Experimental investigation of a Mach 4 shock-wave turbulent boundary layer interaction near an expansion corner
53rd AIAA Aerospace Sciences Meeting
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Expansion Corner Effects on Hypersonic Shock Wave-Turbulent Boundary-Layer Interactions
Online Contents | 1996
|