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
2011-01-01
Conference paper
Electronic Resource
English
MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING
British Library Conference Proceedings | 2011
|Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings (TN)
Online Contents | 2013
|Vortex breakdown over a pitching delta wing
AIAA | 1994
|Vortex Breakdown over a Pitching Delta Wing
British Library Conference Proceedings | 1994
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