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• Low-speed investigation of the effects of angle of attack on the pressure recovery of a circular nose inlet with several lip shapes
• Measurements of free-space oscillating pressures near a propeller at flight Mach numbers to 0.72
• Measurements of the effects of finite span on the pressure distribution over double-wedge wings at Mach numbers near shock attachment
• A fibrous-glass compact as a permeable material for boundary-layer control applications using area suction
• Helicopter instrument flight and precision maneuvers as affected by changes in damping in roll, pitch, and yaw
• Heat transfer at the forward stagnation point of blunt bodies
• Heat loss from yawed hot wires at subsonic Mach numbers
• A note on the drag due to lift of rectangular wings of low aspect ratio
• On the small-disturbance iteration method for the flow of a compressible fluid with application to a parabolic cylinder
• On the Kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow
• Creep and creep-rupture characteristics of some riveted and spot-welded lap joints of aircraft materials
• Criterions for prediction and control of ram-jet flow pulsations
• Determination of inflow distributions from experimental aerodynamic loading and blade-motion data on a model helicopter rotor in hovering and forward flight
• Burning velocities of various premixed turbulent propane flames on open burners
• Comparison between theoretical and experimental stresses in circular semimonocoque cylinders with rectangular cutouts
• Analytical determination of effect of water injection on power output of turbine-propeller engine
• Compressible laminar boundary layer and heat transfer for unsteady motions of a flat plate
• The compressible laminar boundary layer with heat transfer and arbitrary pressure gradient
• Analysis of errors introduced by several methods of weighting nonuniform duct flows
• The effect of Reynolds number on the stalling characteristics and pressure distributions of four moderately thin airfoil sections
• Effect of trailing-edge thickness on lift at supersonic velocities
• Experiments with a rotating-cylinder viscometer at high shear rates
• An evaluation of non-Newtonian flow in pipe lines
• Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
• The effects of various parameters, including mach number, on propeller-blade flutter with emphasis on stall flutter
• Experimental investigation of misaligning couples and eccentricity at ends of misaligned plain bearings
• Estimation of inlet lip forces at subsonic and supersonic speeds
• An experimental comparison of the Lagrangian and Eulerian correlation coefficients in homogeneous isotropic turbulence
• Experimental investigation of blade flutter in an annular cascade
• Experiments on turbulent flow through channels having porous rough surfaces with or without air injection
• The problem of reducing the speed of a jet transport in flight
• Sound propagation into the shadow zone in a temperature-stratified atmosphere above a plane boundary
• A statistical study of wing lift at ground contact for four transport airplanes
• Static stability of fuselages having a relatively flat cross section
• 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
• Propagation of a free flame in a turbulent gas stream
• Similar Solutions for the Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient
• Summary of results of a wind-tunnel investigation of nine related horizontal tails
• A self-excited, alternating-current, constant-temperature hot-wire anemometer
• Effects of sweep and angle of attack on boundary-layer transition on wings at Mach number 4.04
• Hovering flight tests of a four-engine-transport vertical take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream
• Effect of exhaust-nozzle ejectors on turbojet noise generation
• Flame propagation limits of propane and n-pentane in oxides of nitrogen
• An experimental study of orifice coefficients, internal strut pressures, and loads on a small oleo-pneumatic shock strut
• Summary evaluation of toothed-nozzle attachments as a jet-noise-suppression device
• Summary of laminar-boundary-layer solutions for wedge-type flow over convection-and transpiration-cooled surfaces
• Summary of derived gust velocities obtained from measurements within thunderstorms
• The transonic characteristics of 36 symmetrical wings of varying taper, aspect ratio, and thickness as determined by the transonic-bump technique
• The transonic characteristics of 22 rectangular, symmetrical wing models of varying aspect ratio and thickness
• The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique