Leading Edge Bluntness Effects on Shock Wave/Boundary Layer Interactions Near a Convex Corner (AIAA 2015-3601)
AIAA international space planes and hypersonic systems and technologies conference
01.01.2015
16 pages
Aufsatz (Konferenz)
Englisch
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Numerical Investigation of Bluntness Effects on Hypersonic Leading Edge Separation (AIAA 2015-0984)
British Library Conference Proceedings | 2015
|Interactions Between Shock Wave and Hypersonic Laminar Boundary Layer Near Convex Corner
Online Contents | 1995
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