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- 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
- Practical considerations in specific applications of gas-flow interferometry
- Prediction of losses induced by angle of attack in cascades of sharp-nosed blades for incompressible and subsonic compressible flow
- Rotating-stall characteristics of a rotor with high hub-tip radius ratio
- A rapid approximate method for the design of hub shroud profiles of centrifugal impellers of given blade shape
- Rapid radiant-heating tests of multiweb beams
- Some calculations of the lateral response of two airplanes to atmospheric turbulence with relation to the lateral snaking problem
- Pressure rise associated with shock-induced boundary-layer separation
- Development of equipment and of experimental techniques for column creep tests
- Effect of hydrocarbon structure on reaction processes leading to spontaneous ignition
- An automatic viscometer for non-Newtonian materials
- Experimental evaluation of momentum terms in turbulent pipe flow
- Flight investigation at Mach numbers from 0.8 to 1.5 to determine the effects of nose bluntness on the total drag of two fin-stabilized bodies of revolution
- On boattail bodies revolution having minimum wave drag
- One-dimensional calculation of flow in a rotating passage with ejection through a porous wall
- Free-convection effects on heat transfer for turbulent flow through a vertical tube