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
Simeonides Generalized reference enthalpy formulations and simulation of viscous effects in hypersonic flow
Holden et al. Measurements of boundary layer transition on cones at angle of attack for Mach numbers from 11 to 13
SPAID et al. Experimental results for a hypersonic nozzle/afterbody flow field
Wen Hypervelocity flow over spheres
Hopkins Direct Measurements of Turbulent Skin Friction on a Nonadiabatic Flat Plate at Mach Number 6.5 and Comparisons With Eight Theories
Vas et al. An experimental investigation of the flow over simple two-dimensional and axial symmetric bodies at hypersonic speeds
Schaaf Recent progress in rarefied gasdynamics
Lockman et al. Flow over an all-body hypersonic aircraft-experiment and computation
Pinckney Turbulent heat transfer prediction method for application to scramjet engines
Forsyth et al. Experimental Assessment of Hypersonic Convective Heat Transfer Augmentation due to Surface Roughness
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
Rudy et al. Mean flow development and surface heating for an attaching compressible free shear layer
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
Weinstein Heat transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7
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
Ashby et al. A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0
Minucci et al. Investigation of a two-dimensional scramjet inlet, freestream M= 8-18 and T0= 4100 K
Lemmon The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles