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- Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees
- Effect of outer-shell design on performance characteristics of convergent-plug exhaust nozzles
- Effects of several geometric variables on internal performance of short convergent-divergent exhaust nozzles
- Investigation of boattail and base pressures of twin-jet afterbodies at Mach number 1.91
- Effect of area-suction-type boundary-layer control on the landing-approach characteristics of a 35 degree swept-wing fighter
- Comparison of two methods of modulating the throat area of convergent plug nozzles
- Free-spinning-tunnel investigation to determine the effect of spin-recovery rockets and thrust simulation on the recovery characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA DE 392
- The effects of flexibility on the longitudinal and lateral directional response of a large airplane
- A comparison of the maneuvering performance of a monowing versus a cruciform missile
- The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds
- The effect of blunt-trailing-edge elevons on the longitudinal and lateral handling qualities of the semitailless airplane
- Effect of rotor leading-edge sweepback on performance of a transonic turbine
- Description and bibliography of NACA research on wing controls: January 1946 - February 1955
- Design and performance of a 1400-foot-per-second-tip-speed supersonic compressor rotor
- Effects of spanwise location of sweep discontinuity on the low-speed longitudinal stability characteristics of a complete model with wings of M and W plan form
- Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form
- A method for evaluating the loads and controllability aspects of the pitch-up problem
- Application of non-afterburning turbojets to supersonic flight
- Application of statistical theory to beam-rider guidance in the presence of noise 1: Wiener filter theory
- Application of wing-body theory to drag reduction at low supersonic speeds
- Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2
- Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98
- Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures
- Performance of four experimental high btu-per-gallon fuels in a single turbojet combustor
- Performance of a supersonic compressor with swept and tilted diffuser blades
- Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles
- Some design implications of the effects of aerodynamic heating
- Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory
- A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
- Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic
- Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines 4: coolant-flow requirements and performance of engines using air-cooled corrugated-insert blades
- Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
- Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip
- Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90
- A variable-geometry axisymmetric supersonic inlet with telescoping centerbody
- Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25
- Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase
- Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds
- A study of conical camber for triangular and sweptback wings
- Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight
- Analysis of Low-Temperature Nuclear-Powered Ram-Jet Missile for High Altitudes
- Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces
- Transportation of liquid fluorine
- Model investigation of the effect of mounting hydro-skis on shock absorbers
- Lift, drag, and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered model having a tapered unswept wing of aspect ratio 3 and inline tail surfaces
- Performance characteristics of hemispherical target-type thrust reversers
- Performance of YJ73-GE-3 turbojet engine in altitude test chamber
- Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane
- An investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic and loading characteristics in sideslip on a 45 degree sweptback, untapered tail assembly as determined from force tests and integrated vertical-tail span loadings
- The effect of fluid injection on the compressible turbulent boundary layer : preliminary tests on transpiration cooling of a flat plate