Nothing Special   »   [go: up one dir, main page]

Keyes et al., 1973 - Google Patents

Analytical and experimental studies of shock interference heating in hypersonic flows

Keyes et al., 1973

View PDF
Document ID
13098352931451515485
Author
Keyes J
Hains F
Publication year

External Links

Snippet

An analytical and experimental study is presented of the aerodynamic heating resulting from six types of shock interference patterns encountered in high speed flow. Centerline measurements of pressure and heat transfer distributions on basic bodies were obtained in …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Similar Documents

Publication Publication Date Title
Keyes et al. Analytical and experimental studies of shock interference heating in hypersonic flows
Whitmore et al. Measurement uncertainty and feasibility study of a flush airdata system for a hypersonic flight experiment
Hiers et al. Effects of shock-wave impingement on the heat transfer on a cylindrical leading edge
Hopkins Direct Measurements of Turbulent Skin Friction on a Nonadiabatic Flat Plate at Mach Number 6.5 and Comparisons With Eight Theories
Ferri A review of some recent developments in hypersonic flow
SPAID et al. Experimental results for a hypersonic nozzle/afterbody flow field
Schaaf Recent progress in rarefied gasdynamics
Vas et al. An experimental investigation of the flow over simple two-dimensional and axial symmetric bodies at hypersonic speeds
Lockman et al. Flow over an all-body hypersonic aircraft-Experiment and computation
Pinckney Turbulent heat transfer prediction method for application to scramjet engines
Stewart et al. Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds
Keyes Pressures and Heat Transfer on a 75 ̊swept Delta Wing with Trailing-edge Flap at Mach 6 and Angles of Attack to 90
Hefner Lee-surface heating and flow phenomena on space shuttle orbiters at large angles of attack and hypersonic speeds
Forsyth et al. Experimental Assessment of Hypersonic Convective Heat Transfer Augmentation due to Surface Roughness
Rudy et al. Mean flow development and surface heating for an attaching compressible free shear layer
Pinckney Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients
Weinstein Heat transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7
Mallinson et al. Upstream influence and peak heating in hypervelocity shock wave/boundary-layer interaction
Andrews Jr et al. An inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model
Hunt Heating and flow-field studies on a straight-wing hypersonic reentry vehicle at angles of attack from 20 to 80 deg with simulation of real-gas trends
Marvin et al. Convective heat-transfer rates on large-angle conical bodies at hypersonic speeds
Kussoy Hypersonic Rarefied Flow over Sharp Slender Cones
Denman Turbulent boundary layer rough surface heat transfer on blunt bodies at high heating rates.
Seubold Turbulent mixing of a two-dimensional free jet
Anders Wedge-induced laminar-boundary-layer separation on a flat plate in low-density, hypervelocity flow