Supersonic Flow over a Shallow Open Rectangular Cavity

An experimental investigation was conducted on a supersonic flow at a freestream Mach number of 2 over a shallow open cavity, including the effects of adding streamwise serrated edges. These flows have relevance to weapons bays and airframe gaps on high-speed aircraft. The measurements consisted of...

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Veröffentlicht in:Journal of aircraft 2015-03, Vol.52 (2), p.609-616
Hauptverfasser: Gai, Sudhir L, Kleine, Harald, Neely, Andrew J
Format: Artikel
Sprache:eng
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