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- Photographic study of combustion in a rocket engine I : variation in combustion of liquid oxygen and gasoline with seven methods of propellant injection
- Extension of Useful Operating Range of Axial-Flow Compressors by Use of Adjustable Stator Blades
- 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
- Study of effects of sweep on the flutter of cantilever wings
- A fuel-distribution control for gas-turbine engines
- Investigation of interaction effects arising from side-wall boundary layers in supersonic wind-tunnel tests of airfoils
- Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics
- Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel II : the effect of constant-chord leading- and trailing-edge flaps on the low-speed characteristics of the wing
- Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel I : characteristics of a plain wing
- Investigation of flow conditions and the nature of the wall-constriction effect near and at choking by means of the hydraulic analogy
- An investigation of submerged air inlets on a 1/4-scale model of a typical fighter-type airplane
- Investigation of performance of single-stage axial-flow compressor using NACA 5509-34 blade section
- Investigation of performance of Bumblebee 18-inch ram jet with a can-type flame holder
- Method for stress analysis of a swept propeller
- Measurements of the chordwise pressure distributions over the wing of the XS-1 research airplane in flight
- Performance of several air ejectors with conical mixing sections and small secondary flow rates
- NACA Transonic Wing-Tunnel Test Sections
- Preliminary correlation of the effect of compressibility on the location of the section aerodynamic center at subcritical speeds
- Preliminary investigation of combustion in flowing gas with various turbulence promoters
- Preliminary results of natural icing of an axial-flow turbojet engine
- Preliminary survey of the aircraft fire problem
- Wind-tunnel investigation of transonic aileron flutter of a semispan wing model with an NACA 23013 section
- Langley full-scale tunnel investigation of the characteristics in yaw of a trapezoidal wing of aspect ratio 4 with circular-arc airfoil sections
- Low-speed investigation of a small triangular wing of aspect ratio 2.0 III : static stability with twin vertical fins
- Gas-turbine-engine operation with variable-area fuel nozzles
- Ice protection of turbojet engines by inertia separation of water I : alternate-duct system
- Ice protection of turbojet engines by inertia separation of water III : annular submerged inlets
- Ice protection of turbojet engines by inertia separation of water II : single-offset-duct system
- A limit pressure coefficient and an estimation of limit forces on airfoils at supersonic speeds
- Determination of average heat-transfer coefficients for a cascade of symmetrical impulse turbine blades 1: heat transfer from blades to cold air
- Design and performance of experimental axial-discharge mixed-flow compressor II : performance of impeller
- Aerodynamic characteristics of a two-blade NACA 10-(3)(12)-03 propeller
- Analysis of parameters for thrust control of a turbojet engine equipped with air-inlet throttle and variable-area exhaust nozzle
- Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller
- The effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing
- Evaluation of gust and draft velocities from flights of F-61C airplanes within thunderstorms August 21, 1947 to August 25, 1947 at Clinton County Army Air Field, Ohio
- Evaluation of gust and draft velocities from flights of P-61C airplanes within thunderstorms July 31, 1947 to August 6, 1947 at Clinton County Army Air Field, Ohio
- Evaluation of gust and draft velocities from flights of an AT-6 airplane within cumulus clouds July 1, 1947 to July 22, 1947 at Clinton County Army Air Field, Ohio
- Experimental data concerning the effect of high heat-input rates on the pressure drop through radiator tubes
- Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 II : maximum thickness at midchord
- Static longitudinal aerodynamic characteristics of a 52 degree sweptback wing of aspect ratio 2.88 at Reynolds numbers from 2,000,000 to 11,000,000
- Study of stress states in gas-turbine disk as determined from measured operating-temperature distributions
- Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel III : the effectiveness and hinge moments of a skewed wing-tip flap
- Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel II : the effectiveness and hinge moments of a constant-chord plain flap
- Effect of a nacelle on the low-speed aerodynamic characteristics of a swept-back wing
- Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at several angles of attack
- Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift
- Tank spray tests of a jet-powered model fitted with NACA hydro-skis
- Tests of the NACA 64(sub 1)-012 and 64(sub 1)A012 airfoils at high subsonic Mach numbers
- Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller