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- Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine
- Rocket-engine throttling
- Experimental rocket performance with 15 percent fluorine - 85 percent oxygen and JP4
- Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
- Preliminary investigation of the effects of altitude and inlet-pressure distortions on steady-state and surge fuel flow of the J57-P-1 turbojet engine
- Investigation of the effects of body indentation and of wing-plan-form modification on the longitudinal characteristics of a 60 degree swept-wing-body combination at Mach numbers of 1.41, 1.61, and 2.10
- Preliminary investigation of some internal boundary-layer-control systems on a side inlet at Mach number 2.96
- Some effects of propeller operation and location on ability of a wing with plain flaps to deflect propeller slipstreams downward for vertical take-off
- A study of the application of airfoil section data to the estimation of the high-subsonic-speed characteristics of swept wings
- A study of local-pressure fluctuations relative to static-pressure distributions on two-dimensional airfoils at high subsonic Mach numbers
- A Study of the Correlation Between Flight and Wind-Tunnel Buffeting Loads
- Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
- Review of status, methods and potentials of gas-turbine air-cooling
- Thrust and drag characteristics of simulated variable-shroud nozzles with hot and cold primary flows at subsonic and supersonic speeds
- Transonic free-flight investigation of the longitudinal aerodynamic characteristics of a 1/10-scale steel-wing of the Northrop MX-775A missile with leading-edge extensions, inboard trailing-edge flaps, and a speed brake on the vertical tail
- Wing-load measurements of the Bell X-5 research airplane at a sweep angle of 58.7 degrees
- Analytical and experimental study of transient-response characteristics of a turboprop engine
- Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953
- Theoretical pressure distributions for some slender wing-body combinations at zero lift
- Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test
- Aerodynamic heating of rocket-powered research vehicles at hypersonic speeds
- An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations
- Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane
- Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections II : blade-element performance
- Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 II : blade-element performance
- Experimental flutter investigation of a thin unswept wing at transonic speeds
- Experimental performance of fluorine-oxygen with JP4 fuel in a rocket engine
- An experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations
- Experimental investigation of a surge control on a turbojet engine
- Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity
- Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 I : design, over-all performance, and rotating-stall characteristics
- Flight measurements of directional stability to a Mach number of 1.48 for an airplane tested with three different vertical tail configurations
- Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6
- Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers
- Flight Measurements of Elevon Hinge Moments on the XF-92A Delta-Wing Airplane
- 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