Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence
Advances in simulation of wing and nacelle stall: results of the closing symposium of the DFG Research Unit FOR 1066 ; 2014 ; Braunschweig, Germany
01.01.2016
14 pages
Aufsatz (Konferenz)
Englisch
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Shock Wave-Boundary-Layer Interactions in Subsonic Intakes at High Incidence (AIAA 2015-0067)
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