Mach Number Effects on Vortex Breakdown in Subsonic Flow over a Delta Wing
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING
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|Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings (TN)
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|Vortex breakdown over a pitching delta wing
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