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- Pressure distribution at low speed on a 1/4-scale Bell X-5 airplane model
- Load distribution over a fuselage in combination with a swept wing at small angles of attack and transonic speeds
- Liquid-fuel-distribution and fuel-state effects on combustion performance of a single tubular combustor
- Flame velocities over a wide composition range for pentane-air, ethylene-air, and propyne-air flames
- The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight
- Full-scale investigation of cooling shroud and ejector nozzle for a turbojet engine: afterburner installation
- Free-spinning tunnel investigation of the 1/21-scale model of the Chance Vought F7U-3 airplane: TED No. NACA DE 362
- Optical methods involving light scattering for measuring size and concentration of condensation particles in supercooled hypersonic flow
- Correlation of analog solutions with experimental sea-level transient data for controlled turbine-propeller engine, including analog results at altitudes
- Analytical investigation of flow through high-speed mixed-flow turbine
- Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85
- Characteristics of a transonic test section with various slot shapes in the Langley 8-foot high-speed tunnel
- An analysis of base pressure at supersonic velocities and comparison with experiment
- Evaluation of the reduced-mass method of representing wing-lift effects in free-fall drop tests of landing gears
- System analyses and autopilot design for automatic roll stabilization of a supersonic pilotless aircraft
- A simplified instrument for recording and indicating frequency and intensity of icing conditions encountered in flight
- A study of effects of viscosity on flow over slender inclined bodies of revolution
- A small-deflection theory for curved sandwich plates
- The static longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing canard model having a triangular control
- Summary of Methods for Calculating Dynamic Lateral Stability and Response and for Estimating Lateral Stability Derivatives
- Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds
- Hydrodynamic investigation of a 1/13-scale model of the consolidated vultee skate 7 seaplane equipped with twin hydro-skis : TED No. NACA DE 342
- Effects of horizontal-tail position, area, and aspect ratio on low-speed static longitudinal stability and control characteristics of a 60 degrees triangular-wing model having various triangular-all-movable horizontal tails
- Investigation at zero angle of attack of a 16-inch ram jet engine in 8- by 6-foot supersonic wind tunnel
- Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine
- Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine
- Altitude-ignition limit of a turbojet engine using a condenser-discharge ignition system
- Wire cloth as porous material for transpiration-cooled walls
- A wind-tunnel investigation of the aerodynamic characteristics of a full-scale sweptback propeller and two related straight propellers
- Wind-tunnel investigation of the aerodynamic characteristics of a 1/15-scale model of the Northrop MX-775A missile
- Two-dimensional cascade investigation of the maximum exit tangential velocity component and other flow conditions at the exit of several turbine blade designs at supercritical pressure ratios
- A two-dimensional cascade study of the aerodynamic characteristics of a turbine-rotor blade suitable for air cooling
- Theoretical study of some methods for increasing the smoothness of flight through rough air
- Low-speed wind-tunnel investigation of lateral control characteristics of a 60 degrees triangular-wing model having half-delta tip controls
- Schlieren investigation of the wing shock-wave boundary-layer interaction in flight
- Steady-state engine windmilling and engine speed decay characteristics of an axial-flow turbojet engine
- Effect of initial mixture temperature on flame speed of methane-air, propane-air and ethylene-air mixtures
- Flying qualities of a high-performance personal-owner airplane
- Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) : body of revolution with near-parabolic forebody and cylindrical afterbody
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Experimental investigation of an 0.8 hub-tip radius-ratio,nontwisted-rotor-blade turbine
- Preliminary investigation of the pressure fluctuations in the wakes of two-dimensional wings at low angles of attack
- Jet effects on pressures and drags of bodies
- Preliminary investigation of use of conical flow separation for efficient supersonic diffusion
- Applicability of the hypersonic similarity rule to pressure distributions which include the effects of rotation for bodies of revolution at zero angle of attack
- Experimental investigation of a 16-inch impulse-type supersonic-compressor rotor
- Effects of Reynolds number on the aerodynamic characteristics of a delta wing at Mach number of 2.41
- Experimental investigation of air-cooled turbine blades in turbojet engine 9: evaluation of the durability of noncritical rotor blades in engine operation
- Experimental investigation of air-cooled turbine blade in turbojet engine 8: rotor blades with capped leading edges
- Effects of double-slotted flaps and leading-edge modifications on the low-speed characteristics of a large-scale 45 degrees swept-back wing with and without camber and twist