Shock tunnel investigation of boundary-layer transition at M equals 5.5
3rd and 4th Aerospace Sciences Meeting ; 1966 ; New York , NY , U.S.A.
1966-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Investigation on Transition of Shock Induced Boundary Layer
British Library Conference Proceedings | 2009
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