An investigation into wedge-induced turbulent boundary layer separation on a uniformly roughened surface at Mach 6.0
7th Applied Aerodynamics Conference ; 1989 ; Seattle , WA , U.S.A.
1989-01-01
Conference paper
Electronic Resource
English
Supersonic Shock-Turbulent Boundary-Layer Interaction on a Roughened Surface
Online Contents | 1996
|Turbulent boundary-layer characteristics over a flat-plate/wedge configuration at Mach 6
Tema Archive | 1992
|