Investigation of Oblique Breakdown in a Supersonic Boundary Layer at Mach 2 Using DNS
45th AIAA Aerospace Sciences Meeting and Exhibit
2007-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Investigation of Oblique Breakdown in a Supersonic Boundary Layer at Mach 2 Using DNS AIAA Paper
British Library Conference Proceedings | 2007
|Transition Onset Predictions for Oblique Breakdown in a Mach 3 Boundary Layer (TN)
Online Contents | 2014
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