Effect of pressure gradient on the stability of hypersonic boundary layer flows
21st AIAA International Space Planes and Hypersonics Technologies Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Pressure Gradients on Axisymmetric Hypersonic Boundary Layer Stability
British Library Conference Proceedings | 2000
|Boundary layer transition in hypersonic flows
AIAA | 1990
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