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- Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 employing high-velocity blowing over the leading- and trailing-edge flaps
- Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices
- Normal component of induced velocity for entire field of a uniformly loaded lifting rotor with highly swept wake as determined by electromagnetic analog
- Flow induced by a rotor in power-on vertical descent
- Effect of favorable pressure gradients on transition for several bodies of revolution at Mach 3.12
- Effect of environments of sodium hydroxide, air, and argon on the stress-rupture properties of nickel at 1500 F
- Effect of fiber orientation in races and balls under rolling-contact fatigue conditions
- Effect of control trailing-edge thickness or aspect ratio on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds
- Effect of flow incidence and Reynolds number on low-speed aerodynamic characteristics of several noncircular cylinders with applications to directional stability and spinning
- Effect of fuel-orifice diameter on performance of heptane-oxygen rocket-engines
- Creep of aluminum-copper alloys during age hardening
- Corrosion resistance of nickel alloys in molten sodium hydroxide
- Drag minimization for wings in supersonic flow, with various constraints
- Drop-size distributions for impinging-jet breakup in airstreams simulating the velocity conditions in rocket combustors
- Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
- Effect of oxygen recombination on one-dimensional flow at high Mach numbers
- Effect of precipitate particles on creep of aluminum-copper alloys during age hardening
- Effect of pressure and duct geometry on bluff-body flame stabilization
- Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
- Analytical relation for wake momentum thickness and diffusion ratio for low-speed compressor
- Analytical investigation of multistage-turbine efficiency characteristics in terms of work and speed requirements
- An analytical study of turbulent and molecular mixing in rocket combustion
- Effect of angle of attack and thickness on aerodynamic coefficients of a rigid wing oscillating at very low frequencies in two-dimensional supersonic flow
- Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
- Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01
- An Analysis of Ramjet Engines Using Supersonic Combustion
- Analysis of stresses and deflections in a disk subjected to gyroscopic forces
- Analytical investigation of acceleration restriction in a fighter airplane with an automatic control system
- Compressible laminar flow and heat transfer about a rotating isothermal disk
- Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane
- Canard hinge moments and longitudinal stability of a 1/7-scale model of the Convair B-58 external store in a free-flight investigation at Mach numbers from 0.94 to 2.58 : COORD No. AF-204
- Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine
- Central automatic data processing system
- Component performance investigation of L71 experimental turbine X : effect of first-stator adjustment; internal flow conditions of J71-97 turbine with 132-percent-design stator area
- Composition and thermodynamic properties of air in chemical equilibrium
- Skin-friction measurements in incompressible flow
- Analysis of effects of interceptor roll performance and maneuverability on success of collision-course attacks
- Boundary-induced downwash due to lift in a two-dimensional slotted wind tunnel
- Boundary-layer stability diagrams for electrically conducting fluids in the presence of a magnetic field
- Effect of lubricant base stock on rolling-contact fatigue life
- Effect of prior air force over temperature operation on life of J47 buckets evaluated in a sea-level cyclic engine test
- Effect of wall cooling on inlet parameters of a scoop operating in a turbulent boundary layer on a flat or conical surface for Mach numbers 2 to 10
- An evaluation of the effects of flexibility on wing strains in rough air for a large swept-wing airplane by means of experimentally determined frequency-response functions with an assessment of random-process techniques employed
- Experimental ablation cooling
- Effectiveness of various protective coverings on magnesium fins at Mach number 2.0 and stagnation temperatures up to 3,600 R
- Effects of nose and afterbody modifications on aerodynamic characteristics of a body with and without a vertical tail at a Mach number of 2.01
- Effects of Mach number and wall-temperature ratio on turbulent heat transfer at Mach numbers from 3 to 5
- Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives
- Effect of overheating on creep-rupture properties of M-252 alloy
- The effect of moment-of-area-rule modifications on the zero-lift drag of three wing-body combinations