Interaction of an oblique shock with a transitional Mach 5.92 boundary layer
46th AIAA Fluid Dynamics Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
British Library Conference Proceedings | 2016
|Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness (TN)
Online Contents | 2013
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