Browse TRAIL Inventories

Effect of a hot-jet exhaust on pressure distributions and external drag of several afterbodies on a single-engine airplane model at transonic speeds

Dynamic stability of vehicles traversing ascending or descending paths through the atmosphere

Effect of aerodynamic heating on the flutter of a rectangular wing at a Mach number of 2

Effects of nose angle and Mach number on transition on cones at supersonic speeds

Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations

Effects of fixing transition on the transonic aerodynamic characteristics of a wing-body configuration at Reynolds numbers from 2.4 to 12 million

Idealized wings and wing-bodies at a Mach number of 3

Flight investigation of the acceptability of a small side-located controller used with an irreversible hydraulic control system

General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces

Free-flight pressure measurements over a flare-stabilized rocket model with a modified Von Karman nose for Mach numbers up to 4.3

Transonic drag of several jet-noise suppressors

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 4: rotor loss patterns as determined by hot-wire anemometers with rotor operating in a circumferentially uniform inlet flow field

Incipient spin characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA AD 3118

Induction system characteristics and engine surge occurrence for two fighter-type airplanes

Subsonic aerodynamic characteristics up to extreme angles of attack of an airplane model having an unswept wing and a high horizontal tail

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


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