TRAIL - Technical Report Archive and Image Library

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

A correlation by means of transonic similarity rules of the experimentally determined characteristics of 18 cambered wings of rectangular plan form

Design procedure and limited test results for a high solidity, 12-inch transonic impeller with axial discharge

A design and performance study of the nuclear direct-air-cycle supersonic airplane, including the effects of operating temperatures and fuel plate material and thickness

Design and test of mixed-flow impellers 3: design and experimental results for impeller model MFI-2A and comparison with impeller model MFI-1A

Design considerations for mixed-flow centrifugal compressors with high weight-flow rates per unit frontal area

Effect of particle size and stabilizing additives on the combustion properties of magnesium slurry

Analytical studies of the response to longitudinal control of three airplane configurations in landing approaches

An analytical study of sideslip angles and vertical-tail loads in rolling pullouts as affected by some characteristics of modern high-speed airplane configurations

An analytical study of the comparative performance of six air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 2.0

Air-flow characteristics of brazed and rolled wire filter cloth for transpiration-cooled afterburners

Buffeting of a vertical tail on an inclined body at supersonic Mach numbers

Burning rates of single fuel drops and their application to turbojet combustion process

A cascade-general-momentum theory of operation of a supersonic propeller annulus

Analysis of part-speed operation for high-pressure-ratio multistage axial-flow compressors

Static lateral stability characteristics of an airplane model having a 47.7 degree sweptback wing of aspect ratio 6 and the contribution of various model components at a Reynolds number of 4.45 x 10(exp 6)

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