Heat transfer rate for laminar, transition and turbulent boundary layer and transition phenomenon on shock tube wall
20th Aerospace Sciences Meeting ; 1982 ; Orlando , FL , U.S.A.
1982-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Laminar-Turbulent Transition on the Shock-Wave/Boundary-Layer Interaction
British Library Conference Proceedings | 2014
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