Sensitivity analysis for the control of oblique shock wave/laminar boundary layer interactions at Mach 5.92
47th AIAA Fluid Dynamics Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
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