TRAIL - Technical Report Archive and Image Library

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

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