Transition Effect on Shock Wave / Boundary Layer Interaction at M=1.47
53rd AIAA Aerospace Sciences Meeting
2015-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Transition Effect on Shock Wave / Boundary Layer Interaction at M=1.47 (AIAA 2015-1974)
British Library Conference Proceedings | 2015
|Cylinder-induced shock-wave boundary-layer interaction
AIAA | 1992
|