Numerical Study of Transitional Shock-Wave/Boundary-Layer Interactions (SWBLIs) in Hypersonic Flows
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2008-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
FLUID DYNAMICS - Shock Wave-Transitional Boundary-Layer Interactions in Hypersonic Flow
Online Contents | 2006
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