Flow Physics of a Three-Dimensional Rounded Contour Bump in a Mach 1.3 Supersonic Free-stream (AIAA 2015-3011)
Applied aerodynamics ; 2015 ; Dallas, TX
2015-01-01
5 pages
Aufsatz (Konferenz)
Englisch
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A Numerical Analysis on Three-Dimensional Flow Field in a Supersonic Bump Inlet AIAA Paper
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