Browse TRAIL Inventories

Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05

Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957

Theoretical combustion performance of several high-energy fuels for ramjet engines

Aerodynamic heating of blunt nose shapes at Mach numbers up to 14

A wind-tunnel investigation of several wingless missile configurations at supersonic speeds

Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane

Tests of ring-stiffened circular cylinders subjected to a transverse shear load

The adhesion of molten boron oxide to various materials

Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge

Tracking performance of a swept-wing fighter with a director-type radar fire-control system and scope presentation

Torque-speed characteristics for high-specific-work turbines

Investigation of two bluff shapes in axial free flight over a Mach number range from 0.35 and 2.15

Limited investigation of noise suppression by injection of water into exhaust of afterburning jet engine

Limited tests of molybdenum coated with molybdenum disilicide in a supersonic heated-air jet and brief description of the coating facility

Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin, low-aspect-ratio, unswept, untapered, semispan wing and on the wing with leading and trailing-edge flaps

Low tire friction and cornering forces on a wet surface

Prandtl-Meyer expansion of chemically reacting gases in local chemical and thermodynamic equilibrium

Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Performance at low speeds of compressor rotors having low-cambered NACA 65-series blades with high inlet angles and low solities

A performance analysis of methods for handling excess inlet flow at supersonic speeds

Rate of reaction of gaseous fluorine with water vapor at 35 degrees C

Stability investigation of a blunt cone and a blunt cylinder with a square base at Mach numbers from 0.64 to 2.14

Performance of a 28-inch ramjet utilizing gaseous hydrogen at a Mach number of 3.6, angles of attack up to 12 degree, and pressure altitudes up to 110,000 feet

Pressure distributions at transonic speeds for parabolic-arc bodies of revolution having fineness ratios of 10, 12, and 14

Pressure distributions at transonic speeds for slender bodies having various axial locations of maximum diameter

Preliminary investigation of graphite, silicon carbide, and several polymer-glass-cloth laminates in a Mach number 2 air jet at stagnation temperatures of 3,000 F and 4,000 F

Preliminary investigation of land-water operation with a 1/10-scale model of a jet airplane equipped with hydro-skis

Stability of propane-air flames in vortex flow

Stagnation-point heat transfer to blunt shapes in hypersonic flight, including effects of yaw

Influence of heat treatment on microstructure and high-temperature properties of nickel-base precipitation-hardening alloy

Analysis of the creep behavior of a square plate loaded in edge compression

Effect of inlet air distortion on steady-state performance of an axial-flow turbojet engine

Effect of inlet aspect ratio on the starting and pressure recovery characteristics of a rectangular swept scoop inlet tested at a Mach number of 3.1

Force and pressure measurements at transonic speeds for several bodies having elliptical cross sections

Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles

Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying

Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively

Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5

Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants

Experimental investigation of axial and normal force characteristics of skewed nozzles

Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing

Experimental investigation of an impulse-type supersonic compressor rotor having a turning of 73 degrees at the mean radius

Jet effects on the base drag of a cylindrical afterbody with extended nozzles

Dilution of liquid oxygen when nitrogen is used for pressurization

Performance of an All-Internal Conical Compression Inlet with Annular Throat Bleed at Mach Number 5.0

A numerical method for evaluating wave drag

Physical characteristics and test conditions of an ethylene-heated high-temperature jet

Observations of turbulent-burst geometry and growth in supersonic flow

Some effects of flow spoilers and of aerodynamic balance on the oscillating hinge moments for a swept fin-rudder combination in a transonic wind tunnel

Preliminary performance data obtained in a full-scale, free-jet investigation of a side-inlet supersonic diffuser


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