TRAIL - Technical Report Archive and Image Library

Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models

Wing-flow measurements of longitudinal stability and control characteristics of a supersonic airplane configuration having a 42.8 degree sweptback circular arc wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces

Approximate relative-total-pressure losses of an infinite cascade of supersonic blades with finite leading-edge thickness

An experimental investigation of a jet-engine nacelle in several positions on a 37.25 degree swept-back wing

Experimental investigation of a flat plate paddle jet vane operating on a rocket jet

Low-temperature ignition-delay characteristics of several rocket fuels with mixed acid in modified open-cup-type apparatus

Investigation of centrifugal compressor operated as a centripetal refrigeration turbine

Cooling of ram jets and tail-pipe burners : analytical method for determining temperatures of combustion chamber having annular cooling passage

The effects of compressibility on the pressures on a body of revolution and on the aerodynamic characteristics of a wing-nacelle combination consisting of the body of revolution mounted on a swept-back wing

A comparison of the aerodynamic characteristics at transonic speeds of four wing-fuselage configurations as determined from different test techniques

The effect of aspect ratio on the subsonic aerodynamic characteristics of wings with NACA 65(sub 1)-210 sections

Effect of blade-root fit and lubrication on vibration characteristics of ball-root-type axial-flow-compressor blades

A description of the design of highly swept propeller blades

Effect of compressor-outlet bleedoff on turbojet-engine performance

Application of blade cooling to gas turbines

Investigation of downwash and wake characteristics at a Mach number of 1.53 3: swept wings

Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: wing and fuselage pressure distribution

Turbojet combustion efficiency at high altitudes

Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds

Comparison of outside-surface heat-transfer coefficients for cascades of turbine blades

Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids

Aeronautical study of a wing-fuselage combination employing a wing swept back 63 degrees: Characteristics at supersonic speeds of a model with the wing twisted and cambered for uniform load

Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers

Investigation of effects of inlet-air velocity distortion on performance of turbojet engine

Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds

Wind-tunnel investigation at Mach numbers of 2.0 and 2.9 of several configurations of a supersonic ram-jet test vehicle

Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane

Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees

Factors in selecting fuels for gas-turbine powered aircraft

Extension of boundary-layer heat-transfer theory to cooled turbine blades

Experimental investigation of thrust augmentation of 4000-pound-thrust axial-flow-type turbojet engine by interstage injection of water-alcohol mixtures in compressor

Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by bleedoff

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: effect of Reynolds number at supersonic Mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load

Altitude performance characteristics of tail-pipe burner with variable-area exhaust nozzle

Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine

Effects of boundary-layer control on the longitudinal characteristics of a 45 degrees swept-forward wing-fuselage combination

Altitude-wind-tunnel investigation of turbine performance in J47 turbojet engine

A preliminary flight investigation of the effects of vortex generators on separation due to shock

Longitudinal characteristics of two 47.7 degree sweptback wings with aspect ratios of 5.1 and 6.0 at Reynolds numbers up to 10 x 10(exp 6)

Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)

Supplementary analysis of the dynamic lateral stability characteristics of the Bell X-2 airplane as affected by variations in mass and aerodynamic parameters

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered

Free-flight investigation at transonic and supersonic speeds of the rolling effectiveness of a partial-span aileron on an inversely tapered sweptback wing

On the Formation of Shock Waves in Subsonic Flows With Local Supersonic Velocities

Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.90 to 1.95 of 1/14-Scale Model of the Northrop MX-775B Pilotless Aircraft with Small Body

Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine

Further experiments on the flow and heat transfer in a heated turbulent air jet

Fundamental effects of aging on creep properties of solution-treated low-carbon n-155 alloy

Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design

Horizontal tail loads in maneuvering flight

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