Browse TRAIL Inventories

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


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