Numerical Investigation for Hysteresis Phenomena of Shock-Reflection in Overexpanded Axisymmetric Supersonic Jet
Conference; 7th, AIAA aviation technology, integration, and operations ; 2007 ; Belfast
01.01.2007
5839 pages
Held on CD-ROM. Held in conjunction with the 17th lighter-than-air systems technology conference; Shelved in Conference Index
Aufsatz (Konferenz)
Englisch
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Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles
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