Numerical Investigation on Transition of Shock Induced Boundary Layer
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; 2009 ; Orlando , Florida
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Investigation on Transition of Shock Induced Boundary Layer
British Library Conference Proceedings | 2009
|Shock tunnel investigation of boundary-layer transition at M = 5.5
Engineering Index Backfile | 1967
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