACA-TM-1378. NASA. https://ntrs.nasa.gov/citations/19930093852
• 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
• Bogar, T., M. Sajben, and J. Kroutil. 1983. “Response of a Supersonic Inlet to Downstream Perturbations.” In 19th Joint Propulsion Conference. AIAA 1983-2017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2017
• Bogdnoff, Seymour M. 1953. Viscous Effects in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0009823
• Bogue, Rodney K., Harold R. Bagley, David C. Soreide, and David A. Bowdle. 1995. “Coherent Lidar Solution for the HSCT Supersonic Engine Inlet Unstart Problem.” In SPIE Proceedings, vol. 2464, edited by Robert G. Otto, James Lenz. SPIE. https://doi.org/10.1117/12.211479
• 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
• Boland, Joseph, David Riley, and Kevin Citurs. 1993. “Aircraft Control Requirements and Achievable Dynamics Prediction.” In Flight Simulation and Technologies. AIAA 1993-3648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3648
• Bollech, Thomas V., and H. Neale Kelly. 1954. Low-Speed Longitudinal Stability and Lateral-Control Characteristics of a 0.3-Scale Model of the Republic RF-84F Airplane at a Reynolds Number of 9x10(exp 6). NACA-RM-SL54B17. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090022756
• Boo, Koon Yan, Shuhaimi Mansor, and Ainullotfi Abdul-Latif. 2015. “Aerodynamic Damping and Stiffness Determination for Aircraft Wing Flutter Speed Analysis.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2250
• Boothe, E. 1971. “An in-Flight Investigation of Lateral- Directional Dynamics and Rollcontrol Power Requirements for the Landing Approach.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-771
• Boppe, C. 1978. “Computational Transonic Flow about Realistic Aircraft Configurations.” In 16th Aerospace Sciences Meeting. AIAA 1978-104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-104
• Boppe, C. 1984. “Elements of Computational Engine-Airframe Integration.” In 22nd Aerospace Sciences Meeting. AIAA 1984-117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-117
• Borland, C., and D. Rizzetta. 1981. “Nonlinear Transonic Flutter Analysis.” In Dynamics Specialists Conference. AIAA 1981-608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-608
• Bosetti, Paolo, and Stefania Bruschi. 2011. “Springback Evaluation of Parts Made by Single-Point Incremental Sheet Forming.” In Volume 3: Design and Manufacturing. ASMEDC. https://doi.org/10.1115/imece2011-64817
• Boslaugh, David L. n.d. “Research Airplanes without Rockets.” In The Experimental Research Airplanes and the Sound Barrier (Chapter 10), Engineering and Technology History Wiki. https://ethw.org/First-Hand:Research_Airplanes_Without_Rockets_-_Chapter_10_of_the_Experimental_Research_Airplanes_and_the_Sound_Barrier
• Bosworth, J., and J. C. West. 1986. “Real-Time Open-Loop Frequency Response Analysis of Flight Test Data.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9738
• Bottomley, I. E. 1995. “Superplastic Forming and Diffusion Bonding of Aircraft Structures.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 209 (3): 227–31. https://doi.org/10.1243/pime_proc_1995_209_293_02
• Bouhamed, Abir, Warda Ahmed, and Hanen Jrad. 2026. “A Cyclic Shear-Based Identification Framework for Kinematic Hardening: Application to Improved Springback Prediction in Sheet Metal Forming.” Engineering Research Express 8 (14): 145515. https://doi.org/10.1088/2631-8695/ae8b7c
• “Boundary Layer Stability Analysis of a Natural Laminar Flow Glove on the F-Lll TACT Airplane.” 1980. In Viscous Flow Drag Reduction. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865466.0017.0032
• Bowditch, D. N. 1973. “Some Design Considerations for Supersonic Cruise Mixed Compression Inlets.” In AIAA. https://ntrs.nasa.gov/citations/19740001909
• 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, J. S. 1966. Airplane Spinning. NASA. https://ntrs.nasa.gov/citations/19660043787
• Bowman, James S., Jr. 1955a. Emergency Spin-Recovery Device for the 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel. NACA-RM-SL55A25. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029375
• Bowman, James S., Jr. 1955b. Free-Spinning and Recovery Characteristics of a 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel. NACA-RM-SL55H08. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030035
• Bowman, James S., Jr. 1955c. Free-Spinning Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395. Rept-5121. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030040
• Bowman, James S., Jr. 1956a. 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, James S., Jr. 1956b. Free-Spinning and Recovery Characteristics of a 1/19-Scale Model of the North American T-28C Airplane, TED No. NACA AD 3127. NACA-RM-SL56L13. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028470
• Bowman, James S., Jr. 1957. Concluding Report of Free-Spinning, Tumbling, and Recovery Characteristics of a 1/18-Scale Model of the Ryan X-13 Airplane, Coord. No. AF-199. NACA-RM-SL57D11. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028487
• Bowman, James S., Jr. 1958. An Investigation of the Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane with Alternate Nose Configurations with and without Wing Fuel Tanks, TED No. NACA AD 395. NACA-RM-SL58C20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028501
• Bowman, J., Jr. 1970. “Recent Experience with Wind-Tunnel and Analytical Techniques for Prediction of Spin Characteristics of Fighter Aircraft.” In Propulsion and ASW Meeting. AIAA 1970-565. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-565
• Bowman, James S., Jr., and Frederick M. Healy. 1958. Free-Spinning-Tunnel Investigation of a 1/17 Scale Model of the Cessna T-37A Airplane. NASA-MEMO-3-1-59L. NASA. https://ntrs.nasa.gov/citations/19980228403
• Bowman, James S., Jr., and Frederick M. Healy. 1959. Free-Spinning-Tunnel Investigation of a 1/40-Scale Model of the McConnell F-101A Airplane. NASA-MEMO-3-14-59L. NASA. https://ntrs.nasa.gov/citations/19980228366
• Bowman, James S., Jr., and Frederick M. Healy. 1960a. Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of an Unswept-Wing Jet-Propelled Trainer Airplane. NASA-TN-D-381. NASA. https://ntrs.nasa.gov/citations/19980227753
• Bowman, James S., Jr., and Frederick M. Healy. 1960b. Free-Spinning-Tunnel Investigation of a 1/30 Scale Model of a Twin-Jet-Swept-Wing Fighter Airplane. NASA-TM-SX-446. NASA. https://ntrs.nasa.gov/citations/19980223580
• 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
• Boyd, J. 1965. “Optimal Utilization of Supersonic Favorable Interference to Obtain High Lift-Drag Ratios.” In Aircraft Design and Technology Meeting. AIAA 1965-752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-752
• Boyd, William Newsome. 1977. Effect of Chordwise Forces and Deformations and Deformations Due to Steady Lift on Wing Flutter. Defense Technical Information Center. https://doi.org/10.21236/ada053640
• 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
• Boyer, Rodney R. 2003. “Titanium Airframe Applications: Brief History, Present Applications and Future Trends.” In Materials science forum, vol. 426-432. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.426-432.643
• Boylan, D., D. Carver, D. Stallings, and L. Trimmer. 1978. “Measurement and Mapping of Aerodynamic Heating Using a Remote Infrared Scanning Camera in Continuous Flow Wind Tunnels.” In 10th Aerodynamic Testing Conference. AIAA 1978-799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-799
• Bozeman, Michael Dwain, and Jan-renee Carlson. 2022. Identification of Best Practices for Predicting Inlet Performance Using FUN3D Part 2: Installed Inlets. Langley Research Center. https://ntrs.nasa.gov/citations/20210022214
• Bradley, R., and I. Bhateley. 1983. “Computational Aerodynamic Design of Fighter Aircraft Progress and Pitfalls.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2063
• Brady, W. G., H. G. Maier, and Walter P. Targoff. 1954. Part 2: Swept Wings: Subsonic Flutter Model Test of Wings Carrying Heavy Tip Pods. Defense Technical Information Center. https://doi.org/10.21236/ad0055205
• Braithwaite, W., E. Graber Jr., and C. Mehalic. 1973. “The Effect of Inlet Temperature and Pressure Distortion on Turbojet Performance.” In 9th Propulsion Conference. AIAA 1973-1316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1316
• Brajnikoff, George B., and John F. Stroud. 1953. Experimental Investigation of the Effect of Entrance Width-to-Height Ratio on the Performance of an Auxiliary Scoop-Type Inlet at Mach Numbers from 0 to 1.3. NACA-RM-A53E28. NASA. https://ntrs.nasa.gov/citations/19930087644
• Brakes and Skid Controls Committee A-5A Wheels. 1979. Wheel & Brake Design and Test Requirements for Military Aircraft. https://doi.org/10.4271/arp1493
• Brakes and Skid Controls Committee A-5A Wheels. 2007a. Brake Systems, Wheel, Aircraft, Design Of. https://doi.org/10.4271/as8584
• Brakes and Skid Controls Committee A-5A Wheels. 2007b. Wheel and Brake Design and Test Requirements for Military Aircraft. https://doi.org/10.4271/arp1493a
• Brakes and Skid Controls Committee A-5A Wheels. 2008. Brake Systems, Wheel, Military Aircraft. https://doi.org/10.4271/as8584a
• Brakes and Skid Controls Committee A-5A Wheels. 2010a. Maintainability Recommendations for Aircraft Wheel and Brake Design. https://doi.org/10.4271/arp813b
• Brakes and Skid Controls Committee A-5A Wheels. 2010b. Wheel Roll on Rim Criteria for Aircraft Application. https://doi.org/10.4271/arp1786b
• Brakes and Skid Controls Committee A-5A Wheels. 2012. Aircraft Brake Temperature Monitor System (BTMS). https://doi.org/10.4271/as1145b
• Brakes and Skid Controls Committee A-5A Wheels. 2013. Wheel and Hydraulically Actuated Brake Design and Test Requirements for Military Aircraft. https://doi.org/10.4271/arp1493c
• Brakes and Skid Controls Committee A-5A Wheels. 2017a. Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design. https://doi.org/10.4271/arp813c
• Brakes and Skid Controls Committee A-5A Wheels. 2017b. Wheel Roll on Rim Criteria for Aircraft Applications. https://doi.org/10.4271/arp1786c
• Brakes and Skid Controls Committee A-5A Wheels. 2019. Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility. https://doi.org/10.4271/arp1070e
• Brakes and Skid Controls Committee A-5A Wheels. 2021. Aircraft Brake Temperature Monitoring. https://doi.org/10.4271/arp6812
• Brakes and Skid Controls Committee A-5A Wheels. 2022. Aircraft Brake Quality Assurance Rejected Takeoff Test History and Considerations. https://doi.org/10.4271/air6417
• 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
• 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, and Gautam Shah. 1990. “Unsteady Aerodynamic Characteristics of a Fighter Model Undergoing Large-Amplitude Pitching Motions at High Angles of Attack.” In 28th Aerospace Sciences Meeting. AIAA 1990-309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-309
• Braski, D. N., and D. M. Royster. 1966. X-Ray Measurement of Residual Stresses in Titanium Alloy Sheet. NASA-TM-X-57930. NASA. https://ntrs.nasa.gov/citations/19660028823
• Braski, D. N., and D. M. Royster. 1967. “X-Ray Measurement of Residual Stresses in Titanium Alloy Sheet.” In ANNUAL CONFERENCE ON APPLICATIONS OF X-RAY ANALYSIS. https://ntrs.nasa.gov/citations/19680043221
• Braun, James, and Steve Podleski. 2019. “Propulsion Aerodynamics Workshop Special Topics: Supersonic Channeled Centerbody Inlet.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4021
• Breakwell, J. 1976. “Optimal Flight-Path-Angle Transitions in Minimum Time Airplane Climbs.” In Astrodynamics Conference. AIAA 1976-795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-795
• Brès, Guillaume, Ehab Fares, David Williams, and Tim Colonius. 2011. “Numerical Simulations of the Transient Flow Response of a 3D, Low-Aspect-Ratio Wing to Pulsed Actuation.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3440. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3440
• Brewer, Gerald W. 1946. An Estimation of the Flying Qualities of the Kaiser Fleetwing All-Wing Airplane from Tests of a 1/7-Scale Model, TED No. NACA 2340. NACA-RM-L6J18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050031173
• Brewer, Given A. 1953. Predicting Wing Lift Loads, PBY-6A from Accelerometer Measurements. Defense Technical Information Center. https://doi.org/10.21236/ad0009365
• Brewer, H. 1974. “Parameters Affecting Aircraft Tire Control Forces.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-966
• Brewer, H. K. 1975. “Measurement of Steady State and Transient Aircraft Tire Forces.” Tire Science and Technology 3 (2): 111–27. https://doi.org/10.2346/1.2167197
• Bridges, David. 2005. “Finite Wing Lift-Curve Slope Calculations Using Lifting-Line Theory.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4839
• Briesenick, D., M. Liewald, and K. R. Riedmueller. 2021. “New Sheet Metal Forming Process for Springback Reduction by Continuous Stress Superposition.” IOP Conference Series: Materials Science and Engineering 1157 (1): 012030. https://doi.org/10.1088/1757-899x/1157/1/012030
• Briggs, Donald W. 1954. Flight Determination of the Buffeting Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. NACA-RM-L54C17. NASA. https://ntrs.nasa.gov/citations/19930088191
• Briggs, M. 1986. “The Wavethruster Configuration Concept for High Lift/low Drag Supersonic Missiles.” In 24th Aerospace Sciences Meeting. AIAA 1986-571. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-571
• Briggs, M. M., R. E. Reed, and J. N. Nielsen. 1982. Wing-Alone Aerodynamic Characteristics to High Angles of Attack at Subsonic and Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada125764
• Brincklow, J. R., and D. F. Hunsaker. 2021. “Aileron Size and Location to Minimise Induced Drag during Rolling-Moment Production at Zero Rolling Rate.” Aeronautical Journal 125 (1287): 807–29. https://doi.org/10.1017/aer.2020.139
• Brincklow, Joshua R., Zachary S. Montgomery, and Douglas F. Hunsaker. 2021. “Controlling Roll-Yaw Coupling with Aileron Placement and Wing Twist.” In AIAA Scitech 2021 Forum. AIAA 2021-0327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0327
• Brincklow, J. R., Z. S. Montgomery, and D. F. Hunsaker. 2024. “Controlling Roll-Yaw Coupling with Aileron and Twist Design.” Aeronautical Journal 128 (1327): 1961–73. https://doi.org/10.1017/aer.2024.21
• Brindley, William J., Paul A. Bartolotta, James L. Smialek, and Michael P. Brady. 2005. Environmental Studies on Titanium Aluminide Alloys. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/20050179463
• Brinich, Paul F. 1961. Recovery Temperature, Transition, and Heat Transfer Measurements at Mach 5. NASA-TN-D-1047. NASA. https://ntrs.nasa.gov/citations/19980228285
• “Bristol Siddeley Viper Mark 520 Turbojet: A Description of the Development Background to This Small Turbojet Engine, Its Technical Features and Performance.” 1963. Aircraft Engineering and Aerospace Technology 35 (2): 39–43. https://doi.org/10.1108/eb033682
• Brock, B. 1977. “Influence of Structural Dynamics on Fighter Aircraft Design.” In 18th Structural Dynamics and Materials Conference. AIAA 1977-434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-434
• Brockman, R. A., and W. R. Braisted. 1994. “Critical Speed Estimation for Aircraft Tires.” Tire Science and Technology 22 (2): 121–44. https://doi.org/10.2346/1.2139536
• Brodersen, Olaf. n.d. “Computation of Engine-Airframe Installation Drag.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM). Springer Berlin Heidelberg. https://doi.org/10.1007/3-540-32382-1_11
• Brodersen, O., and A. Stuermer. 2001. “Drag Prediction of Engine-Airframe Interference Effects Using Unstructured Navier-Stokes Calculations.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-2414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2414
• 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, J., P. Stainback, and C. Brooks Jr. 1980. “Additional Flow Quality Measurements in the Langley Research Center 8-Foot Transonic Pressure Tunnel.” In 11th Aerodynamic Testing Conference. AIAA 1980-434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-434
• Browman, James S., Jr., and Frederick M. Healy. 1959. Free-Spinning-Tunnel Investigation of a 1/25-Scale Model of the Chance Vought F8U-1P Airplane. NASA-TM-SX-196. NASA. https://ntrs.nasa.gov/citations/19980237091
• Brown, Clinton E. 1946. Theoretical Lift and Drag of Thin Triangular Wings at Supersonic Speeds. NACA-TR-839. NASA. https://ntrs.nasa.gov/citations/19930090940
• Brown, Clinton E. 1950. The Reversibility Theorem for Thin Airfoils in Subsonic and Supersonic Flow. NACA-TR-986. NASA. https://ntrs.nasa.gov/citations/19930092046
• Brown, Stuart C. 1959. Predicted Static Aeroelastic Effects on Wings with Supersonic Leading Edges and Streamwise Tips. NASA-MEMO-4-18-59A. NASA. https://ntrs.nasa.gov/citations/19980228294
• Brown, Robert. 1961. “Supersonic Trim Drag.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/610096
• Brown, R. 1978. “Integration of a Variable Cycle Engine Concept in a Supersonic Cruise Aircraft.” In 14th Joint Propulsion Conference. AIAA 1978-1049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1049
• Brown, Anthony. 2002. “Negative Speed Stability, a Factor in Transport Airplane Icing Upsets.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-3051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3051
• Brown, Clinton E., and Mac C. Adams. 1948a. Damping in Pitch and Roll of Triangular Wings at Supersonic Speeds. NACA-TN-1566. NASA. https://ntrs.nasa.gov/citations/19930082378
• Brown, Clinton E., and Mac C. Adams. 1948b. Damping in Pitch and Roll of Triangular Wings at Supersonic Speeds. NACA-TR-892. NASA. https://ntrs.nasa.gov/citations/19930091961
• Brown, Clinton E., and Harry S. , R. Heinke. 1956. Preliminary Wind-Tunnel Tests of Triangular and Rectangular Wings in Steady Roll at Mach Numbers of 1.62 and 1.92. NACA-TN-3740. NASA. https://ntrs.nasa.gov/citations/19930084532
• Brown, W. W., and D. A. Redwine. 1948. Stess Analysis of Landing Gear XB-36,. Defense Technical Information Center. https://doi.org/10.21236/adb812167
• Brown, W. F., Jr., R. T. Bubsey, and G. B. Espey. 1961b. A Preliminary Report on the NASA Sheet Alloy Screening Program for Mach 3 Transport Skins. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19620003089
• Brown, W. F., Jr., M. H. Jones, and A. J. Repko. 1961a. Influence of Sheet Thickness on Sharp-Edge-Notch Properties of a Beta Titanium Alloy at Room and Low Temperatures. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19620001767
• Brown, W. F., Jr., and A. J. Repko. 1962. Influence of Cold Rolling and Aging on Sharp-Notch Properties of Beta Titanium Sheet. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19630010627
• Brown, W. F., Jr., and J. L. Shannon Jr. 1963. Effects of Several Production and Fabrication Variables on Sharp Notch Properties of 541-2.5sn Titanium Alloy Sheet at Liquid Hydrogen Temperature. NASA-RP-201. NASA. https://ntrs.nasa.gov/citations/19640013362
• Brümmer, A., and D. Hummel. 1993. “Low- Speed Aerodynamic Characteristics of a Slender Wing with Vertical Fins.” In Orbital Transport. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-45720-3_28
• Bruner, H. 1983. “An Improved Method for Predicting Lateral-Directional Dynamic Stability Characteristics.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/830711
• Brunner, Michael T. 1996. High-Fidelity Simulation as a Low Cost Enhancement to Flight Test,. Defense Technical Information Center. https://doi.org/10.21236/ada305291
• 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
• Bruschi, Stefania, and Andrea Ghiotti. 2018. “Cryogenic Machining of Titanium Alloys.” In Machining of Light Alloys. CRC Press. https://doi.org/10.1201/b22153-7
• Bryson, A. E. 1952. “Note on Aerodynamic Heating with a Variable Surface Temperature.” Quarterly of Applied Mathematics 10 (3): 273–75. https://doi.org/10.1090/qam/49749
• Buang, M. S., S. A. Abdullah, and J. Saedon. 2015. “Effect of Die and Punch Radius on Springback of Stainless Steel Sheet Metal in the Air v-Die Bending Process.” Journal of Mechanical Engineering and Sciences 8: 1322–31. https://doi.org/10.15282/jmes.8.2015.7.0129
• 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
• Bui, Van Hung. n.d. “Strategies in 3 and 5-Axis Abrasive Water Jet Machining of Titanium Alloys.” PhD diss., Toulouse 3. https://doi.org/10.70675/35fb214azc042z49ebzab60za3c1ead2749d
• Bulman, M. J., P. W. Stout, and R. Fernandez. 1997. Improved Hypersonic Inlet Performance Using Validated Strut Compression Designs. Aerojet. https://ntrs.nasa.gov/citations/19990080047
• Bunge, Roberto, and Ilan Kroo. 2018. “High Angle of Attack Aerodynamic Model Identification for Spin Recovery Simulation Using Non-Parametric Smoothing Functions.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0772
• 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
• Burcham, F. W., Jr., and P. G. Batterton. 1976. “Flight Experience with a Digital Integrated Propulsion Control System on an F-111E Airplane.” In Propulsion Conference. https://ntrs.nasa.gov/citations/19760059445
• 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., Donald H. Gatlin, and James F. Stewart. 1995. “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., Glenn B. Gilyard, and Paul A. Gelhausen. 1990. “Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes.” In Society of Automotive Engineers (SAE), Inc. Aerotech Conference. https://ntrs.nasa.gov/citations/19910004147
• 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 W., Jr., and Ronald J. Ray. 1987. The Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane. AIAA PAPER 87-2877. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19880027031
• Burcham, Frank W., Jr., Ronald J. Ray, Timothy R. Conners, and Kevin R. Walsh. 1997. Propulsion Flight Research at NASA Dryden from 1967 to 1997. NASA/TP-1998-206554. NASA. https://ntrs.nasa.gov/citations/19980218800
• Burcham, F. W., Jr., G. A. Trippensee, D. F. Fisher, and T. W. Putnam. 1986. Summary of Results of NASA F-15 Flight Research Program. AIAA PAPER 86-9761. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19860052326
• Burchett, Bradley, Justin Paul, Joseph Vasile, and Joshua Bryson. 2021. A High Fidelity Roll Dependent Aerodynamic Model for a Long Range High Speed Missile. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1141614
• Burchitz, I. A. 2008. “Improvement of Springback Prediction in Sheet Metal Forming.” PhD diss.. https://doi.org/10.3990/1.9789036526562
• Bureerat, Sujin. 2026. “Static Aeroelasticity.” In Computational Aeroelasticity. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-8903-6_6
• Burgan, Elmer T., and Fletcher C. Paddison. 1974. Surface Effect Takeoff and Landing System (SETOLS). Defense Technical Information Center. https://doi.org/10.21236/ada000101
• Burk, Sanger M., and Burton E. Hultz. 1951. Static Longitudinal Stability and Dynamic Characteristics at High Angles of Attack and at Low Reynolds Numbers of a Model of the X-3 Supersonic Research Airplane. NACA-RM-L50L19. NASA. https://ntrs.nasa.gov/citations/19930086522
• Burk, S. M., Jr., J. S. Bowman Jr., and W. L. White. 1977. Spin-Tunnel Investigation of the Spinning Characteristics of Typical Single-Engine General Aviation Airplane Designs. 1. Low-Wing Model A: Effects of Tail Configurations. NASA-TP-1009. NASA. https://ntrs.nasa.gov/citations/19770026167
• Burk, Sanger H., Jr., and Frederick M. Healy. 1955. Free-Spinning-Tunnel Investigation to Determine the Effect of Spin-Recovery Rockets and Thrust Simulation on the Recovery Characteristics of a 1/21-Scale Model of the Chance Vought F7U-3 Airplane, TED No. NACA AD 3103. NACA-RM-SL55A04. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029372
• Burke, Brian J., and Jonathan Poggie. 2023. “URANS Simulations of Inlet-Isolator Unstart at Mach 4.9.” In AIAA SCITECH 2023 Forum. AIAA 2023-1467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1467
• Burkhardt, H. 1943. “Stressing of Aircraft Wheels and Brake.” Journal of the Royal Aeronautical Society 47 (389): 133–37. https://doi.org/10.1017/s0368393100105875
• Burkhart, T. 1980. “Numerical Application of Evvard’s Supersonic Wing Theory to Flutter Analysis.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-741
• Burkhart, Eve Taylor, and Larry D. Hefti. 2020. “Advancements of Superplastic Forming and Diffusion Bonding of Titanium Alloys for Heat Critical Aerospace Applications.” SAE International Journal of Advances and Current Practices in Mobility 02 (3): 1202–8. https://doi.org/10.4271/2020-01-0033
• Bürki-Cohen, Judith, and Andrea Sparko. 2008. “Airplane Upset Prevention Research Needs.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2008-6871. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6871
• Burns, B. R. A. 1965. “The Effects of Instrumentation Errors on Stability Derivative Measurements.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50005-1
• Burr, R. 1968. “A Control System Concept for an Axisymmetric Supersonic Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-581
• Burris, P. 1966. “Dynamic Test Method for Supersonic Inlet/engine Development.” In 2nd Aerodynamic Testing Conference. AIAA 1966-741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-741
• Burrows, Travis J., Bojan Vukasinovic, and Ari Glezer. 2017. “Fluidic Control of an Aggressive Offset Diffuser for a Supersonic Inlet.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-4304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4304
• 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
• Burstadt, P., J. Calogeras, and R. Coltrin. 1971. “Instantaneous and Dynamic Analysis of Supersonic Inlet-Engine Compatibility.” In 7th Propulsion Joint Specialist Conference. AIAA 1971-667. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-667
• Bushnell, D. 1990. “Supersonic Aircraft Drag Reduction.” In 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1990-1596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1596
• Bustard, Andrew, Benjamin L. Bemis, and Thomas J. Juliano. 2024. “Global Time-Resolved Measurements of Axisymmetric Inlet/Isolator Unstart Induced by Mass Injection.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3893
• Butler, R. W. 1976a. Aircraft Motion Sensitivity to Cross and Cross-Coupling Damping Derivatives. Defense Technical Information Center. https://doi.org/10.21236/ada032654
• Butler, R. W. 1976b. A Wind Tunnel Captive Aircraft Testing Technique. Defense Technical Information Center. https://doi.org/10.21236/ada023690
• Butler, R. W., and T. F. Langham. 1978. Sensitivity of Aircraft Spinning Motion to Dynamic Cross-Coupling and Acceleration Derivatives. Defense Technical Information Center. https://doi.org/10.21236/ada060516
• 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
• Bylya, Olga I., Rudolf A. Vasin, and Paul L. Blackwell. 2016. “The Mechanics of Superplastic Forming: How to Incorporate and Model Superplastic and Superplastic-Like Conditions.” In Materials science forum, vol. 838-839. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.838-839.468
• Byrdsong, T. A. 1977. Flight Measurements of Lifting Pressures for a Thin Low-Aspect-Ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds. NASA-TM-X-3405. NASA. https://ntrs.nasa.gov/citations/19770010053
• Byreddy, Chakradhar, Ramana V. Grandhi, and Philip Beran. 2003. Dynamic Aeroelastic Instabilities of an Aircraft Wing with Underwing Store in Transonic Regime. Defense Technical Information Center. https://doi.org/10.21236/ada417124
• Byrer, T. G., and F. W. Boulger. 1970. “Heavy Press Forging of Large Titanium Alloy Parts for Aircraft and Aerospace Applications.” In The Science, Technology and Application of Titanium. Elsevier. https://doi.org/10.1016/b978-0-08-006564-9.50018-x
• Byun, Chansup, and Guru Guruswamy. 1996a. “Aeroelastic Computations on Wing-Body-Control Configurations on Parallel Computers.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1389
• Byun, Chansup, and Guru Guruswamy. 1996b. “Static Aeroelasticity Computations for Flexible Wing-Body-Control Configurations.” In 6th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1996-4059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4059
• Caddy, Michael J., and William K. Arnold. 1988. “Energy Maneuverability and Engine Performance Requirements.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/88-gt-303
• Cai, J. 2024. “Research on Flight Test Method and Risk Control of Civil Aircraft with Maximum Practicable Rate for Rotation.” IET Conference Proceedings 2023 (43): 29–31. https://doi.org/10.1049/icp.2024.0625
• 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
• Calder, P., and P. Gupta. 1978. “Engine Options for Supersonic Cruise Aircraft.” In 14th Joint Propulsion Conference. AIAA 1978-1054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1054
• Callan, Kimberly. 2012. “Test and Analysis of the Mass Properties for the PRANDTL-D Aircraft.” Proceedings of the Wisconsin Space Conference. https://doi.org/10.17307/wsc.v0i0.50
• Calogeras, J. 1969. “Supersonic Wind Tunnel Investigation of Inlet- Engine Compatibility.” In 5th Propulsion Joint Specialist. AIAA 1969-487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-487
• Calvin, Arrah C., Nikhil Khobragade, Unnikrishnan Sasidharan, and Rajan Kumar. 2022. “Computational and Experimental Evaluation of Unstart Characteristics of a Mixed-Compression Intake.” In AIAA AVIATION 2022 Forum. AIAA 2022-3712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3712
• Caminez, Harold. 1931. “Trend in Aircraft-Engine Development.” Journal of Fluids Engineering 53 (1): 17–22. https://doi.org/10.1115/1.4022553
• Campbell, Robert C. 1954. Performance of a Supersonic Ramp Inlet with Internal Boundary-Layer Scoop. NACA-RM-E54I01. NASA. https://ntrs.nasa.gov/citations/19930088437
• Campbell, Robert C. 1956. Performance of Supersonic Ramp-Type Side Inlet with Combinations of Fuselage and Inlet Throat Boundary-Layer Removal. NACA-RM-E56A17. NASA. https://ntrs.nasa.gov/citations/19930089340
• Campbell, George S. 1959. “Characteristics of Slender Wing-Body Combinations with Folding Wings: A Method of Computing Aerodynamic Loads on Slender Bodies of Complicated Cross-Section.” Aircraft Engineering and Aerospace Technology 31 (1): 13–20. https://doi.org/10.1108/eb033068
• Campbell, D. 1973. “F-12 Series Aircraft Propulsion System Performance and Development.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-821
• Campbell, James D. 1991. “A Comparison of Fluids Used to Superabrasively Machine a Titanium Alloy.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-321
• Campbell, Newton H., Jared A. Grauer, and Irene M. Gregory. 2021. “Loss of Control Detection for Commercial Transport Aircraft Using Conditional Variational Autoencoders.” In AIAA Scitech 2021 Forum. AIAA 2021-0778. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0778
• Campos, L. 1989. “Comparison of Non-Linear Pitch Stability Theory with Data from BAFR (Basic Aircraft for Flight Research).” In Aircraft Design and Operations Meeting. AIAA 1989-2041. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2041
• Candida, Polliana, Aline Souza de Paula, and Sergio Carneiro. 2019. “Aeroelastic Stability Analysis of a Rectangular Wing with PID Control.” In DINAME2019. ABCM. https://doi.org/10.26678/abcm.diname2019.din2019-0103
• Canin, Dan. 2019. “F-35 High Angle of Attack Flight Control Development and Flight Test Results.” In AIAA Aviation 2019 Forum. AIAA 2019-3227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3227
• Canoro, P. A., and H. N. Kelly. 1955. Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel. Lateral Control and Directional Stability and Control Characteristics of Model Equipped with Drooped, Supersonic-Type, Elliptical Wing-Root Inlet. NACA-RM-SL55J10. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710073550
• Cao, Lina, G. F. Yao, and M. Wang. 2020. “Hopf Bifurcation on Heated Curved Panel Flutter in Supersonic Air Flow.” Preprint, . https://doi.org/10.22541/au.158594503.37165006
• Capey, E. C. 1961. “Transient Temperature Distributions in an Insulated Multi-Spar Wing: An Approximate Method of Solution for a Structure Subjected to Aerodynamic Heating Based on a System of Regions Having Similar Rates of Temperature Rise.” Aircraft Engineering and Aerospace Technology 33 (10): 282–88. https://doi.org/10.1108/eb033463
• Capone, F., E. Bare, D. Hollenback, and R. Hutchison. 1984. “Subsonic/supersonic Aerodynamic Characteristics for a Tactical Supercruiser.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2192
• 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
• Carafoli, Elie. 1969a. “The Calculation of the Overall Forces and Moments on Wings with Trailing Edges of Arbitrary Planform Shape.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50007-8
• Carafoli, Elie. 1969b. “CRUCIFORM WINGS.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50012-1
• Carafoli, Elie. 1969c. “Recapitulative Survey of the Equations of Motion of Perfect Fluids in Supersonic Flow.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50005-4
• Carafoli, Elie. 1969d. “Simple or Cruciform Wing Fitted with a Conical Body.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50013-3
• Carafoli, Elie. 1969e. “Some Theoretical Considerations on Wings with Curved Leading Edges and Wing-Fusiform Body Systems.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50016-9
• Carafoli, Elie. 1969f. “Study of Ordinary Delta Wings.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50008-x
• Carafoli, Elie. 1969g. “Study of Polygonal Wings.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50011-x
• Carafoli, Elie. 1969h. “Trapezoidal and Rectangular Wings.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50010-8
• Carafoli, Elie. 1969i. “Yawed Delta Wings. Delta Wings with General Variation of Incidence.” In Wing Theory in Supersonic Flow. Elsevier. https://doi.org/10.1016/b978-0-08-012330-1.50009-1
• Cardoso, Weidher Possidonio, William Regone, and Rodrigo Furlan de Assis. 2026. “Artificial Neural Network-Based Springback Prediction in Sheet Metal Bending for Industry 4.0 Applications.” In Springer Proceedings in Business and Economics. Springer Nature Switzerland. https://doi.org/10.1007/978-3-032-23282-3_33
• Cardoso Navarro, Lucas, and Luiz Carlos Sandoval. 2019. “Aircraft Braking Dynamics and Brake System Modeling for Fault Detection and Isolation.” In DINAME2019. ABCM. https://doi.org/10.26678/abcm.diname2019.din2019-0181
• Cardoso Navarro, Lucas, and Luiz Carlos Sandoval Goes. 2018. “Aircraft Braking Dynamics and Brake System Modeling for Fault Detection and Isolation.” In Linköping Electronic Conference Proceedings, vol. 156. Linköping University Electronic Press. https://doi.org/10.3384/ecp1815634
• Carico, Dean. 1998. Flight Test Automation Options. Defense Technical Information Center. https://doi.org/10.21236/ada350677
• Carlin, C. M., I. Frisch, J. J. Kolden, et al. 2003. Supersonic Test of the 10-Inch Bifurcated Two-Stage Supersonic Inlet (BTSSI). NASA/CR-2003-212313. NASA. https://ntrs.nasa.gov/citations/20030065839
• Carlson, H. 1964. “A Numerical Method of Estimating and Optimizing the Supersonic Aerodynamic Characteristics of Wings of Arbitrary Planform.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-590
• Carlson, H. W., B. L. Shrout, and C. M. Darden. 1984. Wing Design with Attainable Thrust Considerations. AIAA PAPER 84-2194. Kentron International, Inc. https://ntrs.nasa.gov/citations/19840058559
• Carpenter, Mark R., David M. Sitz, and David C. Nelson. 1996. “The KEEP EAGLE F-15E High Angle-of-Attack Flight Test Program.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/965574
• Carrier, Gerald, Doyle Knight, Khaled Rasheed, and Xavier Montazel. 2001. “Multi-Criteria Design Optimization of Two-Dimensional Supersonic Inlet.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-1064. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1064
• Carrino, L., Valentino Paradiso, Stefania Franchitti, Antonino Squillace, and Salvatore Russo. 2012. “Superplastic Forming/Diffusion Bonding of a Titanium Alloy for the Realization of an Aircraft Structural Component in Multi-Sheets Configuration.” In Key engineering materials, vol. 504-506. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.504-506.717
• Carter, R. V. 1960. Development of Titanium Alloy Casting Method. Defense Technical Information Center. https://doi.org/10.21236/ad0250925
• Carter, Roger V. 1970. “Titanium Applications for Supersonic Airplanes.” In The Science, Technology and Application of Titanium. Elsevier. https://doi.org/10.1016/b978-0-08-006564-9.50124-x
• Carter, John F., and Christopher J. Nagy. 1995. The NASA Landing Gear Test Airplane. NASA-TM-4703. NASA. https://ntrs.nasa.gov/citations/19960012281
• Casner, Stephen. 2010. “Human Factors of Aircraft Loss of Control Accidents.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8006
• Cass, S., and C. Ball. 1988. “Planform Effects on High Speed Civil Transport Design.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4487
• Cassetti, Michele. 1978. “On the Conventional Definitions of Thrust/Drag of an Aircraft Equipped with a Turbojet Engine.” Aircraft Engineering and Aerospace Technology 50 (9): 4–7. https://doi.org/10.1108/eb035480
• Casteel, G., and C. Weyl. 1970. “A Design Approach to Provide Satisfactory Spin Characteristics for Amodern Fighter Aircraft.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-928
• 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
• Catalano, George D., and Walter B. Sturek. 2001. A Numerical Investigation of Supersonic Flow around Aft Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada395936
• Cavanaugh, Michael. 2003. “The Use of Rudder Trailing Edge T-Strips to Improve Dutch Roll Damping.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5613
• Cazier, F., Jr., and M. Kehoe. 1986. “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
• Cecrdle, Jiri. 2011. “Assessment of Aileron Tab Installation Influence to Aircraft Flutter Characteristics.” In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2011-1849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1849
• Çeliktaş, Erhan, Ahmet Topuz, and Zafer Kazancı. 2012. “Friction and Wear Behaviors of Aircraft Brake Linings Material.” Aircraft Engineering and Aerospace Technology 84 (5): 279–86. https://doi.org/10.1108/00022661211255458
• Cen, Fei, Qing Li, Mark H. Lowenberg, Simon Neild, and Yinan Kong. 2018. “Flight Performance and Stability Analysis of Impaired Aircraft Using Constrained Bifurcation and Continuation Method.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0775. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0775
• 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., and M. Madson. 1993. “TranAir Applications to Predicting Transonic Aircraft/store Loads.” In 31st Aerospace Sciences Meeting. AIAA 1993-855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-855
• Cerantola, David J., Dan Handford, and Pradeep Dass. 2024. “Simulating Wing Thermal Loads at Supersonic Speeds.” In AIAA SCITECH 2024 Forum. AIAA 2024-2295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2295
• “CFD Applications to Engine/Airframe Integration.” 1986. In Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865763.0219.0255
• Chaderjian, Neal. 1992. “Navier-Stokes Prediction of Large-Amplitude Delta-Wing Roll Oscillations Characterizing Wing Rock.” In Guidance, Navigation and Control Conference. AIAA 1992-4428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4428
• Chaderjian, Neal, and Lewis Schiff. 1993. “Navier-Stokes Prediction of a Delta Wing in Roll with Vortex Breakdown.” In 11th Applied Aerodynamics Conference. AIAA 1993-3495. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3495
• Chaderjian, Neal M., and Lewis B. Schiff. 1994. “Navier-Stokes Prediction of Large-Amplitude Forced and Free-to-Roll Delta-Wing Oscillations.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19960033241
• Chaderjian, Neal M., and Lewis B. Schiff. 2000. “16C. Large-Amplitude, High-Rate Roll Oscillations of a 65° Delta Wing at High Incidence.” In Verification and Validation Data for Computational Unsteady Aerodynamics. https://ntrs.nasa.gov/citations/20010009857
• Chadrjian, Neal, and Lewis Schiff. 1995. “Navier-Stokes Analysis of a Delta Wing in Static and Dynamic Roll.” In 13th Applied Aerodynamics Conference. AIAA 1995-1868. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1868
• Chalal, Hocine, Sever-Gabriel Racz, and Tudor Balan. 2012a. “Investigation of Thick Sheet AHSS Springback in Combined Bending under Tension.” In Key engineering materials, vol. 504-506. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.504-506.791
• Chaloner, Kathryn, and Isabella Verdinelli. 1995. “Bayesian Experimental Design: A Review.” Statistical Science 10 (3): 273–304. https://doi.org/10.1214/ss/1177009939
• Chamberlain, D. 1968. “Measurement of Drag from Interaction of Jet Exhaust and Airframe.” In 3rd Aerodynamics Testing Conference. AIAA 1968-395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-395
• Chambers, Joseph R., and Robert M. Hall. 2003. “Historical Review of Uncommanded Lateral-Directional Motions at Transonic Conditions.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030010279
• Chandler, Frank O., and Ricardo Montes. 2019. “A CFD Investigation of a Diverterless Supersonic Inlet of Ellipsoidal Entrance Shape.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4274
• Chandra, A. 1987. “Real-Time Identification and Control of Springback in Sheet Metal Forming.” Journal of Engineering for Industry 109 (3): 265–73. https://doi.org/10.1115/1.3187128
• Chandrasekharan, Reuben. 1988. “Improved Method of Analyzing Takeoff Performance Data.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4509
• Chandrashekar, S., and N. Kiran. 1981. “A Cost Effective Method for the Control of Roll Due to Side Slip on a Low Speed Aircraft.” In 1st Flight Test Conference. AIAA 1981-2422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2422
• Chang, J. C. 1970. “FORMING Ti–6Al–4V SHEET METAL IN FOUR HEAT TREATED CONDITIONS.” In The Science, Technology and Application of Titanium. Elsevier. https://doi.org/10.1016/b978-0-08-006564-9.50118-4
• Chang, J. B. 1984. “Durability and Damage-Tolerance Design and Analysis of Titanium Airframe Structures.” In Fracture 84. Elsevier. https://doi.org/10.1016/b978-1-4832-8440-8.50377-x
• Chang, Shupeng. 2024. “Achievement of Martensite Strengthening in Titanium Alloy Thin-Walled Components via Non-Equilibrium Hot Stamping.” In Materials Research Proceedings, vol. 44. Materials Research Forum LLC. https://doi.org/10.21741/9781644903254-79
• Chang, Juntao, and Wen Bao. 2006. “Observers Design for Shock Position of Supersonic Inlet Based on Equilibrium Manifold.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4305
• Chang, Borchin, Harry Kwatny, Elie R. Ballouz, and David Hartman. 2016. “Aircraft Trim Recovery from Highly Nonlinear Upset Conditions.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0880. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0880
• Chang, B-C., Harry Kwatny, Christine Belcastro, and Celeste Belcastro. 2008. “Aircraft Loss-of-Control Accident Prevention: Switching Control of the GTM Aircraft with Elevator Jam Failures.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6507
• Chang, Craig F., and Thomas E. Ulbricht. 2002. “Asymmetric Approach in Solving Aircraft Brake Vibration.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2002-01-2948
• Chang, Nan, Wei Yang, Jian Wang, and Wei Wang. 2010. “Design Optimization of Composite Wing Box for Flutter and Stiffness.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1510
• Chapel, David. 1996. “Benefits of Simultaneous Engine/airframe Performance Interaction.” In 6th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1996-4144. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4144
• Chapman, Bert. 2018. “History of Jet Fighters.” In Global Defense Procurement and the F-35 Joint Strike Fighter. Springer International Publishing. https://doi.org/10.1007/978-3-030-01367-7_2
• Chapman, Chase H., Caleb Robb, and Ryan C. Paul. 2024. “Investigation of Roll-Yaw Coupling for Fixed-Wing Unmanned Air Vehicles.” In AIAA SCITECH 2024 Forum. AIAA 2024-2648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2648
• “Chapter 10. Natural Motions of Rigid Aircraft.” 1994. In Control of Spacecraft and Aircraft. Princeton University Press. https://doi.org/10.1515/9781400880034-013
• “Chapter 2. Aerodynamics of Thin Wings at Subsonic Speeds.” 1960. In High Speed Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400874941-003
• “Chapter 2. Wing-Body Interference at Subsonic Speeds.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-008
• “Chapter 3. Aerodynamics of Thin Wings at Supersonic Speeds.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-005
• “Chapter 3. Aerodynamics of Thin Wings at Supersonic Speeds.” 1960. In High Speed Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400874941-004
• “Chapter 3. Dynamics of Aircraft Motion.” 2005. In Flight Dynamics. Princeton University Press. https://doi.org/10.1515/9781400866816-004
• “Chapter 4. Wing-Tail Plane Interference at Supersonic Speeds.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-010
• “Chapter 5. Wing-Body Interference at Supersonic Speeds.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-011
• “CHAPTER FOUR. Thin Airfoil Theory.” 1990. In Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400860777.53
• “CHAPTER NINE. the Minimum Drag of Thin Wings.” 1990. In Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400860777.159
• “CHAPTER TEN. Drag of Wings and Bodies in Combination.” 1990. In Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400860777.200
• Charit, Indrajit, and Rajiv Mishra. 2007. “Superplasticity and Superplastic Forming.” In Materials Processing Handbook. CRC Press. https://doi.org/10.1201/9781420004823.ch14
• Charles, Guy, Mark Lowenberg, David Stoten, Xiao Fan Wang, and Mario di Bernardo. 2002. “Aircraft Flight Dynamics Analysis and Controller Design Using Bifurcation Tailoring.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4751
• Charters, A. C. 1962. “Section o. Free Flight Range Methods.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-017
• 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, 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
• Chassiakos, Anastassios, Petros Ioannou, Michael Safonov, Marc Nugent, and Doug Moore. 1988. “Adaptive Roll Control of a Dynamic Wind Tunnel Model.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4373
• Chaudhari, Bhargav N., and Timothy T. Takahashi. 2022. “Inlet Diffusor Buoyancy – Its Historical Use in Supersonic Transport Design.” In AIAA SCITECH 2022 Forum. AIAA 2022-2566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2566
• 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
• Cheadle, Christopher, and Nicholas DiZinno. 2026. “The Effect of off-Design Conditions on Inlet Buzz.” In Proceeding of 11th Thermal and Fluids Engineering Conference (TFEC). Begellhouse. https://doi.org/10.1615/tfec2026.fna.061757
• Chedrik, Vasily, Fanil Ishmuratov, Mikhail Zichenkov, and Yuri Azarov. 2004. “Optimization Approach to Design of Aeroelastic Dynamically-Scaled Models of Aircraft.” In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2004-4642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4642
• Chen, R. 1981. “Kinematic Properties of Rotary-Wing and Fixed-Wing Aircraft in Steady Coordinated High-g Turns.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1855
• Chen, Lei. 2005. “Modeling and Optimization of Springback with Contact Evolution in Sheet Metal Forming.” Journal of Mechanical Engineering 41 (11): 189. https://doi.org/10.3901/jme.2005.11.189
• Chen, Lei. 2010. “Numerical Simulation and Experiment of Aluminum Sheet Metal Springback in New Quenching State.” Advanced materials research 97-101: 2567–70. https://doi.org/10.4028/www.scientific.net/amr.97-101.2567
• Chen, Lei. 2011a. “Effect of Material Parameters Wave on Sheet Metal Springback Using Orthogonal Design Simulation.” Advanced materials research 314-316: 585–88. https://doi.org/10.4028/www.scientific.net/amr.314-316.585
• Chen, Lei. 2011b. “Finite Element Simulation of Springback in Sheet Metal Forming.” Applied Mechanics and Materials 50-51: 615–18. https://doi.org/10.4028/www.scientific.net/amm.50-51.615
• Chen, Zhongkai. 2022. “Study on Optimization Method for Airfoil in Supersonic Case Based on Particle Swarm optimization(PSO).” Highlights in Science, Engineering and Technology 13: 100–106. https://doi.org/10.54097/hset.v13i.1337
• Chen, H., K. Chang, T. Tzong, and T. Cebeci. 1998. “Aeroelastic Analysis of Wing and Wing/fuselage Configurations.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-907. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-907
• Chen, S., M. Khalid, M. Beyers, and I. Fejtek. 2001. “Computation of Flows past a Low Aspect-Ratio Swept Wing.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-2485. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2485
• Chen, Wei, Gapyong Kim, and Jiahua Zhang. 2006b. “Springback Prediction and Control in Multi-Stage Sheet Metal Forming.” In Manufacturing Science and Engineering, Parts A and B. ASMEDC. https://doi.org/10.1115/msec2006-21018
• Chen, Fuh-Kuo, and Shen-Fu Ko. 2011. “Deformation Analysis of Springback in L-Bending of Sheet Metal.” Advanced Science Letters 4 (6): 1928–32. https://doi.org/10.1166/asl.2011.1713
• Chen, Shaokun, Jinze Li, Rui Zhao, Jie Zhao, and Kaiping Yu. 2025c. “Supersonic Panel Flutter Analysis by Using the Polygonal Finite Element Method.” International Journal of Structural Stability and Dynamics: 2650403. https://doi.org/10.1142/s0219455426504031
• Chen, Ke, Jian Ping Lin, Mao Kang Lv, and Li Ying Wang. 2010. “Advanced High Strength Steel Sheet Forming and Springback Simulation.” Advanced materials research 97-101: 200–203. https://doi.org/10.4028/www.scientific.net/amr.97-101.200
• Chen, Bing, Liang Liu, Xiaojun Wu, Wenhao Zhang, and Hongyin Jia. 2026a. “The Influence of Variable Geometric Lip on Supersonic Inlet Performance.” In Fluid Mechanics and Industrial Applications. CRC Press. https://doi.org/10.1201/9781003679561-4
• Chen, Robert K., Lisa A. Martinez, and David P. Wilson. 2025a. Computational Fluid Dynamics Analysis of Supersonic Inlet Design. National Aeronautics and Space Administration. https://doi.org/10.64631/abcd8901
• Chen, Du, Mariluz Penalva, Yang Hai, Martin Andér, Frans Coenen, and Anh Nguyen. 2025b. “Sheet Metal Forming Springback Prediction Using Image Geometrics (SPIG): A Novel Approach Using Heatmaps and Convolutional Neural Network.” In International Joint Conference on Knowledge Discovery, Knowledge Engineering and Knowledge Management. https://doi.org/10.5220/0013673100004000
• Chen, P. C., E. Sulaeman, and D. D. Liu. 2002. A Comprehensive Rapid-Assessment-Of-Flutter/Ejection-Loads (RAFEL) Software System for Aircraft/Store Compatibility. Defense Technical Information Center. https://doi.org/10.21236/ada399365
• Chen, Dyi-Cheng, and Hsin-Neng Wang. 2008. “A Finite Element Analysis of the Superplastic Blow-Forming in an Awl-Shaped Die with Titanium Alloy.” Computer Methods in Materials Science 8 (3): 130–37. https://doi.org/10.7494/cmms.2008.3.0198
• Chen, Pengxin, Zhiwen Wu, Yuntao Guo, and Tianyu Lu. 2026b. “Mechanisms of Pressure-Wave Feedback and Shock Evolution during Transient Opening of a Supersonic Inlet.” Physics of Fluids 38 (9): 095119. https://doi.org/10.1063/5.0348275
• Chen, Jingjing, Yadong Wu, Zhonglin Wang, and Anjenq Wang. 2015. “Nacelle Aerodynamic Optimization and Inlet Compatibility.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-42346
• Chen, Xiangying, Gecheng Zha, and Ming-ta Yang. 2006a. “3D Simulation of a Transonic Wing Flutter Using an Efficient High Resolution Upwind Scheme.” In 36th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2006-3216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3216
• Chen, Xingyu, Heng Zhang, Zhao Yang, Xiong Zhang, and Jie Li. 2026c. “Regionally Constrained Sequential Optimization for Coordinated Enhancement of Aerodynamic Efficiency and Rolling Moment Performance of a Transonic Oblique Wing.” Preprint, . https://doi.org/10.2139/ssrn.7380660
• 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, H. K. 1982. “The Transonic-Flow Theories of High- and Low-Aspect-Ratio Wings.” In Numerical and Physical Aspects of Aerodynamic Flows. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-12610-3_23
• Cheng, J.-C. 2009. “Nonlinear Aerodynamic Effects on Transonic Flap Buzz, Tail Flutter and Limit-Cycle Oscillations of Two-Dimensional Wing-Flap-Tail Configurations.” Journal of Mechanics 25 (4): 451–63. https://doi.org/10.1017/s1727719100002938
• Cheng, Changfu, Tianxiang Hu, Peiqing Liu, Zhaosheng Zhang, Qiulin Qu, and Rinie Akkermans. 2018. “Self-Induced Roll Characteristics of Low-Aspect-Ratio Flat-Plate Wings Improved by Sinusoidal Edge.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3968
• Cheng, Guangfeng, Chuh Mei, and Y. Y. Lee. 2002. “Flow Angle, Temperature and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1285. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1285
• Cheng, H., and N. Rott. 1954. “Generalizations of the Inversion Formula of Thin Airfoil Theory.” Indiana University Mathematics Journal 3 (3): 357–82. https://doi.org/10.1512/iumj.1954.3.53018
• Chester, W. 1953. “Supersonic Flow past Wing-Body Combinations.” Aeronautical Quarterly 4 (3): 287–314. https://doi.org/10.1017/s0001925900000950
• Chestnutt, David. 1966. OV-1A Mohawk Flight Loads Investigation Program. Defense Technical Information Center. https://doi.org/10.21236/ad0629632
• 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
• 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
• Chima, Rodrick. 2011a. “Computational Analysis of a Low Boom Supersonic Inlet (Invited).” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3801
• Chima, Rodrick V. 2011b. Computational Analysis of a Low-Boom Supersonic Inlet. NASA/TM-2011-217223. NASA. https://ntrs.nasa.gov/citations/20110023757
• Chima, ROdrick V. 2011c. “Computational Analysis of the Large Scale Low-Boom Supersonic Inlet.” In 2011 Fundamental Aeronautics Program Technical Conference. https://ntrs.nasa.gov/citations/20110011335
• Chima, Rodrick V. 2012. Analysis of Buzz in a Supersonic Inlet. NASA/TM-2012-217612. NASA. https://ntrs.nasa.gov/citations/20120009203
• Chima, Rodrick V., Timothy R. Conners, and Thomas R. Wayman. 2009. “Coupled Analysis of an Inlet and Fan for a Quiet Supersonic Aircraft.” In NASA Fundamental Aeronautics Program 32rd Annual Meeting. https://ntrs.nasa.gov/citations/20100041304
• Chima, Rodrick V., Timothy R. Conners, and Thomas R. Wayman. 2010. Coupled Analysis of an Inlet and Fan for a Quiet Supersonic Jet. NASA/TM-2010-216350. NASA. https://ntrs.nasa.gov/citations/20100024366
• Chima, Rodrick V., Stefanie M. Hirt, and Robert Reger. 2011. Axisymmetric Calculations of a Low-Boom Inlet in a Supersonic Wind Tunnel. NASA/TM-2011-217224. NASA. https://ntrs.nasa.gov/citations/20110023762
• Chin, W. C. 1984. “Thin Airfoil Theory for Planar Inviscid Shear Flow.” Journal of Applied Mechanics 51 (1): 19–26. https://doi.org/10.1115/1.3167572
• 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, Alexander W., Claudia Y. Herrera, Natalie D. Spivey, William A. Fladung, and David Cloutier. 2015. “Testing and Validation of the Dynamic Inertia Measurement Method.” In IMAC Conference and Exposition on Structural Dynamics. https://ntrs.nasa.gov/citations/20150002077
• Chiplunkar, Ankit, Emmanuel Rachelson, Michele Colombo, and Joseph Morlier. 2016. “Adding Flight Mechanics to Flight Loads Surrogate Model Using Multi-Output Gaussian Processes.” In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2016-4000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4000
• Chipman, R., and J. Malone. 1977. “Application of Optimization Technology to Wing/store Flutter Prediction.” In Dynamics Specialists Conference. AIAA 1977-453. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-453
• 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
• Chipman, R., A. Zislin, and C. Waters. 1982. “Active Control of Aeroelastic Divergence.” In 23rd Structures, Structural Dynamics and Materials Conference. AIAA 1982-684. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-684
• Chirita, Bogdan, and Gheorghe Brabie. 2007. “Control of Springback in Sheet Metal U-Bending through Design Experiment.” In AIP Conference Proceedings, vol. 908. AIP. https://doi.org/10.1063/1.2740913
• Cho, Yongseung, and M. Nagati. 1995. “Flight Simulator Modeling Using Neural Networks with Spin Flight Test Data.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-560
• 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
• Choe, Yohan, and Chongam Kim. 2016. “Numerical Investigation of Bleed Effects on Supersonic Inlet under Various Bleed and Inlet Conditions.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-3564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3564
• Choi, S. C. 1967. Design of Sampling Procedures for Flight Loads Studies. Defense Technical Information Center. https://doi.org/10.21236/ad0825512
• Choi, Jonggyu, Jin Choi, and Hyungrok Do. 2026. “Design and Optimization of a Fuselage-Integrated Diverterless Supersonic Intake for Ramjet Vehicles.” Preprint, . https://doi.org/10.2139/ssrn.6438819
• Chopde, Rahul, Prasad Parkhi, and Ganapati Joshi. 2025. “Effect of Micro-Vortex Generator Geometry on Separation Characteristics of Supersonic Inlet.” In Ballistics 2025. Destech Publications, Inc. https://doi.org/10.12783/ballistics25/37185
• Chou, David C., and Theodore F. Smith. 1974. Aerodynamic Heating of Supersonic Blunt Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada001135
• Choudhari, Meelan, and Craig Streett. 1990. “Boundary Layer Receptivity Phenomena in Three-Dimensional and High-Speed Boundary Layers.” In 2nd International Aerospace Planes Conference. AIAA 1990-5258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-5258
• 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
• Chow, J., N. Pedreiro, and S. Rock. 1998. “The Impact of Forebody Geometries at High-Angle-of-Attack with Forebody Tangential Blowing.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4522
• 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
• Christiana, John J. 1963. Improved Methods for the Production of Titanium Alloy Extrusions. Defense Technical Information Center. https://doi.org/10.21236/ad0408203
• Chuang, Hsin-Kung A., and Osama A. Kandil. 1989. “Thickening Oscillation of a Delta Wing Using Navier-Stokes and Navier-Displacement Equations.” In AIAA. https://ntrs.nasa.gov/citations/19890061706
• Chuban, Vitalii Dmitrievich. 2020. “Panel Flutter of Plate under Subsonic Flow in Two-Dimensional Approach.” TsAGI Science Journal 51 (1): 85–98. https://doi.org/10.1615/tsagiscij.2020034274
• Chun, B. K., J. T. Jinn, and J. K. Lee. 2001. “A Constitutive Model Associated with Permanent Softening under Multiple Bend—Unbending Cycles in Sheet Metal Forming and Springback Analysis.” In Computational Fluid and Solid Mechanics. Elsevier. https://doi.org/10.1016/b978-008043944-0/50585-0
• 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, S. 1973. Survey of Literature on Convective Heat Transfer Coefficients and Recovery Factors for High Atmosphere Thermometry. NASA-CR-138747. NASA. https://ntrs.nasa.gov/citations/19740019690
• Chung, Joongkee. 1994. “Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-583
• Chung, Hyoung S., Donghyurn Cho, Jongbum Kim, and Young Il Jang. 2019. “Study on Wing Rock Phenomenon of a Fighter Aircraft Using Free-To-Roll Wind Tunnel Test and Dynamic CFD Method.” In AIAA Aviation 2019 Forum. AIAA 2019-3591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3591
• 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
• Claridge, J. S. 1973. “Design and Simulation of an Aircraft Brake Using a Digital Computer.” Aeronautical Journal 77 (747): 136–46. https://doi.org/10.1017/s0001924000040525
• Clark, S. 1974a. “High Friction Interactive Aircraft Tire-Runway Systems.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-967. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-967
• Clark, L. 1974b. “Statistical Averages of Subsonic Inlet Distortion.” In 10th Propulsion Conference. AIAA 1974-1197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1197
• Clark, Larry. 1995. “Dynamic Response Characteristics of a Mixed Compression Supersonic Inlet as Part of a Larger System.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-36. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-36
• Clark, C. K., and M. R. Bernens. 1991. “High Angle-Of-Attack Flight Characteristics of the VF-22.” In Aircraft Design and Operations Meeting. AIAA 1991-3194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3194
• Clark, A., III. 1984. “An Alternate Aircraft Takeoff System for Tactical Aircraft.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2130
• Clarke, Joseph H. 1960. “The Forces on Wing-Fuselage Combinations in Supersonic Flow.” Journal of Fluid Mechanics 8 (2): 210–26. https://doi.org/10.1017/s0022112060000554
• 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
• Clay, Eugene O. 1961. “Reacting Flight Loads at Forging Temperatures.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/610085
• Clay, Larry E., and Alan P. Berens. 1964. Structral Flight Loads Data from C-130 Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0600470
• Clay, Larry E., and Ronald I. Rockafellow. 1973. T-38 Structural Flight Loads Data for June 1970 through December 1971. Defense Technical Information Center. https://doi.org/10.21236/ad0758891
• Cleary, Joseph W., and Jack A. Mellenthin. 1949. Wind-Tunnel Tests of a 0.16-Scale Model of the Douglas MX-656 Airplane at High Subsonic Speeds. II: Wing and Fuselage Pressure Distribution. NACA-RM-SA9H22. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20090022100
• Cliff, Susan E., Timothy J. Baker, Scott D. Thomas, and Ernest D. Aguayo. 1999. “Simulated Inlet Unstart and Nacelle/Diverter Effects for the Boeing Reference H Configuration.” In First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop. https://ntrs.nasa.gov/citations/20000044877
• “Climb Performance.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0513.0570
• “Climbing Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0259.0292
• Cobleigh, Brent. 1994. “High-Angle-of-Attack Yawing Moment Asymmetry of the X-31 Aircraft from Flight Test.” In 12th Applied Aerodynamics Conference. AIAA 1994-1803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1803
• 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
• Cockbill, Louisa. 2018. “Singularities in Vorticity-Induced Velocity Field Eliminated from Linearized Supersonic Flow.” Scilight 2018 (22): 220001. https://doi.org/10.1063/1.5041743
• Coe, P. L., Jr. 1976. Propulsive-Lift Concepts for Improved Low-Speed Performance of Supersonic Cruise Arrow-Wing Configurations. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19760053942
• Cohen, Doris. 1944. A Theoretical Investigation of the Rolling Oscillations of an Airplane with Ailerons Free. NACA-ARR-4A06. NASA. https://ntrs.nasa.gov/citations/19930092522
• Cohen, Doris. 1951. Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings with Leading Edges behind the Mach Line. NACA-TR-1050. NASA. https://ntrs.nasa.gov/citations/19930092096
• 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, Clarence B., and John C. Evvard. 1948. Graphical Method of Obtaining Theoretical Lift Distributions on Thin Wings at Supersonic Speeds. NACA-TN-1676. NASA. https://ntrs.nasa.gov/citations/19930082314
• Cole, G. 1977. “Atmospheric Effects on Inlets for Supersonic Cruise Aircraft.” In 13th Propulsion Conference. AIAA 1977-874. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-874
• 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, Stanley R. 1989. Flutter of a Low-Aspect-Ratio Rectangular Wing. NASA-TM-4116. NASA. https://ntrs.nasa.gov/citations/19890014076
• Cole, Stanley. 1990. “Effects of Spoiler Surfaces on the Aeroelastic Behavior of a Low-Aspect-Ratio Rectangular Wing.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-981. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-981
• Cole, Stanley R. 1991. Technical Activities of the Configuration Aeroelasticity Branch. NASA-TM-104146. NASA. https://ntrs.nasa.gov/citations/19920004240
• Cole, Stanley R., Steven W. Moss, and Robert V. Doggett Jr. 1990. Some Buffet Response Characteristics of a Twin-Vertical-Tail Configuration. NASA-TM-102749. NASA. https://ntrs.nasa.gov/citations/19910004099
• Cole, Henry A., Jr., and Frances L. Bennion. 1956. Measurement of the Longitudinal Moment of Inertia of a Flexible Airplane. NACA-TN-3870. NASA. https://ntrs.nasa.gov/citations/19930084639
• 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
• Collicott, Steven H., Daniel T. Valentine, E. L. Houghton, and P. W. Carpenter. 2026. “Thin Airfoil Theory.” In Aerodynamics for Engineering Students. Elsevier. https://doi.org/10.1016/b978-0-32-399544-3.00010-4
• Collins, Diarmuid. 2016. 8.2: Wireless Data Acquisition in Flight Test Networks. https://doi.org/10.5162/etc2016/8.2
• 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
• Comenzo, Raymond J., and Ernest A. Mackley. 1952. Preliminary Investigation of a Rectangular Supersonic Scoop Inlet with Swept Sides Designed for Low Drag at a Mach Number of 2.7. NACA-RM-L52J02. NASA. https://ntrs.nasa.gov/citations/19930087347
• Comenzo, Raymond J., and Ernest A. Mackley. 1954. Effect of Yaw and Angle of Attack Pressure Recovery and Mass-Flow Characteristics of a Rectangular Supersonic Scoop Inlet at a Mach Number of 2.71. NACA-RM-L54G22. NASA. https://ntrs.nasa.gov/citations/19930089381
• “Complete Model of Aircraft Perturbed Motion.” n.d. In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0043101
• Compton, H. R., J. R. Schiess, W. T. Suit, W. I. Scallion, and J. W. Hudgins. 1983. “Stability and Control over the Supersonic and Hypersonic Speed Range.” In Shuttle Performance: Lessons Learned, Pt. 1. https://ntrs.nasa.gov/citations/19840002068
• Computational Fluid Dynamics Analysis Method Developed for Rocket-Based Combined Cycle Engine Inlet. 1997. NASA. https://ntrs.nasa.gov/citations/20050177084
• Comtois, Paul, and Scott Glaser. 2010. “Effectiveness of Sustained G Simulation in Loss of Control and Upset Recovery Training.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2010-7798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7798
• Conners, Timothy, and Donald Howe. 2006. “Supersonic Inlet Shaping for Dramatic Reductions in Drag and Sonic Boom Strength.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-30. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-30
• Conners, Timothy, Donald Howe, and John Whurr. 2005. “Impact of Engine Cycle Selection on Propulsion System Integration and Vehicle Performance for a Quiet Supersonic Aircraft.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-1016. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1016
• 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
• Connors, James F., J. Calvin Lovell, and George A. Wise. 1957a. Effects of Internal-Area Distribution, Spike Translation, and Throat Boundary-Layer Control on Performance of a Double-Cone Axisymmetric Inlet at Mach Numbers from 3.0 to 2.0. NACA-RM-E57F03. Lewis Flight Propulsion Laboratory. https://ntrs.nasa.gov/citations/19930089784
• Connors, James F., George A. Wise, and J. Calvin Lovell. 1957b. Investigation of Translating-Double-Cone Axisymmetric Inlets with Cowl Projected Areas 40 and 20 Percent of Maximum at Mach Numbers from 3.0 to 2.0. NACA-RM-E57C06. Lewis Flight Propulsion Laboratory. https://ntrs.nasa.gov/citations/19930089639
• Connors, James F., and Richard R. Woollett. 1952. Experimental Investigation of a Two-Dimensional Split-Wing Ram-Jet Inlet at Mach Number of 3.85. NACA-RM-E52F04. NASA. https://ntrs.nasa.gov/citations/19930087235
• Conrad, E. William, and Carl E. Campbell. 1953. Altitude Investigation of Several Afterburner Configurations for the J40-WE-8 Turbojet Engine. NACA-RM-E52L10. NASA. https://ntrs.nasa.gov/citations/19930087411
• Conrad, E. William, and John E. McAulay. 1951. Altitude-Wind-Tunnel Investigation of Performance Characteristics of a J47D Prototype (RX1-1) Turbojet Engine with Variable-Area Exhaust Nozzle. NACA-RM-E51C15. NASA. https://ntrs.nasa.gov/citations/19930086532
• “Control Authority Assessment in Aircraft Conceptual Design.” 1993. In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-3968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3968
• Conway, S., and J. Johansson. 2001. “Integrated Engine-Airframe Calculations Using CFD.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3201
• Conyers, Howard J., Earl H. Dowell, and Kenneth C. Hall. 2010. “Aeroelastic Studies of a Rectangular Wing with a Hole: Correlation of Theory and Experiment.” In 2010 Aerospace Systems Conference. https://ntrs.nasa.gov/citations/20100005187
• Cook, Charles B. 1946. Effect of an Auxiliary Belly Fuel Tank on the Low-Speed Static Stability Characteristics of a 1/5-Scale Model of the Grumman XF8F-1 Airplane, TED No. NACA 2384. NACA-RM-L6H21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019460
• Cook, R. 1964. “An Automatic Stall Prevention Control for Supersonic Fighter Aircraft.” In 1st Annual Meeting. AIAA 1964-329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-329
• Cook, Stephen, Terence Ghee, Hugo Gonzalez, Alexander Kokolios, Henrik Pettersson, and D. Owens. 2004. “Correlation of the Continuous Beta Sweep Test and Analysis Technique to Transonic Free-to-Roll and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5052
• 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
• Cooney, T. V., and Russell L. Schott. 1956. Initial Results of a Flight Investigation of the Wing and Tail Loads on an Airplane Equipped with a Vane-Controlled Gust-Alleviation System. NACA-TN-3746. NASA. https://ntrs.nasa.gov/citations/19930084592
• 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
• Corlett, W. A. 1979. “Test Technique Development in Interference Free Testing, Flow Visualization, and Remote Control Model Technology at Langley’s Unitary Plan Wind Tunnel.” In Supersonic Tunnel Association. https://ntrs.nasa.gov/citations/19790067080
• Cornette, Elden S. 1961. Wind-Tunnel Investigation of the Effects of Wing Bodies, Fences, Flaps, and a Fuselage Addition on the Wing Buffet Response of a Transonic-Transport Model. NASA-TN-D-637. NASA. https://ntrs.nasa.gov/citations/20040003909
• Cortright, Edgar M., Jr. 1951. Preliminary Investigation of a Translating Cowl Technique for Improving Take-off Performance of a Sharp-Lip Supersonic Diffuser. NACA-RM-E51I24. NASA. https://ntrs.nasa.gov/citations/19930086879
• Cosenza, C., and L. Kummeth. 1974. “Transonic Aircraft Technology /TACT/ Program.” In 8th Aerodynamic Testing Conference. AIAA 1974-620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-620
• Cosner, R. 1985. “Integrated Flowfield Analysis Methodology for Fighter Inlets.” In Aircraft Design Systems and Operations Meeting. AIAA 1985-3071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-3071
• Costakis, W. G. 1977. Characteristics of Random Inlet Pressure Fluctuations during Flights of F-111A Airplane. NASA-TM-X-3540. NASA. https://ntrs.nasa.gov/citations/19770018147
• Costes, Philippe. 2000. “A Theory of the Flight of a Flexible Aircraft in Turbulence: Roll Dynamics.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3977. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3977
• Costigan, Michael, and Robert Calico. 1989. “An Analysis of Lateral-Directional Handling Qualities and Eigenstructure of High Performance Aircraft.” In 27th Aerospace Sciences Meeting. AIAA 1989-17. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-17
• Cosyn, Peter, and Jan Vierendeels. 2005. “Numerical Investigation of Low Aspect Ratio Wings at Low Reynolds Numbers.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4609
• Cotton, James D., Robert D. Briggs, Rodney R. Boyer, et al. 2015. “State of the Art in Beta Titanium Alloys for Airframe Applications.” JOM 67 (6): 1281–1303. https://doi.org/10.1007/s11837-015-1442-4
• Couch, L. 1972. “Transonic Wall Interference Effects on Bodies of Revolution.” In 7th Aerodynamic Testing Conference. AIAA 1972-1008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1008
• Couillaud, Stephane L. n.d. “Experimental Investigation of Spanwise Blowing on a 40 Degree Swept Trapezoidal Wing.” PhD diss., San Jose State University. https://doi.org/10.31979/etd.r4b9-r6zv
• Covert, E. 1984. “Thrust and Drag of Aircraft: Prediction and Verification.” In 13th Aerodynamic Testing Conference. AIAA 1984-611. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-611
• 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, John. 2010. “Aeroplane Upset Recovery Training, History, Core Concepts & Mitigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8002
• 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, H., and E. Erbin. 1965. “Stress Corrosion and Titanium Alloy Design for High Temperature Applications.” In Aircraft Design and Technology Meeting. AIAA 1965-764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-764
• Crabill, Norman L. 1956. Lift, Drag, Static Stability, and Buffet Boundaries of a Model of the McDonnell F3H-1N Airplane at Mach Numbers from 0.40 to 1.27, TED No. NACA DE 351. NACA-RM-SL56A13. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030066
• Craddock, J. 1973. “Weldbonding/rivetbonding: Application Testing of Thin Gauge Aircraft Components.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-805
• Craig, Andrew, and Donald Romani Jr. 1993. “Unsteady Aerodynamics in Airplane Stall-Spin Departure.” In 31st Aerospace Sciences Meeting. AIAA 1993-622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-622
• Craig, R., Jr. 1971. “Optimization of a Supersonic Panel Subject to a Flutter Constraint -A Finite Element Solution.” In 12th Structures, Structural Dynamics and Materials Conference. AIAA 1971-330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-330
• 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
• Crasta, Asha, and S. A. Khan. 2014. “Effect of Angle of Attack on Stiffness Derivative of an Oscillating Supersonic Delta Wing with Curved Leading Edges.” IOSR Journal of Mechanical and Civil Engineering 11 (6): 12–25. https://doi.org/10.9790/1684-11631225
• Crawford, Bradley, and Tom Finley. 2000. “Improved Correction System for Vibration Sensitive Inertial Angle of Attack Measurement Devices.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-415
• Crespo, Luis, Sean Kenny, David Cox, and Daniel Murri. 2012. “Analysis of Control Strategies for Aircraft Flight Upset Recovery.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-5026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5026
• Crider, Dennis. 2010. “Accident Lessons for Stall Upset Recovery Training.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8003
• Crider, Dennis, and John Foster. 2012. “Simulation Modeling Requirements for Loss-of-Control Accident Prevention of Turboprop Transport Aircraft.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2012-4569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4569
• 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
• Crittenden, J., T. Weisshaar, E. Johnson, and M. Rutkowski. 1977. “Aeroelastic Stability Characteristics of an Oblique Wing Aircraft.” In Dynamics Specialists Conference. AIAA 1977-454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-454
• Croom, Mark, David Fratello, Raymond Whipple, Matthew O’Rourke, and Todd Trilling. 1993. “Dynamic Model Testing of the X-31 Configuration for High-Angle-of-Attack Flight Dynamics Research.” In Flight Simulation and Technologies. AIAA 1993-3674. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3674
• Croom, M., S. Grafton, and L. Nguyen. 1982. “High Angle-of-Attack Characteristics of Three-Surface Fighter Aircraft.” In 20th Aerospace Sciences Meeting. AIAA 1982-245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-245
• Crosthwait, E. 1966. “A Parametric Study of the Subsonic Characteristics of Low-Aspect-Ratio Reentry Wings.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-429. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-429
• 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
• Cruz, Christopher, and Alan Wilhite. 1989. “Prediction of High-Speed Aerodynamic Characteristics Using the Aerodynamic Preliminary Analysis System (APAS).” In 7th Applied Aerodynamics Conference. AIAA 1989-2173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2173
• Cubbison, R., and D. Smeltzer. 1968. “Study of a Family of Supersonic Inlet Systems.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-580
• Cui, Haichao, Yanji Hong, Baosheng Du, et al. 2024a. “A High-Precision Measurement Method for Moment of Inertia Based on Torsion Pendulum Method.” Measurement Science and Technology 35 (12): 125013. https://doi.org/10.1088/1361-6501/ad778e
• Cui, X., and Y. Li. 2022. “A Test Method for Traction Load of Aircraft Nose Landing Gear.” IET Conference Proceedings 2022 (7): 178–82. https://doi.org/10.1049/icp.2022.1520
• Cui, Zheng, Wensheng Zhang, Kai Wang, and Yihua Cao. 2024b. “Numerical Investigation of the Powered Take-off Configuration of Civil Transport Using an Improved Thrust-Drag Bookkeeping Method.” Journal of Physics: Conference Series 2707 (1): 012112. https://doi.org/10.1088/1742-6596/2707/1/012112
• Culick, Fred. 1988. “Application of Dynamical Systems Theory to Nonlinear Aircraft Dynamics.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4372
• 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
• Cumming, Stephen B., Mark S. Smith, and Michael A. Frederick. 2007. “Aerodynamic Effects of a 24-Foot, Multisegmented Telescoping Nose Boom on an F-15B Airplane.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20070028417
• Cumming, Stephen B., Mark S. Smith, and Michael A. Frederick. 2008. Aerodynamic Effects of a 24-Foot Multisegmented Telescoping Nose Boom on an F-15B Airplane. NASA/TM-2008-214634. NASA. https://ntrs.nasa.gov/citations/20080015840
• Cunis, Torbjørn. n.d. “Modeling, Analysis, and Control for Upset Recovery: From System Theory to Unmanned Aircraft Flight.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/5f4b14cez5181z4604zaf8dz27dc1744e316
• 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, Kevin, Gautam H. Shah, Neal T. Frink, et al. 2018. “Preliminary Test Results for Stability and Control Characteristics of a Generic T-Tail Transport Airplane at High Angle of Attack.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0529. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0529
• Cunningham, A. M., Jr., D. B. Benepe, D. Watts, and P. G. Waner. 1978. A Method for Predicting Full Scale Buffet Response with Rigid Wind Tunnel Model Fluctuating Pressure Data. Volume 1: Prediction Method Development and Assessment. NASA-CR-3035. NASA. https://ntrs.nasa.gov/citations/19790005849
• Currao, Gaetano, and Chieh-Wei Yeh. 2026. “Vortex Dynamics and Aeroelastic Response of a\\ Finite Wing in Transonic Flow.” Preprint, . https://doi.org/10.2139/ssrn.6450319
• Curry, Robert, and Robert Curry. 1997. “Dynamic Ground Effect for a Cranked Arrow Wing Airplane.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3649. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3649
• 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
• Curtiss, H. C., Jr. 1965. An Analytical Study of the Dynamics of Aircraft in Unsteady Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0627370
• Cyrus, John D., David J. Bents, and David M. Overholt. 1999. “A Supercharged Turbojet for High Altitude Atmospheric Science Investigations.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/99-gt-106
• Czarnecki, Kazimierz Roman, and James N. Mueller. 1950. An Approximate Method of Calculating Pressures in the Tip Region of a Rectangular Wing of Circular-Arc Section at Supersonic Speeds. NACA-TN-2211. NASA. https://ntrs.nasa.gov/citations/19930082858
• Czarnecki, K. R., and James N. Mueller. 1951. Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow over a Rectangular Wing with Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap. NACA-RM-L50J18. NASA. https://ntrs.nasa.gov/citations/19930086627
• Czysz, Paul A. 1963. Correlation of Wind Tunnel Blockage Data. Defense Technical Information Center. https://doi.org/10.21236/ad0407689
• D’Acquisto, L., and L. Fratini. 2000. “Springback Evaluation in Basic Sheet Metal Stamping Processes.” In Proceedings of the 33rd International MATADOR Conference. Springer London. https://doi.org/10.1007/978-1-4471-0777-4_62
• D’Aiutolo, Charles T., and Allen B. Henning. 1955. Lateral Stability Characteristics at Low Lift between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-Arc Sections and 40 Degrees Sweepback. NACA-RM-L55A31. NASA. https://ntrs.nasa.gov/citations/19930088583
• D’Ewart, Benjamin B., and Robert F. 1958. Transonic Flutter Characteristics of a 45 Degree Swept Back All Movable Stabilizer. Defense Technical Information Center. https://doi.org/10.21236/ad0155543
• D’Urso, Gianluca Danilo, Giuseppe Pellegrini, and Giancarlo Maccarini. 2007. “The Effect of Sheet and Material Properties on Springback in Air Bending.” In Key engineering materials. Trans Tech Publications. https://doi.org/10.4028/0-87849-437-5.277
• “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
• Da Ronch, Andrea, Kenneth J. Badcock, Alex Khrabrov, M. Ghoreyshi, and R. Cummings. 2011. “Modeling of Unsteady Aerodynamic Loads.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6524
• Dacquino, D., and R. Raffaele. 1982. “Highlights of a Design Concept for a Close Ground Support Fighter.” In 20th Aerospace Sciences Meeting. AIAA 1982-411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-411
• Dahlke, C. W., and George Batiuk. 1990. HYDRA 70 MK66 Aerodynamics and Roll Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada226182
• Dal’Carobo, Bruno, and Ricardo Augusto Fensterseifer. 2010. “Aircraft Wing Flutter: An Applied Approach.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2010-36-0513
• 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
• Dan, W. J., and W. G. Zhang. 2012. “Springback Angle and Plastic Elongation Prediction of Thin-Walled Tube Bending by FEM.” Applied Mechanics and Materials 152-154: 456–61. https://doi.org/10.4028/www.scientific.net/amm.152-154.456
• Dana, William H. 1993. “The X-15 Airplane: Lessons Learned.” In 31st Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19930039008
• Daniels, Peter, and Samuel R. Hardy. 1975. Roll-Rate Stabilization of a Missile Configuration with Wrap-Around Fins in Incompressible Flow. Defense Technical Information Center. https://doi.org/10.21236/ada019928
• Dann, Andrew. n.d. “Inlet Design for a Mach 2 Pulse Detonation Engine.” PhD diss., The University of Queensland. https://doi.org/10.14264/345514
• Dantsker, Or D., Gavin K. Ananda, and Michael S. Selig. 2017. “GA-USTAR Phase 1: Development and Flight Testing of the Baseline Upset and Stall Research Aircraft.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-4078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4078
• Dantsker, Or D., Moiz Vahora, Saym Imtiaz, and Marco Caccamo. 2018. “High Fidelity Moment of Inertia Testing of Unmanned Aircraft.” In 2018 Applied Aerodynamics Conference. AIAA 2018-4219. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4219
• Darden, C. 1984. “The Influence of Leading-Edge Load Alleviation on Supersonic Wing Design.” In 22nd Aerospace Sciences Meeting. AIAA 1984-138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-138
• Das, Saptak. 2026. “Modeling and Stability Analysis of Inertial Roll Coupling in Supersonic Sounding Rockets.” In 2026 Regional Student Conferences. AIAA 2026-112783. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-112783
• 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
• Daughetee, C. 1974. “Drop Testing Naval Aircraft and the VSD Landing Gear Dynamic Test Facility.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-343
• Daughtridge, Lee T., Jr. 1946. Free-Spinning-Tunnel Tests of a 1/18-Scale Model of the Fairchild XNQ-1 Airplane, TED No. NACA 2398. NACA-RM-L6H28. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050031171
• Daughtridge, Lee T., Jr. 1948. Free-Spinning-Tunnel Tests of a 0.057-Scale Model of the Chance Vought XF7U-1 Airplane. NACA-RM-SL8A13. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028616
• Davidson, John B., and Dominick Andrisani II. 1996. Lateral-Directional Eigenvector Flying Qualities Guidelines for High Performance Aircraft. NASA-TM-110306. NASA. https://ntrs.nasa.gov/citations/19970008392
• Davis, Jake Daniel. n.d. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2018.158
• Davis, J. 1969. “Wing-Tail Interaction Flutter of Moderately Spaced Tandem Airfoils.” In 7th Aerospace Sciences Meeting. AIAA 1969-57. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-57
• Davis, D. F. 1973. Advanced Metallic Structures: Air Superiority Fighter Wing Design for Improved Cost, Weight and Integrity. Volume 2. Design Data. Defense Technical Information Center. https://doi.org/10.21236/ad0781807
• Davis, Milt. 2010. “Prediction and Analysis of Inlet Pressure and Temperature Distortion on Engine Operability from a Recent T-38 Flight Test Program.” In U.S. Air Force T&E Days 2010. AIAA 2010-1721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1721
• Davis, Milt, William Baker, Greg Power, and Dave Beale. 1999. “A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/99-gt-345
• Davis, Gary, and Oddvar Bendiksen. 1993. “Transonic Panel Flutter.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1476. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1476
• Davis, Wallace F., Sherman S. Edwards, and George B. Brajnikoff. 1949. Experimental Investigation at Supersonic Speeds of Twin-Scoop Duct Inlets of Equal Area IV: Some Effects of Internal Duct Shape upon an Inlet Enclosing 37.2 Percent of the Forebody Circumference. NACA-RM-A9A31. NASA. https://ntrs.nasa.gov/citations/19930085928
• Davis, Wallace F., and David L. Goldstein. 1948. Experimental Investigation at Supersonic Speeds of Twin-Scoop Duct Inlets of Equal Area I: An Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody. NACA-RM-A7J27. NASA. https://ntrs.nasa.gov/citations/19930085760
• Davis, Milt W., Alan A. Hale, Charles Vining, and William T. Cousins. 2008. “Application of Numerical Analysis Tools for Airframe-Propulsion Integrated Test and Evaluation.” In Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Manufacturing, Materials and Metallurgy; Microturbines and Small Turbomachinery. ASMEDC. https://doi.org/10.1115/gt2008-50194
• Davis, Jake, and David Marshall. 2020. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” In AIAA Scitech 2020 Forum. AIAA 2020-1748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1748
• Davis, Randall C., Dick M. Royster, and Thomas T. Bales. 1987. Analysis and Test of Superplastically Formed Titanium Hat-Stiffened Panels under Compression. NASA-TM-88989. NASA. https://ntrs.nasa.gov/citations/19870008686
• Davis, Randall C., Dick M. Royster, and Thomas T. Bales. 1990. Superplastically Formed Titanium Hat-Stiffened Panels. LAR-13814. NASA Langley Research Center, Hampton, VA. https://ntrs.nasa.gov/citations/19900000033
• 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, David, Manan Vyas, and John Slater. 2012. “Research on Supersonic Inlet Bleed.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-272. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-272
• Davis, D. D., Jr., and D. E. Wornom. 1958. Buffet Tests of an Attack-Airplane Model with Emphasis on Analysis of Data from Wind-Tunnel Tests. NACA-RM-L57H13. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630002658
• 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
• 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, Richard E., and Jack Fischel. 1955. Stability and Control Characteristics Obtained during Demonstration of the Douglas X-3 Research Airplane. NACA-RM-H55E16. NASA. https://ntrs.nasa.gov/citations/19930088730
• Day, R. P., and A. Guthrie. 1958. Thermal Measurements from Aircraft in Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0339907
• 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
• De Castro, Jonathan, Liang Tang, Kenneth Loparo, and Kai Goebel. 2010. “Stochastic Reachable-Set Policies for Aircraft Upset Reconfiguration Problems with Time-Scale Separation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7867
• De Gaspari, Alessandro, Sergio Ricci, Luca Riccobene, and Alessandro Scotti. 2007. “Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-2138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2138
• de Melo, Felipe Buarque Cordeiro, Flavio L. S. Bussamra, and Angelo A. Verri. 2024. “Static Aeroelastic Rolling of a Highly Flexible Wing: Pazy Wing with Aileron.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3761279/v1
• De Oro Fernandez, Elena, Thomas Andrianne, and Grigorios Dimitriadis. 2020. “A Database of Flutter Characteristics for Simple Low and Medium Aspect Ratio Wings at Low Speeds.” In AIAA Scitech 2020 Forum. AIAA 2020-2172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2172
• de Paula, Adson A., Fabricio M. Porto, and Marcelo S. Sousa. 2017. “Aerodynamic Lateral-Directional Coefficients Modeling during Aircraft Design Phases.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2017-1759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1759
• Deak, A. L., and R. C. Johnston. 1973. Stress Analysis of Loaded Rolling Aircraft Tires. Volume II. Computer Program. Defense Technical Information Center. https://doi.org/10.21236/adb004564
• Deakins, Ralph R., and C. L. Blackburn. 1965. “Simulation of High Sink Speed Landing Gear.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/650845
• 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
• Debiasi, Marco T., Kevin Atkinson, Alistair Saddington, and Mark Finnis. 2023. “Aero-Whisker for the Measurement of Aircraft Flight Speed and Angle of Attack in Compressible Flow Conditions.” In AIAA AVIATION 2023 Forum. AIAA 2023-4079. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4079
• 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
• Dejarnette, F. 1983. “Aerodynamic Heating and Surface Temperatures on Vehicles for Computer-Aided Design Studies.” In 21st Aerospace Sciences Meeting. AIAA 1983-411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-411
• Dejarnette, F., H. Hamilton, and K. Weilmuenster. 1985. “A Review of Some Approximate Methods Used in Aerodynamic Heating Analyses.” In 20th Thermophysics Conference. AIAA 1985-906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-906
• DeJarnette, Fred R., and Kenneth M. Jones. 1978. Development of a Computer Program to Calculate Aerodynamic Characteristics of Bodies and Wing-Body Combinations. Defense Technical Information Center. https://doi.org/10.21236/ada055846
• 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, and John Saltzman. 1992. “In-Flight Flow Visualization Results from the X-29A Aircraft at Highangles of Attack.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4102
• Del Prete, Antonio, Teresa Primo, and Antonio Alberto de Vitis. 2007. “Non Deterministic Approach in Metal Forming Springback Simulation.” In Key engineering materials. Trans Tech Publications. https://doi.org/10.4028/0-87849-437-5.399
• DeLaat, John C. 1998. Distortion Tolerant Control Demonstrated in Flight. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/20050180663
• Delannay, L. 2004. “Prediction of the Planar Anisotropy of Springback after Bending of a Textured Zinc Sheet.” In AIP Conference Proceedings, vol. 712. AIP. https://doi.org/10.1063/1.1766668
• DeLaurier, James. 2022. “Flight Dynamics.” In Aircraft Design Concepts. CRC Press. https://doi.org/10.1201/9781315228167-6
• Della Vecchia, Pierluigi, Fabrizio Nicolosi, and Danilo Ciliberti. 2015. “Aircraft Directional Stability Prediction Method by CFD.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2255. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2255
• Demeri, Mahmoud Y., Maurice Lou, and Michael J. Saran. 2000. “A Benchmark Test for Springback Simulation in Sheet Metal Forming.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2000-01-2657
• Demetriades, A. 1983. The Hydrodynamic Stability of a Supersonic Laminar Boundary Layer over a Rough Wall. Defense Technical Information Center. https://doi.org/10.21236/ada137056
• Demetriades, A. 1985. Supersonic Boundary Layer Stability over a Rough Wall. Defense Technical Information Center. https://doi.org/10.21236/ada179580
• 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
• DeMoss, Joshua, and Roger Simpson. 2010. “Measurements of the Steady Skin Friction and Cross-Flow Separation Location on an Ellipsoidal Model in Yaw or Pitch over a Range of Roll Angles.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-317. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-317
• Deneke, Joseph A., Darius Carter, Ajay Pandya, and Ella Heisterkamp. 2026. “The Effect of Wingtip Geometry on Wake Vortex Dynamics for a Low Aspect Ratio Wing.” In AIAA SCITECH 2026 Forum. AIAA 2026-0884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0884
• 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
• Dennard, John S. 1959. The Total-Pressure Recovery and Drag Characteristics of Several Auxiliary Inlets at Transonic Speeds. NASA-MEMO-12-21-58L. NASA. https://ntrs.nasa.gov/citations/19980231994
• Denney, Russell, Jimmy Tai, and Dimitri Mavris. 2012. “Parametric Geometry for Propulsion-Airframe Integration.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-548. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-548
• Derbel, Khaoula, and Károly Beneda. 2025. “Investigation of Turbojet Engine Performance in Subsonic Flight Conditions with Turbofan Power Ratio as Thrust Parameter.” Periodica Polytechnica Transportation Engineering 53 (2): 194–205. https://doi.org/10.3311/pptr.37560
• DeSisto, Thomas S. 1973. Fracture Toughness Measurements of Three Titanium Alloy Extrusions. Defense Technical Information Center. https://doi.org/10.21236/ad0766682
• Desmarais, R., and W. Reed III. 1980. “Wing/store Flutter with Nonlinear Pylon Stiffness.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-792
• Devan, Leroy. 1989. “Nonaxisymmetric Body, Supersonic, Inviscid Dynamic Derivative Prediction.” In 7th Applied Aerodynamics Conference. AIAA 1989-2195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2195
• “The Development of Anomaly Distributions for Aircraft Engine Titanium Disk Alloys.” 1997. In 38th Structures, Structural Dynamics, and Materials Conference. AIAA 1997-1068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1068
• Development of Longitudinal and Lateral–Directional Transfer Functions. 2014. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102547.0661.0664
• Development of Longitudinal and Lateral–Directional Transfer Functions. 2024. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624107252.0731.0734
• Dewispelare, A., and R. Stager. 1981. “Investigation of Landing Gear Alternatives for High Performance Aircraft.” In Aircraft Systems and Technology Conference. AIAA 1981-1639. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1639
• 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
• Dias, Joaquim N. 2015. “High Angle of Attack Model Identification with Compressibility Effects.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-1477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1477
• Dias, Joaquim N., and Fabio Almeida. 2013. “High Angle of Attack Model Identification without Air Flow Angle Measurements.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4980. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4980
• 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
• Díaz, R., K. Nguyen, F. Montáns, and M. Sanz. 2021. “Numerical Prediction of Springback in Sheet Metal Forming in Anisotropic Elastoplastic Finite Strains.” In 14th WCCM-ECCOMAS Congress. CIMNE. https://doi.org/10.23967/wccm-eccomas.2020.237
• 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
• DiCesare, Eugene. 1961. Hot Rolling of Commercially Pure Titanium and Titanium Alloy Ti-6Al-4V. Defense Technical Information Center. https://doi.org/10.21236/ada952365
• 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
• Dickinson, R. L. 1953. Aerodynamic Data for Structural Loads. Defense Technical Information Center. https://doi.org/10.21236/ada953109
• Dickinson, Luke, Holger Babinsky, and Christopher Sheaf. 2024. “Experimental Investigation of Shock-Induced Inlet Boundary-Layer Separation Due to Crosswind.” In AIAA SCITECH 2024 Forum. AIAA 2024-2845. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2845
• Dickman, Christopher A., and Timothy T. Takahashi. 2016. “Engine/Inlet Matching for Supersonic Aircraft Design.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0771
• Diederich, Franklin W., and Kenneth A. Foss. 1953. Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Loading of Swept and Unswept Wings. NACA-TR-1140. NASA. https://ntrs.nasa.gov/citations/19930092169
• Diederich, Franklin W., and Martin Zlotnick. 1949. Theoretical Spanwise Lift Distributions of Low-Aspect-Ratio Wings at Speeds below and above the Speed of Sound. NACA-TN-1973. NASA. https://ntrs.nasa.gov/citations/19930082642
• Digges, Kennerly H. 1971. Theory of an Air Cushion Landing System for Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0728647
• Diggins, J. L. 1951. Diffuser Investigations in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0895227
• Dikbas, Erdem, and Hediye Atik. 2018. “CFD-Based Planform Design Study of a Low Aspect Ratio Wing.” In 2018 Applied Aerodynamics Conference. AIAA 2018-4127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4127
• Dilan, Rasim Aşkın, Tuna Balkan, and Bülent E. Platin. 2016. “Application of Multivariate Adaptive Regression Splines to Sheet Metal Bending Process for Springback Compensation.” MATEC Web of Conferences 80: 14002. https://doi.org/10.1051/matecconf/20168014002
• Dillenius, Marnix F. E. 1985. Program LRCDM2: Improved Aerodynamic Prediction Program for Supersonic Canard-Tail Missiles with Axisymmetric Bodies. NASA-CR-3883. NASA. https://ntrs.nasa.gov/citations/19870019092
• DİNÇ, Ali. 2021. “Metering Pin Diameter Optimization of an Aircraft Landing Gear Shock Absorber.” Eskişehir Teknik Üniversitesi Bilim ve Teknoloji Dergisi B - Teorik Bilimler 9 (2): 37–46. https://doi.org/10.20290/estubtdb.900786
• Ding, Ziying, Zhidong Chang, and Jun Chen. 2025. “Springback Behaviour of Titanium Alloy at Room Temperature by Flexible Free Incremental Sheet Forming: Experiments and Simulations.” Journal of Physics: Conference Series 3104 (1): 012067. https://doi.org/10.1088/1742-6596/3104/1/012067
• Ding, F., C.-B. Shen, W. Huang, and J. Liu. 2015. “Numerical Validation and Back-Pressure Effect on Internal Compression Flows of Typical Supersonic Inlet.” Aeronautical Journal 119 (1215): 631–45. https://doi.org/10.1017/s0001924000010721
• Ding, Yong Wei, Xiao Hui Wei, Hong Nie, and Yong Ping Li. 2018. “Discharge Coefficient Calculation Method of Landing Gear Shock Absorber and Its Influence on Drop Dynamics.” Journal of Vibroengineering 20 (7): 2550–62. https://doi.org/10.21595/jve.2018.19049
• 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
• Disney, T. 1966. “The Relationship between Aircraft Design and Flight-Measured Loads.” In 3rd Annual Meeting. AIAA 1966-881. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-881
• “Dive Testing for Flutter, Vibration, and Buffeting.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0417.0426
• 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
• Dix, D., and G. Smith. 1971. “Analysis of Combustion Instability in Aircraft Engine Augmentors.” In 7th Propulsion Joint Specialist Conference. AIAA 1971-700. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-700
• 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 Optimization of Tapered Wing Structure.” In Introduction to Aeroelasticity. Springer Nature Singapore. https://doi.org/10.1007/978-981-16-8078-6_19
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2011b. “Supersonic Inlet Duct Unstart Induced by Fuel Jet Injection.” In Proceeding of Seventh International Symposium on Turbulence and Shear Flow Phenomena. Begellhouse. https://doi.org/10.1615/tsfp7.1670
• Do, Hyungrok, Seong-kyun Im, Mark Mungal, and Mark Cappelli. 2011c. “Unstart of a Supersonic Model Inlet/Isolator Flow Induced by Mass Injection.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-68. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-68
• Dobson, R. K., and E. L. Whiffen. 1984. Hot Forming with Electron-Beam Welder. MSC-20413. Rockwell International Corp. https://ntrs.nasa.gov/citations/19830000724
• Dodbele, S., and A. Plotkin. 1985. “Lift Due to Thickness for Low Aspect Ratio Wings in Incompressible Flow.” In 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. AIAA 1985-1588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1588
• Dodds, H. W., and G. F. Davies. 1954. “Hot Pressing, Press Forming Loom as Answers to Titanium Fabrication.” JOM 6 (10): 1116–18. https://doi.org/10.1007/bf03398040
• Dods, J., Jr., and R. Hanly. 1972. “Evaluation of Transonic and Supersonic Wind-Tunnel Background Noise and Effects of Surface Pressure Fluctuation Measurements.” In 7th Aerodynamic Testing Conference. AIAA 1972-1004. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1004
• Doggett, R., Jr., and R. Ricketts. 1977. “Some Experimental and Theoretical Flutter Characteristics of an Arrow-Wing Configuration.” In 18th Structural Dynamics and Materials Conference. AIAA 1977-422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-422
• 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, Jr., and David Soistmann. 1989. “Some Low-Speed Flutter Characteristics of Simple Low-Aspect-Ratio Delta Wing Models.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1325
• 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
• Dollyhigh, S. 1970. “Some Trim Drag Considerations for Maneuvering Aircraft.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-932
• Dollyhigh, S. M. 1974. Subsonic and Supersonic Longitudinal Stability and Control Characteristics of an Aft Tail Fighter Configuration with Cambered and Uncambered Wings and Uncambered Fuselage. NASA-TM-X-3078. NASA. https://ntrs.nasa.gov/citations/19740023306
• Domack, Christopher. 1991. “A Preliminary Investigation of Inlet Unstart Effects on a High-Speedcivil Transport Concept.” In 9th Applied Aerodynamics Conference. AIAA 1991-3327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3327
• Domack, Christopher S. 1992. “Results of a Preliminary Investigation of Inlet Unstart on a High-Speed Civil Transport Airplane Concept.” In NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 3. https://ntrs.nasa.gov/citations/19940029002
• Domingos, Fernando A., Flavio Luiz C. Ribeiro, and Bruno Silva. 2024. “Simultaneous Estimation of Engine Deck and Drag Polar Based on Specific Excess Power Measurement.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4561. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4561
• Dommasch, Daniel O., W. J. Hesse, T. W. Davidson, and Phillip Hufton. 1959. “Performance of Turbojet Airplanes.” In Performance. Elsevier. https://doi.org/10.1016/b978-1-4831-9729-6.50016-4
• Donaldson, D. R. 1952. “Discussion: “Friction Surfaces for Spin-Up Simulation in Landing-Gear Drop Tests” (Drake, D. W., 1952, Trans. ASME, 74, Pp. 1269–1279).” Journal of Fluids Engineering 74 (7): 1279–81. https://doi.org/10.1115/1.4016094
• Donaldson, Steven, James Priest, Kevin Cunningham, and John Foster. 2012. “Upset Simulation and Training Initiatives for U.S. Navy Commercial Derived Aircraft.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2012-4570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4570
• Dong, Lei, Kwing-So Choi, and Yaxing Wang. 2022. “Plasma Flow Control of the Tip Vortices over a Very Low Aspect-Ratio Wing.” Physics of Fluids 34 (8): 087101. https://doi.org/10.1063/5.0101110
• Dongdong, Ge, Zhang Zihao, and Wang Kuan. 2025. “Research on Drop Test Methods for Four-Wheel Bogie-Type Landing Gear for Large Civil Aircraft.” IET Conference Proceedings 2024 (13): 344–48. https://doi.org/10.1049/icp.2024.2873
• Dongmo, Jean-Etienne. 2011. “Aircraft Loss-Of-Control Recovery Using Nonlinear Smooth Feedback Regulators.” In Infotech@Aerospace 2011. AIAA 2011-1562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1562
• Donlan, C. J. 1976. Spin Tests of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range, May 1941. NACA-TN-807. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19770022120
• Donov, A. E. 1956. A Flat Wing with Sharp Edges in a Supersonic Stream. NACA-TM-1394. NASA. https://ntrs.nasa.gov/citations/19930093836
• Dougherty, Nathan S. 2021. “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., 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 Long Beach Ca. 1962. An Investigation of the Landing Loads Experienced by the A4D-2 Airplane during Flight Tests and Drop Tests and a Comparison with Theory. Defense Technical Information Center. https://doi.org/10.21236/ad0404510
• Dowell, E. 1964. “The Flutter of Multi-Bay Panels at High Supersonic Speeds.” In Aerospace Sciences Meeting. AIAA 1964-92. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-92
• Dowell, E. 1970. “Generalized Aerodynamic Forces on a Flexible Plate Undergoing Transient Motion in a Shear Flow with an Application to Panel Flutter.” In 8th Aerospace Sciences Meeting. AIAA 1970-76. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-76
• Dowell, Earl H. 1996. Limit Cycle Oscillations (LCO) and Nonlinear Aeroelastic Wing Response. Defense Technical Information Center. https://doi.org/10.21236/ada325524
• Dowell, Earl H. 1999. Limit Cycle Oscillations (LCO) and Nonlinear Aeroelastic Wing Response: Reduced Order Aerodynamic Models. Defense Technical Information Center. https://doi.org/10.21236/ada362982
• Dowell, Earl H., and Oddvar Bendiksen. 2010. Panel Flutter. Wiley. https://doi.org/10.1002/9780470686652.eae152
• Dowling, James J., Jennifer L. Durkin, and David M. Andrews. 2006. “The Uncertainty of the Pendulum Method for the Determination of the Moment of Inertia.” Medical Engineering & Physics 28 (8): 837–41. https://doi.org/10.1016/j.medengphy.2005.11.007
• Drachinsky, Ariel, Or Avin, Daniella E. Raveh, Yaron Ben-Shmuel, and Moshe Tur. 2022. “Flutter Tests of the Pazy Wing.” In AIAA SCITECH 2022 Forum. AIAA 2022-2186. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2186
• Drake, D. W. 1952a. “Closure to “Discussions of ‘Friction Surfaces for Spin-Up Simulation in Landing-Gear Drop Tests’” (1952, Trans. ASME, 74, Pp. 1279–1281).” Journal of Fluids Engineering 74 (7): 1281–1281. https://doi.org/10.1115/1.4016097
• Drake, D. W. 1952b. “Friction Surfaces for Spin-Up Simulation in Landing-Gear Drop Tests.” Journal of Fluids Engineering 74 (7): 1269–79. https://doi.org/10.1115/1.4016093
• Drake, H. M. 1957. “Flight Research at High Altitude, Part 1.” In AGARD Proc. of the Seventh AGARD Gen. Assembly. https://ntrs.nasa.gov/citations/19820068145
• 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
• Driver, Cornelius. 1958. Longitudinal and Lateral Stability and Control Characteristics of Various Combinations of the Component Parts of Two Canard Airplane Configurations at Mach Numbers of 1.41 and 2.01. NASA-MEMO-10-1-58L. NASA. https://ntrs.nasa.gov/citations/19980232000
• Driver, C. 1960. Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing. NASA-TM-X-328. NASA. https://ntrs.nasa.gov/citations/19650003199
• Drougge, G. 1990. “30th Lanchester Memorial Lecture: The Wave Drag of Delta Wings at Supersonic Speeds: A Recent Study.” Aeronautical Journal 94 (937): 225–30. https://doi.org/10.1017/s000192400002296x
• Dryer, Murray, and Andrew Beke. 1952. Performance Characteristics of a Normal-Shock Side Inlet Located Downstream of a Canard Control Surface at Mach Numbers of 1.5 and 1.8/. NACA-RM-E52F09. NASA. https://ntrs.nasa.gov/citations/19930087106
• Du, Zhihao, Yanbin Han, Dong Han, et al. 2024. “Effect of Heat Treatment and Electromagnetic Forming on Springback and Properties of 7075 Aluminum Alloy Sheet.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4467825/v1
• Du, Changqing, Li Zhang, and Neng-Ming Wang. 1994. “Springback Prediction in Sheet Forming Simulation.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/940937
• Duan, Bin, Khaled Abdel-Motagaly, Xinyun Guo, and Chuh Mei. 2003. “Suppression of Supersonic Panel Flutter and Thermal Deflection Using Shape Memory Alloy.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1513
• Duda, Benjamin M., Andreas Deuring, Francisco Flores Alvarenga, and Gregory M. Laskowski. 2022. “Landing Gear Retraction under Aerodynamic Loads.” In AIAA AVIATION 2022 Forum. AIAA 2022-3527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3527
• Due, H. 1987. “Development of the Model 373 Turbojet Engine.” In 23rd Joint Propulsion Conference. AIAA 1987-1908. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1908
• Dugundji, John. 1965. Theoretical Considerations of Panel Flutter at High Supersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ad0624995
• Dugundji, John, Earl Dowell, and Brian Perkin. 1962. Subsonic Flutter of Panels on Continuous Elastic Foundations: Experiment and Theory. Defense Technical Information Center. https://doi.org/10.21236/ad0278235
• Duncan, R. M., and R. T. J. Hubbard. 1973. “Applications of the High Strength Alloy Ti-4A1-4Mo-2Sn-0.5Si in European Aircraft Projects.” In Titanium Science and Technology. Springer US. https://doi.org/10.1007/978-1-4757-1346-6_9
• 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
• Dunlap, Everett W., and Milton B. Porter. 1971. Theory of the Measurement and Standardization of in-Flight Performance of Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0725741
• 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
• Durvasula, S. 1966. “Flutter of Simply-Supported Parallelogrammic Flat Panels in Supersonic Flow.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-474
• Dusing, Douglas, and Paul Orkwis. 1993. “On Computing Vortex Asymmetries about Cones at Angle of Attack Usingthe Conical Navier-Stokes Equations.” In Flight Simulation and Technologies. AIAA 1993-3628. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3628
• Dussauge, Jean-Paul, Pierre Dupont, Sebastien Piponniau, Lionel Larcheveque, and Alexander John Smits. 2025. “Effects of Limited Resolution on PIV Measurements of Boundary Layer Turbulence in High-Speed Flow.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-7890132/v1
• Dutta, Deepnil, Anubhav Dasgupta, Prince Raj Lawrence Raj, and Koustuv Debnath. 2022. “Drag Reduction and Turbulent Characteristics of a Low Aspect Ratio Wing with Fluidic on-Demand Winglet.” SAE International Journal of Aerospace 16 (1): 39–55. https://doi.org/10.4271/01-16-01-0003
• Dyko, Mark P., and Benjamin T. F. Chung. 1990. “Finite Element Thermal Model of an Aircraft Wheel and Carbon Brake Assembly.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/901909
• Dyko, M. P., and K. Vafai. 1998. “Fundamental Issues and Recent Advancements in Analysis of Aircraft Brake Natural Convective Cooling.” Journal of Heat Transfer 120 (4): 840–57. https://doi.org/10.1115/1.2825903
• “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
• “Dynamics of Aircraft Motion.” 2015. In Flight Dynamics. Princeton University Press. https://doi.org/10.2307/j.ctt1287kgx.6
• “Dynamics of Elastically Supported Rigid Airfoils.” 2023. In Dynamics of Flexible Aircraft. Cambridge University Press. https://doi.org/10.1017/9781108354868.004
• “Dynamics of Flexible Aircraft with Quasi-Steady Deformations.” 2023. In Dynamics of Flexible Aircraft. Cambridge University Press. https://doi.org/10.1017/9781108354868.006
• 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. Time-Dependent in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air5020
• E-33 In Flight Propulsion Measurement Committee. n.d.-e. Uncertainty of in-Flight Thrust Determination. SAE International. https://doi.org/10.4271/air1678a
• E28 Committee. n.d. Test Method for Evaluating Springback of Sheet Metal Using the Demeri Split Ring Test. ASTM International. https://doi.org/10.1520/e2492-07r12
• Eagle, Walter, James Driscoll, and John Benek. 2012. “3-D Inlet Shock-Boundary Layer Interactions: PIV Database for the Second SBLI Workshop.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3214
• Earl, T. Desmond. 1967. Air Cushion Landing Gear Feasibility Study. Defense Technical Information Center. https://doi.org/10.21236/ad0817527
• Early, K. 2000. “Propulsion Airframe Integration Design, Analysis and Challenges Going into the 21st Century.” Aeronautical Journal 104 (1038): 375–82. https://doi.org/10.1017/s0001924000064010
• Eastep, F., and J. Olsen. 1979. “Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1632
• 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
• Eckstrom, C. V. 1976. Flight Loads Measurements Obtained from Calibrated Strain-Gage Bridges Mounted Externally on the Skin of a Low-Aspect-Ratio Wing. NASA-TN-D-8349. NASA. https://ntrs.nasa.gov/citations/19770009075
• Edmondson, James L. 1950. Damping in Roll of Rectangular Wings of Several Aspect Ratios and NACA 65A-Series Airfoil Sections of Several Thickness Ratios at Transonic and Supersonic Speeds as Determined with Rocket-Powered Models. NACA-RM-L50E26. NASA. https://ntrs.nasa.gov/citations/19930090407
• Edwards, R. 1992. “An Approach for Increasing Aeroelastic Divergence Dynamic Pressure of Wind-Tunnel Models.” In 17th Aerospace Ground Testing Conference. AIAA 1992-4002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4002
• Edwards, John W. 1996. “Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method.” In EUROMECH-Colloquium: Simulation of Fluid-Structure Interaction in Aeronautics. https://ntrs.nasa.gov/citations/19960054470
• Edwards, W. H., and R. C. Dickason. 1966. “Hot Forming of Sheet Titanium Alloy.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/660644
• “Effect of High Mach Numbers on High-Speed Aircraft.” 2010. In German Development of the Swept Wing 1935–1945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867552.0375.0442
• “Effect of Sweep Angle and a Half Sine Wave on Roll Damping Derivative of a Delta Wing.” 2019. International Journal of Recent Technology and Engineering (IJRTE) 8 (2S3): 984–89. https://doi.org/10.35940/ijrte.b1184.0782s319
• Ehlers, F., F. Johnson, and P. Rubbert. 1976. “A Higher Order Panel Method for Linearized Supersonic Flow.” In 9th Fluid and PlasmaDynamics Conference. AIAA 1976-381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-381
• Ehrmayr, Robert, and Thomas M. Berens. 2018. “Numerical Investigations on an Advanced Diverterless Supersonic Inlet with a Corner Bump in a Wing-Fuselage Installation.” In 2018 Joint Propulsion Conference. AIAA 2018-4746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4746
• Ehyaei, M. A., A. Anjiridezfuli, and M. A. Rosen. 2013. “Exergetic Analysis of an Aircraft Turbojet Engine with an Afterburner.” Thermal Science 17 (4): 1181–94. https://doi.org/10.2298/tsci110911043e
• El Aziz, A., M. Katary, and I. Mansour. 1993. “Effect of Aerodynamic Cross-Coupling on the Stability of a Rolling Aircraft.” International Conference on Aerospace Sciences and Aviation Technology 5 (ASAT CONFERENCE): 1–8. https://doi.org/10.21608/asat.1993.25599
• El-Sayed, Ahmed F. 2026. “Turbojet Engine.” In Aircraft and Rocket Propulsion and Gas Turbine Engines. CRC Press. https://doi.org/10.1201/9781003561538-5
• “Elements of Computational Engine/Airframe Integration.” 1986. In Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865763.0127.0168
• Ellis, David L. 2012. Effects of Long-Term Thermal Exposure on Commercially Pure Titanium Grade 2 Elevated-Temperature Tensile Properties. NASA/TM-2012-215484. NASA. https://ntrs.nasa.gov/citations/20130001734
• 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
• Elsayed, A., M. Mohamed, M. Shazly, and A. Hegazy. 2017. “An Investigation and Prediction of Springback of Sheet Metals under Cold Forming Condition.” IOP Conference Series: Materials Science and Engineering 280: 012021. https://doi.org/10.1088/1757-899x/280/1/012021
• 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
• Engelbrecht, Alfred Edwin. n.d. “Coupled Bending and Torsional Free Vibration of a Swept Wing.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-14663
• Engelbrecht, Jacobus, Simon Pauck, and Iain Peddle. 2012. “Bifurcation Analysis and Simulation of Stall and Spin Recovery for Large Transport Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4801
• Engelbrecht, Jacobus A., Simon J. Pauck, and Iain K. Peddle. 2013. “A Multi-Mode Upset Recovery Flight Control System for Large Transport Aircraft.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5172
• Engine Inlet, Exhaust, and Nacelle Systems. 2011. Wiley. https://doi.org/10.1002/9781119975489.ch6
• “Engine/Airframe Performance Matching.” 1989. In Aircraft Propulsion Systems Technology and Design. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861499.0167.0237
• English, Roland D., and Howard S. Carter. 1960. Variation in Heat Transfer during Transient Heating of a Hemisphere at a Mach Number of 2. NASA-TN-D-399. NASA. https://ntrs.nasa.gov/citations/19890068389
• Enright, John. 2000. “Reducing Aircraft Brake Squeal with a Damped Brake-Rod.” In 2000 World Aviation Conference. AIAA 2000-5599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5599
• Epstein, Melvin. 1954. The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges. Defense Technical Information Center. https://doi.org/10.21236/ad0037709
• Equipment, Eg-1E Gas Turbine Test Facilities and. 2008. Turbofan and Turbojet Gas Turbine Engine Test Cell Correlation. https://doi.org/10.4271/arp741b
• Erbin, E. F. 1963. “For a Supersonic Transport: II. Titanium.” JOM 15 (3): 192–93. https://doi.org/10.1007/bf03378227
• Eremenko, Paul, Christopher Mouton, and Hans Hornung. 2003. “The Wave Drag of Blunted Cones in Axisymmetric Supersonic Flow.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1269
• Erickson, Gary E. 1991. Wind Tunnel Investigation of Vortex Flows on F/A-18 Configuration at Subsonic through Transonic Speed. NASA-TP-3111. NASA. https://ntrs.nasa.gov/citations/19920005750
• Erickson, Gary, and Jay Brandon. 1987. “On the Nonlinear Aerodynamic and Stability Characteristics of a Generic Chine-Forebody Slender-Wing Fighter Configuration.” In 5th Applied Aerodynamics Conference. AIAA 1987-2617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2617
• Erickson, Gary E., Robert M. Hall, Daniel W. Banks, John H. Del Frate, and John A. Schreiner. 1989a. “Experimental Investigation of the F/A-18 Vortex Flows at Subsonic through Transonic Speeds.” In AIAA. https://ntrs.nasa.gov/citations/19890060307
• Erickson, Gary, John Schreiner, and Lawrence Rogers. 1989b. “On the Structure, Interaction, and Breakdown Characteristics of Slender Wing Vortices at Subsonic, Transonic, and Supersonic Speeds.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3345
• Ericsson, L. 1980. “Wing-Body Pitch Damping at Arbitrary Mach Number.” In Aircraft Systems Meeting. AIAA 1980-1801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1801
• 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
• Ericsson, L. 1986. “Vortex-Induced Effects on Aircraft Dynamics.” In 13th Atmospheric Flight Mechanics Conference. AIAA 1986-2279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2279
• Ericsson, Lars. 1996a. “Analysis of the Effect of Sideslip on Delta Wing Roll Trim Characteristics.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-788. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-788
• Ericsson, Lars. 1996c. “Effect of Angle of Attack on Roll Characteristics of 65 Deg Delta Wing.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3443
• Ericsson, L., and H. King. 1990. “Rapid Prediction of Slender-Wing Aircraft Dynamics.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3037. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3037
• Esenwein, Fred T. 1952. Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane III: Normal Wedge Inlet with Semicircular Cowl. NACA-RM-E52H20. NASA. https://ntrs.nasa.gov/citations/19930087252
• Esenwein, Fred T., and Carl F. Schueller. 1952. Analytical and Experimental Investigation of Inlet-Engine Matching for Turbojet-Powered Aircraft at Mach Numbers up to 2.0. NACA-RM-E51K20. NASA. https://ntrs.nasa.gov/citations/19930087893
• Esser, Steven, and Hans-Joachim K. Ruff-Stahl. 2021. “An HFACS Analysis of German F-104 Starfighter Accidents.” Journal of Aviation Technology and Engineering 9 (2): 19. https://doi.org/10.7771/2159-6670.1218
• Est, Brian, and H. Nelson. 1991. “Fin Dihedral Effects on Aerodynamics of Supersonic Missiles with Square and Triangular Fuselage Cross Sections.” In 9th Applied Aerodynamics Conference. AIAA 1991-3256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3256
• “Estimating the Takeoff Wing Loading.” 2010. In Fundamentals of Aircraft and Airship Design. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867538.0151.0169
• Estman, L., D. Merdol, K.-G. Brask, V. Kalhori, and Y. Altintas. 2013. “Development of Machining Strategies for Aerospace Components, Using Virtual Machining Tools.” In Lecture Notes in Production Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-319-01964-2_9
• Eugeni, Marco, Franco Mastroddi, and Francesco Saltari. 2020. “Damping Models in Aircraft Flutter Analyses.” In Nonlinear Dynamics of Structures, Systems and Devices. Springer International Publishing. https://doi.org/10.1007/978-3-030-34713-0_42
• 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. J., and C. L. Mesiah. 1974. Identification of the Longitudinal Stability and Control Parameters of the YT-2B Airplane. Defense Technical Information Center. https://doi.org/10.21236/ada021994
• 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
• “European Transonic Windtunnel Project.” 1990. Aircraft Engineering and Aerospace Technology 62 (12): 18–19. https://doi.org/10.1108/eb037033
• “Evaluation of Methods for Prediction and Prevention of Wing/store Flutter.” 1981. In Dynamics Specialists Conference. AIAA 1981-606. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-606
• Evans, D. G., C. E. Debogdan, R. H. Soeder, and E. J. Pleban. 1974. “Some Comparisons of the Flow Characteristics of a Turbofan Compressor System with and without Inlet Pressure Distortion.” In Workshop on Unsteady Flows in Jet Engines. https://ntrs.nasa.gov/citations/19740053438
• Eves, Kameron J., and John Valasek. 2024. “Inlet Unstart Prevention by Adaptive Regulation Using a Nonlinear Longitudinal Timescale Model.” In AIAA SCITECH 2024 Forum. AIAA 2024-2874. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2874
• Evvard, John C. 1947a. Distribution of Wave Drag and Lift in the Vicinity of Wing Tips at Supersonic Speeds. NACA-TN-1382. NASA. https://ntrs.nasa.gov/citations/19930082018
• Evvard, John C. 1947b. The Effects of Yawing Thin Pointed Wings at Supersonic Speeds. NACA-TN-1429. NASA. https://ntrs.nasa.gov/citations/19930082174
• Evvard, John C. 1948. Theoretical Distribution of Lift on Thin Wings at Supersonic Speeds: (An Extension). NACA-TN-1585. NASA. https://ntrs.nasa.gov/citations/19930082236
• Evvard, John C. 1950. Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds. NACA-TR-951. NASA. https://ntrs.nasa.gov/citations/19930092016
• Evvard, John C., and L. Richard Turner. 1947. Theoretical Lift Distribution and Upwash Velocities for Thin Wings at Supersonic Speeds. NACA-TN-1484. NASA. https://ntrs.nasa.gov/citations/19930082142
• “Experimental Study of Diffusion Bonding/superplastic Forming of Dissimilar Aluminium Alloys.” 2018. International Journal of Recent Trends in Engineering and Research 4 (5): 172–78. https://doi.org/10.23883/ijrter.2018.4304.mz8a9
• “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
• Ezrokhi, Yury, Daniil Fokin, and Pavel Nyagin. 2020. “Mathematical Modelling Application for Characteristics Estimation of Bypass Turbojet with Common Afterburner.” Vestnik Moskovskogo aviatsionnogo instituta 27 (2): 99–111. https://doi.org/10.34759/vst-2020-2-99-111
• “F. Nonsteady Wing Characteristics.” 1957. In Aerodynamic Components of Aircraft at High Speeds. Princeton University Press. https://doi.org/10.1515/9781400879908-015
• “Fabrication and Properties of Titanium Aluminides.” 2003. Metal Powder Report 58 (3): 39. https://doi.org/10.1016/s0026-0657(03)80087-5
• Fagley, Casey P., Jurgen Seidel, and Thomas E. McLaughlin. 2015. “Investigation of Aeroelastic Flow Control of a Fluttering Wing with HPCMP CREATE™-AV Kestrel.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-1505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1505
• Falempin, Francois, Eric Wendling, Marat Goldfeld, and Alexander Starov. 2006. “Experimental Investigation of Starting Process for a Variable Geometry Air Inlet Operating from Mach 2 to Mach 8.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4513
• Fan, Yuehua, Zhenxun Gao, Chongwen Jiang, and Chun-Hian Lee. 2017. “Effects of Steam Ingestion on under Fuselage Inlet Performance during a Catapult-Assisted Takeoff Process.” Journal of Fluids Engineering 140 (4): 041101. https://doi.org/10.1115/1.4038092
• Fang, Ming Xia. 2011. “Aeroelastic Analysis of Supersonic Airfoil with Hysteretic Nonlinearities.” Applied Mechanics and Materials 141: 180–85. https://doi.org/10.4028/www.scientific.net/amm.141.180
• Fann, Kuang-Jau, Lin-Pen Chen, Chun-Yen Yang, Chen-Yi Lee, Chang-Yu Tsai, and Jyhwen Wang. 2025. “An Artificial Intelligence Application for in-Process Springback Control of Sheet Metal Bending.” Journal of Manufacturing Science and Engineering 147 (6): 061005. https://doi.org/10.1115/1.4067740
• Fano, Devon, Jonathan Poggie, and Gregory A. Blaisdell. 2020. “Aerodynamic Heating in Missile-Fin Interaction Region.” In AIAA Scitech 2020 Forum. AIAA 2020-0583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0583
• Fanta, G., R. Bohn, Michael Dahms, Thomas Klassen, and Rüdiger Bormann. 2000. “Hot-Forming of Silicide-Dispersion-Strengthened Titanium Aluminides (SDS-TiAl) with Grain Sizes in the Submicron Range.” In Materials science forum, vol. 343-346. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.343-346.623
• 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
• Farley, John M., and Ferris L. Seashore. 1955. Full-Scale, Free-Jet Investigation of Methods of Improving Outlet Flow Distribution in a Side-Inlet Supersonic Diffuser. NACA-RM-E54L31a. NASA. https://ntrs.nasa.gov/citations/19930088560
• Farley, J. M., and I. D. Smith. 1954. Preliminary Performance Data Obtained in a Full-Scale Free-Jet Investigation of a Side-Inlet Supersonic Diffuser. NACA-RM-SE54J22. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19710072852
• Farmer, Moses, and Perry Hanson. 1976. “Comparison of Supercritical and Conventional Wing Flutter Characteristics.” In 17th Structures, Structural Dynamics, and Materials Conference. AIAA 1976-1560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1560
• Faroughi, Shirko, Kramet Malekzadeh, and Ieraje Mirzaee. 2012. “Finite Element Supersonic Flutter Analysis of Low Aspect Ratio Stiffened Wing.” Journal of Vibration and Control 19 (14): 2187–98. https://doi.org/10.1177/1077546312455211
• Fazeli, Amir Mohammad, Adnan Cepic, and Susanne Reber. 2016. “Aircraft Weight and Center of Mass Estimation System.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2016-01-2025
• Fazelzadeh, Seyed Ahmad, Amir Hosein Ghasemi, and Abbas Mazidi. 2016. “Aeroelastic Analysis of Unrestrained Aircraft Wing with External Stores under Roll Maneuver.” International Journal of Acoustics and Vibration 21 (3). https://doi.org/10.20855/ijav.2016.21.3427
• Fazelzadeh, S. A., A. Mazidi, A. R. Rahmati, and P. Marzocca. 2009. “The Effect of Multiple Stores Arrangement on Flutter Speed of a Shear Deformable Wing Subjected to Pull-up Angular Velocity.” Aeronautical Journal 113 (1148): 661–68. https://doi.org/10.1017/s0001924000003328
• Feather, J. B. 1980. “Advanced Supersonic Transport Fixed-Base Simulator Evaluations at Landing Approach.” In NASA. Langley Res. Center Supersonic Cruise Res. 1979, Pt. 1. https://ntrs.nasa.gov/citations/19810009469
• Fedorov, A., N. Malmuth, A. Fedorov, and N. Malmuth. 1997. “Supersonic Transitional Airfoil Shapes of Minimum Drag.” In 15th Applied Aerodynamics Conference. AIAA 1997-2231. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2231
• Feifel, Winfried, and Benjamin Kerkam. 1992. “Propulsion/airframe Requirements and Optimization for a Joint Service Cruise Missile Concept.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-82. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-82
• Feig, P. D., and S. C. Gilkey. 1991. “A Propulsion Perspective of the Next Generation Supersonic Transport.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-385
• Fejer, Andrew A., George L. Heath, and Richard T. Driftmyer. 1964. An Investigation of Constant Area Supersonic Flow Diffusion. Defense Technical Information Center. https://doi.org/10.21236/ad0603313
• Fellers, W., and J. Patierno. 1970. “Fighter Requirements and Design for Superiority over Threat Aircraftat Low Cost.” In Fighter Aircraft Conference. AIAA 1970-516. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-516
• Feng, Rui, Minghe Chen, and Lansheng Xie. 2023. “Effect of Elevated Temperature and Stress State on Ductile Fracture Behaviors in Titanium Alloy: Experiments and Modeling.” Preprint, . https://doi.org/10.2139/ssrn.4519279
• Fenwick, Clare, and Christian Allen. 2007. “Flutter Analysis of the BACT Wing with Consideration of Control Surface Representation.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-3805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3805
• Fernandez, Rene, Charles J. Trefny, Scott R. Thomas, and Mel J. Bulman. 2001. Parametric Data from a Wind Tunnel Test on a Rocket-Based Combined-Cycle Engine Inlet. NASA/TM-2001-107181. NASA. https://ntrs.nasa.gov/citations/20020006304
• Ferrarese, J. 1974. “Influence of Runway Traction on Operation of Jet Transport Aircraft.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-958. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-958
• Ferrari, Carlo. 1958. “Influence of the Boundary Layer on Airfoil Pressures at Supersonic Speeds.” In Grenzschichtforschung / Boundary Layer Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-45885-9_21
• Ferri, Antonio, and Louis M. Nucci. 1946. Preliminary Investigation of a New Type of Supersonic Inlet. NACA-RM-L6J31. NASA. https://ntrs.nasa.gov/citations/19930093800
• Figge, Fred A. 1973. Advanced Metallic Structure: Air Superiority Fighter Wing Design for Improved Cost, Weight and Integrity. Volume 1. Defense Technical Information Center. https://doi.org/10.21236/ad0781810
• Fikes, D. H. 1977. Aerodynamic Characteristics and Fin Loads of a Bank-to-Turn, Air-to-Air Missile Concept at Supersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/adb019652
• Filinov, Evgeny, and Kristina Bezborodova. 2021. “Double Bypass Turbojet Engine Structure Analysis.” Vestnik Moskovskogo aviatsionnogo instituta 28 (3): 159–70. https://doi.org/10.34759/vst-2021-2-159-170
• 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
• Fink, M., and W. Anderson. 1982. “Axisymmetric Nose Inlet Effects on Supersonic Missile Airloads.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1302. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1302
• Fischel, Jack, Euclid C. Holleman, and Robert A. Tremant. 1957. Flight Investigation of the Transonic Longitudinal and Lateral Handling Qualities of the Douglas X-3 Research Airplane. NACA-RM-H57I05. NASA. https://ntrs.nasa.gov/citations/19930090141
• 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. 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
• 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
• Fisher, Lewis R. 1951. Low-Speed Static Longitudinal and Lateral Stability Characteristics of Two Low-Aspect-Ratio Wings Cambered and Twisted to Provide a Uniform Load at a Supersonic Flight Condition. NACA-RM-L51C20. NASA. https://ntrs.nasa.gov/citations/19930086565
• 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, D. F., and E. J. Saltzman. 1973. Local Skin Friction Coefficients and Boundary Layer Profiles Obtained in Flight from the XB-70-1 Airplane at Mach Numbers up to 2.5. NASA-TN-D-7220. NASA. https://ntrs.nasa.gov/citations/19730016549
• Fisher, R., and T. Vollmer. 1970. “The Technical Control of the Manufacture of Aircraft Brake Friction Linings.” Powder Metallurgy 13 (26): 309–18. https://doi.org/10.1179/pom.1970.13.26.013
• Fisher, Lewis R., and James L. Williams. 1958. Wind-Tunnel Investigation of Some Effects of Wing Sweep and Horizontal-Tail Height on the Static Stability of an Airplane Model at Transonic Speeds. NASA-MEMO-10-3-58L. NASA. https://ntrs.nasa.gov/citations/19980232008
• Fitzpatrick, Robert, Robert M. Colton, Warren C. Malatesta, and F. J. Rizzitano. 1964. Solid-State Pressure Bonding of Titanium Alloy 6AL-6V-2SN. Defense Technical Information Center. https://doi.org/10.21236/ad0625718
• Fitzsimmons, R., W. Rowe, and E. Johnson. 1978. “Advanced Supersonic Transport Engine Integration Studies for near-Term Technology Readiness Date.” In 14th Joint Propulsion Conference. AIAA 1978-1052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1052
• Flaherty, J. 1979. “An Analysis of High Angle of Attack Missile Aerodynamics at Subsonic Flow Mach Numbers.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1648
• Flansburg, Barrett. 2008. “Maneuver Loads Simulation for an Advanced Transport Aircraft.” In 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 16th AIAA/ASME/AHS Adaptive Structures Conference 10t. AIAA 2008-1906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1906
• Flat Wings in Inviscid Supersonic Flow. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch6
• Fleming, Jon, Semih Olcman, Ricardo Burdisso, and Wing Ng. 2004. “Sensing for Active Flow Control in Advanced Propulsion-Airframe Integration Systems.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1200
• Fleming, William A., and H. Dean Wilsted. 1953. “Turbojet Research Techniques Utilized in Altitude Facilities.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/530075
• Fletcher, J., and B. Burns. 1979. “Supersonic Combat Aircraft Design.” In Atlantic Aeronautical Conference. AIAA 1979-699. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-699
• Fletcher, Jay W., Josh Isom, Mark Davis, James P. Cycon, and James Rozak. 2013. “Flight Test of Technology for Virtual Monitoring of Loads.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/vfs-f69-0356
• “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
• “Flight Envelopes.” 2012. In Advanced Aircraft Flight Performance. Cambridge University Press. https://doi.org/10.1017/cbo9781139161893.011
• Flight Experience with Two High-Speed Airplanes Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. 1955. NACA-RM-H55A13. NASA. https://ntrs.nasa.gov/citations/19930088648
• Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers. 1944. NACA-TR-792. NASA. https://ntrs.nasa.gov/citations/19930091869
• “Flight Test Manual.” 1959. In Instrumentation Catalog. Elsevier. https://doi.org/10.1016/b978-1-4831-9727-2.50001-6
• Flores, Jolen, Eugene Tu, and Lyndell King. 1992. Code Validation for the Simulation of Supersonic Viscous Flow about the F-16XL. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19940029022
• 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 in the Vicinity of the Trailing Edge of a Thin Airfoil.” 1998. In Asymptotic Theory of Separated Flows. Cambridge University Press. https://doi.org/10.1017/cbo9780511983764.005
• Fluid Dynamics Research on Supersonic Aircraft. 1998. AC/323(AVT)TP/6. NASA. https://ntrs.nasa.gov/citations/19990018232
• Follé, M. I. 1983. “Wave Drag of Slender Star-Shaped Bodies at Moderate Supersonic Flight Velocities.” Fluid Dynamics 18 (5): 783–88. https://doi.org/10.1007/bf01091003
• Fomin, V. M., S. G. Mironov, and K. M. Serdyuk. 2009. “Reducing the Wave Drag of Bodies in Supersonic Flows Using Porous Materials.” Technical Physics Letters 35 (2): 117–19. https://doi.org/10.1134/s1063785009020060
• Ford, Terry. 1993. “Developments in Engine-Airframe Integration.” Aircraft Engineering and Aerospace Technology 65 (1): 6–9. https://doi.org/10.1108/eb037329
• Ford, Terry. 1998. “Rejected Takeoff and Landing.” Aircraft Engineering and Aerospace Technology 70 (6): 456–62. https://doi.org/10.1108/00022669810243449
• 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
• Forkey, Joseph, Sandrine Cogne, Alexander Smits, Seymour Bogdonoff, Walter Lempert, and Richard Miles. 1993. “Time-Sequenced and Spectrally Filtered Rayleigh Imaging of Shock Wave and Boundary Layer Structure for Inlet Characterization.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2300. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2300
• “Forming of Titanium Plate, Sheet, Strip, and Tubing.” 2015. In Titanium. ASM International. https://doi.org/10.31399/asm.tb.tpmpa.t54480243
• Fornasier, Luciano, and Stefan Heiss. 1987. “Application of HISSS Panel Code to a Fighter-Type Aircraft Configuration at Subsonic and Supersonic Speeds.” In 5th Applied Aerodynamics Conference. AIAA 1987-2619. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2619
• Forner, J. 1971. “Prediction of Flow Angularity near a Supersonic Fuselage Forebody with Arbitrary Cross-Section.” In 8th Annual Meeting and Technical Display. AIAA 1971-996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-996
• 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, J. F. 1944. “Estimation of Aircraft Ceilings.” Aircraft Engineering and Aerospace Technology 16 (7): 186–87. https://doi.org/10.1108/eb031139
• Foss, R. 1978. “From Propellers to Jets in Fighter Aircraft Design.” In Diamond jubilee of powered flight: The evolution of aircraft design; Proceedings of the Conference. AIAA 1978-3005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-3005
• Foster, G. V., and O. A. Morris. 1960. Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-Sweep Wings. NASA-TM-X-323. NASA. https://ntrs.nasa.gov/citations/19660022441
• Foster, John, Holly Ross, and Patrick Ashley. 1993. “Investigation of High-Alpha Lateral-Directional Control Power Requirements for High-Performance Aircraft.” In Flight Simulation and Technologies. AIAA 1993-3647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3647
• Fouda, Moatasem, and Haitham E. Taha. 2021. “Experimental Investigations of Airplane Maneuverability and Stability in Stall.” In AIAA Scitech 2021 Forum. AIAA 2021-1819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1819
• Fouda, Moatasem, and Haitham E. Taha. 2022. “Effect of Wing Planform on Airplane Stability and Control Authority in Stall.” In AIAA SCITECH 2022 Forum. AIAA 2022-1161. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1161
• 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
• Fradenburgh, Evan A., and Robert C. Campbell. 1953. Characteristics of a Canard-Type Missile Configuration with an Underslung Scoop Inlet at Mach Numbers from 1.5 to 2.0. NACA-RM-E52J22. NASA. https://ntrs.nasa.gov/citations/19930087538
• Fraenkel, L. E. 1958a. “A Note on the Drag of Wing-Body Combinations in Linearised Supersonic Flow.” Aeronautical Quarterly 9 (3): 305–12. https://doi.org/10.1017/s000192590001074x
• Fraenkel, L. E. 1958b. “The Wave Drag of Wing-Quasi-Cylinder Combinations at Zero Incidence.” Aeronautical Quarterly 9 (1): 55–70. https://doi.org/10.1017/s000192590000130x
• Frank, Lazzeroni A., and Frank A. Pfyl. 1956. Effect of Boundary-Layer Control and Inlet Lip Shape on the Performance of a Twin-Scoop Air-Induction System at Mach Numbers from 0 to 1.9. NACA-RM-A55L02. NASA. https://ntrs.nasa.gov/citations/19930089049
• Frank, Joseph L., and Robert A. Taylor. 1951. Comparison of Drag, Pressure Recovery, and Surface Pressure of a Scoop-Type Inlet and an NACA Submerged Inlet at Transonic Speeds. NACA-RM-A51H20a. NASA. https://ntrs.nasa.gov/citations/19930086824
• Frazer, Alson C., and Warren E. Anderson. 1953. Performance of a Normal-Shock Scoop Inlet with Boundary-Layer Control. NACA-RM-A53D29. NASA. https://ntrs.nasa.gov/citations/19930087526
• Frazier, Wayne. 1991. “Longitudinal and Directional Static Stability Effects of a Large Radome Mounted atop a 747-200 Aircraft.” In Aircraft Design and Operations Meeting. AIAA 1991-3173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3173
• Frederick, Mike, Dan Banks, Andres Garzon, and Jason Matisheck. 2014. “Flight Tests of a Supersonic Natural Laminar Flow Airfoil.” In International Symposium on Flow Visualization. https://ntrs.nasa.gov/citations/20140010358
• 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
• Fremaux, C. Michael. 1997. Spin-Tunnel Investigation of a 1/28-Scale Model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without Vertical Tails. NASA-CR-201687. NASA. https://ntrs.nasa.gov/citations/19970019598
• Fremaux, C., D. Vairo, and R. Whipple. 1993. “Effect of Geometry, Static Stability, and Mass Distribution on the Tumbling Characteristics of Generic Flying-Wing Models.” In Flight Simulation and Technologies. AIAA 1993-3615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3615
• French, Mark. 1988. “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
• Fresconi, Frank, and Ilmars Celmins. 2018. “Experimental Flight Characterization of Spin-Stabilized Projectiles at High Angle of Attack.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0769
• 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
• Frey, M., S. Jamme, R. Gojon, M. Fiore, and J. Gressier. 2025. “Large Eddy Simulation of the Control of the Inlet Buzz Phenomenon in a Supersonic Air Inlet.” In Proceedings of the 34th International Symposium on Shock Waves, Volume 1: Fundamentals. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-4767-5_2
• Friedlander, David J. 2018. “Using Numerical Simulations to Explore Top-Mounted Propulsion on a Conceptual Commercial Supersonic Transport Aircraft.” In 2018 Applied Aerodynamics Conference. AIAA 2018-4202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4202
• Friedman, P. A., and S. G. Luckey. 2011. “High-Temperature Lubricants for Superplastic Forming of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.1.72
• Friehmelt, Holger. 2002. “Lift Contribution from Delta Wing Vortices: Flight Test and Predictions.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4711. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4711
• 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, 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
• Frierson, J., and R. Van Meter. 1977. “An Electrostatic Roll Sensor for Supersonic Vehicles. I: Feasibility and Flight Tests.” In Guidance and Control Conference. AIAA 1977-1067. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1067
• Frisby, V. 1960. Design, Fabrication, and Test of High-Flotation Tires and Related Valving Mechanism for Rough Terrain Landing Gear. Defense Technical Information Center. https://doi.org/10.21236/ad0244172
• Frolov, Vladimir A. 2021. “Optimization of Lift-Curve Slope for Wing-Fuselage Combination.” In IntechOpen eBooks. IntechOpen. https://doi.org/10.5772/intechopen.89056
• Fu, Zemin. 2010. “Springback Model for Air-Bending of Sheet Metal Based on Dimensional Analysis Method.” Journal of Mechanical Engineering 46 (12): 53. https://doi.org/10.3901/jme.2010.12.053
• Fu, Ze Min. 2011. “Numerical Simulation of Springback in Air-Bending Forming of Sheet Metal.” Applied Mechanics and Materials 121-126: 3602–6. https://doi.org/10.4028/www.scientific.net/amm.121-126.3602
• Fu, M. 2023. “Fabrication and Superplastic Forming Property Research of TiB Whisker Reinforced Titanium Alloy Matrix Composite Sheet.” In Materials Research Proceedings, vol. 32. Materials Research Forum LLC. https://doi.org/10.21741/9781644902615-6
• Fu, Xuesong, Kang Li, Wei Sun, Chengfang Liu, Guoqing Chen, and Wenlong Zhou. 2016. “Springback Simulation in Air Bending of Titanium Alloy Sheet Using Solid Shell Element.” In Proceedings of the 2015 4th International Conference on Sensors, Measurement and Intelligent Materials. Atlantis Press. https://doi.org/10.2991/icsmim-15.2016.111
• Fu, Jan-Kaung, and Shen-Min Liang. 1993. “Computations of Aerodynamic Drag for Turbulent Transonic Projectileswith and without Spin.” In 11th Applied Aerodynamics Conference. AIAA 1993-3416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3416
• Fu, Ze Min, and Guang Ming Liu. 2011. “Prediction for Air-Bending Springback Radius of Sheet Metal Using Back Propagation Neural Network and Micro Genetic Algorithm.” Advanced materials research 219-220: 1174–77. https://doi.org/10.4028/www.scientific.net/amr.219-220.1174
• Fu, Kunning, Heli Peng, Kailun Zheng, and Shijian Yuan. 2022. “Phenomenological Model of Hardening and Flow for Ti-6Al-4V Titanium Alloy Sheets under Hot Forming Conditions.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-1801729/v1
• Fu, Yu, Wenyan Song, Qiuyin Wang, Xiaoting Wang, and Jianping Li. 2024. “Flight Trajectory Optimization Study of a Variable-Cycle Turbine-Based Combined Cycle Engine Hypersonic Vehicle Based on Airframe/engine Integration.” International Journal of Turbo & Jet-Engines 42 (2): 409–21. https://doi.org/10.1515/tjj-2024-0085
• Fu, Yong Ling, Peng Zhang, Sheng Jun Li, and Zhu Feng Li. 2013. “Drop Dynamic Simulation for Landing Gear via SimMechanics.” Advanced materials research 694-697: 77–83. https://doi.org/10.4028/www.scientific.net/amr.694-697.77
• Fuchiwaki, Masaki, and Kazuhiro Tanaka. 2005. “Vortex Structure and Scale on an Unsteady Air foil(Wing and Airfoil).” Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (0): 591–96. https://doi.org/10.1299/jsmeicjwsf.2005.591
• Fujimoto, Akira, and Nobuo Niwa. 1993. “Experimental and Numerical Investigation of Mach 2.5 Supersonic Mixed Compression Inlet.” In 31st Aerospace Sciences Meeting. AIAA 1993-289. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-289
• Fujimoto, Akira, Nobuo Niwa, and Keisuke Sawada. 1991. “Numerical Investigation of Supersonic Inlet with Realistic Bleed Andbypass Systems.” In 29th Aerospace Sciences Meeting. AIAA 1991-127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-127
• 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
• Fukuoka, Toshimichi, Masataka Nomura, and Takao Hirai. 2014. “Experimental Verification of Finite Element Approach for Designing Robust Bolted Joints Using Titanium and Titanium Alloy Bolts at Elevated Temperature.” In Volume 2: Computer Technology and Bolted Joints. American Society of Mechanical Engineers. https://doi.org/10.1115/pvp2014-28242
• “Functional-Purpose Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-8
• “Fundamentals of Fighter Design.” 2001. Aircraft Engineering and Aerospace Technology 73 (1). https://doi.org/10.1108/aeat.2001.12773aae.001
• Fuqun, Chen, Li Wenlan, Wang Zongyuan, and Cong Mengzi. 1985. “An Experimental Investigation of Response of a Turbojet Engine to Inlet Distortion.” In Volume 1: Aircraft Engine; Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/85-igt-12
• Furey, Roger J. 1980. High-Lift Capability of Low Aspect Ratio Wings Utilizing Circulation Control and Upper Surface Blowing. Defense Technical Information Center. https://doi.org/10.21236/ada112312
• Furuya, H., and I. Fukuchi. 2001. “Evolutionary Structural Optimization of Plate Wing for Supersonic Flutter.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1631
• Furuya, Hiroshi, and Isao Fukuchi. 2002. “Simultaneous Optimization of Plate Wing on Supersonic Flutter Characteristics and Structural Mass.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1482
• Furuya, Hiroshi, Isao Fukuchi, Nozomu Kogiso, and Saburo Matunaga. 2003. “Optimum Design of Plate Wing with Magnesium Alloys on Supersonic Flutter Characteristics and Structural Mass.” In Materials science forum, vol. 419-422. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.419-422.207
• “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
• Gaglio, Emanuela, and Riccardo Bevilacqua. 2026. “AI-Driven Framework for High-Speed Shock Wave Boundary Layer Interaction Analysis and Prediction.” In ASCEND 2026. AIAA 2026-3119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-3119
• Gaglio, Emanuela, Anselmo Cecere, Stefano Mungiguerra, Raffaele Savino, Michele Visone, and Marco Lanzetta. 2021. “Aerodynamic Study of Airframe-Engine Integration of a Supersonic Business Jet.” In ASCEND 2021. AIAA 2021-4200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-4200
• Gale, Lawrence J. 1948. Effect of Landing Flaps and Landing Gear on the Spin and Recovery Characteristics of Airplanes. NACA-TN-1643. NASA. https://ntrs.nasa.gov/citations/19930082260
• Gallagher, Edward J., and Vincent R. Capece. 2004. “Numerical Simulation of Oscillating Airfoil Unsteady Aerodynamics in Supersonic Flow.” International Journal of Turbo and Jet Engines 21 (2). https://doi.org/10.1515/tjj.2004.21.2.87
• Gallagher, James J., and James N. Mueller. 1955. An Investigation of the Maximum Lift of Wings at Supersonic Speeds. NACA-TR-1227. NASA. https://ntrs.nasa.gov/citations/19930092236
• Galloway, Thomas, Paul Gelhausen, Mark Moore, and Mark Waters. 1992. “Oblique Wing Supersonic Transport Concepts.” In Guidance, Navigation and Control Conference. AIAA 1992-4230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4230
• Galway, R. D. 1980. A Comparison of Methods for Calibration and Use of Multi-Component Strain Gauge Wind Tunnel Balances (Comparaison De Methodes d’Etalonnage Et d’Utilisation Des Balances Extensometriques De Soufflerie a Plusieurs Composantes),. Defense Technical Information Center. https://doi.org/10.21236/ada090484
• Gamon, M. 1979. “Airplane Dynamic Wheel Loads during Ground Maneuveringcomputer Program for L-1011 Aircraft.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-739
• Gandhi, Neha, Nathan Richards, and Alec Bateman. 2012. “Desktop Simulator Demonstration of a Joint Human/Automated Upset Recovery System.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4820
• Ganti, Himakar, Luis Bravo, Anindya Ghoshal, and Prashant Khare. 2026. “Mutual Interactions between a Thin Flexible Panel and Supersonic Flows.” Physics of Fluids 38 (6): 066121. https://doi.org/10.1063/5.0301373
• Gapcynski, J. P. 1960. The Aerodynamic Characteristics of a Body in the Flow Field near the Tip of a Circular-Arc Wing of Rectangular Plan Form at a Mach Number of 2.01. NASA-TM-X-211. NASA. https://ntrs.nasa.gov/citations/19630003039
• Gapcynski, John P., and Emma Jean Landrum. 1958. Tabulated Data from a Pressure-Distribution Investigation at Mach Number 2.01 of a 45 Deg Sweptback-Wing Airplane Model at Combined Angles of Attack and Sideslip. NASA-MEMO-10-15-58L. NASA. https://ntrs.nasa.gov/citations/19630002621
• Garcia, Joseph, and Guru Guruswamy. 1999. “Static Aeroelastic Characteristics of an Advanced Wing with a Control Surface Using Navier-Stokes Equations.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-796
• García-Barrachina, L., and A. J. Gámez. 2021. “Superplastic Forming Analysis Techniques.” In Advanced Welding and Deforming. Elsevier. https://doi.org/10.1016/b978-0-12-822049-8.00018-9
• Garcia-Fogeda, Pablo, and D. Liu. 1988. “Unsteady Supersonic Flow Calculations for Wing-Body Combinations Using Harmonic Gradient Method.” In 26th Aerospace Sciences Meeting. AIAA 1988-568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-568
• 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
• Garcon, Francois, Jean-Claude Raffin, Joelle Fontaine, and S. Wolf. 2003. “New Roll Damping, Pitch Damping and Magnus Measurement Rigs at ONERA.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-454
• Gardner, J. E., R. A. Pride, D. M. Royster, and B. A. Stein. 1968. Effects of Longtime Environmental Exposure on Mechanical Properties of Sheet Materials for a Supersonic Transport. NASA-TN-D-4318. NASA. https://ntrs.nasa.gov/citations/19680008428
• Gardner, J. E., and D. M. Royster. 1970. Influence of Salt and Elevated-Temperature Exposure on the Maximum Compressive Strength of Titanium-Alloy Skin-Stringer Panels. NASA-TN-D-5670. NASA. https://ntrs.nasa.gov/citations/19700009635
• 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
• Garrett, J. H. 1956. “Status of Titanium Fabrication and Use.” JOM 8 (1): 30–35. https://doi.org/10.1007/bf03377639
• Garrick, I. E., and S. I. Rubinow. 1947. Theoretical Study of Air Forces on an Oscillating or Steady Thin Wing in a Supersonic Main Stream. NACA-TR-872. NASA. https://ntrs.nasa.gov/citations/19930090944
• Garriz, Javier, Parry Newman, Veer Vatsa, Kara Haigler, and Kenneth Burdges. 1990. “Evaluation of Transonic Wall Interference Assessment and Correction for Semi-Span Wing Data.” In 16th Aerodynamic Ground Testing Conference. AIAA 1990-1433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1433
• Garvin, John B. 1947. Flight Measurements of Aerodynamic Loads on the Horizontal Tail Surface of a Fighter-Type Airplane. NACA-TN-1483. NASA. https://ntrs.nasa.gov/citations/19930082141
• 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
• Gau, Jenn-Terng, and Gary L. Kinzel. 2005. “A New Model for Springback Prediction for Aluminum Sheet Forming.” Journal of Engineering Materials and Technology 127 (3): 279–88. https://doi.org/10.1115/1.1924563
• Gau, Jenn-Terng, Chris Principe, and Fengchen Yang. 2006. “An Experimental Study of the Influence of Size Effect on Springback of Micro Sheet Forming.” In Manufacturing Science and Engineering, Parts A and B. ASMEDC. https://doi.org/10.1115/msec2006-21037
• Gawron, Valerie J., and Patricia M. Jones. 2002. Airplane Upset Training Evaluation Report. NASA/CR-2002-211405. NASA. https://ntrs.nasa.gov/citations/20020068969
• Gayman, W. H. 1946. “Rotational Drop-Testing of Airplane Main Landing Gear.” Journal of Fluids Engineering 68 (7): 773–79. https://doi.org/10.1115/1.4018606
• Gebert, Glenn, Joy Kelly, Juan Lopez, and Johnny Evers. 2000. “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
• Gedeon, Christopher, and Timothy T. Takahashi. 2014. “Multi-Disciplinary Survey of Engine Parameters and Its Impact on Performance and Energy Maneuverability.” In 14th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2014-2032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2032
• Gee, Ken, Russell Cummings, and Lewis Schiff. 1990. “The Effect of Turbulence Models on the Numerical Prediction of the Flowfield about a Prolate Spheroid at High Angle of Attack.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3106. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3106
• Gelder, Thomas F. 1957. Total-Pressure Distortion and Recovery of Supersonic Nose Inlet with Conical Centerbody in Subsonic Icing Conditions. NACA-RM-E57G09. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/19930093764
• Gennaretti, Massimo. 2024. “The Panel Method for Wing Aeroelasticity.” In Fundamentals of Aeroelasticity. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-53379-2_4
• 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, Joseph, and John Bosworth. 1987. “Dynamic Stability and Handling Qualities Tests on a Highly Augmented, Statically Unstable Airplane.” In Guidance, Navigation and Control Conference. AIAA 1987-2258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2258
• 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
• 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
• Gershon, B., and I. Eldror. 2005. “Research and Application of Superplastic Forming Titanium Alloys for Commercial Aircraft Parts.” In Materials science forum. Trans Tech Publications. https://doi.org/10.4028/0-87849-960-1.3047
• Ghalandari, Mohammad, Ibrahim Mahariq, Farhad Ghadak, Oussama Accouche, and Fahd Jarad. 2022. “Aeroelastic Optimization of the High Aspect Ratio Wing with Aileron.” Computers, Materials & Continua 70 (3): 5569–81. https://doi.org/10.32604/cmc.2022.020884
• Ghee, Terence A., and Nigel J. Taylor. 2000. Low-Speed Wind Tunnel Tests on a Diamond Wing High Lift Configuration. Defense Technical Information Center. https://doi.org/10.21236/ada377908
• Ghoreyshi, Mehdi, Pooneh Aref, Mario Stradtner, et al. 2024. “Evaluation of Reduced Order Aerodynamic Models for Transonic Flow over a Multiple-Swept Wing Configuration.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4158
• Ghosh, A. K., and C. H. Hamilton. 1986. “Superplastic Forming and Diffusion Bonding of Titanium Alloys.” Defence Science Journal 36 (2): 153–77. https://doi.org/10.14429/dsj.36.5969
• 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
• Gibson, W. 1932. “Fabrication of the Airframe: Detail Practice in Plate and Press Work.” Aircraft Engineering and Aerospace Technology 4 (12): 319–20. https://doi.org/10.1108/eb029636
• Gibson, Philip T., Graham H. Alexander, and Hobart A. Cress. 1968. Validation of Design Theory for Aircraft Arresting-Gear Cable. Defense Technical Information Center. https://doi.org/10.21236/ad0665328
• 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
• 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
• Gillard, William. 1999. “AFRL F-22 Dynamic Wind Tunnel Test Results.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4015. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4015
• Gillen, Tyler, and Eric Loth. 2011. “Vortex Generators for an Axisymmetric Dual-Stream Supersonic Inlet.” In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2011-5567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-5567
• Gillespie, Warren, Jr. 1957. Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20. NACA-RM-L57A25. NASA. https://ntrs.nasa.gov/citations/19930089506
• Gillespie, Warren, Jr. 1960. Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20. NASA-TN-D-509. NASA. https://ntrs.nasa.gov/citations/20040046997
• Gillig, Frank J., and Glen J. Guarnieri. 1956. A Study of the Tensile and Creep-Rupture Properties of Fifteen Heats of C-110M Titanium Alloy Sheet. Defense Technical Information Center. https://doi.org/10.21236/ad0091903
• 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. 1956. Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3. NACA-RM-L56E17. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019449
• Gillis, Clarence L., and Thomas A. Toll. 1962. “Section b. Stability and Control of High Speed Aircraft.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-004
• 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., D. Berry, and D. Belte. 1972. “Analysis of a Lateral-Directional Airframe/propulsion System Interaction of a Mach 3 Cruise Aircraft.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-961
• Gilyard, Glenn, and John Orme. 1992. “Subsonic Flight Test Evaluation of a Performance Seeking Control Algorithm on an F-15 Airplane.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3743. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3743
• Giragosian, P. 1982. “Aerodynamic Consideration in the Design of a Vertically Launched Advanced Interdiction Missile /VLAIM/.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1340
• Giraudet, Arnaud, Franck Tancret, and Frédéric Christien. 2016. Characterization of the Influence of a Fast Preforming on Superplastic Forming. Wiley. https://doi.org/10.1002/9781119296126.ch231
• Girton, L. D., H. C. Turner, and W. M. Sutherland. 1956. Material: Brazing Alloys: Titanium Alloy Joining Wetability and Erosion Characteristics. Defense Technical Information Center. https://doi.org/10.21236/ad0407737
• Gite, Lk, and R. S. Deodhar. 2020. “Estimation of Roll Damping Coefficient from Roll and Trajectory Data Using Extended Kalman Filter.” Preprint, . https://doi.org/10.21203/rs.3.rs-40593/v1
• Glasgow, E. 1973. “Integrated Airframe-Nozzle Performance for Designing Twin-Engine Fighters.” In 9th Propulsion Conference. AIAA 1973-1303. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1303
• 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
• Goddard, Frank E. 1962. “Section g. Supersonic Tunnels.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-009
• 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
• Goelzer, H. Fred, and Edgar M. Cortright Jr. 1951. Investigation at Mach Number 1.88 of Half of a Conical-Spike Diffuser Mounted as a Side Inlet with Boundary-Layer Control / H. Fred Goelzer and Edgar M. Cortright, Jr. NACA-RM-E51G06. NASA. https://ntrs.nasa.gov/citations/19930086786
• Goetz, G., J. Young, and J. Palcza. 1976. “A Two-Dimensional Airframe Integrated Nozzle Design with Inflight Thrust Vectoring and Reversing Capabilities for Advanced Fighter Aircraft.” In 12th Propulsion Conference. AIAA 1976-626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-626
• Gogish, L. V., and S. G. Dashevskaya. 1990. “Supersonic Nonuniform Flow over a Trapezoidal Profile.” Fluid Dynamics 25 (3): 486–88. https://doi.org/10.1007/bf01049836
• Goland, Martin. 1945. “The Flutter of a Uniform Cantilever Wing.” Journal of Applied Mechanics 12 (4): A197-A208. https://doi.org/10.1115/1.4009489
• Goldbaum, G. C. 1956. Research Work on Supersonic Wind Tunnels to Investigate the Use of Perforated Walls. Defense Technical Information Center. https://doi.org/10.21236/ad0092263
• Goldberg, Theodore J., and Emanuel Boxer. 1959. Investigation on the Use of a Freely Rotating Rotor at the Cowl Face of a Supersonic Conical Inlet to Reduce Inlet Flow Distortion. NASA-MEMO-5-28-59L. NASA. https://ntrs.nasa.gov/citations/19980230685
• Goldsmith, H. A. 1964. “Stability and Control of Supersonic Aircraft at Low Speeds.” In International Council of the Aeronautical Sciences. AIAA 1964-588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-588
• Goldsworthy, F. A. 1952. “Supersonic Flow over Thin Symmetrical Wings with Given Surface Pressure Distribution.” Aeronautical Quarterly 3 (4): 263–79. https://doi.org/10.1017/s000192590000069x
• 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
• Golovkin, Mikhail Alekseyevich. 2013. “Calculation of Rotational Derivatives of Roll and Yaw Moments for High-Aspect-Ratio Wings.” TsAGI Science Journal 44 (4): 491–506. https://doi.org/10.1615/tsagiscij.2013010487
• Golubkin, V. N., G. N. Dudin, and R. Ya. Tugazakov. 2002. “Supersonic Flow past a Bent Delta Wing and Its Aerodynamic Characteristics.” Fluid Dynamics 37 (1): 147–56. https://doi.org/10.1023/a:1015151304222
• Goman, M., A. Khramtsovsky, M. Goman, and A. Khramtsovsky. 1997. “Global Stability Analysis of Nonlinear Aircraft Dynamics.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3721
• Gong, Zhihui, Mandeep Singh, Bohao Fang, and Dongbin Wei. 2021. “An Enhanced Hybrid Springback Compensation Approach: Springback Path – Displacement Adjustment Method for Complex Shaped Products of Sheet Metal Forming.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-980113/v1
• Gonzalez, Hugo, and Allen Winkelmann. 1993. “An Experimental Study of Droop Leading Edge Modifications on High and Low Aspect Ratio Wings up to 50 Deg Angle of Attack.” In 11th Applied Aerodynamics Conference. AIAA 1993-3496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3496
• 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
• 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
• Gopalarathnam, Ashok, Michael Selig, Frank Hsu, Ashok Gopalarathnam, Michael Selig, and Frank Hsu. 1997. “Design of High-Lift Airfoils for Low Aspect Ratio Wings with Endplates.” In 15th Applied Aerodynamics Conference. AIAA 1997-2232. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2232
• Gordnier, Raymond. 1993. “Computation of Delta-Wing Roll Maneuvers.” In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. AIAA 1993-2975. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2975
• Gordnier, Raymond, and Miguel Visbal. 1993. “Numerical Simulation of Delta-Wing Roll.” In 31st Aerospace Sciences Meeting. AIAA 1993-554. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-554
• Gordon, James, Steven Liu, and M. Ozbek. 1996. “A Nonlinear Model for Aircraft Brake Squeal Analysis. II: Stability Analysis and Parametric Studies.” In Dynamics Specialists Conference. AIAA 1996-1252. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1252
• Goshima, Kentaro, Yuka Yamauchi, and Kisa Matsushima. 2019. “Three Dimensional Analysis for Shock Wave Phenomena in Supersonic Flows about a Wing.” Proceedings of Conference of Hokuriku-Shinetsu Branch 2019.56 (0): G022. https://doi.org/10.1299/jsmehs.2019.56.g022
• 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
• Goud, K. Ajay Kumar, and Y. D. Dwivedi. 2022. “Effect of Twin Vertical Stabilizers on Lateral Directional Static Stability of an Aircraft – a Computational Study.” Graduate Research in Engineering and Technology: 89–95. https://doi.org/10.47893/gret.2022.1057
• Gould, J. E., and T. V. Stotler. 1991. “Application of Flash Welding to a Titanium Aluminide Alloy-Microstructural Evaluations.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-231
• 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
• 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. B., J. R. Chambers, and P. L. Coe Jr. 1974. Wind-Tunnel Free-Flight Investigation of a Model of a Spin-Resistant Fighter Configuration. NASA-TN-D-7716. NASA. https://ntrs.nasa.gov/citations/19740018330
• 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, E. W., B. J. Beane, and R. M. Licher. 1955. “The Drag of Non-Planar Thickness Distributions in Supersonic Flow.” Aeronautical Quarterly 6 (2): 99–113. https://doi.org/10.1017/s0001925900009896
• Graham, E. W., P. A. Lagerstrom, B. J. Beane, and R. M. Licher. 1954. Reduction of Drag Due to Lift at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0063453
• Grana, David C., and Robert E. Shanks. 1952. Free-Flight-Tunnel Investigation of the Dynamic Stability and Control Characteristics of a Chance Vought F7U-3 Airplane in Towed Flight. NACA-RM-SL53D07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029465
• 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
• Grasso, F., and D. Falconi. 1993. “On High Speed Turbulence Modeling of Shock-Wave Boundary-Layer Interaction.” In 31st Aerospace Sciences Meeting. AIAA 1993-778. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-778
• Gratton, Guy. 2014. “Lateral and Directional Stability and Control.” In Initial Airworthiness. Springer International Publishing. https://doi.org/10.1007/978-3-319-11409-5_13
• Gratton, Guy. 2018. “Lateral and Directional Stability and Control.” In Initial Airworthiness. Springer International Publishing. https://doi.org/10.1007/978-3-319-75617-2_13
• Gratzer, L., and T. Odonnell. 1964. “The Development of a Blc High-Lift System for High-Speed Airplanes.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-589
• Grauer, Jared A. 2016. “Parameter Uncertainty for Aircraft Aerodynamic Modeling Using Recursive Least Squares.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-2009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2009
• 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, and Eugene Morelli. 2013. “Dynamic Modeling Accuracy Dependence on Errors in Sensor Measurements, Mass Properties, and Aircraft Geometry.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-949
• Grauer, Jared A., Eugene A. Morelli, and Daniel G. Murri. 2017. “Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0935. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0935
• Gravelle, Joseph. n.d. “A Computer Aided Turbojet Engine Trimming System.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1977-13015
• Graves, E. B. 1971. Supersonic Aerodynamic Characteristics of a Rocket-Vehicle Model with Low-Aspect-Ratio Wing and Tail Surfaces. NASA-TM-X-2159. NASA. https://ntrs.nasa.gov/citations/19710010706
• Graves, E. B. 1972. Supersonic Aerodynamic Characteristics of a Low-Aspect-Ratio Missile Model with Wing and Tail Controls and with Tails in Line and Interdigitated. NASA-TM-X-2531. NASA. https://ntrs.nasa.gov/citations/19720013321
• Gray, H. R. 1969. Hot Salt Stress Corrosion of a Titanium Alloy: Generation of Hydrogen and Its Embrittling Effect. NASA. https://ntrs.nasa.gov/citations/19690061445
• 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
• Green, Ralph E. 1958. “Calibrated Torsion Pendulum for Moment of Inertia Measurements.” American Journal of Physics 26 (7): 498–99. https://doi.org/10.1119/1.1934653
• Greenberg, Harry, and Leonard Sternfield. 1943. A Theoretical Investigation of the Lateral Oscillations of an Airplane with Free Rudder with Special Reference to the Effect of Friction. NACA-TR-762. NASA. https://ntrs.nasa.gov/citations/19930091841
• Greenberg, Harry, and Leonard Sternfield. 1944. A Theoretical Investigation of Longitudinal Stability of Airplanes with Free Controls Including Effect of Friction in Control System. AD-A301267. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19960024284
• Greene, J. E. 1957. Static Stability and Magnus Characteristics of the U.s. Navy 1,000 Pound Low-Drag Bomb at Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0132012
• Greene, W. H., and J. Sobieszczanski-Sobieski. 1980. “Minimum Mass Sizing of a Large Low-Aspect Ratio Airframe for Flutter-Free Performance.” In AIAA. https://ntrs.nasa.gov/citations/19800015192
• Greene, W. H., and J. Sobieszczanski-Sobieski. 1982. Minimum Mass Sizing of a Large Low-Aspect Ratio Airframe for Flutter-Free Performance. AIAA PAPER 80-0724. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19820040487
• Greenland, Bradley James. 2021. “Resolution of Indeterminate Landing Gear Structure Design.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14657595
• 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
• Grenson, Pierre, and Samir Beneddine. 2018. “Analysis of Shock Oscillations of an External Compression Supersonic Inlet through Unsteady Numerical Simulations.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3011. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3011
• Gresham, Nick, Zhijin Wang, and Ismet Gursul. 2009a. “Aerodynamics of Free-to-Roll Low Aspect Ratio Wings.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-543. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-543
• 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. E., E. C. Haerter, and B. R. Smith. 1983. Wake Characteristics and Interactions of the Canard/Wing Lifting Surface Configuration of the X-29 Forward-Swept Wing Flight Demonstrator. Defense Technical Information Center. https://doi.org/10.21236/ada133188
• Grigsby, Carl E. 1952. Tests at Mach Number 1.62 of a Series of Missile Configurations Having Tandem Cruciform Lifting Surfaces. NACA-RM-L51J15. NASA. https://ntrs.nasa.gov/citations/19930087120
• Grimm, Tyler J., John T. Roth, and Ihab Ragai. 2016. “Electrically Assisted Global Springback Elimination in AMS-T-9046 Titanium after Single Point Incremental Forming.” In Volume 1: Processing. American Society of Mechanical Engineers. https://doi.org/10.1115/msec2016-8811
• Groesbeck, Donald E., and Daniel J. Peters. 1958. Altitude Performance of the Afterburner on the Iroquois Turbojet Engine. Coord. No. AF-P-6. NACA-RM-SE58G01. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090026526
• Groneck, Daniel, and Dave Harmon. 2001. “Design Development of Unitized Titanium Structure.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/2001-gt-0450
• Grosser, W. 1965. “A Transonic Speed Wind Tunnel Investigation of the Rolling Effectiveness of a Large Swept Wing Transport Aircraft with Conventional Type Ailerons and Various Spoiler Configurations.” In Aircraft Design and Technology Meeting. AIAA 1965-789. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-789
• Grossman, Daniel T. 1980. “F-15 Nose Landing Gear Shimmy, Taxi Test and Correlative Analyses.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/801239
• Ground Manoeuvre Loads. 2014. Wiley. https://doi.org/10.1002/9781118700440.ch24
• Group, Applied Vehicle Technology Panel Task. 2000. Verification and Validation Data for Computational Unsteady Aerodynamics. ISBN: 92-837-1048-7. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/20010009839
• Grund, E., and M. Konarski. 1971. “Predicting Airframe/exhaust Nozzle Interactions at Transonic Mach Numbers.” In 7th Propulsion Joint Specialist Conference. AIAA 1971-720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-720
• Gu, Bin, Ji He, Shuhui Li, Yuan Chen, and Yongfeng Li. 2017a. “Cyclic Sheet Metal Test Comparison and Parameter Calibration for Springback Prediction of Dual-Phase Steel Sheets.” Journal of Manufacturing Science and Engineering 139 (9): 091010. https://doi.org/10.1115/1.4037040
• Gu, Xiangyu, Prajwal S. Prakasha, and Pier Davide Ciampa. 2017b. “Engine Airframe Integration and Optimization for Civil Aircraft Using Response Surface Approach.” In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2017-4438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4438
• Guan, Xiang Yi. 2012. “Verification of FLUENT in the Computation of Supersonic Inlet.” Advanced materials research 591-593: 2064–67. https://doi.org/10.4028/www.scientific.net/amr.591-593.2064
• Guan, Xiaohui. 2013. “Supersonic Bi-Directional Flying Wing Wave Drag Optimization Based on Alternative Form of CST Method.” Applied Mechanics and Materials 477-478: 240–45. https://doi.org/10.4028/www.scientific.net/amm.477-478.240
• 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
• Guan, Yongliang, Zhipeng Xue, Ming Li, and Hongguang Jia. 2017. “A Numerical-Experimental Method for Drop Impact Analysis of Composite Landing Gear.” Shock and Vibration 2017: 1–11. https://doi.org/10.1155/2017/3073524
• Guan, Y., and S. Yarng. 1984. “A Linear Multivariable Dynamical Model of Supersonic Inlet-Engine Combination.” In 20th Joint Propulsion Conference. AIAA 1984-1496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1496
• Guan, Yan-Shen, and Shin Yarng. 1987. “Large Amplitude Supersonic Inlet Dynamics.” In 23rd Joint Propulsion Conference. AIAA 1987-2053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2053
• Guderley, Karl G. 1986. A Semi-Analytical Approach to the Integral Equation (in Terms of the Acceleration Potential) for the Linearized Subsonic, Oscillatory Flow over an Airfoil. Defense Technical Information Center. https://doi.org/10.21236/ada167313
• Guderley, Karl G. 1987. An Integral Equation for the Linearized Unsteady Supersonic Flow over a Wing. Defense Technical Information Center. https://doi.org/10.21236/ada193773
• Guderley, Karl G. 1988. An Integral Equation for the Linearized Supersonic Flow over a Wing. Defense Technical Information Center. https://doi.org/10.21236/ada191408
• Guess, M. K., R. S. Kaneko, and G. G. Wald. 1981. “Advanced Materials and Fabrication Processes for Supersonic Cruise Aircraft.” In NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2. https://ntrs.nasa.gov/citations/19810009488
• Guida, M. 2023. “Landing Gear Shock Absorbers Guidelines.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-19
• Guimarães, Thiago A., Carlos E. S. Cesnik, and Ilya Kolmanovsky. 2021. “Low Speed Aerodynamic Modeling for Control-Related Considerations in Supersonic Aircraft Design.” In AIAA Aviation 2021 Forum. AIAA 2021-2531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2531
• Güllü, Emrah, and Gökhan Aran. 2023. “A Surge/Stall-Capable Dynamic Performance Simulation Methodology for a Turbojet Engine.” In Volume 1: Aircraft Engine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2023-100874
• Gunn, J. C. 1947a. “Linearized Supersonic Aerofoil Theory Part I.” Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences 240 (820): 327–55. https://doi.org/10.1098/rsta.1947.0005
• Gunn, J. C. 1947b. “Linearized Supersonic Aerofoil Theory Part II.” Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences 240 (820): 356–73. https://doi.org/10.1098/rsta.1947.0006
• Guo, Yuqin. 2005. “Springback Prediction in Sheet Metal Forming Process Based on the Hybrid SA.” In AIP Conference Proceedings, vol. 778. AIP. https://doi.org/10.1063/1.2011233
• Guo, Shijun, Wenyuan Cheng, and Degang Cui. 2005a. “Optimization of Composite Wing Structures for Maximum Flutter Speed.” In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2005-2132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-2132
• Guo, Xinyun, and Chuh Mei. 2002. “Using Aeroelastic Modes for Nonlinear Panel Flutter at Arbitrary Supersonic Yawed Angle.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1486. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1486
• Guo, Xinyun, Adam Przekop, and Chuh Mei. 2005b. “Supersonic Panel Flutter Analysis and Suppression Using Aeroelastic Modes and Shape Memory Alloys.” In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2005-2372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-2372
• Guohui Chen, Jinsong Liu, Qianggang, Xiaojun Ma, Zhangjiao, and Kexun Luo. 2018. “Analysis & Simulation Modeling for Brake Control System of Civil Aircraft.” In CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2018.0233
• Gupta, Pankaj. 2026. “Critical Flutter Speed Determination of a Flat-Plate Aluminum Wing Using Coupled Field Simulation Capabilities of ANSYS.” In Materials Research Proceedings, vol. 71. Materials Research Forum LLC. https://doi.org/10.21741/97816449042312-19
• Gupta, Vivudh, Balbir Singh, and R. K. Mishra. 2020. “Machining of Titanium and Titanium Alloys by Electric Discharge Machining Process: A Review.” International Journal of Machining and Machinability of Materials 22 (2): 99. https://doi.org/10.1504/ijmmm.2020.105661
• Gur’ev, Yu. V., I. V. Tkachenko, and E. I. Yakushenko. 2011. “Effect of Fluid Boundaries on Flow around a Low-Aspect Ratio Wing.” Fluid Dynamics 46 (6): 901–10. https://doi.org/10.1134/s001546281106007x
• Guruswamy, P., and P. M. Goorjian. 1982. Comparison between Computations and Experimental Data in Unsteady Three-Dimensional Transonic Aerodynamics, Including Aeroelastic Applications. AIAA PAPER 82-0690. Informatics, Inc. https://ntrs.nasa.gov/citations/19820046622
• Guruswamy, G., and P. Goorjian. 1984. “An Efficient Coordinate Transformation Technique for Unsteady, Transonic Aerodynamic Analysis of Low Aspect-Ratio Wings.” In 25th Structures, Structural Dynamics and Materials Conference. AIAA 1984-872. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-872
• Guy, Lawrence D., and William M. Hadaway. 1955. Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers from 0.70 to 1.96, Including an Evaluation of Techniques Used. NACA-RM-L55H12. NASA. https://ntrs.nasa.gov/citations/19930093831
• Gwin, L. 1974. “Optimal Aeroelastic Design of an Oblique Wing Structure.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-349
• Haas, Anthony P., Christoph Hader, and Hermann F. Fasel. 2021. “Linear Stability Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil.” In AIAA Aviation 2021 Forum. AIAA 2021-2848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2848
• Haas, Anthony P., Christoph Hader, and Hermann F. Fasel. 2022. “Numerical Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil.” In AIAA SCITECH 2022 Forum. AIAA 2022-1074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1074
• Haas, M., and A. Karanian. 1980. “Small-Scale Supersonic Inlet Test Facility.” In 16th Joint Propulsion Conference. AIAA 1980-1145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1145
• Häberle, Jürgen, and Ali Gülhan. 2007. “Investigation of the Flow Field of a 2D SCRAM Jet Inlet at Mach 7 with Optional Boundary Layer Bleed.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5068
• Hacker, T., and C. Oprişiu. 1974. “A Discussion of the Roll-Coupling Problem.” Progress in Aerospace Sciences 15: 151–80. https://doi.org/10.1016/0376-0421(74)90005-0
• Haderlie, Jacob, and William Crossley. 2010. “Multiobjective Optimization of a Supersonic-Inlet Bypass-Duct Splitter via Surrogate Modeling.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9170
• Haefeli, Rudolph C., Harold Mirels, and John L. Cummings. 1950. Charts for Estimating Downwash behind Rectangular, Trapezoidal, and Triangular Wings at Supersonic Speeds. NACA-TN-2141. NASA. https://ntrs.nasa.gov/citations/19930082761
• Hahn, Andrew. 2012. “Application of Cart3D to Complex Propulsion-Airframe Integration with Vehicle Sketch Pad.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-547
• Hahne, David E. 1999. 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop: Configuration Aerodynamics: Volume 1. NASA/CP-1999-209704/VOL1/PT1. NASA. https://ntrs.nasa.gov/citations/20000014369
• Hajela, P., and R. Glowasky. 1991. “Application of Piezoelectric Elements in Supersonic Panel Flutter Suppression.” In Aircraft Design and Operations Meeting. AIAA 1991-3191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3191
• Hale, Alan, Milt Davis, and Jim Sirbaugh. 2004. “A Numerical Simulation Capability for Analysis of Aircraft Inlet – Engine Compatibility.” In Volume 2: Turbo Expo 2004. ASMEDC. https://doi.org/10.1115/gt2004-53473
• Hale, Lawrence E., Mayuresh Patil, and Christopher J. Roy. 2015. “Nondeterministic Simulation for Probability of Loss of Control Prediction for Unmanned Aircraft Systems.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-2329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2329
• Halilovič, Miroslav, Marko Vrh, and Boris Štok. 2007. “Impact of Elastic Modulus Degradation on Springback in Sheet Metal Forming.” In AIP Conference Proceedings, vol. 908. AIP. https://doi.org/10.1063/1.2740929
• Hall, Charles F., and John C. Heitmeyer. 1951. Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Twisted and Cambered Triangular Wing of Aspect Ratio 2 with NACA 0003-63 Thickness Distribution. NACA-RM-A51E01. NASA. https://ntrs.nasa.gov/citations/19930086624
• Hallissy, J. B., and C. D. Harris. 1974. Wind-Tunnel Investigation of Aerodynamic Load Distribution on a Variable-Wing-Sweep Fighter Airplane with a NASA Supercritical Airfoil. NASA-TM-X-3095. NASA. https://ntrs.nasa.gov/citations/19830002846
• Hallstaff, T. 1966. “Aerodynamics of Powerplant Installation on Supersonic Aircraft.” In 2nd Propulsion Joint Specialist Conference. AIAA 1966-665. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-665
• Halwas, Hussein K., and Suresh K. Aggarwal. 2019b. “Effect of Side Gust on the Performance of Supersonic Inlet with Bleed System.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4422
• Hama, Takayuki, Yuhta Kariyazaki, Keisuke Ochi, Hitoshi Fujimoto, and Hirohiko Takuda. 2010. “Springback Characteristics of Magnesium Alloy Sheet AZ31B in Draw-Bending.” Materials Transactions 51 (4): 685–93. https://doi.org/10.2320/matertrans.p-m2010803
• Hama, T., T. Sakai, Y. P. Korkolis, and H. Takuda. 2018. “Crystal-Plasticity Finite-Element Simulation of Time-Dependent Springback in a Commercially-Pure Titanium Sheet.” Journal of Physics: Conference Series 1063: 012122. https://doi.org/10.1088/1742-6596/1063/1/012122
• Hamed, Awatef. 1995. An Investigation of Bleed Configurations and Their Effect on Shock Wave/boundary Layer Interactions. NASA-CR-199439. NASA. https://ntrs.nasa.gov/citations/19960000871
• Hamer, Harold A., John P. Mayer, and Wilber B. Huston. 1961. Application of Monte Carlo Technique for Determining Maneuvering Loads from Statistical Information on Airplane Motions. NASA/TN-D-524. NASA. https://ntrs.nasa.gov/citations/20040027944
• Hamilton, C. H., and Neil E. Paton. 1988. Superplasticity and Superplastic Forming: Proceedings of an International Conference on Superplasticity and Superplastic Forming Held in Blaine, Washington on 1-4 August 1988. Defense Technical Information Center. https://doi.org/10.21236/ada209678
• Hamilton, Gordon L., and H. Robert Welge. 1992. “Civil Aircraft Challenges in Engine/Airframe Integration.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-045
• Han, Jae-Do. 2008. “Design & Fabrication for Small Aircraft Landing Gear Drop Test Rig System.” Journal of the Korean Society for Aeronautical & Space Sciences 36 (11): 1121–25. https://doi.org/10.5139/jksas.2008.36.11.1121
• Han, Kyu Bin, Ryan George, Srihari Kurukuri, Michael J. Worswick, and Sooky Winkler. 2017. “Springback of Aluminum Alloy Brazing Sheet in Warm Forming.” In AIP Conference Proceedings, vol. 1892. Author(s). https://doi.org/10.1063/1.5008096
• Han, Kyu Bin, Ryan George, Michael J. Worswick, and Sooky Winkler. 2018. “Effect of Warm Forming on Formability and Springback of Aluminum Alloy Brazing Sheet.” Journal of Physics: Conference Series 1063: 012127. https://doi.org/10.1088/1742-6596/1063/1/012127
• Han, Jianhuan, and Guanxin Hong. 2015. “Modeling of Aircraft with Time-Varying Inertia Properties.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-1133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1133
• Han, Fei, Jian Hua Mo, Xiaohui Cui, and Zai Lin Wang. 2010b. “Studies on the Springback Mechanism of Incremental Sheet Forming Based on FEM Simulation.” Advanced materials research 102-104: 242–46. https://doi.org/10.4028/www.scientific.net/amr.102-104.242
• Han, Jun, Fa Zhong Shi, and Li Kang Shao. 2010a. “Improvement of the Iterative Algorithm for Numerical Simulation of Springback in Sheet Metal Forming.” Advanced materials research 102-104: 1–6. https://doi.org/10.4028/www.scientific.net/amr.102-104.1
• Han, Zhi Ren, Jing Xu, and Xiang Tao Meng. 2012. “Research on Algorithm of Springback in Sheet Metal Forming.” Advanced materials research 472-475: 2969–74. https://doi.org/10.4028/www.scientific.net/amr.472-475.2969
• Hancock, G. J. 1959b. “Notes on Thin Wing Theory at Low Supersonic Speeds: Part I. the Design of Lifting Surfaces.” Aeronautical Quarterly 10 (3): 247–65. https://doi.org/10.1017/s0001925900001487
• Hancock, G. J. 1965. “Static Aeroelasticity: A Reappraisal.” In Symposium on Structural Dynamics and Aeroelasticity. AIAA 1965-1120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1120
• Hanff, E., and X. Huang. 1991. “Roll-Induced Cross-Loads on a Delta Wing at High Incidence.” In 9th Applied Aerodynamics Conference. AIAA 1991-3223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3223
• 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
• Hanloser, K. J., and R. Cullom. 1979. “Test Verification of a Turbofan Partial Swirl Afterburner.” In ASME. https://ntrs.nasa.gov/citations/19790054968
• Hanson, P. W., and G. M. Levey. 1959. Experimental and Calculated Results of a Flutter Investigation of Some Very Low Aspect-Ratio Flat-Plate Surfaces at Mach Numbers from 0.62 to 3.00. NASA-TM-X-53. NASA. https://ntrs.nasa.gov/citations/19630003076
• Hao Zhang, Yaoxing Shang, Zongxia Jiao, Shuai Wu, and Xiaochao Liu. 2018. “A Pressure Servo Device Based on Switching Valves Designed for More-Electric Aircraft Brake System.” In CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2018.0239
• Harada, Toshiaki, Keiichi Kitamura, and Satoshi Nonaka. 2019. “Roll Moment Characteristics of Supersonic Flight Vehicle Equipped with Asymmetric Protuberance.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 17 (2): 111–19. https://doi.org/10.2322/tastj.17.111
• Hardrath, H. F., and G. J. Heimerl. 1965. An Assessment of a Titanium Alloy for Supersonic Transport Operations. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19650021522
• Hardy, M. C. 1996. “The Influence of Mean Stress on the Elevated Temperature Fatigue Life of a near-α Titanium Alloy.” In Fatigue ‘96. Elsevier. https://doi.org/10.1016/b978-008042268-8/50007-1
• Hardy, M. C. 1998. “The Effects of Oxidation and Creep on the Elevated Temperature Fatigue Behaviour of a near-α Titanium Alloy.” In Low Cycle Fatigue and Elasto-Plastic Behaviour of Materials. Elsevier. https://doi.org/10.1016/b978-008043326-4/50008-8
• Harloff, Gary, and Gregory Smith. 1995. “On Supersonic-Inlet Boundary-Layer Bleed Flow.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-38. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-38
• Harmon, Sidney M. 1947. Theoretical Supersonic Wave Drag of Untapered Sweptback and Rectangular Wings at Zero Lift. NACA-TN-1449. NASA. https://ntrs.nasa.gov/citations/19930082081
• Harmon, Sidney M. 1948. Stability Derivatives of Thin Rectangular Wings at Supersonic Speeds: Wing Diagonal Ahead of Tip Mach Lines. NACA-TN-1706. NASA. https://ntrs.nasa.gov/citations/19930082713
• Harmon, Sidney M. 1949a. Stability Derivatives at Supersonic Speeds of Thin Rectangular Wings with Diagonals Ahead of Tip Mach Lines. NACA-TR-925. NASA. https://ntrs.nasa.gov/citations/19930091990
• Harmon, Sidney M. 1949b. Theoretical Relations between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow. NACA-TN-1943. NASA. https://ntrs.nasa.gov/citations/19930082616
• Harmon, Dm, Ma Finefield, Cr Saff, and Ja Harter. 1996. “Titanium Matrix Composite Durability Analyses for the Design of Airframe Structures.” In Life Prediction Methodology for Titanium Matrix Composites. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp18239s
• Harmon, Sidney M., and Isabella Jeffreys. 1950. Theoretical Lift and Damping in Roll of Thin Wings with Arbitrary Sweep and Taper at Supersonic Speeds: Supersonic Leading and Trailing Edges. NACA-TN-2114. NASA. https://ntrs.nasa.gov/citations/19930082815
• Harmon, Sidney M., and Margaret D. Swanson. 1947. Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept behind the Mach Lines. NACA-RM-L6K29. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930085735
• Harper, Madison E., Bikash Kunwar, and Imon Chakraborty. 2026. “Extending an Automated Methodology for Simulation Model Calibration to Manufacturer and Flight Test Validation Data.” In AIAA SCITECH 2026 Forum. AIAA 2026-2019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2019
• Harri, J. 1964. The Aerodynamic Heating of a Vehicle Traveling at Supersonic Velocities through a Compressible Fluid. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4597699
• 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
• Hart, H. 1968. “Effect of Supersonic Interference on Lateral Stability of Low-Aspect-Ratio Missiles in Combined Pitch and Yaw.” In 6th Aerospace Sciences Meeting. AIAA 1968-21. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-21
• Hart, R., and D. Picha. 1979. “Dutch Roll Excitation and Recovery Techniques on a C-141A Starlifter.” In Aircraft Systems and Technology Meeting. AIAA 1979-1801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1801
• Hartley, Richard M., Roger J. Furey, Letendre Jr., and Robert P. 1965. Leading-Edge Wedges to Reduce the Drag of Thick Wings at Supersonic Speeds and to Increase Lift at Low Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0626655
• Hartmann, Christoph, Lorenz Maier, and Wolfram Volk. 2021. “Springback and Compensation in Sheet Metal Forming Reconsidered as an Ill-Posed Problem.” IOP Conference Series: Materials Science and Engineering 1157 (1): 012044. https://doi.org/10.1088/1757-899x/1157/1/012044
• 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
• Haseeb, Syed M. 2026. “Aerodynamic Validation of the ONERA M6 Wing Using Transonic CFD Simulation.” Preprint, . https://doi.org/10.36227/techrxiv.176827253.34525913/v1
• 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
• Hasel, Lowell E., John L. Lankford, and A. W. Robins. 1953. Investigation of a Half-Conical Scoop Inlet Mounted at Five Alternate Circumferential Locations around a Circular Fuselage Pressure-Recovery Results at a Mach Number 2.01. NACA-RM-L53D30B. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019413
• Haskind, M. D., and S. V. Falkovich. 1950. Vibration of a Wing of Finite Span in a Supersonic Flow. NACA-TM-1257. Langley Research Center. https://ntrs.nasa.gov/citations/20050019613
• Hassell, James L., Jr., and Donald E. Hewes. 1960. Investigation of the Subsonic Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane with and without Fuselage Forebody Strakes. NASA-TM-X-210. NASA. https://ntrs.nasa.gov/citations/19980228451
• Hastings, Earl C., Jr., and Waldo L. Dickens. 1957. Effects of Inlet Modification and Rocket-Rack Extension on the Longitudinal Trim and Low-Lift Drag of the Douglas F5D-1 Airplane as Obtained with a 0.125-Scale Rocket-Boosted Model between Mach Numbers of 0.81 and 1.64: TED No. NACA AD 399. NACA-RM-SL57D30. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20040034084
• Hatipoğlu, H. A., and C. O. Alkaş. 2016. “Process Modelling and Die Design Concepts for Forming Aircraft Sheet Parts.” Journal of Physics: Conference Series 734: 032088. https://doi.org/10.1088/1742-6596/734/3/032088
• Hausknecht, Donald F., and Ramojus P. Vaitys. 1961. An Investigation of Two Methods of Arrestment of High-Speed Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0268378
• 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
• Hayashi, Hisashi. 1996. “The Control of Shape Fixation and Springback of Aluminum Alloy Sheet in Model Forming.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/960819
• Hazen, R. M. 1941. “The ALLISON AIRCRAFT-ENGINE DEVELOPMENT.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/410137
• He, Xufei, Zhitao Song, Zhigang Wu, and Fengrui Liu. 2020. “Aeroelastic Testing for Freeplay Induced Limit Cycles of Flexible Wing-Aileron System.” In AIAA Scitech 2020 Forum. AIAA 2020-1908. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1908
• He, Xufei, Xiangyu Wang, and Guowei Tang. 2021. “Wind Tunnel Testing of Flexible Wing Model with Aileron Freeplay Nonlinearity.” In AIAA Aviation 2021 Forum. AIAA 2021-2534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2534
• He, Shun, ZhiChun Yang, and YingSong Gu. 2014. “Frequency Domain Analysis for Wing Transonic Flutter.” SCIENTIA SINICA Physica, Mechanica & Astronomica 44 (3): 285–92. https://doi.org/10.1360/132013-258
• Head, V. L. 1972. Flight Investigation of an Underwing Nacelle Installation of an Auxiliary-Inlet Ejector Nozzle with a Clamshell Flow Diverter from Mach 0.6 to 1.3. NASA-TM-X-2655. NASA. https://ntrs.nasa.gov/citations/19730003066
• Heald, W., and B. Brassell. 1976. “History and Development of a System for Stall-Departure Improvement for the a-7 Attack Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1976-891. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-891
• Healy, F. M. 1952. Free-Spinning-Tunnel Investigation of a 1 30-SCALE Model of the Grumman XS2F-1 Airplane. NACA-RM-SL52117. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630038253
• Healy, Frederick M. 1958. Free-Spinning-Tunnel Investigation of a 1/28-Scale Model of the North American FJ-4 Airplane with External Fuel Tanks, TED No. NACA AD 3112. NACA-RM-SL58H07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028462
• Heard, W., Jr. 1965. “Flutter of a Simply Supported Panel Subjected to a Nonlinear Temperature Distribution and Supersonic Flow.” In 2nd Aerospace Sciences Meeting. AIAA 1965-112. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-112
• Hearth, Donald P., and Robert W. Cubbison. 1956. Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles. NACA-RM-E55J12a. NASA. https://ntrs.nasa.gov/citations/19930088935
• Heath, Christopher M., John W. Slater, and iram K. Rallabhandi Sr. 2016. “Inlet Trade Study for a Low-Boom Aircraft Demonstrator.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170002621
• Heeg, Jennifer, and Pawel Chwalowski. 2017. “Investigating the Transonic Flutter Boundary of the Benchmark Supercritical Wing.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0191
• Heeg, Jennifer, Bret K. Stanford, Carol D. Wieseman, et al. 2018. “Status Report on Aeroelasticity in the Vehicle Development for X-57 Maxwell.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20200002314
• Hefti, Larry D. 2010a. “Elevated Temperature Fabrication of Titanium Aerospace Components.” Key Engineering Materials 433: 49–55. https://doi.org/10.4028/www.scientific.net/kem.433.49
• Hefti, Larry D. 2010b. “Fabrication of Titanium Aerospace Hardware Using Elevated Temperature Forming Processes.” SAE International Journal of Aerospace 03 (1): 173–79. https://doi.org/10.4271/2010-01-1834
• Hefti, Larry D. 2010c. “Fine-Grain Titanium 6AI-4V for Superplastic Forming and Diffusion Bonding of Aerospace Products.” JOM 62 (5): 42–45. https://doi.org/10.1007/s11837-010-0076-9
• Hefti, Larry D. 2012. “Elevated Temperature Forming of Titanium Aircraft Hardware.” In Materials science forum, vol. 735. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.735.338
• Hegazy, A. A., and J. D. Mote. 1985. “Explosive Welding of Aluminum, Titanium and Zirconium to Copper Sheet Metal.” In NASA. Langley Research Center Welding, Bonding and Fastening, 1984. https://ntrs.nasa.gov/citations/19860001774
• Hegde, Amruthkiran, Mingtai Chen, Semih Olcmen, James P. Hubner, Jim Crafton, and Colleen Ryan. 2021. “Pressure and Strain Measurement on a Thin Clamped Plate in Supersonic Flow Using a Dual-Layer Luminescent Coating.” In AIAA Aviation 2021 Forum. AIAA 2021-2920. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2920
• Heimerl, George, J., o M. Kurg IV, and John E. Inge. 1956. Tensile Properties of Inconel and RS-120 Titanium-Alloy Sheet under Rapid-Heating and Constant-Temperature Conditions. NACA-TN-3731. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930084484
• Heinle, Donovan R. 1950. Effect of Dihedral Change on the Theoretical Dynamic Lateral Response Characteristics of a Low-Aspect-Ratio Straight-Wing Supersonic Airplane. NACA-RM-A50H02. NASA. https://ntrs.nasa.gov/citations/19930086335
• Heitmeyer, John C. 1952. Lift, Drag and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Plane Tapered Wing of Aspect Ratio 3.1 with 3 Percent Thick Rounded Nose Section. NACA-RM-A52D23. NASA. https://ntrs.nasa.gov/citations/19930087211
• Heitmeyer, John C. 1954. Effect of a Leading-Edge Flap upon the Lift, Drag, and Pitching Moment of an Airplane Employing a Thin, Unswept Wing. NACA-RM-SA54B16. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20090032234
• Heitmeyer, John C., and Willard G. Smith. 1952. Effects of Simulated Skin Wrinkles on the Wing Surface on the Aerodynamic Characteristics of Two Wing-Body Combinations Employing Wings of Low Aspect Ratio at Subsonic and Supersonic Speeds. NACA-RM-A52E23. NASA. https://ntrs.nasa.gov/citations/19930087209
• Hemsch, M., and J. Nielsen. 1982. “The Equivalent Angle-of-Attack Method for Estimating the Nonlinear Aerodynamic Characteristics of Missile Wings and Control Surfaces.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1338
• 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, William P. 1987. “Propulsion-Airframe Integration for Commercial and Military Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/872411
• Henderson, William P. 1990. “Airframe/Propulsion Integration at Transonic Speeds.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-338
• Henderson, W. P. 1991. “Airframe/Propulsion Integration at Transonic Speeds.” Journal of Engineering for Gas Turbines and Power 113 (1): 51–59. https://doi.org/10.1115/1.2906530
• Henderson, Dennis. 1999. “Impacts of Structural Dynamics on Inlet Flow Incidence Angle and Inlet Unstart.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-369. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-369
• Henderson, Arthur, Jr. 1957. Wind-Tunnel Investigation of Static Lateral and Longitudinal Stability Characteristics of a 1/62-Scale Model of the X-1E Airplane at Combined Angles of Attack and Sideslip at Supersonic Speeds. NACA-RM-L57G22. NASA. https://ntrs.nasa.gov/citations/19930089811
• Hendrickson, R., R. Grossman, and A. Sclafani. 1978. “Design Evolution of a Supersonic Cruise Strike-Fighter.” In Aircraft Systems and Technology Conference. AIAA 1978-1452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1452
• Henning, Allen B. 1959. Stability Characteristics of Two Missiles of Fineness Ratios 12 and 18 with Six Rectangular Fins of Very Low Aspect Ratio over a Mach Number Range of 1.4 to 3.2. NASA-MEMO-12-2-58L. NASA. https://ntrs.nasa.gov/citations/19980228138
• 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
• Herges, Thomas, J. Dutton, and Gregory Elliott. 2012. “High-Speed Schlieren Analysis of Buzz in a Relaxed-Compression Supersonic Inlet.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-4146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4146
• Hermach, C. A., Samuel Kraus, and John O. Reller Jr. 1957. Reductions in Temperature-Recovery Factor Associated with Pulsating Flows Generated by Spike-Nosed Cylinders at a Mach Number of 3.50. NACA-RM-A56L05. NASA. https://ntrs.nasa.gov/citations/19930089897
• Hermann, Rudolf. 1956. “Engine Inlet Air Diffuser Controls for Supersonic Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/560270
• Hernandez, Santiago, Aitor Baldomir, and Clara Cid. 2019. “Numerical Approach to the Setting of Aircraft in-Flight Target Loads Problem.” In AIAA Aviation 2019 Forum. AIAA 2019-3070. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3070
• Hernandez, Gloria, Richard M. Wood, and Peter F. Covell. 1994. Effect of Leading- and Trailing-Edge Flaps on Clipped Delta Wings with and without Wing Camber at Supersonic Speeds. NASA-TM-4542. NASA. https://ntrs.nasa.gov/citations/19950003616
• Herrick, P. 1986. “Fighter Aircraft/propulsion Integration.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2658. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2658
• 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
• Herrmann, P. 1996. “Propulsion Integration Aspects in Advanced Military Aircraft.” In ASME 1996 Turbo Asia Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/96-ta-057
• 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
• Heslet, Max A., Harvard Lomax, and Arthur L. Jones. 1947. Voltera’s Solution of the Wave Equation as Applied to Three-Dimensional Supersonic Airfoil Problems. NACA-TR-889. NASA. https://ntrs.nasa.gov/citations/19930090945
• Hess, R. 1986. “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, and Ronald Hess. 1997a. “A Theory for the Roll-Ratchet Phenomenon in High Performance Aircraft.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3498
• Hess, R., and R. Hess. 1997b. “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
• Hess, Robert, William McNamara, and Mark Franko. 1988. “Recent Results in the Identification of High Angle-of-Attack F/TF-18aerodynamics.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4348. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4348
• 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
• Hewes, Donald E. 1951. The Effects of Mass Distribution on the Low-Speed Dynamic Lateral Stability and Control Characteristics of a Model with 45 Degree Sweptback Wing. NACA-TN-2313. NASA. https://ntrs.nasa.gov/citations/19930082991
• Hewes, Donald E., James S. Bowman Jr., and James L. Hassell Jr. 1958. Low-Speed Stability and Control and Spinning Characteristics of Dynamic Models of the X-15 Airplane. NASA. https://ntrs.nasa.gov/citations/19930092385
• Hewitt, Rl, Jp Weiss, and Pk Nor. 2005. “Spectrum Editing for a Full-Scale Fatigue Test of a Fighter Aircraft Wing with Buffet Loading.” In Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp11301s
• 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
• Hidayat, Dony, Jos Istiyanto, and Danardono Agus Sumarsono. 2018. “Comparison Virtual Landing Gear Drop Test for Commuter Aircraft Utilize MSC ADAMS and Solidworks Motion Analysis.” Journal of Physics: Conference Series 1005: 012007. https://doi.org/10.1088/1742-6596/1005/1/012007
• “High Supersonic Speed Wind Tunnel: Details of the New Facility Constructed at the Royal Aircraft Establishment, Bedford.” 1961. Aircraft Engineering and Aerospace Technology 33 (5): 136–44. https://doi.org/10.1108/eb033409
• “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-Temperature Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-7
• Hiley, P., and D. Bowers. 1981. “Advanced Nozzle Integration for Supersonic Strike Fighter Application.” In 17th Joint Propulsion Conference. AIAA 1981-1441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1441
• Hill, P. 1970. “Airframe-Inlet Integration.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-933. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-933
• Hill, W. A., Jr., and G. E. Kaattari. 1956. Force and Pressure-Distribution Investigation to High Angles of Attack on All-Movable Triangular and Rectangular Wings in Combination with a Body at Supersonic Speeds. NACA-RM-A56C12. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19660024059
• Hinkley, Jeffrey A., Norman J. Johnston, A. Bruce Hulcher, Joseph M. Marchello, and Bernadette C. Messier. 1999. Utilization of Induction Bonding for Automated Fabrication of TIGR. NASA/TM-1999-209123. NASA. https://ntrs.nasa.gov/citations/19990041100
• Hinz, W., and E. Miller. 1979. “Propulsion Integration of a Supersonic Cruise Strike-Fighter.” In 17th Aerospace Sciences Meeting. AIAA 1979-100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-100
• Hirose, Kenya, Kohei Suzuki, and Wataru Yamazaki. 2024. “Efficient Aerodynamic Topology Optimization for Supersonic Airfoil Using Dimensionality Reduction Methods.” In AIAA SCITECH 2024 Forum. AIAA 2024-1406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1406
• Hirschel, Ernst Heinrich, Arthur Rizzi, Christian Breitsamter, and Werner Staudacher. 2020a. “Selected Flow Problems of Small Aspect-Ratio Delta-Type Wings.” In Separated and Vortical Flow in Aircraft Wing Aerodynamics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-61328-3_11
• Hirschel, Ernst Heinrich, Arthur Rizzi, Christian Breitsamter, and Werner Staudacher. 2020b. “Small Aspect-Ratio Delta-Type Wing Flow.” In Separated and Vortical Flow in Aircraft Wing Aerodynamics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-61328-3_10
• Hirt, Stefanie M., Rodrick V. Chima, Manan A. Vyas, Thomas R. Wayman, Timothy R. Conners, and Robert W. Reger. 2011. “Experimental Investigation of a Large-Scale Low-Boom Inlet Concept.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110014468
• Hodder, B., B. Farquhar, and M. Dudley. 1981. “A Large-Scale Investigation of Engine Influence on Inlet Performanceat Angle-of-Attack.” In 1st Flight Test Conference. AIAA 1981-2481. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2481
• 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
• Hoerner, S. 1936. “Skin Drag of High Speed Aircraft: The Laws for the Drag of Smooth and Rough Flat Surfaces Applied to Aircraft.” Aircraft Engineering and Aerospace Technology 8 (4): 103–8. https://doi.org/10.1108/eb030033
• Hoffman, T. R. 2000. Two-Dimensional Bifurcated Inlet Variable Cowl Lip Test Completed in 10- by 10-Foot Supersonic Wind Tunnel. NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20050194574
• Hoffmann, E. K., R. K. Bird, and T. T. Bales. 1989. “Fabrication and Evaluation of Enhanced Diffusion Bonded Titanium Honeycomb Core Sandwich Panels with Titanium Aluminide Face Sheets.” In Minerals, Metals and Materials Society. https://ntrs.nasa.gov/citations/19900057153
• Hoffmann, C., D. Eylon, and Aj McEvily. 1982. “Influence of Microstructure on Elevated-Temperature Fatigue Resistance of a Titanium Alloy.” In Low-Cycle Fatigue and Life Prediction. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp32420s
• Hofmann, Rodolfo, Seyedbarzin Hosseini, and Florian Holzapfel. 2025a. “Automated Maneuver Injection for General Aviation Aircraft for System Identification: Lessons Learned.” In AIAA SCITECH 2025 Forum. AIAA 2025-2172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2172
• Hofmann, Rodolfo, Seyedbarzin Hosseini, and Florian Holzapfel. 2025b. “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
• 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., and Jack A. Mellenthin. 1960a. Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-Body Combinations of Sonic Design with Diamond, Delta, and Arrow Plan Forms. NASA-TM-X-372. NASA. https://ntrs.nasa.gov/citations/19980235518
• Holdaway, George H., and Jack A. Mellenthin. 1960b. Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-Body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms. NASA-TM-X-390. NASA. https://ntrs.nasa.gov/citations/19980223980
• Holdaway, George H., Jack A. Mellenthin, and Elaine W. Hatfield. 1959. Investigation at Mach Numbers of 0.20 to 3.50 of a Blended Diamond Wing and Body Combination of Sonic Design but with Low Wave-Drag Increase with Increasing Mach Number. NASA-TM-X-105. NASA. https://ntrs.nasa.gov/citations/19980232906
• 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
• Holloway, C. M., and C. W. Johnson. 2008. “How past Loss of Control Accidents May Inform Safety Cases for Advanced Control Systems on Commercial Aircraft.” In 3rd IET International Conference on System Safety 2008. IEE. https://doi.org/10.1049/cp:20080732
• 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, M., and T. M. Lee. 1973. “First-Order Frequency Effects in Supersonic Panel Flutter of Finite Cylindrical Shells.” Journal of Applied Mechanics 40 (2): 464–70. https://doi.org/10.1115/1.3423007
• 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
• Holzman, Jon K., Lannie D. Webb, and Frank W. Burcham Jr. 1996. Flight and Static Exhaust Flow Properties of an F110-GE-129 Engine in an F-16XL Airplane during Acoustic Tests. NASA-TM-104326. NASA. https://ntrs.nasa.gov/citations/19970003552
• Hom, K., O. Morris, and D. Hahne. 1983. “Low-Speed Investigation of the Maneuver Capability of Supersonic Fighter Wings.” In 21st Aerospace Sciences Meeting. AIAA 1983-426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-426
• Hong, J. 1965. “Resolution of Speed Stability for Supersonic Aircraft.” In Propulsion Joint Specialist Conference. AIAA 1965-622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-622
• Hong, John. 1993. An Aerodynamic Model for One and Two Degree of Freedom Wing Rock of Slender Delta Wings. NASA-CR-193130. NASA. https://ntrs.nasa.gov/citations/19930017961
• Hong, Wooram, and Chongam Kim. 2011. “Numerical Study on Supersonic Inlet Buzz under Various Throttling Conditions and Fluid-Structure Interaction.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3967. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3967
• Hopkins, E. 1975. “Effects of Wing Bend on the Aerodynamic Characteristics of a Low Aspect Ratio Oblique Wing.” In Aircraft Systems and Technology Meeting. AIAA 1975-995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-995
• Hopko, Russell N. 1951. A Flight Investigation of the Damping in Roll and Rolling Effectiveness Including Aeroelastic Effects of Rocket Propelled Missile Models Having Cruciform, Triangular, Interdigitated Wings and Tails. NACA-RM-L51D16. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19680068649
• “Horizontal Tail Loads.” 1996. In Structural Loads Analysis for Commercial Transport Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862465.0115.0142
• Horne, Walter B., Upshur T. Joyner, and Trafford J. W. Leland. 1960. Studies of the Retardation Force Developed on an Aircraft Tire Rolling in Slush or Water. NASA-TN-D-552. NASA. https://ntrs.nasa.gov/citations/20010057773
• Horne, W. B., J. L. McCarty, and J. A. Tanner. 1976. Some Effects of Adverse Weather Conditions on Performance of Airplane Antiskid Braking Systems. NASA-TN-D-8202. NASA. https://ntrs.nasa.gov/citations/19760019083
• Horton, Amanda, and Melissa McDaniel. 2005. “Identification and Correction of Axial Force Prediction Discrepancies Due to Angle of Attack Effects in Missile DATCOM.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4833. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4833
• Hosek, J., P. Lyons, and C. Schmid. 1981. “Development of Airframe Structural Design Loads Prediction Techniques for Flexible Military Aircraft: Theoretical Development.” In Aircraft Systems and Technology Conference. AIAA 1981-1696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1696
• Hoshi, Ritsuya, Yuichi Kuya, and Keisuke Sawada. 2020. “Numerical Simulations of Transonic Flutter on a Three-Dimensional Wing.” In AIAA Scitech 2020 Forum. AIAA 2020-0091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0091
• Hosseini, Seyedbarzin, Rodolfo Hofmann, Florian Holzapfel, and Juergen Rauleder. 2025. “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
• Hou, Gene, and Arunkumar Satyanarayana. 2000. “Analytical Sensitivity Analysis of a Static Aeroelastic Wing.” In 8th Symposium on Multidisciplinary Analysis and Optimization. AIAA 2000-4824. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4824
• Houghton, E. L., P. W. Carpenter, Steven H. Collicott, and Daniel T. Valentine. 2017. “Thin Airfoil Theory.” In Aerodynamics for Engineering Students. Elsevier. https://doi.org/10.1016/b978-0-08-100194-3.00006-7
• Howard, E., R. W. Luidens, and J. L. Allen. 1951. Force and Pressure Characteristics for a Series of Nose Inlets at Mach Numbers from 1.59 to 1.99 V: Analysis and Comparison on Basis of Ram-Jet Aircraft Range and Operational Characteristics. NACA-RM-E51G23. NASA. https://ntrs.nasa.gov/citations/19930086661
• Howell, Robert R. 1958. An Initial Experimental Study of the Effect of Variations in Frequency and Impulse on the Reduction in Temperature Recovery Factor Afforded by Large-Scale Unsteady Flow. NACA-RM-L57I27. NASA. https://ntrs.nasa.gov/citations/19930090007
• 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, William E., John R. McGehee, Robert H. Daugherty, and William A. Vogler. 1990. F-106B Airplane Active Control Landing Gear Drop Test Performance. NASA-TM-102741. NASA. https://ntrs.nasa.gov/citations/19910004132
• Howell, We, Se Perez, and Wa Vogler. 1986. “Aircraft Tire Footprint Forces.” In The Tire Pavement Interface. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp20005s
• Hower, Fred C., E. W. Feddersen, C. F. Crabtree, and W. O. Sunafrank. 1956. Fabrication and Test of Titanium Jet Pods. Defense Technical Information Center. https://doi.org/10.21236/ad0097198
• Howerton, Layton W., and John W. Slater. n.d. “Auxiliary Inlet Design Study for Mach 1.4.” In 2021 AIAA Propulsion and Energy Forum. https://ntrs.nasa.gov/citations/20210018078
• Howland, W. Lavern. 1953. “Flight Test Instrumentation Status.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/530162
• Howlett, D., and L. Hunter. 1986. “A Study of a Supersonic Axisymmetric Spiked Inlet at Angle of Attackusing the Navier-Stokes Equations.” In 24th Aerospace Sciences Meeting. AIAA 1986-308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-308
• Hoy, W. W. 1963. A Method for Establishing Landing Design Criteria for Carrier-Based Airplanes. Defense Technical Information Center. https://doi.org/10.21236/ad0409438
• Hoy, J. R. 1976. “Toward a Second Generation Fuel Efficient Supersonic Cruise Aircraft Structural Design for Efficiency.” In NASA. Langley Res. Center Proc. of the SCAR Conf., Pt. 2,. https://ntrs.nasa.gov/citations/19770011094
• Hreha, M., and F. Lutze. 1983. “A Dynamic Model for Aircraft Poststall Departure.” In 21st Aerospace Sciences Meeting. AIAA 1983-367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-367
• Hsiao, F. B., C. Y. Lin, Y. C. Liu, D. B. Wang, C. C. Hsu, and C. H. Chiang. 2008. “Thickness Effect on Low-Aspect-Ratio Wing Aerodynamic Characteristics at a Low Reynolds Number.” Journal of Mechanics 24 (3): 223–28. https://doi.org/10.1017/s1727719100002288
• Hu, Biao, Gaoshen Cai, Jubo Fu, Yanxi Xin, Kangning Liu, and Lihui Lang. 2021. “Investigation on Granular Medium Forming Formability of TA1 Titanium Alloy Cylinder-Shaped Parts.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-564767/v1
• Huang, Adam, Chris Folk, Chris Silva, et al. 2001. “Applications of MEMS Devices to Delta Wing Aircraft: From Concept Development to Transonic Flight Test.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-124. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-124
• Huang, Juan-Chen, Herng Lin, and Ching-Chang Chieng. 2002. “Computations of Roll-Damping Stability Derivative for Body/Cruciform-Tail Configuration.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2721
• Huang, Daning, Ashwin Renganathan, and Mark A. Miller. 2023. “Design of an Aeroelastically Scaled Model in a Compressible Air Wind Tunnel Facility Using Multifidelity Multi-Objective Bayesian Optimization.” In AIAA SCITECH 2023 Forum. AIAA 2023-2040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2040
• Huang, Chao, Zhigang Wu, Chao Yang, and Yuting Dai. 2017. “Flutter Boundary Prediction for a Flying-Wing Model Exhibiting Body Freedom Flutter.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0415
• Huerta, Joseph. 1969. An Experimental Investigation at Supersonic Mach Numbers of Base Drag of Various Boattail Shapes with Simulated Base Rocket Exhaust. Defense Technical Information Center. https://doi.org/10.21236/ad0855156
• Huffman, J., and C. Fox Jr. 1985. “Subsonic Pressure Distributions near a Wing-Fin Juncture on a Supersonic Arrow-Wing Configuration with Wing-Mounted Vertical Fins.” In 23rd Aerospace Sciences Meeting. AIAA 1985-276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-276
• 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
• 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
• Hui, Zhu, and Zhi Gang Yang. 2013. “Design for Wind Tunnel Testing of Scaled Model by CFD Method.” Applied Mechanics and Materials 275-277: 567–71. https://doi.org/10.4028/www.scientific.net/amm.275-277.567
• 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
• Hultberg, Randy, James Bowman Jr., and Colin Martin. 1988. “Measurements of Pressures on the Tail and Aft Fuselage of an Airplane Model during Rotary Motions at Spin Attitudes.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4338
• Hultz, Burton E. 1951. Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the Douglas X-3 Airplane. NACA-RM-L51K12. NASA. https://ntrs.nasa.gov/citations/19930087177
• Hunczak, Henry R. 1952. Investigation at Mach Numbers 2.98 and 2.18 of Axially Symmetric Free-Jet Diffusion with a Ram-Jet Engine. NACA-RM-E51L24. NASA. https://ntrs.nasa.gov/citations/19930087850
• Hunczak, Henry R., and Emil J. Kremzier. 1950. Characteristics of Perforated Diffusers at Free-Stream Mach Number 1.90. NACA-RM-E50B02. NASA. https://ntrs.nasa.gov/citations/19930086237
• Hunt, B., and N. Gowadia. 1981. “Determination of Thrust and Throttle-Dependent Drag for Fighter Aircraft.” In Aircraft Systems and Technology Conference. AIAA 1981-1692. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1692
• Hunter, L., and J. Cawthon. 1984. “Improved Supersonic Performance Design for the F-16 Inlet Modified for the J-79 Engine.” In 20th Joint Propulsion Conference. AIAA 1984-1272. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1272
• Hunter, L., J. Tripp, and D. Howlett. 1985. “A Mach 2.0 Plus Supersonic Inlet Study Using the Navier-Stokes Equations.” In 21st Joint Propulsion Conference. AIAA 1985-1211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1211
• 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, W. V. 1951. “Turbojet-Engine Design for High-Speed Flight.” Journal of Fluids Engineering 73 (7): 915–20. https://doi.org/10.1115/1.4016500
• Hurwitz, Wayne, Kyle Whitcomb, Wayne Hurwitz, and Kyle Whitcomb. 1997. “Flight Test Validation of B-2 Inlet/engine Compatibility: A Risk Management Approach.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3157
• Hussain, G., and L. Gao. 2006. “Fundamental Studies on Incremental Forming of Titanium Sheet-Metal.” In Manufacturing Science and Engineering, Parts A and B. ASMEDC. https://doi.org/10.1115/msec2006-21015
• Hutchinson, Rhys, Jeremy Lawrence, and Keith F. Joiner. 2021. “Conceptual Design and Integration of a Propulsion System for a Supersonic Transport Aircraft.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 236 (3): 583–92. https://doi.org/10.1177/09544100211016952
• 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
• Hwang, C., and W. Pi. 1975b. “Transonic Buffet Behavior of Northrop F-5A Aircraft.” In 13th Aerospace Sciences Meeting. AIAA 1975-70. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-70
• Hwang, Kyu C., Surrendra N. Tiwari, and Stanley J. Miley. 1995. Experimental Investigation of the Inlet Detector Configuration Variation in the Flow Field at Mach 1.9. NASA-CR-199617. NASA. https://ntrs.nasa.gov/citations/19960002555
• Hyde, David C., Frank Brown, Kamal M. Shweyk, Kevin Cunningham, and Gautam H. Shah. 2018. “High Angle of Attack Static and Dynamic Modeling Methods for Flight Dynamics Loss of Control Research.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-1021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1021
• Hyde, David, Ross Gadient, and Eugene Lavretsky. 2011. “Flight Testing the X-48B Angle-of-Attack and Sideslip Limiting System.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6471
• Iannelli, Joe. 2007a. “Supersonic-Inlet Start Amelioration and Unstart Mitigation via Mass and Heat Transfer.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-522
• Iannelli, Joe. 2007b. “Unstart Mitigation in Inlet and Isolator via Wall Mass Transfer: A Computational Study.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5071
• Ibrahim, Aws Khalid. 2026. “Springback in Sheet Metal Bending: A Comprehensive Review of Influencing Factors, Prediction Methods, Monitoring Techniques and Compensation Strategies.” Open Access Research Journal of Engineering and Technology 11 (1): 052–070. https://doi.org/10.53022/oarjet.2026.11.1.0057
• Ide, H., and D. Ominsky. 1990. “Simulation of Static and Dynamic Aeroelastic Behavior of a Flexible Wing with Multiple Control Surfaces.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-1075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1075
• “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
• Igoe, W. B. 1967. Wind-Tunnel Buffeting Measurements on Two Wing End-Plate Airplane Model Configurations. NASA-TM-X-1454. NASA. https://ntrs.nasa.gov/citations/19670030773
• Ilie, Marcel, and John Havenar. 2023. “Dynamic Aeroelastic Instabilities of Fixed-Wing Aircraft in Transonic and Supersonic Flows Using a Fully-Coupled Model.” In AIAA SCITECH 2023 Forum. AIAA 2023-1041. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1041
• Ilie, Marcel, and Geoffrey Sullivan. 2020. “Aerodynamics and Aeroacoustics Studies of Supersonic Flow past Wing.” In AIAA Aviation 2020 Forum. AIAA 2020-2602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2602
• 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
• Illg, W., and L. A. Imig. 1969. Fatigue of Notched Ti-8Al-1Mo-1V Titanium Alloy at Room Temperature and 550 Deg F (560 Deg K) with Flight-by-Flight Loading Representative of a Supersonic Transport. NASA-TN-D-5294. NASA. https://ntrs.nasa.gov/citations/19690020229
• Illg, W., and L. A. Imig. 1971. Fatigue of Four Stainless Steels, Four Titanium Alloys, and Two Aluminum Alloys before and after Exposure to Elevated Temperatures for up to Three Years. NASA-TN-D-6145. NASA. https://ntrs.nasa.gov/citations/19710012601
• Iloputaife, Obi, and Lily Ma. 1987. “Handling Qualities Design of a Northrop High-Performance Fighter.” In Guidance, Navigation and Control Conference. AIAA 1987-2450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2450
• Ilyukhin, I. M., and Ivan Vladimirovich Egorov. 2024. Numerical Simulation of Nonlinear Disturbance Propagation over Unswept Parabolic Airfoil in Supersonic Flow. https://doi.org/10.53954/9785604990148_78
• Im, Hongsik, Xiangying Chen, and Gecheng Zha. 2012. “Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-39. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-39
• Imig, L. A. 1967. Effect of Initial Loads and of Moderately Elevated Temperature on the Room-Temperature Fatigue Life of Ti-8Al-1Mo-1V Titanium- Alloy Sheet. NASA-TN-D-4061. NASA. https://ntrs.nasa.gov/citations/19670022210
• Imrak, Rumed, Emre Karaselvi, Bulent Tutkun, and Melike Nikbay. 2021. “Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft.” In AIAA Aviation 2021 Forum. AIAA 2021-2469. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2469
• 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
• “Inertia Coupling and Spin.” 2004. In Performance, Stability, Dynamics, and Control of Airplanes, Second Edition. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862274.0631.0676
• “Inertia Coupling and Spin.” 2015. In Performance, Stability, Dynamics, and Control of Airplanes, Third Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102745.0681.0730
• “Influence of Back Pressure on the Flow in the Diffuser of a Supersonic Air Inlet.” 2017. Perm National Research Polytechnic University Aerospace Engineering Bulletin, no. 49. https://doi.org/10.15593/2224-9982/2017.49.02
• “Influence of Wing Geometry on Leading-Edge Vortices and Vortex-Induced Aerodynamics at Supersonic Speeds.” 1989. In 27th Aerospace Sciences Meeting. AIAA 1989-85. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-85
• Innocenti, Mario. 1989. “Roll Response Criteria for High Maneuverable Aircraft Using Gibson’smethod.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3391
• Inoue, Toshiaki, Jun-Ichi Hirokawa, Toshio Hanai, and Hikaru Takami. 1991. “Conceptual Study of Supersonic Propulsion Systems.” In Aircraft Design and Operations Meeting. AIAA 1991-3133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3133
• “Instrumentation for in-Flight Determination of Steady-State and Dynamic Inlet Performance in Supersonic Aircraft.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0041.0058
• “Investigations of Propulsion Integration Interference Effects on a Transport Aircraft Configuration.” 1992. In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3097
• IOM3. 2024. “15th World Conference on Titanium Chapter 2: Aerospace Applications.” Preprint, . https://doi.org/10.7490/f1000research.1119882.1
• Iosilevskii, Gil. 2025a. “Linearized Theory of Thin Wings of Finite Span.” In Wing Theory—Incompressible Fluids. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-73625-4_7
• Iosilevskii, Gil. 2025b. “Low-Aspect-Ratio Wings in Nonuniform Motion.” In Wing Theory—Incompressible Fluids. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-73625-4_11
• Iosilevskii, Gil. 2025c. “Thin Wing Sections in Non-Uniform Motion.” In Wing Theory—Incompressible Fluids. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-73625-4_4
• Iosilevskii, Gil. 2025d. “Thin Wing Sections in Steady Motion.” In Wing Theory—Incompressible Fluids. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-73625-4_3
• Iqbal, Shaheed. 2003. “Analysis of Flight Test Manoeuvres Using Bifurcation Analysis Methods in Support of Flight Clearance.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5321. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5321
• Ishihara, T. 1995. “Application of Metal Matrix Composites for Supersonic Aeroplane Engines.” In Advanced Technology for Design and Fabrication of Composite Materials and Structures. Springer Netherlands. https://doi.org/10.1007/978-94-015-8563-7_29
• 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
• 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
• Islam, M., C. Fermin, and H. Aglan. 2015. “Microscopic Origin of Strength and Microhardness of Titanium Alloy at Elevated Temperature.” Microscopy and Microanalysis 21 (S3): 287–88. https://doi.org/10.1017/s1431927615002238
• Ison, David. 2017. “Qualitative Analysis of Loss of Control Aircraft Accidents Using Text Mining Techniques.” International Journal of Aviation, Aeronautics, and Aerospace. https://doi.org/10.15394/ijaaa.2017.1095
• Israq, Md Ahad, Mahi Uddin Ahmaad, Ashiquzzaman Sadi, Jolok Banarjee, and Saifur Rahman Bakaul. 2025. “Structural Analysis and Material Selection for Wing of a Newly Designed Supersonic Fighter Aircraft.” In 2025 Regional Student Conferences. AIAA 2025-106584. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-106584
• Item, Cem C., and Oktay Baysal. 1995. “Wing-Section Optimization for Supersonic Viscous Flow.” In CFD for Design and Optimization. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0952
• Ito, Ryotaro, and Toshiaki Tsuchiya. 2018. “The Influence of Compressed Air Bleeding on Turbojet Engine Performance.” Proceedings of the Thermal Engineering Conference 2018 (0): 0079. https://doi.org/10.1299/jsmeted.2018.0079
• Ito, Ryotaro, and Toshiaki Tsuchiya. 2019. “The Influence of Compressed Air Bleeding on Turbojet Engine Performance.” Proceedings of Conference of Hokuriku-Shinetsu Branch 2019.56 (0): C014. https://doi.org/10.1299/jsmehs.2019.56.c014
• Ivanov, V. V., and A. V. Krasil’nikov. 1972. “Experimental Investigation of the Distribution of the Pressure on a Triangular Airfoil with Blunt Edges at Small Angles of Attack.” Fluid Dynamics 7 (2): 339–42. https://doi.org/10.1007/bf01186484
• Ivey, H. Reese, and Edward N. Bowen Jr. 1947. Theoretical Supersonic Lift and Drag Characteristics of Symmetrical Wedge-Shape-Airfoil Sections as Affected by Sweepback outside the Mach Cone. NACA-TN-1226. NASA. https://ntrs.nasa.gov/citations/19930081841
• Iwata, Noritoshi, Hideo Tsutamori, Masatomo Niihara, et al. 2007. “Numerical Prediction of Springback Shape of Severely Bent Sheet Metal.” In AIP Conference Proceedings, vol. 908. AIP. https://doi.org/10.1063/1.2740908
• Jackson, M. 2011. “Superplastic Forming and Diffusion Bonding of Titanium Alloys.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.3.227
• Jackson, L. R., and S. A. Gordon. 1957. “The Application of a New Structural Index to Compare Titanium Alloys with Other Materials in Airframe Structures.” Journal of Fluids Engineering 79 (5): 949–58. https://doi.org/10.1115/1.4013199
• Jackson, Bruce, and Keith D. Hoffler. 2017. “Effects of Atmospheric Motion on a Derived Angle-of-Attack Estimator.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4062. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4062
• 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
• Jacobs, P. F. 1983. Aileron Effectiveness for a Subsonic Transport Model with a High-Aspect-Ratio Supercritical Wing. NASA-TM-85674. NASA. https://ntrs.nasa.gov/citations/19850007386
• Jacobson, Steven. 2010. “Aircraft Loss of Control Causal Factors and Mitigation Challenges.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8007. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8007
• Jacocks, J. L., and K. R. Kneile. 1975. Statistical Prediction of Maximum Time-Variant Inlet Distortion Levels. Defense Technical Information Center. https://doi.org/10.21236/ada004104
• Jaeger, Sam, Martin Thome, Demoz Gebre-Egziabher, and Maziar S. Hemati. 2026. “Parametric Thrust and Drag Identification from Flight Test via Energy Maneuverability.” In AIAA AVIATION 2026 Forum. AIAA 2026-4164. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4164
• 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
• Jagannathan, Rangesh, and Craig T. Johansen. 2019. “Numerical Assessment of Intake Buzz with Nano-Particles across a Supersonic External Compression Intake.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4425. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4425
• Jain, Anshul A. 2025. “Component Sizing and Design-Point Performance Evaluation of a Two-Spool Turbofan Engine with Mixed Exhaust and Afterburner.” International Journal of Science and Research (IJSR): 1945–48. https://doi.org/10.21275/sr251223120745
• Jain Sudhir, Prathik, Ravindra Holalu Venkatadas, and Ugrasen Gonchikar. 2021. “Machining Characteristics Estimation in WEDM Process While Machining Titanium Grade-2 Material Using ANN.” Preprint, . https://doi.org/10.1115/1.0004046v
• James, Jintu K., and T. M. Muruganandam. 2019. “Shock Oscillations in a Supersonic Diffuser Flow with Varying Stagnation Pressure.” In 31st International Symposium on Shock Waves 2. Springer International Publishing. https://doi.org/10.1007/978-3-319-91017-8_103
• Janakiram, Sushmitha, and Subrahmanyam Duvvuri. 2024. “Unstart Dynamics in a Curved Compression Ramp Air Intake.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3977. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3977
• Janardhan, Srinivasan, and Ramana V. Grandhi. 2003. Multidisciplinary Optimization of an Aircraft Wing/Tip Store in the Transonic Regime. Defense Technical Information Center. https://doi.org/10.21236/ada417106
• Janardhan, Srinivasan, Ramana Grandhi, Frank Eastep, and Brian Sanders. 2003. “Design Studies of Transonic Flutter and Limit-Cycle Oscillation of an Aircraft Wing/Tip Store.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1944. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1944
• 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
• Jardin, Matthew, and Eric Mueller. 2007. “Optimized Measurements of UAV Mass Moment of Inertia with a Bifilar Pendulum.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6822
• Jarosław, Milczarczyk, Rogólski Robert, and Olejnik Aleksander. 2026. “Comparative Wing Stiffness Analysis of a Dynamically Scaled Model and a Reference Aircraft Taking into Account Diverse Manufacturing Technologies.” In The 15th EASN International Conference on “Innovation in Aviation & Space Towards Sustainability Today & Tomorrow”. MDPI. https://doi.org/10.3390/engproc2026133092
• Jategaonkar, Ravindra, and Ermin Plaetschke. 1988. “Identification of Moderately Nonlinear Flight Mechanics Systems Withadditive Process and Measurement Noise.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4347. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4347
• Jeans, Ll, and Wl Tribble. 1979. “Test Simulation of Fighter Aircraft Maneuver Load Spectra.” In Service Fatigue Loads Monitoring, Simulation, and Analysis. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp35876s
• Jebáček, Ivo, and Marek Horák. 2016. “Measuring of a Nose Landing Gear Load during Take-Off and Landing.” Applied Mechanics and Materials 821: 325–30. https://doi.org/10.4028/www.scientific.net/amm.821.325
• 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
• Jee, Craig, and Jason Etele. 2018. “Multi-Objective Optimization of a Supersonic Rocket Based Combined Cycle Inlet through Differential Evolution.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0409. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0409
• Jekabsons, Eriks, Prodyot Basu, N. Khot, and F. Eastep. 2002. “Optimization of an Internal Actuating System for the Enhancement of Wing Flutter Speed.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1424. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1424
• Jenke, Leroy M. 1976. Experimental Roll-Damping, Magnus, and Static-Stability Characteristics of Two Slender Missile Configurations at High Angles of Attack (0 to 90 Deg) and Mach Numbers 0.2 through 2.5. Defense Technical Information Center. https://doi.org/10.21236/ada027027
• Jenkins, J. M. 1984. Effect of Creep in Titanium Alloy Ti-6Al-4V at Elevated Temperature on Aircraft Design and Flight Test. NASA-TM-86033. NASA. https://ntrs.nasa.gov/citations/19840010617
• Jenkins, J. M., R. A. Field, and W. J. Sefic. 1979. “Elevated-Temperature Effects on Strain Gages on the YF-12A Wing: Effect of Slope Changes and Thermal Effects on the Calibrated Strain Gages of the Complex Delta Wing of the Supersonic YF-12A Airplane.” Experimental Mechanics 19 (3): 81–86. https://doi.org/10.1007/bf02324195
• Jenn, A., and H. Nelson. 1988. “Effect of Wing Vertical Position on Lift for Supersonic Delta Wing Missile Configurations.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4381
• Jenquin, Chase, Ethan Johnson, and Venkateswaran Narayanaswamy. 2022. “Effects of Pressure Sensitive Paint on the Dynamics of Half-Inlet Shock Dynamics.” In AIAA SCITECH 2022 Forum. AIAA 2022-0068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0068
• Jeong, Shinkyu, Shigeru Obayashi, Kazuhiro Nakahashi, Toshiyuki Iwamiya, and Kisa Matsushima. 1998. “Supersonic Inverse Design Method for Wing-Fuselage Design.” In Inverse Problems in Engineering Mechanics. Elsevier. https://doi.org/10.1016/b978-008043319-6/50044-3
• “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
• 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
• Ji, Ming, Shao-Hung Lan, and Yi-Chuang Wu. 2026. “Analytical Solution for Supersonic Flutter of Rectangular Thin Plates Using the Superposition-Galerkin Method.” International Journal of Applied Mechanics 18 (04): 2650019. https://doi.org/10.1142/s1758825126500195
• Ji, Xiu Ling, Haipeng Wang, Shi Ming Zeng, and Chen Yang Jia. 2011. “Lateral-Directional Aerodynamics of a Canard Guided Spin Stabilized Projectile at Supersonic Velocity.” Applied Mechanics and Materials 110-116: 4343–50. https://doi.org/10.4028/www.scientific.net/amm.110-116.4343
• Ji Teng and A. Z. Shahneh. 2018. “Design of Landing Gear Shock Absorber Using Magnetorheological Fluid.” In CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2018.0227
• Jia, Zhong Hu, Wei Han, Xiao Hong Zheng, and Yang Tao. 2011. “Analysis of the Arresting Dynamic Loads of Aircraft’s Landing Gear.” Applied Mechanics and Materials 105-107: 470–73. https://doi.org/10.4028/www.scientific.net/amm.105-107.470
• Jia, Li Bin, Lin Li, and Yi Ru. 2013. “Constitutive Analysis to Predict Elevated Temperature Flow Behavior of TC21 Titanium Alloy.” Advanced materials research 811: 152–56. https://doi.org/10.4028/www.scientific.net/amr.811.152
• Jian, Tang, Zhu Ke-Qin, and Tan Guang-Kun. 2004. “A Stationary Vortex Phenomenon above a Low-Aspect-Ratio Wing.” Chinese Physics Letters 21 (2): 352–55. https://doi.org/10.1088/0256-307x/21/2/039
• Jiang, S. 2023. “Precise Forming of Ti60 Alloy by Superplastic Forming /Diffusion Bonding.” In Materials Research Proceedings, vol. 32. Materials Research Forum LLC. https://doi.org/10.21741/9781644902615-8
• Jiang, Shuyong. 2026. “Finite Element Simulation for Superplastic Forming Based on Composite Sheet.” In Plastic Forming and Deformation of Metals Based on Multiscale Simulation. CRC Press. https://doi.org/10.1201/9781003755913-9
• Jiang, Feng, Michael An, and Stephen Mysko. 2000a. “Computational Analysis of Aileron Effectiveness Characteristics on an Advanced Wing.” In 18th Applied Aerodynamics Conference. AIAA 2000-4324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4324
• Jiang, Shuangshuang, M. Garnett, and S.-D. Liu. 2000b. “Springback of Sheet Metal Subjected to Multiple Bending-Unbending Cycles.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2000-01-1112
• Jiang, Hongwei, Zhaohui Yuan, and Yajuan Zhao. 2009. “Research on Flight Test Calibration Strategy Based on Data Fusion.” In Proceedings of the first ACM/SIGEVO Summit on Genetic and Evolutionary Computation. ACM. https://doi.org/10.1145/1543834.1543957
• Jiao, Fujun. 2018. “Oil Damping Energy Loss Analysis of Landing Gear Shock Absorber.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (8): 3096–3106. https://doi.org/10.1177/0954410018793788
• Jin, Hyeon, Jae Ho Lee, Seungheon Yang, and Eunhye Choi. 2025. “An Experimental Study on Internal Drag Correction Methods for a Supersonic Vehicle with a Coaxial Inlet.” Journal of the Korean Society for Aeronautical & Space Sciences 53 (12): 1229–35. https://doi.org/10.5139/jksas.2025.53.12.1229
• Jin, Xia, and Shi Hong Lu. 2010. “3D FEM Simulation and Experimental Research of Springback in Bending Process of Aluminum Alloy Sheet.” In Key engineering materials, vol. 431-432. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.431-432.487
• Jin, Yi, Yue Zhang, Hui-jun Tan, and Hang Yu. 2023b. “Unstart/Restart Boundary Broadening Method for a Two-Dimensional Supersonic Variable Inlet Based on a Distributed Bleed System.” Journal of Aerospace Engineering 36 (1): 04022115. https://doi.org/10.1061/jaeeez.aseng-4615
• Jirasek, Adam, Mats J. Dalenbring, and Jan Navratil. 2016. “Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1551
• Jischke, Martin C. 1978. Supersonic Flow past Conical Bodies with Nearly Circular Cross-Sections. Defense Technical Information Center. https://doi.org/10.21236/ada068004
• Johns, D. J. 1960. “Supersonic Flutter of a Cylindrical Panel in an Axi–Symmetric Mode.” Journal of the Royal Aeronautical Society 64 (594): 362–63. https://doi.org/10.1017/s0368393100072977
• Johns, D. J. 1965. “A Review of Panel Flutter at Low Supersonic Speeds.” Journal of the Royal Aeronautical Society 69 (657): 627–31. https://doi.org/10.1017/s0001924000058759
• Johns, A. L., and F. W. Steffen. 1970. Performance of a Fixed Geometry Wind Tunnel Model of an Auxiliary Inlet Ejector with a Clamshell Flow Diverter from Mach 0 to 1.2. NASA-TM-X-2037. NASA. https://ntrs.nasa.gov/citations/19700023009
• Johnsen, R. L., and R. R. Cullom. 1977. Altitude Test of Several Afterburner Configurations on a Turbofan Engine with a Hydrogen Heater to Simulate an Elevated Turbine Discharge Temperature. NASA-TP-1068. NASA. https://ntrs.nasa.gov/citations/19780003163
• Johnson, C. V. 1934. “The Airplane Landing-Gear Shock-Absorbing System.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/340107
• Johnson, David T. 1972. Evaluation of Energy Maneuverability Procedures in Aircraft Flight Path Optimization and Performance Estimation. Defense Technical Information Center. https://doi.org/10.21236/ad0754909
• Johnson, C. 1980. “A Study of Nonadiabatic Boundary-Layer Stabilization Time in a Cryogenic Tunnel for Typical Wing and Fuselage Models.” In 11th Aerodynamic Testing Conference. AIAA 1980-417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-417
• Johnson, C. B., and J. B. Adcock. 1981. “Measurement of Recovery Temperature on an Airfoil in the Langley 0.3-m Transonic Cryogenic Tunnel.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19810054670
• Johnson, H. J., and E. J. Montoya. 1973. Local Flow Measurements at the Inlet Spike Tip of a Mach 3 Supersonic Cruise Airplane. NASA-TN-D-6987. NASA. https://ntrs.nasa.gov/citations/19730015310
• Johnson, Ethan C., and Venkateswaran Narayanaswamy. 2026. “Investigations of Intermediate Buzz Phenomenon during Streamtraced Inlet Restart.” Physics of Fluids 38 (4): 046103. https://doi.org/10.1063/5.0313906
• 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, J. A., and B. J. C. Wu. 1975. “Pressure Recovery in Supersonic Diffusers.” Journal of Fluids Engineering 97 (3): 374–76. https://doi.org/10.1115/1.3447318
• 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, Joseph A., III, and Benjamin J. Wu. 1974. Pressure Recovery and Related Properties in Supersonic Diffusers: A Review. Defense Technical Information Center. https://doi.org/10.21236/ada017631
• Johnston, D., and J. Hogge. 1974. “The Effect of Non-Symmetric Flight on Aircraft High Angle of Attack Handling Qualities and Departure Characteristics.” In Mechanics and Control of Flight Conference. AIAA 1974-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-792
• Jone, J. B., H. L. McKaig, and John G. Thomas. 1961. Investigation of Ultrasonic Welding of All-Beta Titanium Alloy. Defense Technical Information Center. https://doi.org/10.21236/ad0264117
• Jones, Logan. n.d. “Modeling the Contact Forces between an Aircraft Tire and the Runway.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/8350a83cz0b64z4a57zb574z637ee99b32bc
• 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 T. 1947a. Estimated Lift-Drag Ratios at Supersonic Speed. NACA-TN-1350. NASA. https://ntrs.nasa.gov/citations/19930082051
• Jones, Robert J. 1947b. Wing Plan Forms for High-Speed Flight. NACA-TR-863. NASA. https://ntrs.nasa.gov/citations/19930091936
• Jones, Robert T. 1948. Subsonic Flow over Thin Oblique Airfoils at Zero Lift. NACA-TR-902. NASA. https://ntrs.nasa.gov/citations/19930091969
• Jones, I. W. 1961. Heated Wing Analysis Method Formulas and Details. Defense Technical Information Center. https://doi.org/10.21236/ada377257
• Jones, J. G. 1962. “Quasi-Cylindrical Surfaces with Prescribed Loadings in the Linearized Theory of Supersonic Flow.” Quarterly Journal of Mechanics and Applied Mathematics 15 (4): 471–85. https://doi.org/10.1093/qjmam/15.4.471
• Jones, L. B. 1967a. “The Effects on Wing Lift and Pitching Moment Due to the Fin of an Aircraft Flying at Supersonic Speeds.” Journal of the Royal Aeronautical Society 71 (674): 134–36. https://doi.org/10.1017/s0001924000056232
• Jones, Robert T. 1976b. Leading-Edge Singularities in Thin-Airfoil Theory. Ames Research Center. https://ntrs.nasa.gov/citations/19760012004
• Jones, Robert T. 1976c. The Minimum Drag of Thin Wings in Frictionless Flow. Ames Research Center. https://ntrs.nasa.gov/citations/19760012006
• Jones, R. T. 1976d. Subsonic Flow over Thin Oblique Airfoils at Zero Lift. REPT-902. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19760011998
• Jones, R. T. 1976e. The Use of Conical and Cylindrical Fields in Supersonic Wing Theory. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19760012001
• Jones, R. 1980. “Some Observations on Supersonic Wing Design.” In The evolution of aircraft wing design; Proceedings of the Symposium. AIAA 1980-3040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-3040
• Jones, K. 1983. “Application of a Full Potential Method for Predicting Supersonic Flow Fields and Aerodynamic Characteristics.” In Applied Aerodynamics Conference. AIAA 1983-1802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1802
• Jones, Gregory R. 2011. Titanium Sandwich Airframe Structure. Volume 1: Program Overview. Defense Technical Information Center. https://doi.org/10.21236/ada552062
• Jones, Arthur L., and Alberta Alksne. 1948. The Damping Due to Roll of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow. NACA-TN-1548. NASA. https://ntrs.nasa.gov/citations/19930082350
• Jones, Albert L., and Alberta Alksne. 1949. The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow. NACA-TN-1850. NASA. https://ntrs.nasa.gov/citations/19930082523
• Jones, Arthur L., and Alberta Alksne. 1951. A Summary of Lateral-Stability Derivatives Calculated for Wing Plan Forms in Supersonic Flow. NACA-TR-1052. NASA. https://ntrs.nasa.gov/citations/19930092097
• Jones, R. T., and J. W. Nisbet. 1976. “Aeroelastic Stability and Control of an Oblique Wing.” Aeronautical Journal 80 (788): 365–69. https://doi.org/10.1017/s0001924000034138
• Jones, Arthur L., Robert M. Sorenson, and Elizabeth E. Lindler. 1949. The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow. NACA-TN-1916. NASA. https://ntrs.nasa.gov/citations/19930082594
• Jones, Arthur L., John R. Spreiter, and Alberta Alksne. 1948. The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow. NACA-TN-1700. NASA. https://ntrs.nasa.gov/citations/19930082386
• Jones, George W., Jr. 1957. Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6. NACA-RM-L56L14a. NASA. https://ntrs.nasa.gov/citations/19930089681
• Jones, George W., Jr., and Hugh C. Dubose. 1953. Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms. NACA-RM-L53G10a. NASA. https://ntrs.nasa.gov/citations/19930087626
• Jones, G. W., Jr., and J. R. Unangst. 1963. Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6. NASA-TN-D-1594. NASA. https://ntrs.nasa.gov/citations/19630002604
• 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, 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
• Jorgensen, L. H., and E. D. Katzen. 1956. Wing-Body Combinations with Wings of Very Low Aspect Ratio at Supersonic Speeds. NACA-RM-A56G16. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19660030330
• Joshi, Pranav, Om Kolhatkar, and Prithviraj Ghule. 2024. “An Investigation on the Effect of Changing Bump Geometry on a 2D Supersonic Inlet.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-5752-1_72
• Joshi, D., and W. Rickard. 1981. “Lateral-Directional Flying Qualities of Transport Aircraft.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1887
• Jovanov, Kristofer, and Roeland De Breuker. 2015. “Accelerated Convergence of Static Aeroelasticity Using Low-Fidelity Aerodynamics.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-0175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0175
• Joyner, U. 1969. “Steerable Landing Gear for Vehicles with Main Gear Skids.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-790. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-790
• Ju Min, Kyung, and Ho-Sung Lee. 2015. “Integrated Manufacturing of Aerospace Components by Superplastic Forming Technology.” MATEC Web of Conferences 30: 02003. https://doi.org/10.1051/matecconf/20153002003
• Jukes, R. A. 1970. “The Fatigue Properties of a High Strength Titanium Alloy (IMI.680).” In The Science, Technology and Application of Titanium. Elsevier. https://doi.org/10.1016/b978-0-08-006564-9.50103-2
• Jules, Kenol, and Paul J. Barnhart. 1998. Inlet Performance Analysis Code Developed. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/20050177169
• Jung, Suk Young, Jung Hwa Lee, and Min Gyu Kim. 2015. “Additive Drag Computation of Supersonic Inlet by Numerical Analysis on Inviscid Flow.” Journal of the Korean Society for Aeronautical & Space Sciences 43 (5): 387–95. https://doi.org/10.5139/jksas.2015.43.5.387
• Jung, Timothy P., Steven L. Morris, Jean H. Slane, Robert C. Winn, Steven A. Brandt, and Kara M. Greene. 2021. “Use of Specific Excess Power in Aviation Accident Analysis.” In AIAA Scitech 2021 Forum. AIAA 2021-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1337
• 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
• Kadkhodayan, Mehran�. 2004. “Numerical Prediction of Springback and Side-Wall Curl in U-Bending of Anisotropic Sheet Metals.” In Key engineering materials, vol. 274-276. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.274-276.583
• Kaganovich, I. N., M. V. Efimova, Z. F. Zvereva, Yu. I. Potapenko, and V. K. Kataya. 1982. “Structure of Semifinished Alpha + Beta Titanium Alloy Products.” In Titanium and Titanium Alloys. Springer US. https://doi.org/10.1007/978-1-4757-1758-7_15
• Kahms, Stephanie, and Matthias Wangenheim. 2021. “Experimental Investigation and Simulation of Aircraft Tire Wear.” Tire Science And Technology 49 (1): 55–74. https://doi.org/10.2346/tire.20.180201
• Kahn, S., V. Oskay, and J. Whiteside. 1972. “Verification of Ground Test Data by Instrumented Flight Test of an Artillery Shell.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-979. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-979
• 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
• Kalkhoran, Iraj, Michael Smart, and Alexander Betti. 1995. “Interaction of Supersonic Wing Tip Vortices with a Normal Shock.” In Fluid Dynamics Conference. AIAA 1995-2283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2283
• 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
• Kamal, W., and J. Livesey. 1979. “Diffuser Inlet Flow Structure Following a Shock-Boundary Layer Interaction.” In 4th International Symposium on Air Breathing Engines. AIAA 1979-7026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-7026
• Kamble, Prashant, Avinash Kumar Jha, Jatin Kumar Gola, and Manish Dhawan. 2026. “Design and Dynamic Performance Analysis of Functionalized Carbon Nanotube-Natural Rubber Composites for Aircraft Landing Gear Shock Absorber Disks.” Preprint, . https://doi.org/10.2139/ssrn.7539139
• Kamei, Hidemasa. 1960. “Construction of Turbojet Engine.” Journal of the Society of Mechanical Engineers 63 (503): 1649–55. https://doi.org/10.1299/jsmemag.63.503_1649
• Kamm, Robert W. 1942a. The Effect of Spanwise Mass Distribution upon the Spin Characteristics of Airplanes as Determined by Model Tests Conducted in the Free-Spinning Wind Tunnel. NACA-WR-L-351. NASA. https://ntrs.nasa.gov/citations/19930093630
• Kamm, Robert W. 1942b. Multiengine Airplane Spin Characteristics as Indicated by Model Tests in the Free-Spinning Wind Tunnel. NACA-WR-L-721. NASA. https://ntrs.nasa.gov/citations/19930093685
• Kamm, Robert W. 1945. Spin-Tunnel Tests of Airplane Models with Extreme Variations in Mass Distribution along the Three Body Axes. NACA-ARR-L5C09. NASA. https://ntrs.nasa.gov/citations/19930092697
• Kanamori, Masashi, Osamu Imamura, and Kojiro Suzuki. 2009. “Numerical Analysis on Aerodynamic Characteristics of Delta Wing with Variable Geometry Device in Supersonic Flow.” Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan 7 (ists26): Pe_1-Pe_7. https://doi.org/10.2322/tstj.7.pe_1
• Kandil, Osama A., and H. Andrew Chuang. 1989. Unsteady Navier-Stokes Computations past Oscillating Delta Wing at High Incidence. AIAA PAPER 89-0081. Old Dominion Univ. https://ntrs.nasa.gov/citations/19890037700
• 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 A., and Ahmed A. Salman. 1991. “Unsteady Supersonic Flow around Delta Wings with Symmetric and Asymmetric Flaps Oscillation.” In AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. https://ntrs.nasa.gov/citations/19910047398
• Kaneko, R. S., G. W. Davis, C. A. Woods, and D. M. Royster. 1982. Low Cost Fabrication of Sheet Structure Using a New Beta Titanium Alloy, Ti-15V-3Cr-3Al-3Sn. Lockheed-California Co. https://ntrs.nasa.gov/citations/19830039251
• Kaneko, R. S., and C. A. Woods. 1983. Low-Temperature Forming of Beta Titanium Alloys. NASA-CR-3706. NASA. https://ntrs.nasa.gov/citations/19840003185
• Kang, Byung-Hyuk, Bang-Hyun Jo, Bo-Gyu Kim, Jai-Hyuk Hwang, and Seung-Bok Choi. 2023b. “Linear and Nonlinear Models for Drop Simulation of Aircraft Landing Gear System with MR Dampers.” Preprint, . https://doi.org/10.20944/preprints202305.1795.v1
• Kang, Byung-Hyuk, Bo-Gyu Kim, and Seung-Bok Choi. 2023a. “Aircraft Landing Gear System with Magnetorheological Shock Strut: Performance Evaluation via Drop Test.” Journal of Intelligent Material Systems and Structures 34 (13): 1471–85. https://doi.org/10.1177/1045389x221147632
• Kanneganti, Girish Kumar Chowdary, Bhaskar Charan, Vesapogu Chandrakala, and V. Varun. 2022. “Effect of Anhedral and Dihedral on the Lateral Directional Static Stability of the Aircraft.” Graduate Research in Engineering and Technology: 44–51. https://doi.org/10.47893/gret.2022.1085
• 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
• Kansas Univ Lawrence. 1952a. Launching and Landing of Carrier Aircraft. Part 3. a Multi-Jet Driven Catapult (Hydrapult). Defense Technical Information Center. https://doi.org/10.21236/ad0009895
• Kansas Univ Lawrence. 1952b. The Launching and Landing of Carrier Aircraft. Part 4. Barricades. Defense Technical Information Center. https://doi.org/10.21236/ad0021570
• Kaplan, Mp, Ja Reiman, and Ma Landy. 1979. “Derivation of Flight-by-Flight Spectra for Fighter Aircraft.” In Service Fatigue Loads Monitoring, Simulation, and Analysis. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp35873s
• Kapoor, Kamlesh, Bernhard H. Anderson, and Robert J. Shaw. 1994. A Full Navier-Stokes Analysis of Subsonic Diffuser of a Bifurcated 70/30 Supersonic Inlet for High Speed Civil Transport Application. NASA-TM-106637. NASA. https://ntrs.nasa.gov/citations/19950004408
• Karania, Sameer, Manu Mohan, and Satya Prakash. 2021. “Diverterless Supersonic Intake for a Generic Stealth Fighter Aircraft.” In Lecture Notes in Mechanical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-9601-8_38
• Karaselvi, Emre, and Melike Nikbay. 2021. “Implementation of Propulsion System Integration Losses to a Supersonic Military Aircraft Conceptual Design.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3551
• Karpouzian, G., and L. Librescu. 1992. “The Equations Governing the Motion of Wing-Aileron Structural Systems Constructed from Advanced Anisotropic Composite Materials.” In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2469. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2469
• Karpouzian, G., and E. Librescu. 1993. “Exact Flutter Solution of Advanced Anisotropic Composite Cantilevered Wing Structures.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1535. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1535
• Karunanidhi, Karthik, Mohanraj Manoharan, and Sathish Rajamanickam. 2025. “An Aircraft Hydraulic Brake System Model Analysis Using LMS Amesim Tool.” Applied Engineering 9 (1): 9–36. https://doi.org/10.11648/j.ae.20250901.12
• Kase, Masataka, Makoto Mizoguchi, and Hajime Itoh. 2020. “PIV Flow Visualization around Low Aspect Ratio Wing at Low Reynolds Numbers.” Proceedings of Mechanical Engineering Congress, Japan 2020 (0): S05403. https://doi.org/10.1299/jsmemecj.2020.s05403
• Kassem, H. I., and J. R. Banerjee. 2015. “Transonic Speed Flutter Analysis of a Rectangular Wing Using the OpenFOAM Computational Fluid Dynamics Code and the Dynamic Stiffness Method.” Civil-comp proceedings. https://doi.org/10.4203/ccp.108.110
• Katary, M. 1983. “An Experimental Study of the Development of a Supersonic Zone near the Leading Edge of an Airfoil Oscillating in Subsonic Flow.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2133
• Kaushik, Mrinal. 2018. “Thin Airfoil Theory.” In Theoretical and Experimental Aerodynamics. Springer Singapore. https://doi.org/10.1007/978-981-13-1678-4_5
• 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
• Kawamura, T., W. Chyu, and D. Bencze. 1987. “Numerical Simulation of Three-Dimensional Supersonic Inlet Flow Fields.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-160
• Kawamura, Ryuma, and Keiichi Karashima. 1957. “On the Wave Drag of Wing-Body Combination Moving at Supersonic Speeds.” Journal of the Japan Society of Aeronautical Engineering 5 (39): 93–99. https://doi.org/10.2322/jjsass1953.5.93
• Kawazoe, Hiromitsu, and Susumu Kato. 2005. “Effects of Leading Edge Separation Vortex of Flexible Structure Delta Wing on Its Aerodynamic Characteristics(Wing and Airfoil).” Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (0): 583–89. https://doi.org/10.1299/jsmeicjwsf.2005.583
• Kaynak, U., T. Holst, R. Sorenson, and B. Cantwell. 1986. “Numerical Simulation of Transonic Separated Flows over Low-Aspect Ratio Wings.” In 24th Aerospace Sciences Meeting. AIAA 1986-508. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-508
• 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
• Kazula, Stefan, and Klaus Höschler. 2020a. “Evaluation of Variable Pitot Inlet Concepts for Transonic and Supersonic Civil Aviation.” Aircraft Engineering and Aerospace Technology 92 (6): 807–15. https://doi.org/10.1108/aeat-11-2019-0225
• Kazula, Stefan, and Klaus Höschler. 2020b. “A Variable Pitot-Inlet Concept for Supersonic Aviation.” In Proceedings of Global Power & Propulsion Society. GPPS. https://doi.org/10.33737/gpps20-tc-49
• Kazula, Stefan, Marcel Mischke, Paul König, and Klaus Höschler. 2019a. “Evaluation of Variable Pitot Inlet Concepts for Transonic and Supersonic Civil Aviation.” MATEC Web of Conferences 304: 02016. https://doi.org/10.1051/matecconf/201930402016
• Kazula, Stefan, Mark Wöllner, David Grasselt, and Klaus Höschler. 2019b. “Parametric Design Study on Aerodynamic Characteristics of Variable Pitot Inlets for Transonic and Supersonic Civil Aviation.” MATEC Web of Conferences 304: 02017. https://doi.org/10.1051/matecconf/201930402017
• Kędzierski, Piotr, and Arkadiusz Popławski. 2019. “Development of Test Device for Springback Study in Sheet Metal Bending Operation.” In AIP Conference Proceedings, vol. 2078. Author(s). https://doi.org/10.1063/1.5092019
• Keenan, James A., and John M. Kuhlman. 1991a. “The Effects of Winglets on Low Aspect Ratio Wings at Supersonic Mach Numbers.” PhD diss., West Virginia Univ.. https://ntrs.nasa.gov/citations/19920004778
• Keenan, J., and J. Kuhlman. 1991b. “Winglet Effectiveness on Low Aspect Ratio Wings at Supersonic Mach Numbers.” In 9th Applied Aerodynamics Conference. AIAA 1991-3305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3305
• 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
• Keener, Earl R., and Gareth H. Jordan. 1956. Wing Loads and Load Distributions throughout the Lift Range of the Douglas X-3 Research Airplane at Transonic Speeds. NACA-RM-H56G13. NASA. https://ntrs.nasa.gov/citations/19930090104
• Keener, Earl R., Norman J. McLeod, and Norman V. Taillon. 1958. Effect of Leading-Edge-Flap Deflection on the Wing Loads, Load Distributions, and Flap Hinge Moments of the Douglas X-3 Research Airplane at Transonic Speeds. NACA-RM-H58D29. NASA. https://ntrs.nasa.gov/citations/19930090188
• Keerthana, M., and P. Harikrishna. 2014. “Improved ERA Based Identification of Flutter Derivatives of a Thin Plate.” In Advances in Structural Engineering. Springer India. https://doi.org/10.1007/978-81-322-2193-7_110
• 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
• Kehoe, Michael W. 1987. “Aircraft Ground Vibration Testing at NASA Ames-Dryden Flight Research Facility.” In International Modal Analysis Conference. https://ntrs.nasa.gov/citations/19880063604
• 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
• Kehrer, William. 1964. “Longitudinal Stability and Control of Large Supersonic Aircraft at Low Speeds.” In International Council of the Aeronautical Sciences. AIAA 1964-586. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-586
• Kehrer, W. 1971. “The Performance Benefits Derived for the Supersonic Transport Througha New Approach to Stability Augmentation.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-785
• Keith, Arvid L., Jr. 1957. Transonic Investigation of Internal-Flow Characteristics of a Square-Shaped Scoop Inlet Mounted at Three Chordwise Positions above a High 45 Degree Sweptback Wing and Body Combination. NACA-RM-L57A29. NASA. https://ntrs.nasa.gov/citations/19930089512
• Keller, Jeffrey, Robert McKillip, and Sungwan Kim. 2009. “Aircraft Flight Envelope Determination Using Upset Detection and Physical Modeling Methods.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6259
• Kelley, Amanda, Richard L. Newman, Ben D. Lawson, and Angus H. Rupert. 2014. “A Materiel Solution to Aircraft Upset.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-0445. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0445
• 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., W. H. Dana, and A. G. Sim. 1975. Flight Evaluation of the M2-F3 Lifting Body Handling Qualities at Mach Numbers from 0.30 to 1.61. NASA-TN-D-8027. NASA. https://ntrs.nasa.gov/citations/19750018943
• Kempel, Robert W., Walter E. McNeill, Glenn B. Gilyard, and Trindel A. Maine. 1988b. A Piloted Evaluation of an Oblique-Wing Research Aircraft Motion Simulation with Decoupling Control Laws. NASA-TP-2874. NASA. https://ntrs.nasa.gov/citations/19890006559
• Kempel, Robert W., Walter E. McNeill, and Trindel A. Maine. 1988a. Oblique-Wing Research Airplane Motion Simulation with Decoupling Control Laws. AIAA PAPER 88-0402. PRC Kentron, Inc. https://ntrs.nasa.gov/citations/19880035069
• Kenger, Arthur, and George Leavy. 1955. Development and Fabrication of the F-80C Magnesium Alloy Airframe. Defense Technical Information Center. https://doi.org/10.21236/ad0097491
• Kennon, Stephen. 1989. “Supersonic Inlet Calculations Using an Upwind Finite-Volume Method on Adaptive Unstructured Grids.” In 27th Aerospace Sciences Meeting. AIAA 1989-113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-113
• Kepler, C. Edward, and Frank W. Barry. 1965. “Engine Air Inlet Compatibility for the Supersonic Transport.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/650225
• Keppler, C. R. 1966. Perforations in Jet Engine Supersonic Inlet Increase Shock Stability. NEO-8. NASA. https://ntrs.nasa.gov/citations/19660000528
• Kerlick, G. 1985. “Adaptive Mesh Solution for Supersonic Conical Flow in a Rectilinear Inlet.” In 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. AIAA 1985-1626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1626
• Keys, R. D., T. F. Kiefer, and F. R. Schwartzberg. 1965. Fatigue Behavior of Aluminum and Titanium Sheet Materials down to -423 Deg f. NASA. https://ntrs.nasa.gov/citations/19650049380
• Khademi, V., M. Ikeda, D. Hernández-Escobar, and C. J. Boehlert. 2019. “The Elevated-Temperature Strength Enhancement of a Low-Cost β Titanium Alloy through Thermomechanically-Induced Phase Transformation.” JOM 71 (10): 3621–30. https://doi.org/10.1007/s11837-019-03598-2
• Khalid, S. 1989. “Role of Dynamic Simulation in Fighter Engine Design and Development.” In 25th Joint Propulsion Conference. AIAA 1989-2467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2467
• Khan, Akhtar S. 2006. Dynamic Multi-Axial Loading Response and Constitutive/Damage Modeling of Titanium and Titanium Alloys. Defense Technical Information Center. https://doi.org/10.21236/ada455627
• Khan, Md. Raihan Ali, and A. B. M. Toufique Hasan. 2019. “Effect of Geometric Modification on Flow and Performance Characteristics of a Supersonic Inlet Isolator.” In International Symposium on Shock Waves (ISSW). https://doi.org/10.3850/978-981-11-2730-4_0377-cd
• Khan, Mohd. Shahid, Kasturi Rangan Madabushi, Santanu Ghosh, Jack Edwards, and Venkateswaran Narayanaswamy. 2024. “Numerical Investigations of Shock/Boundary-Layer Interaction and Control for Mach 2.5 Flow in an Axisymmetric Inlet.” Preprint, . https://doi.org/10.2139/ssrn.4750680
• Khan, Kamrul Hasan, Wrik Mallik, Rakesh K. Kapania, and Joseph A. Schetz. 2021. “Distributed Design Optimization of Large Aspect Ratio Wing Aircraft with Rapid Transonic Flutter Analysis in Linux.” In AIAA Scitech 2021 Forum. AIAA 2021-1354. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1354
• Khan, Tauha I., Jehanzeb Masud, Zakria G. Toor, and Bilal Mufti. 2019. “Analysis of High Alpha Aerodynamic Characteristics of a Supersonic Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-2307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2307
• Khan, Hassan N., Jehanzeb Masud, Usman Zia, and Muhammad Muneeb Safdar. 2025b. “Investigation for Reduction of Wave Drag through Design and Analysis of Supersonic Fuel Tanks.” In AIAA SCITECH 2025 Forum. AIAA 2025-1051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1051
• Khan, Sher Afghan, Javed Shoukat Shaikh, Krishna Kumar, Khizar Ahmed Pathan, and Fayaz Husain Kharadi. 2025a. “Estimation of the Damping Derivative in Pitch for a Wedge at Supersonic Mach Numbers Using Design of Experiments.” Journal of Advanced Research in Experimental Fluid Mechanics and Heat Transfer 18 (1): 106–17. https://doi.org/10.37934/arefmht.18.1.106117
• Khan, Mohd S., Jatinder Pal Singh Sandhu, Santanu Ghosh, and Jack R. Edwards. 2023. “Numerical Investigations of Shock/Boundary-Layer Interaction Control for a Mach 2.5 Flow in an Axisymmetric Inlet.” In AIAA SCITECH 2023 Forum. AIAA 2023-1576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1576
• Khan, Md. Raihan Ali, Shadman Tahmid, and A. B. M. Toufique Hasan. 2018. “Control of Shock/boundary-Layer Interactions in a Supersonic Inlet Isolator Using Geometric Modification.” In AIP Conference Proceedings, vol. 1983. Author(s). https://doi.org/10.1063/1.5044323
• Khandelwal, Suresh C., Gary Cole, and Joongkee Chung. 1996. “Parallel Computation of Unsteady Supersonic-Inlet Flows.” In Parallel Computational Fluid Dynamics 1995. Elsevier. https://doi.org/10.1016/b978-044482322-9/50138-9
• Khanna, Navneet, and Chetan Agrawal. 2019. “Titanium Machining Using Indigenously Developed Sustainable Cryogenic Machining Facility.” In Materials Forming, Machining and Tribology. Springer International Publishing. https://doi.org/10.1007/978-3-030-18854-2_8
• Kharsansky Atallah, Ivan. n.d. “Low Frequency Dynamics and Coherent Flow Structures on a Thin Airfoil at Stall.” PhD diss., Institut polytechnique de Paris. https://doi.org/10.70675/8fd76227zb1c9z4d53zb017zf38ece464c54
• Khatri, Amit K., Jatinder Singh, and Nandan K. Sinha. 2013. “Aircraft Design Using Constrained Bifurcation and Continuation Method.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-5079. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5079
• Khleif, Ali Abbar, Lujain H. Kashkool, and O. H. Hassoon. 2020. “Experimental Investigation of Hold Time Effect on Springback in V-Bending Sheet Metal Forming Process.” IOP Conference Series: Materials Science and Engineering 881 (1): 012071. https://doi.org/10.1088/1757-899x/881/1/012071
• Khot, N., K. Appa, J. Ausman, and F. Eastep. 1998a. “Deformation of a Flexible Wing Using an Actuating System for a Rolling Maneuver without Ailerons.” In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1998-1802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1802
• Khot, N., K. Appa, and F. Eastep. 1998b. “Optimization of a Flexible Wing without Ailerons for the Rolling Maneuver.” In 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 1998-4886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4886
• Khot, N., K. Appa, and F. Eastep. 1999a. “Actuating System for Enhancement of Rolling Maneuver of a Wing with Ailerons.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1397
• Khot, N., F. Eastep, and R. Kolonay. 1996b. “Optimization of a Composite Wing Structure for Enhancement of the Rolling Maneuver.” In 6th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1996-3998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3998
• Khot, N., F. Eastep, R. Kolonay, N. Khot, F. Eastep, and R. Kolonay. 1997b. “Wing Twist and Camber for the Rolling Maneuver of a Flexible Wing without Aileron.” In 38th Structures, Structural Dynamics, and Materials Conference. AIAA 1997-1268. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1268
• Khot, Narendra, Raymond Kolonay, and Frank Eastep. 1996a. “A Method for Enhancement of the Rolling Maneuver of a Flexible Wing.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1391
• Khudadad, Ahmed Rahman, Safaa Kadhim Ghazi, Rasool R. K. Al-Arkawazi, Mudhar Abdul Alwahab Al-Obaidi, and Mostafa Adel Abdullah. 2025. “Comparative Study of Springback in Different Sheet Metal Alloys and Thicknesses in V-Shaped Bending Process.” Applied Mechanics and Materials 928: 3–9. https://doi.org/10.4028/p-rlc8bw
• Ki, Dock, and Yoon Lee. 1998. “An Experimental Study on the Intake Boundary Layer Diverter Heights for Transonic Aircraft.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3581
• 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
• Kier, Thiemo. 2005. “Comparison of Unsteady Aerodynamic Modelling Methodologies with Respect to Flight Loads Analysis.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6027
• Kikuchi, Ryoya, Toma Miyake, Satoshi Kuruhara, and Hiroshi Terashima. 2026. “Transonic Flutter Prediction for a Benchmark Supercritical Wing at High Angles of Attack.” In AIAA AVIATION 2026 Forum. AIAA 2026-4526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4526
• Kim, David. 1999. “General Aviation Aircraft Empennage Flight Loads.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/1999-01-1573
• Kim, H. Y. 2007. “Experiments for Forming Limit Diagram and Springback Characteristics of AZ31B Magnesium Alloy Sheet at Elevated Temperature.” Transactions of Materials Processing 16 (5): 364–69. https://doi.org/10.5228/kspp.2007.16.5.364
• Kim, Matteo. 2023. “Artificial Runway Design for Shimmy Testing on Nose Landing Gear.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/24625116
• Kim, H. H., and C. G. Kang. 2011. “The Effect of Die Curvature and Material Anisotropy in u-Bending of AZ31 Magnesium Alloy Sheet on Springback.” In Engineering Plasticity and Its Applications. WORLD SCIENTIFIC. https://doi.org/10.1142/9789814324052_0061
• Kim, Hyun-gi, Sung-Chan Kim, Byung-geon Ha, and Su-hong An. 2024. “Test Fixture and Error Analysis for Measuring Mass Moment of Inertia for Aircraft External Fuel Tank.” Journal of the Korea Academia-Industrial cooperation Society 25 (7): 356–62. https://doi.org/10.5762/kais.2024.25.7.356
• Kim, Y., J. Kim, Y. Jeon, et al. 2002a. “Multidisciplinary Aerodynamic-Structural Design Optimization of Supersonic Fighter Wing Using Response Surface Methodology.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-322. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-322
• Kim, Eung-tai, Yeong-cheol Kim, Kie-jeong Seong, Myoung-shin Hwang, and Hee-bong Eun. 2003a. “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, Hyoung Jin, Takayasu Kumano, Meng-Sing Liou, and Louis Povinelli. 2011b. “Optimal Bypass Shape Design of Low Boom Supersonic Inlet.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3191. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3191
• Kim, Dong-Hyun, and In Lee. 2001. “Transonic and Supersonic Flutter Characteristics of a Wing-Box Model with Tip Stores.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-1464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1464
• Kim, Dong-Hyun, In Lee, Taehyoun Kim, James Lee, and William Moon. 2003b. “Transonic/Supersonic Aeroelastic Instability of an All Movable Wing with Structural Nonlinearity.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1412
• Kim, Yushin, Dong-Ho Lee, Yonghyup Kim, and Kwanjung Yee. 2002b. “Multidisciplinary Design Optimization of Supersonic Fighter Wing Using Response Surface Methodology.” In 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 2002-5408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5408
• Kim, David, and Maciej Marciniak. 1998. “Prediction of Vertical Tail Maneuver Loads Using Backpropagation Neural Networks.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4259
• Kim, E. C., and S. H. Park. 2026. “Flow Separation Suppression of Swept Shock Wave-Boundary Layer Interaction by Using Bleed Slots over Supersonic Inlet Sidewall.” Journal of computational fluids engineering 31 (2): 84–103. https://doi.org/10.6112/kscfe.2026.31.2.084
• 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
• Kimble, K., S. Ruo, J. Wu, and D. Liu. 1973. “Unsteady Transonic Flow Analysis for Low Aspect Ratio, Pointed Wings.” In 11th Aerospace Sciences Meeting. AIAA 1973-122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-122
• King, E. J. 1962. Short Time Tensile and Creep Properties of Commercially Pure Titanium and Three Titanium Alloys. Defense Technical Information Center. https://doi.org/10.21236/ad0296199
• 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. 1975. “Joint USAF/NASA Hypersonic Research Aircraft Study.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750055459
• Kirschbaum, H. W. 1936. Estimation of Moments of Inertia of Airplanes from Design Data. NACA-TN-575. NASA. https://ntrs.nasa.gov/citations/19930081330
• Kishawy, Hossam A., and Ali Hosseini. 2018. “Titanium and Titanium Alloys.” In Materials Forming, Machining and Tribology. Springer International Publishing. https://doi.org/10.1007/978-3-319-95966-5_3
• Kishi, Y., Masahiro Kanazaki, Yoshikazu Makino, and Kisa Matsushima. 2016. “Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic.” Journal of Flow Control Measurement & Visualization 04 (01): 38–48. https://doi.org/10.4236/jfcmv.2016.41004
• Kishi, Yuki, Shinya Kitazaki, Atthaphon Ariyarit, Yoshikazu Makino, and Masahiro Kanazaki. 2017. “Planform Dependency of Optimum Supersonic Airfoil for Wing-Body-Nacelle Configuration Using Multi-Fidelity Design Optimization.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-4468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4468
• Kislov, Oleh, and Mykhailo Shevchenko. 2021. “Development of a Method for Selecting a Cruising Mode and Engine Control Program of a Ramjet Aircraft.” Eastern-European Journal of Enterprise Technologies 3 (3 (111)): 6–14. https://doi.org/10.15587/1729-4061.2021.233850
• Kitowski, J. 1992a. “Combat Effectiveness Methodology as a Tool for Conceptual Fighter Design.” In Aerospace Design Conference. AIAA 1992-1197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1197
• Kitowski, J. 1992b. “Fighter Airframe/propulsion Integration: A General Dynamics Perspective.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3332
• Klaus, Leonard. 2017. “Comparison of Two Experiments Based on a Physical and a Torsion Pendulum to Determine the Mass Moment of Inertia Including Measurement Uncertainties.” Measurement Science Review 17 (1): 9–18. https://doi.org/10.1515/msr-2017-0002
• 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, 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, and Patrick Murphy. 2001. “Estimation of Aircraft Unsteady Aerodynamic Parameters from Dynamic Wind Tunnel Testing.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4016. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4016
• 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
• Klepper, Jason B., James R. Sirbaugh, and Milt W. Davis. 2017. “Dynamic Inlet Simulation Demonstration for Airframe-Propulsion Integration Using HPCMP CREATE™-AV Kestrel.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2017-63072
• Klinar, Walter J. 1946. Free-Spinning Tunnel Tests of a 1/20-Scale Model of the Chance Vought XF6U-1 Airplane, TED No. NACA 2390. NACA-RM-L6H27. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019259
• Klinar, Walter J. 1947. Supplementary Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the McDonnell XB-85 Airplane Equipped with a Conventional-Tail Arrangement. NACA-RM-l7I11. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019298
• Klinar, Walter J., and Theodore Berman. 1948. Spin Tests of 1/20-Scale Models of the Chance Vought Revised XF6U-1 and F6U-1 Airplanes, TED No. NACA 2390. NACA-RM-SL8F03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028620
• Klinar, Walter J., and Lawrence J. Gale. 1949. Wind-Tunnel Investigation of the Spinning Characteristics of a Model of a Twin-Tail Low-Wing Personal-Owner-Type Airplane with Linked and Unlinked Rudder and Aileron Controls. NACA-TN-1801. NASA. https://ntrs.nasa.gov/citations/19930082476
• Klinar, Walter J., and Frederick M. Healy. 1952. Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman F9F-6 Airplane TED No. NACA DE 364. NACA-RM-SL52G03A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029457
• Klinar, Walter J., and Frederick M. Healy. 1955. Free-Spinning-Tunnel Investigation of a 0.034-Scale Model of the Production Version of the Chance Vought F7U-3 Airplane, TED No. NACA AD 3103. NACA-RM-SL55G15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030056
• Klinar, Walter J., and Ira P. Jones Jr. 1949. Spin Investigation of a 1/29-Scale Model of the Republic XF-91 Airplane with a Conventional Tail Installed. NACA-RM-SL9E20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030060
• Klinar, Walter J., and Henry A. Lee. 1953. Free-Spinning-Tunnel Investigation of a Model Having a 60 Degrees Delta Wing with Half-Delta Ailerons Installed. NACA-RM-L52K24a. NASA. https://ntrs.nasa.gov/citations/19930087409
• Klinar, Walter J., and Henry A. Lee. 1954. Supplementary Investigation in the Free-Spinning Tunnel of a 1/24-Scale Model of the Grumman F9F-6 Airplane Incorporating Only Flaperons for Lateral Control, TED No. NACA DE 364. NACA-RM-SL54L01a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029445
• Klinar, Walter J., and Henry A. Lee. 1955. Supplementary Investigation in the Langley Free-Spinning Tunnel of a 1/20-Scale Model of the Douglas XF4D-1 Airplane Including Spin-Recovery Parachute Tests of the Model Loaded to Simulate the Douglas F5D-1 Airplane. Rept-5269. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030045
• Klinar, Walter J., and Thomas L. Snyder. 1948. Influence of Tail Length upon the Spin-Recovery Characteristics of a Trainer-Type-Airplane Model. NACA-TN-1764. NASA. https://ntrs.nasa.gov/citations/19930082437
• Klinar, Walter J., and Jack H. Wilson. 1950. Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman AF-2S, -2W Airplane. NACA-RM-SL51B20. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029448
• Klinar, Walter J., and Jack H. Wilson. 1951. Spin-Tunnel Investigation of the Effects of Mass and Dimensional Variations on the Spinning Characteristics of a Low-Wing Single-Vertical-Tail Model Typical of Personal-Owner Airplanes. NACA-TN-2352. NASA. https://ntrs.nasa.gov/citations/19930083028
• 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
• Klopfer, Goetz H., and Jack N. Nielsen. 1979. Basic Studies of Wing-Body Interference at High Angles of Attack and Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada087134
• Klopfer, G., and J. Nielsen. 1980. “Euler Solutions for Wing and Wing-Body Combination at Supersonic Speeds with Leading-Edge Separation.” In 18th Aerospace Sciences Meeting. AIAA 1980-126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-126
• Klyde, David, Bimal Aponso, David Mitchell, and Roger Hoh. 1995. “Development of Roll Attitude Quickness Criteria for Fighter Aircraft.” In Guidance, Navigation, and Control Conference. AIAA 1995-3205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3205
• Klyde, David, Chuck Harris, Peter M. Thompson, and Edward N. Bachelder. 2004. System Identification Methods for Improving Flutter Flight Test Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada426452
• Knight, Montgomery. 1928. Wind Tunnel Tests on Autorotation and the “Flat Spin.”. NACA-TR-273. NASA. https://ntrs.nasa.gov/citations/19930091341
• 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
• 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, 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
• Kobryn, Pamela A. 1996. Casting of Titanium Alloys. Defense Technical Information Center. https://doi.org/10.21236/ada312008
• Kochendorfer, Fred D. 1953. Investigation at a Mach Number of 1.90 of a Diverter-Type Boundary-Layer Removal System for a Scoop Inlet. NACA-RM-E53D07. NASA. https://ntrs.nasa.gov/citations/19930087800
• Kochin, N. E. 1953. Steady Vibrations of Wing of Circular Plan Form. NACA-TM-1324. NASA. https://ntrs.nasa.gov/citations/19930093906
• Kodera, Masatoshi, Takeshi Kanda, and Kouichiro Tani. 2000. “Effect of Airframe Geometry on Thrust Performance of Aerospace Plane.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3342. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3342
• Kodigaddi, Siddalingappa P. 2026. “Time-Domain Two-Way Fluid–Structure Interaction Analysis of the HIRENASD Transonic Wing: Static Aeroelastic Response and Flutter Prediction.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-10227402/v1
• 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
• Kolesnikov, Evgeny, and Mikhail Goman. 2012. “Analysis of Aircraft Nonlinear Dynamics Using Non-Gradient Based Numerical Methods and Attainable Equilibrium Sets.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4406
• 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
• Kondetimmanahalli, Ramamohan. n.d. “Springback of Sheet Metals in Fabrication of Miniature Components.” PhD diss., Drexel University. https://doi.org/10.17918/00009424
• Kong, Yakang, Jun Li, Hua Liang, and Shanguang Guo. 2022. “Experimental Study on the Dynamic Characteristics and Surface Arc Plasma Control of Shock Train in the Supersonic Inlet.” Journal of Aerospace Engineering 35 (5): 04022077. https://doi.org/10.1061/(asce)as.1943-5525.0001470
• 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
• Kopasakis, George, and Joseph Connolly. 2009. “Shock Positioning Controls Design for a Supersonic Inlet.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5117
• Koppenhofer, R. L., W. J. Lewis, G. E. Faulkner, and P. J. Rieppel. 1961. Development of Procedures for Welding 2-INCH-THICK Titanium-Alloy Plate. Defense Technical Information Center. https://doi.org/10.21236/ad0258855
• Kordes, E. E., and J. M. McKay. 1961. Landing Loads an Dynamics of the X-15 Airplane. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19710070134
• Kordes, E. E., and J. M. McKay. 1962. Landing Loads and Dynamics of the X-15 Airplane. NASA-TM-X-639. NASA. https://ntrs.nasa.gov/citations/19630002688
• Kornecki, A. 1964. “A Note on the Supersonic Panel Flutter of Oblique Clamped Plates.” Journal of the Royal Aeronautical Society 68 (640): 270–71. https://doi.org/10.1017/s0001924000060929
• Korner, Lars, and Hengan Ou. 2025. “Investigation of Frictional Behaviour in Incremental Sheet Forming of Grade One Titanium Sheet.” MATEC Web of Conferences 408: 01036. https://doi.org/10.1051/matecconf/202540801036
• 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
• Korr, A. L., and Paul Hyer. 1962. A Trifilar Pendulum for the Determination Moments of Inertia. Defense Technical Information Center. https://doi.org/10.21236/ad0287534
• Kostić, Čedomir J., Boško P. Rašuo, and Aleksandar M. Janković. 2015. “Flying Spin Qualities Testing of Airplane.” Tehnika 70 (5): 789–803. https://doi.org/10.5937/tehnika1505789k
• Kotov, M. A., L. B. Ruleva, S. I. Solodovnikov, and S. T. Surzhikov. 2018. “Preliminary Experimental Assessment of Supersonic Airflow Behavior over ExoMars and X–43 Inlet Models Using Multiple Flow Regime Shock Tube.” Journal of Physics: Conference Series 1009: 012038. https://doi.org/10.1088/1742-6596/1009/1/012038
• Kouyoumjian, W. L. 1957. Preliminary Wind-Tunnel Investigation of the Performance of Republic F-105 Wing-Root Inlet Configurations at Various Angles of Attack and a Mach Number of 2.01. NACA-RM-SL56L12. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19660082192
• Kowalska, Anna, and Tomasz Goetzendorf-Grabowski. 2022. “Impact of the Aileron Gap Sealing on the Aileron Effectiveness.” Aircraft Engineering and Aerospace Technology 95 (1): 26–37. https://doi.org/10.1108/aeat-01-2022-0001
• Kraft, David C., Henry Luming, and J. R. Hoppenjans. 1971. Multiwheel Landing Gear-Soils Interaction and Flotation Criteria: Phase 3, Part 1. Defense Technical Information Center. https://doi.org/10.21236/ad0885275
• 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
• Kranz, M. 1954. Drop Hammer Tests with Three Oleo Strut Models and Three Different Shock Strut Oils at Low Temperatures. NACA-TM-1372. NASA. https://ntrs.nasa.gov/citations/19930093858
• Krasilschchikova, E. A. 1956. Finite Span Wings in Compressible Flow. NACA-TM-1383. NASA. https://ntrs.nasa.gov/citations/19930093847
• Krause, Helmut, and Dieter Dinkler. 1998. “The Influence of Curvature on Supersonic Panel Flutter.” In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1998-1841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1841
• Kremer, K. L., R. J. Lord, and R. J. Roehrs. 1973. “Ultrasonic Inspection of Titanium Airframe Components.” In Titanium Science and Technology. Springer US. https://doi.org/10.1007/978-1-4757-1346-6_52
• Kremzier, Emil J., and Robert C. Campbell. 1954. Angle-of-Attack-Supersonic Performance of a Configuration Consisting of a Ramp-Type Scoop Inlet Located Either on Top or Bottom of a Body of Revolution. NACA-RM-E54C09. NASA. https://ntrs.nasa.gov/citations/19930088174
• Kremzier, Emil J., and George A. Wise. 1955. Effect of Centerbody Boundary-Layer Removal near the Throat of Three Coniccal Nose Inlets at Mach 1.6 to 2.0. NACA-RM-E55H16a. NASA. https://ntrs.nasa.gov/citations/19930089080
• Krieger, R. 1980. “A Technique for Developing Low Drag Nose Shapes for Advanced Supersonic Missile Concepts.” In 18th Aerospace Sciences Meeting. AIAA 1980-361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-361
• 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
• Kroll, Wilhelmina D. 1956. Landing Gear Loads Resulting from Taxying Airplane over a Projecting Runway Light:: Progress Report 1. National Bureau of Standards. https://doi.org/10.6028/nbs.rpt.4574
• Kroll, Wilhelmina D. 1957. Landing Gear Loads Resulting from Taxying an Airplane over a Projecting Runway Light:: Progress Report 2. National Bureau of Standards. https://doi.org/10.6028/nbs.rpt.5641
• Kroo, I. 1986. “The Aerodynamic Design of Oblique Wing Aircraft.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2624. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2624
• Kruggel, Benjamin, Asher Sigal, Bob Whyte, and Wayne Hathaway. 1999. “High Angle of Attack Free Flight Missile Testing.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-435. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-435
• 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
• Küçük, Umut C., Özgür U. Baran, and Oguz Uzol. 2015. “Passive Flow Control in Boundary Layer Ingesting Semi Submerged Inlet.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3803
• Kucuk, Umut Can, and Ismail Hakki Tuncer. 2023. “Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets.” In AIAA AVIATION 2023 Forum. AIAA 2023-4085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4085
• Kudryavtsev, B. Y. 2014. “Plate Thickness’ Distribution Optimization Problem in Panel Flutter Case Analysis.” Izvestiya MGTU MAMI 4 (1–4): 77–82. https://doi.org/10.17816/2074-0530-67451
• 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
• Kuester, Matthew S., Aurelien Borgoltz, and William J. Devenport. 2016. “Pressure Tap Effects on the Lift Measurement of an Airfoil Section.” In 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2016-3654. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3654
• 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
• Kuhlman, John, and Christopher Brown. 1989. “Computational Design of Low Aspect Ratio Wing-Winglets for Transonicwind-Tunnel Testing.” In 27th Aerospace Sciences Meeting. AIAA 1989-644. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-644
• Kuhlman, John, Michael Cerney, and Paul Liaw. 1988. “Transonic Low Aspect Ratio Wing-Winglet Designs.” In 26th Aerospace Sciences Meeting. AIAA 1988-7. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-7
• Kuhlman, John, and Paul Liaw. 1987. “Winglets on Low Aspect Ratio Wings.” In 5th Applied Aerodynamics Conference. AIAA 1987-2482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2482
• Kulfan, Brenda. 2008. “New Supersonic Wing Far Far-Field Composite Element Wave Drag Optimization Method ‘FCE’.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-132
• Kumar, Neeraj. 2022. “Review of Supersonic Intake Buzz, Problems Associated and Possible Solutions.” Journal of Thermal and Fluid Science 3 (1). https://doi.org/10.26706/jtfs.3.1.20211202
• Kumar, Priyank, and Sudip Das. 2024. “Influence of Plasma on the Supersonic Air-Intake Buzz.” Journal of Applied Fluid Mechanics 17 (8). https://doi.org/10.47176/jafm.17.8.2512
• 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, Ajit, and A. K. Ghosh. 2023. “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, Pawan, Pradeep K. Karsh, Joy P. Misra, and Jatinder Kumar. 2021. “Multi-Objective Optimization of Machining Parameters during Green Machining of Aerospace Grade Titanium Alloy Using Grey–Taguchi Approach.” Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering: 09544089211043610. https://doi.org/10.1177/09544089211043610
• Kumar, Jatinder, J. S. Khamba, and S. K. Mohapatra. 2008. “An Investigation into the Machining Characteristics of Titanium Using Ultrasonic Machining.” International Journal of Machining and Machinability of Materials 3 (1/2): 143. https://doi.org/10.1504/ijmmm.2008.017631
• 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
• Kuroda, Shinichi. 1993. “Numerical Simulation of Supersonic Flow around Space Plane for Airframe-Engine Integration.” In 31st Aerospace Sciences Meeting. AIAA 1993-886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-886
• Kuroda, Shinichi, and Kozo Fujii. 1991. “Supersonic Inlet Flow Computations Using Fortified Navier-Stokes Approach.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1730
• Kurzke, Joachim. 2006. “Effects of Inlet Flow Distortion on the Performance of Aircraft Gas Turbines.” In Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs. ASMEDC. https://doi.org/10.1115/gt2006-90419
• Kurzke, Joachim, and Ian Halliwell. 2018. “Inlet Flow Distortion.” In Propulsion and Power. Springer International Publishing. https://doi.org/10.1007/978-3-319-75979-1_6
• Kusakin, S. I. 1980. “Velocity Field near a Wing—Fuselage Combination at an Angle of Attack in a Supersonic Stream.” Fluid Dynamics 15 (6): 902–12. https://doi.org/10.1007/bf01096643
• Kutney, John. 2007. “Aircraft Propulsion System Integration Case Studies of Challenges at General Electric.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5345
• Kuzina, Janet. n.d. “A Wind Tunnel Apparatus for Determination of Translational Acceleration Stability Derivatives.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1986-01124
• Kwak, Einkeun, and Seungsoo Lee. 2011. “Convergence Study of Inlet Buzz Frequency with Computational Parameters.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3362
• Kwak, Einkeun, and Seungsoo Lee. 2013a. “Numerical Study of the Effect of Exit Configurations on Supersonic Inlet Buzz.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3025
• Kwak, E., and S. Lee. 2013b. “Supersonic Inlet Buzz Control Using Corrected Bleed Model.” Journal of computational fluids engineering 18 (4): 82–89. https://doi.org/10.6112/kscfe.2013.18.4.082
• Kwak, E., N. Lee, H. Gong, and S. Lee. 2013. “Numerical Simulations of Low- and High-Frequency Buzz around an Axisymmetric Supersonic Inlet.” Journal of computational fluids engineering 18 (2): 78–84. https://doi.org/10.6112/kscfe.2013.18.2.078
• 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
• Kwatny, Harry, Celeste Belcastro, Christine Belcastro, and Bor-Chin Chang. 2008. “Aircraft Loss-of-Control Accident Prevention, Part I: Safety State Assessment and Preliminary Results.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6506
• Kwatny, Harry, Jean-Etienne Dongmo, Robert Allen, Bor-Chin Chang, and Gaurav Bajpai. 2010. “Loss-of-Control: Perspectives on Flight Dynamics and Control of Impaired Aircraft.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8005
• Kwatny, Harry, Jean-Etienne Dongmo, Bor-Chin Chang, Gaurav Bajpai, Murat Yasar, and Christine Belcastro. 2009. “Aircraft Accident Prevention: Loss-of-Control Analysis.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6256
• Kwiek, Agnieszka, Krzysztof Bogdański, Jarosław Hajduk, and Andrzej Tarnowski. 2022. “Technique Used to Perform Rocket-Plane Free-Flight Tests.” Transactions on Aerospace Research 2022 (3): 74–90. https://doi.org/10.2478/tar-2022-0018
• Kwon, Hyuk-Jun. 2005. “Transonic Wing Flutter Analysis Using a Parallel Euler Solver.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (10): 10–16. https://doi.org/10.5139/jksas.2005.33.10.010
• Kwon, Hyuk Jun, Soo Hyung Park, Jae Hun Lee, Yoonsik Kim, In Lee, and Jang Hyuk Kwon. 2005. “Transonic Wing Flutter Simulation Using Navier-Stokes and k-w Turbulent Model.” In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2005-2294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-2294
• Kyser, A., and C. Willis. 1973. “Parametric Studies of the Wing Flutter Behavior of a STOL Transport.” In 14th Structures, Structural Dynamics, and Materials Conference. AIAA 1973-394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-394
• Lacey, David W. 1979. Aerodynamic Characteristics of the Close-Coupled Canard as Applied to Low-to-Moderate Swept Wings. Volume 3. Transonic-Supersonic Speed Regime. Defense Technical Information Center. https://doi.org/10.21236/ada085065
• 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
• Lacy, Cecil. 1968. CMajor Advancement in Fabrication of Large Titanium Aircraft Structures. Presented at the Materials Engineering Exposition and Congress(1968) Held in Detroit, Michigan on 14-17 October 1968. Defense Technical Information Center. https://doi.org/10.21236/ada382566
• Ladd, John, and William Norby. 1998. “Dynamic Inlet Distortion Predictions Using a CFD/distortion Synthesis Approach.” In 16th AIAA Applied Aerodynamics Conference. AIAA 1998-2735. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2735
• Laguardia, Joel, Dimas A. Dutra, and Ricardo Luiz U. Pinto. 2017. “Data Reduction Methods for Dutch-Roll Analysis.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-0938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0938
• Lai, Brian, Torbjørn Cunis, and Laurent Burlion. 2021. “Nonlinear Trajectory Based Region of Attraction Estimation for Aircraft Dynamics Analysis.” In AIAA Scitech 2021 Forum. AIAA 2021-0253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0253
• Lai, H. C., and N. M. Kamaruddin. 2018. “Effect of Fuselage Diameter on Aerodynamic Characteristics for Straight Wing at Low and High Aspect Ratio.” IOP Conference Series: Materials Science and Engineering 370: 012055. https://doi.org/10.1088/1757-899x/370/1/012055
• Lai, Kwok Leung, Xiaoqin Zhang, and Taehyoun Kim. 2014. “Numerical Study of Effect of Control Surface on Wing Flutter in Transonic Flow.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-1200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1200
• Lamar, J. E. 1975. “Prediction of Vortex Flow Characteristics of Wings at Subsonic and Supersonic Speeds.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750034345
• Lamb, Mark. 1999. “Wind Tunnel Investigations of the AGM-130 Turbojet-Powered Configurations.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4257. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4257
• Lampropoulos, Nikolaos Konstantinos, and Ioannis Eleftherios Sarris. 2025. “On Wing Tip Flow around a Low Aspect Ratio Wing at Low Flight Speeds Using OpenFOAM® and Parallel Processing.” Journal of Aircraft and Spacecraft Technology 9 (1): 1–11. https://doi.org/10.3844/jastsp.2025.1.11
• 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. 2006a. “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, C. E., and C.-H. Hsu. 1982. “Effects of Vortex Breakdown on Longitudinal and Lateral-Directional Aerodynamics of Slender Wings by the Suction Analogy.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820055606
• Landers, Stephen F., John A. Saltzman, and Lisa J. Bjarke. 1997. F-16XL Wing Pressure Distributions and Shock Fence Results from Mach 1.4 to Mach 2.0. NASA/TM-97-206219. NASA. https://ntrs.nasa.gov/citations/19970037581
• “Landing Loads.” 1996. In Structural Loads Analysis for Commercial Transport Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862465.0079.0091
• Landrum, E., and D. Miller. 1980. “Assessment of Analytic Methods for the Prediction of Aerodynamic Characteristics of Arbitrary Bodies at Supersonic Speeds.” In 18th Aerospace Sciences Meeting. AIAA 1980-71. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-71
• Lane, R. J. 1966. “A Review of Propulsion for High Mach Number Aircraft: A Survey of the Types of Engine That Will Be Used in the Next Generation of Supersonic and Hypersonic Aircraft.” Aircraft Engineering and Aerospace Technology 38 (1): 11–18. https://doi.org/10.1108/eb034114
• Lane, R. J., and J. Behenna. 1990. “EJ200: The Engine for the New European Fighter Aircraft.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-119
• Langan, Kevin, and Jeffrey Samuels. 1995. “Experimental Investigation of Maneuver Performance Enhancements on an Advanced Fighter/attack Aircraft.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-442. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-442
• Lange, Peter, Philipp Kurrle, and Ulrike Padó. 2024. “Prädiktionsgüte der Rückfederung in der Blechbearbeitung/Prediction quality of springback in sheet metal working – A comparative study of machine learning models.” wt Werkstattstechnik online 114 (03): 106–11. https://doi.org/10.37544/1436-4980-2024-03-78
• Langtry, Robin, Martin Kuntz, and Florian Menter. 2004. “Drag Prediction of Engine-Airframe Interference Effects with CFX 5.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-392
• Lankford, John L. 1947. Investigation of the Pressure-Loss Characteristics of a Turbojet Inlet Screen. NACA-TN-1418. NASA. https://ntrs.nasa.gov/citations/19930082112
• Lanser, Wendy R. 1994. “Wind Tunnel Measurements on a Full-Scale F/A-18 with a Tangentially Blowing Slot.” In 1993 Technical Paper Contest for Women. Gear Up 2000: Women in Motion. https://ntrs.nasa.gov/citations/19940031458
• Lapins, M., R. Klein, R. Martorella, J. Cangelosi, and W. Neely Jr. 1982. “Piloted Simulator Evaluation of a Relaxed Static Stability Fighter at High Angle-of-Attack.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1295. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1295
• Lapygin, V. I., and P. V. Tret’yakov. 1986. “Conical Wing of Maximum Lift-Drag Ratio in a Supersonic Gas Flow.” Fluid Dynamics 21 (3): 445–50. https://doi.org/10.1007/bf01409732
• 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
• Larson, E. 1985. “Crossflow Drag of Finite-Length Rectangular Wing-Bodies.” In 23rd Aerospace Sciences Meeting. AIAA 1985-451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-451
• 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
• 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 Control Power (Rolling Performance).” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0323.0340
• “Lateral-Directional Dynamic Modes.” 2016. In Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods. CRC Press. https://doi.org/10.1201/b15956-11
• “Lateral-Directional Dynamics.” 1998. In Introduction to Aircraft Flight Dynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862052.0207.0256
• “Lateral-Directional Flying Qualities in Forward Flight.” 2002. In Dynamics, Control, and Flying Qualities of V/STOL Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861758.0107.0120
• “Lateral-Directional Motion.” 2016. In Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods. CRC Press. https://doi.org/10.1201/b15956-10
• “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
• Latif G.A.L. Younes, Abdel. 2025. “Relationship between Uphill Runway Slope, Acceleration and Takeoff Distance of Fixed: Wing Aircrafts.” IOP Conference Series: Earth and Environmental Science 1530 (1): 012037. https://doi.org/10.1088/1755-1315/1530/1/012037
• Laughrey, J. 1969. “Calculation of the Performance of Installed Exhaust Nozzles on Supersonic Aircraft.” In 5th Propulsion Joint Specialist. AIAA 1969-428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-428
• Lauten, William T., Jr., and Herbert C. Nelson. 1957. Results of Two Free-Fall Experiments on Flutter of Thin Unswept Wings in the Transonic Speed Range. NACA-TN-3902. NASA. https://ntrs.nasa.gov/citations/19930084784
• Lavrinenko, V. Yu., and Шагалеев Руслан Ринатович. 2019. “The Method of Reducing of Springback Effect during Impact Bending of Sheet Steel Blanks.” In Materials science forum, vol. 973. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.973.85
• Lawing, Pierce L., Julio Chu, William E. Milholen II, and Ndaona Chokani. 1991. Comparison of Cryogenic Wind Tunnel, Flight, and Computational Results for a Thin, Low-Aspect-Ratio Wing. AIAA PAPER 91-1626. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910057913
• Lawrence, J. T. 1965. Some Aspects of the Flight Dynamics of the Aerobee 350 in Region of Pitch-Roll Coupling. NASA-TM-X-55236. NASA. https://ntrs.nasa.gov/citations/19650021461
• 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. 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, G. P., Jr., and J. G. McTigue. 1969. “Lifting Body Flight Tests and Analysis.” In SOCIETY OF AUTOMOTIVE ENGINEERS. https://ntrs.nasa.gov/citations/19700039724
• Lazoglu, Ismail, S. Ehsan Layegh Khavidaki, and Ali Mamedov. 2014. “Mechanics of Titanium Machining.” In Materials Forming, Machining and Tribology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9_3
• Lazzeroni, F. A., E. A. Mossman, and F. A. Pfyl. 1955. An Experimental Investigation of the Air- Flow Stability of a Scoop-Type Normal-Shock Inlet. NACA-RM-A55A13. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19680068703
• Le, Thi Thai, and Thi Kim Dung Hoang. 2026. “Effect of Delta Wing Shape on Aerodynamic Characteristics at Low Speed.” Engineering and Technology For Sustainable Development 36 (3): 070–078. https://doi.org/10.51316/jst.191.etsd.2026.36.3.10
• Leach, A. E., and J. D. McDonough. 1978. Weldability of Formable Sheet Titanium Alloy: Ti-15V-3Cr-Al-3Sn. Defense Technical Information Center. https://doi.org/10.21236/ada070747
• Leacock, Alan G., Shane Quinn, Gregor Volk, David McCracken, and D. Brown. 2015. “The Influence of Strain Rate on the Springback of Commercially Pure Titanium in a Stretch Forming Operation.” In Key engineering materials, vol. 639. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.639.107
• Leamer, P. C., and I. G. Kennon. 1978. Experimental Investigation of a 0.15-Scale Model of an Underfuselage Normal-Shock Inlet. NASA-CR-3049. NASA. https://ntrs.nasa.gov/citations/19790003843
• Lebacqz, J. V., Robert C. Radford, and R. E. Smith. 1974. “An Experimental Investigation of Stol Lateral-Directional Flying Qualities and Roll Control Power Requirements Using the Variable Stability X-22A Aircraft.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f30-024
• Lebon, Jérémy, Guénhaël Le Quilliec, Rajan Filomeno Coelho, Piotr Breitkopf, and Pierre Villon. 2013b. “A Two-Pronged Approach for the Assessment of Springback Variability for Sheet Metal Forming Applications.” In Key engineering materials, vol. 554-557. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.554-557.957
• Lebon, J., G. Lequilliec, R. Filomeno Coelho, P. Breitkopf, and P. Villon. 2013a. “Multi-Level Modeling for Sensitivity Assessment of Springback in Sheet Metal Forming.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.4806891
• Lee, Henry A. 1952. Investigation of Spinning and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultee XFY-1 Airplane in the Free-Spinning Tunnel, TED No. NACA DE 370. NACA-RM-SL52L10. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029463
• Lee, Henry A. 1953. Investigation of the Spinning and Tumbling Characteristics of a 1/25-Scale Model of the Lockheed XFV-1 Airplane in the Langley 20-Foot Free-Spinning Tunnel. NACA-RM-SL53G24. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029432
• Lee, Henry A. 1959. Free-Spinning Characteristics of a 1/30-Scale Model of the Grumman WF-2 Airplane. NASA-AD-3134. NASA. https://ntrs.nasa.gov/citations/19980228233
• Lee, Henry A. 1963. Spin Investigation of a 1/20-Scale Model of an Unswept-Wing, Twin-Engine, Observation Airplane. NASA-TN-D-1516. NASA. https://ntrs.nasa.gov/citations/19630002367
• Lee, Usik. 1994. “Equivalent Continuum Beam-Rod Models of Aircraft Wing Structures for Aeroelastic Analysis.” In Dynamics Specialists Conference. AIAA 1994-1695. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1695
• Lee, Y. S. 2004. “Experimental and FE Analysis to Improve the Accuracy of Springback Prediction on Sheet Metal Forming.” Transactions of Materials Processing 13 (6): 490–96. https://doi.org/10.5228/kspp.2004.13.6.490
• Lee, Taeseung. 2008. “Calculation of Low Aspect Ratio Wing Aerodynamics by Using Nonlinear Vortex Lattice Method.” Journal of the Korean Society for Aeronautical & Space Sciences 36 (11): 1039–48. https://doi.org/10.5139/jksas.2008.36.11.1039
• Lee, Ho-Sung. 2017. “Application of Solid State Welding and Superplastic Forming to Aerospace Vehicles.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2017-01-2148
• Lee, Chang-Hyuck, Joongki Ahn, Hyo-Gil Bae, and Jang-Hyuk Kwon. 2010. “Reliability Based Design Optimization for the Pressure Recovery of Supersonic Double-Wedge Inlet.” Journal of the Korean Society for Aeronautical & Space Sciences 38 (11): 1067–74. https://doi.org/10.5139/jksas.2010.38.11.1067
• Lee, C., and C. Boedicker. 1985. “Subsonic Diffuser Design and Performance for Advanced Fighter Aircraft.” In Aircraft Design Systems and Operations Meeting. AIAA 1985-3073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-3073
• Lee, Changwook, and Seong Man Choi. 2021. “Study on the Effect of Total Pressure Loss by Bell Mouth Inlet Screen.” Journal of the Korean Society of Propulsion Engineers 25 (6): 29–35. https://doi.org/10.6108/kspe.2021.25.6.029
• Lee, H.-J., and I.-S. Jeung. 2009. “Experimental and Numerical Investigation on the Supersonic Inlet Buzz with Angle of Attack.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_51
• Lee, Jin-Hyeok, Ho-Yung Kim, and Hae-Sung Yoon. 2019. “Sustainability Analysis in Titanium Alloy Machining.” Journal of the Korean Society of Manufacturing Process Engineers 18 (12): 73–81. https://doi.org/10.14775/ksmpe.2019.18.12.073
• Lee, In, Hyuk Jun Kwon, and Jong Yun Kim. 2005. “Aeroelastic Design of High Performance Supersonic Aircrafts.” Proceedings of Design & Systems Conference 2005.15 (0): 15–18. https://doi.org/10.1299/jsmedsd.2005.15.15
• Lee, Seungjun, In Lee, and Jae-Hung Han. 2006. “Transonic Flutter Suppression of the 2-D Flap Wing with External Store Using CFD-Based Aeroservoelasticity.” International Journal of Aeronautical and Space Sciences 7 (2): 121–27. https://doi.org/10.5139/ijass.2006.7.2.121
• Lee, Henry A., and Charles E. Libbey. 1961. Incipient- and Developed-Spin and Recovery Characteristics of a Modern High-Speed Fighter Design with Low Aspect Ratio as Determined from Dynamic-Model Tests. NASA-TN-D-956. NASA. https://ntrs.nasa.gov/citations/19980227452
• 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, Chang-Ho, Young-Min Park, Byeong-Hee Chang, and Yung-Gyo Lee. 2017. “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, Keum W., Sahjendra Singh, and Kaushik Raj. 2025. “Composite Adaptive Roll-Coupled Aircraft Maneuvers and Parameter Estimation.” In AIAA SCITECH 2025 Forum. AIAA 2025-2078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2078
• Lee, H. C., and A. R. Swegle. 1963. Landing Gear Development. Defense Technical Information Center. https://doi.org/10.21236/ad0408930
• Lee, Henry A., and L. Faye Wilkes. 1954. Free-Spinning-Tunnel Investigation of a 1/25-Scale Model of the McDonnell F3H-1N Airplane, TED No. NACA AD 3100. NACA-RM-SL55A10a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029373
• Lee, Ho Sung, Jong Hoon Yoon, and Joon Tae Yoo. 2014. “Superplastic Blow Forming of Aerospace Components.” In Key engineering materials, vol. 622-623. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.622-623.819
• Lee-Rausch, Elizabeth, and John Batina. 1993a. “Calculation of AGARD Wing 445.6 Flutter Using Navier-Stokes Aerodynamics.” In 11th Applied Aerodynamics Conference. AIAA 1993-3476. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3476
• Lee-Rausch, Elizabeth, and John Batina. 1993b. “Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1422
• Leen, S. B. 2011. “Predicting Instability in Superplastic Forming of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.2.184
• Leen, S. B., Aditya A. Deshpande, and Thomas H. Hyde. 2010. “Finite Element Modelling and Experimental Testing of Thermomechanical Behaviour and Failure of Titanium Superplastic Forming Dies.” In Key engineering materials, vol. 433. Trans Tech Publications. https://doi.org/10.4028/scientific5/kem.433.247
• Lehman, Larry, and Ronald Stearman. 1977. Analytical Flutter Studies of a Subsonic, Actively Controlled, Variable Geometry Wind Tunnel Model. Volume I.. Defense Technical Information Center. https://doi.org/10.21236/ada039245
• Lehrach, R. 1987. “Thrust/drag Accounting for Aerospace Plane Vehicles.” In 23rd Joint Propulsion Conference. AIAA 1987-1966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1966
• Lei, Zhijin, and Gecheng Zha. 2021. “Lift Enhancement of Supersonic Thin Airfoil at Low Speed by Co-Flow Jet Active Flow Control.” In AIAA Aviation 2021 Forum. AIAA 2021-2591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2591
• Lei, Zhijin, and Gecheng Zha. 2023. “Control Surfaces for Supersonic Airfoil Using Co-Flow Jet Active Flow Control.” In AIAA AVIATION 2023 Forum. AIAA 2023-4236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4236
• Leissler, L. A., and J. C. Nettles. 1954. Investigation of Adjustable Supersonic Inlet in Combination with J34 Engine up to Mach 2.0. NACA-RM-E54H11. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19630004111
• Leland, T. J. W., and W. C. Thompson. 1975. Landing Impact Studies of a 0.3-Scale Model Air Cushion Landing System for a Navy Fighter Airplane. NASA-TN-D-7875. NASA. https://ntrs.nasa.gov/citations/19750009270
• Lemley, Clark E. 1968. Design Criteria for the Prediction and Prevention of Panel Flutter. Volume 2. Background and Review of State of the Art. Defense Technical Information Center. https://doi.org/10.21236/ad0840550
• Lemmin, Jürgen. 1986. “An Approach to an Integrated Control System for a Modern Fighter Aircraft Engine.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/86-gt-277
• Lenning, G. A., and W. H. Heil. 1973. “Flat Rolled Beta Titanium Alloys for Airframe Application.” In Titanium Science and Technology. Springer US. https://doi.org/10.1007/978-1-4757-1346-6_8
• Leo, Romeo Di, Angelo De Fenza, Marco Barile, and Leonardo Lecce. 2014. “Drop Test Simulation for an Aircraft Landing Gear via Multi-Body Approach.” Archive of Mechanical Engineering 61 (2): 287–304. https://doi.org/10.2478/meceng-2014-0017
• Leonard, Michael, and Venkateswaran Narayanaswamy. 2018. “Preliminary Investigation of Unstart Physics and Dynamics in an Axisymmetric Isolator.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1619. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1619
• Leone, Adam. 2010. “Static Design Flight Loads with Fly-By-Wire Technology.” In Vertical Flight Society Annual Forum & Technology Display (VFS Forum). https://doi.org/10.4050/vfs-f66-000432
• Leonov, S., D. Yarantsev, and F. Falempin. 2012. “Flow Control in a Supersonic Inlet Model by Electrical Discharge.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203557
• Lerch, Bradley A., and Steven M. Arnold. 2014. Viscoelastic Response of the Titanium Alloy Ti-6-4: Experimental Identification of Time- and Rate-Dependent Reversible and Irreversible Deformation Regions. NASA/TM-2014-216584. NASA. https://ntrs.nasa.gov/citations/20140008853
• Lernbeiss, R., and M. Plöchl. 2007. “Simulation Model of an Aircraft Landing Gear Considering Elastic Properties of the Shock Absorber.” Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics 221 (1): 77–86. https://doi.org/10.1243/1464419jmbd63
• Lesieutre, Daniel, John Love, and Marnix Dillenius. 1996. “High Angle of Attack Missile Aerodynamics Including Rotational Rates: Program M3HAX.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3392
• Leslie, D. C. M., and J. D. Perry. 1954. “Wave Drag of Wings at Supersonic Speeds.” Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences 225 (1161): 213–25. https://doi.org/10.1098/rspa.1954.0198
• Lesoinne, Michael. 2007. High Performance and High-Fidelity Aeroelastic Simulation of Fixed Wing Aircraft with Deployable Control Surfaces. Defense Technical Information Center. https://doi.org/10.21236/ada481320
• Lesuer, D. 2001. Development of Weldable Superplastic Forming Aluminum Alloy Sheet Final Report CRADA No. TC-1086-95. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/790147
• 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
• Leventhal, S., A. Keel, G. Heiche, and J. Bell. 1977. “An Electrostatic Roll Sensor for Supersonic Vehicles. II: Theoretical Analysis and Experimental Results.” In Guidance and Control Conference. AIAA 1977-1068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1068
• Levin, Daniel, and Joseph Katz. 1990. “Self-Induced Roll Oscillations of Low-Aspect-Ratio Rectangular Wings.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2811
• Levin, Daniel, and Asher Sigal. 2002. “Wind Tunnel Tests of a Missile Having Elliptic Cross Sectioned Body.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4419
• Li, Zhiqiang. 2023a. “Design and Evaluation Method of Superplastic Forming/Diffusion Bonding Structure.” In Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1_6
• Li, Zhiqiang. 2023b. “Microstructure and Properties of Superplastic Forming/Diffusion Bonding Process.” In Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1_4
• Li, Zhiqiang. 2023c. “Principles of Superplastic Forming/Diffusion Bonding.” In Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1_2
• Li, Zhiqiang. 2023d. “Test Method of Superplastic Forming/Diffusion Bonding Structure.” In Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1_5
• Li, Zhiqiang. 2023e. “Titanium and Titanium Alloy.” In Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1_1
• Li, Jian, Yang An, and Kunyuan Zhang. 2022b. “Study on Variable Geometry Scheme of High Mach Axisymmetric Inlet.” Journal of Physics: Conference Series 2228 (1): 012052. https://doi.org/10.1088/1742-6596/2228/1/012052
• Li, Li, Junqiang Bai, Tongbiao Guo, Xiaolong He, and Ziyuan Fu. 2018a. “Aerodynamic Design of the Supersonic Aircraft Wing-Shape and Wing-Twist Optimization.” International Journal of Aeronautical and Space Sciences 19 (2): 340–53. https://doi.org/10.1007/s42405-018-0046-y
• Li, Yuming, Fabien Bogard, Boussad Abbes, and Yingqiao Guo. 2009. “Surface Reconstruction of the “False” Tools to Compensate for the Springback in Sheet Forming Process.” In Computational Structural Engineering. Springer Netherlands. https://doi.org/10.1007/978-90-481-2822-8_141
• Li, Xiaoqiang, Hongrui Dong, Guiqiang Guo, and Dongsheng Li. 2018b. “Hot Stretch Forming of Titanium Sheet by Resistance Heating.” MATEC Web of Conferences 190: 07003. https://doi.org/10.1051/matecconf/201819007003
• Li, Bing, Jin Dong, Peng Xiao, and Qingtang Meng. 2021c. “Research on Locked Wheel Protection Function of Aircraft Brake System.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2021-01-1269
• Li, Zhi Qiang, and He Ping Guo. 2005. “Application of Superplastic Forming and Diffusion Bonding in the Aerospace Industry.” In Materials science forum. Trans Tech Publications. https://doi.org/10.4028/0-87849-960-1.3037
• Li, Xinqi, and Shicheng Hu. 2021. “Research Progress of Springback in Multi-Point Forming of Sheet Metal.” Journal of Physics: Conference Series 2101 (1): 012006. https://doi.org/10.1088/1742-6596/2101/1/012006
• Li, Jie, Fengwei Li, E. Qin, Jicang Liu, and Chaojun Qiao. 2000. “CFD Applications to Airframe/propulsion Integration for Civil Aircraft.” In Fluids 2000 Conference and Exhibit. AIAA 2000-2228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2228
• Li, Hong, Maoquan Li, and Weixin Yu. 2016. Rapid Fabrication of Bond with High Strength in the Press Bonding of Titanium Alloy. Wiley. https://doi.org/10.1002/9781119296126.ch49
• Li, Fen Qiang, and Jian Hua Mo. 2012. “Springback Analysis of TC4 Titanium Alloy Complex Part with Double Curvature under Single Point Incremental Forming Process.” Advanced materials research 468-471: 1094–98. https://doi.org/10.4028/www.scientific.net/amr.468-471.1094
• Li, Wen, Xiao-ming Tan, Yuanhong Leng, Chunhua Wang, Yong Shan, and Jing-zhou Zhang. 2024a. “Experimental and Numerical Study on the Cooling Performance of Flame Stabilizer in One-Piece Afterburner with Different Cooling Configurations.” Preprint, . https://doi.org/10.2139/ssrn.4970459
• Li, Kai-Lun, Jia-Zhong Zhang, and Peng-Fei Lei. 2010. “Simulation and Nonlinear Analysis of Panel Flutter with Thermal Effects in Supersonic Flow.” In Dynamical Systems. Springer New York. https://doi.org/10.1007/978-1-4419-5754-2_7
• Li, Yadong, Junyao Zhang, Fengtian Yang, and Yongliang Chen. 2021b. “Research on High Attack Angle Stall and Spin Characteristics with Flight Test of a General Electric Aircraft.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 39 (3): 650–59. https://doi.org/10.1051/jnwpu/20213930650
• Lian, Chenchen, Peiyan Wang, Shizhen Zhao, et al. 2024. “Experimental and Numerical Research of Aircraft Tire Debris Impact on Landing Gear Brake Pipe.” Preprint, . https://doi.org/10.2139/ssrn.4862132
• Liang, S. M., R. N. Wu, and J. J. Chan. n.d. “An Upwind Scheme for Oblique Shock/boundary Layer Interaction in a Supersonic Inlet.” In Lecture Notes in Physics. Springer Berlin Heidelberg. https://doi.org/10.1007/3-540-56394-6_243
• Liao, Juan, Chi Zhou, Feng Ruan, and Yin Lian Zhu. 2010. “A New Springback Compensation Method for Sheet Metal Bending Based on Curvature Correction.” Advanced materials research 97-101: 130–34. https://doi.org/10.4028/www.scientific.net/amr.97-101.130
• Librescu, Liviu, Sungsoo Na, Piergiovanni Marzocca, Chanhoon Chung, and Moon Kwak. 2003. “Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1414
• “Lift/Drag Ratios of Optimised Slewed Wings at Supersonic Speeds.” 1962. Aeronautical Quarterly 13 (1): 91–92. https://doi.org/10.1017/s0001925900002274
• “Lightweight Low-Cost Flight Test Instrumentation.” 2007. Aircraft Engineering and Aerospace Technology 79 (1). https://doi.org/10.1108/aeat.2007.12779aad.010
• Lijewski, Lawrence. 1980. Trajectory Prediction Theory of Supersonic High Fineness Ratio, Cruciform Fin Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada104989
• Lilley, J., and S. Pengelly. 1992. “Wind Tunnel Evaluation of the Installed Performance of Mid-Airframe Mounted Tactical Missile Turbojet Sustainers.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3752
• 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
• Limitations and Flight Envelope. 2017. Wiley. https://doi.org/10.1002/9781118534786.ch20
• Lin, J., T. Zhu, and L. Zhan. 2011. “Constitutive Equations for Modelling Superplastic Forming of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.2.154
• 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
• Lindsey, W. F. 1946. Effect of Compressibility on the Pressure and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-Chord Flap. NACA-WR-L-76. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092792
• Linehan, Thomas I., and Kamran Mohseni. 2016a. “Aerodynamics and Lateral Stability of Low-Aspect-Ratio Wings with Dihedral at Low Reynolds Numbers.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1063
• Linehan, Thomas, and Kamran Mohseni. 2017. “Leading-Edge Flow Reattachment and the Lateral Static Stability of Low-Aspect-Ratio Rectangular Wings.” Physical Review Fluids 2 (11): 113901. https://doi.org/10.1103/physrevfluids.2.113901
• Linnell, R. D. 1963. Estimation of Takeoff Ground-Run Distances for Jet-Propelled Conventional and STOL Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0408661
• Liou, May-Fun, and Thomas Benson. 2010. “Optimization of Bleed for Supersonic Inlet.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9172
• Liston, G., and L. Small. 1992. “Fighter Airframe/propulsion Integration: A Wright Laboratory Perspective.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3337
• Littleboy, D., and P. Smith. 1996. “Closed Loop Analysis of a Simple Aircraft Model Using Bifurcation Methods.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3366
• Littleboy, D., P. Smith, D. Littleboy, and P. Smith. 1997. “Bifurcation Analysis of a High Incidence Aircraft with Nonlinear Dynamic Inversion Control.” In 22nd Atmospheric Flight Mechanics Conference. AIAA 1997-3717. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3717
• Liu, Hong. 1999. “Three-Dimension Numerical Study on the Combustion Flow in an Afterburner.” In 33rd Thermophysics Conference. AIAA 1999-3752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3752
• Liu, Yuqi. 2003. “Quantitative Prediction for Springback of Unloading and Trimming in Sheet Metal Stamping Forming.” Chinese Journal of Mechanical Engineering 16 (02): 190. https://doi.org/10.3901/cjme.2003.02.190
• Liu, Peiqing. 2022a. “Aerodynamic Characteristics of Low-Speed Fuselage and Wing-Body Configuration.” In Aerodynamics. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4586-1_10
• Liu, Peiqing. 2022b. “Aerodynamic Characteristics of Subsonic Thin Airfoil and Wing.” In Aerodynamics. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4586-1_11
• Liu, Peiqing. 2022c. “Aerodynamic Characteristics of Supersonic Thin Airfoil and Wing.” In Aerodynamics. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4586-1_12
• Liu, Peiqing. 2022d. “Aerodynamic Characteristics of Transonic Thin Airfoil and Wing.” In Aerodynamics. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4586-1_13
• Liu, Jun. 2024a. “FEM Study of Process Parameters in a Novel Superplastic Forming of Titanium Alloy Ti-6Al-4V.” In Materials Research Proceedings, vol. 44. Materials Research Forum LLC. https://doi.org/10.21741/9781644903254-23
• Liu, Yang. 2024b. “Superplastic Microstructure Characteristics and Unified Constitutive Model of TA32 Titanium Alloy.” In Materials Research Proceedings, vol. 44. Materials Research Forum LLC. https://doi.org/10.21741/9781644903254-9
• Liu, Hong Liang, Yu Chen, Chun Cheng Li, Lin Guan, and Xiao Nan Wang. 2021a. “Design and Analysis of Hot Forming Parts with Extra Thick Specification.” In Materials science forum, vol. 1026. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.1026.59
• Liu, Steven, James Gordon, and M. Ozbek. 1996. “A Nonlinear Model for Aircraft Brake Squeal Analysis. I: Model Description and Solution Methodology.” In Dynamics Specialists Conference. AIAA 1996-1251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1251
• Liu, Fangfei, and Peter Grant. 2010. “Ground Based Simulation of Airplane Upset Recovery Using an Enhanced Aircraft Model.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2010-7797. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7797
• Liu, Zehua, Junjie Jia, Yan Xie, and Xinping Zhao. 2025e. “Research and Development of Aircraft Automatic Brake Technology.” IET Conference Proceedings 2024 (13): 147–53. https://doi.org/10.1049/icp.2024.2828
• Liu, J., and P. F. Weng. 2007. “Computational Study of Aerodynamics of Low Aspect Ratio Wings.” In New Trends in Fluid Mechanics Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-75995-9_87
• 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, Geng Wu, and Zhen Zhong. 2010. “Study and Design of Sheet Metal Bending Springback Adjustable Die.” Advanced materials research 152-153: 1092–96. https://doi.org/10.4028/www.scientific.net/amr.152-153.1092
• Liu, Xiaochuan, Shi Xing Zhu, and Yong Gang Yang. 2014a. “Design and Drop Test of Aircraft Landing Gear’s Shock Absorber Based on Magnetorheological Damper.” Applied Mechanics and Materials 665: 601–6. https://doi.org/10.4028/www.scientific.net/amm.665.601
• Lium, J. 1971. “Development of a Torsional-Flexural Stability Analysis of Stiffened Titanium Panels for Application to the U.S. Supersonic Transport.” In 12th Structures, Structural Dynamics and Materials Conference. AIAA 1971-338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-338
• Livneh, Rafael. 1995b. “Improved Literal Approximations for the Lateral-Directional Dynamics of Rigid Aircraft.” In Guidance, Navigation, and Control Conference. AIAA 1995-3307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3307
• Lobanovskii, Yu. I. 1983. “Maximal Lift-Drag Ratio of Wing-Cone and Wing-Half-Cone Combinations at High Supersonic Velocities.” Fluid Dynamics 18 (3): 481–83. https://doi.org/10.1007/bf01090577
• 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, R. C. 1958. “An Extension of the Linearized Theory of Supersonic Flow past Quasi-Cylindrical Bodies, with Applications to Wing-Body Interference.” Journal of Fluid Mechanics 4 (1): 33–63. https://doi.org/10.1017/s002211205800029x
• Lock, R. C. 1961. “Theoretical Pressure Distribution at Zero Lift at Supersonic Speeds for Slender Delta Wings Having Fuselages of Circular Cross Section.” Aeronautical Quarterly 12 (2): 95–130. https://doi.org/10.1017/s0001925900002006
• Lock, R. C. 1963. “The Aerodynamic Design of Swept Winged Aircraft at Transonic and Supersonic Speeds.” Journal of the Royal Aeronautical Society 67 (630): 325–37. https://doi.org/10.1017/s0001924000062758
• Lock, R. C., and J. Bridgewater. 1967. “Theory of Aerodynamic Design for Swept-Winged Aircraft at Transonic and Supersonic Speeds.” Progress in Aerospace Sciences 8: 139–228. https://doi.org/10.1016/0376-0421(67)90004-8
• Lockard, David, Mehdi Khorrami, and Fei Li. 2004. “High Resolution Calculation of a Simplified Landing Gear.” In 10th AIAA/CEAS Aeroacoustics Conference. AIAA 2004-2887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2887
• Lockheed Aircraft Corp Marietta Ga. 1962. Determination of Design Data for Heat Treated Titanium Alloy Sheet. Volume 3. Tables of Data Collected. Defense Technical Information Center. https://doi.org/10.21236/ad0297803
• Lockwood, V. E. 1966. Low-Speed Wind-Tunnel Studies Relating to Pitch-up on a Supersonic Transport Model with a High-Aspect-Ratio Variable-Sweep Wing. NASA-TN-D-3542. NASA. https://ntrs.nasa.gov/citations/19660023730
• Logan, H. L. 1964. The Mechanisms of Stress Corrosion of the Titanium Alloy Ti 8-1-1 Exposed to Salt Environments at Elevated Temperatures Final Report. NASA-CR-82511. NASA. https://ntrs.nasa.gov/citations/19670009758
• Loh, C., and W. Hui. 1989. “Applications of Lagrangian Time to Steady Supersonic Airfoil Computation.” In 9th Computational Fluid Dynamics Conference. AIAA 1989-1963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1963
• Loh, J., and A. Lusty Jr. 1974. “A Display of Energy-Maneuverability Performance Information for Fighter Aircraft.” In Mechanics and Control of Flight Conference. AIAA 1974-814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-814
• Lokos, William, Andrew Lizotte, Ned Lindsley, and Rick Stauf. 2005. “Shock Location Dominated Transonic Flight Loads on the Active Aeroelastic Wing.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6315
• Lokos, William A., Eric J. Miller, Larry D. Hudson, Andrew C. Holguin, David C. Neufeld, and Ronnie Haraguchi. 2015. “Strain Gage Loads Calibration Testing with Airbag Support for the Gulfstream III SubsoniC Research Aircraft Testbed (SCRAT).” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-2020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2020
• Lokos, William, Candida Olney, Tony Chen, Natalie Crawford, Rick Stauf, and E. Reichenbach. 2002a. “Strain-Gage Loads Calibration Testing of the Active Aeroelastic Wing F/A-18 Aircraft.” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-2926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2926
• Lokos, William, Candida Olney, Natalie Crawford, Rick Stauf, and Eric Reichenbach. 2002b. “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
• Lomax, Harvard. 1953. Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds. NACA-TN-2925. NASA. https://ntrs.nasa.gov/citations/19930083653
• Lomax, Harvard. 1954. Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds. NACA-TR-1162. NASA. https://ntrs.nasa.gov/citations/19930092190
• Lomax, Harvard. 1959. Two-Dimensional, Supersonic, Linearized Flow with Heat Addition. NASA-MEMO-1-10-59A. NASA. https://ntrs.nasa.gov/citations/19980227969
• Lomax, Harvard, Franklyn B. Fuller, and Loma Sluder. 1954. Generalized Indicial Forces on Deforming Rectangular Wings in Supersonic Flight. NACA-TN-3286. NASA. https://ntrs.nasa.gov/citations/19930083985
• Lomax, Harvard, Franklyn B. Fuller, and Loma Sluder. 1955. Generalized Indical Forces on Deforming Rectangular Wings in Supersonic Flight. NACA-TR-1230. NASA. https://ntrs.nasa.gov/citations/19930092239
• Lomax, Harvard, and Max A. Heaslet. 1956b. A Special Method for Finding Body Distortions That Reduce the Wave Drag of Wing and Body Combinations at Supersonic Speeds. NACA-TR-1282. NASA. https://ntrs.nasa.gov/citations/19930092279
• 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
• Lone, Mohammad M., and Alessandro Pontillo. 2020. “Flight Loads Assessment of Failure Cases with Pilot Models.” In AIAA Scitech 2020 Forum. AIAA 2020-0283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0283
• Long, Tang, Wang Hu, Cai Yong, Mao Lichen, and Li Guangyao. 2011. “Springback Control of Sheet Metal Forming Based on High Dimension Model Representation and Genetic Algorithm.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3623719
• 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. https://doi.org/10.2514/5.9781600861840.0275.0283
• Lopes, Elias Dias Rossi, and Helon Vicente Hultmann Ayala. 2020. “Nonlinear Grey-Box Identification of a Landing Gear Based on Drop Test Data.” Anais do Congresso Brasileiro de Automática 2020. https://doi.org/10.48011/asba.v2i1.1299
• Lorber, Peter, and Franklin Carta. 1991. “Incipient Torsional Stall Flutter Aerodynamic Experiments on a Sweptthree-Dimensional Wing.” In 32nd Structures, Structural Dynamics, and Materials Conference. AIAA 1991-935. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-935
• Loshelder, Augustine E., and Weihua Su. 2026. “Rapid Predictions of Nonlinear Flight Dynamics for Rigid Aircraft with Physics-Informed Neural Networks.” In ASME 2026 Aerospace Structures, Structural Dynamics, and Materials Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/ssdm2026-183357
• Loth, Eric, Sean Candon, and Michael Rybalko. 2016. “Mass Flow Ratio Influence on Shock and Pressure Spectra for a Low-Boom Supersonic Inlet.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0532
• Love, Michael. 2003. “Identification of Critical Flight Loads.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1893
• 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
• Lowenberg, Mark. 2010. Fixed-Wing Lateral and Directional Dynamic Stability. Wiley. https://doi.org/10.1002/9780470686652.eae255
• Lowenberg, Mark, and Hilton Kyle. 2002. “Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4879
• Lu, Honggang, Ruoyang Guan, Tao Huang, Yaming Guo, and Yuan Zheng. 2023a. “Simulation and Analysis of Hot Cylindrical Flow Forming Process of Titanium Alloy.” Journal of Physics: Conference Series 2566 (1): 012059. https://doi.org/10.1088/1742-6596/2566/1/012059
• Lu, Zhiyong, Hongyu Lu, Yidong Li, and Zhili Yang. 1992. “The Flow Field Characteristics about a Fighter Configuration at Highangles of Attack.” In Guidance, Navigation and Control Conference. AIAA 1992-4358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4358
• Lu, Weiming, and Ziyang Wang. 2024. “Research on Brake Torque Design of Civil Aircraft.” Journal of Physics: Conference Series 2741 (1): 012031. https://doi.org/10.1088/1742-6596/2741/1/012031
• 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
• Luber, Wolfgang G. 2018. “Buffeting and Single Degree of Freedom Flutter at Transonic Speeds.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3643
• Luce, Richard W., Jr. 1949. Deflections of a Supersonic Wing Due to Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ada278113
• Lucero, E. 1984. “Empirical Curves for Predicting Supersonic Aerodynamics of Very-Low-Aspect-Ratio Lifting Surfaces.” In 22nd Aerospace Sciences Meeting. AIAA 1984-575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-575
• 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
• Lukashevich, Sergey, Sergey Morozov, and Aleksandr Shiplyuk. 2023. “Measurement of the Distribution of Pressure Pulsations along the Axis of the Supersonic Nozzle.” In AIP Conference Proceedings, vol. 2504. AIP Publishing. https://doi.org/10.1063/5.0132273
• Lum, Peter T., and Richard Chait. 1977. Monotonic and Low-Cycle Fatigue Response of a Maraging Steel and Metastable Beta Titanium Alloy under Torsional Loading. Defense Technical Information Center. https://doi.org/10.21236/ada038837
• Lunde, T. 1977. Real-Time Testing of Titanium Sheet and Extrusion Coupon Specimens Subjected to Mach 2.7 Supersonic Cruise Aircraft Wing Stresses and Temperatures. NASA-CR-2754. NASA. https://ntrs.nasa.gov/citations/19780005535
• Lundell, John H., Richard Scherrer, and Lewis A. Anderson. 1961. Investigation of an Axisymmetric Internal Compression Inlet at a Mach Number of about 3.8. NASA-TN-D-854. NASA. https://ntrs.nasa.gov/citations/20040008090
• Luo, Shijun, and Hsien Cheng. 1996. “A Second-Order Small-Disturbance Solution for Wing at Supersonic Speeds.” In Theroretical Fluid Mechanics Conference. AIAA 1996-2166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2166
• Luo, Shiquan, Jianzhe Huang, Lanhao Zhao, Xue Zhang, and Jing Zhongliang. 2024a. “Electrical Brake Anti-Skid Control Design for Aircraft Considering Subjective Vertical Conflict Theory.” Preprint, . https://doi.org/10.2139/ssrn.4932282
• Luo, Wenguo, Yang Tao, Jianfeng Zhu, and Yancheng You. 2024b. “Evolution Characteristics Analysis of Supersonic Inlet Buzz with High-Order Dynamic Mode Decomposition Method.” Journal of Aerospace Engineering 37 (3): 04024026. https://doi.org/10.1061/jaeeez.aseng-5388
• Luo, Zhicong, and Iryna Voronko. 2023. “Aircraft Landing Gear Test for Emerging Loads.” ГРААЛЬ НАУКИ, no. 24: 389–90. https://doi.org/10.36074/grail-of-science.17.02.2023.070
• Lustig, Sanford, David W. Jackson, and Fred E. Hussong. 1960. Structural Test Program F-106A Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0249771
• Luty, Grzegorz, Agata Wrońska, Jacek Andres, and Tomasz Gałaczynski. 2018. “Advanced Techniques for the Fabrication of Airframe Structures Using Innovative Friction Stir Welding (FSW) Technology.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0074-2018-12804
• Luu, HuySon, and Yoshimasa Ochi. 2023. “Wind Estimation Based on Estimation of Lateral-Directional Stability Derivatives of Aircraft.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 21 (0): 1–7. https://doi.org/10.2322/tastj.21.1
• Luyi, Dou, Li Xiaoqiang, Dong Hongrui, Li Dongsheng, and Peng Xingyi. 2020. “Development of Springback Tester and the Effect of Forming Speed on the Springback of Four Sheet Metal Bending Processes.” IOP Conference Series: Materials Science and Engineering 967 (1): 012065. https://doi.org/10.1088/1757-899x/967/1/012065
• Lyons, Leonard J. 1952. “Turbojet Installation Cooling and Associated Performance Losses.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/520163
• Lystad, H. D. 1975. Fatigue Investigation of the E-2B/C Nose Landing Gear. Defense Technical Information Center. https://doi.org/10.21236/ada024072
• Macdougall, George F., Jr. 1942. Free-Spinning-Tunnel Tests of a 1/23.75-Scale Model of the Douglas DC-3 Airplane. NACA-WR-L-783. NASA. https://ntrs.nasa.gov/citations/19930092702
• MacDougall, George F., Jr. 1947. Investigations of Tumbling Characteristics of a 1/20-Scale Model of the Northrop N-9M Airplane. NACA-RM-L6L10. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050031170
• MacDougall, George F., Jr., and Jacob H. Lichtenstein. 1946. Free-Spinning-Tunnel Tests of a 1/20-Scale Model of the Northrop N-9M Airplane. NACA-RM-L6G30. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019257
• Mace, James, and Gregory Nyberg. 1992. “Fighter Airframe/propulsion Integration: A McDonnell Aircraft Perspective.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3333
• Mace, J., and D. Sedlock. 1981. “A Perspective on Developing New Inlet Distortion Measurement and Predictive Methods.” In 17th Joint Propulsion Conference. AIAA 1981-1589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1589
• Machida, Shigeru, Takao Kikuchi, Hitoshi Arizono, Kenichi Saitoh, and Jiro Nakamichi. 2005. “Transonic Flutter Characteristics of an Arrow Wing Mounted with Engine.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-835
• “Machining and Chemical Shaping of Titanium.” 2015. In Titanium. ASM International. https://doi.org/10.31399/asm.tb.tpmpa.t54480293
• “Machining for Air Data Measurement.” 1989. Aircraft Engineering and Aerospace Technology 61 (8): 14–14. https://doi.org/10.1108/eb036823
• “Machining of Aerospace Materials.” 1986. Aircraft Engineering and Aerospace Technology 58 (5): 6–7. https://doi.org/10.1108/eb036277
• Mackintosh, G., and J. Dawson. 1979. “A New Technique to Compute Installed Jet Engine Thrust: Applications to Trimming for Economic and Operational Benefits.” In 4th International Symposium on Air Breathing Engines. AIAA 1979-7010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-7010
• Macquisten, M., and A. Dowling. 1993. “Combustion Oscillations in a Twin-Stream Afterburner.” In 15th Aeroacoustics Conference. AIAA 1993-4392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4392
• Madelung, G. 1977. “Characteristics of Fighter Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1977-1219. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1219
• Madson, Michael, and Larry Ericksont. 1985. “Application of Pan Air to an Advanced Supersonic Fighter/attack Aircraft.” In 3rd Applied Aerodynamics Conference. AIAA 1985-4093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4093
• Maemori, Ken’ichi, Naoki Tanigawa, Reiko Koganei, and Toshio Morihara. 2003. “Optimization of a Semi-Active Shock Absorber for Aircraft Landing Gear.” In Volume 2: 29th Design Automation Conference, Parts A and B. ASMEDC. https://doi.org/10.1115/detc2003/dac-48765
• Magill, J., L. Darden, N. Komerath, and J. Dorsey. 1994. “Measurement of Aircraft Stability Parameters in the Wind Tunnel Using a Wind Driven Manipulator.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3457
• Magill, J., N. Komerath, and J. Dorsey. 1995. “An Experimental Evaluation of Controllers for Wind Driven Manipulators (in Aircraft Dynamic Testing).” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3502. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3502
• 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
• Mahlmeister, J. E., T. Ishimoto, and A. Ambrosio. 1955. Studies on Thermal Stresses for Aircraft Structures Exposed to Transient External Heating. Volume 1. Evaluation of the Thermal Response, Force and Moment in a Plate. Defense Technical Information Center. https://doi.org/10.21236/ad0093337
• Mahzan, Muhammad Iyas, Sallehuddin Muhamad, Sa’ardin Abdul Aziz, and Mohamed Sukri Mat Ali. 2013a. “Composite Wing Flutter Speed and Frequency Due to Variable Control Surface Deflection in Low Speed Wind Tunnel.” Applied Mechanics and Materials 390: 3–7. https://doi.org/10.4028/www.scientific.net/amm.390.3
• Mahzan, Muhammad Iyas, Sallehuddin Muhamad, Mat Ali Mohamed Sukri, and Mansor Shuhaimi. 2013b. “Wind Tunnel Testing of Composite Wing Flutter Speed Due to Control Surface Excitation.” Applied Mechanics and Materials 315: 359–63. https://doi.org/10.4028/www.scientific.net/amm.315.359
• Maia, A., E. Ferreira, M. C. Oliveira, L. F. Menezes, and A. Andrade-Campos. 2017. “Numerical Optimization Strategies for Springback Compensation in Sheet Metal Forming.” In Computational Methods and Production Engineering. Elsevier. https://doi.org/10.1016/b978-0-85709-481-0.00003-3
• Maier, L., C. Hartmann, B. Ünver, and W. Volk. 2022. “Three-Dimensional Control Point Based Surface Description for Data Reduction, Reverse Engineering and Springback Compensation in Sheet Metal Forming.” In The Minerals, Metals & Materials Series. Springer International Publishing. https://doi.org/10.1007/978-3-031-06212-4_24
• Maikapar, G. I. 1993. “Lift-to-Drag Ratio at Supersonic Speeds.” Fluid Dynamics 28 (5): 696–701. https://doi.org/10.1007/bf01050055
• Maikapar, G. I. 2000. “Reduction of the Induced Drag of a Supersonic Wing.” Fluid Dynamics 35 (5): 778–83. https://doi.org/10.1023/a:1026611503563
• 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., 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
• Maji, Arnesh, Jawahar Sivabharathy Samuthira Pandi, and Sanjay Mittal. 2024. “Aerodynamic Center of a Wing at Low Reynolds Number.” Physics of Fluids 36 (3): 033627. https://doi.org/10.1063/5.0195947
• Majumdar, Neelakshi, Karen B. Marais, and Arjun H. Rao. 2021. “Analysis of General Aviation Fixed-Wing Aircraft Accidents Involving Inflight Loss of Control Using a State-Based Approach.” Aviation 25 (4): 283–94. https://doi.org/10.3846/aviation.2021.15837
• Makarov, Kirill, and Alexander Pavlenko. 2016. “Optimization of Chine-Shaped Forebody of an Aircraft in Terms of Providing Directional Stability.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-3723. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3723
• Malan, Pieter J., Jacobus A. Engelbrecht, and Herman A. Engelbrecht. 2016. “Angle of Attack Upset Detection for Passenger Airliners Using Classification of Anemometric and Inertial Sensor Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3847
• Malcolm, G. 1978. “New Rotation-Balance Apparatus for Measuring Airplane Spin Aerodynamics in the Wind Tunnel.” In 10th Aerodynamic Testing Conference. AIAA 1978-835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-835
• Malcolm, Gerald, T. Ng, Liane Lewis, and Daniel Murri. 1989. “Development of Non-Conventional Control Methods for High Angle of Attack Flight Using Vortex Manipulation.” In 7th Applied Aerodynamics Conference. AIAA 1989-2192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2192
• Malisani, Simone, and Elisa Capello. 2021. “Modeling Framework for Dynamic Wing Loads and Control Design of a Flexible Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-0117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0117
• Mallik, Wrik, Rakesh K. Kapania, and Joseph A. Schetz. 2015. “Aeroelastic Analysis and Optimization of Flexible Wing Aircraft with a Novel Control Effector.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-1175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1175
• Mallik, Wrik, Lior Poplingher, and Daniella E. Raveh. 2022. “Flutter Analysis of the Benchmark Supercritical Wing at Moderate Angles of Attack.” In AIAA SCITECH 2022 Forum. AIAA 2022-2316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2316
• 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
• Malone, Michael B., and Charles C. Peavey. 1999. “Installed Transonic 2D Nozzle Nacelle Boattail Drag Study.” In First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop. https://ntrs.nasa.gov/citations/20000044629
• Malone, J., N. Sankar, and W. Sotomayer. 1984. “Unsteady Aerodynamic Modeling of a Fighter Wing in Transonic Flow.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1566
• Malvestuto, Frank S., Lawrence J. Gale, and John H. Wood. 1947. Compilation of Test Data on 111 Free-Spinning Airplane Models Tested in the Langley 15-Foot and 20-Foot Free-Spinning Tunnels. NACA-RM-L7E15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090025259
• Malvestuto, Frank S., Jr., and Dorothy M. Hoover. 1951a. Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds. NACA-TN-2294. NASA. https://ntrs.nasa.gov/citations/19930082953
• Malvestuto, Frank S., Jr., and Dorothy M. Hoover. 1951b. Supersonic Lift and Pitching Moment of Thin Sweptback Tapered Wings Produced by Constant Vertical acceleration.Subsonic Leading Edges and Supersonic Trailing Edges. NACA-TN-2315. NASA. https://ntrs.nasa.gov/citations/19930082993
• Malvestuto, Frank S., Jr., and Kenneth Margolis. 1950. Theoretical Stability Derivatives of Thin Sweptback Wings Tapered to a Point with Sweptback or Sweptforward Trailing Edges for a Limited Range of Supersonic Speeds. NACA-TR-971. NASA. https://ntrs.nasa.gov/citations/19930092032
• Malvestuto, Frank S., Jr., Kenneth Margolis, and Herbert Spencer Ribner. 1949. Theoretical Lift and Damping in Roll of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds Subsonic Leading Edges and Supersonic Trailing Edges. NACA-TN-1860. NASA. https://ntrs.nasa.gov/citations/19930082532
• Malvestuto, Frank S., Jr., Kenneth Margolis, and Herbert S. Ribner. 1950. Theoretical Lift and Damping in Roll at Supersonic Speeds of Thin Sweptback Tapered Wings with Streamwise Tips, Subsonic Leading Edges, and Supersonic Trailing Edges. NACA-TR-970. NASA. https://ntrs.nasa.gov/citations/19930091081
• 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
• 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
• Mann, C. D. 1964. Six-Degree-of-Freedom Flight Path Study Generalized Computer Program. Part 1. Volume 2. Structural Loads Formulation. Defense Technical Information Center. https://doi.org/10.21236/ad0449828
• Mann, Michael, and Harry Carlson. 1991. “An Assessment of Current Methods for Drag-Due-to-Lift Minimization at Supersonic Speeds.” In 9th Applied Aerodynamics Conference. AIAA 1991-3302. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3302
• Mansfield, Eric H. 1963. “Torsional Vibrations of a Solid Wing of Diamond Section.” Aeronautical Quarterly 14 (3): 295–98. https://doi.org/10.1017/s0001925900002845
• Mansour, N. 1984. “Numerical Simulation of the Tip Vortex off a Low-Aspect-Ratio Wing at Transonic Speed.” In 22nd Aerospace Sciences Meeting. AIAA 1984-522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-522
• Marchman, J., III, D. Donatelli, and J. Terry. 1983. “Wing Loading on a 60 Degree Delta Wing with Vortex Flaps.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2555. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2555
• Marcy, William L. 1958. High-Speed Landing Loads Measured on the Douglas X-3 Research Airplane. NACA-RM-H57L06. NASA. https://ntrs.nasa.gov/citations/19930090201
• 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
• Mardoc, V. 1970. “Distortion and Turbulence Interaction: A Method for Evaluating Engine/inlet Compatibility.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-632
• Margetts, Rebecca, Roger F. Ngwompo, and Marcelin Fortes da Cruz. 2013. “Modelling a Drop Test of a Landing Gear Using a Hybrid Bond Graph.” In Artificial Intelligence and Applications / 794: Modelling, Identification and Control / 795: Parallel and Distributed Computing and Networks / 796: Software Engineering / 792: Web-based Education. ACTAPRESS. https://doi.org/10.2316/p.2013.794-072
• Margolis, Kenneth. 1947. Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift. NACA-TN-1448. NASA. https://ntrs.nasa.gov/citations/19930082080
• Margolis, Kenneth. 1950. Theoretical Lift and Damping in Roll of Thin Sweptback Tapered Wings with Raked-in and Cross-Stream Wing Tips at Supersonic Speeds.subsonic Leading Edges. NACA-TN-2048. NASA. https://ntrs.nasa.gov/citations/19930082719
• Margolis, Kenneth, and Miriam H. Elliott. 1959. Formulas Pertinent to the Calculation of Flow-Field Effects at Supersonic Speeds Due to Wing Thickness. NASA-MEMO-4-3-59L. NASA. https://ntrs.nasa.gov/citations/19980228306
• Margolis, Kenneth, Frank S. Malvestuto Jr., and Peter J. Maxie Jr. 1958. Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement. NACA-TN-4120. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930084830
• Marion, Le Fournier, Nazaret Fabien, Barrau Olivier, Lebard Etienne, and Vidal Vanessa. 2016. The Use of Infra-Red Heater in Superplastic Forming: A Way of Saving Costs. Wiley. https://doi.org/10.1002/9781119296126.ch263
• Marion, Andrew, and Gaurav Sharma. 2025. “Numerical Study of Transonic Flow Characteristics around a Compound Delta Wing.” In 2025 Regional Student Conferences. AIAA 2025-97857. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-97857
• MarİZa, Duaa, and Süleyman Baştürk. 2021. “Experimental Investigation of Drawbead Effect on Springback in Profile of Double Circular, Rectangular and Triangular Bending Sheet Metal Forming Processes.” AURUM Journal of Engineering Systems and Architecture 5 (1): 51–64. https://doi.org/10.53600/ajesa.724818
• Marshall, Laurie A. 2000. Summary of Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment. H-2410. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20000080123
• 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
• Martin, John C. 1950. The Calculation of Downwash behind Wings of Arbitrary Plan Form at Supersonic Speeds. NACA-TN-2135. NASA. https://ntrs.nasa.gov/citations/19930082757
• Martin, John C. 1953. A Vector Study of Linearized Supersonic Flow Applications to Nonplanar Problems. NACA-TR-1143. NASA. https://ntrs.nasa.gov/citations/19930092172
• Martin, G. 1964. “Design and Fabrication of Welded Titanium Wing Leading Edge.” In General Aviation Aircraft Design and Operations Meeting. AIAA 1964-163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-163
• Martin, Larry. 1996. Final Report, Methodology Investigation, Global Positioning System (GPS) Vehicle Tracking System for Flight Testing of Fixed- and Rotary-Wing Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada315263
• Martin, John C., and Nathan Gerber. 1953a. The Effect of Thickness on Pitching Airfoils at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0014217
• Martin, John C., and Nathan Gerber. 1953b. On the Effect of Thickness on the Damping in Roll of Airfoils at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0005479
• Martin, John C., and Frank S. Malvestuto Jr. 1955. Aerodynamics of a Rectangular Wing of Infinite Aspect Ratio at High Angles of Attack and Supersonic Speeds. NACA-TN-3421. NASA. https://ntrs.nasa.gov/citations/19930084235
• Martin, Glenn, David Tice, Don Marcum Jr., and Jonathan Seidel. 1991. “A Comparison of Arrow, Trapezoidal and M Wing Concepts Using a Mach 2 Supersonic Cruise Transport Mission.” In Aircraft Design and Operations Meeting. AIAA 1991-3102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3102
• Martinez, E. 1961. A New Facility for the Study of Aircraft Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ad0265941
• 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
• Martos, Borja, Paul Kiszely, and John V. Foster. 2011. “Flight Test Results of a GPS-Based Pitot-Static Calibration Method Using Output-Error Optimization for a Light Twin-Engine Airplane.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110015011
• Martz, C. William, and James D. Church. 1951. Flight Investigation at Subsonic, Transonic, and Supersonic Velocities of the Hinge-Moment Characteristics, Lateral-Control Effectiveness, and Wing Damping in Roll of a 60 Degrees Sweptback Delta Wing with Half-Delta Tip Ailerons. NACA-RM-L51G18. NASA. https://ntrs.nasa.gov/citations/19930086858
• Marusak, A., J. Pietrucha, and K. Sibilski. 2000. “Prediction of Aircraft Critical Flight Regimes Using Continuation and Bifurcation Methods.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-976. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-976
• Maruyama, Daigo, Kisa Matsushima, Kazuhiro Kusunose, and Kazuhiro Nakahashi. 2006. “Aerodynamic Design of Biplane Airfoils for Low Wave Drag Supersonic Flight.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3323. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3323
• Marvin, I. 1968. “Integrated Math Modeling for Turbofan and Supersonic Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-648
• Masak, M. 1965. “Lateral Instability of Swept-Winged Aircraft Induced by Pitching Oscillations.” In 2nd Annual Meeting. AIAA 1965-315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-315
• Mascitti, V. R. 1966. Charts of Additive Drag Coefficient and Mass-Flow Ratio for Inlets Utilizing Right Circular Cones at Zero Angle of Attack. NASA-TN-D-3434. NASA. https://ntrs.nasa.gov/citations/19660016261
• Maslov, A. A., Jiachun Li, and Song Fu. 2011. “High Speed Boundary Layer Stability and Control.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3651827
• Mason, Homer P. 1953. Flight Test Results of Rocket-Propelled Buffet-Research Models Having 45 Degree Sweptback Wings and 45 Degree Sweptback Tails Located in the Wing Chord Plane. NACA-RM-L53I10. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050041783
• Mason, W. 1983. “SC3: A Wing Concept for Supersonic Maneuvering.” In Applied Aerodynamics Conference. AIAA 1983-1858. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1858
• Mason, W., M. Siclari, D. Miller, and J. Pittman. 1983. “A Supersonic Maneuver Wing Designed for Nonlinear Attached Flow.” In 21st Aerospace Sciences Meeting. AIAA 1983-425. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-425
• Masood, Imran. 2019. “Sustainable Machining for Titanium Alloy Ti-6Al-4V.” In IntechOpen eBooks. IntechOpen. https://doi.org/10.5772/intechopen.82344
• Masud, Jehanzeb, and Omar Khan. 2015a. “Computed Effect of Wing Tip Configuration on Wing Load Characteristics of a High Speed Aircraft.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0773. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0773
• Masud, Jehanzeb, and Omar Khan. 2015b. “Evaluating an Experimental Streamlined Fairing for a Diverter Less Supersonic Inlet (DSI) Equipped Aircraft.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0248
• Masud, Jehanzeb, and Omer Khan. 2016. “Evaluating an Experimental Streamlined Fairing for a Diverterless Supersonic Inlet (DSI) Equipped Aircraft.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1566
• Masud, Jehanzeb, Tauha I. Khan, and Zakria G. Toor. 2018. “Analysis of High Alpha Aerodynamic Characteristics of a Supersonic Aircraft.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-2057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2057
• Matak, Leo, and Karolina Krajček Nikolić. 2022. “CFD Analysis of F-16 Wing Airfoil Aerodynamics in Supersonic Flow.” In The Science and Development of Transport—ZIRP 2021. Springer International Publishing. https://doi.org/10.1007/978-3-030-97528-9_13
• Mateescu, D. 1986. “Wing and Conical Body of Arbitrary Cross-Section Combinations in Supersonic Flow.” In 4th Applied Aerodynamics Conference. AIAA 1986-1826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1826
• 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. W., and D. H. Gatlin. 1978. Flight Evaluation of the Transonic Stability and Control Characteristics of an Airplane Incorporating a Supercritical Wing. NASA-TP-1167. NASA. https://ntrs.nasa.gov/citations/19780012197
• Matos, Marcondes Azevedo, and Vanessa Cunha Mendes Cadete. 2022. “Aircraft Brake System Simulation.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2021-36-0434
• Matranga, Gene J. 1961. 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 Neil A. Armstrong. 1959. Approach and Landing Investigation at Lift-Drag Ratios of 2 to 4 Utilizing a Straight-Wing Fighter Airplane. NASA-TM-X-31. NASA. https://ntrs.nasa.gov/citations/19980235626
• Matsugi, Kouki, Takumi Araki, Naohiro Namba, and Ryutaro Hino. 2025. “Influence of a Wide Range of Bend-Holding Time on Springback and Time-Dependent Springback in Sheet Metal Bending.” Proceedings of International Conference on Leading Edge Manufacturing in 21st century: LEM21 2025.11 (0): OS08-5. https://doi.org/10.1299/jsmelem.2025.11.os08-5
• Matsugi, Kouki, and Ryutaro Hino. 2024. “Influence of Bend Holding on Springback and Time-Dependent Springback in Sheet Metal Bending.” Materials Transactions 65 (10): 1373–76. https://doi.org/10.2320/matertrans.mt-p2024003
• Matsuo, Munetsugu. 1991. “Development in Processing Technology of Gamma Titanium Aluminides for Potential Application to Airframe Structures.” ISIJ International 31 (10): 1212–22. https://doi.org/10.2355/isijinternational.31.1212
• Matsuo, Kazuyasu, Heuy-Dong Kim, Jong-Woo Hong, and Shigetoshi Kawagoe. 2023. “Unsteadiness of Normal Shock Wave/boundary Layer Interaction in a Supersonic Diffuser.” In Proceeding of Transport Phenomena in Thermal Engineering. Volume 2. Begellhouse. https://doi.org/10.1615/istp-vi.940
• Matsushita, H., T. Miyata, L. E. Christiansen, T. Lehn-Schioler, and E. Mosekilde. 2002. “Nonlinear Dynamics Approach of Modeling the Bifurcation for Aircraft Wing Flutter in Transonic Speed.” In Proceedings of the 41st SICE Annual Conference. SICE 2002., vol. 2. Soc. Instrument & Control Eng. (SICE). https://doi.org/10.1109/sice.2002.1195240
• Mattingly, Jack. 1989. “Easy Method of Matching Fighter Engine to Airframe for Use in Aircraft Engine Design Courses.” In 25th Joint Propulsion Conference. AIAA 1989-2260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2260
• Matviichuk, Vladyslav, and Vladimir Nesterenkov. 2026. “Electron Beam Powder Bed Fusion of VT6 Titanium Alloy for Aircraft Applications.” Preprint, . https://doi.org/10.2139/ssrn.7091839
• 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
• May, R., and G. Richey. 1979. “Propulsion System and Airframe Integration Consideration for Advanced Air-to-Surface Aircraft.” In 15th Joint Propulsion Conference. AIAA 1979-1120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1120
• Mayer, David, and Gerald Paynter. 1994. “Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-580
• Maykuth, D. J., and R. H. Ernst. 1964. Fire Hazards Associated with the Use of Titanium in Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0609342
• Mayo, Wilbur L. 1961. Skid Landings of Airplanes on Rocker-Type Fuselages. NASA-TN-D-760. NASA. https://ntrs.nasa.gov/citations/20040006362
• Mayo, E. E., and M. B. Nolan. 1966. The Effect of Antenna Location on Pitch/roll Coupling Characteristics of the Apache. NASA-TM-X-55562. NASA. https://ntrs.nasa.gov/citations/19660028122
• Maywald, P. V., and D. K. Beale. 1991. “Development of a Freejet Capability for Evaluating Inlet-Engine Compatibility.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-401
• Mazhul, I. I. 2020. “Supersonic Flow in the Rectangular Duct of an Air Inlet with the Separation-Induced Interaction of the Boundary Layer with Shock Waves.” Thermophysics and Aeromechanics 27 (4): 507–18. https://doi.org/10.1134/s0869864320040046
• Mazurov, Anatoliy Pavlovich, and Sergey Alexandrovich Takovitsky. 2013. “The Method of Optimal Profiling of Flying Vehicle Fuselage and Nozzle at the Cruising Supersonic Flight.” TsAGI Science Journal 44 (3): 405–17. https://doi.org/10.1615/tsagiscij.2013010195
• McAnally, R. 1974. “Air Superiority Fighter Wing Design for Cost and Weight Reduction.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-338
• McAulay, John E., and Harold R. Kaufman. 1953. Altitude Wind Tunnel Investigation of the Prototype J40-WE-8 Turbojet Engine without Afterburner. NACA-RM-E52K10. NASA. https://ntrs.nasa.gov/citations/19930087366
• McBrearty, J. F. 1952. “Discussion: “Friction Surfaces for Spin-Up Simulation in Landing-Gear Drop Tests” (Drake, D. W., 1952, Trans. ASME, 74, Pp. 1269–1279).” Journal of Fluids Engineering 74 (7): 1281–1281. https://doi.org/10.1115/1.4016095
• McClinton, C., R. Voland, S. Holland, W. Engelund, J. White, and J. Pahle. 1998. “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
• McConnell, Jeff. 2006. “Use of Transonic Free to Roll Testing in the Design Phase of the Joint Strike Fighter.” In 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2006-3925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3925
• 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
• McCrink, Matthew, and James W. Gregory. 2017. “Aerodynamic Parameter Estimation for Derived Angle-of-Attack Systems.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4061. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4061
• McCuish, A., and B. Caldwell. 2018. “Development and Flight Experience of the Control Laws and the Aeroservoelastic Solution in the Experimental Aircraft Programme (EAP).” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-12
• McDaniel, Melissa. 2012. “Methods for Determining Supersonic Roll Damping Coefficients for Slender Cruciform Configurations.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-412
• 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
• McDearmon, Russel W., and William B. Boatright. 1956. Experimental and Theoretical Studies of Interference Effects on the Damping in Roll of the Bell X-1A Research Airplane at Supersonic Speeds (Including Canopy Shape Effects). NACA-RM-L56G27. NASA. https://ntrs.nasa.gov/citations/19930089573
• McDearmon, Russell W., and Frank L. Clark. 1956a. Wind-Tunnel Investigation of the Damping in Roll of the Bell X-1A Research Airplane and Its Components at Supersonic Speeds. NACA-RM-L55I19. NASA. https://ntrs.nasa.gov/citations/19930088921
• McDearmon, Russell W., and Frank L. Clark. 1956b. Wind-Tunnel Investigation of the Damping in Roll of the Bell X-1E Research Airplane and Its Components at Supersonic Speeds. NACA-RM-L56B15. NASA. https://ntrs.nasa.gov/citations/19930089155
• McDearmon, Russell W., and Harry S. Heinke Jr. 1953. Investigations of the Damping in Roll of Swept and Tapered Wings at Supersonic Speeds. NACA-RM-L53A13. NASA. https://ntrs.nasa.gov/citations/19930087488
• McDearmon, Russell W., and Robert A. Jones. 1956. Wind-Tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack. NACA-RM-L56F13a. NASA. https://ntrs.nasa.gov/citations/19930089304
• McDonough, Kevin, Ilya Kolmanovsky, and Ella M. Atkins. 2014. “Recoverable Sets of Initial Conditions and Their Use for Aircraft Flight Planning after a Loss of Control Event.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-0786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0786
• McElderry, E. D. 1973. Boundary Layer Transition Mapping at Supersonic Speeds Measured by Liquid Crystals. Defense Technical Information Center. https://doi.org/10.21236/ada377039
• McFadden, Norman M., and Donovan R. Heinle. 1954. Flight Investigation of the Effects of Horizontal-Tail Height, Moment of Inertia, and Control Effectiveness on the Pitch-up Characteristics of a 35 Degree Swept-Wing Fighter Airplane at High Subsonic Speeds. NACA-RM-A54F21. NASA. https://ntrs.nasa.gov/citations/19930088281
• McGann, Rick L. 1995. “Flight Test Results from a Low-Power Doppler Optical Air Data Sensor.” In SPIE Proceedings, vol. 2464, edited by Robert G. Otto, James Lenz. SPIE. https://doi.org/10.1117/12.211483
• McGehee, J. R., and H. D. Carden. 1976. A Mathematical Model of an Active Control Landing Gear for Load Control during Impact and Roll-out. NASA-TN-D-8080. NASA. https://ntrs.nasa.gov/citations/19760010002
• McGehee, J. R., and R. C. Dreher. 1982. Experimental Investigation of Active Loads Control for Aircraft Landing Gear. NASA-TP-2042. NASA. https://ntrs.nasa.gov/citations/19820023445
• McGrath, Brian. 1993. “Computational Study of a Conical Wing Having Unit Aspect Ratio at Supersonic Speeds.” In 11th Applied Aerodynamics Conference. AIAA 1993-3505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3505
• McGuigan, W. 1970. “Inflight Thrust Control for Fighter Aircraft.” In Fighter Aircraft Conference. AIAA 1970-513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-513
• McKay, Gary E. 2010. “Calculation of Dynamic Tire Forces from Aircraft Instrumentation Data.” Tire Science and Technology 38 (3): 182–93. https://doi.org/10.2346/1.3481649
• McKay, J. M., and R. B. Noll. 1965. “A Summary of the X-15 Landing Loads.” In Progr. of the X-15 Res. Airplane Program. https://ntrs.nasa.gov/citations/19730062065
• McKay, J. M., and R. J. Wilson. 1968. Landing Loads and Accelerations of the XB-70-1 Airplane. NASA-TN-D-4836. NASA. https://ntrs.nasa.gov/citations/19680026601
• McKee, John W., and John M. Riebe. 1952. An Investigation of a 0.16-Scale Model of the Douglas X-3 Airplane to Determine Means of Improving the Low-Speed Longitudinal Stability and Control Characteristics. NACA-RM-L52H01. NASA. https://ntrs.nasa.gov/citations/19930087541
• McKevitt, F., D. J. Vargo, and M. I. Weinstein. 1957. Investigation of an Underslung Scoop Inlet at Mach Numbers to 1.99. NACA-RM-E56L11. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19650018860
• McKinney, Marion O., and Bernard Maggin. 1944. Experimental Verification of the Rudder-Free Stability Theory for an Airplane Model Equipped with Rudders Having Negative Floating Tendency and Negligible Friction. NACA-ARR-L4J05A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092686
• 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
• 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
• McMillin, S., and R. Wood. 1986. “Planform Effects for Low-Fineness Ratio Multibody Configurations at Supersonic Speeds.” In 4th Applied Aerodynamics Conference. AIAA 1986-1799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1799
• McMurray, Robert J., Alan G. Leacock, and D. Brown. 2007. “Double Curvature Springback in Stretch Formed 2024-T3 Aluminium.” In Key engineering materials. Trans Tech Publications. https://doi.org/10.4028/0-87849-437-5.391
• McQuilkin, F. T. 1982. Feasibility of SPF/DB Titanium Sandwich for LFC Wings. NASA-CR-165929. NASA. https://ntrs.nasa.gov/citations/19820019338
• 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
• 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
• Md Akhtar Khan. 2014. “Effect of Spikes Integrated to Airfoil at Supersonic Speed.” International Journal of Research in Engineering and Technology 03 (10): 226–38. https://doi.org/10.15623/ijret.2014.0310035
• Mead, George J. 1925. “Some Aspects of Aircraft-Engine Development.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/250066
• “The Measurement of Moment of Inertia by Using Three Wire Pendulum.” 2022. Academic Journal of Engineering and Technology Science 5 (12). https://doi.org/10.25236/ajets.2022.051203
• Medekshas, H. 2008. “Effect of Elevated Temperature and Welding on Low Cycle Fatigue Strength of Titanium Alloys.” Mechanika 70 (2): 5–10. https://doi.org/10.5755/j02.mech.14946
• Medina, Jose A., Harinkumar Patel, and Bernd Chudoba. 2021. “2D Mixed-Compression Inlet Sizing of Supersonic Vehicles.” In AIAA Aviation 2021 Forum. AIAA 2021-2780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2780
• Medzorian, John P. 1992. “High Speed Aircraft Tire Dynamics/Issues.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/921037
• Megson, T. H. G. 2010. “Airframe Loads.” In Introduction to Aircraft Structural Analysis. Elsevier. https://doi.org/10.1016/b978-1-85617-932-4.00013-0
• Megson, T. H. G. 2013. “Airframe Loads.” In Aircraft Structures for Engineering Students. Elsevier. https://doi.org/10.1016/b978-0-08-096905-3.00048-6
• Megson, T. H. G. 2017. “Airframe Loads.” In Aircraft Structures for Engineering Students. Elsevier. https://doi.org/10.1016/b978-0-08-100914-7.00014-1
• Megson, T. H. G. 2018. “Airframe Loads.” In Introduction to Aircraft Structural Analysis. Elsevier. https://doi.org/10.1016/b978-0-08-102076-0.00013-0
• Megson, T. H. G. 2022. “Airframe Loads.” In Aircraft Structures for Engineering Students. Elsevier. https://doi.org/10.1016/b978-0-12-822868-5.00014-0
• Meher-Hornji, Cyrus B. 1997. “The Development of the Whittle Turbojet.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/97-gt-528
• Mehra, R., and J. Carroll. 1980. “Bifurcation Analysis of Aircraft High Angle-of-Attack Flight Dynamics.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1599
• Mehta, Unmeel. 1986. The Computation of Flow past an Oblique Wing Using the Thin-Layer Navier-Stokes Equations. NASA-TM-88317. NASA. https://ntrs.nasa.gov/citations/19880020390
• Meijer, Jos, and Atlee Cunningham Jr. 1992. “Understanding and Development of a Prediction Method of Transonic Limit Cycle Oscillation Characteristics of Fighter Aircraft.” In Astrodynamics Conference. AIAA 1992-4501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4501
• Mellquist, Erik C., and Oddvar O. Bendiksen. 2014. “Computational Transonic Flutter Solutions for Cranked Wing Planforms.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0674. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0674
• Mellquist, Erik C., and Oddvar O. Bendiksen. 2015. “Analysis of the Transonic Flutter of Supersonic Transport Wings.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-0443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0443
• Melville, Reid. 2002. “Aeroelastic Instability of Tactical Aircraft in Nonlinear Flow Regimes.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2970. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2970
• Melville, Reid, and Raymond Gordnier. 1998. “Numerical Simulation of Large Amplitude Aeroelastic Wing Response.” In 29th AIAA, Fluid Dynamics Conference. AIAA 1998-2657. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2657
• Merchant, Ali, Umair Ashun, James Paduano, and Mark Drela. 2003. “Design of an Actively Stabilized, near-Isentropic Supersonic Inlet.” In 16th AIAA Computational Fluid Dynamics Conference. AIAA 2003-4096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4096
• Mercure, Robert A. 1996. “Propulsion System Considerations for Future Supersonic Transports: A Global Perspective.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/96-gt-245
• Meriwether, H. D., and I. E. Harris. 1962. Landing Loads Investigation Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ad0404420
• Merkli, Peter E. 1975. Pressure Recovery in Rectangular Adjustable Area Supersonic Diffusers. Defense Technical Information Center. https://doi.org/10.21236/ada033630
• 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
• Merrett, Craig G. 2015. “Time to Flutter of a Viscoelastic Goland Wing.” In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2015-0193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0193
• Merrett, Craig. 2016. “Time to Flutter of a Maneuvering Viscoelastic Goland Wing.” In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2016-1962. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1962
• Merrett, Craig, and Harry Hilton. 2011. “Aero-Servo-Viscoelastic Flutter and Torsional Divergence Alleviation for a Wing in Subsonic, Compressible Flow.” In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2011-1716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1716
• 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 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
• Metz, Paul. 1992. “Flight Test of the YF-23A Advanced Tactical Fighter.” In Aerospace Design Conference. AIAA 1992-1039. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1039
• Meyer, J. 1992. “Effects of the Roll Angle on Cruciform Wing-Body Configurations at High Incidences.” In Guidance, Navigation and Control Conference. AIAA 1992-4356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4356
• Meyer, R., and W. Fields. 1978. “Configuration Development of a Supersonic Cruise Strike-Fighter.” In 16th Aerospace Sciences Meeting. AIAA 1978-148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-148
• Meyersburg, R. 1968. “Research Flight Testing in the 80’s.” In Aircraft Design for 1980’s Operations Meeting. AIAA 1968-204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-204
• Michaelsen, O. E. 1957. “Stability and Control Problems of Supersonic Aircraft: Reprinted from Part 2 (April l-June 30, 1956) of the Quarterly Bulletin of the National Aeronautical Establishment, Ottawa, Canada.” Aircraft Engineering and Aerospace Technology 29 (8): 241–47. https://doi.org/10.1108/eb032860
• Micromechanical Characterization and Texture Analysis of Direct Cast Titanium Alloys Strips. 2000. Langley Research Center. https://ntrs.nasa.gov/citations/20000067654
• Migdal, David, and William K. Greathouse. 1968. “Optimizing Exhaust — Nozzle/Airframe Thrust Minus Drag.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/680294
• Migdal, D., E. Miller, and W. Schnell. 1969. “An Experimental Evaluation of Exhaust Nozzle/airframe Interference.” In 5th Propulsion Joint Specialist. AIAA 1969-430. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-430
• Migliorini, Matteo, Pavlos Zachos, and David MacManus. 2019. “The Impact of Inlet Boundary Layer Thickness on the Unsteady Aerodynamics of S-Duct Intakes.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4202
• Mikhail, Ameer G. 1979. Numerical Solution of a Supersonic Nozzle Afterbody Flow with Jet Exhaust. Defense Technical Information Center. https://doi.org/10.21236/ada076116
• 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
• Mikhail, Ameer. 1993. “Roll Damping for Projectiles Including Wraparound, Offset, and Arbitrary Number of Fins.” In 11th Applied Aerodynamics Conference. AIAA 1993-3460. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3460
• Miki, Hajime, Masaharu Kameda, and Yasushi Watanabe. 2014. “Low Drag Design and Aerodynamic Performance Evaluation of Supersonic Air Inlet.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3798
• Miklosovic, David, Robin Imber, Michael Britt-Crane, and Kyle Colantonio. 2012. “Mid-Span PIV Measurements of a Low Aspect Ratio Circulation Control Wing.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2893
• Miklosovic, David S., and Matthew Perry. 2014. “PIV Wake Measurements of a Low Aspect Ratio Circulation Control Wing with Spanwise Variation in Efflux.” In 7th AIAA Flow Control Conference. AIAA 2014-2796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2796
• Mikułowski, Grzegorz, and Łukasz Jankowski. 2009. “Adaptive Landing Gear: Optimum Control Strategy and Potential for Improvement.” Shock and Vibration 16 (2): 175–94. https://doi.org/10.1155/2009/732803
• Miles, John W. 1951. “The Oscillating Rectangular Airfoil at Supersonic Speeds.” Quarterly of Applied Mathematics 9 (1): 47–65. https://doi.org/10.1090/qam/40138
• Miles, John W. 1953a. “A General Solution for the Rectangular Airfoil in Supersonic Flow.” Quarterly of Applied Mathematics 11 (1): 1–8. https://doi.org/10.1090/qam/53715
• Miles, John W. 1953b. “On the Low Aspect Ratio Oscillating Rectangular Wing in Supersonic Flow.” Aeronautical Quarterly 4 (2): 231–44. https://doi.org/10.1017/s0001925900000901
• 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
• Milholen, William E., II, and Ndaona Chokani. 1992. Numerical Modeling of Transonic Juncture Flow. AIAA PAPER 92-4036. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920074234
• 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, Daniel, and G. Addington. 2004. “Invited: Aerodynamic Flowfield Control Technologies for Highly Integrated Airframe Propulsion Flowpaths.” In 2nd AIAA Flow Control Conference. AIAA 2004-2625. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2625
• Miller, L. E., and P. G. Koch. 1985. Aircraft Flight Performance Methods. Revision 2. Defense Technical Information Center. https://doi.org/10.21236/ada158227
• 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, D., J. Pittman, and R. Wood. 1983. “An Overview of Two Nonlinear Supersonic Wing Design Studies.” In 21st Aerospace Sciences Meeting. AIAA 1983-182. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-182
• Miller, E. H., and J. Protopapas. 1985. “Nozzle Design and Integration in an Advanced Supersonic Fighter.” International Journal of Turbo and Jet Engines 2 (4). https://doi.org/10.1515/tjj.1985.2.4.273
• Miller, E., J. Protopapas, R. Obye, and W. Wooten. 1979. “Nozzle Design and Integration in an Advanced Supersonic Fighter.” In Aircraft Systems and Technology Meeting. AIAA 1979-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1813
• Miller, D., and R. Schemensky. 1979. “Design Study Results of a Supersonic Cruise Fighter Wing.” In 17th Aerospace Sciences Meeting. AIAA 1979-62. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-62
• Miller, Daniel N., and Brian R. Smith. 2003. “CFD-Based Simulation of Inlet Unstart Phenomena: Toward Supersonic Inlet Flow Control Techniques.” In Volume 2: Symposia, Parts A, B, and C. ASMEDC. https://doi.org/10.1115/fedsm2003-45471
• Miller, D., and R. Wood. 1983. “An Investigation of Wing Leading-Edge Vortices at Supersonic Speeds.” In Applied Aerodynamics Conference. AIAA 1983-1816. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1816
• 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
• 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
• Milward, Thomas O., Michael A. Bromfield, Nadjim Horri, Rashid Ali, and Steve Scott. 2019. “Multipoint Angle of Attack Sensing for Avoidance of Loss of Control in Flight.” In AIAA Scitech 2019 Forum. AIAA 2019-1540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1540
• Min, Ke, Zhenqi Sun, Zejun Cai, et al. 2026a. “A Physics-Informed Generative Framework for Predicting Symmetry-Plane Unstart Flow Evolution in a Turbine-Based Combined-Cycle Inlet.” Preprint, . https://doi.org/10.2139/ssrn.7133946
• Min, Ke, Zhenqi Sun, Zhancang Hu, Chunliang Dai, Chengxiang Zhu, and Yancheng You. 2026b. “Predicting Start and Unstart Flow-Field Evolution during Mode Transition in an Inward-Turning TBCC Inlet Based on a Self-Developed Physics-Informed Video Diffusion Transformer.” Preprint, . https://doi.org/10.2139/ssrn.7445820
• “Miniaturised Inertia! Measurement Unit for Dynamic Aircraft Control.” 2005. Aircraft Engineering and Aerospace Technology 77 (1): aeat.2005.12777aad.007. https://doi.org/10.1108/aeat.2005.12777aad.007
• Minkiewicz, Gregory, and Neil Bosmajian. 1996. “Effects of Supersonic Bounded Flow on a Modified Double Wedge Airfoil.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-561. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-561
• Minshall, Timothy, Michael J. Candon, Robert Carrese, Pier Marzocca, and Oleg Levinski. 2017. “Fighter Aircraft Buffet Load Prediction Using Nonlinear System Identification Algorithms.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0864
• Mirels, Harold. 1948. Theoretical Method for Solution of Aerodynamic Forces on Thin Wings in Nonuniform Supersonic Stream with an Application to Tail Surfaces. NACA-TN-1736. NASA. https://ntrs.nasa.gov/citations/19930082432
• Mirels, Harold. 1951. A Lift-Cancellation Technique in Linearized Supersonic-Wing Theory. NACA-TR-1004. NASA. https://ntrs.nasa.gov/citations/19930092061
• Mirels, Harold, and Rudolph C. Haefeli. 1949. Line-Vortex Theory for Calculation of Supersonic Downwash. NACA-TN-1925. NASA. https://ntrs.nasa.gov/citations/19930082603
• Mishler, R., and T. Wilkinson. 1992. “Emerging Airframe/propulsion Integration Technologies at General Electric.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3335
• Mishra, R. K., K. S. Jayasimha, and S. N. Mistry. 2023. “Effect of Fuel System Snags on the Performance of a Military Turbojet Engine.” Journal of Aerospace Sciences and Technologies: 293–97. https://doi.org/10.61653/joast.v65i3.2013.851
• Miskin, Daniel L., and Timothy T. Takahashi. 2019. “Preliminary Design of a Wing Considering Transonic Aerodynamic, Weight and Aeroelastic Behavior.” In AIAA Aviation 2019 Forum. AIAA 2019-3068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3068
• Misté, Gianluigi Alberto, and Ernesto Benini. 2013. “Turbojet Engine Performance Tuning with a New Map Adaptation Concept.” In ASME 2013 Gas Turbine India Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/gtindia2013-3533
• Mitcham, Grady L., Willard S. Blanchard, and Earl C. Hastings Jr. 1952. Summary of Low-Lift Drag and Directional Stability Data from Rocket Models of the Douglas XF4D-1 Airplane with and without External Stores and Rocket Packets at Mach Numbers from 0.8 to 1.38 TED No. NACA DE-349. NACA-RM-SL52G11. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029440
• Mitcham, Grady L., Willard S. Blanchard Jr., and Earl C. Hastings Jr. 1951a. 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
• Mitcham, Grady L., Joseph E. Stevens, Norman L. Crabill, and Arthur H. Hinners Jr. 1951b. Low-Lift Drag and Duct Pressure Recovery of a 1/8.25-Scale Model of the Consolidated Vultee XF-92 Airplane at Mach Numbers from 0.7 to 1.4. NACA-RM-SL51E23. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030034
• Mitchell, Glenn A., and Robert C. Campbell. 1957. Performance of a Supersonic Ramp-Type Side Inlet with Ram-Scoop Throat Bleed and Varying Fuselage Boundary-Layer Removal: Mach Number Range 1.5 to 2.0 / Glenn a. Mitchell and Robert C. Campbell. NACA-RM-E56I26. NASA. https://ntrs.nasa.gov/citations/19930089448
• Mitchell, D., and D. Johnston. 1980. “Effects of the Aerodynamic Cross-Coupling and Lateral Acceleration Derivatives on Airplane Dynamic Characteristics.” In 18th Aerospace Sciences Meeting. AIAA 1980-170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-170
• Mitchell, Jesse L., and Robert F. Peck. 1955. Investigation of the Lateral Stability Characteristics of the Douglas X-3 Configuration at Mach Numbers from 0.6 to 1.1 by Means of a Rocket-Propelled Model. NACA-RM-L54L20. NASA. https://ntrs.nasa.gov/citations/19930088585
• Mitchell, G. A., B. W. Sanders, and R. J. Shaw. 1974. Throat Stability-by Pass Systems to Increase the Stable Airflow Range of a Mach 2.5 Inlet with 60-Percent Internal Contraction. NASA-TM-X-2976. NASA. https://ntrs.nasa.gov/citations/19740020363
• Mittal, Sanchit, Sanjay Mittal, and L. Venkatakrishnan. 2026. “Stability and Buzz Characteristics of a Y-Shaped Conventional and Diverterless Supersonic Inlet.” Physics of Fluids 38 (9): 096136. https://doi.org/10.1063/5.0346197
• Miura, Hideshi. 2015. “Direct Laser Forming of Titanium Alloy Powders for Medical and Aerospace Applications.” KONA Powder and Particle Journal 32 (0): 253–63. https://doi.org/10.14356/kona.2015017
• Miyaji, Koji, and Hiroto Takegawa. 2022. “Prediction of Transonic 2D Wing Flutter Using the Time-Spectral Computational Fluid Dynamics.” Journal of Fluid Science and Technology 17 (2): JFST0004-JFST0004. https://doi.org/10.1299/jfst.2022jfst0004
• Mizoguchi, Makoto, and Hajime Itoh. 2016. “Experimental Investigation of Aspect-Ratio-One Wing Characteristics at Low Reynolds Numbers.” In 46th AIAA Fluid Dynamics Conference. AIAA 2016-4341. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4341
• Mizoguchi, Makoto, Yusuke Kajikawa, and Hajime Itoh. 2014. “Static Stall Hysteresis of Low-Aspect-Ratio Wings.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2014
• Mocerino, N. J., and Billy Burroughs. 1979. “Superplastic Forming Diffusion Bonding of Titanium Helicopter Airframe Components.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f35-032
• Mocquard, Clément. n.d. “Simulation of Fighter Jet Engine’s Afterburner.” PhD diss., Université de Toulouse (2023-2025). https://doi.org/10.70675/e123b7eez7672z4477z8d31zafe6c917761c
• “Modal Analysis of a Typical Landing Gear Oleo Strut.” 2018. International Journal of Recent Trends in Engineering and Research 4 (1): 1–6. https://doi.org/10.23883/ijrter.2018.4001.t6fhs
• Moeckel, W. E. 1955. Estimation of Inlet Lip Forces at Subsonic and Supersonic Speeds. NACA-TN-3457. NASA. https://ntrs.nasa.gov/citations/19930084178
• Moeckel, W. E., and P. J. Evans Jr. 1951. Preliminary Investigation of Use of Conical Flow Separation for Efficient Supersonic Diffusion. NACA-RM-E51J08. NASA. https://ntrs.nasa.gov/citations/19930090411
• Moeckel, W. E., and J. C. Evvard. 1948. Load Distributions Due to Steady Roll and Pitch for Thin Wings at Supersonic Speeds. NACA-TN-1689. NASA. https://ntrs.nasa.gov/citations/19930082327
• Moes, Timothy R., Brent R. Cobleigh, Timothy H. Cox, Timothy R. Conners, Kenneth W. Iliff, and Bruce G. Powers. 1998. Flight Stability and Control and Performance Results from the Linear Aerospike SR-71 Experiment (LASRE). NASA/TM-1998-206565. NASA. https://ntrs.nasa.gov/citations/19980217098
• Moes, Timothy, and Stephen Whitmore. 1991. “Preliminary Results from an Airdata Enhancement Algorithm with Application to High-Angle-of-Attack Flight.” In 29th Aerospace Sciences Meeting. AIAA 1991-672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-672
• Mofidi Tabatabaei, H. 2023. “Effect of Friction Stir Forming Parameters on Mechanical Properties and Plastic Flow of Material in the Mechanical Interlocking of Optical Fiber and SP-700 Superplastic Titanium Alloy.” In Materials Research Proceedings, vol. 32. Materials Research Forum LLC. https://doi.org/10.21741/9781644902615-10
• Moga, Nicholas J. 1980. Optimal Bodies for Minimum Total Drag at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada091235
• Moga, N., and F. Dejarnette. 1981. “Optimal Bodies for Minimum Total Drag at Supersonic Speeds.” In 19th Aerospace Sciences Meeting. AIAA 1981-75. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-75
• Moguel, Hever Moncayo Israel. 2015. “Biologically-Inspired Approach for Aircraft Management under Upset Conditions.” Journal of Applied Mechanical Engineering 04 (01). https://doi.org/10.4172/2168-9873.1000147
• 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
• Mohamed, M., and N. Joy. 2021. “Lateral Directional Aircraft Aerodynamic Parameter Estimation Using Adaptive Stochastic Nonlinear Filter.” Aeronautical Journal 125 (1294): 2217–28. https://doi.org/10.1017/aer.2021.61
• Mohammed, A. R. 2007. “Effect of Airplane Tail Aspect Ratio on Lateral- Directional Stability.” Engineering and Technology Journal 25 (6): 746–56. https://doi.org/10.30684/etj.25.6.5
• Mohanty, R. 2013. “Climate Based Performance of Carbon-Carbon Disc Brake for High Speed Aircraft Braking System.” Defence Science Journal 63 (5): 531–38. https://doi.org/10.14429/dsj.63.3932
• Moin, Parviz, and Sanjiva K. Lele. 1998. Large Eddy Simulation of Supersonic Inlet Flows. Defense Technical Information Center. https://doi.org/10.21236/ada343835
• Monis, Renita Sharon, Aysha Shabana, Asha Crasta, and S. A. Khan. 2016. “Supersonic Flow Analysis and Evaluation of Damping Derivative.” IOSR Journal of Mechanical and Civil Engineering 16 (053): 29–36. https://doi.org/10.9790/1684-16053032936
• 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
• Montoya, L. C., and R. D. Banner. 1977. F-8 Supercritical Wing Flight Pressure, Boundary Layer, and Wake Measurements and Comparisons with Wind Tunnel Data. NASA-TM-X-3544. NASA. https://ntrs.nasa.gov/citations/19770022154
• Moore, F. L. 1969. An Investigation of the Effects of Roll-Spiral Coupling on the Lateral-Directional Handling Qualities of a STOL Subsonic Transport. NASA-TM-X-61898. NASA. https://ntrs.nasa.gov/citations/19690030716
• Moore, Frank, and L. Moore. 2008. “A New Method to Predict Nonlinear Roll Damping Moments.” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-4375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4375
• 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
• 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 A. 2021. “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, 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, and Vladislav Klein. 1995. “Determining the Accuracy of Aerodynamic Model Parameters Estimated from Flight Test Data.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3499
• Morelli, Eugene, and Mark Smith. 2008. “Real-Time Dynamic Modeling: Data Information Requirements and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6201
• 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
• Moritoki, Hitoshi. 1972. “Analytical Investigation on the Plastic Bending of Sheet Metal: 1st Report, Stress Distribution and Springback on the Bending and Re-Straightening Process of Rigid Plastic Sheet.” Transactions of the Japan Society of Mechanical Engineers 38 (314): 2514–24. https://doi.org/10.1299/kikai1938.38.2514
• Morris, Stephen James. 1990. “Integrated Aerodynamic and Control System Design of Oblique Wing Aircraft.” PhD diss., Stanford Univ.. https://ntrs.nasa.gov/citations/19930074026
• Morris, Asa, Christian Allen, and Thomas Rendall. 2008. “Wing Design by Aerodynamic and Aeroelastic Shape Optimisation.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-7054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7054
• Morris, S. J., Jr., W. P. Nelms Jr., and R. O. Bailey. 1976. A Simplified Analysis of Propulsion Installation Losses for Computerized Aircraft Design. NASA-TM-X-73136. NASA. https://ntrs.nasa.gov/citations/19770009073
• Morse, Daniel R., and James A. Liburdy. 2009a. “Experiments on the Velocity Field around a Low Aspect Ratio Wing at Low Reynolds Numbers.” In Volume 9: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B and C. ASMEDC. https://doi.org/10.1115/imece2009-13172
• Morse, Daniel R., and James A. Liburdy. 2009b. “Vortex Dynamics and Shedding of a Low Aspect Ratio, Flat Wing at Low Reynolds Numbers and High Angles of Attack.” Journal of Fluids Engineering 131 (5): 051202. https://doi.org/10.1115/1.3112385
• Morton, J. P. 1956. “A Programme for Low Aspect Ratio Wing Analysis: A Digital Computer Programme to Analyse the Structure of a Low Aspect Ratio Wing.” Aircraft Engineering and Aerospace Technology 28 (12): 415–18. https://doi.org/10.1108/eb032772
• Morton, Scott, and Philip Beran. 1995. “Nonlinear Analysis of Airfoil Flutter at Transonic Speeds.” In 13th Applied Aerodynamics Conference. AIAA 1995-1905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1905
• Mosby, L. 1965. “Ground Loads for Aircraft with Multiple Wheels and Multiple Landing Gear and with Requirements for Semi-Improved Airfield Operations.” In Low-Speed Flight Meeting. AIAA 1965-711. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-711
• Moses, Robert W. 2005. Blended Buffet-Load-Alleviation System for Fighter Airplane. LAR-16375-1. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20110014728
• Moskowitz, Barry, and W. E. Moeckel. 1950. First-Order Theory for Unsteady Motion of Thin Wings at Supersonic Speeds. NACA-TN-2034. NASA. https://ntrs.nasa.gov/citations/19930082691
• Moss, Steven W., Stanley R. Cole, and Robert V. Doggett Jr. 1991. “Some Subsonic and Transonic Buffet Characteristics of the Twin-Vertical-Tails of a Fighter Airplane Configuration.” In AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. https://ntrs.nasa.gov/citations/19910047386
• Moszczynski, Gregory J., Abhisehk Goudar, Angela Schoellig, Peter R. Grant, and Vincent Myrand-Lapierre. 2026. “On Flight Path Reconstruction in the Absence of Angle of Attack and Sideslip Measurements.” In AIAA SCITECH 2026 Forum. AIAA 2026-2659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2659
• 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, Maciej. 2019. “Hot Deformation of Quench Hardened Titanium Alloys as a Modern Production Method of High Strength Structural Parts?” Modern Concepts in Material Science 1 (4). https://doi.org/10.33552/mcms.2019.01.000518
• 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, Martin T., and Lawrence W. Brown. 1959. Effect of Artificial Pitch Damping on the Longitudinal and Rolling Stability of Aircraft with Negative Static Margins. NASA-MEMO-5-5-59L. NASA. https://ntrs.nasa.gov/citations/19980228212
• Moul, T., and L. 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 Aircraft Systems Meeting. AIAA 1980-1845. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1845
• Moulton, Ben, Troy Abraham, and Douglas F. Hunsaker. 2024. “Stick-Fixed Maneuver Points in Roll, Pitch, and Yaw and Associated Handling Qualities.” In AIAA SCITECH 2024 Forum. AIAA 2024-2480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2480
• Mount, J. 1964. “Effect of Inlet Additive Drag on Aircraft Performance.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-599
• Mouton, Sylvain, Sylvain Masseboeuf, and Raffaello Mariani. 2017. “Simulation of Atmospheric Boundary Layer Flow for Air Inlet Testing in F1 Wind-Tunnel.” In 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2017-4132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4132
• Movahedi, Mohammad Reza, and Mahdi Gerdooei. 2024. “Analytical Approach to Investigate the Effects of through-Thickness Stress on Springback in Bending of Isotropic Sheet Metal.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3926501/v1
• Mueller, J., K. Chiba, and Y. Oba. 2024. “Identification of Losses from Engine-Airframe Interaction for a Passenger Aircraft through Integrated Simulation.” In 9th European Congress on Computational Methods in Applied Sciences and Engineering. CIMNE. https://doi.org/10.23967/eccomas.2024.304
• Mugler, John P., Jr. 1957. Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-Aspect-Ratio Delta Wing in Combination with Basic and Indented Bodies. NACA-RM-L57G19. NASA. https://ntrs.nasa.gov/citations/19930089808
• Mugler, J. P., Jr. 1959. Effects of Three Spanwise Twist Variations on the Longitudinal Aerodynamic Characteristics of a Thin 45 Deg Sweptback Highly Tapered Wing at Transonic Speeds. NASA-TM-X-126. NASA. https://ntrs.nasa.gov/citations/19650003091
• Mukherjee, Amiya K., and A. Arieli. 1982. Fundamental Investigations of Superplastic Forming Processes. Defense Technical Information Center. https://doi.org/10.21236/ada118614
• Mukherjee, Bijoy K., and Manoranjan Sinha. 2016. “Modeling and Bifurcation Analysis of Combat Aircraft Dynamics under Lateral C.M. Shift.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1037. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1037
• Mukhopadhyay, Vivek. 1995. “Interactive Flutter Analysis and Parametric Study for Conceptual Wing Design.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3943
• Mullen, J., Jr. 1979. “Combined Strength and Aeroelastic Wing Synthesis via Constraint Approximation.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-724
• Murav’ev, Vasily, Pavel Bakhmatov, and Vladimir Grigor’ev. 2019. “Specific Defects Forming Features While Aircraft Bulky Titanium Structures Assembling.” Vestnik Moskovskogo aviatsionnogo instituta 26 (4): 17–27. https://doi.org/10.34759/vst-2019-4-17-27
• 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
• Murman, Scott M., Yehia M. Rizk, and Paul Kutler. 1994. Computational Investigation of an F-18 Aircraft in the High-Alpha Regime. MCAT Inst. https://ntrs.nasa.gov/citations/20010048685
• Murphy, Patrick, and Vladislav Klein. 2007. “On Problems Associated with Modeling Wing-Tail Configurations from Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6722
• 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 C., Vladislav Klein, and Neal T. Frink. 2016. “Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data: Invited.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-1042. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1042
• 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, A. C., R. P. Peloubet, R. M. Bolding, and J. J. Hosek. 1976. Design, Fabrication, Testing and Analysis of Torsion Free Wing Trend Flutter Models. Defense Technical Information Center. https://doi.org/10.21236/adb013257
• 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
• 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
• 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
• Musa, Nur Amalina, Shuhaimi Mansor, Airi Ali, and Shabudin Mat. 2026. “V-Tail Dihedral Effect on the Aircraft Directional Stability in Response to Crosswind Conditions.” Preprint, . https://doi.org/10.2139/ssrn.7319830
• Musial, Norman T. 1957. Comparison of Effect of a Turbojet Engine and Three Cold-Flow Configurations on the Stability of a Full-Scale Supersonicle Inlet. NACA-RM-E56K23. NASA. https://ntrs.nasa.gov/citations/19930089651
• Myers, D. E. 1962. Dod High Strength Titanium Alloy Sheet Research Program. Defense Technical Information Center. https://doi.org/10.21236/ad0287545
• Myers, L., and F. Burcham Jr. 1984. “Preliminary Flight Test Results of the F100 EMD Engine in an F-15 Airplane.” In 20th Joint Propulsion Conference. AIAA 1984-1332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1332
• Myers, M., P. Guruswamy, and P. Goorjian. 1983. “Flutter Analysis of a Transport Wing Using XTRAN3S.” In 24th Structures, Structural Dynamics and Materials Conference. AIAA 1983-922. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-922
• 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
• Naamane, A., and M. Hasnaoui. 2019. “Modeling and Experimentation of a Supersonic Flow around an Airfoil.” Modelling, Measurement and Control B 88 (2–4): 9–15. https://doi.org/10.18280/mmc_b.882-402
• NACA Conference on Aerodynamic Problems of Transonic Airplane Design. 1947. NASA-TM-804-2. NASA. https://ntrs.nasa.gov/citations/19790079919
• 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, Structures, and Flutter. 1957. NACA-CONF-1957. NASA. https://ntrs.nasa.gov/citations/19710070068
• NACA Conference on High-Speed Aerodynamics. a Compilation of Papers Presented. 1958. NACA-TM-X-67369. Ames Research Center. https://ntrs.nasa.gov/citations/19710069971
• NACA: University Conference on Aerodynamics. 1948. NASA-TM-80403. NASA. https://ntrs.nasa.gov/citations/19790079941
• Naceur, H. 2004. “Response Surface Methodology for the Design of Sheet Metal Forming Parameters to Control Springback Effects Using the Inverse Approach.” In AIP Conference Proceedings, vol. 712. AIP. https://doi.org/10.1063/1.1766826
• Nae, Catalin C. 2026. “Wind Tunnel Testing Using a Robotic Sting for Lateral-Directional Stability Evaluation of a Tailless SST Aircraft Configuration.” In AIAA SCITECH 2026 Forum. AIAA 2026-2110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2110
• Nagao, Tsukasa, Hidekazu Yoshida, Masakazu Sano, Tetsuya Sato, and Atsushi Hashimoto. 2019. “Numerical Analysis on Supersonic Inlet Buzz.” Aerospace Technology Japan, the Japan Society for Aeronautical and Space Sciences 18 (0): 81–89. https://doi.org/10.2322/astj.jsass-d-18-00007
• 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
• Nahas, Mahmoud Nadim. 1991. “The Finite Element Technique in the Determination of Wing Flutter Speed of Aircraft.” Journal of King Abdulaziz University-Engineering Sciences 3 (1): 61–70. https://doi.org/10.4197/eng.3-1.5
• Najafiyazdi, Alireza, Rabi Tahir, Evgeny Timofeev, and Sannu Molder. 2007. “Analytical and Numerical Study of Flow Starting in Supersonic Inlets by Mass Spillage.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5072. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5072
• Nakai, Eiichi, Toshiro Takagi, and Koji Isogai. 1967a. “Experimental and Calculated Results of Supersonic Flutter Characteristics of a Low Aspect-Ratio Flat-Plate Surfaces.” In Sounding Rocket Vehicle Technology Specialist Conference. AIAA 1967-1340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-1340
• Nakamura, Sadayuki. 1988. “Development of Free-Machining Pure Titanium and Free-Machining Titanium Alloys.” DENKI-SEIKO 59 (2): 79–86. https://doi.org/10.4262/denkiseiko.59.79
• Nakayama, Tomohiro, Tetsuya Sato, Masahiro Akatsuka, Atsushi Hashimoto, Takayuki Kojima, and Hideyuki Taguchi. 2011. “Investigation on Shock Oscillation Phenomenon in a Supersonic Air Inlet.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3094. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3094
• Naksuk, Nirut, Pattarawadee Poolperm, Jiradech Nakngoenthong, Waravut Printrakoon, and Rattanapon Yuttawiriya. 2022. “Experimental Investigation of Hot-Wire Laser Deposition for the Additive Manufacturing of Titanium Parts.” Materials Research Express 9 (5): 056515. https://doi.org/10.1088/2053-1591/ac6ec2
• Nam, Changho, Aditi Chattopadhyay, and Youdan Kim. 1998. “An Optimal Wing Planform Design for Aeroelastic Control.” In 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 1998-4834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4834
• Namkoung, Hyuck-Joon, Wooram Hong, Jungmin Kim, Junsok Yi, and Chong-Am Kim. 2012. “Effects of Angles of Attack and Throttling Conditions on Supersonic Inlet Buzz.” International Journal of Aeronautical and Space Sciences 13 (3): 296–306. https://doi.org/10.5139/ijass.2012.13.3.296
• Nangia, Raj, Mehdi Ghoreyshi, and Michel van Rooij. 2023. “Reynolds Number Effects on Transonic Designed Multi-Swept Combat Wing at Subsonic & Supersonic Speeds.” In AIAA SCITECH 2023 Forum. AIAA 2023-0821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0821
• Napolitano, Marcello, Giampiero Campa, Brad Seanor, and Yongkyu Song. 2001. “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
• Narayan, K. Yegna. 1975. “The Flow over a “High” Aspect Ratio Gothic Wing at Supersonic Speeds.” Aeronautical Quarterly 26 (3): 189–201. https://doi.org/10.1017/s0001925900007332
• Nardi, L. 1970. “Fighter Flight Control System Design Considerations.” In Fighter Aircraft Conference. AIAA 1970-515. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-515
• Naruse, Hiroki, Tatsuya Ishii, Hideshi Oinuma, et al. 2022. “Effect of Inlet Distortion with Crosswind on Aircraft-Engine Intake Aerodynamic Performance.” Transactions of the JSME (in Japanese) 88 (910): 21-00357-21-00357. https://doi.org/10.1299/transjsme.21-00357
• 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
• Nash, Daniel, Sebastian Timme, U. S. Vevek, and John Pattinson. 2025. “Study of Transonic Flutter and Shock Buffet on Benchmark Supercritical Wing.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3767. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3767
• Nastase, Adriana. 2008a. “The Aerodynamical Characteristics of Flying Configurations with Arbitrary Shapes, in Supersonic Flow.” In Computation of Supersonic Flow over Flying Configurations. Elsevier. https://doi.org/10.1016/b978-008044957-9.50008-1
• Nastase, Adriana. 2008b. “The Visualizations of the Surfaces of Pressure Coefficients and Aerodynamical Characteristics of Wedged Delta and Wedged Rectangular Wings, in Supersonic Flow.” In Computation of Supersonic Flow over Flying Configurations. Elsevier. https://doi.org/10.1016/b978-008044957-9.50009-3
• Nastase, A., and C. Rudianu. 1990. “Theoretical Prediction of Pressure Distribution on Wedged Delta Wing at Higher Supersonic Mach Numbers and Its Agreement with Experimental Results.” In Zeitschrift für Angewandte Mathematik und Mechanik Volume 70, Number 5. De Gruyter. https://doi.org/10.1515/9783112571101-032
• Nastase, A., and U. Weisensee. 1984. “Prediction of Pressure Distribution Cp on a Long Rectangular Wing in Transonic — Supersonic Flow.” In Zeitschrift für Angewandte Mathematik und Mechanik Volume 64, Number 4. De Gruyter. https://doi.org/10.1515/9783112550908-091
• Naval Ordnance Systems Command Washington DC. 1957. Handbook of Supersonic Aerodynamics Three-Dimensional Airfoils. Section 7. Volume 3. Defense Technical Information Center. https://doi.org/10.21236/ada278207
• Nävert, Uno G., and Yngve C.-J. Sedin. 1992. “Drag Prediction for Aircraft at Transonic Speed.” In European Consortium for Mathematics in Industry. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-663-09834-8_43
• Nayfeh, A. H., and D. T. Mook. 1978. Subsonic Aerodynamic Loads on Missiles. Defense Technical Information Center. https://doi.org/10.21236/ada061937
• Nazemizadeh, mostafa, mehran Samadi Foroushan, and mohamad mehdi mohammadi ghanaghestani. 2023. “Aerodynamic modeling and calculating the flutter speed of a rectangular plate in supersonic air flow.” Mechanic of Advanced and Smart Materials 3 (2): 194–215. https://doi.org/10.61186/masm.3.2.194
• Ndebele, B. B. 2025. “Flat Plate Flutter in a Supersonic Flow Field.” In Proceedings of the 34th International Symposium on Shock Waves, Volume 3: Applications 2. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-4775-0_38
• 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, T., and R. Smith. 1970a. “Development of a Flying Qualities Criterion for the Design of Fighter Flight Control Systems.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-927. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-927
• Neal, T. P., and Rogers E. Smith. 1970b. An in-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 1. Defense Technical Information Center. https://doi.org/10.21236/ad0880426
• Neaves, Michael D., and D. Scott McRae. 1995. “Numerical Investigation of the Unstart Phenomenon in an Axisymmetric Supersonic Inlet.” In Computational Fluid Dynamics in Aeropropulsion. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0407
• Neaves, Michael, D. McRae, and Jack Edwards. 2001. “High-Speed Inlet Unstart Calculations Using an Implicit Solution Adaptive Mesh Algorithm.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-825. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-825
• 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
• Neihouse, A. I. 1940. The Aileron as an Aid to Recovery from the Spin. NACA-TN-776. NASA. https://ntrs.nasa.gov/citations/19930081639
• Neihouse, A. I., and J. W. Klinar. 1942. Spin Tests of a 1/20-Scale Model of the Bell XP-39E Airplane. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/20150015767
• Nele, Luigi, and Roberto Teti. 2018. “Advanced Technologies in Drilling of Light Alloys and CFRP Hybrid Stacks for Airframe Structure Manufacturing in the Aerospace Industry.” In Machining of Light Alloys. CRC Press. https://doi.org/10.1201/b22153-8
• Nelson, H. 1990. “Potential Flow Approach for Wing Body Interference for Missiles in Supersonic Flow.” In 28th Aerospace Sciences Meeting. AIAA 1990-277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-277
• Nelson, Herbert C., and Julian H. Berman. 1953. Calculations on the Forces and Moments for an Oscillating Wing-Aileron Combination in Two-Dimensional Potential Flow at Sonic Speed. NACA-TR-1128. NASA. https://ntrs.nasa.gov/citations/19930092163
• Nelson, Herbert C., Ruby A. Rainey, and Charles E. Watkins. 1954. Lift and Moment Coefficients Expanded to the Seventh Power of Frequency for Oscillating Rectangular Wings in Supersonic Flow and Applied to a Specific Flutter Problem. NACA-TN-3076. NASA. https://ntrs.nasa.gov/citations/19930083750
• Nenni, J. P., and C. Tung. 1971. A Second Order Slender Wing Theory for Wings with Leading Edge Separation in Supersonic Flow. NASA-CR-1860. NASA. https://ntrs.nasa.gov/citations/19710024528
• Neto, D. M., M. C. Oliveira, J. L. Alves, A. D. Santos, and L. F. Menezes. 2016. “Prediction of Wrinkling and Springback in Sheet Metal Forming.” MATEC Web of Conferences 80: 03005. https://doi.org/10.1051/matecconf/20168003005
• Neville, W., S. O’Flarity, and C. Selvidge. 1992. “Flight Testing the Prototype Advanced Tactical Fighter Engine.” In Aerospace Design Conference. AIAA 1992-1036. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1036
• Nevo, Jedidiah C., Karl Y. Kurniawan, Henry Saari, and Hamza M. abo El Ella. 2025. “Optimum Pressure Ratio in a Turbojet Engine: Mathematical Expression to Determine the Pressure Ratio Required for Optimization of the Specific Thrust.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2025-153051
• Newey, William Barton D. n.d. “A Study of the Utilization of Panel Method for Low Aspect Ratio Wing Analysis.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2020.107
• Newman, Michael, Ben D. Lawson, Braden J. McGrath, and Angus H. Rupert. 2014. “Perceptual Modeling as a Tool to Prevent Aircraft Upset Associated with Spatial Disorientation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-0443. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0443
• 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
• Newsome, R. 1985. “A Comparison of Euler and Navier-Stokes Solutions for Supersonic Flow over a Conical Delta Wing.” In 23rd Aerospace Sciences Meeting. AIAA 1985-111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-111
• 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, Nhan. 2008. “Integrated Flight Dynamic Modeling of Flexible Aircraft with Inertial Force-Propulsion-Aeroelastic Coupling.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-194
• Nguyen, L. T., W. P. Gibert, and S. B. Grafton. 1979a. “Control Considerations for CCV Fighters at High Angles of Attack.” In AGARD. https://ntrs.nasa.gov/citations/19790053282
• Nguyen, Luat T., William P. Gilbert, and Marilyn E. Ogburn. 1980. Control-System Techniques for Improved Departure/spin Resistance for Fighter Aircraft. NASA-TP-1689. NASA. https://ntrs.nasa.gov/citations/19800020743
• Nguyen, Le Thanh, Quoc Quan Nguyen, and Ha Hiep Nguyen. 2023. “Research on Operating Characteristics of Single-Spool Turbojet Enginewith the Afterburner AL-21F.” Ministry of Science and Technology, Vietnam 65 (3): 39–45. https://doi.org/10.31276/vjst.65(3).39-45
• Nguyen, L. T., M. E. Ogburn, W. P. Gilbert, K. S. Kibler, P. W. Brown, and P. L. Deal. 1979b. 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., Eric Ting, and Sonia Lebofsky. 2016. “Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft.” In 15th Dynamics Specialists Conference. AIAA 2016-1094. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1094
• Nguyen, Nhan, and Ilhan Tuzcu. 2009. “Flight Dynamics of Flexible Aircraft with Aeroelastic and Inertial Force Interactions.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-6045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6045
• Nguyen, Nam Thanh, Cuong Van Vo, Dien Khanh Le, and Sy Van Le. 2010. “A Calculation for Compensating the Errors Due to Springback When Forming Metal Sheet by Single Point Incremental Forming (Spif).” Science and Technology Development Journal 13 (3): 14–24. https://doi.org/10.32508/stdj.v13i3.2131
• Nharwal, Tarun, and Kishan Pal Singh. 2026. “Effect of Variation in Elastic Properties on Springback in Aluminium Sheet Metal Forming: A Parametric Finite Element Study with Four Drawbead Geometries.” Adolescência e Saúde: 1693–1701. https://doi.org/10.67440/ahj.vi.2178
• 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
• Nicholas, Joseph L. 2007. “Advanced Dynamic Simulation for Determination of Landing Gear Loads.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f63-000237
• Nichols, R., A. Denny, J. Calahan, J. Sirbaugh, J. Klepper, and B. Heikkinen. 2011. “Firebolt v2.0: Structured Grid Navier-Stokes Code for Airframe/Propulsion Integration.” In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2011-5970. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-5970
• Nichols, Mark R., and Edwin B. Goral. 1952. A Low-Speed Investigation of a Fuselage-Side Air Inlet for Use at Transonic Flight Speeds. NACA-TN-2684. NASA. https://ntrs.nasa.gov/citations/19930083896
• Nichols, R., and Bonnie Heikkinen. 2010. “Firebolt: A High Fidelity Computational Tool for Airframe/Propulsion Integration.” In U.S. Air Force T&E Days 2010. AIAA 2010-1720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1720
• Nichols, Robert H., David R. McDaniel, Todd Tuckey, Roy Koomullil, Yasushi Ito, and Jason Klepprt. 2015. “Firebolt c2.0: Unstructured Grid Navier-Stokes Code for Airframe/Propulsion Integration.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0043
• Nichols, Mark R., and Robert E. Pendley. 1952. Performance of Air Inlets at Transonic and Low Supersonic Speeds. NACA-RM-L52A07. NASA. https://ntrs.nasa.gov/citations/19930086995
• Nichols, Mark R., and Donald W. Rinkoski. 1952. A Low-Speed Investigation of an Annular Transonic Air Inlet. NACA-TN-2685. NASA. https://ntrs.nasa.gov/citations/19930083216
• Nicolaides, John D. 1952. Variation of the Aerodynamic Force and Moment Coefficients with Reference Position. Defense Technical Information Center. https://doi.org/10.21236/ad0005541
• 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, Agostino De Marco, Vito Sabetta, and Pierluigi Della Vecchia. 2015. “Roll Performance Assessment of a Light Aircraft: Flight Tests and Flight Simulation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2238. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2238
• Nie, Yuanbo, Tobias Bellmann, Andreas Labusch, Gertjan Looye, Erik-Jan Van Kampen, and Q. Ping Chu. 2015a. “Aircraft Upset and Recovery Simulation with the DLR Robot Motion Simulator.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-1142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1142
• Nie, Baoping, Zhufei Li, Rong Fung Huang, and Jiming Yang. 2019. “Effect of Boundary Layer Suction on Shock Train Oscillations in an Inlet/Isolator Model.” In International Symposium on Shock Waves (ISSW). https://doi.org/10.3850/978-981-11-2730-4_0155-cd
• Nie, Yuanbo, Erik-Jan Van Kampen, Q. Ping Chu, Thiemo M. Kier, and Gertjan Looye. 2015b. “Geometry Based Quick Aircraft Modeling Method for Upset Recovery Applications.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-2034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2034
• Nielsen, Jack N. 1947. Effect of Aspect Ratio and Taper on the Pressure Drag at Supersonic Speeds of Unswept Wings at Zero Lift. NACA-TN-1487. NASA. https://ntrs.nasa.gov/citations/19930082144
• Nielsen, Jack N. 1955. Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment. NACA-TR-1252. NASA. https://ntrs.nasa.gov/citations/19930090999
• Nielsen, J. 1986. “Supersonic Wing-Body Inteference at High Angles of Attack with Emphasis on Low Aspect Ratios.” In 24th Aerospace Sciences Meeting. AIAA 1986-568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-568
• Nielsen, Jack N., George E. Kaattari, and Robert F. Anastasio. 1953. A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds. NACA-RM-A53G08. NASA. https://ntrs.nasa.gov/citations/19930093732
• Nielsen, Jack N., and William C. Pitts. 1952. Wing-Body Interference at Supersonic Speeds with an Application to Combinations with Rectangular Wings. NACA-TN-2677. NASA. https://ntrs.nasa.gov/citations/19930083838
• Nietubicz, Charles J. 1975. Some Aerodynamic Characteristics of Supersonic Lifting Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada009704
• Nikaido, Ben, and Garth V. Hobson. 2025. “RANS Predictions of Inlet/Isolator Unstart at Mach 4.” In AIAA SCITECH 2025 Forum. AIAA 2025-0335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0335
• Nikhare, Chetan P. 2019. “Bending and Springback Analysis on Sheet Metal Material Discontinuity.” In Volume 2: Processes; Materials. American Society of Mechanical Engineers. https://doi.org/10.1115/msec2019-2905
• Nikhare, Chetan P. 2020. “Effect of Metal-Composite Layer Thickness on Springback after U-Bending.” In Volume 2A: Advanced Manufacturing. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2020-23155
• Nikhare, Chetan. 2021. “Effect of Metal-Composite Layer Thickness on Springback after U-Bending.” Preprint, . https://doi.org/10.1115/1.0003972v
• Niknam, Seyed Ali, Raid Khettabi, and Victor Songmene. 2014. “Machinability and Machining of Titanium Alloys: A Review.” In Materials Forming, Machining and Tribology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9_1
• Nikolaidis, Theoklis, Alvise Pellegrini, Herbert I. H. Saravanamuttoo, Ioanna Aslanidou, Anestis Kalfas, and Pericles Pilidis. 2022. “Off-Design Performance Comparison between Single and Two-Shaft Engines Part 1—Fixed Geometry.” Journal of Engineering for Gas Turbines and Power 144 (8): 081006. https://doi.org/10.1115/1.4054749
• 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
• Nikoueeyan, Pourya, and Jonathan Naughton. 2022. “Analysis of the Unsteady Surface Pressure Distribution of a Pitching Airfoil Using Modal Decomposition.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-1910091/v1
• Ning, Jingchong. n.d. “Numerical Analysis of the Influence of DBD Plasma Actuator on Supersonic Inlet Flow near Inlet Tip for Unstart Mitigation.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2026-17071
• Noftz, Mark E., and Joseph S. Jewell. 2025. “Unstart Modes of a Streamtraced Busemann Inlet in Mach 6 Quiet Flow.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3620
• Noll, T., R. Calico, and F. Eastep. 1983. “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., 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
• Noll, T., L. Huttsell, and D. Cooley. 1980. “Investigation of Internal Control Laws for Wing/store Flutter Suppression.” In 21st Structures, Structural Dynamics, and Materials Conference. AIAA 1980-764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-764
• Noma, Nobuyasu, Toshihiko Kuwabara, Francisco Chinesta, Yvan Chastel, and Mohamed El Mansori. 2011. “Springback Analysis of Draw-Bending of 980 MPa Cold Rolled Steel Sheet and Its Experimental Validation.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3552397
• Nomura, Toshiyuki. 2003. “Stability Analysis of Supersonic Swept-Wing Boundary Layers.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-4145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4145
• “Nonlinear Aerolasticity, Continuum Theory, Flutter/divergence Speed, Plate Wing Model.” 2007. In Free and Moving Boundaries. Chapman and Hall/CRC. https://doi.org/10.1201/9781420011159-15
• Noori, F., M. Gorji, A. Kazemi, and H. Nemati. 2010. “Thermodynamic Optimization of Ideal Turbojet with Afterburner Engines Using Non-Dominated Sorting Genetic Algorithm II.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 224 (12): 1285–96. https://doi.org/10.1243/09544100jaero771
• Norman, D., R. Hynes, and D. Gangsaas. 1983. “An Integrated Maneuver Enhancement and Gust Alleviation Mode for theAFTI/F-111 MAW Aircraft.” In Guidance and Control Conference. AIAA 1983-2217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2217
• Norris, R., S. Paris, and E. White. 1989. “The Flying Wind Tunnel.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3378
• Northrop Aircraft INC Hawthorne CA. 1952a. 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. 1952b. Research on High Lift Boundary Layer Suction Investigations on Thin High Speed Wings. Defense Technical Information Center. https://doi.org/10.21236/ad0004591
• Northrop Aircraft INC Hawthorne CA. 1953a. Dynamics of the Airframe. Defense Technical Information Center. https://doi.org/10.21236/ad0022941
• Northrop Aircraft INC Hawthorne CA. 1953b. Research on High Lift Boundary Layer Suction Investigations on Thin High Speed Wings. Defense Technical Information Center. https://doi.org/10.21236/ad0013465
• Norton, F. H. 1923. The Pressure Distribution over the Horizontal Tail Surfaces of an Airplane I. NACA-TR-118. NASA. https://ntrs.nasa.gov/citations/19930091182
• 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
• Norton, F. H., and D. L. Bacon. 1921. The Pressure Distribution over the Horizontal Tail Surfaces of an Airplane II. NACA-TR-119. NASA. https://ntrs.nasa.gov/citations/19930091183
• Norton, F. H., and W. G. Brown. 1923. Pressure Distribution over the Rudder and Fin of an Airplane in Flight. NACA-TR-149. NASA. https://ntrs.nasa.gov/citations/19930091214
• Nouari, M., Madalina Calamaz, B. Haddag, and Franck Girot. 2013. “Analysis of Coating Performances in Machining Titanium Alloys for Aerospace Applications.” International Journal of Machining and Machinability of Materials 13 (2/3): 158. https://doi.org/10.1504/ijmmm.2013.053220
• Nouari, Mohammed, and Hamid Makich. 2014. “Analysis of Physical Cutting Mechanisms and Their Effects on the Tool Wear and Chip Formation Process When Machining Aeronautical Titanium Alloys: Ti-6Al-4V and Ti-55531.” In Materials Forming, Machining and Tribology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9_4
• 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
• Null, null. 2025. Aircraft Tire Selection and Qualification. https://doi.org/10.4271/arp6822
• Null, null. 2026a. Aircraft Tire Chine Design. https://doi.org/10.4271/air8776
• Null, null. 2026b. Airplane Design and Test Considerations for Tire Spray Suppression. https://doi.org/10.4271/arp1904
• Nussdorfer, Theodore J., Leonard J. Obery, and Gerald W. Englert. 1952. Pressure Recovery, Drag, and Subcritical Stability Characteristics of Three Conical Supersonic Diffusers at Stream Mach Numbers from 1.7 to 2.0. NACA-RM-E51H27. NASA. https://ntrs.nasa.gov/citations/19930086890
• Nyberg, S.-E., and H. Sorensen. 1980. “Experimental Investigation of the Interference-Free Flow Field around a Lifting Wing-Body Model to Establish Cross Flow Characteristics for Ventilated Wind Tunnel Walls at Low Supersonic Mach Numbers.” In 11th Aerodynamic Testing Conference. AIAA 1980-444. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-444
• O’Donnell, Richard S., and Kamran Mohseni. 2017. “Manipulation of Wing Tip Vortices on Low Aspect Ratio Wings Using Winglet Control Surfaces.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1270
• 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
• Oberkampf, W. 1974. “Theoretical Prediction of Roll Moments on Finned Bodies in Supersonic Flow.” In 12th Aerospace Sciences Meeting. AIAA 1974-111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-111
• Oberkampf, W. 1978. “Symmetric Body Vortex Wake Characteristics in Supersonic Flow.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1337
• Obermark, Jeff. 2004. Verification of Simulation Results Using Scale Model Flight Test Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ada422954
• Obey, Leonard T., Gerald W. Englert, and Theodore J. Nussdorfer Jr. 1952. Pressure Recovery, Drag, and Subcritical Stability Characteristics of Conical Supersonic Diffusers with Boundary-Layer Removal. NACA-RM-E51H29. NASA. https://ntrs.nasa.gov/citations/19930094389
• Obikane, Y. 1984. “Numerical Computation of the Reynolds Stress in Supersonic Inlet Flows.” In 20th Joint Propulsion Conference. AIAA 1984-1364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1364
• Oblique Wing Aircraft. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch10
• Oehman, W. I. 1983. Stability and Control of a Supersonic Transport Airplane during Landing Approach. NASA-TM-84659. NASA. https://ntrs.nasa.gov/citations/19830015046
• 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, Hideo, Kento Shigeishi, and Junichi Koyama. 2006. “Sheet Metal V-Bending without Springback.” Journal of the Japan Society for Technology of Plasticity 47 (541): 144–48. https://doi.org/10.9773/sosei.47.144
• Ogburn, Marilyn, John Foster, and Keith Hoffler. 1991. “Use of Piloted Simulation for High-Angle-of-Attack Agility Research and Design Criteria Development.” In Flight Simulation Technologies Conference. AIAA 1991-2954. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2954
• Ogburn, Marilyn, John Foster, Joseph Pahle, R. Wilson, and James Lackey. 1993. “Status of the Validation of High-Angle-of-Attack Nose-down Pitch Control Margin Design Guidelines.” In Flight Simulation and Technologies. AIAA 1993-3623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3623
• Ogburn, Marilyn, Luat Nguyen, and Keith Hoffler. 1988. “Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4357
• Oggioni, Riccardo Andrew, Carlo Emanuele Dionigi Riboldi, and Filippo Coacci. 2026. “Wind Tunnel Investigation of Spoileron Effectiveness on a Low-Aspect-Ratio Swept Wing with Reflex Airfoils.” In IOCAE 2026. MDPI. https://doi.org/10.3390/engproc2026142017
• 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
• Oh, Jong, and Vigor Yang. 1994. “Interactions between Shock and Acoustic Waves in a Supersonic Inlet Diffuser.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-2706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2706
• Ohme, Per. 2009. “A Model-Based Approach to Aircraft Takeoff and Landing Performance Assessment.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-6154. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6154
• Ojiaku, Favour, and Atma Prakash. 2026. “CFD Analysis of Supersonic Flow on Aircraft Wing.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9271663/v1
• Okabe, Taika, Takeshi Miyazaki, Kenichi Saitoh, and Hirotaka Sakaue. 2013. “Unsteady Pressure Distribution on a Fluttering Airfoil Using Motion-Capturing PSP System.” In 44th AIAA Thermophysics Conference. AIAA 2013-3014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3014
• Okada, Hideki, Takumi Wada, Hiroki Oribe, et al. 2023. “Intelligence Press Brake for Aircraft Skin Bending.” In Key engineering materials, vol. 968. Trans Tech Publications. https://doi.org/10.4028/p-7uqwd5
• Okafor, Anthony Chukwujekwu. 2020. “Cooling and Machining Strategies for High Speed Milling of Titanium and Nickel Super Alloys.” In High Speed Machining. Elsevier. https://doi.org/10.1016/b978-0-12-815020-7.00005-9
• Oktay, E., and C. Asma. 2000. “Drag Prediction with a Euler Solver at Supersonic Speeds.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-392
• Olsen, Michael, and H. Seegmiller. 1992. “Low Aspect Ratio Wing Code Validation Experiment.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-402
• Olson, W. T., J. H. Childs, and E. R. Jonash. 1955. “The Combustion-Efficiency Problem of the Turbojet at High Altitude.” Journal of Fluids Engineering 77 (5): 605–15. https://doi.org/10.1115/1.4014444
• Olwi, Ibrahim. 1995. “Side Gust Loads on a Fighter Aircraft during Maneuver.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3465
• Omran, Ashraf, and Brett Newman. 2010. “Aircraft Volterra Parameter-Varying Modeling Approach.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7804. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7804
• Ooi, Hong Yee Julian. 2024. “Aerodynamic Challenges and Innovations in Wing Designs for Supersonic Flight: A Comprehensive Review.” International Journal of Science and Healthcare Research 9 (4): 454–63. https://doi.org/10.52403/ijshr.20240450
• Ordaz, Irian, Sriram K. Rallabhandi, Eric J. Nielsen, and Boris Diskin. 2017. “Mitigation of Engine Inlet Distortion through Adjoint-Based Design.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3410
• 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
• Osborne, R. S. 1963. Stability and Control Characteristics of a 0.0667-SCALE Model of the Final Version of the North American X-15 Research Airplane Configuration 3 at Transonic Speeds. NASA-TM-X-758. NASA. https://ntrs.nasa.gov/citations/19630004371
• Osborne, R. S., and V. C. Stafford. 1960. Basic Pressure Measurements on a 0.0667-SCALE Model of the North American X-15 Research Airplane at Transonic Speeds. NASA-TM-X-344. NASA. https://ntrs.nasa.gov/citations/19630002684
• Osmon, R. 1967. “Improved Methods of Spillage Drag Prediction for Two-Dimensional Inlets.” In 3rd Propulsion Joint Specialist Conference. AIAA 1967-449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-449
• Ossa, William A., and Dick M. Royster. 1987. Material Characterization of Superplastically Formed Titanium (Ti-6Al-2Sn-4Zr-2Mo) Sheet. NASA-TP-2674. NASA. https://ntrs.nasa.gov/citations/19870010974
• Ostrander, M., M. Thomas, and J. Clegern. 1995. “Inlet Analysis for ATR-Powered Supersonic Missile.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2805
• Oswatitsch, Klaus. 1980. “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (the Efficiency of Shock Diffusers).” In Contributions to the Development of Gasdynamics. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-91082-0_18
• Otiefy, R. A. H., and H. M. Negm. 2010. “Wing Box Transonic-Flutter Suppression Using Piezoelectric Self-Sensing Actuators Attached to Skin.” Smart Materials and Structures 19 (12): 125001. https://doi.org/10.1088/0964-1726/19/12/125001
• ŌTomo, Shūji, and Kiran Ramesh. 2026. “Closed-Form Unsteady Thin-Airfoil Theory for High-Amplitude Problems.” Preprint, . https://doi.org/10.2139/ssrn.6438821
• Otto, Samuel E., Charles J. Trefny, and John W. Slater. 2015. “Inward-Turning Streamline-Traced Supersonic Inlet Design Method for Low-Boom, Low-Drag Applications.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3700. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3700
• Ouellette, Jeffrey A. 2025. “Using Importance Sampling Monte Carlo to Analyze Aircraft Takeoff and Landing.” In AIAA SCITECH 2025 Forum. AIAA 2025-1055. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1055
• Ouyang, Xing, Xiongqing Yu, and Yu Wang. 2014. “Flutter Analysis for Wing Structure Using Finite Element Modeling with Equivalent Stiffness.” Journal of Vibroengineering 16 (3): 1483–93. https://doi.org/10.21595/jve.2014.14973
• Owens, D. Bruce, Elaine M. Bryant, and Jewel B. Barlow. 2005. Free-to-Roll Investigation of the Pre-Production F/A-18E Powered Approach Wing Drop. AFIT-CI04-1033. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20050177128
• 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
• Oza, Utsav, Zhiwei Hu, and Xin Zhang. 2015. “Effect of Cavity Flow on Landing Gear Aerodynamic Loads.” In 22nd AIAA Computational Fluid Dynamics Conference. AIAA 2015-2288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2288
• 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
• Pačák, Tomáš, František Tatíček, and Michal Valeš. 2019. “Compensation of Springback in Large Sheet Metal Forming.” Acta Polytechnica 59 (5): 483–89. https://doi.org/10.14311/ap.2019.59.0483
• Padmanabhan, K. A., S. Balasivanandha Prabu, and S. Madhavan. 2016. “Superplastic Forming of Aerospace Materials.” In Indian Institute of Metals Series. Springer Singapore. https://doi.org/10.1007/978-981-10-2143-5_3
• Pagliuca, Giampaolo, and Matt Forster. 2022. “Aeroelastic Solutions of the AGARD 445.6 Wing Using Linear- and Nonlinear-CFD.” In AIAA SCITECH 2022 Forum. AIAA 2022-1326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1326
• Painter, W. D., and L. J. Caw. 1978. Design and Physical Characteristics of the Transonic Aircraft Technology (TACT) Research Aircraft. NASA-TM-56048. NASA. https://ntrs.nasa.gov/citations/19790005843
• Pal, D., and H. A. Gaberson. 1973. “Surmounting the Inherent Errors in the Trifilar Pendulum Measurement of Moment of Inertia.” Journal of the Acoustical Society of America 54 (1_Supplement): 292–292. https://doi.org/10.1121/1.1978066
• Palaniappan, Karthik, and Antony Jameson. 2004. “Bodies Having Minimum Pressure Drag in Supersonic Flow: Investigating Nonlinear Effects.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5383
• Palazzo, Edward B., and M. Leroy Spearman. 1954. Static Longitudinal and Lateral Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane at a Mach Number of 1.41. NACA-RM-SL54G08. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023310
• Palko, R. L. 1974. Experimental Verification of a Transonic Test Technique for Full-Scale Inlet/Engine Systems Simulating Maneuvering Attitudes. Defense Technical Information Center. https://doi.org/10.21236/ad0787659
• 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, J. R. 1956. “Some Aspects of Turbojet Performance Calculation at High Flight Mach Numbers: Problems of Performance Prediction in Truly Supersonic Engines.” Aircraft Engineering and Aerospace Technology 28 (11): 376–80. https://doi.org/10.1108/eb032757
• 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
• Palusamy, Arun, and Kenneth Sivier. 1993. “Conceptual Design of an Advanced Tactical Fighter-Bomber System.” In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-4010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4010
• Pamadi, B., and L. Taylor Jr. 1982. “An Estimation of Aerodynamic Forces and Moments on an Airplane Modelunder Steady State Spin Conditions.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1311
• Pan, Dartzi, and Jen-Chieh Cheng. 1994. “Unstructured Euler Flutter Analysis of Two-Dimensional Wing-Tail Configuration.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-284
• Pan, Yalin, and Jun Huang. 2018. “Research on Lateral-Directional Stability Augmentation System of Flying Wing Aircraft Based on Reliability Model.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (11): 4214–21. https://doi.org/10.1177/0954410018817449
• Pan, Ya Lin, and Jun Huang. 2019. “Effect of Aerodynamic Configuration Parameters on Lateral-Directional Stability of Double-Swept Flying Wing Aircraft.” Journal of Aerospace Technology and Management: e3919. https://doi.org/10.5028/jatm.v11.1074
• “Panel Flutter in a Low-Density Atmosphere.” 1991. In 29th Aerospace Sciences Meeting. AIAA 1991-746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-746
• Pany, Chıtaranjan. 2023. “Panel Flutter Numerical Study of Thin Isotropic Flat Plates and Curved Plates with Various Edge Boundary Conditions.” Politeknik Dergisi 26 (4): 1467–73. https://doi.org/10.2339/politeknik.1139958
• Parameswaran, V., G. Girija, and Jitendra Raol. 2003. “Estimation of Parameters from Large Amplitude Maneuvers with Partitioned Data for Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5703. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5703
• “Parameter Sensitivity of High-Speed Aircraft.” 2010. In Multiple Scales Theory and Aerospace Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867644.0269.0291
• “A Parametric Sensitivity and Optimization Study for the Active Flexible Wing Wind-Tunnel Model Flutter Characteristics.” 1991. In 32nd Structures, Structural Dynamics, and Materials Conference. AIAA 1991-1054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1054
• Paranjape, Aditya, and N. Ananthkrishan. 2005. “Airplane Level Turn Performance, Including Stability Constraints, Using EBAC Method.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-5800. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5800
• 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, Sanghyuk. 2011. “Estimation Method Combining Aircraft Kinematics, GPS, and Low-Quality Rate Gyros.” Aircraft Engineering and Aerospace Technology 83 (3): 160–70. https://doi.org/10.1108/00022661111131258
• Park, Hyeon Don, Doyong Lee, Kim Ki Ro, Eunsa Kim, and Chongam Kim. 2023. “Effects of Boundary-Layer Bleed Slots on a Sidewall Compression Inlet.” In AIAA SCITECH 2023 Forum. AIAA 2023-1646. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1646
• 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
• Park, Chang-Doo, Ko Matuda, and Tadashi Tokai. 1996. “Effects of Wing-Tip Vortices on Lift of the Flat Plates with Low Aspect Ratio.” Nippon Suisan Gakkaishi 62 (2): 248–53. https://doi.org/10.2331/suisan.62.248
• Parker, Ellen, Charles Spain, and David Soistmann. 1991. “Aileron Buzz Investigated on Several Generic NASP Wing Configurations.” In 32nd Structures, Structural Dynamics, and Materials Conference. AIAA 1991-936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-936
• Parnell, L. A. 1986. “Flutter Analysis of Low Aspect Ratio Wings.” In COSMIC 14th NASTRAN (R) Users’ Colloquium. https://ntrs.nasa.gov/citations/19860016366
• Parris, W. M., R. G. Sherman, and H. D. Kessler. 1957. “Elevated-Temperature Properties of the 6 per Cent Aluminum, 4 per Cent Vanadium Titanium Alloy.” In Symposium on Titanium. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp44147s
• Pasley, L., W. Rohling, and W. Wattman. 1973. “Compatibility of Maneuver Load Control and Relaxed Static Stability.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-791. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-791
• “Passive Wing/store Flutter Suppression.” 1982. Journal of the Acoustical Society of America 71 (4): 1041–1041. https://doi.org/10.1121/1.387660
• Pastor-Barsi, Christine M., and John W. Slater. n.d. “Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5.” In AIAA SciTech Forum 2022. https://ntrs.nasa.gov/citations/20210024681
• Pasupuleti, Thejasree, Manikandan Natarajan, Pc Krishnamachary, Lakshmi Narasimhamu Katta, and R. Silambarasan. 2025. “Grey Relational Analysis for Multi-Objective Optimization in Aerospace Machining of Titanium Grade 19.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2025-28-0047
• Patel, Harinkumar, and Bernd Chudoba. 2026. “Advancing Early-Phase Conceptual Design Tool (AVDS) with Propulsion-Airframe Integration: Methodology and Verification.” Aircraft Engineering and Aerospace Technology 98 (6–7): 782–804. https://doi.org/10.1108/aeat-01-2025-0015
• Patel, Devang, Hardik Dodiya, and Sekar Saladi. 2025. “An Investigation of Springback, Thickness Distribution, and Sheet Thinning in Incremental Sheet Metal Forming Process for Aluminum Alloy AA8011.” In AIP Conference Proceedings, vol. 3330. AIP Publishing. https://doi.org/10.1063/5.0292015
• Patel, Anant, Alex Forbes, and Narayanan Komerath. 2011. “Drag Prediction for Supersonic Hydrogen-Fueled Airliners.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3968
• Patel, Kailen, and Demetrios Lefas. 2025. “Role of Shocks in Transonic Bending-Torsion Flutter.” In AIAA SCITECH 2025 Forum. AIAA 2025-0818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0818
• Patel, Y., and P. Smith. 1996. “Departure Analysis of a Twin-Finned, High Performance Combat Aircraft.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3369. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3369
• Patel, Purvic, and Gecheng Zha. 2021. “Improved Delayed Detached Eddy Simulation of AGARD Wing Flutter with Fully Coupled Fluid-Structure Interaction.” In AIAA Scitech 2021 Forum. AIAA 2021-0365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0365
• Pattinson, John, Mark Lowenberg, and Mikhail Goman. 2011. “Characterisation of Wind Tunnel Observed, Large-Amplitude Pitch Limit-Cycles.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6526
• Patton, J. M., Jr. 1980. NASA General Aviation Stall/spin Flight Testing. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19800024832
• Patton, J. M., Jr., H. P. Stough III, and D. J. Dicarlo. 1979. “Spin Flight Research Summary.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19790052693
• Paul, Alexander, Markus Werner, Ricardo Trân, and Dirk Landgrebe. 2017. “Hot Metal Gas Forming of Titanium Grade 2 Bent Tubes.” In AIP Conference Proceedings, vol. 1892. Author(s). https://doi.org/10.1063/1.5008054
• Paulsen, J., and G. Schadt. 1966. “A Study of the Pressure and Heat Transfer Distribution on Highly Swept Slab Delta Wings in Supersonic Flow.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-130
• 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
• Payne, J. 1968. “An Investigation of Optimization Criteria for the Aircraft Landing Flare Maneuver.” In 6th Aerospace Sciences Meeting. AIAA 1968-57. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-57
• Paynter, Gerald. 1994. “CFD Status for Supersonic Inlet Design Support.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-465
• Paynter, G., and H. Chen. 1983. “Progress toward the Analysis of Supersonic Inlet Flows.” In 19th Joint Propulsion Conference. AIAA 1983-1371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1371
• Paynter, Gerald, David Mayer, and Elling Tjonneland. 1993a. “Flow Stability Issues in Supersonic Inlet Flow Analyses.” In 31st Aerospace Sciences Meeting. AIAA 1993-290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-290
• Paynter, G. C., and E. Tjonneland. 1992. “Accuracy Issues in the Prediction of Supersonic Inlet Flows.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-400
• Paynter, Gerald, David Treiber, and W. Kneeling. 1992. “Modeling Supersonic Inlet Boundary Layer Bleed Roughness.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-269
• Peake, D., D. Fisher, and D. McRae. 1981. “Flight Experiments with a Slender Cone at Angle of Attack.” In 19th Aerospace Sciences Meeting. AIAA 1981-337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-337
• Pearson, H. A. 1937. Pressure-Distribution Measurements on O-2H Airplane in Flight. NACA-TR-590. NASA. https://ntrs.nasa.gov/citations/19930091665
• Pearson, Henry A., and William S. Aiken. 1946. Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane. NACA-WR-L-270. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092725
• Pearson, H. A., and J. B. Garvin. 1941. Velocity Gained and Altitude Lost in Recoveries from Inclined Flight Paths. NACA-TN-829. NASA. https://ntrs.nasa.gov/citations/19930081560
• Pearson, Henry A., William A. McGowan, and James J. Donegan. 1951. Horizontal Tail Loads in Maneuvering Flight. NACA-TR-1007. NASA. https://ntrs.nasa.gov/citations/19930092064
• Pearson, Henry A., William A. McGowna, and James J. Donegan. 1950. Horizontal Tail Loads in Maneuvering Flight. NACA-TN-2078. NASA. https://ntrs.nasa.gov/citations/19930082901
• Pechaud, Laure, and David Kim. 2001. “Maneuver Recognition and Prediction of Empennage Flight Loads of General Aviation Aircraft.” In 1st AIAA, Aircraft, Technology Integration, and Operations Forum. AIAA 2001-5273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-5273
• Pečinka, Jiří, Gabriel Thomas Bugajski, Petr Kmoch, and Adolf Jílek. 2017. “Jet Engine Inlet Distortion Screen and Descriptor Evaluation.” Acta Polytechnica 57 (1): 22–31. https://doi.org/10.14311/ap.2017.57.0022
• Peck, Robert F., and James A. Hollinger. 1953. A Rocket-Model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail Aspect Ratio 4.33. NACA-RM-L53F19a. NASA. https://ntrs.nasa.gov/citations/19930087734
• Pedreiro, Nelson. 1997. Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-Alpha. NASA-CR-203760. NASA. https://ntrs.nasa.gov/citations/19970017299
• Pedreiro, Nelson, Stephen Rock, Zeki Celik, and Leonard Roberts. 1996. “Roll-Yaw Control at High Angle of Attack by Forebody Tangential Blowing.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-773. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-773
• Peele, E. L., and C. V. Eckstrom. 1975. Strain-Gage Bridge Calibration and Flight Loads Measurements on a Low-Aspect-Ratio Thin Wing. NASA-TN-D-7979. NASA. https://ntrs.nasa.gov/citations/19750023957
• Pegram, James P., and William A. Anemaat. 2000. “Preliminary Estimation of Airplane Moments of Inertia Using CAD Solid Modeling.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/2000-01-1700
• Pejack, Edwin R., Joseph Meick, Adnan Ahmad, Nordin Lateh, and Omar Sadeq. 1988. Wind Tunnel Pressurization and Recovery System. NASA-CR-184591. NASA. https://ntrs.nasa.gov/citations/19890009128
• Pelikan, R. 1983. “F/A-18 High Angle of Attack Departure Resistant Criteria for Controllaw Development.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2126
• Pelletier, Alain, and Thomas Mueller. 1999. “Low Reynolds Number Aerodynamics of Low Aspect-Ratio Wings.” In 17th Applied Aerodynamics Conference. AIAA 1999-3182. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3182
• Pendleton, Edmund, Mark Lee, and Lee Wasserman. 1991. “An Application of the Active Flexible Wing Concept to an F-16 Derivative Wing Model.” In 32nd Structures, Structural Dynamics, and Materials Conference. AIAA 1991-987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-987
• 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
• Pendley, Robert E., and Harold L. Robinson. 1950. An Investigation of Several NACA 1-Series Nose Inlets with and without Protruding Central Bodies at High-Subsonic Mach Numbers and at a Mach Number of 1.2. NACA-RM-L9L23a. NASA. https://ntrs.nasa.gov/citations/19930093714
• Pengelley, C. D., and L. E. Wilson. 1954. Flutter Characteristics of a t-Tail. Defense Technical Information Center. https://doi.org/10.21236/ad0061591
• Pepoon, Philip W. 1943. Free-Spinning-Tunnel Tests of a Model of a Canard Airplane. NACA-WR-L-222. NASA. https://ntrs.nasa.gov/citations/19930093607
• Pepoon, Philip W. 1944. Spin-Tunnel Tests of a 1/57.33-Scale Model of the Northrop XB-35 Airplane. NACA-WR-L-739. NASA. https://ntrs.nasa.gov/citations/19930092703
• Pepper, Edward, and Gerald V. Foster. 1946. Longitudinal Stability and Stalling Characteristics of a 1/8.33-Scale Model of the Republic XF-12 Airplane. NACA-RM-L6L12. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019304
• “Performance Evaluation by Flight Tests.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0419.0462
• Perkins, C. 1969. “The Development of Airplane Stability and Control Technology.” In 6th Annual Meeting and Technical Display. AIAA 1969-1137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-1137
• Perry, Matthew, and David Miklosovic. 2012. “Tip Flowfield of a Low Aspect Ratio Circulation Control Wing with Spanwise Variation in Efflux.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2012-85266
• Perry, Elmer M., and John F. Rievley. 1961. Structural Flight Loads Data from Jet-Tanker Operations. Defense Technical Information Center. https://doi.org/10.21236/ad0259391
• Persoon, A., J. Horsten, and J. Meijer. 1983. “On Measuring Transonic Dips in the Flutter Boundaries of a Supercritical Wing in the Wind Tunnel.” In 24th Structures, Structural Dynamics and Materials Conference. AIAA 1983-1031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1031
• Persoon, A. J., R. Roos, and P. Schippers. 1980. Transonic and Low Supersonic Wind-Tunnel Tests on a Wing with Inboard Control Surface. Part I. General Description. Defense Technical Information Center. https://doi.org/10.21236/ada097094
• Perveen, Asma, and Samad Nadimi Bavil Oliaei. 2020. “Spark Erosion Machining of Aerospace Materials.” In Spark Erosion Machining. CRC Press. https://doi.org/10.1201/9780429085758-6
• 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
• Peters, M., J. Kumpfert, C. H. Ward, and C. Leyens. 2003. Titanium Alloys for Aerospace Applications. Wiley. https://doi.org/10.1002/3527602119.ch13
• Peters, M., and C. Leyens. 2003. Fabrication of Titanium Alloys. Wiley. https://doi.org/10.1002/3527602119.ch8
• 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
• Peterson, Eric D. 2024. “Linear Models for Lateral-Directional Aerodynamic Stability in Unsteady Flow.” In AIAA SCITECH 2024 Forum. AIAA 2024-2873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2873
• Peterson, J. B., Jr. 1982. “Wind-Tunnel/flight Correlation Program on XB-70-1.” In Wind-Tunnel(Flight Correlation, 1981. https://ntrs.nasa.gov/citations/19820017325
• Petersson, Ögmundur, Martin Leitner, and Felix Stroscher. 2010. “Structural Optimization Framework for Aircraft Subject to Transient Maneuver and Gust Loads.” In 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. AIAA 2010-9122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9122
• Petrak, Gerald J. 1970. An Investigation of Stress Corrosion Crack Arrest and Crack Propagation in a Titanium Alloy. Defense Technical Information Center. https://doi.org/10.21236/ad0720235
• Petre, A., and H. Ashley. 1975. “Drag Effects on Wing Flutter.” In 16th Structural Dynamics, and Materials Conference. AIAA 1975-775. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-775
• Petterson, Kristian. 2006. “Low-Speed Aerodynamic and Flowfield Characteristics of a UCAV.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-2986. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-2986
• 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
• Pfaff, Larry J. 1965. Force and Pressure Tests on a Semi-Span Delta Wing at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0467448
• 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, Werner, and Chandra S. Vemuru. 1988. “Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings.” In Aerospace Technology Conference and Exposition. https://ntrs.nasa.gov/citations/19890063986
• Pfyl, Frank A. 1955. An Investigation of the Effects of Nose and Lip Shapes for an Underslung Scoop Inlet at Mach Numbers from 0 to 1.9. NACA-RM-A55G13. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/19650003100
• Pfyl, Frank A., and Leroy L. Presley. 1961. Experimental Determination of the Recovery Factor and Analytical Solution of the Conical Flow Field for a 20 Deg Included Angle Cone at Mach Numbers of 4.6 and 6.0 and Stagnation Temperatures to 2600 Degree R. NASA-TN-D-353. NASA. https://ntrs.nasa.gov/citations/19980228128
• Pham, Quoc Tuan, Jung Han Song, Joong Cheul Park, and Young Suk Kim. 2019. “Investigation of Springback Prediction for an Aluminum 7000 Sheet Subjected to Press Forming.” Applied Mechanics and Materials 889: 203–10. https://doi.org/10.4028/www.scientific.net/amm.889.203
• Philipsen, Iwan, and Junnai Zhai. 2007. “Comparative Study of Strain-Gauge Balance Calibration Procedures Using the Balance Calibration Machine.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-143
• 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. 1948. Effect of Steady Rolling on Longitudinal and Directional Stability. NACA-TN-1627. NASA. https://ntrs.nasa.gov/citations/19930082293
• Phillips, E. P. 1969. Effect of Outdoor Exposure at Elevated Temperature on the Fatigue Life of Ti-8Al-1Mo-1V Titanium Alloy and AM 350 Stainless Steel Sheet. NASA-TN-D-5362. NASA. https://ntrs.nasa.gov/citations/19690023180
• Phillips, E. P. 1974. Effect of Outdoor Exposure at Ambient and Elevated Temperatures on Fatigue Life of Ti-6Al-4V Titanium Alloy Sheet in the Annealed and the Solution Treated and Aged Condition. NASA-TN-D-7540. NASA. https://ntrs.nasa.gov/citations/19740018251
• Phillips, W. 2000a. “An Accurate Closed Form Approximation for Dutch Roll.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-499
• Phillips, Warren F. 2013. “Analytical Decomposition of Wing Roll and Flapping Using Lifting-Line Theory.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2918. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2918
• Phillips, Alfred D., and Frank K. Everest. 1953. Phase 2 Performance and Stability Tests of the YF-100A Airplane. Defense Technical Information Center. https://doi.org/10.21236/ada636692
• 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
• Phinney, Davis G. 1959. “The JT12 Pratt & Whitney Aircraft’s 3000 Lb. Thrust Turbojet Engine.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/590349
• Phythian, J. E. 1966a. “Body-Wing Interference at Supersonic Speeds Part II. Overall Body-Wing Characteristics.” Journal of the Royal Aeronautical Society 70 (671): 1016–22. https://doi.org/10.1017/s0368393100082936
• Phythian, J. E. 1966b. “Body-Wing Interference at Supersonic Speeds: Part I. Pressure Distribution.” Journal of the Royal Aeronautical Society 70 (664): 497–505. https://doi.org/10.1017/s0001924000058139
• Piatak, David J., and Craig S. Cleckner. 2002. “A New Forced Oscillation Capability for the Transonic Dynamics Tunnel.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030013003
• Picard, Mary. 2002. F/A-18A/B/C/D Main Landing Gear Control Unit Hydraulic 2A Supply Line Pressure Spikes and Emergency Port Restrictor Ground and Flight Tests Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada409130
• Piccirillo, Albert. 1998. “Heinkel and the Turbojet Engine: Origin of the First Jet Fighter.” In AIAA and SAE, 1998 World Aviation Conference. AIAA 1998-5598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5598
• Pierson, B. 1972. “A Discrete Variable Approximation to Minimum Weight Panel Designs Subject to a Supersonic Flutter-Speed Constraint.” In 10th Aerospace Sciences Meeting. AIAA 1972-170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-170
• Piette, D. S., O. J. Crooks, W. B. McCreary, and F. Cazier Jr. 1985. “Experimental Transonic Steady State and Unsteady Pressure Measurement on a Supercritical Wing during Flutter and Forced Discrete Frequency Oscillations.” In 26th Structures, Structural Dynamics, and Materials Conference. AIAA 1985-664. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-664
• PiĽA, Ján, Peter Korba, and Michal Hovanec. 2017. “Safety Is Critical throughout All Stages of Aircraft Operation, from Air Mission to Ground Operation. One of the Most Important Airframe Systems That Influences the Efficacy of Ground Safety Is a Wheel Brake System. Aircraft Ground Speed Deceleration Requires the Dissipation of Kinetic Energy, Which Depends on Aircraft Weight and Speed. Significant Levels of Aircraft Kinetic Energy Must Be Dissipated in the Form of Heat Energy. the Brakes of Heavy Aircraft Are Especially Prone to Overheating during Landing and Taxiing on the Ground. the Aim of This Paper Is to Focus on the Dangers Caused by Aircraft Brakes When Overheating and Ways in Which to Eliminate Brake Overheating Problems from a Safety Perspective.” Scientific Journal of Silesian University of Technology. Series Transport 94: 175–86. https://doi.org/10.20858/sjsutst.2017.94.16
• Piland, Robert O. 1949. Summary of the Theoretical Lift, Damping-in-Roll, and Center-of-Pressure Characteristics of Various Wing Plan Forms at Supersonic Speed. NACA-TN-1977. NASA. https://ntrs.nasa.gov/citations/19930082644
• Piland, Robert O. 1951. Some Theoretical Characteristics of Trapezoidal Wings in Supersonic Flow and a Comparison of Several Wing-Flap Combinations. NACA-TN-2336. NASA. https://ntrs.nasa.gov/citations/19930082971
• Pilyugin, N. N., and V. S. Khlebnikov. 2005. “Study of the Effect of the Depth of the Cavity of a Braking Device on the Aerodynamic Drag of a Model in Transonic and Supersonic Flow.” Fluid Dynamics 40 (2): 332–37. https://doi.org/10.1007/s10697-005-0073-9
• Piovesan, Tommaso, Pavlos K. Zachos, David MacManus, et al. 2025. “Use of Non-Intrusive Flow Diagnostics for Aero-Engine Inlet Flow Distortion Measurements in an Industrial Wind-Tunnel.” In AIAA SCITECH 2025 Forum. AIAA 2025-2111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2111
• Pismennyi, V. L. n.d. “Bypass Turbojet Engine of Pismennyi.” In Scientific research of the SCO countries: synergy and integration. Crossref. https://doi.org/10.34660/inf.2019.16.36674
• Pitkin, Marvin. 1943. Effect of Wing Leading-Edge Slots on the Spin and Recovery Characteristics of Airplanes. NACA-WR-L-504. NASA. https://ntrs.nasa.gov/citations/19930092699
• Pitt, Franna, and Mamidala Ramulu. 2012. “Mechanical and Fatigue Properties of Titanium Alloy SP 700 after Simulated Superplastic Forming Conditions.” In Materials science forum, vol. 735. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.735.372
• Pittman, J. 1986. “Supersonic Airfoil Optimization.” In 4th Applied Aerodynamics Conference. AIAA 1986-1818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1818
• Pittman, James, and Daryl Bonhaus. 1987. “A Strake Design Method for Supersonic Speeds and Low Lift.” In 5th Applied Aerodynamics Conference. AIAA 1987-2638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2638
• Pittman, J., and G. Giles. 1986. “Combined, Nonlinear Aerodynamic and Structural Method for the Aeroelastic Design of a Three-Dimensional Wing in Supersonic Flow.” In 4th Applied Aerodynamics Conference. AIAA 1986-1769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1769
• Pivko, Svetopolk. 1956. “Pressure Distribution and Aerodynamic Properties of High-Speed Aircraft: A Method for Determining the Main Aerodynamic Properties of High-Speed Aeroplanes.” Aircraft Engineering and Aerospace Technology 28 (8): 259–61. https://doi.org/10.1108/eb032722
• Plaban, Punya, and Timothy T. Takahashi. 2021. “Aerodynamic Design Challenges of a Thin Transonic Wing.” In AIAA Aviation 2021 Forum. AIAA 2021-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2423
• Planeaux, James. 1990. “Bifurcation Analysis of a Model Fighter Aircraft with Control Augmentation.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2836. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2836
• 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
• Planeaux, James, and Thomas Barth. 1988. “High-Angle-of-Attack Dynamic Behavior of a Model High-Performance Fighter Aircraft.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4368
• Platanitis, George, and Thomas Strganac. 2003. “Analyses and Experiments of Suppression of Control Reversal Using a Wing Section with Multiple Control Surfaces.” In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2003-1488. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1488
• 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
• 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
• Platzer, M. 1965a. On Linearized Compressible Flow over Pulsating and Oscillating Bodies. NASA. https://ntrs.nasa.gov/citations/19650046429
• Platzer, M. F. 1965b. On Quasi-Slender Body Theory for Oscillating Low Aspect Ratio Wings and Bodies of Revolution in Supersonic Flow. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19660026259
• Plews, Larry. 1983. “Have Bounce Aircraft Test Results.” In 2nd Flight Testing Conference. AIAA 1983-2737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2737
• Plotkin, A. 1978. “Unsteady Transonic Thin-Airfoil Theory for Power-Law Upwash.” Journal of Applied Mechanics 45 (2): 440–41. https://doi.org/10.1115/1.3424324
• Podleski, S. D. 1993. “Installed F/A-18 Inlet Flow Calculations at 60 Deg Angle-of-Attack and 10 Deg Side Slip.” In SAE. https://ntrs.nasa.gov/citations/19930065698
• Podruzhin, Evgeny G., Artem R. Zagidulin, and Dmitry A. Shinkarev. 2021. “Drop Testing Simulation of the Mainline Aircraft Landing Gear.” Vestnik Moskovskogo aviatsionnogo instituta 28 (4): 106–17. https://doi.org/10.34759/vst-2021-4-106-117
• Poirier, D. R., and P. K. Sung. 2006. Simulating Macrosegregation in Var Ingots of Titanium Alloy during Solidification. Defense Technical Information Center. https://doi.org/10.21236/ada456517
• Pollock, Luke, and Graham Wild. 2024a. “An Examination of High-Speed Aircraft – Part 1: Past, Present, and Future.” Preprint, . https://doi.org/10.2139/ssrn.4729643
• Pollock, Luke, and Graham Wild. 2024b. “An Examination of High-Speed Aircraft: Part 2: Safety and Reliability.” Preprint, . https://doi.org/10.2139/ssrn.4765698
• Poncet-Montanges, Adrien, Jonathan E. Cooper, Dorian Jones, Ann Gaitonde, and Yves Lemmens. 2016. “Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling Applied to a 3D Wing.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2016-4010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4010
• Poncet-Montanges, Adrien, Dorian Jones, Ann Gaitonde, Jonathan E. Cooper, and Yves Lemmens. 2017. “Frequency Domain Approach for Transonic Aerodynamic Modelling Applied to a Viscous Wing.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0075
• Pond, James W. 1973. Run Flat Tire for C-130 Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0779728
• Pond, James W. 1977. Replaceable Tread Tire Prototype Development for C-130 Military Aircraft Flight Tests. Defense Technical Information Center. https://doi.org/10.21236/adb025971
• Poole, Richard J. 2010. Takeoff and Landing of Fixed-Wing Aircraft. Wiley. https://doi.org/10.1002/9780470686652.eae246
• Poolla, Chaitanya, and Abraham K. Ishihara. 2015. “Temporal Prediction of Aircraft Loss-of-Control: A Dynamic Optimization Approach.” Intelligent Control and Automation 06 (04): 241–48. https://doi.org/10.4236/ica.2015.64023
• Popescu, Bogdan. 2002. “Flutter Characteristics of the Reversed Sweep Wing.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1291. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1291
• Poplingher, Lior, and Daniella E. Raveh. 2023. “Stall Flutter of the Benchmark Supercritical Wing at High Angles of Attack.” In AIAA SCITECH 2023 Forum. AIAA 2023-0760. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0760
• Poplingher, Lior, and Daniella E. Raveh. 2024. “Computational Study of Stall Flutter of the Benchmark Supercritical Wing.” In AIAA SCITECH 2024 Forum. AIAA 2024-0828. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0828
• Porcher, C. E., and F. J. Thebiay. 1962. “Development of the Variable Geometry Inlet for the B-58 Airplane.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/620327
• 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
• Pototzky, Anthony S. 2014. “Roll Damping Derivatives from Generalized Lifting-Surface Theory and Wind Tunnel Forced-Oscillation Tests.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0731. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0731
• Poulinakis, Konstantinos, Dimitris Drikakis, Ioannis William Kokkinakis, and S. Michael Spottswood. 2023. “Deep Learning Reconstruction of Pressure Fluctuations in Supersonic Shock–boundary Layer Interaction.” Physics of Fluids 35 (7): 076117. https://doi.org/10.1063/5.0156444
• Powell, A., H. Welge, and C. Trefny. 1985. “Low-Speed Aerodynamic Test of an Axisymmetric Supersonic Inlet with Variable Cowl Slot.” In 21st Joint Propulsion Conference. AIAA 1985-1210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1210
• Powers, S., and M. Robinson. 1992. “Fighter Airframe/propulsion Integration: A Rockwell Perspective.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3334. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3334
• Prakash, Satya, Biju Uthup, and K. P. Singh. 2009. “A Computational Study of Onset of Pitch-Up on a Low Aspect Ratio Wing Fighter Aircraft Configuration.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3631
• Pramanik, Alokesh, Mohammad Nazrul Islam, Animesh Kumar Basak, and Guy Littlefair. 2013. “Machining and Tool Wear Mechanisms during Machining Titanium Alloys.” Advanced materials research 651: 338–43. https://doi.org/10.4028/www.scientific.net/amr.651.338
• Prandtl, L. 1928. Motion of Fluids with Very Little Viscosity. NACA-TM-452. NASA. https://ntrs.nasa.gov/citations/19930090813
• Prat, D., T. Surply, D. Gisquet, D. Prat, T. Surply, and D. Gisquet. 1997. “Application of CFD Methods to Propulsion System Integration in the Future Supersonic Transport Aircraft.” In 15th Applied Aerodynamics Conference. AIAA 1997-2212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2212
• Pratt, George L. 1955. Experimental Flutter Investigation of a Thin Unswept Wing at Transonic Speeds. NACA-RM-L55A18. NASA. https://ntrs.nasa.gov/citations/19930088680
• Pratt and Whitney Aircraft (United States), J. Larson, and DOE. 1960. J-58 Turbojet Engine for NAA B-70 Airplane. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12393926
• Praveen, P., and Seok-Soon Lee. 2017. “Meta-Model Based Approach to Minimize the Springback in Sheet Metal Forming.” International Journal of Mechanical Systems Engineering 3 (1). https://doi.org/10.15344/2455-7412/2017/121
• “Prediction and Verification of Aerodynamic Drag, Part I: Prediction.” 1985a. In Thrust and Drag: Its Prediction and Verification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865732.0121.0171
• “Prediction and Verification of Aerodynamic Drag, Part II: Wind-Tunnel/Flight Correlation of Lift, Drag, and Pitching Moment.” 1985b. In Thrust and Drag: Its Prediction and Verification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865732.0173.0206
• “Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment.” 1981. In Dynamics Specialists Conference. AIAA 1981-609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-609
• Preisighe Viana, Marcus Vinicius. 2025. “In-Flight Evaluation of Multipoint Loads Model for Flexible Aircraft Loads Monitoring.” In AIAA SCITECH 2025 Forum. AIAA 2025-0462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0462
• Prem, R., Prasobh J. Mechery, Sudeep Kb, and Suresh Mt. 2025. “Optimization of Turn around SortieTime of aTypical Fighter Aircraft by Enhancement of Brake System Heat Dissipation through Forced Convection.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-6186480/v1
• Premanond, Varunee, Pongpan Kaewtatip, Nutthanun Moolsradoo, Anak Khantachawana, and Komgrit Lawanwong. 2011. “Effect of Bending Direction on Springback of High Strength Steel Sheet.” Advanced materials research 299-300: 1103–6. https://doi.org/10.4028/www.scientific.net/amr.299-300.1103
• Price, H. L. 1943. “The Lateral Stability of Aeroplanes: Disturbed and Controlled Motions.” Aircraft Engineering and Aerospace Technology 15 (11): 325–30. https://doi.org/10.1108/eb031071
• 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, 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
• Pridham, Barry, Brian Ginty, and Adam B. Marriott. 2001. “Process Simulation of Superplastic Forming of Titanium Structure.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2001-01-2624
• 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
• Pritulo, T., A. Gubanov, and N. Voevodenko. 1995. “Favorable Interference of Optimized Wing-Body Combination with Inlet at Supersonic Speed.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3946
• Probstein, Ronald F. 1953. On the Flow at the Rear of a Two-Dimensional Supersonic Airfoil with Thickness. Defense Technical Information Center. https://doi.org/10.21236/ad0009822
• “Processing and Machining of Aerospace Metals.” 2012. In Introduction to Aerospace Materials. Elsevier. https://doi.org/10.1533/9780857095152.154
• “Production of Aerospace Titanium Parts from Powder by Laser Forming.” 2001. Metal Powder Report 56 (11): 39. https://doi.org/10.1016/s0026-0657(01)80812-2
• “Production Progress with Superplastic Forming and Diffusion Bonding at British Aerospace.” 1984. Aircraft Engineering and Aerospace Technology 56 (12): 5–6. https://doi.org/10.1108/eb036040
• 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
• 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
• Pruitt, V. R., and William F. Moroney. 1980. “Energy Maneuverability Displays for Air Combat Training.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/801185
• Pulley, J. K. 1977. Preliminary Design of Low-Cost Titanium Structure. Defense Technical Information Center. https://doi.org/10.21236/ada053327
• Purcarea, Mihail, and Andrei Dumitrescu. 2017. “Study Regarding the Springback of Metal Sheet Parts after Bending.” MATEC Web of Conferences 112: 02005. https://doi.org/10.1051/matecconf/201711202005
• Pusch, Manuel, Daniel Ossmann, Johannes Dillinger, Thiemo M. Kier, Martin Tang, and Jannis Lübker. 2019. “Aeroelastic Modeling and Control of an Experimental Flexible Wing.” In AIAA Scitech 2019 Forum. AIAA 2019-0131. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0131
• 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
• 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
• 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
• Pytka, Jaroslaw A. 2023a. “Airfield Performance of an Airplane – the State-of The-Art.” In Airplane Performance on Grass Airfields. CRC Press. https://doi.org/10.1201/9781003312765-2
• Pytka, Jaroslaw A. 2023b. “Modeling of Airfield Performance of Airplane on a Grass Runway.” In Airplane Performance on Grass Airfields. CRC Press. https://doi.org/10.1201/9781003312765-3
• Qi, Shaocong, Gaochao Yu, Liu Yang, et al. 2025. “Springback Characteristics of Metal Sheets under Reciprocating Bending Process.” Preprint, . https://doi.org/10.2139/ssrn.5518940
• Qian, Wei, and De Guan. 2012. “The Design, Manufacture and Wind Tunnel Test of the Full Aircraft Transonic Flutter Model.” Advanced materials research 487: 267–72. https://doi.org/10.4028/www.scientific.net/amr.487.267
• Qiao, Lina, Zhou Zhou, and Chi Zhang. 2018. “Static Aeroelastic Characteristics of Grid Structure Wing.” In 2018 Aviation Technology, Integration, and Operations Conference. AIAA 2018-4148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4148
• Qiushi, Li, Lv Yongzhao, and Li Shaobin. 2014. “A Quasi One-Dimensional Bleed Flow Rate Model for Terminal Normal Shock Stability in Mixed Compression Supersonic Inlet.” Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 228 (14): 2569–83. https://doi.org/10.1177/0954406213519975
• Quan, lidi, jiajie Du, bing Li, liangyou Li, and yuanbin Wang. 2024. “A Wavelet Neural Network Model Optimized by Gray Wolf Algorithm for Springback Prediction of Metal Tube Bending.” In Ninth International Symposium on Sensors, Mechatronics, and Automation System (ISSMAS 2023), edited by Lijia Pan, Zaifa Zhou. SPIE. https://doi.org/10.1117/12.3014764
• Quảng, Vũ Đức. 2025. “The Optimization of Rotary Bending Die Process: Criteria for the Metal Sheet Angles and Springback Effects.” Engineering Technology & Applied Science Research 15 (1): 20553–58. https://doi.org/10.48084/etasr.9706
• 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
• Quattrocchi, L. S., and D. A. Koss. 1992. Deformation Behavior of an Age-Hardenable Beta+Alpha-Two Titanium Alloy. Defense Technical Information Center. https://doi.org/10.21236/ada246362
• Quattrocchi, L. S., D. A. Koss, and G. Scarr. 1991. Precipitation Hardening of a Beta Titanium Alloy by the Alpha-Two Phase. Defense Technical Information Center. https://doi.org/10.21236/ada241566
• Qudeiri, Jaber E. Abu, Fayez Y. Abu Khadra, Usama Umer, and Hussein M. A. Hussein. 2015. “Response Surface Metamodel to Predict Springback in Sheet Metal Air Bending Process.” International Journal of Materials, Mechanics and Manufacturing 3 (4): 266–69. https://doi.org/10.7763/ijmmm.2015.v3.208
• 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
• 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
• Raab, Christian, and Kai Rohde-Brandenburger. 2020. “In-Flight Testing of MEMS Pressure Sensors for Flight Loads Determination.” In AIAA Scitech 2020 Forum. AIAA 2020-0512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0512
• Racisz, Stanley F. 1946. Development of Wing Inlets. NACA-ACR-L6B18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092761
• Rademakers, Ruud, Thomas Kächele, Stefan Bindl, and Reinhard Niehuis. 2014. “Approach for an Optimized Evaluation of Pressure and Swirl Distortion in S-Shaped Engine Inlet Con[|#12#|]figurations.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3594. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3594
• Radonjic, R., and M. Liewald. 2016. “Approaches for Springback Reduction When Forming Ultra High-Strength Sheet Metals.” IOP Conference Series: Materials Science and Engineering 159: 012028. https://doi.org/10.1088/1757-899x/159/1/012028
• Rafi, Melvin, Justin M. Schmitz, Robert Ross, James E. Steck, and Animesh Chakravarthy. 2022. “A Predictive and Adaptive Integrated Flight Display for Aircraft Loss-of-Control Avoidance.” In AIAA SCITECH 2022 Forum. AIAA 2022-1591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1591
• Rafi, Melvin, James E. Steck, and Animesh Chakravarthy. 2019. “Real-Time Adaptive Prediction of Loss-of-Control Margins on a Fourth Order Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-0368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0368
• Rafi, Melvin, James E. Steck, and Animesh Chakravarthy. 2020. “Adaptive Prediction of Aircraft Loss-of-Control Margins and Safe Control Envelopes with Longitudinally and Laterally Coupled Higher-Order Dynamics.” In AIAA Scitech 2020 Forum. AIAA 2020-0850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0850
• Rafi, Melvin, James E. Steck, and Animesh Chakravarthy. 2021. “Real-Time Adaptive Optimal Prediction of Safe Control Spaces and Augmented-Reality Head-Up Displays towards Aircraft Loss-of-Control Mitigation.” In AIAA Scitech 2021 Forum. AIAA 2021-0757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0757
• Rafi, Melvin, James E. Steck, Animesh Chakravarthy, and Tansel Yucelen. 2017. “Approaches to Real-Time Predictive Estimation of Loss-of-Control Events & Boundaries on Transport Aircraft.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1716
• Rafiq, Chaudry Rohan, and Waqar Ahmed Qureshi. 2022. “Development of a Computational Tool for Maneuver Loads Estimation in Initial Design Phase for Fighter Aircraft.” In The 2nd International Conference on Advances in Mechanical Engineering. MDPI. https://doi.org/10.3390/engproc2022023002
• Ragai, Ihab, and James A. Nemes. 2010. “Springback in Sheet Metal Forming of Stainless Steel 410.” In ASME 2010 International Manufacturing Science and Engineering Conference, Volume 2. ASMEDC. https://doi.org/10.1115/msec2010-34045
• Raghavan, Brijesh, and N. Ananthkrishnan. 2005a. “First-Principles Aerodynamic Modeling for Delta Wing Roll Dynamics.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-618
• Raghavan, Brijesh, and N. Ananthkrishnan. 2005b. “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
• Raghavan, Brijesh, and N. Ananthkrishnan. 2023. “Small-Perturbation Analysis of Airplane Dynamics with Dynamic Stability Derivatives Redefined.” Journal of Aerospace Sciences and Technologies: 365–80. https://doi.org/10.61653/joast.v61i3.2009.554
• Rahman, Mokdad Hayawi, Mohammed Wahhab Aljibory, Farhan Lafta Rashid, and Emad Qasem Hussein. 2022. “Sweep Angles Influence on the Aerodynamic Characteristics of NACA 2412 Wing with Supersonic Flow.” Mathematical Modelling of Engineering Problems 9 (3): 757–61. https://doi.org/10.18280/mmep.090323
• Rainey, Robert W. 1950. Pressure Measurements at Supersonic Speeds on a Section of a Rectangular Wing Having an NACA 65-009 Profile. NACA-RM-L9L16. NASA. https://ntrs.nasa.gov/citations/19930086240
• Rainey, A. Gerald, and William B. Igoe. 1958. Measurements of the Buffeting Loads on the Wing and Horizontal Tail of a 1/4-Scale Model of the X-1E Airplane. NACA-RM-L58F25. NASA. https://ntrs.nasa.gov/citations/19930093826
• 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
• Rajagopalan, R., and S. Siddiqi. 1985. “Aircraft Turbojet Engine Modeling Using Artificial Intelligence Techniques.” In 23rd Aerospace Sciences Meeting. AIAA 1985-253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-253
• Rajamurthy, M. S. 2002. “Modelling of the Nonlinear Lift and Pitching Moment Characteristics of 60 Degrees Delta Wing and Wing-Bodies.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4712
• Rajaram, Kiran, Melvin Rafi, James E. Steck, and Animesh Chakravarthy. 2017. “Laplace-Based Predictive Estimation of Loss-of-Control Boundaries on a Transport Aircraft.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1022
• 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, and Dimitri Mavris. 2003. “An Unstructured Wave Drag Code for Preliminary Design of Future Supersonic Aircraft.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3877
• Rallabhandi, Sriram, and Dimitri Mavris. 2008. “Simultaneous Airframe and Propulsion Cycle Optimization for Supersonic Aircraft Design.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-143
• Ramachandra, Lusitha S., Nicolas P. Avdelidis, and Ian K. Jennions. 2026. “Emissivity-Corrected Thermography for Post Landing Aircraft Wheel and Brake Cooling.” In Thermosense: Thermal Infrared Applications XLVIII, edited by Marc Genest, Giovanni Ferrarini, Peter Spaeth. SPIE. https://doi.org/10.1117/12.3097420
• 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
• Ramasubramanian, S. 2026. “Comparative Thermal and Structural Analysis of Aircraft Brake Disc Materials.” INTERANTIONAL JOURNAL OF SCIENTIFIC RESEARCH IN ENGINEERING AND MANAGEMENT 10 (4). https://doi.org/10.55041/ijsrem61915
• Rambacher, Collin B., Ethan J. Butler, and Jeffrey P. Bons. 2024. “Analysis of a Passive vs. Active Boundary Layer Fence on a Low Aspect Ratio Swept Wing in Subsonic Flow.” In AIAA SCITECH 2024 Forum. AIAA 2024-1936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1936
• Ramette, Philippe, and Jean Christophe Corde. 1992. “Aircraft Engine Integration for the M88-RAFALE Couple.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-403
• 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
• Ramprasadh, C., and V. Devanandh. 2015. “A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying Wing to Improve Lift Performance.” International Journal of Micro Air Vehicles 7 (3): 361–73. https://doi.org/10.1260/1756-8293.7.3.361
• Ran, Hongjun, and Dimitri Mavris. 2005. “Preliminary Design of a 2D Supersonic Inlet to Maximize Total Pressure Recovery.” In AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences. AIAA 2005-7357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-7357
• Ranard, E. D., and B. J. Davison. 1961. “Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic Transports.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/610097
• Rankin, James, Etienne Coetzee, Bernd Krauskopf, and Mark Lowenberg. 2008. “Nonlinear Ground Dynamics of Aircraft: Bifurcation Analysis of Turning Solutions.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2008-6529. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6529
• Rankin, James, Bernd Krauskopf, Mark Lowenberg, and Etienne Coetzee. 2010. “Operational Parameter Study of Aircraft Dynamics on the Ground.” Journal of Computational and Nonlinear Dynamics 5 (2): 021007. https://doi.org/10.1115/1.4000797
• 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. 2023. “System Identification and Parameter Estimation for Aircraft.” In Flight Mechanics Modeling and Analysis. CRC Press. https://doi.org/10.1201/9781003293514-10
• Rasmussen, H. 1968. “Captive Flight Testing by Means of Rocket Sleds.” In 3rd Aerodynamics Testing Conference. AIAA 1968-364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-364
• Ratchford, Jasmine, Jeremy Redding, and Luis Bravo. 2025. “Early Prediction of Inlet Unstart Using Upstream Flow Indicators.” Physics of Fluids 37 (11): 111701. https://doi.org/10.1063/5.0299691
• Ratnayake, Nalin, Erin Waggoner, and Brian Taylor. 2011. “Lateral-Directional Parameter Estimation on the X-48B Aircraft Using an Abstracted Multi-Objective Effector Model.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3014
• Rauh, G., and W. Anders. 1986. “Aircraft/Engine Integration for an Advanced Fighter Considering Mission Specifics.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/86-gt-295
• 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
• Ravichandran, K. S. 2000. Fatigue of Bet Titanium Alloys. Defense Technical Information Center. https://doi.org/10.21236/ada375114
• Rawe, R. A. 1967. Sustained-Load Tests of Partially Cracked 0.220-in. Solution-Treated and Aged Ti-6Al-4V. NASA-CR-83076. NASA. https://ntrs.nasa.gov/citations/19670014146
• Rayhan, Saiaf Bin, and Mohsin Islam. 2019. “Numerical Aero-Thermal-Structural Analyses of a Fighter Jet Wing during Supersonic Flights.” In AIP Conference Proceedings, vol. 2121. AIP Publishing. https://doi.org/10.1063/1.5115879
• Raymer, Daniel. 1991. “Post-Stall Maneuver and the Classic Turn Rate Plot.” In Aircraft Design and Operations Meeting. AIAA 1991-3170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3170
• Raymer, Daniel. 1995. “National Design of an Advanced Strike Fighter.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3922. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3922
• Readshaw, D. 1961. “Predicting Temperature Rises, Due to Aerodynamic Heating: An Analogue Method Utilizing Trajectory Data to Calculate Temperature Distribution throughout a Missile Radome.” Aircraft Engineering and Aerospace Technology 33 (1): 8–11. https://doi.org/10.1108/eb033353
• Reams, Richard H., Thomas M. Fischer, Robert E. Reifenberg, et al. 2012. Nonconforming Titanium Task Force Actions to Resolve Aircraft Safety Issues Due to Improperly Substituted Material. Defense Technical Information Center. https://doi.org/10.21236/ada565297
• “Recent Developments in the Supersonic Flow over Axisymmetric Bodies with Continuous or Discontinuous Slope.” 1967. In 5th Aerospace Sciences Meeting. AIAA 1967-25. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-25
• Reda, Daniel C. 1977. Boundary-Layer Transition Experiments on Sharp, Slender Cones in Supersonic Freeflight. Defense Technical Information Center. https://doi.org/10.21236/ada054591
• 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
• 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
• 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, Wendell E. 1956. “A New Approach to Turbojet and Ramjet Engine Control.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/560042
• 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. 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
• Reehorst, Andrew L., Harold E. Addy Jr., and Renato O. Colantonio. 2010. “Examination of Icing Induced Loss of Control and Its Mitigations.” In Atmospheric and Space Environments Conference. https://ntrs.nasa.gov/citations/20100042407
• Regan, F. J. 1964. Roll Damping Moment Measurements for the Basic Finner at Subsonic and Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0600975
• Regenie, Victoria, Donald Gatlin, Robert Kempel, and Neil Matheny. 1992. “The F-18 High Alpha Research Vehicle: A High-Angle-of-Attack Testbed Aircraft.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4121
• 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
• Reinhart, W. A., and E. Tjonneland. 1965. “Inlet Flow Field Studies for the Supersonic Transport.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/650198
• Reissner, Eric. 1944. On the General Theory of Thin Airfoils for Nonuniform Motion. NACA-TN-946. Massachusetts Institute of Technology. https://ntrs.nasa.gov/citations/19930085011
• “Rejected Takeoff Performance.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0813.0848
• “Rejected Takeoff Performance Testing and AFM Takeoff Field Length.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0849.0892
• Rejeske, J., and D. Stava. 1974. “A Test Technique for Inlet/aircraft Drag Evaluation.” In 10th Propulsion Conference. AIAA 1974-1145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1145
• Reller, John O., and Harry W. Dowman. 1949. Altitude-Test-Chamber Investigation of Mcdonnell Afterburner on J34 Engine. NACA-RM-SE9D19. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090023627
• Renas, Paul E., Willis M. Braithwaite, and Emmert T. Jansen. 1952. Altitude Investigation of Three Flame-Holder and Fuel-Systems Configurations in a Short Converging Afterburner on a Turbojet Engine. NACA-RM-E52G29. NASA. https://ntrs.nasa.gov/citations/19930087244
• Renas, P. E., E. T. Jansen, and R. W. Harvey Sr. 1953. Altitude Starting Characteristics of an Afterburner with Autoignition and Hot-Streak Ignition. NACA-RM-E53B02. NASA. https://ntrs.nasa.gov/citations/19930087619
• Render, Peter M. 2010. Maneuver of Fixed-Wing Combat Aircraft. Wiley. https://doi.org/10.1002/9780470686652.eae249
• Renita Sharon Monis et al, Renita Sharon Monis et al., and TJPRC. 2019. “An Effect of Sweep Angle on Roll Damping Derivative for a Delta Wing with Curved Leading Edges in Unsteady Flow.” International Journal of Mechanical and Production Engineering Research and Development 9 (2): 361–74. https://doi.org/10.24247/ijmperdapr201935
• “Requirements of a Commercial Supersonic Aircraft on Its Engines.” 1967. In Commercial Aircraft Design and Operation Meeting. AIAA 1967-376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-376
• Reschke, Christian. 2005. “Flight Loads Analysis with Inertially Coupled Equations of Motion.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2005-6026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6026
• “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. 1958. NASA. https://ntrs.nasa.gov/citations/19930092380
• Reukauf, P. J., F. W. Burcham Jr., and J. K. Holzman. 1975. “Status of a Digital Integrated Propulsion/flight Control System for the YF-12 Airplane.” In Propulsion Conference. https://ntrs.nasa.gov/citations/19760027286
• 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
• Reuther, J., and A. Jameson. 1995. “Supersonic Wing and Wing-Body Shape Optimization Using an Adjoint Formulation.” In CFD for Design and Optimization. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0954
• “Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics.” 1986. In Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865763.0481.0502
• Rey, William K. 1956. Elevated-Temperature Fatigue Properties of Two Titanium Alloys. NACA-RM-56B07. University of Alabama. https://ntrs.nasa.gov/citations/19930090205
• Reyhner, T., and T. Hickcox. 1972. “A Procedure for Combined Viscous-Inviscid Analysis of Supersonic Inlet Flow Fields.” In 10th Aerospace Sciences Meeting. AIAA 1972-44. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-44
• Reynolds, James, Ethan Baumann, Claudia Sales, and Timothy Williams. n.d. “Flight-Test Approach for X-57 Mod II Configuration.” In Aviation 2024. https://ntrs.nasa.gov/citations/20240007413
• 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
• Rhode, R. V. 1929. The Pressure Distribution over the Horizontal and Vertical Tail Surfaces of the F6C-4 Pursuit Airplane in Violent Maneuvers. NACA-TR-307. NASA. https://ntrs.nasa.gov/citations/19930091375
• 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
• Rhodeside, G. 1986. “Investigation of Aircraft Departure Susceptibility Using a Total-G Simulator.” In 24th Aerospace Sciences Meeting. AIAA 1986-492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-492
• Ribeiro, Andre F., Damiano Casalino, and Carlos Ferreira. 2022a. “Free Wake Panel Method Simulations of a Highly Flexible Wing at Flutter.” In AIAA AVIATION 2022 Forum. AIAA 2022-3595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3595
• Ribeiro, Andre F. P., Damiano Casalino, and Carlos Ferreira. 2022b. “Free Wake Panel Method Simulations of a Highly Flexible Wing in Flutter and Gusts.” Preprint, . https://doi.org/10.2139/ssrn.4314579
• Ribner, Herbert S. 1947. The Stability Derivatives of Low-Aspect-Ratio Triangular Wings at Subsonic and Supersonic Speeds. NACA-TN-1423. NASA. https://ntrs.nasa.gov/citations/19930082119
• Ribner, Herbert Spencer. 1950. On the Effect of Subsonic Trailing Edges on Damping in Roll and Pitch of Thin Sweptback Wings in a Supersonic Stream. NACA-TN-2146. NASA. https://ntrs.nasa.gov/citations/19930082764
• Ribner, Herbert S. 1951. Damping in Roll of Cruciform and Some Related Delta Wings at Supersonic Speeds. NACA-TN-2285. NASA. https://ntrs.nasa.gov/citations/19930082942
• Ribner, Herbert S., and Frank S. Malvestuto Jr. 1948. Stability Derivatives of Triangular Wings at Supersonic Speeds. NACA-TR-908. NASA. https://ntrs.nasa.gov/citations/19930091975
• 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
• Rich, B. 1973. “The F-12 Series Aircraft Aerodynamic and Thermodynamic Design in Retrospect.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-820
• Richards, Phillip W., and Andrew Erickson. 2019. “Dynamic Ground Loads Analysis Using Detailed Modeling of Landing Gear and Aircraft Aeroservoelastics.” In AIAA Scitech 2019 Forum. AIAA 2019-0759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0759
• 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., B. Berrier, and J. Palcza. 1977. “Two-Dimensional Nozzle/airframe Integration Technology: An Overview.” In 13th Propulsion Conference. AIAA 1977-839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-839
• 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
• Richey, G. K., D. Stava, Brian Brimelow, and H. Ivan Bush. 1968. “Airframe-Propulsion Integration for Future Aircraft Systems.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/680288
• Richey, G. K., L. E. Surber, and B. L. Berrier. 1983. “Airframe-Propulsion Integration for Fighter Aircraft.” In 21st Aerospace Sciences Meeting. AIAA 1983-84. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-84
• 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, and David Fisher. 1991. “In-Flight Leading-Edge Vortex Flow-Field Survey Measurements on a F-18 Aircraft at High Angle of Attack.” In 9th Applied Aerodynamics Conference. AIAA 1991-3248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3248
• Ridgway, Keith, Michael. S. Turner, Adrian. R. C. Sharman, James Hughes, Tim Chapman, and Sergio Durante. 2010. Machining Aerospace Materials. Wiley. https://doi.org/10.1002/9780470686652.eae364
• Ridley, Norman. 2003. “Superplastic Forming.” In Handbook of Aluminum. CRC Press. https://doi.org/10.1201/9780203912591.ch22
• Ridley, Norman. 2010. Superplastic Forming and Diffusion Bonding of Titanium Alloys. Wiley. https://doi.org/10.1002/9780470686652.eae223
• Ridley, N. 2011. “Metals for Superplastic Forming.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.1.3
• Ridley, Norman. 2019. “Superplastic Forming.” In Encyclopedia of Aluminum and Its Alloys. CRC Press. https://doi.org/10.1201/9781351045636-140000440
• Righi, Marcello, Sven Düzel, David Anderegg, Andrea Da Ronch, David Massegur Sampietro, and Issam Soukhmane. 2022. “ROM-Based Uncertainties Quantification of Flutter Speed Prediction of the BSCW Wing.” In AIAA SCITECH 2022 Forum. AIAA 2022-0179. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0179
• “Rigid-Body Flight Dynamics.” 2026. In Analytical Aircraft Flight. Cambridge University Press. https://doi.org/10.1017/9781009399913.005
• 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
• Ritter, Markus, Mathias S. Roeser, and Lars Reimer. 2020. “CFD-Based Multi-Axis Maneuver Simulation for System Identification of Flexible Transport Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-2125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2125
• Rizzetta, Donald. 1991. “Numerical Simulation of a Supersonic Inlet.” In 29th Aerospace Sciences Meeting. AIAA 1991-128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-128
• Rizzetta, Donald. 1995. “Numerical Investigation of Supersonic Wing-Tip Vortices.” In Fluid Dynamics Conference. AIAA 1995-2282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2282
• Rizzetta, Donald, and Miguel Visbal. 2012a. “Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number.” In 6th AIAA Flow Control Conference. AIAA 2012-2956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2956
• Rizzetta, Donald, and Miguel Visbal. 2012b. “Plasma Flow Control Simulation of a Low-Reynolds Number Low-Aspect-Ratio Wing.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-1138. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-1138
• Rizzi, Arthur, and Charles J. Purcell. 1986. “Numerical Experiment with Inviscid Vortex-Stretched Flow around a Cranked Delta Wing: Supersonic Speed.” Engineering Computations 3 (3): 230–34. https://doi.org/10.1108/eb023661
• Rizzi, A., and W. Schmidt. 1978. “Study of Pitot-Type Supersonic Inlet-Flowfields Using the Finite-Volume Approach.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1115
• Roberge, Heather. 2025. “Superplastic Forming.” In Fabricating Plasticity in Aluminum. Routledge. https://doi.org/10.4324/9781315856926-9
• 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
• Robinson, Brandon. n.d. “Aeroelastic Oscillations of a Pitching Cantilever Wing with Structural Geometric Nonlinearities: Theory, Numerical Simulation and Global Sensitivity Analysis.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2018-13315
• Robinson, A. 1948. “On Source and Vortex Distributions in the Linearized Theory of Steady Supersonic Flow.” Quarterly Journal of Mechanics and Applied Mathematics 1 (1): 408–32. https://doi.org/10.1093/qjmam/1.1.408
• Robinson, Ross B. 1957. Aerodynamic Characteristics of Missile Configurations with Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01. NACA-RM-L57D19. NASA. https://ntrs.nasa.gov/citations/19930089792
• 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
• 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
• “ROCKET-POWERED AIRCRAFT.” 2017. In The History of Human Space Flight. University Press of Florida. https://doi.org/10.2307/j.ctvx072b5.11
• Rockwell, Donald O. 1994. Unsteady Structure of Leading-Edge Vortices on a Delta Wing. Defense Technical Information Center. https://doi.org/10.21236/ada278988
• Rockwell, Donald. 2011. Unsteady Flow Structure on Low Aspect Ratio Wings. Defense Technical Information Center. https://doi.org/10.21236/ada562723
• Rodchenko, Victor, Larisa Zaichik, and Yury Yashin. 2002. “HQ Criterion for Roll Control of High-Augmented Aircraft.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4801
• Rodgers, C. 2004. “A Performance Diagnosis of the 1939 Heinkel He S3B Turbojet.” In Volume 2: Turbo Expo 2004. ASMEDC. https://doi.org/10.1115/gt2004-53014
• Rodriguez, David. 2004. “Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method.” In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2004-4492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4492
• Rodriguez, David. 2007. “Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1048
• Rogal, B. 1965. “Differential Pressure Measurements in Sensing Sideslip and Angle of Attack.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50004-x
• 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, Robert, and Stephen Chan. 2004. “Aerocoefficients for Low Aspect Ratio Cylinders from Subsonic to Mach 5.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-4839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4839
• Rogers, Lynn C. 1970. Optimum Selection of Design Variable Increments to Improve Flutter Characteristics. Defense Technical Information Center. https://doi.org/10.21236/ada367071
• 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
• 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
• Rokhsaz, Kamran, and Linda K. Kliment. 2019. “Effect of Data Filtering on Flight Loads Spectra.” In AIAA Aviation 2019 Forum. AIAA 2019-3367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3367
• Rokhsaz, Kamran, Linda K. Kliment, and John Nelson. 2022. “Flight Loads Analysis of CL-415 Scoopers.” In AIAA AVIATION 2022 Forum. AIAA 2022-4015. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4015
• Rolf, Rl, and Ep Patrick. 1978. “Bending and Springback of Aluminum Alloy Sheet and Plate.” In Formability Topics—Metallic Materials. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp30046s
• Rollin, Maxime. n.d. “Study and Optimization of Cooling Conditions of Titanium Alloy Parts Manufactured by Superplastic Forming Process.” PhD diss., Ecole nationale des Mines d’Albi-Carmaux. https://doi.org/10.70675/b21a8cc7za67fz42e9z87f7z0947805bfaba
• “Rolling Maneuvers.” 1996. In Structural Loads Analysis for Commercial Transport Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862465.0027.0036
• Rolls, L. Stewart. 1953. A Flight Comparison of a Submerged Inlet and a Scoop Inlet at Transonic Speeds. NACA-RM-A53A06. NASA. https://ntrs.nasa.gov/citations/19930087457
• Rolston, S., and S. Raghunathan. 1994. “An Application of Passive Control to the Shock Wave Boundary Layer Interaction in High Speed Intakes.” In 12th Applied Aerodynamics Conference. AIAA 1994-1837. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1837
• Romine, H. E. 1962. GC Tests of Welds in TI-13V-11CR-3A1 Alloy Sheets from Company a and GC Tests of Age-Strengthened Base Metal and of Welds in TI-6A1-4V and TI-13V-11CR- 3A1 Alloy Sheets from Company f-Summary Review of Fracture Toughness Results on Titanium Alloys Being Considered for Solid-Propellant Rocket Motor Cases. Defense Technical Information Center. https://doi.org/10.21236/ad0273711
• Rominiyi, Azeez Lawan, and Peter Madindwa Mashinini. 2025. “Processing and Machining of Aerospace Metals.” In Aerospace Materials. Elsevier. https://doi.org/10.1016/b978-0-443-22118-7.00006-3
• Röntsch, Bernhard, Lutz Taubert, Philipp Tewes, Jesse C. Little, and Israel J. Wygnanski. 2016. “Application of Active Flow Control to a Generic Low Aspect-Ratio Trapezoidal Wing for High Lift Generation.” In 8th AIAA Flow Control Conference. AIAA 2016-3169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3169
• Rook, Todd E. 2010. “Noise and Vibration Phenomena in Aircraft Wheel and Brake Systems.” Journal of the Acoustical Society of America 127 (3_Supplement): 1792–1792. https://doi.org/10.1121/1.3383986
• 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, 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
• 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, Eugene S., and Dan M. 1952. Spin and Recovery Tests of a 1/28-SCALE Model of the YF-93A Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0014890
• Rose, J. Bruce Ralphin, and G. R. Jinu. 2016. “Influence of Aeroelastic Flow Induced Oscillations on Fatigue Life of an Airplane Wing Structure.” International Journal of Modelling, Identification and Control 25 (3): 199. https://doi.org/10.1504/ijmic.2016.075811
• Rose, O., David Miller, James Pittman, P. Ashill, and J. Fulker. 1988. “A Full-Potential Theory Analysis of the Supersonic Aerodynamics of a60-Deg Delta Wing-Body Configuration.” In 26th Aerospace Sciences Meeting. AIAA 1988-480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-480
• Rosen, Marc A. 2001. “Exergy Analysis of a Turbojet Engine over a Complete Flight Cycle.” In Advanced Energy Systems. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2001/aes-23645
• 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
• 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
• 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
• 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
• Roxbee Cox, H. 1946. “British Aircraft Gas Turbine Engine Progress: A General Review of the Development of Jet-Propulsion Engines in Great Britain.” Aircraft Engineering and Aerospace Technology 18 (2): 50–59. https://doi.org/10.1108/eb031336
• 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, Anish, and Vadim V. Silberschmidt. 2014. “Ultrasonically Assisted Machining of Titanium Alloys.” In Materials Forming, Machining and Tribology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9_6
• Roysdon, Paul, and Mahmood Khalid. 2010. “Lateral-Directional Stability Investigation of a Blended-Wing Body.” In 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. AIAA 2010-9167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9167
• 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
• Royster, D. M. 1968. Hot Salt Stress Corrosion Cracking and Its Effect on Tensile Properties of Ti-8Al-1Mo-1V Titanium-Alloy Sheet. NASA-TN-D-4674. NASA. https://ntrs.nasa.gov/citations/19680020528
• Royster, D. M. 1969. Hot-Salt-Stress-Corrosion Cracking and Its Effect on Tensile and Stress-Rupture Properties of Ti-6Al-4V Titanium-Alloy Sheet. NASA-TN-D-5417. NASA. https://ntrs.nasa.gov/citations/19690026843
• Royster, D. M., and T. T. Bales. 1983. Elevated Temperature Behavior of Superplastically Formed/weld-Brazed Titanium Compression Panels Having Advanced Shaped Stiffeners. NASA-TP-2123. NASA. https://ntrs.nasa.gov/citations/19830011618
• Royster, D. M., T. T. Bales, and R. C. Davis. 1985. “Evaluation of Superplastic Forming and Weld-Brazing for Fabrication of Titanium Compression Panels.” In Welding, Bonding and Fastening, 1984. https://ntrs.nasa.gov/citations/19860001778
• Royster, D. M., T. T. Bales, R. C. Davis, and H. R. Wiant. 1983. Fabrication and Evaluation of Cold/formed/weldbrazed Beta-Titanium Skin-Stiffened Compression Panels. NASA-TP-2201. NASA. https://ntrs.nasa.gov/citations/19830026829
• Royster, D. M., T. T. Bales, and H. R. Wiant. 1982. Superplastic Forming/weld-Brazing of Titanium Skin-Stiffened Compression Panels. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19830039249
• Rudnitski, D. n.d. “A Detailed Procedure for Measuring Turbojet Engine Performance in an Enclosed Sea-Level Test Facility.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1983-00812
• Rudolph, Peter K. C. 1996. High-Lift Systems on Commercial Subsonic Airliners. NASA-CR-4746. NASA. https://ntrs.nasa.gov/citations/19960052267
• Ruflin, S. J., and W. D. Grantham. 1984. A Preliminary Look at the Effects of Coupled Lateral Modes on Aircraft Handling Qualities. AIAA PAPER 84-2096. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840059585
• Ruhlin, C., R. Destuynder, and R. Gregory. 1974. “Some Tunnel-Wall Effects on Transonic Flutter.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-406
• 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
• Ruhlin, C., F. Rauch Jr., and C. Waters. 1982. “Transonic Flutter Study of a Wind-Tunnel Model of a Supercritical Wing With/without Winglet.” In 23rd Structures, Structural Dynamics and Materials Conference. AIAA 1982-721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-721
• Rule, John, Robert Richard, and Robert Clark. 2000. “Experimental Investigation of Delta Wing Active Flutter Control.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1629
• Rullan, Jose, Pavlos Vlachos, and Demetri Telionis. 2006. “Flow Control over Trapezoidal-Wing Planforms with Sharp Edges.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-857. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-857
• 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
• Rusak, Z. 1993. “2. Subsonic and Transonic Flows around a Thin Airfoil with a Parabolic Nose.” In Transonic Aerodynamics: Problems in Asymptotic Theory. Society for Industrial and Applied Mathematics. https://doi.org/10.1137/1.9781611970975.ch2
• Russell, J. B. 1996. “Lateral Static Stability and Control.” In Performance and Stability of Aircraft. Elsevier. https://doi.org/10.1016/b978-034063170-6/50008-6
• Rustenburg, John W. 1973. Development of a Rolling Maneuver Spectrum from Statistical Flight Loads Data. Defense Technical Information Center. https://doi.org/10.21236/ad0761491
• Růžička, Jan. 2021. “Strain Gauge Placement Optimization Methodology to Measure Multiaxial Loads of Complex Structure.” Journal of Strain Analysis for Engineering Design 57 (7): 614–28. https://doi.org/10.1177/03093247211063088
• Rybalko, Michael, Sean Candon, and Eric Loth. 2013. “Pressure and Shock Dynamics of a Low-Boom Inlet.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-15. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-15
• Rybalko, Michael, Eric Loth, Rodrick V. Chima, Stefanie M. Hirt, and James R. DeBonis. 2010. Micro-Ramps for External Compression Low-Boom Inlets. NASA/TM-2010-216351. NASA. https://ntrs.nasa.gov/citations/20100024367
• Rymanova, Anastasia, Evgenia Guseva, and Vitaly Gunchin. 2023. “Implementation of the Methodology of Coupled Modelling of Aerodynamics and Strength to Determine the Onset Speed of the Bending-Torsional Flutter of the Wing Console.” E3S Web of Conferences 446: 03005. https://doi.org/10.1051/e3sconf/202344603005
• 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
• Ryu, Shiyang, and Dominick Andrisani. 2000. “Longitudinal Flying Qualities Prediction for Nonlinear Aircraft.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3989
• S-16 Turbine Engine Inlet Flow Distortion Committee. 1998. Gas Turbine Engine Inlet Flow Distortion Guidelines. https://doi.org/10.4271/arp1420a
• S-16 Turbine Engine Inlet Flow Distortion Committee. 2011. Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines. https://doi.org/10.4271/air1419a
• S-16 Turbine Engine Inlet Flow Distortion Committee. 2021. Guidelines for Characterization of Gas Turbine Engine Total-Pressure, Planar-Wave, and Total-Temperature Inlet-Flow Distortion. https://doi.org/10.4271/arp6420
• Sabari Vihar, R., J. V. M. Lal Jeyan, and K. Sai Priyanka. 2023. “Experimental Flutter Analysis over Different Selected Wing Planforms by Varying the Wing Cross Section Geometry.” ACS Journal for Science and Engineering 3 (2): 52–60. https://doi.org/10.34293/acsjse.v3i2.85
• Sabourin, Francis. 2004. “Sheet Forming with a Specific Inverse Approach for a Further Springback Analysis.” In AIP Conference Proceedings, vol. 712. AIP. https://doi.org/10.1063/1.1766630
• Sachs, George, and John G. Sessler. 1961. “Effect of Stress Concentration on Tensile Strength of Titanium and Steel Alloy Sheet at Various Temperatures.” In Symposium on Low-Temperature Properties of High-Strength Aircraft and Missile Materials. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp46980s
• 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. 1953. Flight Measurements of the Horizontal-Tail Loads on a Swept-Wing Fighter Airplane at Transonic Speeds. NACA-RM-A53G10. NASA. https://ntrs.nasa.gov/citations/19930087620
• Sadoff, Melvin, and Lawrence A. Clousing. 1948. Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight III: Tail Loads in Abrupt Pull-up Push-down Maneuvers. NACA-TN-1539. NASA. https://ntrs.nasa.gov/citations/19930082221
• Sadoff, Melvin, Frederick H. Matteson, and Rudolph D. Van Dyke Jr. 1954. The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane. NACA-RM-A54C31. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/19650075959
• Sadraey, Mohammad H. 2017. “Takeoff and Landing.” In Aircraft Performance. CRC Press. https://doi.org/10.1201/9781315366913-8
• Sadraey, Mohammad H. 2022a. “Lateral-Directional Control.” In Synthesis Lectures on Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-18765-0_6
• Sadraey, Mohammad H. 2022b. “Lateral-Directional Stability.” In Synthesis Lectures on Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-18765-0_4
• Sadraey, Mohammad H. 2023. “Takeoff and Landing.” In Aircraft Performance. CRC Press. https://doi.org/10.1201/9781003279068-8
• Safarov, I. I., A. U. Yavov, Z. I. Boltaev, X. E. Ergashev, and U. U. Rajabov. 2026. “Flexural-Torsional Flutter of an Aircraft Wing with Distributed Parameters in Subsonic Flight Mode.” In AIP Conference Proceedings, vol. 3390. AIP Publishing. https://doi.org/10.1063/5.0328032
• Safiullin, Rinat V., and Ramil Ya. Lutfullin. 1996. “Solid State Joint Formation of the Titanium Alloy VT6S under Superplastic Forming Conditions.” In Materials science forum, vol. 243-245. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.243-245.763
• Safronov, Oleksandr, Bohdan Semon, Oleksandr Nedilko, and Anna Horina. 2023. “Conditions for Simulation of Transonic Flutter of Aerodynamic Control Surfaces of Supersonic Aircraft in Wind Tunnels.” Strength of Materials and Theory of Structures, no. 110: 81–96. https://doi.org/10.32347/2410-2547.2023.110.81-96
• Safronov, Oleksandr, Bogdan Semon, Oleksandr Nedilko, and Anna Horina. 2024. “Method of Estimating the Number M of Occurrence of Transonic Flutter of Aerodynamic Control Surfaces of Supersonic Aircraft and Aerospace Systems.” Strength of Materials and Theory of Structures, no. 113: 116–23. https://doi.org/10.32347/2410-2547.2024.113.116-123
• Saito, Naoko, Mitsugi Fukahori, Daisuke Hisano, Hiroshi Hamasaki, and Fusahito Yoshida. 2016. “Effect of Stress Relaxation on Springback of Steel Sheet in Warm Forming.” In Key engineering materials, vol. 725. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.725.671
• Saitoh, K., M. Hashidate, H. Matsushita, and T. Kikuchi. 1995. “Elastic Deflection Effects on Transonic Aerodynamics of a Flutter Wing Model with Control Surfaces.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3926
• Saitoh, Kenichi, Masato Tamayama, Norio Yoshimoto, and Tetsuhiko Ueda. 2012. “Unsteady Transonic Aerodynamics during Wing Flutter.” Open Engineering 2 (3): 410–17. https://doi.org/10.2478/s13531-012-0008-2
• 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
• Salahudden, Salahudden, Prasiddha N. Dwivedi, and Ajoy K. Ghosh. 2021. “Aircraft Spin Recovery with Altitude Loss Reduction Using Closed-Loop Thrust Control.” In AIAA Scitech 2021 Forum. AIAA 2021-0717. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0717
• Salem, A. A., J. B. Shaffer, S. R. Niezgoda, et al. 2016. Microstructure Uncertainty Propagation in Sheet Metal Forming Fe-Simulations: Springback of Commercial-Purity Titanium. Wiley. https://doi.org/10.1002/9781119296126.ch314
• Salguero, Jorge, Moises Batista, Irene del Sol, and Juan Manuel Vazquez. 2024. “High-Speed Machining of Aluminum Alloys for Aircraft Structures.” In Modern Manufacturing Processes for Aircraft Materials. Elsevier. https://doi.org/10.1016/b978-0-323-95318-4.00005-7
• 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
• Sallee, V. 1990. “ADAM 2.0: An ASE Analysis Code for Aircraft with Digital Flight Control Systems.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-1077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1077
• 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
• Samimy, Mo, Nathan Webb, and Christopher Clifford. 2011. Supersonic Inlet Flow Control Using Localized Arc Filament Plasma Actuators. Defense Technical Information Center. https://doi.org/10.21236/ada564713
• Sana, Guillaume, Alain Petiot, and Arnaud Giraudet. 2016. “Hot Forming and Superplastic Forming: Presses Evolution and New Applications in the Aerospace Industry.” In Materials science forum, vol. 838-839. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.838-839.563
• Sandahl, Carl A. 1948. Free-Flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42.7 Degree Sweptback Wing Having Partial-Span Ailerons. NACA-RM-L8E25. NASA. https://ntrs.nasa.gov/citations/19930085384
• Sanders, D. G. 2005. “The Current Status of Superplastic Forming Manufacturing in the United States(Keynote III).” Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (0): 23. https://doi.org/10.1299/jsmeintmp.2005.23_2
• Sanders, Daniel G., Paul D. Edwards, Mamidala Ramulu, and G. J. Grant. 2010. “Optimization of the Friction Stir Welding Process for Superplastic Forming and Improved Surface Texture for Titanium Aerospace Structures.” In Key engineering materials, vol. 433. Trans Tech Publications. https://doi.org/10.4028/scientific5/kem.433.153
• Sanders, Daniel G., and Mamidala Ramulu. 2012. “Friction Stir Welding Combined with Superplastic Forming for Monolithic Titanium Aircraft Structure: Influence of Post Welding Thermal Treatments on Weld Nugget Residual Stress.” In Materials science forum, vol. 735. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.735.395
• Sanders, E. Claude, Jr. 1951. Damping in Roll of Straight and 45 Degree Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-Powered Models. NACA-RM-L51H14. NASA. https://ntrs.nasa.gov/citations/19930086866
• Sanders, E. Claude, Jr. 1952. Damping in Roll of Models with 45, 60 and 70 Degree Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-Powered Models. NACA-RM-L52D22a. NASA. https://ntrs.nasa.gov/citations/19930087208
• 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
• Sandstrom, Rune. 1971. “The Load on the Brake Parachute of a Jet Aeroplane under the Influence of the Engine Wake.” Aircraft Engineering and Aerospace Technology 43 (11): 26–30. https://doi.org/10.1108/eb034832
• Sanghi, Divya, Cristina Riso, Carlos Cesnik, and Fabio Vetrano. 2020. “Influence of Aileron Placement on Roll Response of High-Aspect-Ratio-Wing Aircraft.” In AIAA Aviation 2020 Forum. AIAA 2020-2645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2645
• Sano, Masakazu, Hidekazu Yoshida, Sho Wakabayashi, et al. 2018. “Numerical Simulation of the Side-Clearance Effect on the Supersonic Air-Inlet Performance for High Mach Integrated Control Experiment “HIMICO”.” In 2018 Joint Propulsion Conference. AIAA 2018-4539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4539
• Sansica, Andrea, and Atsushi Hashimoto. 2023b. “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, Marcio Wagner Batista dos. n.d.-a. “Investigation of the Mechanical Behaviour and Microstructure Evolution of Titanium Alloys under Superplastic and Hot Forming Conditions.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/t.3.2018.tde-05032018-112239
• Santos, Luiz Guilherme Pancini dos. n.d.-b. “Nonlinear Aeroelastic Stability Analysis and Gust Response of Airfoil Section under Stall Flutter Oscillation.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/d.18.2021.tde-08012026-155540
• Santos, Victor, and Helio De Assis Pegado. 2019. “Finite Element Method Modeling of Supersonic Panel Flutter with Piston Theory.” In Proceedings of the 25th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2019.cob2019-0370
• Saprykin, B. Ju. 2013. “Analysis of Calculation Methods of Springback of Sheet Materials.” Izvestiya MGTU MAMI 7 (2–2): 133–39. https://doi.org/10.17816/2074-0530-68124
• 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
• Saravanan, R., S. L. N. Desikan, and T. M. Muruganandam. 2017. “Effect of Back Pressure and Freestream Dynamic Pressure on a Typical Ramjet Engine Duct under Realistic Supersonic Inlet Condition.” Aeronautical Journal 122 (1247): 83–103. https://doi.org/10.1017/aer.2017.115
• 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
• Sarmazdeh, Ali Momeny, Mojtaba Tahani, and Mohsen Motahari Nezhad. 2014. “Numerical Investigation of Symmetrical Supersonic Inlet with Boundary Layer Suction.” International Journal of Fluid Mechanics Research 41 (3): 185–93. https://doi.org/10.1615/interjfluidmechres.v41.i3.10
• Sarrazin-Baudoux, C., S. Lesterlin, and J. Petit. 1997. “Atmospheric Influence on Fatigue Crack Propagation in Titanium Alloys at Elevated Temperature.” In Elevated Temperature Effects on Fatigue and Fracture. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp16321s
• Sarwar, Md Gulam, Mushtaque Momin, Gulam Anwar, Petha Sethuraman Vignesh Ram, and Saista Tabssum. 2024. “Experimental and Numerical Investigation on Supersonic Intake Buzz: A Survey.” In Advances in Aerospace Technologies. River Publishers. https://doi.org/10.1201/9788770046299-8
• Sasoh, Akihiro, Manabu Myokan, Henny Bottini, and Akira Iwakawa. 2018. “Mechanisms of Pressure Loss Recovery by Repetitive Energy Deposition in Supersonic Intake Model.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3179. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3179
• Sastry, S. M. L., R. J. Lederich, T. L. Mackay, and W. R. Kerr. 1983b. “Superplastic Forming Characterization of Titanium Alloys.” JOM 35 (1): 48–53. https://doi.org/10.1007/bf03338184
• Sastry, S. M., R. J. Lederich, and J. E. O’Neal. 1983a. Optimum Microstructures for SPF (Superplastic Forming) Using Hydrovac. Defense Technical Information Center. https://doi.org/10.21236/ada130944
• Sathish, T. 2018. “Prediction of Springback Effect by the Hybridisation of ANN with PSO in Wipe Bending Process of Sheet Metal.” Progress in Industrial Ecology, An International Journal 12 (1/2): 112. https://doi.org/10.1504/pie.2018.095881
• 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
• Saunders, J., and T. Keith Jr. 1991. “Results from Computational Analysis of a Mixed Compression Supersonic Inlet.” In 27th Joint Propulsion Conference. AIAA 1991-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2581
• Savin, Raymond C. 1958. Approximate Solutions for the Flow about Flat-Top Wing-Body Configurations at High Supersonic Airspeeds. NACA-RM-A58F02. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/19630002629
• Sazonov, M. B., and A. N. Zhidyaev. 2022. “Research on End Mill Vibration in Machining of VT9 Titanium Alloy.” VESTNIK of Samara University. Aerospace and Mechanical Engineering 20 (4): 89–99. https://doi.org/10.18287/2541-7533-2021-20-4-89-99
• Scadron, Marvin D., Clarence C. Gettelman, and George J. Pack. 1950. Performance of Three High-Recovery-Factor Thermocouple Probes for Room-Temperature Operation. NACA-RM-E50I29. NASA. https://ntrs.nasa.gov/citations/19930086452
• Scanlan, R. H. 1948. Outline of an Acceptable Method of Vibration and Flutter Analysis for a Conventional Airplane. Defense Technical Information Center. https://doi.org/10.21236/ada955900
• 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
• Scharnhorst, Richard. 2012. “An Overview of Military Aircraft Supersonic Inlet Aerodynamics.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-13. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-13
• Scher, Stanley H. 1946. Wind-Tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-3 Airplane. NACA-RM-L8K18a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019273
• Scher, Stanley H. 1947a. Effect of 40 Degree Sweepback on the Spin and Recovery Characteristics of a 1/25-Scale Model of a Typical Fighter-Type Airplane as Determined by Free-Spinning-Tunnel Tests. NACA-TN-1256. NASA. https://ntrs.nasa.gov/citations/19930081844
• Scher, Stanley H. 1947b. 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. 1947c. 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. 1956. Analysis of a Spin and Recovery from Time Histories of Attitudes and Velocities as Determined for a Dynamic Model of a Contemporary Fighter Airplane in the Free-Spinning Tunnel. NACA-TN-3611. NASA. https://ntrs.nasa.gov/citations/19930084325
• Scherberg, Max, and R. V. Rhode. 1927. Mass Distribution and Performance of Free Flight Models. NACA-TN-268. NASA. https://ntrs.nasa.gov/citations/19930081026
• Scherrer, Richard. 1951. Comparison of Theoretical and Experimental Heat-Transfer Characteristics of Bodies of Revolution at Supersonic Speeds. NACA-TR-1055. NASA. https://ntrs.nasa.gov/citations/19930092100
• Schierman, John, and David Schmidt. 1991. “Analysis of Airframe/engine Interactions in Integrated Flight and Propulsion Control.” In Navigation and Control Conference. AIAA 1991-2794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2794
• Schiff, L., M. Tobak, and G. Malcolm. 1980. “Mathematical Modeling of the Aerodynamics of High-Angle-of-Attack Maneuvers.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1583
• Schikorra, Marco, Rajarajan Govindarajan, Alexander Brosius, and Matthias Kleiner. 2005. “Springback Analysis of Sheet Metals Regarding Material Hardening.” In Advanced materials research. Trans Tech Publications. https://doi.org/10.4028/0-87849-972-5.721
• Schkolnik, Gerald. 1993. “Identification of Integrated Airframe-Propulsion Effects on an F-15 Aircraft for Application to Drag Minimization.” In Guidance, Navigation and Control Conference. AIAA 1993-3764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3764
• Schlichting, H. 1939. Airfoil Theory at Supersonic Speed. NACA-TM-897. NASA. https://ntrs.nasa.gov/citations/19930094519
• Schlimm, Karl A. 2015. “A Model for Situational Awareness in Aircraft Upset Prevention and Recovery.” In 15th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2015-2900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2900
• Schmidt, D. 1983. “A Modal Analysis of Flexible Aircraft Dynamics with Handling Qualities Implications.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2074
• Schmidt, L. 1991. “Static Aeroelastic Effects upon Wing Span Loads.” In 9th Applied Aerodynamics Conference. AIAA 1991-3316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3316
• 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, David, John Schierman, and Sanjay Garg. 1990. “Analysis of Airframe/engine Interactions: An Integrated Control Perspective.” In 26th Joint Propulsion Conference. AIAA 1990-1918. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1918
• Schmidt, L., and S. Wright. 1991. “Aircraft Wing Rock by Inertial Coupling.” In 18th Atmospheric Flight Mechanics Conference. AIAA 1991-2885. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2885
• Schneiter, Leslie E. 1945. Spin Tests of a 0.059-Scale Model of the Curtiss-Wright XP-55 Airplane. NACA-MR-L5G31A. NASA. https://ntrs.nasa.gov/citations/19930092701
• Schnoebelen, Steven, and Thomas Yechout. 2003. “X-38 Component Build-up and Lateral-Directional Stability Analysis.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-204
• 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
• Schuelein, Erich, Manuel Schenk, and Benedikt Buchmann. 2017. “A Joint Study on the Starting Limits of a Generic Supersonic Inlet.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-3121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3121
• Schueler, C. J. 1963. A Comparison of Transition Reynolds Numbers from 12-IN. and 40-IN. Supersonic Tunnels. Defense Technical Information Center. https://doi.org/10.21236/ad0299290
• Schuet, Stefan, John Kaneshige, Thomas Lombaerts, et al. 2016. “Emerging Technologies for Airplane State Awareness and Prediction.” In NASA Ames Research Center. https://ntrs.nasa.gov/citations/20190025130
• 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
• Schuman, William C. 2018. “A Computational Study of Transonic Wall Interference for High Aspect Ratio Wind Tunnel Models at Sideslip Using Wings-Level-Yaw and Pitch-Roll Attitude Techniques.” In 2018 Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2018-3875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3875
• 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, Joshua A. 1988. Fighter Aircraft Design System User’s Manual. Defense Technical Information Center. https://doi.org/10.21236/ada200453
• Schweikhard, William G., and Donald T. Berry. 1974. “Cooperative Airframe/Propulsion Control for Supersonic Cruise Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/740478
• Schweinoch, Matthias, Alexei Sacharow, Dirk Biermann, and Christoph Buchheim. 2015. “An Error-Adaptive, Non-Rigid Registration Method for the Analysis of Springback in Sheet Metal Forming.” In Key engineering materials, vol. 651-653. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.651-653.1015
• Schwendemann, M., and B. Sanders. 1982. “Tangential Blowing for Control of Strong Normal Shock: Boundary Layer Interactions on Inlet Ramps.” In 18th Joint Propulsion Conference. AIAA 1982-1082. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1082
• Schy, A. A., and M. E. Hannah. 1976. Prediction of Jump Phenomena in Roll-Coupled Maneuvers of Airplanes. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19760053936
• Scott, R. W. 1972. Bonding Titanium to Rene 41 Alloy. ARC-10311. GE. https://ntrs.nasa.gov/citations/19720000041
• Scott, James, and Hafiz Atassi. 1989. “Numerical Solution of Periodic Vortical Flows about a Thin Airfoil.” In 24th Thermophysics Conference. AIAA 1989-1691. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1691
• Scudder, Nathan F. 1933. A Study of Factors Affecting the Steady Spin of an Airplane. NACA-TN-468. NASA. https://ntrs.nasa.gov/citations/19930081239
• Scudder, Nathan F. 1934. A Flight Investigation of the Spinning of the NY-1 Airplane with Varied Mass Distribution and Other Modifications, and an Analysis Based on Wind-Tunnel Tests. NACA-TR-441. NASA. https://ntrs.nasa.gov/citations/19930091515
• Scudder, N. F. 1935. A Flight Investigation of the Effect of Mass Distribution and Control Setting on the Spinning of the XN2Y-1 Airplane. NACA-TR-484. NASA. https://ntrs.nasa.gov/citations/19930091558
• Scudder, N. F. 1937. The Forces and Moments Acting on Parts of the XN2Y-1 Airplane during Spins. NACA-TR-559. NASA. https://ntrs.nasa.gov/citations/19930091634
• Scudder, N. F., and M. P. Miller. 1932. The Nature of Air Flow about the Tail of an Airplane in a Spin. NACA-TN-421. NASA. https://ntrs.nasa.gov/citations/19930081225
• Scudder, N. F., and Oscar Seidman. 1935. A Flight Investigation of the Spinning of the F4B-2 Biplane with Various Loads and Tail Surfaces. NACA-TR-529. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930091602
• Seacord, Charles L., and John P. Campbell. 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-ARR-3H31. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092518
• Seacord, Charles L., Jr. 1943. Effect of Wing Loading and Altitude on Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free-Flight Tunnel. NACA-WR-L-522. NASA. https://ntrs.nasa.gov/citations/19930092562
• Seacord, Charles L., Jr., and J. M. Teitelbaum. 1947. Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat. NACA-RM-L7B03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20010062501
• 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
• Seashore, Ferris L., and John M. Farley. 1958. Preliminary Performance Data Obtained in a Full-Scale, Free-Jet Investigation of a Side-Inlet Supersonic Diffuser. NACA-RM-E57E24. NASA. https://ntrs.nasa.gov/citations/19930089791
• Seaver, Ethan, Christopher J. Bennett, and Nicholas Lawson. 2023. “Flight Testing of the Effects of Airspeed and Aircraft Configuration in Lateral-Directional Static Stability for a Jetstream 31.” In AIAA AVIATION 2023 Forum. AIAA 2023-3293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3293
• Seckel, Edward. 1964a. “Characteristic Lateral-Directional Transients.” In Stability and Control of Airplanes and Helicopters. Elsevier. https://doi.org/10.1016/b978-0-12-634450-9.50021-x
• Seckel, Edward. 1964b. “Lateral-Directional Equations and Derivatives.” In Stability and Control of Airplanes and Helicopters. Elsevier. https://doi.org/10.1016/b978-0-12-634450-9.50019-1
• Seckel, Edward. 1964c. “Lateral-Directional Motions.” In Stability and Control of Airplanes and Helicopters. Elsevier. https://doi.org/10.1016/b978-0-12-634450-9.50028-2
• Seckel, Edward. 1964d. “Lateral-Directional Statics; Control for Trim.” In Stability and Control of Airplanes and Helicopters. Elsevier. https://doi.org/10.1016/b978-0-12-634450-9.50020-8
• Sedlock, Dennis. 1985. Improved Statistical Analysis Method for Prediction of Maximum Inlet Distortion. Defense Technical Information Center. https://doi.org/10.21236/ada153767
• 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
• 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, Cory A., and Darin Haudrich. 2024. “Gradient-Boosted Tree Model Development for Aircraft Landing Gear Jig Drop Analysis.” In AIAA SCITECH 2024 Forum. AIAA 2024-0195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0195
• 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
• Seidman, Oscar, and William H. McAvoy. 1940. Spin Tests of a Low-Lying Monoplane in Flight and in the Free-Spinning Wind Tunnel. NACA-TN-769. NASA. https://ntrs.nasa.gov/citations/19930081616
• Seidman, Oscar, and A. I. Neihouse. 1937. Free-Spinning Wind-Tunnel Tests of a Low-Wing Monoplane with Systemic Changes in Wings and Tails. NACA-TN-608. NASA. https://ntrs.nasa.gov/citations/19930081399
• Sekar, Chandra, Ramraj Sundararaj, Rajat Arora, and Abhijit Kushari. 2021. “Analysis of Failed Startup Sequence of a Single Spool Turbojet Engine.” Preprint, . https://doi.org/10.1115/1.0002966v
• Selna, James, Loren G. Bright, and Bernard A. Schlaff. 1952. Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range. NACA-RM-A52F27. NASA. https://ntrs.nasa.gov/citations/19930087214
• Selna, James, and Bernard A. Schlaff. 1951. An Investigation of the Drag and Pressure Recovery of a Submerged Inlet and a Nose Inlet in the Transonic Flight Range with Free-Fall Models. NACA-RM-A51H20. NASA. https://ntrs.nasa.gov/citations/19930093734
• Selvam, R. Panneer, Zu-Qing Qu, and Qun Zheng. 2002. “Three-Dimensional Nonlinear Panel Flutter at Supersonic Euler Flow.” In 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2002-1485. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-1485
• Semiatin, S. L., B. C. Kirby, and G. A. Salishchev. 2004. Coarsening Behavior of an Alpha-Beta Titanium Alloy. Defense Technical Information Center. https://doi.org/10.21236/ada428814
• Sen, J. K. 1990a. Advanced Technology Landing Gear. Volume 1 Design. Defense Technical Information Center. https://doi.org/10.21236/ada227196
• Sen, J. K. 1990b. Advanced Technology Landing Gear. Volume 2. Test. Defense Technical Information Center. https://doi.org/10.21236/ada227197
• ŞEn, Nuri, and Ömer SeÇGİN. 2020. “Experimental, Statistical, and Analytical Evaluation of the Springback Behavior of Martensitic 1400 Sheet in V-Bending.” Preprint, . https://doi.org/10.21203/rs.3.rs-106435/v1
• Send, W., and R. Voß. 1999. “Effects of a Contour Bump on the Unsteady Transonic Aerodynamic Forces of the AMP Wing.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-663-10901-3_56
• SenGupta, Gautam. 2024. “Flutter of Periodically Supported Plates in Supersonic Flow.” In Vibration of Periodic Structures. Elsevier. https://doi.org/10.1016/b978-0-32-399022-6.00019-9
• “Separation at the Leading Edge of a Thin Airfoil.” 1998. In Asymptotic Theory of Separated Flows. Cambridge University Press. https://doi.org/10.1017/cbo9780511983764.006
• Șerban, Florica Mioara, Nicolae Bâlc, Gheorghe Achimaş, and Cristea Ciprian. 2013. “Research Concerning the Springback Prediction in the Bending Operations.” Advanced engineering forum 8-9: 490–99. https://doi.org/10.4028/www.scientific.net/aef.8-9.490
• Sereez, Mohamed, Nikolay Abramov, and Mikhail G. Goman. 2018. “Impact of Ground Effect on Airplane Lateral Directional Stability during Take-Off and Landing.” Open Journal of Fluid Dynamics 08 (01): 1–14. https://doi.org/10.4236/ojfd.2018.81001
• Sevier, John R., Jr. 1960. Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body. NASA-TM-X-172. NASA. https://ntrs.nasa.gov/citations/19980228048
• Sezawa, Katsutada, Satosi Kubo, and Hirosi Miyazaki. 1936. “A Method of Raising the Critical Speed for Wing Flutter.” Proceedings of the Imperial Academy 12 (10): 335–37. https://doi.org/10.2183/pjab1912.12.335
• Sezgin, Aziz, Birkan Durak, Alaattin Sayın, et al. 2023. “Flutter of a Plate at High Supersonic Speeds.” Preprint, . https://doi.org/10.20944/preprints202311.0916.v1
• Sforza, Pasquale. 2014. “Landing Gear Design.” In Commercial Airplane Design Principles. Elsevier. https://doi.org/10.1016/b978-0-12-419953-8.00007-3
• 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. 1982. “Flight-Determined Correction Terms for Angle of Attack and Sideslip.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1374. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1374
• 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
• Shagiev, Marat, Alexey Kruglov, Oleg Rudenko, and Mariya Murzinova. 2022. “Superplastic Forming of Titanium Alloys at 700°C.” Letters on Materials 12 (4): 332–35. https://doi.org/10.22226/2410-3535-2022-4-332-335
• Shah, Syed Hassan R., and Anwar Ahmed. 2023. “An Investigation of the Canard Aspect Ratio and Spacing on the Aerodynamics of the Main Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-1982. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1982
• Shah, Gautam, and J. Granda. 1998. “Application of Forebody Strakes for Directional Stability and Control of Transport Aircraft.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4448
• Shams, Taimur A., Syed Irtiza Ali Shah, Muhammad Ayaz Ahmad, Aamer Shahzad, Syed Tauqeer ul Islam Rizvi, and Zahid Mehmood. 2023. “Experimental Investigation of Wing Rock on a Low Aspect Ratio Flying Wing Micro Aerial Vehicle Using Pyramidal Balance.” In AIAA SCITECH 2023 Forum. AIAA 2023-0814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0814
• Shan, Ti Kun, and Li Liu. 2011. “Springback Prediction of the TRIP Sheet Steel Stamping.” Advanced materials research 221: 152–58. https://doi.org/10.4028/www.scientific.net/amr.221.152
• Shanabarger, Mickey R. 1990. “Characterization of Hydrogen Interactions with the Surface of Alpha-2 Titanium Aluminide Alloys.” In International Conference on the Effect of Hydrogen on the Behavior of Materials. https://ntrs.nasa.gov/citations/19910044163
• Shang, Baozhong, W. F. Mao, and Z.-Q. Li. 1996. “Superplastic Forming of a Ti3 Al Alloy and Its Application in Aerospace.” In Materials science forum, vol. 243-245. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.243-245.775
• Shanmugam, Ragavanantham, Muthuramalingam Thangaraj, Geethapriyan Thangamani, and Monsuru Ramoni. 2023. “Enhancing the Performance Measures of Electrical Discharge Machining Using Additive Manufactured Copper Tool Electrode on Drilling Titanium Alloy Specimens.” In Volume 4: Advanced Materials: Design, Processing, Characterization and Applications; Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2023-112922
• Shantz, I. 1953. Wind-Tunnel Investigation of the Cvac Supersonic Bomber (HUSTLER-MX-1964). Defense Technical Information Center. https://doi.org/10.21236/ad0037850
• Shao, Lin. 2010. “Flutter of a Cantilevered Plate.” PhD diss.. https://doi.org/10.5353/th_b4559031
• Sharma, Pankaj Kumar, Vijay Gautam, and Atul Kumar Agrawal. 2020. “Analytical and Numerical Prediction of Springback of SS/Al-Alloy Cladded Sheet in V-Bending.” Journal of Manufacturing Science and Engineering 143 (3): 031011. https://doi.org/10.1115/1.4048953
• Sharp, W. H. 1957. “Alloy Titanium in the J57 Turbojet Engine.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/570197
• 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
• Shaw, R. J., J. F. Wasserbauer, and H. E. Neumann. 1976. Boundary Layer Bleed System Study for a Full-Scale, Mixed-Compression Inlet with 45 Percent Internal Contraction. NASA-TM-X-3358. NASA. https://ntrs.nasa.gov/citations/19760012992
• Shearwood, Thomas R., Mostafa R. Nabawy, William Crowther, and Clyde Warsop. 2021. “A Control Allocation Method to Reduce Roll-Yaw Coupling on Tailless Aircraft.” In AIAA Scitech 2021 Forum. AIAA 2021-1826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1826
• Shelton, Andrew, Christopher Martin, and Walter Silva. 2018. “Characterizing Aerodynamic Damping of a Supersonic Missile with CFD.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20180006293
• Shen, Guozhe. 2005. “Springback Simulation and Tool Surface Compensation Algorithm for Sheet Metal Forming.” In AIP Conference Proceedings, vol. 778. AIP. https://doi.org/10.1063/1.2011242
• Shen, Yanjie, Chen Bu, Yanling Wang, Shuai Feng, and Hao Chen. 2023. “Experimental Study on Low-Speed Wing Rock Characteristics of Low Aspect Ratio Flying Wing.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-7652-0_11
• Shen, Lin, Da Huang, and Genxing Wu. 2018. “Experimental Investigation of Yawing–rolling Coupling Effects on Unsteady Aerodynamic Characteristics of an Aircraft.” Modern Physics Letters B 32 (12n13): 1840033. https://doi.org/10.1142/s021798491840033x
• Shen, Jiwu, Konstanty Masiulaniec, and Abdollah Afjeh. 2006. “Turbojet Engine Simulation Using Dymola.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4796
• Shevchenko, A. M. 2018. “The Energy Method for Predicting the Aircraft Brake-Way.” Mehatronika, Avtomatizacia, Upravlenie 19 (6): 424–30. https://doi.org/10.17587/mau.19.424-430
• Shevchenko, Andrey, and Galina Nachinkina. 2018. “Development of Method for Predicting the Aircraft Brake-Way and Investigation of Its Reliability.” In AIP Conference Proceedings, vol. 2046. Author(s). https://doi.org/10.1063/1.5081607
• Shi, Fenghui. 2019. “Multi-Objective Optimization of Passive Shock Absorber for Landing Gear.” American Journal of Mechanical Engineering 7 (2): 79–86. https://doi.org/10.12691/ajme-7-2-4
• Shi, X., J-T. Chang, W. Bao, D. Yu, and B. Li. 2010. “Supersonic Inlet Buzz Margin Control of Ducted Rockets.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 224 (10): 1131–39. https://doi.org/10.1243/09544100jaero687
• Shi, Fenghui, Warren Isaac Anak Dean, and Taikei Suyama. 2019. “Single-Objective Optimization of Passive Shock Absorber for Landing Gear.” American Journal of Mechanical Engineering 7 (3): 107–15. https://doi.org/10.12691/ajme-7-3-1
• Shields, Matt, and Kamran Mohseni. 2012b. “Static and Dynamic Lateral Loads for a Low Aspect Ratio Wing at Low Reynolds Numbers.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3117
• Shields, Matthew C., and Kamran Mohseni. 2013a. “Aerodynamic Damping Derivatives of Low Aspect Ratio Wings at Low Reynolds Numbers.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3192
• Shigematsu, Junji, Kazuomi Yamamoto, Kazuo Shiraishi, and Atsushige Tanaka. 1990. “A Numerical Investigation of Supersonic Inlet Using Implicit TVD Scheme.” In 26th Joint Propulsion Conference. AIAA 1990-2135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2135
• Shigematsu, Junji, Kazuomi Yamamoto, Kazuo Shiraishi, and Atsushige Tanaka. 1991. “A Numerical Investigation for Supersonic Inlet with Throat Cavity.” In 27th Joint Propulsion Conference. AIAA 1991-2477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2477
• Shimabukuro, K., H. Welge, and A. Lee. 1979. “Inlet Design Studies for a Mach 2.2 Advanced Supersonic Cruise Vehicle.” In Aircraft Systems and Technology Meeting. AIAA 1979-1814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1814
• Shin, Phil-Kwon. 2005. “Buzz Suppression of Supersonic Air Inlet by Cowl Position Modification.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (3): 10–17. https://doi.org/10.5139/jksas.2005.33.3.010
• Shirizly, A. 2005. “Forming Limit Diagram of Titanium and Stainless Steel Alloys to Study the Formability of Hydro-Mechanical Deep Drawing Parts.” In AIP Conference Proceedings, vol. 778. AIP. https://doi.org/10.1063/1.2011268
• Shiryaev, A. V., M. V. Maysak, V. V. Kremenchutsky, R. M. Safin, and V. V. Demidov. 2023. “On the Issue of Reducing the Temperature Heating of the Airframe Structure of a Supersonic Aircraft.” E3S Web of Conferences 383: 05009. https://doi.org/10.1051/e3sconf/202338305009
• 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
• Shives, T. Robert. 1973. Fractographic Examination of Sabreliner Landing Gear Fracture. National Bureau of Standards. https://doi.org/10.6028/nbs.ir.73-117
• Shmilovich, Arvin, Yoram Yadlin, Paul M. Vijgen, and Rene Woszidlo. 2023. “Flow Control for Enhanced Aileron Effectiveness on a Commercial Aircraft.” In AIAA SCITECH 2023 Forum. AIAA 2023-0655. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0655
• Shortal, Joseph A., and William J. O’Sullivan. 1962. “Section m. Instrumented Models in Free Flight.” In High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030-015
• Shrout, B. L. 1965. Zero Lift-Drag at Mach 1.42, 1.83, and 2.21 of a Series of Wings with Variations of Thickness Ratio and Chord. NASA-TN-D-2811. NASA. https://ntrs.nasa.gov/citations/19650014089
• Shrout, Barrett L. 1977. Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of a Supersonic Cruise Fighter Configuration with a Design Mach Number of 1.8. NASA-TM-X-3559. NASA. https://ntrs.nasa.gov/citations/19770025137
• Shu, Ning, Hongbin Gu, and Hui Liu. 2020. “Analysis of Temperature Effect on Damping Characteristics of Landing Gear Shock Absorber.” In Proceedings of the 2020 International Conference on Aviation Safety and Information Technology. ACM. https://doi.org/10.1145/3434581.3434593
• Shucheng, Zhang, and Huang Xijun. 1994. Numerical Investigation to S-Inlet Flows (Numerical Simulation Study of S-Inlet Flows). Defense Technical Information Center. https://doi.org/10.21236/ada289590
• Shulman, A., H. J. Parry, and N. Shapiro. 1966. “Study of Wall-Pressure Fluctuations in a Supersonic-Engine Inlet Duet.” Journal of the Acoustical Society of America 39 (6_Supplement): 1254–1254. https://doi.org/10.1121/1.1942873
• Siano, Claas. 2014. “Der Lockheed F-104(G) Starfighter: Ein Amerikanisches Flugzeug Für Europäische Luftwaffen?” In Sonderfall Bundeswehr?. DE GRUYTER. https://doi.org/10.1524/9783110348231.351
• Sibilski, Krzysztof, and Wieslaw Wróblewski. 2012. “Prediction of Aircraft Spin Characteristics by Continuation and Bifurcation Methos.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4799
• 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
• Silton, Sidra I., Frank Fresconi, and Ilmars Celmins. 2014. High Maneuverability Airframe: Investigation of Fin and Canard Sizing for Optimum Maneuverability. Defense Technical Information Center. https://doi.org/10.21236/ada611082
• Silva, Murilo Caetano da. n.d. “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, Tarcisio M. P., and Carlos De Marqui Junior. 2014. “Self-Powered Active Control for an Aeroelastic Plate-Like Wing Using Piezoelectric Material.” In Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation and Control of Adaptive Systems; Structural Health Monitoring; Keynote Presentation. American Society of Mechanical Engineers. https://doi.org/10.1115/smasis2014-7539
• 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
• Sim, Alex G., and Robert E. Curry. 1985. Flight Characteristics of the AD-1 Oblique-Wing Research Aircraft. NASA-TP-2223. NASA. https://ntrs.nasa.gov/citations/19870009137
• Simenz, Rod F. 1965. Evaluation of Large Titanium Alloy Forgings. Defense Technical Information Center. https://doi.org/10.21236/ad0477212
• Simmons, Benjamin M., James L. Gresham, and Craig A. Woolsey. 2023a. “Nonlinear Dynamic Model Identification for Aircraft with Unknown Mass Properties Using Flight Data.” In AIAA SCITECH 2023 Forum. AIAA 2023-0040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0040
• Simon, James, and William Blake. 1999. “Missile Datcom: High Angle of Attack Capabilities.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4258
• Simon, James, William Blake, and Dieter Multhopp. 1993. “Control Concepts for a Vertical Tailless Fighter.” In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-4000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4000
• 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, Graham, and Trevor Birch. 2001. “Some Aerodynamic Characteristics of Missiles Having Very Low Aspect Ratio Wings.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-2410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2410
• 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
• 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
• Singh, Raghwendra Kishore, and A. Chowdhury. 2021. “State Feedback Based Stability Augmentation System for Airplane Aviation.” In Mantech Publications eBooks. https://doi.org/10.47531/mantech/ecc.2021.42
• 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, Kamaljit, and Virat Khanna. 2020. “Current Developments in Machining of Titanium Based Alloys Using Wire EDM.” In Advances in Nonconventional Machining Processes. BENTHAM SCIENCE PUBLISHERS. https://doi.org/10.2174/9789811483653120010009
• 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, P. N., B. K. Singh, and V. Singh. 1998. “Phase Instability in Titanium Alloy GTM-900 during Lowcycle Fatigue at Elevated Temperature.” In Low Cycle Fatigue and Elasto-Plastic Behaviour of Materials. Elsevier. https://doi.org/10.1016/b978-008043326-4/50062-3
• Singh Sandhu, Jatinder Pal, Ik Soo Park, and Narayan Ananthkrishnan. 2025a. “CFD Analysis of Supersonic Intakes.” In Computational Design and Optimization of Supersonic Intakes. CRC Press. https://doi.org/10.1201/9781003492108-5
• Singh Sandhu, Jatinder Pal, Ik Soo Park, and Narayan Ananthkrishnan. 2025b. “Reduced-Order Modeling of Supersonic Intakes.” In Computational Design and Optimization of Supersonic Intakes. CRC Press. https://doi.org/10.1201/9781003492108-4
• Singh Sandhu, Jatinder Pal, Ik Soo Park, and Narayan Ananthkrishnan. 2025c. “Supersonic Diffuser Duct Design.” In Computational Design and Optimization of Supersonic Intakes. CRC Press. https://doi.org/10.1201/9781003492108-6
• Singh Sandhu, Jatinder Pal, Ik Soo Park, and Narayan Ananthkrishnan. 2025d. “Supersonic Diffuser Optimization.” In Computational Design and Optimization of Supersonic Intakes. CRC Press. https://doi.org/10.1201/9781003492108-7
• Sinha, Jayanta, Sanjay Singh, and Om Prakash. 2026. “Optimizing MRD Inlet Performance through Disk Geometry Modification at Supersonic Flow Regime.” FME Transactions 54 (2): 380–89. https://doi.org/10.5937/fme2602380s
• Siring, Janina. 2025. “Numerical Process Design for Hot Forging of Steel Encased Titanium Workpieces.” In Materials Research Proceedings, vol. 54. Materials Research Forum LLC. https://doi.org/10.21741/9781644903599-92
• Sisk, Thomas R., and William H. Andrews. 1955. Flight Experience with a Delta-Wing Airplane Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. NACA-RM-H55H03. NASA. https://ntrs.nasa.gov/citations/19930088985
• Siu, Marie-Michele, Borja Martos, and John Foster. 2013. “Flight Test Results of an Angle of Attack and Angle of Sideslip Calibration Method Using Output-Error Optimization.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-5086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5086
• Sivan, M. 1971. “A Lateral Directional Oscillation Problem in a Conventional STOL Aircraft.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-792. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-792
• Sivo, J. N., and J. P. Wanhainen. 1958. Use of Highly Reactive Chemical Additives to Improve Afterburner Performance at Altitude. NACA-RM-E58G10. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19650014455
• “Sizing the Engine: Installed Performance.” 2002. In Aircraft Engine Design, Second Edition. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861444.0189.0230
• “Sizing the Engine: Installed Performance.” 2018. In Aircraft Engine Design, Third Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105173.0221.0272
• Skare, Steven Edward. n.d. “An Inverse Design Method for Supersonic Airfoils.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2012.44
• Skarman, B. 1978. “Estimation of Parameters in the Time Variable Dynamics of a Missile from Flight Test Data.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1330
• Skira, Charles. 1999. “Will There Ever Be Another New Military Aircraft Engine Development Program?” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2660
• Sklar, Andrew, and Zvi Rusak. 2020. “Busemann-Sears-Haack Hybrid Geometries Applied toward Supersonic Commercial Vehicles for Improved Wave Drag Performance.” In AIAA Scitech 2020 Forum. AIAA 2020-0752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0752
• Skorupka, Zbigniew, Rafał Kajka, R. Harla, et al. 2009. “Active Control of Landing Gear Shock Absorber Characteristic Using Magnetoreological Fluids.” In Diffusion and defect data, solid state data. Part B, Solid state phenomena/Solid state phenomena, vol. 154. Scientific.net. https://doi.org/10.4028/www.scientific.net/ssp.154.195
• Slater, John W. n.d.-a. “Off-Design Analysis of Axisymmetric External-Compression Supersonic Inlets for Mach 1.4 to 2.0.” In International Society for Airbreathing Engines (ISABE) Conference. https://ntrs.nasa.gov/citations/20240007797
• Slater, John W. n.d.-b. “Streamline-Traced, External-Compression Supersonic Inlets for Mach 2.” In 25th Conference of the International Society for Air Breathing Engines (2022 ISABE). https://ntrs.nasa.gov/citations/20220012800
• Slater, John. 2001. “Verification Assessment of Flow Boundary Conditions for CFD Analysis of Supersonic Inlet Flows.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3882
• Slater, John W. 2011. “External-Compression Supersonic Inlet Design Code.” In 2011 Fundamental Aeronautics Program Technical Conference. https://ntrs.nasa.gov/citations/20110011374
• Slater, John W. 2012. Design and Analysis Tool for External-Compression Supersonic Inlets. NASA/TM-2012-217660. NASA. https://ntrs.nasa.gov/citations/20120013600
• Slater, John W. 2014. “Methodology for the Design of Streamline-Traced External-Compression Supersonic Inlets.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140016826
• Slater, John W. 2015. “Enhanced Performance of Streamline-Traced External-Compression Supersonic Inlets.” In NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20150021040
• Slater, John W. 2016. “SUPIN: A Computational Tool for Supersonic Inlet Design.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0530
• Slater, John W. 2019. “Refinement of Vortex Generators in a Streamline-Traced, External-Compression Supersonic Inlet.” In AIAA Scitech 2019 Forum. AIAA 2019-1447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1447
• Slater, John W. 2020. “Design Factors for Two-Dimensional, External-Compression Supersonic Inlets.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20200000515
• Slater, John W. 2024. SUPIN: A Tool for the Aerodynamic Design and Analysis of Supersonic Inlets. NASA/TM-20240008586. NASA. https://ntrs.nasa.gov/citations/20240008586
• Slater, John W., and J. Dave Saunders. 2011. “Status of the Combined-Cycle Engine Large-Scale Inlet Mode Transition Experiment.” In 2011 Fundamental Aeronautics Program Technical Conference. https://ntrs.nasa.gov/citations/20110011363
• Sleeman, William C., Jr. 1953. Investigation of the Effects of Propeller Operation on the Low-Speed Stability and Control Characteristics of a 1/6-Scale Model of a Revised Configuration of the Republic XF-84H Airplane. NACA-RM-SL53I24. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028463
• Sleeman, William C., Jr. 1957. Investigation at High Subsonic Speeds of the Static Longitudinal and Lateral Stability Characteristics of Two Canard Airplane Configurations. NACA-RM-L57J08. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019253
• Sleeman, William C., Jr., and William D. Morrison Jr. 1953. Low-Speed Investigation of the Static Lateral Stability and Control Characteristics of a 1/6-Scale Model of the Republic XF-84H Airplane with the Propeller Operating. NACA-RM-SL53G10. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029410
• 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
• Slota, Ján, and Miroslav Jurčišin. 2012. “Experimental and Numerical Prediction of Springback in V-Bending of Anisotropic Sheet Metals for Automotive Industry.” Scientific Letters of Rzeszow University of Technology - Mechanics 84 (3/2012): 55–68. https://doi.org/10.7862/rm.2012.5
• Slota, Ján, Miroslav Jurčišin, Emil Spišák, and Tomáš Sleziak. 2014. “An Investigation of Springback in Sheet Metal Forming of High Strength Steels.” Applied Mechanics and Materials 693: 370–75. https://doi.org/10.4028/www.scientific.net/amm.693.370
• Smaili, Hafid. 2002. “Simulator Evaluation of New Experimental Techniques for Aircraft Pilot Coupling Susceptibility Assessment.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4802
• Smart, Michael, Iraj Kalkhoran, and James Bentson. 1994. “Measurements of Supersonic Wing Tip Vortices.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2576
• 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
• Smeltzer, D., and N. Sorensen. 1972a. “Performance Estimates for a Supersonic Axisymmetric Inlet System.” In 10th Aerospace Sciences Meeting. AIAA 1972-45. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-45
• Smeltzer, D. B., and N. E. Sorensen. 1972b. Tests of a Mixed Compression Axisymmetric Inlet with Large Transonic Mass Flow at Mach Numbers 0.6 to 2.65. NASA-TN-D-6971. NASA. https://ntrs.nasa.gov/citations/19730005050
• Smeltzer, D. B., and N. E. Sorensen. 1973. Analytic and Experimental Performance of Two Isentropic Mixed Compression Axisymmetric Inlets at Mach Numbers 0.8 to 2.65. NASA-TN-D-7320. NASA. https://ntrs.nasa.gov/citations/19730017090
• 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, J. H. B. 1961. “Lift/Drag Ratios of Optimised Slewed Elliptic Wings at Supersonic Speeds.” Aeronautical Quarterly 12 (3): 201–18. https://doi.org/10.1017/s0001925900002067
• 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, Charles, Judy Bergmann, and Terry Riddle. 2004. “Current Airframe Propulsion Integration Testing Techniques at AEDC.” In USAF Developmental Test and Evaluation Summit. AIAA 2004-6819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6819
• Smith, R., and V. Dahlem. 1981. “Experimental and Analytical Development of an Advanced Supersonic Fighter Concept.” In Aircraft Systems and Technology Conference. AIAA 1981-1659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1659
• Smith, Norman F., and Lowell E. Hasel. 1952. As Investigation at Mach Numbers of 1.41 and 2.01 of the Aerodynamic Characteristics of an 0.025-Scale Model of the MX-1712. NACA-RM-SL52J17. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090024216
• Smith, Wade, and Paul Pellicano. 1992. “X-29 High Angle-of-Attack Military Utility Flight Test Results.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4080
• Smith, Stephen W., and Robert S. Piascik. 2001. Fatigue Crack Growth Characteristics of Thin Sheet Titanium Alloy Ti 6-2-2-2-2. NASA/TM-2001-210830. NASA. https://ntrs.nasa.gov/citations/20010032404
• Smith, C. Frederic, and Steve D. Podleski. 1994. Installed F/A-18 Inlet Flow Calculations at 30 Degrees Angle-of-Attack: A Comparative Study. NASA-CR-195297. NASA. https://ntrs.nasa.gov/citations/19940028613
• Smith, Luke, and Kunihiko Taira. 2024. “The Effect of Reynolds Number on the Separated Flow over a Low-Aspect-Ratio Wing.” Journal of Fluid Mechanics 992: R2. https://doi.org/10.1017/jfm.2024.748
• Smith, an D., IV, Charles V. Leonard, and Harry E. Bloomer. 1953. Altitude Performance and Operational Characteristics of YJ71-A-7 Turbojet Engine. NACA-RM-E53E13. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090023637
• Smits, A. J. 1988. Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers. Defense Technical Information Center. https://doi.org/10.21236/ada191494
• Snell, S., William Garrard Jr., and Dale Enns. 1991. “Optimization of Lateral-Directional Dynamics for an Aircraft Operating at High Angle of Attack.” In Navigation and Control Conference. AIAA 1991-2711. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2711
• Snyder, Thomas L. 1947. 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, Thomas L. 1948. Free-Spinning-Tunnel Tests of a 1/29-Scale Model of the Republic XP-91 Airplane with a Vee Tail Installed. NACA-RM-L7L03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019414
• Snyder, Deryl, and Curtis Memory. 2005. “A Modified Vortex Algorithm for Low Reynolds Number, Low Aspect-Ratio Wings.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4608
• Sóbester, András. 2010. Propulsion Integration: Supersonic Transport Aircraft. Wiley. https://doi.org/10.1002/9780470686652.eae489
• Sogukpinar, Haci. 2018. “Estimation of Supersonic Fighter Jet Airfoil Data and Low Speed Aerodynamic Analysis of Airfoil Section at the Mach Number 0.15.” In AIP Conference Proceedings, vol. 1935. Author(s). https://doi.org/10.1063/1.5025956
• Soistmann, David L., and Charles V. Spain. 1993. “An Experimental and Analytical Study of a Lifting-Body Wind-Tunnel Model Exhibiting Body-Freedom Flutter.” 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/19930049894
• Solies, U. 1995. “Low Speed Handling Qualities of the High Speed Civil Transport.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3912. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3912
• Soltani, Mohammad Reza, and Rasoul Askari. 2018. “Experimental Study on the Performance of a Body-Integrated Y-Shaped Supersonic Inlet.” In 2018 Joint Propulsion Conference. AIAA 2018-4456. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4456
• Soltani, Mohammad Reza, Abbas Daliri, and Javad Sepahi Younsi. 2016. “Effects of Shock Wave/Boundary-Layer Interaction on Performance and Stability of a Mixed-Compression Inlet.” Scientia Iranica 23 (4): 1811–25. https://doi.org/10.24200/sci.2016.3928
• Soltani, M. R., M. Farahani, and M. H. Asgari Kaji. 2011. “An Experimental Study of Buzz Instability in an Axisymmetric Supersonic Inlet.” Scientia Iranica 18 (2): 241–49. https://doi.org/10.1016/j.scient.2011.03.019
• “Some Current Types of Landing Gear: A Survey of the Solutions Adopted in Landing Gear Design for a Range of Modern Aircraft.” 1968. Aircraft Engineering and Aerospace Technology 40 (1): 26–31. https://doi.org/10.1108/eb034335
• Sorbilli, Rodrigo, Davi H. Di Bianchi, Pedro Ciloni, Walter Afonso, Raphael Pereira, and Adson A. de Paula. 2018. “Evaluation of Transonic Airfoil Geometrical Parameters Effect in Drag Divergence Mach Number and the Associated Impact in Aircraft Design Multi-Disciplinary Optimization.” In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2018-1653. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1653
• Soreide, Davis, Rodney Bogue, Jonathan Seidel, et al. 1997. “The Use of a Lidar Forward-Looking Turbulence Sensor for Mixed-Compression Inlet Unstart Avoidance and Gross Weight Reduction on a High Speed Civil Transport.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3035
• Sorensen, N., and D. Bencze. 1973. “Possibilities for Improved Supersonic Inlet Performance.” In 9th Propulsion Conference. AIAA 1973-1271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1271
• Sorensen, N., E. Latham, and D. Smeltzer. 1974. “Variable Geometry for Supersonic Mixed-Compression Inlets.” In 10th Propulsion Conference. AIAA 1974-1172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1172
• Sorenson, J. 1974. “Influence of Boundary Layer Blowing on the Low-Speed Aerodynamic Performance of a 45 Degree Swept-Wing Airplane.” In 10th Annual Meeting and Technical Display. AIAA 1974-269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-269
• Sornsuwit, Nuttaphong, and Sunthorn Sittisakuljaroen. 2014. “The Influence of Temperature on Secondary Forming of Titanium Gr 2 Sheet by Use of Single Point Incremental Forming.” Advanced materials research 979: 351–54. https://doi.org/10.4028/www.scientific.net/amr.979.351
• Sorrells, R., M. Towne, C. Anderson, and R. Tolbert. 1984. “Effects of Inlet Spillage on Store Carriage Loads and Launch Trajectories.” In 13th Aerodynamic Testing Conference. AIAA 1984-615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-615
• Sorrells, Russell B., Matthew C. Towne, Charles F. Anderson, and Ronald H. Tolbert. 1985. Effects of Inlet Spillage on Store Carriage Loads and Launch Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ada531358
• Sotheran, A. 1987. “High Performance Turbofan Afterburner Systems.” In 23rd Joint Propulsion Conference. AIAA 1987-1830. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1830
• Soto, Hector, and Corey Hernandez. 2004. “Comparison of Engine/inlet Distortion Measurements with MEMS and ESP Pressure Sensors.” In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2004-2398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2398
• 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
• 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
• Spaid, F. 1984. “Transonic Airfoil and Wing Flowfield Measurements.” In 22nd Aerospace Sciences Meeting. AIAA 1984-100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-100
• Spathopoulos, Stefanos C., and Georgios E. Stavroulakis. 2020. “Springback Prediction in Sheet Metal Forming, Based on Finite Element Analysis and Artificial Neural Network Approach.” Applied Mechanics 1 (2): 97–110. https://doi.org/10.3390/applmech1020007
• Spearman, M. 1979. “Historical Development of Worldwide Supersonic Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1979-1815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1815
• Spearman, M. L. 1983. Effect of External Stores on the Stability and Control Characteristics of a Delta Wing Fighter Model at Mach Numbers from 0.60 to 2.01. NASA-TM-84596. NASA. https://ntrs.nasa.gov/citations/19830009237
• Spearman, M. 1986. “Effects of Some Geometric Variations on Missile Aerodynamic Characteristics at Supersonic Speeds.” In 24th Aerospace Sciences Meeting. AIAA 1986-570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-570
• Spearman, M. Leroy, and Cornelius Driver. 1956. Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104A Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. AF-245. NACA-RM-SL56H06. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026345
• 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
• Spearman, M. Leroy, Ross B. Robinson, and Cornelius Driver. 1956. Longitudinal and Lateral Stability, Control Characteristics, and Vertical-Tail-Load Measurements for 0.03-Scale Model of the Avro CF-105 Airplane at Mach Number 1.41. NACA-RM-SL56H27. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028458
• Spearman, M., David Tice, and Dorothy Braswell. 1992. “Some Effects of Wing and Body Geometry on the Aerodynamic Characteristics of Configurations Designed for High Supersonic Mach Numbers.” In Guidance, Navigation and Control Conference. AIAA 1992-4246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4246
• “Special Features of Antiaircraft Rockets with Swept or Low-Aspect-Ratio Wings.” 2010. In German Development of the Swept Wing 1935–1945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867552.0545.0614
• Spencer, B., Jr. 1960. Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-Sweep Wings. NASA-TM-X-303. NASA. https://ntrs.nasa.gov/citations/19660024029
• Spiral Failure: “O” Ring Seals: Landing Gear Shock Struts. 1953. https://doi.org/10.4271/air36
• Spreiter, John R. 1950. The Aerodynamic Forces on Slender Plane- and Cruciform-Wing and Body Combinations. NACA-TR-962. NASA. https://ntrs.nasa.gov/citations/19930092025
• Spreiter, John R., and Alberta Y. Alksne. 1957. Thin Airfoil Theory Based on Approximate Solution of the Transonic Flow Equation. NACA-TN-3970. NASA. https://ntrs.nasa.gov/citations/19930084679
• “Springback Analysis in Sheet Metal Forming by Using the Ramberg-Osgood Stress-Strain Relation.” 2016. Прикладная механика и техническая физика, no. 6. https://doi.org/10.15372/pmtf20160622
• “Springback Simulation of U-Channel Forming Process Based on Finite Element Analysis.” 2016. International Journal of Science and Research (IJSR) 5 (3): 1487–90. https://doi.org/10.21275/v5i3.nov162218
• 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. 1967. “Calculated Pressure Distributions and Shock Shapes on Thick Conical Wings at High Supersonic Speeds.” Aeronautical Quarterly 18 (2): 185–206. https://doi.org/10.1017/s0001925900004182
• Squires, Kyle D. 2002. A New Approach to Prediction of Aircraft Spin. Defense Technical Information Center. https://doi.org/10.21236/ada410100
• Squires, Kyle D. 2004. A High Resolution Aeroelasticity Method for Fighter Aircraft at Flight Reynolds Numbers. Defense Technical Information Center. https://doi.org/10.21236/ada427305
• Srichitturi, Ishaan. 2026. “Machine-Learning Surrogates for Airfoil Pitching Moment: Accuracy, Extrapolation, and the Finite-Thickness Shift of the Aerodynamic Center.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-11247822/v1
• Srinathkumar, S., Padma Madhuranath, and Girija Gopalratnam. 1993. “Estimation of Neutral and Maneuver Points of Aircraft by Dynamic Maneuvers.” In Flight Simulation and Technologies. AIAA 1993-3620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3620
• 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
• Srivastava, Shashank, Murali Damodaran, and Boo Cheong Khoo. 2019. “A Computational Framework for Assessment of Fuel Sloshing Effects on Transonic Wing Flutter Characteristics.” In AIAA Scitech 2019 Forum. AIAA 2019-1527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1527
• 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
• “The Stability and Control of Slender Delta Aircraft: An Evaluation of the Different Behaviour Characteristics of a Large Supersonic Transport Aircraft of Slender Delta Form When Compared with a Conventional Aircraft.” 1968. Aircraft Engineering and Aerospace Technology 40 (6): 22–29. https://doi.org/10.1108/eb034386
• Stachiw, Terrin. n.d. “Synthesis and Optimization of Mechanical Networks with Inerters in Landing Gear for Improved Landing Performance and Vibration Control at Touchdown Considering Airframe Flexibility.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2020-14047
• Stagner, R. 1980. Application of Accelerated Tool Life Tests to Machining of Titanium. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/5028457
• 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
• Stallings, R., Jr. 1979. “Effect of Reynolds Number on the Aerodynamic Characteristics of a Cruciform Wing-Body Configuration.” In 17th Aerospace Sciences Meeting. AIAA 1979-301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-301
• Stallings, R., Jr., and M. Lamb. 1981. “Wing-Alone Aerodynamic Characteristics at High Angles of Attack.” In 19th Aerospace Sciences Meeting. AIAA 1981-8. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-8
• Stalnov, Oksana, David Angland, and Xin Zhang. 2013. “On the Contribution of Individual Landing Gear Components to Landing Gear Loads and Noise.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3153
• Stanbrook, A. 1954. “Lift-Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight-Tapered Wings.” Aircraft Engineering and Aerospace Technology 26 (8): 244–57. https://doi.org/10.1108/eb032455
• Stander, Nielen, Mike Burger, Xinhai Zhu, and Bradley Maker. 2002. “Springback Compensation in Sheet Metal Forming Using a Successive Response Surface Method.” In 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. AIAA 2002-5539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5539
• Stanford, Bret. 2021. “Scaled Aeroelastic Wind Tunnel Model Design with Topology Optimization.” In AIAA Aviation 2021 Forum. AIAA 2021-3083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3083
• Stanford, Bret K., and Kevin E. Jacobson. n.d. “Transonic Flutter Dips of the AGARD 445.6 Wing.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20220017734
• Stanford, Bret, and Kevin Jacobson. 2023. “Transonic Flutter Dips of the AGARD 445.6 Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-0589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0589
• Stanford, Bret, Steve Massey, Kevin Jacobson, and Pawel Chwalowski. 2026. “Transonic Aeroelastic Flutter Computations with Mesh Adaptation.” In AIAA SCITECH 2026 Forum. AIAA 2026-0811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0811
• Stanford, Bret, Andrew Thelen, and Kevin Jacobson. 2024. “Multifidelity Optimization with Transonic Flutter Constraints.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4025
• Stanišić, Milomir M. 1962. “On a Theory for Unsteady Motion of Rectangular Wing in Supersonic Flow.” Quarterly of Applied Mathematics 20 (3): 231–40. https://doi.org/10.1090/qam/142273
• Staples, D., and M. Nagati. 1990. “Finite Wing Lift Prediction at High Angles of Attack.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3079. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3079
• 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, 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
• “Static Aeroelasticity.” 2002. In Introduction to Structural Dynamics and Aeroelasticity. Cambridge University Press. https://doi.org/10.1017/cbo9780511809170.004
• “Static Aeroelasticity.” 2005. In Solid Mechanics and Its Applications. Springer Netherlands. https://doi.org/10.1007/1-4020-2106-2_2
• “Static Aeroelasticity.” 2011. In Introduction to Structural Dynamics and Aeroelasticity. Cambridge University Press. https://doi.org/10.1017/cbo9780511997112.006
• Static Aeroelasticity and Flutter. 2014. Wiley. https://doi.org/10.1002/9781118700440.ch22
• Static Aeroelasticity – Effect of Wing Flexibility on Control Effectiveness. 2014a. Wiley. https://doi.org/10.1002/9781118700440.ch8
• Static Aeroelasticity – Effect of Wing Flexibility on Lift Distribution and Divergence. 2014b. Wiley. https://doi.org/10.1002/9781118700440.ch7
• “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
• Stauffer, Amy C., and Ernest J. Czyryca. 2004. Fatigue Crack Growth Rate Behavior in Titanium Alloy Ti-5111 Weld Metal. Defense Technical Information Center. https://doi.org/10.21236/ada430233
• Stauffer, Amy C., Ernest J. Czyryca, and Donald A. Koss. 2004. The Influence of Processing on the Microstructure and Properties of the Titanium Alloy Ti-5111. Defense Technical Information Center. https://doi.org/10.21236/ada430238
• Stein, Jared J. 1998. “The Effect of Process Variables on Sheet Metal Springback.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/982299
• 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
• Stelmack, Marc, Stephen Batill, and Bryan Beck. 1999. “Design of an Aircraft Brake Component Using an Interactive Multidisciplinary Design Optimization Framework.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1346
• Stengel, R. 1969. “Altitude Stability in Supersonic Cruising Flight.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-813
• Stengel, Robert F. 2005. “Flight Dynamics.” Aircraft Engineering and Aerospace Technology 77 (3). https://doi.org/10.1108/aeat.2005.12777cae.002
• Stengel, R., and G. Miller. 1978. “Flying Qualities of an Aircraft with Strong Lateral-Directional Coupling.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1361
• Stephen, D. 1995. “Superplastic Forming.” In High Performance Materials in Aerospace. Springer Netherlands. https://doi.org/10.1007/978-94-011-0685-6_9
• 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, Harriet J. 1956. Flight Measurements of Horizontal-Tail Loads on the Douglas X-3 Research Airplane. NACA-RM-H56A23. NASA. https://ntrs.nasa.gov/citations/19930090107
• Sternfield, Leonard. 1949. Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds. NACA-TN-1818. NASA. https://ntrs.nasa.gov/citations/19930082492
• Stevens, Joseph E. 1955. Low-Lift Drag of the Grumman F9F-9 Airplane as Obtained by a 1/7.5-Scale Rocket-Boosted Model and by Three 1/45.85-Scale Equivalent-Body Models between Mach Numbers of 0.8 and 1.3, TED No. NACA DE 391. Rept-4987. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029377
• Stevens, F., T. On, and T. Clare. 1974. “Wrap-around vs. Cruciform Fins: Effects on Rocket Flight Performance.” In Mechanics and Control of Flight Conference. AIAA 1974-777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-777
• Stewart, H. J. 1946. “The Lift of a Delta Wing at Supersonic Speeds.” Quarterly of Applied Mathematics 4 (3): 246–54. https://doi.org/10.1090/qam/17096
• 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
• Stewartson, K. 1950a. “On the Linearized Potential Theory of Unsteady Supersonic Motion.” Quarterly Journal of Mechanics and Applied Mathematics 3 (2): 182–99. https://doi.org/10.1093/qjmam/3.2.182
• Stewartson, K. 1950b. “Supersonic Flow over an Inclined Wing of Zero Aspect Ratio.” Mathematical Proceedings of the Cambridge Philosophical Society 46 (2): 307–15. https://doi.org/10.1017/s0305004100025779
• Stewartson, K. 1952. “On the Linearized Potential Theory of Unsteady Supersonic Motion. II.” Quarterly Journal of Mechanics and Applied Mathematics 5 (2): 137–54. https://doi.org/10.1093/qjmam/5.2.137
• Stickney, Truman M. 1955. Recovery and Time-Response Characteristics of Six Thermocouple Probes in Subsonic and Supersonic Flow. NACA-TN-3455. NASA. https://ntrs.nasa.gov/citations/19930084168
• Stifel, J. M. 1979. A Time Response Approach to Equivalent Aircraft Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada085873
• Stijnen, Bas. 2026. “An Open-Source Camera-Based Trifilar Pendulum Setup for Measuring Mass Moment of Inertia of Small.” Preprint, . https://doi.org/10.2139/ssrn.6714352
• Stijnen, Bas, Joseph Thomson, Eoghan Somers, and David J. McKeown. 2023. Moment of Inertia Measurement of a CubeSat through Object Motion Tracking of Trifilar Pendulum Oscillations. https://doi.org/10.5270/esa-gnc-icatt-2023-165
• 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
• Stine, Howard A., and Richard Scherrer. 1952. Experimental Investigation of the Turbulent-Boundary-Layer Temperature-Recovery Factor on Bodies of Revolution at Mach Numbers from 2.0 to 3.8. NACA-TN-2664. NASA. https://ntrs.nasa.gov/citations/19930083361
• Stitt, Leonard E., Frank X. McKevitt, and Albert B. Smith. 1956. Effect of Throat Bleed on the Supersonic Performance of a Half-Conical Side-Inlet System. NACA-RM-E55J07. NASA. https://ntrs.nasa.gov/citations/19930088953
• Stocker, P. M. 1951. “Supersonic Flow past Bodies of Revolution with Thin Wings of Small Aspect Ratio.” Aeronautical Quarterly 3 (1): 61–79. https://doi.org/10.1017/s0001925900000548
• 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
• Stojanović, Marijana, Aleksandar Stefanović, Nebojša Jovičić, and Ivan Marić. 2024. “Testing the Roll Stabilization of a Supersonic Surface-to-Air Guided Missile.” In 11th International Scientific Conference on Defensive Technologies - OTEX 2024 - zbornik radova. Military Technical Institute, Belgrade. https://doi.org/10.5937/oteh24053s
• Stokke, Allen R., and William S. Aiken Jr. 1948. Flight Measurements of Buffeting Tail Loads. NACA-TN-1719. NASA. https://ntrs.nasa.gov/citations/19930082412
• Stone, A. H. 1945. The Aerodynamics of a Slightly Yawing Supersonic Cone. Defense Technical Information Center. https://doi.org/10.21236/ada801302
• Stone, Ralph W., and Theodore Berman. 1946. Free-Spinning-Tunnel Tests of a 1/26th Scale Model of the Douglas XTB2D-1 Airplane. NACA-RM-L6K18. NASA. https://ntrs.nasa.gov/citations/19930093799
• Stone, Ralph W., Jr. 1956. Some Notes on the Violent Lateral-Longitudinal Coupling Motions of the Douglas X-3 Airplane in Aileron Rolls. NACA-RM-L56C15. NASA. https://ntrs.nasa.gov/citations/19930089124
• Stone, R. W., Jr. 1957. Influence of Automatic Control of Roll Coupling and Pitch-up on Tail Loads. NACA-RM-L57D18A. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630008164
• Stone, Ralph W., Jr., Sanger M. Burk Jr., and William Bihrle Jr. 1950. The Aerodynamic Forces and Moments on a 1/10-Scale Model of a Fighter Airplane in Spinning Attitudes as Measured on a Rotary Balance in the Langley 20-Foot Free-Spinning Tunnel. NACA-TN-2181. NASA. https://ntrs.nasa.gov/citations/19930082832
• Stone, Ralph W., Jr., and Lee T. Daughtridge Jr. 1948. The Influence of Dimensional Modifications upon the Spin and Recovery Characteristics of a Tailless Airplane Model Having Its Wings Swept Forward 15 Deg (Cornelius XFG-1). NACA-RM-SL8H17. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019380
• Stone, Ralph W., Jr., and Richard P. White. 1948. Free-Spinning, Longitudinal-Trim, and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultke MX-813 (Prototype of XP-92) Airplane as Determined in the Langley 20-Foot Free-Spinning Tunnel. NACA-RM-SL8G26. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030064
• Stouder, D. 1981. “An Advanced Facility for Processing Aircraft Dynamic Test Data.” In 1st Flight Test Conference. AIAA 1981-2398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2398
• Stough, H. Paul, Daniel J. DeCarlo, and James M. Patton. 1987c. “Spin Resistance Evaluation of a Light Airplane.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/871021
• Stough, H., III, Daniel Dicarlo, and James Patton. 1987a. “Evaluation of Airplane Spin Resistance Using Proposed Criteria for Light General Aviation Airplanes.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2562
• Stough, H., III, and J. Patton Jr. 1979. “The Effects of Configuration Changes on Spin and Recovery Characteristics of a Low-Wing General Aviation Research Airplane.” In Aircraft Systems and Technology Meeting. AIAA 1979-1786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1786
• Stough, H. Paul, III, James M. Patton Jr., and Steven M. Sliwa. 1987b. Flight Investigation of the Effect of Tail Configuration on Stall, Spin, and Recovery Characteristics of a Low-Wing General Aviation Research Airplane. NASA-TP-2644. NASA. https://ntrs.nasa.gov/citations/19870007382
• Straight, D., and R. Cullom. 1982. “Performance of a 2D-CD Nonaxisymmetric Exhaust Nozzle on a Turbojet Engine at Altitude.” In 18th Joint Propulsion Conference. AIAA 1982-1137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1137
• Stringfield, G. 1984. The Study of an Idealized Wing/Body Junction. Defense Technical Information Center. https://doi.org/10.21236/ada139933
• Striz, Alfred G. 1991. Influence of Structural and Aerodynamic Modeling on Flutter Analysis and Structural Optimization. Defense Technical Information Center. https://doi.org/10.21236/ada248487
• Striz, Alfred G., and Vipperla B. Venkayya. 1990. “Influence of Structural and Aerodynamic Modeling on Optimization with Flutter Constraint.” In NASA. Langley Research Center, The Third Air Force(NASA Symposium on Recent Advances in Multidisciplinary Analysis and Optimization. https://ntrs.nasa.gov/citations/19940004721
• Stromberg, W. J. 1981. Performance Deterioration Based on Simulated Aerodynamic Loads Test, JT9D Jet Engine Diagnostics Program. NASA-CR-165297. NASA. https://ntrs.nasa.gov/citations/19810014553
• Stroud, John F. 1952. Experimental Investigation of the Effect of Forebody Bluntness on the Pressure Recovery and Drag of a Twin-Scoop Inlet-Body Combination at Mach Numbers of 1.4 and 1.7. NACA-RM-A51K14. NASA. https://ntrs.nasa.gov/citations/19930087185
• “Structural Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-6
• “Structure of Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-5
• Struts and Couplings Committee A-5B Gears. 1993. Plain Bearing Selection for Landing Gear Applications. https://doi.org/10.4271/air1594
• Struts and Couplings Committee A-5B Gears. 1995. Aircraft Landing Gear. https://doi.org/10.4271/arp1311a
• Struts and Couplings Committee A-5B Gears. 2006. Design Recommendations for Spare Seals in Landing Gear Shock Struts. https://doi.org/10.4271/arp4912a
• Struts and Couplings Committee A-5B Gears. 2007. Verification of Landing Gear Design Strength. https://doi.org/10.4271/air1494a
• Struts and Couplings Committee A-5B Gears. 2011. Landing Gear: Aircraft. https://doi.org/10.4271/arp1311
• Struts and Couplings Committee A-5B Gears. 2012a. Extraordinary and Special Purpose Landing Gear Systems. https://doi.org/10.4271/air4846a
• Struts and Couplings Committee A-5B Gears. 2012b. Landing Gear Shock Struts Bearing Selection. https://doi.org/10.4271/air5883
• Struts and Couplings Committee A-5B Gears. 2012c. Tests, Impact, Shock Absorber Landing Gear, Aircraft. https://doi.org/10.4271/as6053a
• Struts and Couplings Committee A-5B Gears. 2016. Landing Gear Shock Strut Heat Damage. https://doi.org/10.4271/air5913
• Struts and Couplings Committee A-5B Gears. 2017. Landing Gear Fatigue Tests with Equivalent Damage Spectra. https://doi.org/10.4271/arp5429a
• Struts and Couplings Committee A-5B Gears. 2018a. External Hydraulic Fluid Leakage Definition for Landing Gear Shock Absorbers. https://doi.org/10.4271/arp6408
• Struts and Couplings Committee A-5B Gears. 2018b. Landing Gear Component Heat Damage. https://doi.org/10.4271/air5913a
• Struts and Couplings Committee A-5B Gears. 2018c. Landing Gear Structures and Mechanisms. https://doi.org/10.4271/arp1311d
• Struts and Couplings Committee A-5B Gears. 2020. Landing Gear Shock Absorption Testing of Civil Aircraft. https://doi.org/10.4271/arp5644a
• Struts and Couplings Committee A-5B Gears. 2023. Recommended Practice for Landing Gear Integrity Programs. https://doi.org/10.4271/arp6412
• Struts and Couplings Committee A-5B Gears. 2024. Landing Gear Shock Strut Bearing Selection. https://doi.org/10.4271/air5883b
• Stubbs, William. 1956. “Supersonic Air Inlet Controls.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/560075
• “Study of Supersonic Cavity Flow in Advanced Variable Geometry Inlet.” 2004. In 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-04-s.5.06
• A Study of the Effects of Aeroelastic Divergence on the Wing Structure of an Oblique-Wing Supersonic Transport Configuration. 1973. NASA-CR-112262. NASA. https://ntrs.nasa.gov/citations/19730009309
• Su, Jingke, Anxiong Liu, Kun Luo, and Jianren Fan. 2025a. “Computational Investigation of Airframe Integration Effects on Turbojet Engine Aerodynamics and Combustion.” Journal of Engineering for Gas Turbines and Power 148 (3): 031008. https://doi.org/10.1115/1.4069792
• “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
• Suckow, Timon, Janosch Günzel, Lukas Schell, Erik Sellner, Jonathan Dagnew, and Peter Groche. 2019. “Temperatureinfluss in der Aluminiumblechumformung*/Temperature influence in aluminum sheet metal forming – springback behavior and process limits during V-bending of EN AW-6082 and EN AW-7075.” wt Werkstattstechnik online 109 (10): 733–39. https://doi.org/10.37544/1436-4980-2019-10-37
• Sudhakar Rao, P., Vikas Sharma, Harish Kumar, and Sri Phani Sushma. 2024. “Electro-Chemical Machining of Titanium Alloys and Various Composites for Efficient Machining Process.” In Fabrication Techniques and Machining Methods of Advanced Composite Materials. CRC Press. https://doi.org/10.1201/9781003427735-4
• Sudhir, Prathik Jain, Ravindra Holalu Venkatadas, and Ugrasen Gonchikar. 2020. “Machining Characteristics Estimation in WEDM Process While Machining Titanium Grade-2 Material Using ANN.” In Volume 2A: Advanced Manufacturing. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2020-23347
• Sugiyama, Yoshiyuki. 1971. “On the Characteristics of Wing with Tip Clearance: Part 3, the Force Acting on a Rectangular Wing of Low Aspect Ratio.” Bulletin of JSME 14 (76): 1077–87. https://doi.org/10.1299/jsme1958.14.1077
• Sui, Shao Chun, Cheng Li Du, and Li Min Tang. 2013. “Research on Anti-Burnt Method during Machining Complex Titanium Alloy Aircraft Structural Parts.” In Key engineering materials, vol. 589-590. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.589-590.299
• Sullins, Gary, and Frederick Billig. 1987. “Force Accounting for Airframe Integrated Engines.” In 23rd Joint Propulsion Conference. AIAA 1987-1965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1965
• Sullivan, T. L. 1967a. Texture Strengthening and Fracture Toughness of 4Al-0.2 and 5Al-2.5Sn ELI Titanium Sheet Biaxial Stress Fields at Room and Cryogenic Temperatures. NASA. https://ntrs.nasa.gov/citations/19670048713
• Sullivan, T. L. 1967b. Texture Strengthening and Fracture Toughness of 4Al-0.2O and 5Al-2.5Sn ELI Titanium Sheet Biaxial Stress Fields at Room and Cryogenic Temperatures. NASA-TM-X-52272. NASA. https://ntrs.nasa.gov/citations/19670008503
• Sullivan, T. L. 1967c. Uniaxial and Biaxial Fracture Toughness of Extra-Low-Interstitial 5A1-2.5Sn Titanium Alloy Sheet at 20 Deg K. NASA-TN-D-4016. NASA. https://ntrs.nasa.gov/citations/19670018970
• Sullivan, T. L. 1968. Texture Strengthening and Fracture Toughness of Titanium Alloy Sheet at Room and Cryogenic Temperatures. NASA-TN-D-4444. NASA. https://ntrs.nasa.gov/citations/19680013415
• Sullivan, T. L. 1971. Behavior of Ti-5Al-2.5Sn ELI Titanium Alloy Sheet Parent and Weld Metal in the Presence of Cracks at 20 K. NASA-TN-D-6544. NASA. https://ntrs.nasa.gov/citations/19720005262
• Sun, Yuchen. 2023. “Civil Aircraft Brake Energy Scenario Selection and Analysis Method.” Journal of Physics: Conference Series 2551 (1): 012031. https://doi.org/10.1088/1742-6596/2551/1/012031
• 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, Bohua, and Elaine S. Oran. 2018. “New Principle for Aerodynamic Heating.” National Science Review 5 (5): 606–7. https://doi.org/10.1093/nsr/nwy035
• Sun, silu, kaikai Yu, and Jinglei Xu. 2026c. “The Unstart and Restart Dynamic Processes of an Inlet Caused by Instantaneous Velocity Change.” Preprint, . https://doi.org/10.2139/ssrn.6182785
• 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
• Sun Jing, Qiang Gang, Liu Jinsong, et al. 2018. “Simulation Analysis on the Performance of Hydraulic Fuse for Aircraft Brake.” In CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2018.0229
• Sundén, Bengt, and Juan Fu. 2017. “Aerodynamic Heating.” In Heat Transfer in Aerospace Applications. Elsevier. https://doi.org/10.1016/b978-0-12-809760-1.00003-x
• “Superplastic Forming and Diffusion Bonding.” 1983. Aircraft Engineering and Aerospace Technology 55 (9): 22–22. https://doi.org/10.1108/eb035900
• “Superplastic Forming and Diffusion Bonding.” 1997. In Superplasticity in Metals and Ceramics. Cambridge University Press. https://doi.org/10.1017/cbo9780511525230.015
• “Supersonic Aircraft: High-Speed Civil Transports and High-Performance Aircraft.” 1997. In Future Aeronautical and Space Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866449.0173.0210
• “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
• Surber, L. 1975. “Effect of Forebody Shape and Shielding Technique on 2-D Supersonic Inlet Performance.” In 11th Propulsion Conference. AIAA 1975-1183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1183
• Surber, L., and C. Robinson. 1983. “Survey of Inlet Development for Supersonic Aircraft.” In 19th Joint Propulsion Conference. AIAA 1983-1164. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1164
• Surber, L., and D. Sedlock. 1978. “Effects of Airframe-Inlet Integration on Half-Axisymmetric and Two-Dimensional Supersonic Inlet Performance.” In 14th Joint Propulsion Conference. AIAA 1978-960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-960
• Sutton, Fred B. 1959. A Buffet Investigation at High Subsonic Speeds of Wing-Fuselage-Tail Combinations Having Sweptback Wings with NACA Four-Digit Thickness Distributions, Fences, and Body Contouring. NASA-MEMO-3-23-59A. NASA. https://ntrs.nasa.gov/citations/19980230678
• Svorcan, Jelena, Toni Ivanov, Ognjen Peković, and Aleksandar Simonović. 2024. “Computing Aerodynamic Damping in Roll and Pitch of a Supersonic Finner Model.” In 11th International Scientific Conference on Defensive Technologies - OTEX 2024 - zbornik radova. Military Technical Institute, Belgrade. https://doi.org/10.5937/oteh24005s
• Swale, W., and R. Broughton. 2004. “Applying Superplastic Forming Principles to Titanium Sheet Metal Forming Problems.” In Materials science forum, vol. 447-448. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.447-448.239
• 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
• Swavely, C., and J. Soileau. 1972. “Aircraft Aftbody/propulsion System Integration for Low Drag.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1101
• Świa̧toniowski, Andrzej, and Paweł Bałon. 2015. “Compensation of Springback Deformation in Sheet Metal Forming Analysis.” Journal of KONES Powertrain and Transport 19 (3): 459–68. https://doi.org/10.5604/12314005.1138155
• Syberg, J., and J. L. Koncsek. 1975a. Experimental Evaluation of a Mach 3.5 Axisymmetric Inlet. NASA-CR-2563. NASA. https://ntrs.nasa.gov/citations/19750022092
• Syberg, J., and J. Koncsek. 1975b. “Experimental Evaluation of an Analytically Derived Bleed System for a Supersonic Inlet.” In 11th Propulsion Conference. AIAA 1975-1210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1210
• Syberg, J., G. Paynter, and C. Carlin. 1981. “Inlet Design Technology Development: Supersonic Cruise Research.” In 17th Joint Propulsion Conference. AIAA 1981-1598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1598
• 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
• Systems, E-25 General Standards for Aerospace and Propulsion. 1941. ALTITUDE GRAPHS Aircraft Engine Performance. https://doi.org/10.4271/as1
• Systems, E-25 General Standards for Aerospace and Propulsion. 2018. Altitude Graphs Aircraft Reciprocating Engine Performance. https://doi.org/10.4271/as1c
• Szczepanski, C. J., S. K. Jha, J. M. Larsen, and J. W. Jones. 2011. The Role of Microstructure on Various Stages of the Very High Cycle Fatigue Behavior of an a + Beta Titanium Alloy, Ti-6Al-2Sn-4Zr-6Mo (Preprint). Defense Technical Information Center. https://doi.org/10.21236/ada553384
• Szpunar, M., T. Trzepieciński, R. Ostrowski, and M. Zwolak. 2022. “Research on Forming Parameters Optimization of Incremental Sheet Forming Processf or Commercially Pure Titanium Grade 2 Sheets.” Archives of Metallurgy and Materials: 1411–18. https://doi.org/10.24425/amm.2022.141068
• 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
• “T-4 Inlet/engine Compatibility Flight Test Results.” 1989. In 25th Joint Propulsion Conference. AIAA 1989-2466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2466
• Tabanli, Hasan, and Kemal B. Yuceil. 2015. “An Experimental Investigation of the Effect of Boundary Layer on an Internal Compression Inlet.” In 45th AIAA Fluid Dynamics Conference. AIAA 2015-2936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2936
• Tabernaus, Richard, Martin Bugaj, and Michal Hrúz. 2023. “Wing Platforms of Supersonic Aircraft.” In Práce a štúdie. University of Žilina. https://doi.org/10.26552/pas.z.2023.1.03
• Tagashira, Takeshi, Nanahisa Sugiyama, and Masaharu Koh. 2007. “Dynamic Characteristic Tests of Single Spool Turbojet Engine Using Altitude Test Facility.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5012. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5012
• Taherian, Reza. 2026. “Design and Materials of Aircraft Brake Pads: Types, Formulations, and Case Studies.” In Brake Pads. Elsevier. https://doi.org/10.1016/b978-0-443-26645-4.00004-9
• Taillon, Norman V. 1959. Flow Characteristics about Two Thin Wings of Low Aspect Ratio Determined from Surface Pressure Measurements Obtained in Flight at Mach Numbers from 0.73 to 1.90. NASA-MEMO-5-1-59H. NASA. https://ntrs.nasa.gov/citations/19980228214
• Taira, Kunihiko, Clarence Rowley, and Tim Colonius. 2010. “Feedback Control of High-Lift State for a Low-Aspect-Ratio Wing.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-357
• Takahashi, Timothy. 2005. “Integrated Propulsion/Airframe Analysis for Mission Effectiveness Driven Systems Design.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4556
• Takahashi, Timothy. 2012. “Aircraft Concept Design Performance Visualization Using an Energy-Maneuverability Presentation.” In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2012-5704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5704
• Takahashi, Hidemi. 2017. “Conceptual Study of Supersonic Transports Employing Airframe-Integrated Advanced Nozzle Configuration.” Journal of Fluid Science and Technology 12 (3): JFST0026-JFST0026. https://doi.org/10.1299/jfst.2017jfst0026
• Takahashi, Yusuke. 2021. “Fluid-Structure Interaction Analysis of Thin Delta Wing at Transonic Speed.” Proceedings of The Computational Mechanics Conference 2021.34 (0): 163. https://doi.org/10.1299/jsmecmd.2021.34.163
• Takahashi, Timothy T., and Brandon Gaydusek. 2026. “Rethinking the Flying Qualities of the Avro Canada CF-105, the First Stability Augmented Supersonic Fighter.” In AIAA AVIATION 2026 Forum. AIAA 2026-4269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4269
• Takamatsu, Ryosuke, and Wataru Yamazaki. 2021. “Global Topology Optimization of Supersonic Airfoil Using Machine Learning Technologies.” Proceedings of The Computational Mechanics Conference 2021.34 (0): 112. https://doi.org/10.1299/jsmecmd.2021.34.112
• Takasaki, Satoru, Akira Fujimoto, Brett Churchill, and Toru Takasu. 1998. “Inlet Unstart Influence on Aerodynamic Characteristics of Next Generation Supersonic Transport (SST).” In AIAA and SAE, 1998 World Aviation Conference. AIAA 1998-5546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5546
• “Take-off and Landing.” n.d. In Fundamentals of Airplane Flight Mechanics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-46573-7_6
• “Takeoff and Landing.” 1997. In An Introduction to Aircraft Performance. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861529.0151.0170
• “Takeoff and Landing Analysis.” 2010. In Fundamentals of Aircraft and Airship Design. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600867538.0255.0282
• “Takeoff and Landing Performance.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0377.0402
• “Takeoff and Landing Theory and Methods.” 2003. In Flight Testing Of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861840.0177.0197
• Takeoff Performance. 2017. Wiley. https://doi.org/10.1002/9781118534786.ch9
• “Takeoff Performance.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0677.0740
• “Takeoff Performance Testing.” 2021. In Operational Aircraft Performance and Flight Test Practices. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624105920.0741.0812
• Takovitskii, Sergey. 2020. “Axisymmetric Forebodies Having Minimum Drag in Supersonic Flow.” In AIAA Aviation 2020 Forum. AIAA 2020-3120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3120
• Talmage, Donald B., and John P. Reeder. 1947. Data Obtained in the Flight Measurements to Determine the Stability and Control Characteristics of a C-54D Airplane (AAF No. 42-72713) and a Summary of the Test Program. NACA-RM-L7L17a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019271
• Tamayama, Masato. 2017. “Reduced Order Modeling of Aeroelasticity Analysis for a Wing under Static Deformation Effect.” In AIP Conference Proceedings, vol. 1798. Author(s). https://doi.org/10.1063/1.4972751
• 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
• Tamrat, B. 1983. “Flight Path/nose Pointing: A Required Criterion in Future Fighter Aircraft Design.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2123
• Tamrat, B. 1988. “Fighter Aircraft Agility Assessment Concepts and Their Implication on Future Agile Fighter Design.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4400
• Tamura, Shun, and Takaaki Yumitori. 2024. “Accurate Aeroelastic Analysis of the Wing Structure with Control Surface.” In AIAA SCITECH 2024 Forum. AIAA 2024-2446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2446
• Tang, S. 1978. “Analysis of Superplastic Forming of Titanium Sheet into Shallow Hat-Section.” In 19th Structures, Structural Dynamics and Materials Conference. AIAA 1978-496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-496
• Tang, Steve S. 2019. “An Introduction to Inertial-Coupling-Moment-Induced Aircraft Pitch Instability.” In AIAA Aviation 2019 Forum. AIAA 2019-3274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3274
• Tang, Haohui, and Shuanghou Deng. 2024. “Aerodynamic, Kinematic and Control Coupling Simulation of Aircraft Maneuvering Flight.” World Journal of Engineering and Technology 12 (04): 1126–45. https://doi.org/10.4236/wjet.2024.124071
• Tani, Kouichiro. 2003. “Flight Test Vehicles: Japanese View.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2720
• Tani, Junji, Yu-zhou Liu, and Seiji Chonan. 1994. “Flutter Control of a Cantilever Thin Plate Using Piezoelectric Film as Actuators.” In Adaptive Structures and Composite Materials: Analysis and Application. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1994-1570
• Tanner, J. A., and S. M. Stubbs. 1977. Behavior of Aircraft Antiskid Breaking Systems on Dry and Wet Runway Surfaces: A Slip-Ratio-Controlled System with Ground Speed Reference from Unbraked Nose Wheel. NASA-TN-D-8455. NASA. https://ntrs.nasa.gov/citations/19770026206
• Tao, Yang, Zhongliang Zhao, Junqiang Wu, Zhaolin Fan, and Yi Zhang. 2018. “Pitching Effect on Transonic Wing Stall of a Blended Flying Wing with Low Aspect Ratio.” Modern Physics Letters B 32 (12n13): 1840040. https://doi.org/10.1142/s0217984918400407
• 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
• Taşdemir, Vedat. 2022. “Finite Element Analysis of the Springback Behavior after V Bending Process of Sheet Materials Obtained by Differential Speed Rolling (DSR) Method.” Revista de Metalurgia 58 (2): e219. https://doi.org/10.3989/revmetalm.219
• Taşdemir, Vedat, Nuri Şen, and Ömer Seçgin. 2021. “Investigation of the Springback Behavior of Erdemir 7136 Sheet Formed by Rolling Blank Holder Incremental Sheet Forming Method.” Pamukkale University Journal of Engineering Sciences 27 (1): 90–95. https://doi.org/10.5505/pajes.2020.40325
• Tassanbi, Aidana, Junzi Sun, and Jacco Hoekstra. 2026. “Aircraft Mass Estimation Considering Temperature Variations Based on Optimal Control Theory and Statistical Learning.” Preprint, . https://doi.org/10.2139/ssrn.6684161
• Tatum, Kenneth, and Gary Giles. 1987. “Integrating Nonlinear Aerodynamic and Structural Analysis for a Complete Fighter Configuration.” In Aircraft Design, Systems and Operations Meeting. AIAA 1987-2863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2863
• Taylor, Albert E. 1958. Evaluation of Take-Off and Landing Facility. Defense Technical Information Center. https://doi.org/10.21236/ad0428384
• Taylor, Robert T. 1959. An Experimental Investigation to Determine the Effect of Speed-Brake Position on the Longitudinal Stability and Trim of a Swept-Wing Fighter Airplane. NASA-TM-X-188. NASA. https://ntrs.nasa.gov/citations/19980235623
• 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, R. E., T. R. Goerz, and J. V. Beck. 2021. “Automatic Non-Destructive Brake Tester for Thermal Diffusivity/Conductivity of Aircraft Brake Disks.” In Thermal Conductivity 23. CRC Press. https://doi.org/10.1201/9781003210719-5
• Taylor, Gordon, and Ismet Gursul. 2004. “Lift Enhancement over a Flexible Delta Wing.” In 2nd AIAA Flow Control Conference. AIAA 2004-2618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2618
• 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., Jr., and G. Miller Jr. 1982. “An Analytical Technique for the Analysis of Airplane Spin Entry and Recovery.” In 20th Aerospace Sciences Meeting. AIAA 1982-243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-243
• Taylor, L., Jr., and B. Pamadi. 1983. “Estimation of Parameters Involved in High Angle-of-Attack Aerodynamic Theory Using Spin Flight Test Data.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2086
• “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
• “Technological Properties of Titanium Alloys.” 2005. In Titanium Alloys. CRC Press. https://doi.org/10.1201/9781420037678-9
• Tekaslan, Huseyin E., Rumed Imrak, and Melike Nikbay. 2021. “Reliability Based Design Optimization of a Supersonic Engine Inlet.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3541. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3541
• Telionis, Demetri P. 1990. The Transient Development of Vortices over a Delta Wing. Defense Technical Information Center. https://doi.org/10.21236/ada231946
• Temgoua Dongmo, Jean-Etienne, and Harry G. Kwatny. n.d. “Aircraft Loss-of-Control Prevention and Recovery: A Hybrid Control Strategy.” PhD diss., Drexel University. https://doi.org/10.17918/etd-3252
• Teper, G., and R. Stapleford. 1965. “An Assessment of the Lateral-Directional Handling Qualities of a Large Aircraft in Landing Approach.” In Guidance Control Conference. AIAA 1965-1237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1237
• Terashima, Hiroshi, and Kozo Fujii. 2004. “Effects of Number of Stores on the Transonic Flutter Characteristics of a Delta Wing Configuration.” In 34th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2004-2234. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2234
• “Testing Aircraft Wheel, Tyre and Brake Units.” 1973. Measurement and Control 6 (4): 139–40. https://doi.org/10.1177/002029407300600401
• Testing Relevant to Aeroelasticity and Loads. 2014. Wiley. https://doi.org/10.1002/9781118700440.ch25
• Tetervin, Neal. 1963. Approximate Analysis of Effect on Drag of Truncating the Conical Nose of a Body of Revolution in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0400708
• Teti, Roberto, and Alessandra Caggiano. 2018. “Sensor Monitoring of Titanium Alloy Machining.” In Machining of Light Alloys. CRC Press. https://doi.org/10.1201/b22153-6
• 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
• Thawait, Amit K., Parag Tandaiya, and Abhilash J. Chandy. 2022. “Effects of Turbulence Models on Flutter Characteristics of the AGARD 445.6 Wing in Transonic Flow Using Strongly Coupled Two-Way Fluid-Structure Interaction.” In Proceeding of 7th Thermal and Fluids Engineering Conference (TFEC). Begellhouse. https://doi.org/10.1615/tfec2022.aer.040842
• Then, John W., and Kang-rong Chiang. 1970. “Experimental Determination of Moments of Inertia by the Bifilar Pendulum Method.” American Journal of Physics 38 (4): 537–39. https://doi.org/10.1119/1.1976385
• 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
• Thevenot, Françoise, Norbert Frestel, Alain Liot, Hervé Tretout, and René De Mol. 1993. “Scanning Acoustic Microscopy for Quantitative Analysis of Superplastic Forming Diffusion Bonding of Titanium Aerospace Components.” In Ultrasonics International 93. Elsevier. https://doi.org/10.1016/b978-0-7506-1877-9.50015-9
• Thin Wing Sections. 2012. Wiley. https://doi.org/10.1002/9781118346167.ch6
• Thomas, Richard N. 1942. Some Comments on the Form of the Drag Coefficient at Supersonic Velocity. Defense Technical Information Center. https://doi.org/10.21236/ad0494220
• Thomas, T. Y. 1949. “First Approximation of Pressure Distribution on Curved Profiles at Supersonic Speeds.” Proceedings of the National Academy of Sciences 35 (11): 617–27. https://doi.org/10.1073/pnas.35.11.617
• Thomas, Charles E. 1961a. Flight Vibration Survey of F-100C-1 Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0400232
• Thomas, Charles E. 1961b. Flight Vibration Survey of F-101A Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0400231
• Thomas, H. H. B. M. 1973. “On Problems of Flight over an Extended Angle-of-Attack Range.” Aeronautical Journal 77 (752): 412–23. https://doi.org/10.1017/s0001924000049344
• Thomas, Suba, Gaurav Bajpai, Harry Kwatny, and Bor-Chin Chang. 2005. “Nonlinear Dynamics, Stability and Bifurcation in Aircraft: Simulation and Analysis Tools.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6428
• Thompson, S., S. Batill, and R. Nelson. 1990. “Delta Wing Surface Pressures for High Angle of Attack Maneuvers.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2813
• Thomson, William T. 1947. “Rate of Roll of Aeroplanes.” Aircraft Engineering and Aerospace Technology 19 (1): 18–26. https://doi.org/10.1108/eb031458
• Thornton, A. L. 1981. LOVEL: A Low-Velocity Aerodynamic Heating Code for Flat-Plates, Wedges, and Cones. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/6611421
• “Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft.” 1986. In Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865763.0431.0480
• Throckmorton, D. A., and D. R. Stone. 1974. Model Wall and Recovery Temperature Effects on Experimental Heat Transfer Data Analysis. NASA-TM-X-71967. NASA. https://ntrs.nasa.gov/citations/19740017702
• “Thrust-Drag Accounting Methodology.” 1985. In Thrust and Drag: Its Prediction and Verification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865732.0029.0045
• “Thrust-to-Weight Ratio and Wing Loading.” 2024. In Aircraft Design: A Conceptual Approach, Seventh Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624107290.0119.0150
• Tian, Pengzhi, Haiyang Chao, Yu Gu, and Steven G. Hagerott. 2016. “UAV Flight Test Evaluation of Fusion Algorithms for Estimation of Angle of Attack and Sideslip Angle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0645
• Tielking, John T. 1989. Aircraft Tire/Pavement Pressure Distribution. Defense Technical Information Center. https://doi.org/10.21236/ada279100
• Tijdeman, H., J. W. G. van Nunen, A. N. Draan, A. J. Persoon, and R. Poestkoke. 1979a. Transonic Wind Tunnel Tests on an Oscillating Wing with External Store. Part IV. the Wing with Underwing: Store. Defense Technical Information Center. https://doi.org/10.21236/ada077370
• Tijdeman, H., J. W. G. van Nunen, A. N. Kraan, A. J. Persoon, and R. Poestkoke. 1979b. Transonic Wind Tunnel Tests on an Oscillating Wing with External Stores. Part II. the Clean Wing. Defense Technical Information Center. https://doi.org/10.21236/ada071420
• Tilmann, Carl P. 1998. Characterization of the Flowfield near a Wrap-Around Fin at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada359861
• Tinapple, Jon, and Lewis Surber. 2012. “Evaluation of Non-Bleed Shock Wave Boundary Layer Interaction Control Using a New Mixed Compression Inlet Simulator Model.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-271
• Tindell, R. 1980. “Inlet Drag and Stability Considerations for M/0/ = 2.00 Design.” In 16th Joint Propulsion Conference. AIAA 1980-1105. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1105
• Ting, Lu. 1959. “The Pressure Distribution on Dihedral Wings at Supersonic Speed.” Journal of Fluid Mechanics 6 (2): 302–12. https://doi.org/10.1017/s0022112059000635
• Ting, Kuang-Ying, Kenneth Wiersema, Reza Soltani, Chester Nelson, and Eli Livne. 2025. “Supersonic Configurations at Low Speeds (SCALOS) Lateral-Directional Aerodynamics: Configuration Variations and Control Surface Effects.” In AIAA SCITECH 2025 Forum. AIAA 2025-2361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2361
• Tingas, S. A., and D. M. Rao. 1982. Subsonic Balance and Pressure Investigation of a 60 Deg Delta Wing with Leading Edge Devices. NASA-CR-165923. NASA. https://ntrs.nasa.gov/citations/19830011443
• Tinger, Herbert. 1987. “Analysis and Application of Aircraft Departure Prediction Criteria to the AV-8B Harrier II.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2561. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2561
• Tinoco, E., and A. Chen. 1984. “Transonic CFD Applications to Engine/airframe Integration.” In 22nd Aerospace Sciences Meeting. AIAA 1984-381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-381
• 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
• “Titanium Alloys for Aerospace Structures and Engines.” 2012. In Introduction to Aerospace Materials. Elsevier. https://doi.org/10.1533/9780857095152.202
• “Titanium in Aerospace.” 1975. Aircraft Engineering and Aerospace Technology 47 (1): 34–41. https://doi.org/10.1108/eb035218
• Titchener, Neil, Holger Babinsky, and Eric Loth. 2012. “Can Fundamental Shock-Wave/Boundary-Layer Interaction Research Be Relevant to Inlet Aerodynamics?” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-17. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-17
• Tjatra, I. W., R. K. Kapania, and B. Grossman. 1992. “Structural Non-Linearity Effects on Flutter of a Swept Wing in Transonic Flows.” Computing Systems in Engineering 3 (1–4): 131–38. https://doi.org/10.1016/0956-0521(92)90100-w
• 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
• Toenskoetter, H. 1984. “Aspects of Advanced Fighter Engine Design on the Basis of Equal Technology.” In 20th Joint Propulsion Conference. AIAA 1984-1271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1271
• Token, K. H. 1974. Heat Transfer Due to Shock Wave Turbulent Boundary Layer Interactions on High Speed Weapon Systems. Defense Technical Information Center. https://doi.org/10.21236/ada002685
• 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
• Tong, Michael T. 2020. “A Machine-Learning Approach to Assess Aircraft Engine System Performance.” In Volume 1: Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2020-14661
• Tong, Michael T. 2023. “Aero-Engines AI: A Machine-Learning App for Aircraft Engine Concepts Assessment.” In Volume 1: Aircraft Engine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2023-102024
• Torii, Hiroshi, and Yumi Matsuzaki. 1991. “Response Characteristics of a Wing in Supersonic Flow near Flutter Boundary.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/911999
• Torii, Hiroshi, and Yuji Matsuzaki. 1992. “Subcritical Flutter Characteristics of a Swept-Back Wing in a Turbulent Supersonic Flow: Comparison between Analysis and Experiment.” In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2393
• Torres, George Lucas S., Ashok Gopalarathnam, and Flavio D. Marques. 2025. “A Uniformly Convergent Series Expansion for the Bound Vorticity Distribution in the Unsteady Thin Airfoil Theory.” In AIAA SCITECH 2025 Forum. AIAA 2025-1886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1886
• Torres, George Lucas S., and Flavio D. Marques. 2025. “Resolving the Leading-Edge Singularity in the Thin Airfoil Theory for General Airfoil Shapes via Nonlinear Geometric Decomposition.” In AIAA SCITECH 2025 Forum. AIAA 2025-0027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0027
• Torrigiani, Francesco, and Marco Berci. 2021. “Multifidelity Parametric Aeroelastic Stability Analyses of Goland’s Wing.” In AIAA Scitech 2021 Forum. AIAA 2021-1911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1911
• “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 Computational Experience for Advanced Tactical Aircraft.” 1982. In Transonic Aerodynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865558.0451.0465
• Trapier, S., S. Deck, and P. Duveau. n.d. “Delayed Detached-Eddy Simulation of Supersonic Inlet Buzz.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-77815-8_25
• Trapier, Simon, Sébastien Deck, Philippe Duveau, and Philippe Guillen. 2007a. “Delayed Detached-Eddy Simulation of Supersonic Inlet Buzz.” In 37th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2007-4353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4353
• 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
• Travis, Matt H. 2005. “Predicting Landing Gear Carbon Brake Vibration and Performance via Subscale Test and Analysis.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2005-01-3437
• Trefny, Charles J. 2020. “CFD Simulation of an Inward-Turning Supersonic Inlet Unstart at Flight Mach Number 1.7.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3771
• Trefny, Charles J., Stefanie M. Hirt, Bernhard H. Anderson, Lawrence E. Fink, and Todd E. Magee. 2014. “Performance of a Supersonic over-Wing Inlet with Application to a Low-Sonic-Boom Aircraft.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/20140011175
• Trefny, C. J., and J. W. Wasserbauer. 1986. Low-Speed Performance of an Axisymmetric, Mixed-Compression, Supersonic Inlet with Auxiliary Inlets. NASA-TP-2557. NASA. https://ntrs.nasa.gov/citations/19860015223
• Triplett, W. 1979. “Aeroelastic Tailoring Studies in Fighter Aircraft Design.” In 20th Structures, Structural Dynamics, and Materials Conference. AIAA 1979-725. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-725
• Triplett, W., H.-P. Kappus, and R. Landy. 1973. “Active Flutter Control: An Adaptable Application to Wing/store Flutter.” In 11th Aerospace Sciences Meeting. AIAA 1973-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-194
• Tritschler, John K., and Brandon Dotson. 2022. “Energy-Maneuverability as a Framework for Performance and Handling Qualities Testing.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0078-2022-1300
• Trobaugh, Lynn A., David G. Lee, and Michael J. Harris. 1980. Low Speed Aerodynamic Characteristics of Wings of Aspect Ratios 3 and 4 Equipped with High Lift Systems. Defense Technical Information Center. https://doi.org/10.21236/ada087768
• Trobaugh, L., and F. Obrimski. 1980. “Consistent Takeoff and Landing Criteria for Naval Aircraft of Various Basing Concepts.” In Aircraft Systems Meeting. AIAA 1980-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1813
• Tromp, Jeffrey. 1998. “Flowfield Simulation about a 65-Degree Delta Wing during Constant Roll-Rate Motions.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4453. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4453
• Trussa, Colin W., Clifford A. Whitfield, Lian Duan, and Jacob A. Brandon. 2022. “Aerodynamic Characteristics of a Flat Plate Delta Wing with Deflected Wing Tips.” In AIAA AVIATION 2022 Forum. AIAA 2022-3297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3297
• Tsay, Tain-Sou. 2022. “Linear Quadratic Regulation Method for a Roll Yaw Coupled Supersonic Flight Vehicle.” International Journal of Applied Mathematics Computational Science and Systems Engineering 4: 39–43. https://doi.org/10.37394/232026.2022.4.5
• Tsuyama, Seishi, Shinji Mitao, and Kuni-nori Minakawa. 1992. “Alloy Modification of γ-Base Titanium Aluminide for Improved Oxidation Resistance, Creep Strength and Fracture Toughness.” In High Temperature Aluminides and Intermetallics. Elsevier. https://doi.org/10.1016/b978-1-85166-822-9.50073-x
• Tsuzuku, Takayuki. 1999. “Superplastic Forming of Aerospace Metallic Materials.” In Materials science forum, vol. 304-306. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.304-306.831
• Tu, Eugene. 1992. “Effect of Canard Position on the Longitudinal Aerodynamic Characteristics of a Close-Coupled Canard-Wing-Body Configuration.” In Astrodynamics Conference. AIAA 1992-4632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4632
• Tu, Lianghui, Chao Yan, Xingyu Liu, Yuhao Wang, and Yang Yang. 2024. “Prediction of Aircraft Departure/Spin Characteristics by Improving Kalviste Decomposing and Weak Nonlinear Analysis Method.” International Journal of Aeronautical and Space Sciences 25 (4): 1232–42. https://doi.org/10.1007/s42405-024-00735-3
• Tucker, Warren A. 1948a. Characteristics of Thin Triangular Wings with Constant-Chord Full-Span Control Surfaces at Supersonic Speeds. NACA-TN-1601. NASA. https://ntrs.nasa.gov/citations/19930082249
• Tucker, Warren A. 1948b. Characteristics of Thin Triangular Wings with Triangular-Tip Control Surfaces at Supersonic Speeds with Mach Lines behind the Leading Edge. NACA-TN-1600. NASA. https://ntrs.nasa.gov/citations/19930082247
• Tucker, Maurice, and Stephen H. Maslen. 1951. Turbulent Boundary-Layer Temperature Recovery Factors in Two-Dimensional Supersonic Flow. NACA-TN-2296. NASA. https://ntrs.nasa.gov/citations/19930082955
• Tucker, Warren A., and Robert L. Nelson. 1948a. The Flexible Rectangular Wing in Roll at Supersonic Flight Speeds. NACA-TN-1769. NASA. https://ntrs.nasa.gov/citations/19930082442
• Tucker, Warren A., and Robert L. Nelson. 1948b. Theoretical Characteristics in Supersonic Flow of Constant-Chord Partial-Span Control Surfaces on Rectangular Wings Having Finite Thickness. NACA-TN-1708. NASA. https://ntrs.nasa.gov/citations/19930082397
• Tucker, Warren A., and Robert L. Nelson. 1949. Theoretical Characteristics in Supersonic Flow of Two Types of Control Surfaces on Triangular Wings. NACA-TR-939. NASA. https://ntrs.nasa.gov/citations/19930092004
• Tucker, Warren A., and Robert O. Piland. 1950. Estimation of the Damping in Roll of Supersonic-Leading-Edge Wing-Body Combinations. NACA-TN-2151. NASA. https://ntrs.nasa.gov/citations/19930082769
• Tucker, Aaron A., William S. Saric, and Helen L. Reed. 2014. “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
• Tudosie, Alexandru Nicolae. 2017a. “Control Laws for an Aircraft Supersonic Inlet with Mobile Panel.” Scientific Research and Education in the AIR Force 19 (1): 231–42. https://doi.org/10.19062/2247-3173.2017.19.1.26
• Tudosie, Alexandru-Nicolae. 2017b. “Pneumo-Hydro-Mechanical Control System for an Aircraft Supersonic Inlet with Mobile Ramp.” Review of the Air Force Academy 15 (1): 123–30. https://doi.org/10.19062/1842-9238.2017.15.1.16
• Tudosie, Alexandru Nicolae. 2018. “Axisymmetric Frontal Supersonic Inlet for Trisonic Aircraft.” Scientific Research and Education in the AIR Force 20: 243–52. https://doi.org/10.19062/2247-3173.2018.20.33
• Tudosie, Alexandru Nicolae, and Mádálina Luciana PĂUnescu. 2017. “Automatic Control System for an Aircraft Plan Supersonic Inlet with Mobile Panel.” Scientific Research and Education in the AIR Force 19 (1): 243–52. https://doi.org/10.19062/2247-3173.2017.19.1.27
• Tudosie, Alexandru-Nicolae, and Vasile Prisacariu. 2022. “Supersonic Air Inlet for a High Velocity Propulsion System.” In Scientific Research and Education in the AIR Force. Publishing House of “Henri Coanda” Air Force Academy. https://doi.org/10.19062/2247-3173.2021.22.19
• Tuling, Sean, Laurent Dala, and Christine Toomer. 2013. “An Engineering Method for Very Low Aspect Ratio Cruciform Wing-Body Configurations.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2823
• Turan Abi, Tuğçe, and Ahmet Yılmaz. 2019. “Springback Compansation with Using Two Different Radius in Bending u Form Shape Sheet Metal Parts.” In Proceedings of the 4th International Conference on Modern Approaches in Science, Technology & Engineering. Acavent. https://doi.org/10.33422/4ste.2019.02.17
• “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
• “Turbojet Engines.” 2022. In Introduction to Aerospace Flight Vehicles. Embry-Riddle Aeronautical University. https://doi.org/10.15394/eaglepub.2022.1066.n32
• Türkkahraman, Zeliha, Muhammed Enes Özcan, and Buğrahan Alabaş. 2024. “Optimization of Plenum for Control of Boundary Layer-Shock Interaction in Supersonic Inlet.” Politeknik Dergisi 27 (4): 1269–79. https://doi.org/10.2339/politeknik.1247300
• Turnbull, W. J., W. K. Boyd, C. R. Foster, J. M. Griffith, and O. B. Ray. 1952. Design of Flexible Airfield Pavements for Multiple-Wheel Landing Gear Assemblies. Report Number 1. Test Section with Lean Clay Subgrade. Defense Technical Information Center. https://doi.org/10.21236/ada319272
• Turner, William N. 1944. Flight Measurements of Horizontal Tail Loads on a Typical Propeller-Driven Pursuit Airplane during Stalled Pull-Outs at High Speed. NACA-WR-A-81. NASA. https://ntrs.nasa.gov/citations/19930092857
• Turner, Howard L. 1947a. Buffeting of External Fuel Tanks at High Speeds on a Gruman F7F-3 Airplane. NACA-RM-SA7A07. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026362
• Turner, Howard L. 1947b. Buffeting of External Fuel Tanks at High Speeds on a Grumman F7F-3 Airplane. NACA-RM-A7A07. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20030063241
• Turner, Howard L. 1950. Measurement of the Moments of Inertia of an Airplane by a Simplified Method. NACA-TN-2201. NASA. https://ntrs.nasa.gov/citations/19930082849
• Turner, C. 1981. “A Study of the Effect of Store Aerodynamics of Wing/store Flutter.” In Dynamics Specialists Conference. AIAA 1981-604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-604
• 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. 1948. Measurements in Flight of the Longitudinal-Stability Characteristics of a Republic YF-84A Airplane (Army Serial No. 45-59488) at High Subsonic Mach Numbers. NACA-RM-SA8K03. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019276
• Turner, M. J., and D. L. Grande. 1978. Study of Advanced Composite Structural Design Concepts for an Arrow Wing Supersonic Cruise Configuration. NASA-CR-2825. NASA. https://ntrs.nasa.gov/citations/19780012173
• Turner, Howard L., and George A. Rathert Jr. 1945. Pressure Lag in Tubing Used in Flight Research. NACA-RB-5F15. NASA. https://ntrs.nasa.gov/citations/19930090910
• “Turning Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0293.0312
• 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
• “Two-Dimensional, Supersonic Flows around Thin Airfoils.” 2021. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009105842.011
• “Two-Dimensional, Supersonic Flows around Thin Airfoils.” 2025. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009501293.011
• Ueno, Makoto, Takashi Matsuno, and Yoshiaki Nakamura. 1998. “Unsteady Aerodynamics of Rolling Thick Delta Wing with High Aspect Ratio.” In 16th AIAA Applied Aerodynamics Conference. AIAA 1998-2520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2520
• 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
• Ulbrich, Norbert. 2004. “Trapezoidal Approximation of a Complex Wing Planform for Wall Interference Calculations.” In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2004-2307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2307
• 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
• Unangst, John R. 1959. Transonic Flutter Characteristics of an Aspect-Ratio-4, 45 Deg. Sweptback, Taper-Ratio-0.2 Plan Form. NASA-TM-X-136. NASA. https://ntrs.nasa.gov/citations/19980236841
• “Unorthodox Landing Gears.” 1988. In Aircraft Landing Gear Design: Principles and Practices. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861468.0305.0321
• “Unsteady Surface Pressure Measurements on a Pitching Airfoil.” 1985. In Shear Flow Control Conference. AIAA 1985-532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-532
• 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, and Timothy Smith. 2011. “Use of Propulsion Commands to Prevent Loss-of-Control Aircraft Accidents.” In Infotech@Aerospace 2011. AIAA 2011-1567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1567
• Useller, James W., and William E. Mallett. 1954. Preliminary Altitude Performance Data of J71-A2 Turbojet Engine Afterburner. NACA-RM-SE54J06. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090021752
• Useller, James W., and Robert E. Russey. 1955. Altitude Performance of Modified J71 Afterburner with Revised Engine Operating Conditions. NACA-RM-SE55D12. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090026462
• Usha, G., P. Narayana Rao, N. Shanta Kumar, G. Girija, and M. T. Abilash. 2023. “Aircraft Fuel Mass Estimation Using Global Nonlinear Parametric Modeling.” Journal of Aerospace Sciences and Technologies: 342–48. https://doi.org/10.61653/joast.v65i4.2013.874
• Uslu, Emin, Gul Tosun, and Nihat Tosun. 2016. “Investigation of Springback Behavior of DP Series Sheet Metal in Bending Process.” In Fourth International Conference on Advances in Mechanical and Automation Engineering - MAE 2016. Institute of Research Engineers and Doctors. https://doi.org/10.15224/978-1-63248-102-3-44
• 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
• Vachon, Michael Jacob, and Ronald J. Ray. 2004. “Calculated Drag of an Aerial Refueling Assembly through Airplane Performance Analysis.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20040013408
• Vadyak, Joseph, Marilyn Smith, and David Schuster. 1987. “Navier-Stokes Simulations of Supersonic Fighter Intake Flowfields.” In 23rd Joint Propulsion Conference. AIAA 1987-1752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1752
• Vaidyaraman, Sundar, Mark Purdy, Terence Walker, and Susan Horst. 2001. C/SiC Material Evaluation for Aircraft Brake Applications. Wiley. https://doi.org/10.1002/3527605622.ch122
• Vail, Edwin G., and Richard G. Willis. 1958. Pilot Protection for the X-15 Aircraft. NASA. https://ntrs.nasa.gov/citations/19930092391
• Valasek, John, Joshua Harris, Shawn Pruchnicki, Matthew McCrink, James W. Gregory, and David Sizoo. 2017. “Characterization of Derived Angle-of-Attack and Sideslip Angle Algorithms Using Monte Carlo and Piloted Simulation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4059
• Valasek, John, and Lawrence Walchli. 1998. “High Speed, Low Angle-of-Attack Pneumatic Vortex Control.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4449
• Valenti, Luca, and Samuel Stanton. 2024. “Dynamics of an Aircraft with Varying Mass and Inertial Properties.” In 2024 Regional Student Conferences. AIAA 2024-85365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-85365
• Valjavec, Marko, and David E. Hardt. 1999. “Closed-Loop Shape Control of the Stretch Forming Process over a Reconfigurable Tool: Precision Airframe Skin Fabrication.” In Manufacturing Science and Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1999-0756
• 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 Dam, C., and B. Holmes. 1986. “Boundary-Layer Transition Effects on Airplane Stability and Control.” In Astrodynamics Conference. AIAA 1986-2229. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2229
• van Dommelen, Dennis, Adam D’Silva, and Willem A. Anemaat. 2019. “Comparison of Methods to Predict Aerodynamic Center Shift Due to Bodies.” In AIAA Aviation 2019 Forum. AIAA 2019-3569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3569
• Van Dyke, Rudolph D., Jr., Walter E. McNeill, and Fred J. Drinkwater III. 1953. A Flight Study of the Effects on Tracking Performance of Changes in the Lateral-Oscillatory Characteristics of a Fighter Airplane. NACA-RM-A53H10. NASA. https://ntrs.nasa.gov/citations/19930087832
• Van Orden, J. M., and L. L. Soffa. 1968. Effect of Beta Working on 6A1-4V Titanium Alloy. Defense Technical Information Center. https://doi.org/10.21236/ada382375
• 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
• Vanino, R., and S. Rohlfs. 1976. “Supercritical Wing Design for a Fighter Type Experimental Aircraft.” In Symposium Transsonicum II. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_31
• Vannelli, R. J. 1955. “Turbojet Engine Test Cell Design and Correlation.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/550022
• Vargo, D. J., and M. I. Weinstein. 1957. Investigation of an Underslung Normal-Wedge Inlet at Free-Stream Mach Numbers from 1.50 to 1.99. NACA-RM-E56F27. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19650013683
• Vartanov, Gregory. 2020. “Cost-Effective Alternative to Titanium for Aircraft Parts.” AM&P Technical Articles 178 (3): 22–25. https://doi.org/10.31399/asm.amp.2020-03.p022
• Varunkumar, K. S., and Nikhil N. Gangamkote. 2023. “CFD-Based Comparison of Flutter Effect in Supersonic Wing Designs at Steady Aerodynamic Condition.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3200268/v1
• Varwig, R. L. 1963. A Shock Tube for Producing Subsonic, Transonic, and Supersonic Flows for Aerodynamic Testing. Defense Technical Information Center. https://doi.org/10.21236/ad0403045
• Vasil’chenko, V. I. 1981. “Decrease in the Wave Resistance of the Combination of a Body of Revolution with a Wing in a Supersonic Gas Stream.” Fluid Dynamics 16 (3): 464–67. https://doi.org/10.1007/bf01092388
• Vasu, George, Glennon V. Schwent, and James R. Ketchum. 1951. Preliminary Transient Performance Data for Afterburner Operation of Westinghouse Electronic Power Regulator on XJ34-WE-32 Turbojet Engine in Altitude Wind Tunnel. NACA-RM-SE50L29. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090022362
• Vatsa, V., J. Thomas, and B. Wedan. 1987. “Navier-Stokes Computations of Prolate Spheroids at Angle of Attack.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2627
• Vaughan, R. W., and R. J. Jones. 1971. The Development of Autoclave Processable, Thermally Stable Adhesives for Titanium Alloy and Graphite Composite Structures. NASA-CR-112003. NASA. https://ntrs.nasa.gov/citations/19720005843
• Vaughn, M., Jr. 1982. “Pressure Distribution on an Ogee Wing in Supersonic Flow.” In 20th Aerospace Sciences Meeting. AIAA 1982-414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-414
• Vedeneev, V. V. 2005. “Flutter of a Wide Strip Plate in a Supersonic Gas Flow.” Fluid Dynamics 40 (5): 805–17. https://doi.org/10.1007/s10697-005-0118-0
• Vedeneev, V. V. 2009. “Numerical Investigation of Supersonic Plate Flutter Using the Exact Aerodynamic Theory.” Fluid Dynamics 44 (2): 314–21. https://doi.org/10.1134/s001546280902015x
• Vedeneev, Vasily. 2013. “Interaction of Panel Flutter with Inviscid Boundary Layer Instability in Supersonic Flow.” Journal of Fluid Mechanics 736: 216–49. https://doi.org/10.1017/jfm.2013.522
• Vedeneev, V. V., S. V. Guvernyuk, A. F. Zubkov, and M. E. Kolotnikov. 2009. “Experimental Observation of Single-Mode Panel Flutter in a Supersonic Gas Flow.” Doklady Physics 54 (8): 389–91. https://doi.org/10.1134/s1028335809080102
• Vedeneev, V. V., S. V. Guvernyuk, A. F. Zubkov, and M. E. Kolotnikov. 2010a. “Experimental Investigation of Single-Mode Panel Flutter in Supersonic Gas Flow.” Fluid Dynamics 45 (2): 312–24. https://doi.org/10.1134/s001546281002016x
• Velden, A. 1997. “Supersonic Aircraft Shape Optimization.” In New Design Concepts for High Speed Air Transport. Springer Vienna. https://doi.org/10.1007/978-3-7091-2658-5_16
• Veley, Duane E., Narendra S. Khot, Jeffrey V. Zweber, and Alicia R. Hartong. 2008. Optimum Design of a Flexible Wing Structure to Enhance Roll Maneuver in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ada478915
• Vepa, Ranjan. 2023a. “Aircraft Non-Linear Dynamics.” In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/9781003266310-4
• Vepa, Ranjan. 2023b. “Flight Dynamics of Elastic Aircraft.” In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/9781003266310-10
• Vepa, Ranjan. 2023c. “Longitudinal and Lateral Linear Stability and Control.” In Flight Dynamics, Simulation, and Control. CRC Press. https://doi.org/10.1201/9781003266310-6
• 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
• Verhoff, August. 1987. “CFD Validation Experiments at McDonnell Aircraft Company.” In NASA. Ames Research Center, NASA CFD Validation Workshop. https://ntrs.nasa.gov/citations/19920075820
• 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
• Vermeersch, Olivier, Kenji Yoshida, Yoshine Ueda, and Daniel Arnal. 2015. “Natural Laminar Flow Wing for Supersonic Conditions: Wind Tunnel Experiments, Flight Test and Stability Computations.” Progress in Aerospace Sciences 79: 64–91. https://doi.org/10.1016/j.paerosci.2015.07.003
• “Versatile ATI 425 Titanium Alloy.” 2004. Aircraft Engineering and Aerospace Technology 76 (1): aeat.2004.12776aad.005. https://doi.org/10.1108/aeat.2004.12776aad.005
• Vershinin, Y. A. 2004. “A Method of Separation of an Aircraft Motion on a Roll and Sideslip.” Aircraft Engineering and Aerospace Technology 76 (2): 179–84. https://doi.org/10.1108/00022660410526042
• Vescelus, G. E. 1952. “Discussion: “Friction Surfaces for Spin-Up Simulation in Landing-Gear Drop Tests” (Drake, D. W., 1952, Trans. ASME, 74, Pp. 1269–1279).” Journal of Fluids Engineering 74 (7): 1281–1281. https://doi.org/10.1115/1.4016096
• Vey, Stefan, David Greenblatt, Christian Nayeri, and Christian Paschereit. 2010. “Leading Edge and Wing Tip Flow Control on Low Aspect Ratio Wings.” In 40th Fluid Dynamics Conference and Exhibit. AIAA 2010-4865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4865
• Vey, Stefan, Christian Nayeri, Christian Paschereit, and David Greenblatt. 2012. “On the Frequency Scaling of the Forced Flow above a Low Aspect Ratio Wing.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-317. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-317
• Viana, Felipe A. C., Valder Steffen, Marcelo A. X. Zanini, Sandro A. Magalhães, and Luiz C. S. Góes. 2007. “Identification of a Non-Linear Landing Gear Model Using Nature-Inspired Optimization.” Shock and Vibration 15 (3–4): 257–72. https://doi.org/10.1155/2008/246271
• Vigdortchik, S. A., and A. N. Tupolev. 1982. “The Technological Aspects of Titanium Application in the TU-144 Aircraft Structure.” In Titanium and Titanium Alloys. Springer US. https://doi.org/10.1007/978-1-4757-1758-7_53
• 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
• Vincent, J., N. Gupta, and W. Hall Jr. 1979. “Recent Results in Parameter Identification for High Angle-of-Attack Stall Regimes.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1640. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1640
• Vindigni, C. R. 2023. “Time Domain Aeroelastic Analysis of Wing Structures by Means of an Alternative Aeroelastic Beam Approach.” In Materials Research Proceedings, vol. 33. Materials Research Forum LLC. https://doi.org/10.21741/9781644902677-31
• 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
• Vinogradov, Vyacheslav Afanasievich, A. Yu. Makarov, N. A. Melkonyan, and Vladimir Alekseevich Stepanov. 2017b. “Experimental Investigation of a 3D Fixed-Geometry Inlet for a Supersonic Business Aircraft.” TsAGI Science Journal 48 (3): 261–76. https://doi.org/10.1615/tsagiscij.2017022808
• Vinogradov, Vyacheslav Afanasievich, Yakov Aleksandrovich Melnikov, and Vladimir Alekseevich Stepanov. 2017a. “Choice and Design of a 3D Fixed-Geometry Inlet for a Small Supersonic Business Aircraft.” TsAGI Science Journal 48 (2): 141–58. https://doi.org/10.1615/tsagiscij.2017021109
• Vinogradov, Yu. I., and G. B. Menkov. 2020. “Study of Stress-Strain State of an Aircraft Body at Steering Loads.” Mechanics of Solids 55 (3): 423–36. https://doi.org/10.3103/s0025654420030164
• Vinogradov, Viacheslav, and Vladimir Stepanov. 2008. “Scheme and Inlet Performance of Supersonic Business Aircraft.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-4585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4585
• Vinogradov, V., V. Stepanov, and E. Aleksandrovich. 1989. “Numerical and Experimental Investigation of Airframe-Integrated Inlet for High Velocities.” In 25th Joint Propulsion Conference. AIAA 1989-2679. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2679
• Visbal, Miguel. 2011. “Three-Dimensional Flow Structure on a Heaving Low-Aspect-Ratio Wing.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-219. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-219
• Visbal, Miguel R. 2017. “Unsteady Flow Structure and Loading of a Pitching Low-Aspect-Ratio Wing.” Physical Review Fluids 2 (2): 024703. https://doi.org/10.1103/physrevfluids.2.024703
• Visbal, Miguel R., and Daniel J. Garmann. 2012. “Flow Structure above Stationary and Oscillating Low-Aspect-Ratio Wing.” In Volume 1: Symposia, Parts A and B. American Society of Mechanical Engineers. https://doi.org/10.1115/fedsm2012-72405
• Viswanathan, Vikram, Brad Kinsey, and Jian Cao. 2003. “Experimental Implementation of Neural Network Springback Control for Sheet Metal Forming.” Journal of Engineering Materials and Technology 125 (2): 141–47. https://doi.org/10.1115/1.1555652
• Vladimirov, Ivaylo N., and Stefanie Reese. 2007. “A Finite Strain Isotropic/kinematic Hardening Model for Springback Simulation of Sheet Metals.” In AIP Conference Proceedings, vol. 907. AIP. https://doi.org/10.1063/1.2729501
• Voevodenko, N. V., and I. M. Panteleev. 1989. “Combined Method of Calculating Supersonic Ideal-Gas Flow over a Wing with a Supersonic Blunt Leading Edge.” Fluid Dynamics 24 (1): 133–38. https://doi.org/10.1007/bf01051491
• Vogel, J. M. 1973. “Numerical Calculation of Flow Fields about Rectangular Wings of Finite Thickness in Supersonic Flow.” PhD diss., Iowa State Univ. of Science and Technology. https://ntrs.nasa.gov/citations/19730009542
• Vohra, Yaman. 2024. “Optimization of Supersonic Multi-Row Disk Inlet Devices: Analyzing Shock Structures and Performance with Various Semi-Cone Angles and Microcavity Integration.” In 2024 Regional Student Conferences. AIAA 2024-90590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-90590
• Volobuyev, Valerii Semyonovich, Anton Roaldovich Gorbushin, Iraida Alekseevna Sudakova, and V. I. Tikhomirov. 2017. “Two Methods for Calibration of Strain-Gauge Balances Using Tsagi Balance Calibration Machines.” TsAGI Science Journal 48 (2): 187–97. https://doi.org/10.1615/tsagiscij.2017021104
• 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. 2007. Flight Test of the F/A-18 Active Aeroelastic Wing Airplane. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20070024435
• “Vortical Flow Topology on Windward and Leeward Side of Delta Wing at Supersonic Speed.” 2009. Journal of Applied Fluid Mechanics 2 (02). https://doi.org/10.36884/jafm.2.02.11860
• Voytovych, Dmytro, and Charles Merkle. 2010. “Simulation of Coupled Supersonic Inlet and a Fan.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-7115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7115
• Vrebalovich, T. 1967. Heat Loss and Recovery Temperature of Fine Wires in Transonic Transition Flow. NASA. https://ntrs.nasa.gov/citations/19670049448
• Vyalkov, A. V. 2020. “Attitude Angles Determination by Vectors Observations in Airplane Free Spin Investigation.” Gyroscopy and Navigation 11 (4): 300–309. https://doi.org/10.1134/s2075108720040112
• Wadley, Jason, Dallas Hopper, and James Buffington. 2005. “Integrated Failure Accommodation and Upset Recovery.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-5934. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5934
• Wages, N. 1971. “In-Flight Flow Research on a Fighter Type Aircraft.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-762
• Wagner, Justin, Agustin Valdivia, Kemal Yuceil, Noel Clemens, and David Dolling. 2007. “An Experimental Investigation of Supersonic Inlet Unstart.” In 37th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2007-4352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4352
• Wagner, Justin, Kemal Yuceil, and Noel Clemens. 2009b. “PIV Measurements of Unstart of an Inlet-Isolator Model in a Mach 5 Flow.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-4209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-4209
• Wagner, Justin, Kemal Yuceil, Agustin Valdivia, Noel Clemens, and David Dolling. 2008. “PIV Measurements of the Unstart Process in a Supersonic Inlet/Isolator.” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-3849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-3849
• Wagoner, Robert H. 2004. Sheet Springback. Wiley. https://doi.org/10.1002/3527603786.ch42
• Walczyk, Daniel F., Vinay Raju, and Ron Miller. 1998. “A Simplified Method for Fixturing Aircraft Sheet Metal Parts during Post-Forming Operations.” In Manufacturing Science and Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1998-1107
• 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, Harold J., and Mary B. Ballantyne. 1950. Pressure Distribution and Damping in Steady Roll at Supersonic Mach Numbers of Flat Swept-Back Wing with Subsonic Edges. NACA-TN-2047. NASA. https://ntrs.nasa.gov/citations/19930082702
• Walker, Harold J., and Robert E. Berggren. 1948. Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 II: Maximum Thickness at Midchord. NACA-RM-A8I20. NASA. https://ntrs.nasa.gov/citations/19930090356
• Walker, Curtis L., Willis M. Braithwaite, and Joseph N. Sivo. 1953. Altitude Evaluation of Several Afterburner Design Variables on a J47-GE-17 Turbojet Engine. NACA-RM-E53F10. NASA. https://ntrs.nasa.gov/citations/19930087752
• 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
• Wallace, Richard E. 1952. Wind-Tunnel Tests of the ONR Swept-Wing Research Model. Defense Technical Information Center. https://doi.org/10.21236/ad0043099
• Wallner, Lewis E., and Emmert T. Jansen. 1951. Full-Scale Investigation of Cooling Shroud and Ejector Nozzle for a Turbojet Engine: Afterburner Installation. NACA-RM-E51J04. NASA. https://ntrs.nasa.gov/citations/19930086959
• 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
• Walter, Sibylle F., and Ryan P. Starkey. 2016. “Interpolation Methods for Inlet Distortion Determination.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0531
• Walters, John Justin, and David W. Netzer. 1978. A Validation of Mathematical Models for Turbojet Test Cells. Defense Technical Information Center. https://doi.org/10.21236/ada055991
• Wan-Nawang, Wan-Adlan, Yi Qin, and Xiaoyu Liu. 2015. “An Experimental Study on the Springback in Bending of w-Shaped Micro Sheet-Metal Parts.” MATEC Web of Conferences 21: 09015. https://doi.org/10.1051/matecconf/20152109015
• Wang, Jinyan. 2005a. “Finite Element Models in Springback Numerical Simulation of Sheet Metal Forming and the Incompatible Modes.” Journal of Mechanical Engineering 41 (10): 6. https://doi.org/10.3901/jme.2005.10.006
• Wang, J. 2005b. “Modeling and Simulation of Induced Anisotropic Hardening and Springback in Sheet Metals during Non-Proportional Loading.” In AIP Conference Proceedings, vol. 778. AIP. https://doi.org/10.1063/1.2011224
• Wang, D. 2011. “Algebraic Analysis of Stability and Bifurcation for Nonlinear Flight Dynamics.” Aeronautical Journal 115 (1168): 345–49. https://doi.org/10.1017/s0001924000005868
• 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, Y. 2022. “Analysis of Emergency Landing Load of Civil Aircraft with Single Main Landing Gear Extended Landing.” IET Conference Proceedings 2022 (7): 336–39. https://doi.org/10.1049/icp.2022.1550
• Wang, Lei. 2024. “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, Xingang, and Hongjun Cao. 2026. “Dynamics of the Aircraft Nose Landing Gear with Two Time Delays.” Journal of Applied Nonlinear Dynamics 16 (1): 187–210. https://doi.org/10.5890/jand.2027.03.010
• Wang, Gang, Jun Chen, and X. Y. Ruan. 2005b. “A Study on Gas Pressure for Superplastic Forming of Titanium Alloy Bellows.” In Materials science forum. Trans Tech Publications. https://doi.org/10.4028/0-87849-960-1.3051
• Wang, Rongtao, Wei Cheng, Yujing Sun, Hailong Ge, Wenqiu Xu, and Jun Wang. 2020a. “The Effect of Ultrasonic Vibration on the Springback of Incremental Sheet Forming.” Journal of Physics: Conference Series 1678 (1): 012042. https://doi.org/10.1088/1742-6596/1678/1/012042
• Wang, Hengyu, Zheng Fang, Weiliang Zhao, and Yunjun Rui. 2020c. “A Modified Trifilar Pendulum for Simultaneously Determining the Moment of Inertia and the Mass of an Irregular Object.” European Journal of Physics 42 (1): 015002. https://doi.org/10.1088/1361-6404/abb348
• Wang, Xiting, Ai He, Zhongzhi Hu, and Jincen Jiang. 2024a. “An Adaptive Modeling Method of Hydrogen-Fueled Turbojet Engine.” In AIAA SCITECH 2024 Forum. AIAA 2024-0521. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0521
• Wang, Fusheng, Shihui Huo, Zhufeng Yue, and Wei Qian. 2011b. “Further Study on Aeroelastic Response of Aircraft Wing with Freeplay.” Journal of Vibration and Control 18 (11): 1690–97. https://doi.org/10.1177/1077546311424306
• Wang, Chuan-Tao, Gary L. Kinzel, and Taylan Altan. 1993. “Process Simulation and Springback Control in Plane Strain Sheet Bending.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/930280
• Wang, Zijin, Zhenshui Li, and Wei Li. 2017c. “Research of Aircraft Electric Brake Control System.” DEStech Transactions on Engineering and Technology Research, no. ismii. https://doi.org/10.12783/dtetr/ismii2017/16669
• Wang, Zijin, Zhenshui Li, and Wei Li. 2018. “Research on Brake System of Civil Aircraft.” IOP Conference Series: Materials Science and Engineering 392 (6): 062158. https://doi.org/10.1088/1757-899x/392/6/062158
• Wang, Shiyun, Lei Song, Jingxin Guan, Tianjun Dong, and Xiaoqiang Lu. 2026c. “A Transfer Learning Neural Network–Based Method for Aircraft Specific Excess Power Model Identification.” Preprint, . https://doi.org/10.2139/ssrn.7560478
• Wang, Chen, Ximing Sun, and Xian Du. 2023f. “Installed Performance Seeking Control Based on Supersonic Variable Inlet/engine Coupling Model.” International Journal of Turbo & Jet-Engines 41 (2): 189–200. https://doi.org/10.1515/tjj-2023-0030
• Wang, Zhao, Xiang Tang, Meng Huang, Xiaotao Tian, and Bo Zhang. 2025b. “An Equal-Margin Control Method for Inlet Unstart Protection in the Solid Rocket Ramjet.” Journal of Physics: Conference Series 3041 (1): 012024. https://doi.org/10.1088/1742-6596/3041/1/012024
• Wang, J., S. Verma, and R. Alexander. 2005a. “PLF-18: Springback Control of Sheet Metal Air Bending Process(PLF-III: PLASTIC FORMING AND ADVANCED PRODUCTS).” Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (0): 40. https://doi.org/10.1299/jsmeintmp.2005.40_5
• Wang, K., J. Y. Wang, H. X. Huang, L. R. Xie, Y. Liu, and H. J. Tan. 2023e. “Effects of Backpressure on Unstart and Restart Characteristics of a Supersonic Inlet.” Aeronautical Journal 127 (1316): 1774–92. https://doi.org/10.1017/aer.2023.19
• Wang, Ming Wei, Chun Yan Wang, and Li Wen Zhang. 2011a. “Finite Element Simulation of Vacuum Hot Bulge Forming of Titanium Alloy Cylindrical Workpiece.” In Materials science forum, vol. 675-677. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.675-677.921
• Wang, Huaitao, Dafang Wu, and Feng Wang. 2017b. “A New Method for Determining Horizontal Impact Load Based on Rotational Speed of Aircraft Wheel in Landing Gear Drop Test.” MATEC Web of Conferences 114: 03004. https://doi.org/10.1051/matecconf/201711403004
• Wang, Jian, Jiahuan Yao, Renjie Shen, Tao Gui, and Baolin Niu. 2026b. “Impact of Lobe Mixer Height on the Performance of an Afterburner in a Wide Bypass Ratio Engine.” Gas Turbine Experiment and Research 39 (4): 117–26. https://doi.org/10.3724/j.gter.20260044
• Wang, Peiyao, Mingxin Yu, Guang Yan, Jiabin Xia, Jiawei Liu, and Lianqing Zhu. 2023c. “A Deep Learning-Based Method for Calculating Aircraft Wing Loads.” Measurement and Control 56 (7–8): 1129–41. https://doi.org/10.1177/00202940221145971
• Wang, Yunfei, Huacheng Yuan, Jinsheng Zhang, and Zhenggui Zhou. 2021a. “Design and Aerodynamic Performance Analysis of a Variable Geometry Axisymmetric Inlet for TBCC.” International Journal of Turbo & Jet-Engines 40 (4): 379–85. https://doi.org/10.1515/tjj-2020-0030
• Wang, Yong, Tao Zhang, Xianyu Jin, and Yin Yin. 2023j. “Shimmy Suppression of an Aircraft Nose Landing Gear Using Torsional Nonlinear Energy Sink.” Journal of Computational and Nonlinear Dynamics 18 (10): 101002. https://doi.org/10.1115/1.4062909
• Wang, De Min, Jian Zhang, Jian Liu, Tong Zhu, Fangchao Shao, and Lei Zhong. 2016c. “Research on Measurement Equipment for Moment of Inertia of Triple Torsion Bars Based on Torsion Pendulum.” Applied Mechanics and Materials 851: 286–91. https://doi.org/10.4028/www.scientific.net/amm.851.286
• Wang, Yuhui, Junhua Zhang, Zhaoyang Tian, and Lei Shi. 2025c. “Freejet Tests on a Variable Geometry Supersonic Inlet Driven by Shape Memory Alloys.” Journal of Physics: Conference Series 3041 (1): 012007. https://doi.org/10.1088/1742-6596/3041/1/012007
• Wang, Guofeng, Tao Zhao, Yuelin Wang, Xuesong Wu, Xiangxiang Dai, and Qi Liu. 2015. “Current Assisted Superplastic Forming of Titanium Alloy.” MATEC Web of Conferences 21: 04001. https://doi.org/10.1051/matecconf/20152104001
• Wang, Guo Feng, Tao Zhao, Mo Yang, and Xiang Yu Zhao. 2016a. “Current Assisted Superplastic Forming of Titanium Alloy Bellows.” In Materials science forum, vol. 838-839. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.838-839.135
• Wang, Jun, Liu Zheng, Xiaoling Zhang, Zhenhua Li, and Qichao Zhou. 2022d. “Torsion Pendulum Measurement Method for Time Varying Moment of Inertia.” Measurement Science and Technology 34 (3): 035011. https://doi.org/10.1088/1361-6501/aca5a7
• Wang Mingwei, Zhang Liwen, Pei Jibin, and Li Chenhui. 2006. “FEM Simulation of Vacuum Hot Bulge Forming Process of BT20 Titanium Alloy Cylindrical Workpiece.” In International Technology and Innovation Conference 2006 (ITIC 2006), vol. 2006. IEE. https://doi.org/10.1049/cp:20060923
• Ward, G. N. 1949. “Calculation of Downwash behind a Supersonic Wing.” Aeronautical Quarterly 1 (1): 35–38. https://doi.org/10.1017/s0001925900000056
• Ward, Richard. 1989. “Fighter Design from the Soviet Perspective.” In Aircraft Design and Operations Meeting. AIAA 1989-2074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2074
• 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, G., L. Christensen, and R. Sayles. 1975. “Application of New Development Concepts to F101 Engine for B-1 Aircraft.” In 11th Propulsion Conference. AIAA 1975-1290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1290
• Ward, T. R., and James Neeley. 1959. Altitude Performance Evaluation of Two Afterburner Fuel Manifold Configurations in an Iroquois Series 2 Turbojet Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0221389
• Waring Brown, R. 1934. “Aeroplane Brake Development: An Examination of the Possibilities of Tandem Wheel Undercarriages Fitted with Brakes.” Aircraft Engineering and Aerospace Technology 6 (2): 49–50. https://doi.org/10.1108/eb029775
• Waring-Brown, R. 1948. “Disk Brakes for Aircraft: A Review of Disk Brake Development with Examples of Modern Designs.” Aircraft Engineering and Aerospace Technology 20 (3): 89–90. https://doi.org/10.1108/eb031615
• Warner, R. W. 1975. “A General Aerodynamic Approach to the Problem of Decaying or Growing Vibrations of Thin, Flexible Wings with Supersonic Leading and Trailing Edges and No Side Edges.” In Flight Flutter Testing Symp.. https://ntrs.nasa.gov/citations/19760003009
• Warnken, J. A., and W. H. Busch. 1963. Fabrication of an HK31A Magnesium Alloy Airframe Skin. Defense Technical Information Center. https://doi.org/10.21236/ad0419031
• Warrier, Sunil G., and Ray Y. Lin. 1993. “Using Rapid Infrared Forming to Control Interfaces in Titanium-Matrix Composites.” JOM 45 (3). https://ntrs.nasa.gov/citations/19930048068
• Washington, W., and D. Spring. 1982. “An Experimental Investigation of Wing-Tail Interference for a Typical Supersonic Missile.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1339. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1339
• Wasmi, Hatem Rahim, Ali Abdul Mohsin Hasan, and Waleed Jasim Mhaimeed. 2015. “Aeroelastic Flutter of Subsonic Aircraft Wing Section with Control Surface.” Journal of Engineering 21 (12): 104–23. https://doi.org/10.31026/j.eng.2015.12.07
• Wasserbauer, J. F., E. T. Meleason, and P. L. Burstadt. 1996. Experimental Investigation of the Performance of a Mach-2.7 Two-Dimensional Bifurcated Duct Inlet with 30 Percent Internal Contraction. NASA-TM-106728. NASA. https://ntrs.nasa.gov/citations/19960026650
• Wasserbauer, J., R. Shaw, and H. Neumann. 1973. “Minimizing Boundary Layer Bleed for a Mixed Compression Inlet.” In 9th Propulsion Conference. AIAA 1973-1270. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1270
• Wasserbauer, J., and R. Willoh. 1968. “Experimental and Analytical Investigation of the Dynamic Response Ofa Supersonic Mixed- Compression Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-651
• Wasserman, Lee S. 1952. Doublets at Supersonic Speed. Defense Technical Information Center. https://doi.org/10.21236/ad0015929
• 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, 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, 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
• Watkins, Charles E. 1949. Effect of Aspect Ratio on Undamped Torsional Oscillations of a Thin Rectangular Wing in Supersonic Flow. NACA-TN-1895. NASA. https://ntrs.nasa.gov/citations/19930082576
• Watkins, Charles E. 1951. Effect of Aspect Ratio on the Air Forces and Moments of Harmonically Oscillating Thin Rectangular Wings in Supersonic Potential Flow. NACA-TR-1028. NASA. https://ntrs.nasa.gov/citations/19930092082
• Watkins, J., and G. Hammitt. 1966. Aircraft Ground-Flotation Investigation. Part Xiii. Data Report on Test Section 13. Defense Technical Information Center. https://doi.org/10.21236/ad0809193
• Watmuff, Jonathan H., and Alexander J. Smits. 1987. Fundamental Aspects of the Structure of Supersonic Turbulent Boundary. Defense Technical Information Center. https://doi.org/10.21236/ada186366
• Watson, Earl C. 1953. An Analytical Study of the Comparative Performance of Six Air-Induction Systems for Turbojet-Powered Airplanes Designed to Operate at Mach Numbers up to 2.0. NACA-RM-A53H03. NASA. https://ntrs.nasa.gov/citations/19930087828
• Weatherill, Warren H., and Garabed Zartarian. 1958. Tabular Presentation of Supersonic Flutter Trends from Piston Theory Calculations. Defense Technical Information Center. https://doi.org/10.21236/ad0142154
• 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, S., K. Jones, J. Ekaterinaris, and M. Platzer. 1999. “Transonic Flutter Computations for a 2D Supercritical Wing.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-798
• Webster, F., and J. Bucy. 1979. “ASALM-PTV Chin Inlet Technology overviewAdvanced Strategic Air Launched Missile Propulsion Technology Validation of Integral Rocket/ramjet.” In 15th Joint Propulsion Conference. AIAA 1979-1240. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1240
• Weeks, T. 1986. “X-29 Advanced Technology Integration for Tomorrow’s Fighter Aircraft.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2613
• Wegener, Peter P. 1977. Supersonic Diffuser Research. Defense Technical Information Center. https://doi.org/10.21236/ada038280
• Wei, XueTao, caixue Yue, DeSheng Hu, XianLi Liu, YunPeng Ding, and Steven Y. Liang. 2021. “Research on Surface Roughness of Supersonic Vibration Auxiliary Side Milling for Titanium Alloy.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-704632/v1
• Wei, Bo, Feifei Zhang, Kai He, Zheng Li, and Ruxu Du. 2022a. “Deformation and Springback Behavior of Sheet Metal with Convex-Shaped Surfaces in Heat-Assisted Incremental Bending Process Based on Minimum Energy Method.” Journal of Manufacturing Science and Engineering 145 (3): 031003. https://doi.org/10.1115/1.4055961
• Weil, Joseph, and Richard E. Day. 1956a. An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling. NACA-RM-H56A06. NASA. https://ntrs.nasa.gov/citations/19930089282
• Weil, Joseph, and Richard E. Day. 1956b. Correlation of Flight and Analog Investigations of Roll Coupling. NACA-RM-H56F08. NASA. https://ntrs.nasa.gov/citations/19930090285
• 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
• Weinschenk, Annika, and Wolfram Volk. 2014. “Decrease of Springback by Geometrical Modification of the Sheet Metal Part.” Advanced materials research 1018: 277–84. https://doi.org/10.4028/www.scientific.net/amr.1018.277
• Weinstein, Maynard I. 1952. Performance of Supersonic Scoop Inlets. NACA-RM-E52A22. NASA. https://ntrs.nasa.gov/citations/19930087858
• Weisshaar, T. 1973. “Static Aeroelasticity and the Flying Wing.” In 14th Structures, Structural Dynamics, and Materials Conference. AIAA 1973-397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-397
• 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, Terrence A. 1979. Forward Swept Wing Static Aeroelasticity. Defense Technical Information Center. https://doi.org/10.21236/adb042815
• Weisshaar, Terrence, and Jonathan Bohlmann. 1987. “Supersonic Flutter of Aeroelastically Tailored Oblique Wings.” In 28th Structures, Structural Dynamics and Materials Conference. AIAA 1987-734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-734
• Weisshaar, T. A., and J. B. Crittenden. 1976. Flutter of Asymmetrically Swept Wings. NASA-CR-146815. NASA. https://ntrs.nasa.gov/citations/19760014076
• Weisshaar, T. A., and T. A. Zeiler. 1982. “Dynamic Stability of Flexible Forward Swept Wing Aircraft.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820055567
• Weissman, R. 1969. “Influence of Inertia Characteristics on Spin Susceptibility and Spincharacteristics of Fighter-Type Airplanes.” In 7th Aerospace Sciences Meeting. AIAA 1969-188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-188
• Weissman, R. 1972. “Development of Design Criteria for Predicting Departure Characteristics and Spin Susceptibility of Fighter-Type Aircraft.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-984. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-984
• Welge, H., R. Radkey, and P. Henne. 1976. “Nacelle Aerodynamic Design and Integration Study on a Mach 2.2 Supersonic Cruise Aircraft.” In 12th Propulsion Conference. AIAA 1976-757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-757
• Wells, W., and S. Banda. 1981. “Data Analysis for Aircraft Parameter Estimates.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1864
• 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
• Welsh, C. J., and R. M. Watt. 1967. Effects of Roll on the Free-Flight Motion of Statically Stable Bodies. Defense Technical Information Center. https://doi.org/10.21236/ad0658433
• Wen, Shiyu, Xiao-Lei Cui, and Shijian Yuan. 2026. “Stress and Springback Adjustment in Pressing Forming of 316L Stainless Steel Sheet Using Rigid-Elastic Compound Die.” Composite Design and Manufacturing 2 (2): wqag012. https://doi.org/10.1093/cdm/wqag012
• Wen, Hou, Peng Fei Xue, and Tie Hua Ma. 2011. “High Precision Measurement of Moment of Inertia Based on Compound Pendulum.” Applied Mechanics and Materials 105-107: 2055–58. https://doi.org/10.4028/www.scientific.net/amm.105-107.2055
• West, Thomas K., and Michael Bynum. 2021. “HiFIRE Flight 2 Unstart Reliability Analysis.” In ASCEND 2021. AIAA 2021-4139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-4139
• Wetzel, Benton E. 1954. Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well above the Wing Plane: Lateral and Directional Stability. NACA-RM-SA54H26b. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20090025891
• Whalen, Paul P., and Fred A. Wilcox. 1956. Use of Subsonic Diffuser Mach Number as a Supersonic-Inlet Control Parameter. NACA-RM-E56F05. NASA. https://ntrs.nasa.gov/citations/19930089419
• Whipple, R. D., and J. L. Ricket. 1986. Low-Speed Aerodynamic Characteristics of a 1/8-Scale X-29A Airplane Model at High Angles of Attack and Sideslip. NASA-TM-87722. NASA. https://ntrs.nasa.gov/citations/19860022060
• 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
• White, Richard P. 1947. Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the Chance Vought XF5U-1 Airplane, TED No. NACA 2349. NACA-RM-L7I23. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019312
• White, Herbert E. 1963. Wind-Tunnel Investigation of the Use of Wing Tip Blowing to Reduce Drag for Take-off and Landing. Defense Technical Information Center. https://doi.org/10.21236/ad0296103
• White, J. 1994. “A Method for Predicting Combined Dorsal Normal Force and Center-of-Pressure Location at Supersonic Mach Numbers.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3466
• White, J., T. Janssen, and T. Yantis. 1983. “Progress in Propulsion System/airframe Structural Integration.” In 19th Joint Propulsion Conference. AIAA 1983-1123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1123
• 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
• Whitford, Ray. 1988. “Four Decades of Transonic Fighter Design: A Comparison of the Hawker Hunter and British Aerospace Hawk 200.” In Aircraft Design, Systems and Operations Conference. AIAA 1988-4461. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4461
• Whitford, Ray. 1994. Advanced Design Methodologies for Combat Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada338919
• Whitford, Ray. 1995. “A Fighter Design Chronology.” In Aircraft Engineering, Technology, and Operations Congress. AIAA 1995-3920. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3920
• Whitmore, Stephen, Timothy Moes, and Terry Larson. 1990. “Preliminary Results from a Subsonic High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System: Design, Calibration, Algorithm Development, and Flight Test Evaluation.” In 28th Aerospace Sciences Meeting. AIAA 1990-232. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-232
• Whittaker, I. C. 1972. Development of Titanium and Steel Fatigue Variability Model for Application of Reliability Analysis Approach to Aircraft Structures. Defense Technical Information Center. https://doi.org/10.21236/ad0758219
• Whoric, J. M. 1973. Effect of Various External Stores on the Static Longitudinal Stability, Longitudinal Control, and Drag Characteristics of the Model F-4C Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0914456
• Widayati, Niken Tri, Nadia Wahyu Lurinda, Hartono Hartono, and Supriyadi Supriyadi. 2019. “Measurement of Moment of Inertia through a Bifilar Pendulum Swing Based on a Microcontroller.” Journal of Natural Sciences and Mathematics Research 5 (2): 28–33. https://doi.org/10.21580/jnsmr.2019.5.2.11028
• Wiezorek, Joerg M., and Michael J. Mills. 1998. Microstructural Characterization of Interfaces in SiC-Reinforced Titanium Alloy-Matrix Composites. Defense Technical Information Center. https://doi.org/10.21236/ada351754
• Wilcox, F., T. Birch, and J. Allen. 2004. “Force, Surface Pressure, and Flowfield Measurements on a Slender Missile Configuration with Square Cross-Section at Supersonic Speeds.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5451
• Wiler, C., and S. White. 1984. “Projected Advantage of an Oblique Wing Design on a Fighter Mission.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2474
• Wilks, Brett L. 2006. Aerodynamics of Wraparound Fins in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ada447214
• William Ruffles and Sam M. Dakka. 2016. “Aerodynamic Flow Characteristics of Utilizing Delta Wing Configurations in Supersonic and Subsonic Flight Regimes.” Journal of Communication and Computer 13 (6). https://doi.org/10.17265/1548-7709/2016.06.004
• 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, M. 1979. “Unsteady Thin Airfoil Theory for Transonic Flows with Embedded Shocks.” In 17th Aerospace Sciences Meeting. AIAA 1979-204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-204
• Williams, N. R. 1982. “SPF/DB Titanium LFC Porous Panel Concept.” In NASA. Langley Research Center Laminar Flow Control. https://ntrs.nasa.gov/citations/19820012281
• Williams, Walter C. 1991. “X-15 Concept Evolution.” In Proceedings of the X-15 First Flight 30th Anniversary Celebration. https://ntrs.nasa.gov/citations/19910010759
• Williams, M. H., M. R. Chi, E. H. Dowell, and C. S. Ventres. 1977. “Effects of Inviscid Parallel Shear Flows on Steady and Unsteady Aerodynamics and Flutter.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19770037012
• Williams, T. O., and J. C. Duerden. 1970. “Titanium Hot Forming.” In The Science, Technology and Application of Titanium. Elsevier. https://doi.org/10.1016/b978-0-08-006564-9.50117-2
• 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 R., Michael A. Niestroy, and Joseph Borrelli. 2025. “NATO AVT-350 Task Group: Comparison of the Lateral-Directional Stability Provided by Conventional and Active Flow Control Effectors on Tailless Aircraft.” In AIAA SCITECH 2025 Forum. AIAA 2025-1451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1451
• Williams, Matthew, and Kenneth Stevens. 2006. “Computational Prediction of Subsonic Intake Spillage Drag.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3871. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3871
• Williams, D., II, and R. Nelson. 1994. “Roll Behavior of Low Aspect Ratio, Rectangular Wings.” In 12th Applied Aerodynamics Conference. AIAA 1994-1909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1909
• Williams, I, D., and R. Nelson. 1995. “Testing of Low Aspect Ratio, Rectangular Wings at High Angle-of-Attack.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3487
• 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, V. E. 1982. “SPF/DB Titanium Concepts for Structural Efficiency Foi HC.” In NASA. Langley Research Center Laminar Flow Control. https://ntrs.nasa.gov/citations/19820012280
• Wilson, J., and J. Benson. 1978. “Propulsion System Airframe Integration Studies: Advanced Supersonictransport.” In 14th Joint Propulsion Conference. AIAA 1978-1053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1053
• Wilson, David, Kevin Citurs, and John Davidson. 1994. “Development of Flying Qualities Criteria for 60 Deg Angle of Attack.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3506
• Wilson, David J., David R. Riley, and Kevin D. Citurs. 1993. Aircraft Maneuvers for the Evaluation of Flying Qualities and Agility. Volume 2. Maneuver Descriptions and Section Guide. Defense Technical Information Center. https://doi.org/10.21236/ada273685
• Wilson, J., and B. Wright. 1977. “Airframe/engine Integration with Variable Cycle Engines.” In 13th Propulsion Conference. AIAA 1977-798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-798
• Wilson, J., and V. Wright. 1987. “Use of RPM Trim to Automate the Supersonic Engine/inlet Match in theSR-71A.” In 23rd Joint Propulsion Conference. AIAA 1987-1848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1848
• Wilson, Philip, and Liwei Zhang. 2025. “Supersonic Inlet Design Using Method of Characteristics and Computational Fluid Dynamics.” In 2025 Regional Student Conferences. AIAA 2025-98188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-98188
• 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. 2022. Wiley. https://doi.org/10.1002/9781119988281.ch3
• “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
• “Wing Loads.” 1996. In Structural Loads Analysis for Commercial Transport Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600862465.0163.0190
• 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
• Winkelmann, Allen. 1989. “The Effects of Aspect Ratio on the Stall of a Finite Wing.” In 27th Aerospace Sciences Meeting. AIAA 1989-570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-570
• Winkler, E. M. 1954. Stagnation Temperature Probes for Use at High Supersonic Speeds and Elevated Temperatures. Defense Technical Information Center. https://doi.org/10.21236/ad0058826
• Winograd, Lee, and John W. Miles. 1956. “Numerical Results for the Longitudinal Stability Derivatives and Stability Loci of a Low Aspect Ratio Rectangular Wing in Supersonic Flow.” Aeronautical Quarterly 7 (2): 106–8. https://doi.org/10.1017/s0001925900010167
• Winski, Courtney S., Michael D. Bozeman, Alaa A. Elmiligui, et al. 2023. “X-59 Air Data Probe Calibration Wind Tunnel Test.” In AIAA AVIATION 2023 Forum. AIAA 2023-4491. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4491
• 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
• Wissler, J. G. 1981. “Aircraft Testing: Old Art or New Technology?” In 1st Flight Test Conference. AIAA 1981-2379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2379
• Wittliff, Charles E., and Robert W. Byrne. 1951. Preliminary Investigation of a Supersonic Scoop Inlet Derived from a Conical-Spike Nose Inlet. NACA-RM-L51G11. NASA. https://ntrs.nasa.gov/citations/19930086825
• Wokoeck, Ralf, and Rolf Radespiel. 2011. “Measurements of the Aerodynamic Characteristics of Low Aspect Ratio Wings in Complex Motions.” In 41st AIAA Fluid Dynamics Conference and Exhibit. AIAA 2011-3577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3577
• 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
• Woll, Edward. 1948. “Turbojet Engine Performance Characteristics with Reference to Methods of Augmentation.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/480070
• Wolowicz, C. H., and R. B. Yancey. 1973. Summary of Stability and Control Characteristics of the XB-70 Airplane. NASA-TM-X-2933. NASA. https://ntrs.nasa.gov/citations/19730023226
• Wolowicz, C. H., and R. B. Yancey. 1974. Experimental Determination of Airplane Mass and Inertial Characteristics. NASA-TR-R-433. NASA. https://ntrs.nasa.gov/citations/19750001990
• Wood, Richard M. 1999. First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop. NASA/CP-1999-209690/PT3. NASA. https://ntrs.nasa.gov/citations/20000044865
• Wood, Richard, and Steven Bauer. 1988. “Evaluation of a Three-Dimensional Empirically Derived Wing at Supersonic Speeds.” In 26th Aerospace Sciences Meeting. AIAA 1988-481. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-481
• Wood, R. M., and P. F. Covell. 1985. Experimental and Theoretical Study of the Longitudinal Aerodynamic Characteristics of Delta and Double-Delta Wings at Mach Numbers of 1.60, 1.90, and 2.16. NASA-TP-2433. NASA. https://ntrs.nasa.gov/citations/19850021610
• Wood, R. M., S. M. Dollyhigh, and D. S. Miller. 1982. An Initial Look at the Supersonic Aerodynamics of Twin-Fuselage Aircraft Concepts. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19820057473
• Wood, R., and D. Miller. 1984a. “Assessment of Preliminary Prediction Techniques for Wing Leading-Edge Vortex Flows at Supersonic Speeds.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2208
• Wood, R., and D. Miller. 1984b. “Impact of Fuselage Incidence on the Supersonic Aerodynamics of Two Fighter Configurations.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2193
• Wood, R., and D. Miller. 1985a. “Impact of Airfoil Profile on the Supersonic Aerodynamics of Delta Wings.” In 3rd Applied Aerodynamics Conference. AIAA 1985-4073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4073
• Woods-Vedeler, Jessica, and Anthony Pototzky. 1992. “Rolling Maneuver Load Alleviation Using Active Controls.” In Dynamics Specialists Conference. AIAA 1992-2099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2099
• Woodward, F. A. 1956. “Aeroelastic Problems of Low Aspect Ratio Wings: Part II. Aerodynamic Forces on an Elastic Wing in Supersonic Flow.” Aircraft Engineering and Aerospace Technology 28 (3): 77–81. https://doi.org/10.1108/eb032671
• Woolf, Reagan K. 2008. Initial Calibration of an F-16B Pacer Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada495484
• Woolf, Reagan K. 2012. 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
• Woollett, R. R., E. T. Meleason, and D. A. Choby. 1974. Transonic off-Design Drag and Performance of an Axisymmetric Inlet with 40 Percent Internal Contraction on Design. NASA-TM-X-3042. NASA. https://ntrs.nasa.gov/citations/19740023304
• Woolston, Donald S., Frederick W. Gibson, and Herbert J. Cunningham. 1960. Some Divergence Characteristics of Low-Aspect-Ratio Wings at Transonic and Supersonic Speeds. NASA-TN-D-461. NASA. https://ntrs.nasa.gov/citations/19980228192
• Wooten, W. H., J. T. Blozy, D. W. Speir, and R. A. Lottig. 1984. “Altitude Testing of a Flight Weight, Self-Cooled, 2D Thrust Vectoring Exhaust Nozzle.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/841557
• Wortman, A. 1970. “Boundary-Layer Flow at Three-Dimensional Stagnation Points in High-Speed Air Streams.” In 3rd Fluid and Plasma Dynamics Conference. AIAA 1970-806. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-806
• Wrestler Jr. and Clifton G. 1965. Analytic Study of Aircraft Agility in the Turnaround Maneuver. Defense Technical Information Center. https://doi.org/10.21236/ad0622404
• Wu, Longwu. 1996. “Generate Tooling Mesh by FEM Virtual Forming Model for Springback Compensation in Die Surface Design of Sheet Metal Stamping.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/960592
• Wu, G. Q., and G. X. Luo. 2011. “The Use of Laser Surface Modification in Combined Superplastic Forming and Diffusion Bonding of Metals.” In Superplastic Forming of Advanced Metallic Materials. Elsevier. https://doi.org/10.1533/9780857092779.1.83
• Wu, Da Fang, Shuang Wu, Yuewu Wang, Zhen Tong Gao, and Jia Ling Yang. 2013. “Rapid High-Precision Non-Linear Calibration for Temperature Sensors in Transient Aerodynamic Heating Simulation Systems.” Applied Mechanics and Materials 321-324: 618–23. https://doi.org/10.4028/www.scientific.net/amm.321-324.618
• 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
• Wyatt, Demarquis D., and Henry R. Hunczak. 1947. An Investigation of Convergent-Divergent Diffusers at Mach Number 1.85. NACA-RM-E6K21. Aircraft Engine Research Lab. https://ntrs.nasa.gov/citations/19930085709
• Xi, Ming Zhe. 2013. “Investigation on the Microstructures and Tensile Properties of TA15 Titanium Alloy Thick-Wall Parts Formed by Laser Rapid Forming Process.” Advanced materials research 650: 7–11. https://doi.org/10.4028/www.scientific.net/amr.650.7
• Xiang, Xiaojun, Shuai Zhang, and Liangjun Xie. 2022. “Research on Calculation for Rejected Takeoff Distance of Civil Aircraft on Wet and Contaminated Runway.” In 2022 3rd Asia-Pacific Conference on Image Processing, Electronics and Computers. ACM. https://doi.org/10.1145/3544109.3544120
• Xiao, Chunyan, Shuai Gao, and Jun Zhang. 2016. “A Novel Bidirectional and Dual-Redundancy Hybrid Electromagnetic Brake for Aircraft.” Advances in Mechanical Engineering 8 (9): 1687814016669478. https://doi.org/10.1177/1687814016669478
• Xie, Hairun, Yadong Wu, Anjenq Wang, and Hua Ouyang. 2015a. “Numerical Investigation of Inlet Distortion for Different Rear Mounted Engine Installations at Taking-Off Conditions.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-42350
• Xie, Jiang, Zhichun Yang, and Shijun Guo. 2012. “Aerodynamic and Aeroelastic Characteristics of Conformal Control Surfaces and Application in Active Aeroelastic Wing Technology.” In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 20th AIAA/ASME/AHS Adaptive Structures Conference 14th AIAA. AIAA 2012-1513. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-1513
• Xie, Haitong, Honggang Zeng, Mingqiang Luo, Jian Zhai, and Ziliang Guo. 2026. “Study on a Passive Control Device for Inlet Unstart Mitigation via Shock Wave Attenuation.” Preprint, . https://doi.org/10.2139/ssrn.6770201
• Xin, Qi, and Zhongke Shi. 2016. “Prediction and Recovery of Aircraft Unstable Nonlinear Phenomena Using Bifurcation Analysis and Backstepping Method.” Journal of Computational and Nonlinear Dynamics 11 (6): 061007. https://doi.org/10.1115/1.4034049
• Xingjian, Zhu, Wang Xueyu, and Yan Qingjin. 1985. “Convergence of Performance Calculation of Twin Spool Turbojet and Turbofan.” In Volume 1: Aircraft Engine; Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/85-igt-82
• 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, Jinyang. n.d. “Numerical and Experimental Study of Machining Titanium-Composite Stacks.” PhD diss., Paris, ENSAM. https://doi.org/10.70675/204e37d2zd708z4996z9810z13e2b8238cf3
• Xu, Jinyang. 2020. “Machining Challenges and Solutions to Aerospace Grade Composite-Titanium Stacks.” Video Proceedings of Advanced Materials 1 (1): 2020-0812-2020-0812. https://doi.org/10.5185/vpoam.2020.0812
• Xu, Lixin. 2023. “Design of a New Sweptback Wing for a Future Supersonic Aircraft—Research on Lift Drag Characteristics and Aerodynamic Analysis.” Theoretical and Natural Science 18 (1): 1–9. https://doi.org/10.54254/2753-8818/18/20230256
• Xu, Wan, Junrui Li, Boyang Zhang, and Lianxiang Yang. 2019a. “A New Approach to Reduce Springback in Sheet Metal Bending Using Digital Image Correlation.” International Journal of Materials Research 110 (8): 726–33. https://doi.org/10.3139/146.111799
• Xu, Yuanzhi, Xiaolong Tong, Yuemei Yuan, and Xiaofei Wan. 2026. “Fatigue Life Analysis of Aircraft Hydraulic Titanium-Alloy Tube Considering the Influence of Forming Process Factors.” Preprint, . https://doi.org/10.2139/ssrn.7269063
• Xu, Zaifeng, Ke Zhao, Mian Chen, Chen Du, and Mo Liu. 2020. “Research on the Influence of Air Resistance in Spacecraft Moment of Inertia Measurement.” Journal of Physics: Conference Series 1634 (1): 012170. https://doi.org/10.1088/1742-6596/1634/1/012170
• Xue, Hui, H. Khawaja, and M. Moatamedi. 2014a. “Conceptual Design of High Speed Supersonic Aircraft: A Brief Review on SR-71 (Blackbird) Aircraft.” In AIP Conference Proceedings, vol. 1637. AIP Publishing LLC. https://doi.org/10.1063/1.4904694
• Xue, Zhi-Peng, Ming Li, Yan-Hui Li, and Hong-Guang Jia. 2014b. “A Simplified Flexible Multibody Dynamics for a Main Landing Gear with Flexible Leaf Spring.” Shock and Vibration 2014: 1–10. https://doi.org/10.1155/2014/595964
• Xue, David, and Chuh Mei. 1992. “Finite Element Nonlinear Panel Flutter with Arbitrary Temperatures in Supersonic Flow.” In Dynamics Specialists Conference. AIAA 1992-2129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2129
• Xue, David, Chuh Mei, and Charles Shore. 1990. “Finite Element Two-Dimensional Panel Flutter at High Supersonic Speeds and Elevated Temperature.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-982. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-982
• Xue, Caijun, Yue Wang, Bin Sun, and Fenjin Xu. 2012b. “Optimization of the Cushion Properties of Amphibious Aircraft Landing Gear by Simulation and Drop Test.” Journal of Vibration and Control 19 (11): 1753–60. https://doi.org/10.1177/1077546312451612
• Xuebin, Zheng, Han Longshuai, Li Xuetao, E. Hongwei, Wu Xiangdong, and Wan Min. 2024. “Study on Influencing Factors of U-Bending Springback Prediction of DP780 Dual-Phase Steel.” Journal of Mechanical Engineering 60 (6): 197. https://doi.org/10.3901/jme.2024.06.197
• Yadav, Umacharan Singh, and Vinod Yadava. 2015. “Experimental Modelling and Optimisation of Process Parameters of Hole Drilling by Electrical Discharge Machining of Aerospace Titanium Alloy.” International Journal of Manufacturing Technology and Management 29 (3/4): 211. https://doi.org/10.1504/ijmtm.2015.069256
• Yaghmaee, S., and D. Roberts. 1986. “A Numerical Algorithm for Simulating 3D Viscous Supersonic Inlet Flows.” In 24th Aerospace Sciences Meeting. AIAA 1986-552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-552
• Yahalom, Rafael. 1971. An Experimental Investigation of Supersonic Flow past Yawed Cones. Defense Technical Information Center. https://doi.org/10.21236/ad0728233
• 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
• Yaman, Kemal, and M. Burak Dalmış. 2026. “Influence of under-Wing Store Mass on the Flutter Response of an F-16 Model Wing.” Transactions of FAMENA 50 (2): 21–38. https://doi.org/10.21278/tof.502080725
• Yamane, Gen, Vincent Velay, Vanessa Vidal, and Hiroaki Matsumoto. 2018. “Mechanical Behavior of Ti-6Al-2Sn-4Zr-2Mo Titanium Alloy under Hot and Superplastic Forming Conditions: Experiment and Modeling.” Defect and diffusion forum/Diffusion and defect data, solid state data. Part A, Defect and diffusion forum 385: 413–18. https://doi.org/10.4028/www.scientific.net/ddf.385.413
• Yamazaki, Kiyoshi, Takashi Yamaguchi, Yohei Murayama, Ken-ichiro Mori, and Tomoyoshi Maeno. 2014. “Development of Hot Stamping Process for Aircraft Titanium Alloy Parts Using Resistance Heating.” Journal of the Japan Society for Technology of Plasticity 55 (647): 1097–1101. https://doi.org/10.9773/sosei.55.1097
• Yan, Hong. 2012. “Thermal Perturbations in Supersonic Transition.” In InTech eBooks. https://doi.org/10.5772/38991
• Yan, Hong. 2013. “Near-Surface Discharge in Supersonic Inlet Control.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-530
• Yan, Bin, Ning Kong, Jie Zhang, and Hongbo Li. 2019. “High Temperature Formability of Ti–4Al–2V Titanium Alloy under Hot Press Forming Process.” Materials Research Express 6 (12): 126501. https://doi.org/10.1088/2053-1591/ab539b
• Yan, Hao, Guang Yang, and Tong Huang. 2025. “A Boundary Layer Transition Criteria on Three-Dimensional Flow for High-Speed Aircraft.” AIP Advances 15 (12): 125225. https://doi.org/10.1063/5.0283545
• Yang, Jian. n.d. “Experimental Study and Modeling of the Superplastic Forming for Un Aluminium Alloy Al7475.” PhD diss., Paris, ENSAM. https://doi.org/10.70675/b03bdd86z2d0cz479az8fd0z12b27ab2c3db
• Yang, Tingwu. 2021. “Aviation Sensors and Their Calibration.” In Telemetry Theory and Methods in Flight Test. Springer Singapore. https://doi.org/10.1007/978-981-33-4737-3_3
• Yang, Rui, Jiahui Jin, and Yuxin Zhao. 2024a. “The Law of the Total Pressure Loss in Supersonic Streamwise Corner Flow.” Journal of Physics: Conference Series 2860 (1): 012009. https://doi.org/10.1088/1742-6596/2860/1/012009
• Yang, Yong, Hui Hui Li, and Guang Yao Meng. 2010. “Study on Prediction of Machining Distortion for Titanium Alloy Aircraft Monolithic Component by FEM.” Advanced materials research 97-101: 2951–54. https://doi.org/10.4028/www.scientific.net/amr.97-101.2951
• Yang, Xiaoxi, Baokuan Li, Yang Nie, and Zhibo Ren. 2026. “Effects of Jet Exhaust on Engine Inlet Distortion during Carrier-Based Aircraft Takeoff.” Thermal Science 30 (2 Part B): 1547–61. https://doi.org/10.2298/tsci250222228y
• Yang, Lei, Nan Li, Baoyu Wang, Jianguo Lin, Huijun Zhao, and Wenyu Ma. 2016b. “Unified Constitutive Modelling for Two-Phase Lamellar Titanium Alloys at Hot Forming Conditions.” Manufacturing Review 3: 14. https://doi.org/10.1051/mfreview/2016016
• Yang, Xiang An, and Feng Ruan. 2010. “A Study on Objective Functions for Springback Control in Multi-Objective Optimization of Sheet Metal Forming Process.” Applied Mechanics and Materials 34-35: 98–104. https://doi.org/10.4028/www.scientific.net/amm.34-35.98
• Yang, Yiyan, Zhaoyang Tian, Xue Yang, Xiaowei Liu, and Lei Shi. 2024b. “Start/unstart Hysteresis Characteristics Driven by Embedded Rocket of a Rocket-Based Combined-Cycle Inlet.” Physics of Fluids 36 (8): 086101. https://doi.org/10.1063/5.0212881
• Yang, Henry T. Y., and C. H. Wan. 1978. Investigation of Torsion Free Wing Trend Flutter Models. Defense Technical Information Center. https://doi.org/10.21236/ada061942
• Yang, Lejie, Junqiang Wu, Yang Tao, Shang Ma, Guoshuai Li, and Jifei Wu. 2025. “Study on Leading-Edge Vortex/shock Interaction and Unsteady Characteristics of a Transonic Low-Aspect-Ratio Flying Wing.” Physics of Fluids 37 (7): 075220. https://doi.org/10.1063/5.0280452
• Yang, Zhi, Xiang Zhao, Sijun Zhang, and Chien-Pin Chen. 2011. “Fluid-Structure Interaction for Flutter Predictions in Transonic and Supersonic Flows.” In ASME-JSME-KSME 2011 Joint Fluids Engineering Conference: Volume 1, Symposia – Parts A, B, C, and D. ASMEDC. https://doi.org/10.1115/ajk2011-08030
• Yao, P. P. 2002. “Development of PM Aircraft Brake Materials.” Metal Powder Report 57 (4): 42. https://doi.org/10.1016/s0026-0657(02)80158-8
• Yarlett, Amanda, Ronald Adrezin, Alfred Gates, and Fu-Shang Wei. 2000. “Analysis and Manufacture of Dynamically Scaled Wind Tunnel Models.” In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 2000-1694. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1694
• Yates, John. 1963. “Flutter of Supersonic Wing-Body Configurations.” In Summer Meeting. AIAA 1963-205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-205
• Yates, John E. 1976. Pressure Distribution on the Trailing Edge of an Airfoil Oscillating in a Shear Layer. Defense Technical Information Center. https://doi.org/10.21236/ada030887
• Yates, J. 1977. “Pressure Distribution on the Trailing Edge of a Semi-Infinite Airfoil Oscillating in a Shear Layer.” In 15th Aerospace Sciences Meeting. AIAA 1977-157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-157
• Yates, J. 1978. “Viscous Thin Airfoil Theory and the Kutta Condition.” In 16th Aerospace Sciences Meeting. AIAA 1978-152. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-152
• Yates, John E. 1980. Viscous Thin Airfoil Theory. Defense Technical Information Center. https://doi.org/10.21236/ada082744
• Yates, Carson, Jr. 1967. Subsonic and Supersonic Flutter Analysis of a Highly Tapered Swept-Wing Planform, Including Effects of Density Variation and Finite Wing Thickness, and Comparison with Experiments. NASA-TN-D-4230. NASA. https://ntrs.nasa.gov/citations/20040047107
• Yates, E. C., Jr., H. J. Cunningham, R. N. Desmarais, W. A. Silva, and B. Drobenko. 1982c. “Subsonic Aerodynamic and Flutter Characteristics of Several Wings Calculated by the SOUSSA P1.1 Panel Method.” In Structural Dynamics and Materials Conference. https://ntrs.nasa.gov/citations/19820046658
• Yates, E., Jr., E. Wynne, and M. Farmer. 1982a. “Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing.” In 23rd Structures, Structural Dynamics and Materials Conference. AIAA 1982-647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-647
• Yatskikh, Aleksey, Marina Rumenskikh, Yury Yermolaev, Aleksander Kosinov, and Nikolay Semionov. 2017. “Excitation of Localized Wave Packet in Swept-Wing Supersonic Boundary Layer.” MATEC Web of Conferences 115: 02015. https://doi.org/10.1051/matecconf/201711502015
• Yeager, Richard A., and Laurence W. Gertsma. 1958. Investigation of an Underslung Half-Cone Inlet with Compression Surface Mounted Outboard from Fuselage at Mach Numbers of 1.5, 1.8, and 2.0. NACA-RM-E58A27b. NASA. https://ntrs.nasa.gov/citations/19930090049
• Yetna n’jock, M., B. Houssem, C. Labergere, K. Saanouni, and Y. Zhenming. 2018. “Explicit and Implicit Springback Simulation in Sheet Metal Forming Using Fully Coupled Ductile Damage and Distortional Hardening Model.” In AIP Conference Proceedings, vol. 1960. Author(s). https://doi.org/10.1063/1.5034940
• Yi, H. K., D. W. Kim, C. J. Van Tyne, and Y. H. Moon. 2008. “Analytical Prediction of Springback Based on Residual Differential Strain during Sheet Metal Bending.” Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 222 (2): 117–29. https://doi.org/10.1243/09544062jmes682
• Yilamu, K., R. Hino, H. Hamasaki, and F. Yoshida. 2010. “Bauschinger Effect on Springback of Clad Sheet Metals in Draw Bending.” Materials Transactions 51 (7): 1364–66. https://doi.org/10.2320/matertrans.m2010058
• Yildiz, Anil, Ugur Akcal, Batuhan Hostas, Nazim K. Ure, and Gokhan Inalhan. 2018. “Finite State Automata Based Approach to Autonomous Stall and Upset Recovery for Agile Aircraft.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1867
• Yonezawa, Masahito, Hiroshi Yamashita, Shigeru Obayashi, and Kazuhiro Kusunose. 2007. “Investigation of Supersonic Wing Shape Using Busemann Biplane Airfoil.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-686. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-686
• Yong, Wentao. 2019. “Study on Aerodynamic Characteristics of Supersonic Airfoil.” Modern Mechanical Engineering 09 (01): 13–19. https://doi.org/10.4236/mme.2019.91002
• Yong, Shan, Zhang JingZhou, and Wang Yameng. 2014. “Numerical Investigation on Aerodynamic and Combustion Performance of Chevron Mixer inside an Afterburner.” Journal of Engineering for Gas Turbines and Power 136 (11): 111501. https://doi.org/10.1115/1.4027604
• Yoon, Jong Hoon, Ho Sung Lee, Yeong Moo Yi, and Young Soon Jang. 2007. “Finite Element Analysis on Superplastic Blow Forming of Ti-6Al-4V Multi-Sheets.” In Materials science forum. Trans Tech Publications. https://doi.org/10.4028/0-87849-432-4.1361
• 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, Fusahito, F. Barlat, Y. H. Moon, and M. G. Lee. 2010. “Material Models for Accurate Simulation of Sheet Metal Forming and Springback.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3457626
• Yoshida, Fusahito, and Takeshi Uemori. 2015. “Cyclic Plasticity Model for Accurate Simulation of Springback of Sheet Metals.” In 60 Excellent Inventions in Metal Forming. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46312-3_10
• Yoshikawa, K. 1982. “Transient Phenomena of Shock-Induced Turbulent Separation for a Spikebody and Stalling Airfoil at Transonic and Supersonic Speeds.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1362
• Yoshiki, Haruo, Nobuhisa Kamikawa, Yasukata Tsutsui, and Nobuyuki Takama. 1985. “Pressure Distribution around an Airfoil Placed in a Periodically Fluctuating Air Flow: 2nd Report, a Thin Airfoil Approximation.” Bulletin of JSME 28 (246): 2907–14. https://doi.org/10.1299/jsme1958.28.2907
• Yotsuya, T., Masahiro Kanazaki, Yoshikazu Makino, and Kisa Matsushima. 2014. “Multi-Point Design of a Supersonic Wing Using Modified Par-Sec Airfoil Representation.” In Blucher Mechanical Engineering Proceedings, vol. 1. https://doi.org/10.5151/meceng-wccm2012-16733
• Young, Steven D. 2019. “Airplane State Awareness and Prediction Technologies – Research Overview (2014-2018).” In AIAA Scitech 2019 Forum. AIAA 2019-0716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0716
• Young, David, Stewart Jenkins, and Daniel Miller. 2005. “An Investigation of Active Flowfield Control for Inlet Shock/Boundary Layer Interaction.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4020. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4020
• Young, A. D., and S. Kirkby. 1955. “The profile drag of biconvex wing sections at supersonic speeds.” In 50 Jahre Grenzschichtforschung. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-663-20219-6_39
• Young, J., A. Schy, and K. Johnson. 1977. “Prediction of Jump Phenomena in Rotationally-Coupled Maneuvers of Aircraft, Including Nonlinear Aerodynamic Effects.” In Guidance and Control Conference. AIAA 1977-1126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1126
• Young, J. W., A. A. Schy, and K. G. Johnson. 1980. Pseudosteady-State Analysis of Nonlinear Aircraft Maneuvers. NASA-TP-1758. NASA. https://ntrs.nasa.gov/citations/19810004554
• Yu, Huai-Te. 2023. “Some Considerations for Large Angle Unsteady Thin Airfoil Theoretical Modeling.” In AIAA SCITECH 2023 Forum. AIAA 2023-0996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0996
• Yu, Huai-Te, and Luis P. Bernal. 2016. “Experimental Investigation of Three-Dimensional Flow Development by Pitching Low-Aspect-Ratio Wing.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1066
• Yu, Huai-Te, Luis P. Bernal, and Michael V. Ol. 2013. “Effects of Planform Geometry and Pivot Axis Location on the Aerodynamics of Pitching Low Aspect Ratio Wings.” In 43rd Fluid Dynamics Conference. AIAA 2013-2992. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2992
• Yu, Hang, and Sanjeeb T. Bose. 2026. “Large-Eddy Simulations for the Flutter Prediction of the NASA Benchmark Supercritical Wing.” In AIAA AVIATION 2026 Forum. AIAA 2026-4664. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4664
• 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, Li, Bin Lv, Hong Tao Guo, Yu Yan, Xing Hua Yang, and Jian Guo Luo. 2014a. “Research on Transonic Wind Tunnel Flutter Test for a Wing Model.” Advanced materials research 1006-1007: 26–29. https://doi.org/10.4028/www.scientific.net/amr.1006-1007.26
• Yu, Li, Bin Lv, Hong Tao Guo, Yu Yan, Jun Zha, and Bo Lu. 2014b. “Static Aeroelasticity Solution for Divergence Dynamic Pressure of Wing.” Applied Mechanics and Materials 633-634: 1233–36. https://doi.org/10.4028/www.scientific.net/amm.633-634.1233
• Yuceil, Kemal, Agustin Valdivia, Justin Wagner, Noel Clemens, and David Dolling. 2009. “Active Control of Supersonic Inlet Unstart Using Vortex Generator Jets.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-4022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-4022
• Yurkovich, Rudy. 1996. “Wing-Tail Interaction Flutter Revisited.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1447
• Zafar, Muhammad I., Francesca Fusi, and Giuseppe Quaranta. 2017. “Multiple Input Describing Function Analysis of Non-Classical Aileron Buzz.” Advances in aircraft and spacecraft science 4 (2): 203–18. https://doi.org/10.12989/aas.2017.4.2.203
• Zakkay, V., and G. Miller. 1978. “The Use of Fluidized Beds for Heating Air for Wind Tunnels.” In 10th Aerodynamic Testing Conference. AIAA 1978-818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-818
• 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
• Zartarian, Garabed. 1956. Theoretical Studies on the Prediction of Unsteady Supersonic Airloads on Elastic Wings. Part 2. Rules for Application of Oscillatory Supersonic Aerodynamic Influence Coefficients. Defense Technical Information Center. https://doi.org/10.21236/ad0110592
• Zartarian, Garabed, and Pao-Tan Hsu. 1955. Theoretical Studies on the Prediction of Unsteady Supersonic Airloads on Elastic Wings. Part i. Investigations on the Use of Oscillatory Supersonic Aerodynamic Influence Coefficients. Defense Technical Information Center. https://doi.org/10.21236/ad0110591
• Zeis, Joseph, Jr., Heather Lambert, Robert Calico, and Daniel Gleason. 1988. “Angle of Attack Estimation Using an Inertial Reference Platform.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4351
• Zeng, Weiyi, Zhongliang Zhao, Haiyong Yang, and Hao Li. 2022. “Research on Dynamic Aerodynamic Characteristics of Flying Wing Model with Low Aspect Ratio.” Journal of Physics: Conference Series 2228 (1): 012011. https://doi.org/10.1088/1742-6596/2228/1/012011
• Zengin, Yasemin, and Sedat Tokgoz. 2022. “Tahliye Havasının Turbojet Performansına Etkisi.” ASREL. https://doi.org/10.56753/asrel.2022.1.3
• Zha, Ge-Cheng, Doyle Knight, and Donald Smith. 1998b. “Numerical Investigations of HSCT Inlet Unstart Transient at Angle of Attack.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3583
• 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, G., B. Chen, and S. Dong. 2021c. “Research on Hydraulic Dump Response Performance of Civil Aircraft Brake System.” IET Conference Proceedings 2020 (3): 164–70. https://doi.org/10.1049/icp.2021.0286
• Zhang, Jiyuan, Min Chen, Hailong Tang, and Xin Liu. 2020b. “A Study of Two Variable Cycle Engine Concepts for High Speed Civil Aircraft.” In Volume 1: Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2020-16248
• Zhang, Yufei, Haixin Chen, Miao Zhang, Meihong Zhang, and Song Fu. 2014c. “A Thrust Drag Bookkeeping Method Based on Computational Fluid Dynamics.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3686. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3686
• Zhang, Yongjie, Wenhao Chen, hang Zhou, and Bo Cui. 2026a. “Dynamics Simulation and Anti-Bird Impact Design for Landing of Civil Aircraft Landing Gear after Bird Strike.” Preprint, . https://doi.org/10.2139/ssrn.6582445
• Zhang, Wei, Qian Dong, and Xian Min Zhang. 2015c. “Study on Mechanical Response Changes of Pavement to Aircraft Loads with Different Landing Gear Configurations.” Applied Mechanics and Materials 723: 60–64. https://doi.org/10.4028/www.scientific.net/amm.723.60
• Zhang, Shuai, Chengyu Fu, Zhenming Yue, and Hao Qu. 2026d. “Springback Prediction in Tube Free Bending Based on Simulation and WOA-Attention-BP Hybrid Neural Network.” Preprint, . https://doi.org/10.2139/ssrn.6885028
• Zhang, Shu, Yu Huang, and Jian Xu. 2011. “Time-Delayed Feedback Control for Flutter of Supersonic Aircraft Wing.” In Springer Proceedings in Physics. Springer Netherlands. https://doi.org/10.1007/978-94-007-2069-5_100
• Zhang, K. F., and S. S. Jiang. 2014. “Superplastic Forming.” In Comprehensive Materials Processing. Elsevier. https://doi.org/10.1016/b978-0-08-096532-1.00527-6
• Zhang, Z. T., and Daeyong Lee. 1996. “Springback Analysis and Control in Forming Two-Step Rail-Shaped Sheet Metal Parts.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/960596
• Zhang, Yaobing, Bin Li, Pengcheng Cui, Naichun Zhou, and Xiaojun Wu. 2020a. “Numerical Simulation of Support Interference Characteristics on a Low-Aspect Ratio Flying-Wing Model.” Journal of Physics: Conference Series 1600 (1): 012036. https://doi.org/10.1088/1742-6596/1600/1/012036
• Zhang, Hui, Jie Li, and Qiong Liu. 2014b. “Flight Loads Analysis of a Maneuvering Transport Aircraft.” Advanced materials research 1016: 460–64. https://doi.org/10.4028/www.scientific.net/amr.1016.460
• Zhang, Zhibing, Yu Qi Liu, Ting Du, and Zhi Gang Li. 2008b. “Fast Prediction of Springback at Product Design Stage for Sheet Metal Forming.” In Materials science forum, vol. 575-578. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.575-578.525
• Zhang, Guangcan, Qingtang Meng, and Shaopeng Dong. 2025b. “Simulation Analysis of Key Component of Aircraft Brake System.” IET Conference Proceedings 2024 (13): 1153–58. https://doi.org/10.1049/icp.2024.3047
• Zhang, Xu, JiXiang Shan, and Yong Huang. 2017. “Effect of Nose Thickness Distribution on the Stall Characteristics of Low Aspect Ratio Flying Wing Configuration at Transonic Flow.” SCIENTIA SINICA Technologica 47 (9): 985–91. https://doi.org/10.1360/n092016-00329
• Zhang, Kai Feng, G. Wang, Guo Feng Wang, C.-W. Wang, and Daren Wu. 2004. “The Superplastic Forming Technology of Ti-6Al-4V Titanium Alloy Bellows.” In Materials science forum, vol. 447-448. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.447-448.247
• Zhang, Xia, Wei Wei, and Feng Lu. 2025a. “Parametric Study on Dynamic Response Characteristics of Aircraft Hydraulic Brake System.” IET Conference Proceedings 2024 (13): 1608–13. https://doi.org/10.1049/icp.2024.3122
• Zhang, Shen, and Jianjun Wu. 2016. “Springback Prediction of Three-Dimensional Variable Curvature Tube Bending.” Advances in Mechanical Engineering 8 (3): 1687814016637327. https://doi.org/10.1177/1687814016637327
• Zhang, Li, and Cai Jun Xue. 2011. “A Landing Gear Drop Dynamic Simulation Based on the LMS. Virtual. Lab.” Applied Mechanics and Materials 55-57: 684–87. https://doi.org/10.4028/www.scientific.net/amm.55-57.684
• Zhang, Xiao Lin, Lie Shan Zhang, Bin Zou, Wen Yan Tang, and Qiu Feng Shao. 2015b. “Study on Detection Method of Moment of Inertia with Torsion Pendulum Method in Frequency Domain Based on FFT.” Applied Mechanics and Materials 738-739: 826–31. https://doi.org/10.4028/www.scientific.net/amm.738-739.826
• Zhao, Yan. 2011. Measurement of Moment of Inertia Based on Torsion Pendulum Considering Air Damping. https://doi.org/10.5813/www.ieit-web.org/ips.1.89
• Zhao, Xuwen, Cai Maolin, Peng Shi, Zirui Li, Dongjiang Han, and Xiaomeng Tong. 2025. “Intelligent Method Combining Models and Process Data for Springback Prediction in Sheet Metal Stamping.” Preprint, . https://doi.org/10.2139/ssrn.5355627
• Zhao, Wei, Weiping Zeng, Yingying Shen, Xiangpeng Hu, and Jiangtao Chen. 2023. “Research on Low-Speed Aerodynamic Characterictics of Flying Wing Standard Model with Low-Aspect Ratio.” Highlights in Science Engineering and Technology 77: 150–55. https://doi.org/10.54097/hset.v77i.14434
• Zhao, Yan, Xiao Lin Zhang, Jun Wang, and Wen Yan Tang. 2012a. “Measurement of Moment of Inertia Based on Torsion Pendulum.” Advanced materials research 588-589: 964–67. https://doi.org/10.4028/www.scientific.net/amr.588-589.964
• Zhao, Y. L., Yiheng Zhou, and Yilong Zhao. 2022. “Experimental Study of the Unstart/Restart Process of a Two-Dimensional Supersonic Inlet Induced by Backpressure.” Journal of Applied Fluid Mechanics 15 (2). https://doi.org/10.47176/jafm.15.02.33220
• Zheng, Xuebin. 2024. “Influence of Hardening Model on Draw-Bending Springback Prediction of DP980 Dual-Phase Steel.” In Materials Research Proceedings, vol. 44. Materials Research Forum LLC. https://doi.org/10.21741/9781644903254-62
• Zhi, Pengbo, Li Zhou, and Tao Qiu. 2020. “Compensation Method for Torsional Stiffness of Flexible Wing.” In Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2020, edited by Daniele Zonta, Haiying Huang. SPIE. https://doi.org/10.1117/12.2557758
• Zhiqiang, Liu. 2014. “Green Machining of Ti-6Al-4V under Minimum Quantity Lubrication (MQL) Condition.” In Materials Forming, Machining and Tribology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9_5
• Zhong, Jiaxiang, Feng Qu, Di Sun, Qingsong Liu, Qing Wang, and Junqiang Bai. 2024. “Low-Frequency Unsteadiness Mechanisms of Unstart Flow in an Inlet with Rectangular-to-Elliptical Shape Transition under off-Design Condition at a Mach Number of 4.” Journal of Fluid Mechanics 991: A9. https://doi.org/10.1017/jfm.2024.504
• Zhou, Xiao. n.d. “Numerical Prediction of Springback in U-Channel Forming of Aluminum Tailor Welded Blanks.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1999-04345
• Zhou, Chi, Juan Liao, Yin Zhu, et al. 2010. “A Method of Springback Prediction and Tool Shape Compensation for Multi-Curvature Sheet Metal Bending.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.3457647
• Zhou, Huifang, Shuyou Zhang, Lemiao Qiu, and Zili Wang. 2021a. “Springback Angle Prediction of Circular Metal Tube Considering the Interference of Cross-Sectional Distortion in Mandrel-Less Rotary Draw Bending.” Science Progress 104 (1): 0036850420984303. https://doi.org/10.1177/0036850420984303
• Zhu, Lei, and Nan Li. 2023. “Springback Prediction for Sheet Metal Cold Stamping Using Convolutional Neural Networks.” In 2022 Workshop on Electronics Communication Engineering, edited by Letian Huang. SPIE. https://doi.org/10.1117/12.2675249
• Zhu, Biao, and Zhide Qiao. 2009. “Calculation of Wing Flutter Using Euler Equations with Approximate Boundary Conditions.” In Computational Fluid Dynamics 2008. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-01273-0_11
• Zhu, Fanghui, and Xiaomei Wang. 2025. “Study on Heat Transfer Performance of Aircraft Brake Using CFD Simulation.” IET Conference Proceedings 2024 (13): 316–21. https://doi.org/10.1049/icp.2024.2860
• Zien, T. F., and W. C. Ragsdale. 1979. Predictions of Aerodynamic Heating on Tactical Missile Domes. Defense Technical Information Center. https://doi.org/10.21236/ada073217
• Ziffrin, L. B. 1962. Welding Study on Titanium Alloys. Defense Technical Information Center. https://doi.org/10.21236/ad0687291
• Zimmerman, C. H. 1936. Effect of Changes in Tail Arrangement upon the Spinning of a Low-Wing Monoplane Model. NACA-TN-570. NASA. https://ntrs.nasa.gov/citations/19930081317
• Zlatin, Norman, and Michael Field. 1973. “Procedures and Precautions in Machining Titanium Alloys.” In Titanium Science and Technology. Springer US. https://doi.org/10.1007/978-1-4757-1346-6_37
• ИЛЮХИН, И.М., and И.В. ЕГОРОВ. 2024. “Turbulent Spot in the Supersonic Boundary Layer on a Parabolic Airfoil.” Preprint, . https://doi.org/10.15372/pmtf202415496
• Шифрин, Б.М. 2004. “Self-Oscillations of Aircraft Landing Gear Shock-Strut at Considerable Non-Linear Friction.” Proceedings of National Aviation University 19 (1). https://doi.org/10.18372/2306-1472.19.989
• 君, 郭. 亭. 2024. “Dynamic Mechanical Properties of the High-Strength Titanium Alloy Ti5553.” Preprint, . https://doi.org/10.2139/ssrn.5065174

Secondary Sources

• Abzug, Malcolm J., and E. Eugene Larrabee. 2002. Airplane Stability and Control, Second Edition: A History of the Technologies That Made Aviation Possible. Cambridge University Press. https://doi.org/10.1017/cbo9780511607141
• Aircraft and Engine Development Testing. 1986. National Academies Press. https://doi.org/10.17226/19206
• Aircraft Tires: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604641
• Aircraft Wheels, Brakes, and Brake Controls: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604702
• Airfield Compatibility: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604672
• 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. 2002. 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, 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
• Baals, William Corliss Donald, and Corliss. 1981. Wind Tunnels of NASA. NATIONAL AERONAUTICS & SPACE. https://openlibrary.org/works/OL31504107W
• 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. 1989. Orders of Magnitude: A History of the NACA and NASA, 1915-1990. United States Govt Printing Office. https://openlibrary.org/works/OL18823771W
• Bisplinghoff, Raymond L., Ashley, Halfman, and Aeroelasticity. 1955. Aeroelasticity. Addison-Wesley Pub. Co. https://openlibrary.org/works/OL3240762W
• Boley, Bruno A., and J. H. Weiner. 1960. Theory of Thermal Stresses. John Wiley & Sons Inc. https://openlibrary.org/works/OL19334049W
• 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
• Bruhn, E. F. 1973. Analysis and Design of Flight Vehicle Structures. Jacobs Pub. https://openlibrary.org/works/OL8796483W
• Carslaw, H. S., & Jaeger, J. C., and Jaeger. 1959. Conduction of Heat in Solids. Second Edition. Clarendon P. https://openlibrary.org/works/OL34686169W
• 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
• Cohen, Doris, and Robert Thomas Jones. 1960. High Speed Wing Theory. Princeton University Press. https://doi.org/10.1515/9781400874941
• Cover, Thomas M., and Joy A. Thomas. 2006. Elements of Information Theory. Wiley & Sons Canada, Limited, John. https://openlibrary.org/works/OL21500808W
• Currey, Norman S. 1988. Aircraft Landing Gear Design: Principles and Practices. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.861468
• Davim, J. Paulo, ed. 2014. Machining of Titanium Alloys. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-43902-9
• Donovan, Allen F., ed. 1962. High Speed Problems of Aircraft and Experimental Methods. Princeton University Press. https://doi.org/10.1515/9781400875030
• 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
• Flight Test Instrumentation. 1965. Elsevier. https://doi.org/10.1016/c2013-0-01867-1
• Flight-Loads Prediction and Structural-Life Management. 1981. National Academies Press. https://doi.org/10.17226/19736
• Francillon, René J. 1920. McDonnell Douglas Aircraft since 1920. Putnam. https://openlibrary.org/works/OL1686392W
• 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
• Giuliano, Gillo. 2011. Superplastic Forming of Advanced Metallic Materials. Woodhead Publishing Limited. https://doi.org/10.1533/9780857092779
• 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. 2001. Expanding the Envelope: Flight Research at NACA and NASA. University Press of Kentucky. https://openlibrary.org/works/OL4400572W
• 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. 1984. On the Frontier: Flight Research at Dryden, 1946-1981. Scientific and Technical Information Branch, National Aeronautics and Space Administration. https://openlibrary.org/works/OL2688458W
• 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
• 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
• Holder, William G. 2006. Lost Fighters: A History of U.S. Jet Fighter Programs That Didn’t Make It. SAE International eBooks. https://doi.org/10.4271/r-374
• 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
• Incropera, Frank P., David P. DeWitt, Fundamentals of Heat, and Mass Transfer. 1985. Fundamentals of Heat and Mass Transfer. Wiley. https://openlibrary.org/works/OL2975219W
• Jenkins, Dennis R. 2000. Hypersonics before the Shuttle: A Concise History of the X-15 Research Airplane. https://openlibrary.org/works/OL813290W
• Jenkins, Dennis R. 2007. X-15: Extending the Frontiers of Flight. NASA. https://ntrs.nasa.gov/citations/20080008340
• 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
• 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
• Launius, Roger, and Dennis Jenkins. 2012. Coming Home: Reentry and Recovery from Space. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL39998199W
• Li, Zhiqiang. 2024. Superplastic Forming/Diffusion Bonding Technology of Titanium Alloys: Theories and Applications. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-3909-1
• Liepmann, Hans Wolfgang, and Roshko. 1957. Elements of Gasdynamics, by H.W. Liepmann [and] a. Roshko. Wiley. https://openlibrary.org/works/OL13214987W
• Louis, Gilles. 2022. Dynamics of Aircraft Flight. Wiley. https://doi.org/10.1002/9781119988281
• 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
• Murthy, S. N. B., and Gerald C. Paynter, eds. 1986. Numerical Methods for Engine-Airframe Integration. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.865763
• 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. 2010. Fundamentals of Aircraft and Airship Design: Aircraft Design. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL15909375W
• 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
• 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
• 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
• Reason, James. 1990. Human Error. Cambridge University Press. https://openlibrary.org/works/OL9006915W
• 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
• 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
• Schmidt, Robert Kyle. 2015. Advances in Aircraft Landing Gear. SAE International eBooks. https://doi.org/10.4271/pt-169
• Schmidt, Robert Kyle. 2021. The Design of Aircraft Landing Gear. SAE International eBooks. https://doi.org/10.4271/9780768099430
• Shapiro, Ascher H. 1953. The Dynamics and Thermodynamics of Compressible Fluid Flow. Ronald Press Co. https://openlibrary.org/works/OL5908243W
• Shazly, Mostafa, Vikas Prakash, Susan Draper, and Arun Shukla. 2006. Dynamic Fracture Initiation Toughness at Elevated Temperatures with Application to the New Generation of Titanium Aluminide Alloys. Case Western Reserve Univ. https://ntrs.nasa.gov/citations/20070018030
• Sinha, Nandan K., and N. Ananthkrishnan. 2016. Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods. CRC Press. https://doi.org/10.1201/b15956
• Sinha, Nandan K., and N. Ananthkrishnan. 2021. Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods. CRC Press. https://doi.org/10.1201/9781003096801
• Sorgente, Donato, and Gianfranco Palumbo. 2020. Superplastic Forming. Trans Tech Publications. https://doi.org/10.4028/b-9pgv8g
• 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
• Suharevs, Artūrs. 2022. Research of Aircraft Ground Path Control Devices and Optimization at Takeoff and Landing Stages. RTU Press. https://doi.org/10.7250/9789934227684
• 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
• Thompson, Milton O. 1992. At the Edge of Space: The X-15 Flight Program. Smithsonian Books. https://openlibrary.org/works/OL1994111W
• Truitt, Robert Wesley. 1960. Fundamentals of Aerodynamic Heating. Ronald Press. https://openlibrary.org/works/OL178473W
• Vaughan, Diane. 1996. The Challenger Launch Decision: Risky Technology, Culture, and Deviance at NASA. University of Chicago Press. https://openlibrary.org/works/OL2962391W
• 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
• 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
• 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
• Winchester, Jim. 2005. X Planes Prototypes/Experimental Aircraf. Grange Books. https://openlibrary.org/works/OL8492617W
• Wing Theory in Supersonic Flow. 1969. Elsevier. https://doi.org/10.1016/c2013-0-02078-6
• Wolfe, Tom. 1979. The Right Stuff. https://openlibrary.org/works/OL1925474W
• Zitoune, Rédouane, V. Krishnaraj, and João Paulo Davim. 2013. Machining of Titanium Alloys and Composites for Aerospace Applications. Trans Tech Publications. https://doi.org/10.4028/b-2okvsv

Commercial Sources

• “Armstrong Flight Research Center.” n.d. NASA. Accessed October 25, 2026. https://www.nasa.gov/centers-and-facilities/armstrong/
• Dinius, Dede. 2014. “X-3 Stiletto.” National Aeronautics and Space Administration, February 28. https://www.nasa.gov/aeronautics/x-3-stiletto/
• “NASA History Office.” n.d. Accessed October 24, 2026. https://www.nasa.gov/history/

General Sources

• “NASA Technical Reports Server.” n.d. Accessed October 25, 2026. https://ntrs.nasa.gov/

Tertiary Sources

• “2024 Aluminium Alloy.” 2026. Wikipedia. Last modified February 23, at 03:57 (UTC). https://en.wikipedia.org/w/index.php?title=2024_aluminium_alloy&oldid=1339954462
• “Accelerometer.” 2026. Wikipedia. Last modified June 22, at 23:53 (UTC). https://en.wikipedia.org/w/index.php?title=Accelerometer&oldid=1360682135
• “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
• “Afterburner.” 2026. Wikipedia. Last modified February 2, at 23:39 (UTC). https://en.wikipedia.org/w/index.php?title=Afterburner&oldid=1336290664
• “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
• “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
• “Bell Aircraft.” 2026. Wikipedia. Last modified July 17, at 09:26 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_Aircraft&oldid=1364578865
• “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
• “Biot Number.” 2024. Wikipedia. Last modified December 28, at 19:40 (UTC). https://en.wikipedia.org/w/index.php?title=Biot_number&oldid=1265809960
• “Boundary Layer.” 2026. Wikipedia. Last modified April 24, at 16:14 (UTC). https://en.wikipedia.org/w/index.php?title=Boundary_layer&oldid=1350882651
• “Concorde.” 2026. Wikipedia. Last modified October 20, at 16:30 (UTC). https://en.wikipedia.org/w/index.php?title=Concorde&oldid=1381196080
• “Creep (Deformation).” 2026. Wikipedia. Last modified April 27, at 15:38 (UTC). https://en.wikipedia.org/w/index.php?title=Creep_(deformation)&oldid=1351378240
• “Directional Stability.” 2026. Wikipedia. Last modified March 5, at 03:42 (UTC). https://en.wikipedia.org/w/index.php?title=Directional_stability&oldid=1341800113
• “Douglas Aircraft Company.” 2026. Wikipedia. Last modified July 20, at 14:35 (UTC). https://en.wikipedia.org/w/index.php?title=Douglas_Aircraft_Company&oldid=1365142764
• “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
• “Duralumin.” 2026. Wikipedia. Last modified July 23, at 14:50 (UTC). https://en.wikipedia.org/w/index.php?title=Duralumin&oldid=1365630935
• “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
• “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
• “Ejection Seat.” 2026. Wikipedia. Last modified July 7, at 17:11 (UTC). https://en.wikipedia.org/w/index.php?title=Ejection_seat&oldid=1363029764
• “Euler’s Equations (Rigid Body Dynamics).” 2026. Wikipedia. Last modified June 23, at 23:43 (UTC). https://en.wikipedia.org/w/index.php?title=Euler’s_equations_(rigid_body_dynamics)&oldid=1360843412
• “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
• “Flow Separation.” 2026. Wikipedia. Last modified February 20, at 22:27 (UTC). https://en.wikipedia.org/w/index.php?title=Flow_separation&oldid=1339506051
• “Fourier Number.” 2025. Wikipedia. Last modified November 25, at 18:43 (UTC). https://en.wikipedia.org/w/index.php?title=Fourier_number&oldid=1324128555
• “Heat Equation.” 2026. Wikipedia. Last modified August 3, at 22:18 (UTC). https://en.wikipedia.org/w/index.php?title=Heat_equation&oldid=1367572093
• “Heat Flux.” 2026. Wikipedia. Last modified February 4, at 19:37 (UTC). https://en.wikipedia.org/w/index.php?title=Heat_flux&oldid=1336610285
• “Hypersonic Flight.” 2026. Wikipedia. Last modified July 16, at 04:32 (UTC). https://en.wikipedia.org/w/index.php?title=Hypersonic_flight&oldid=1364374853
• “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
• “Intake Ramp.” 2025. Wikipedia. Last modified October 15, at 12:27 (UTC). https://en.wikipedia.org/w/index.php?title=Intake_ramp&oldid=1316952019
• “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
• “Joseph a. Walker.” 2026. Wikipedia. Last modified January 17, at 20:02 (UTC). https://en.wikipedia.org/w/index.php?title=Joseph_A._Walker&oldid=1333438443
• “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
• “Landing Gear.” 2026. Wikipedia. Last modified July 29, at 13:12 (UTC). https://en.wikipedia.org/w/index.php?title=Landing_gear&oldid=1366675243
• “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
• “Liquid Oxygen.” 2026. Wikipedia. Last modified July 10, at 08:16 (UTC). https://en.wikipedia.org/w/index.php?title=Liquid_oxygen&oldid=1363456540
• “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
• “Load Factor (Aeronautics).” 2026. Wikipedia. Last modified May 25, at 07:04 (UTC). https://en.wikipedia.org/w/index.php?title=Load_factor_(aeronautics)&oldid=1356015221
• “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 SR-71 Blackbird.” 2026. Wikipedia. Last modified July 23, at 15:06 (UTC). https://en.wikipedia.org/w/index.php?title=Lockheed_SR-71_Blackbird&oldid=1365633739
• “Longitudinal Stability.” 2026. Wikipedia. Last modified March 13, at 01:57 (UTC). https://en.wikipedia.org/w/index.php?title=Longitudinal_stability&oldid=1343225347
• “Measurement Uncertainty.” 2026. Wikipedia. Last modified August 2, at 18:11 (UTC). https://en.wikipedia.org/w/index.php?title=Measurement_uncertainty&oldid=1367370535
• “Moment of Inertia.” 2026. Wikipedia. Last modified July 30, at 07:06 (UTC). https://en.wikipedia.org/w/index.php?title=Moment_of_inertia&oldid=1366791098
• “NASA.” 2026. Wikipedia. Last modified July 30, at 01:25 (UTC). https://en.wikipedia.org/w/index.php?title=NASA&oldid=1366759859
• “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
• “National Museum of the United States Air Force.” 2026. Wikipedia. Last modified July 11, at 01:47 (UTC). https://en.wikipedia.org/w/index.php?title=National_Museum_of_the_United_States_Air_Force&oldid=1363573310
• “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
• “North American XB-70 Valkyrie.” 2026. Wikipedia. Last modified July 24, at 06:40 (UTC). https://en.wikipedia.org/w/index.php?title=North_American_XB-70_Valkyrie&oldid=1365752091
• “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
• “Oblique Shock.” 2026. Wikipedia. Last modified July 1, at 19:03 (UTC). https://en.wikipedia.org/w/index.php?title=Oblique_shock&oldid=1362066213
• “Phugoid.” 2026. Wikipedia. Last modified March 25, at 19:48 (UTC). https://en.wikipedia.org/w/index.php?title=Phugoid&oldid=1345375911
• “Prandtl Number.” 2026. Wikipedia. Last modified June 3, at 23:53 (UTC). https://en.wikipedia.org/w/index.php?title=Prandtl_number&oldid=1357669388
• “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
• “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
• “Reynolds Number.” 2026. Wikipedia. Last modified July 2, at 12:53 (UTC). https://en.wikipedia.org/w/index.php?title=Reynolds_number&oldid=1362194896
• “Rocket Engine.” 2026. Wikipedia. Last modified July 23, at 23:20 (UTC). https://en.wikipedia.org/w/index.php?title=Rocket_engine&oldid=1365700012
• “Shock Wave.” 2026. Wikipedia. Last modified July 18, at 23:07 (UTC). https://en.wikipedia.org/w/index.php?title=Shock_wave&oldid=1364857321
• “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
• “Stabilator.” 2025. Wikipedia. Last modified September 28, at 07:24 (UTC). https://en.wikipedia.org/w/index.php?title=Stabilator&oldid=1313811257
• “Stagnation Temperature.” 2025. Wikipedia. Last modified March 15, at 22:24 (UTC). https://en.wikipedia.org/w/index.php?title=Stagnation_temperature&oldid=1280690173
• “Stainless Steel.” 2026. Wikipedia. Last modified July 11, at 06:27 (UTC). https://en.wikipedia.org/w/index.php?title=Stainless_steel&oldid=1363607177
• “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
• “Strain Gauge.” 2026. Wikipedia. Last modified June 23, at 08:27 (UTC). https://en.wikipedia.org/w/index.php?title=Strain_gauge&oldid=1360739250
• “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
• “Takeoff.” 2026. Wikipedia. Last modified July 22, at 14:57 (UTC). https://en.wikipedia.org/w/index.php?title=Takeoff&oldid=1365457052
• “Telemetry.” 2026. Wikipedia. Last modified July 14, at 15:08 (UTC). https://en.wikipedia.org/w/index.php?title=Telemetry&oldid=1364108053
• “Thermal Conductivity and Resistivity.” 2026. Wikipedia. Last modified June 1, at 03:01 (UTC). https://en.wikipedia.org/w/index.php?title=Thermal_conductivity_and_resistivity&oldid=1357166756
• “Thermal Expansion.” 2026. Wikipedia. Last modified July 25, at 15:38 (UTC). https://en.wikipedia.org/w/index.php?title=Thermal_expansion&oldid=1365984240
• “Thermal Stress.” 2025. Wikipedia. Last modified December 20, at 23:05 (UTC). https://en.wikipedia.org/w/index.php?title=Thermal_stress&oldid=1328627048
• “Thermocouple.” 2026. Wikipedia. Last modified July 7, at 18:22 (UTC). https://en.wikipedia.org/w/index.php?title=Thermocouple&oldid=1363042310
• “Ti-6Al-4V.” 2026. Wikipedia. Last modified September 17, at 18:02 (UTC). https://en.wikipedia.org/w/index.php?title=Ti-6Al-4V&oldid=1375422979
• “Titanium.” 2026. Wikipedia. Last modified July 19, at 03:14 (UTC). https://en.wikipedia.org/w/index.php?title=Titanium&oldid=1364893223
• “Titanium Alloys.” 2026. Wikipedia. Last modified June 21, at 13:29 (UTC). https://en.wikipedia.org/w/index.php?title=Titanium_alloys&oldid=1360433891
• “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
• “Turbopump.” 2026. Wikipedia. Last modified July 16, at 23:47 (UTC). https://en.wikipedia.org/w/index.php?title=Turbopump&oldid=1364505469
• “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
• “Wave Drag.” 2025. Wikipedia. Last modified November 22, at 19:16 (UTC). https://en.wikipedia.org/w/index.php?title=Wave_drag&oldid=1323602563
• “Westinghouse J34.” 2026. Wikipedia. Last modified April 30, at 07:52 (UTC). https://en.wikipedia.org/w/index.php?title=Westinghouse_J34&oldid=1351812608
• “Westinghouse J46.” 2026. Wikipedia. Last modified June 14, at 00:49 (UTC). https://en.wikipedia.org/w/index.php?title=Westinghouse_J46&oldid=1359235071
• “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
• “Yield (Engineering).” 2026. Wikipedia. Last modified February 26, at 02:21 (UTC). https://en.wikipedia.org/w/index.php?title=Yield_(engineering)&oldid=1340501409

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