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- A study of the radiation from laminar and turbulent open propane-air flames as a function of flame area, equivalence ratio, and fuel flow rate
- Study of the physical properties of petrolatum-stabilized magnesium-hydrocarbon slurry fuels
- Study of the attack of an automatically controlled interceptor on a maneuvering bomber with emphasis on proper coordination of lift-acceleration and roll-angle commands during rolling maneuvers
- Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet
- A revised gust-load formula and a re-evaluation of v-g data taken on civil transport airplanes from 1933 to 1950
- Rocket-model investigation of the longitudinal stability and drag characteristics of a 1/10-scale model of the Convair XF2Y-1 airplane having open ducts and the elevons deflected upward 3.5 degrees : TED No. NACA DE 375
- Analytical and experimental studies of a divided-flow ram-jet combustor
- Analysis of the turbojet for propulsion of supersonic bombers
- Analytical determination of effect of turbine cooling-air-impeller performance on engine performance and comparison of experimentally determined performance of impellers with and without inducer vanes
- Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bumb method
- Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates
- Experimental influence coefficients for the deflection of the wing of a full-scale, swept-wing bomber
- Impingement of water droplets on wedges and double-wedge airfoils at supersonic speeds
- Preliminary investigation of performance of variable-throat extended-plug-type nozzles over wide range of nozzle pressure ratios
- An Investigation of the Hydrodynamic Characteristics of a 1/10-Size Powered Dynamic Model of the Martin M-267 Patrol-Type Seaplane with Two Forebody Configurations: TED No. NACA DE 376
- Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02
- Investigation of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at positive and negative thrust at Mach numbers up to 0.90, including some aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade, single-rotat
- Effect of plug design on performance characteristics of convergent-plug exhaust nozzles
- Effect of divergence angle on the internal performance characteristics of several conical convergent-divergent nozzles
- Preliminary investigation of several target-type thrust-reversal devices
- Investigation of noise field and velocity profiles of an afterburning engine
- Effect of several jet-engine air-inlet configurations on the low-speed static longitudinal stability characteristics and quantity flow of a 1/6-scale model of the MX-1764 airplane
- The effect of several jet-engine air-inlet configurations on the low-speed static lateral stability characteristics of a 1/6-scale model of the MX-1764 airplane
- Effect of jet-nozzle-expansion ratio on drag of parabolic afterbodies
- Design and experimental investigation of light-weight bases for air-cooled turbine rotor blades
- Effects of secondary-air flow on annular base force of a supersonic airplane
- Effects of rigid spoilers on the two-dimensional flutter derivatives of airfoils oscillating in pitch at high subsonic speeds
- The aerodynamic characteristics at transonic speeds of a model with a 45 degree sweptback wing, including the effect of leading edge slats and a low horizontal tail
- Analysis and construction of design charts for turbines with downstream stators
- The application of a simplified lifting-surface theory to the prediction of the rolling effectiveness of plain spoiler ailerons at subsonic speeds
- Application of several methods for determining transfer functions and frequency response of aircraft from flight data
- An experimental investigation of hollow turbine blades for expandable jet engines
- Axial-load fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several laboratories
- The effect of ground on the low-speed aerodynamics control, and control hinge-moment characteristics of a delta-wing-fuselage model with trailing-edge controls
- Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment
- Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98
- A wind-tunnel investigation of bomb release at a Mach number of 1.62
- Force, moment, and pressure characteristics of several annular nose inlets at Mach number 3.85
- Performance of a supersonic rotor having high mass flow
- Investigation of an on-off inlet shock-position control on a 16-inch ram-jet engine
- Investigation of thrust and drag characteristics of a plug-type exhaust nozzle
- Thrust and drag characteristics of a convergent-divergent nozzle with various exhaust jet temperatures
- High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging
- Investigation of effect of increased diffusion of rotor-blade suction-surface velocity on performance of transonic turbine
- Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.50 to 2.16
- Theoretical performance characteristics of sharp-lip inlets at subsonic speeds
- Wind-tunnel investigation at low speed of static and yawing characteristics of a 0.085-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA DE 392
- Wind-tunnel investigation at low speed of the yawing stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane: TED No. NACA DE 389
- Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane: TED No. NACA DE 389
- Comparison at supersonic speeds of translating spike inlets having blunt- and sharp-lip cowls