Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness (TN)
AIAA journal ; 51 , 1 ; 266-269
2013
Aufsatz (Zeitschrift)
Englisch
Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
British Library Conference Proceedings | 2016
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