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.
01.01.1989
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Supersonic Shock-Turbulent Boundary-Layer Interaction on a Roughened Surface
Online Contents | 1996
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