PRESSURE AND HEAT-TRANSFER MEASUREMENTS ON THE FLAT FACE OF A BLUNTED 10 DEG HALF-CONE BODY SEMIDISK AT A MACH NUMBER OF 6.15
Pressure and heat-transfer measurements of flat face of blunted 10 deg half-cone body or semidisk at mach 6.15
HALF-CONE↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Effects of transverse center-of-gravity displacement, afterbody geometry, and front-face curvature on the aerodynamic characteristics of Mercury-type models at a Mach number of 5.5
Effects of transverse barycenter displacement, conical afterbody, curved front face on mercury capsule supersonic aerodynamic characteristics
BARYCENTER↗
Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01
Effect of canted forward faces on static longitudinal stability characteristics of escape and exit configurations of Mercury capsule at Mach 2.01
LONGITUDINAL STABILITY AND CONTROL↗
Effect of face-sheet stiffness on buckling of curved plates and cylindrical shells of sandwich construction in axial compression
Effect of face sheet flexural stiffness on buckling of elastic curved plates and cylindrical shells of sandwich construction in axial compression
CYLINDRICAL SHELL↗
A transonic investigation of base pressures associated with shallow three-dimensional rearward-facing steps
Transonic tests of base pressures associated with shallow three-dimensional rearward-facing steps
BASE PRESSURE↗
Development of large size bellows face type seals for liquid oxygen and oxygen/hydrogen hot gas service at moderate to high pressures
Four-element dynamic face seal for positive separation of cryogenic coolant and hot gas in turbopump, using neutral gaseous nitrogen purge
CRYOGENIC FLUID↗
Effect of face-sheet stiffness on buckling of cylindrical shells of sandwich construction
Effect of face sheet stiffness on buckling of cylindrical shells of sandwich construction
CYLINDRICAL SHELL↗
Heat-transfer and pressure distributions on a flat-face rounded-corner body of revolution with and without a flap at a Mach number of 8
Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg
FLAT SURFACE↗
Free-flight aerodynamics of a blunt-faced reentry shape with and without ablation.
Hypersonic aerodynamic stability and drag of ablating and nonablating models of blunt-faced reentry shape
BLUNT BODY↗
Dynamic instability of undamped bellows face seals in cryogenic liquid.
Dynamic instability in undamped bellows face seals operating in cryogenic environment with torsional oscillation and diametrical rocking as primary motion
DYNAMIC STABILITY↗
The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocket
Effects of injector face baffle configurations on screech in hydrogen-oxygen rocket engine
INJECTOR↗
Compression tests of open-face truss-core sandwich panels
Compression tests of open-face truss core sandwich panels
TRUSS↗
Improving performance of face contact seal in liquid sodium /400 deg to 1000 deg F/ by incorporation of spiral-groove geometry
Improved performance of face contact seal in liquid sodium by incorporation of spiral groove geometry
LIQUID SODIUM↗
Diffraction study of oxygen adsorption on a /110/ tungsten face.
Oxygen adsorption on tungsten crystal face studied by back-reflection low energy electron diffraction
ADSORPTION↗
The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocket.
Effect of several injector face baffle configurations on screech in 20,000-lb thrust hydrogen-oxygen rocket
HYDROGEN OXYGEN /HOPE/ SPACECRAFT↗
Dynamic instability of undamped bellows face seals in cryogenic liquid.
Dynamic instability in undamped bellows face seals operating in cryogenic environment with torsional oscillation and diametrical rocking as primary motion
BELLOWS↗
Effect of forward-facing jets on aerodynamic characteristics of blunt configurations at Mach 6.
Forward facing jets effect on blunt configurations aerodynamic characteristics from wind tunnel tests at Mach 6, emphasizing drag increase
HYPERSONIC WIND TUNNEL↗
Pressure distribution on forward face of blunt bodies at angle of attack.
Pressure-distribution estimation over entire forward face of blunt body at angle of attack
BLUNT BODY↗