A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniques
12th Aerospace Sciences Meeting ; 1974 ; Washington , DC , U.S.A.
1974-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Asymmetric Crossing-Shock-Wave-Turbulent-Boundary-Layer Interaction
Online Contents | 1995
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