Leading Edge Bluntness Effects on Shock Wave/Boundary Layer Interactions Near a Convex Corner
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Interactions Between Shock Wave and Hypersonic Laminar Boundary Layer Near Convex Corner
Online Contents | 1995
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