TRAIL - Technical Report Archive and Image Library

Investigation of a 10-stage subsonic axial-flow research compressor 3: investigation of rotating stall, blade vibration and surge at low and intermediate compressor speeds

Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages II : preliminary analysis of over-all performance

Initial flutter tests in the Langley transonic blowdown tunnel and comparison with free-flight flutter results

An investigation of three NACA 1-series nose inlets at subsonic and transonic speeds

A flight comparison of a submerged inlet and a scoop inlet at transonic speeds

Investigation of water-spray cooling of turbine blades in a turbojet engine

Investigation to determine effects of rectangular vortex generators on the static pressure drop through a 90 degrees circular elbow

An investigation of some factors affecting the drag of relatively large nonlifting bodies of revolution in a slotted transonic wind tunnel

Investigation of Spoiler Ailerons with and Without a Gap Behind the Spoiler on a 45 Degree Sweptback Wing-Fuselage Combination at Mach Numbers from 0.60 to 1.03

Investigation of low-pressure performance of experimental tubular combustors differing in air-entry-hole geometry

Vapor pressures of concentrated nitric acid solutions in the composition range 83 to 97 percent nitric acid 0 to 6 percent nitrogen dioxide, 0 to 15 percent water, and in the temperature range 20 to 80 C

Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds

Stability and control characteristics at low speed of a modified 1/10-scale model of the MX-1554A design

Stability and control characteristics at low speed of a 1/10-scale model of MX-1554A design

Jet effects on flow over afterbodies in supersonic stream

Evaluation of effects of random permeability variations on transpiration-cooled surfaces

Effect of circumferential location on angle of attack performance of twin half-conical scoop-type inlets mounted symmetrically on the RM-10 body of revolution

An investigation of high-frequency combustion oscillations in liquid-propellant rocket engines

An experimental investigation of boundary interference on force and moment characteristics of lifting models in the Langley 16- and 8-foot transonic tunnels

Effect of uneven air-flow distribution to the twin inlets of an axial-flow turbojet engine

Performance of separation nose inlets at Mach number 5.5

Orthotoluidine and triethylamine in rocket engine applications

Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with a variable-incidence triangular wing and an all-movable horizontal tail

Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 3 triangular wing and an all-movable horizontal tail: Longitudinal and lateral characteristics

Preliminary comparison of 17- and 75-millimeter-bore cageless cylindrical roller bearings with conventional cylindrical roller bearings at high speeds

Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54

Preliminary flight measurements of the dynamic longitudinal stability characteristics of the Convair XF-92A delta-wing airplane

Preliminary investigation of a variable-area auxiliary air-intake system at Mach numbers from 0 to 1.3

Preliminary experimental investigation of transpiration cooling for an afterburner with a sintered, porous stainless-steel combustion-chamber wall

Pressure distribution at Mach numbers up to 0.90 on a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10, including the effects of fences

Langley full-scale-tunnel tests of the Custer Channel Wing airplane

Lift and Drag Characteristics of the Bell X-5 Research Airplane at 59 Degrees Sweepback for Mach Numbers from 0.60 to 1.03

The lateral control characteristics of constant-percent-chord trailing-edge elevons on a pointed wing of aspect ratio 2 at Mach numbers up to 0.95

Loads experienced in flights of two swept-wing research airplanes in the angle-of-attack range of reduced stability

Low-lift drag and stability data from rocket models of a modified-delta-wing airplane with and without external stores at Mach numbers from 0.8 to 1.36

Longitudinal flight characteristics of the Bell X-5 research airplane at 59 degree sweepback with modified wing roots

Longitudinal-control effectiveness and downwash characteristics at transonic speeds of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method

Measurements of fluctuating pressures on a 1/4-scale model of the X-1 airplane with a 10-percent-thick wing in the Langley 16-foot transonic tunnel

Measurement and analysis of turbulent flow containing periodic flow fluctuations

Evaluation of ethyl ether as an ignition aid for turbojet engine fuels

An experimental investigation of the applicability of the hypersonic similarity law to bodies of revolution

Effect of engine and control limits on steady-state and transient performance of turbojet engine with variable-area exhaust nozzle

Effect of drawbar upstream location on air velocity distribution at the inlet face of reactor segment designed by the General Electric Company

The effect of nacelle combinations and size on the zero-lift drag of a 45 degree sweptback wing and body configuration as determined by free-flight tests at Mach numbers between 0.8 and 1.3

Effect of flame-holder design on altitude performance of louvered-liner afterburner

Effect of fuels on combustion efficiency of 5-inch ram-jet-type combustor

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