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- Wind-Tunnel Investigation of the Low-Speed Static Longitudinal Characteristics of the Republic RF-84F Airplane
- Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro-Skis: TED No. NACA DE 357
- Time Variation of the Distance Separating Bomb and Dive Bomber Subsequent to Bomb Release
- Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman F9F-6 Airplane: TED No. NACA DE 364
- Thrust Augmentation of a Turbojet Engine at Simulated Flight Conditions by Introduction of a Water-Alcohol Mixture into the Compressor
- Hydrocarbon and nonhydrocarbon derivatives of cyclopropane
- The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements
- Dynamic response at altitude of a turbojet engine with variable area exhaust nozzle
- Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane
- Theoretical and experimental investigation of mufflers with comments on engine-exhaust muffler design
- Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
- Effect of initial mixture temperature on flame speed of methane-air, propane-air, and ethylene-air mixtures
- Two-and three-dimensional unsteady lift problems in high-speed flight
- Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane
- Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane
- Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons
- The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives
- An Investigation of the Effects of a Vortex-Generator Configuration on the Aerodynamic Characteristics of a 1/4-Scale Model of the X-1 Airplane (10-Percent-Thick Wing)
- Axisymmetric supersonic flow in rotating impellers
- Effects of compressibility on the performance of two full-scale helicopter rotors
- Discussion of boundary-layer characteristics near the wall of an axial-flow compressor
- Flight Characteristics of a 1/4-Scale Model of the XFV-1 Airplane (TED No. NACA DE-378)
- Control characteristics at transonic speeds of a linked flap and spoiler on a tapered 45 degrees sweptback wing of aspect ratio 3
- Investigation of engine performance and high-temperature properties of precision-cast turbine blades of high carbon Stellite 21 and controlled grain-size-Stellite 21
- Investigation of flow fluctuations at the exit of a radial-flow centrifugal impeller
- Aerodynamic characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a full-span flap type of control with overhang balance : transonic-bump method
- Flight determination of the longitudinal stability of a 1/10-scale rocket-powered model of the Northrop MX-775A missile at low lift coefficients and Mach numbers from 0.89 to 1.34
- Effects of the spanwise, chordwise and vertical location of an external store on the aerodynamic characteristics of a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Control characteristics of trailing-edge spoilers on untapered blunt trailing-edge wings of aspect ratio 2.7 with 0 degree and 45 degrees sweepback at Mach numbers of 1.41 and 1.96
- Effects of systematically varying the spanwise and vertical location of an external store on the aerodynamic characteristics of an unswept tapered wing of aspect ratio 4 at Mach numbers of 1.41, 1.62, and 1.96
- Full-scale wind-tunnel investigation of the effects of wing modifications and horizontal-tail location on the low-speed static longitudinal characteristics of a 35 degree swept-wing airplane
- Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds
- Investigation of performance of several double-shroud ejectors and effect of variable-area exhaust nozzle on single ejector performance
- Investigation of power extraction characteristics and braking requirements of a windmilling turbojet engine
- Investigation of losses in the XJ35-A-23 two-stage turbine
- Investigation of internal film cooling of exhaust nozzle of a 1000-pound-thrust liquid-ammonia liquid-oxygen rocket
- Investigation of a 10-stage subsonic axial-flow research compressor I : aerodynamic design
- Investigation of heat-transfer coefficients in an afterburner
- Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory
- Variation of pressure limits of flame propagation with tube diameter for various isooctane-oxygen-nitrogen mixtures
- Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds - drag due to lift and lift-drag ratio
- Instrumentation and calibration technique for flight calibration of angle-of-attack systems on aircraft
- Instrumentation of the Ames supersonic free-flight wind tunnel
- Investigation of thrust augmentation using water-alcohol injection on a 5200-pound-thrust axial-flow-type turbojet engine at static sea-level conditions
- Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed II : velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area
- Investigation of stresses due to thermal gradients in typical aircraft structures
- Investigation of vanes immersed in the jet of a solid-fuel rocket motor
- Investigations of air-cooled turbine rotors for turbojet engines 2: mechanical design, stress analysis, and burst test of modified J33 split-disk rotor
- Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed
- Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed I : turbine-design requirements for several engine operating conditions