Transient Growth in Oblique Shock Wave/laminar Boundary Layer Interactions at Mach 5.92 (AIAA 2018-3221)
Fluid dynamics (Conference)
01.01.2018
17 pages
Aufsatz (Konferenz)
Englisch
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Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
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