Control of Cowl Shock/Boundary-Layer Interaction in Hypersonic Inlets by Bump
AIAA Journal ; 53 , 11 ; 3492-3496
01.11.2015
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Control of Cowl Shock/Boundary-Layer Interaction in Hypersonic Inlets by Bump
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