Title: Parametric studies of shock wave/boundary layer interactions over 2D compression corners at Mach 6
First published: 1992
Subjects: Hypersonic vehicles, Shock-boundary layer interaction, Shock waves, Mathematical models, Turbulent boundary layer, Laminar flow, Hypersonic Aerodynamics, Space vehicles, Atmospheric entry, Heat, Transmission, Thermography, Hypersonic planes, Design and construction