Shock-Boundary Layer Interaction due to a Sharp Unswept Fin in a Mach 2 Flow
53rd AIAA Aerospace Sciences Meeting
2015-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Shock-Boundary Layer Interaction due to a Sharp Unswept Fin in a Mach 2 Flow (AIAA 2015-1517)
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