MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
01.01.2011
14 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings (TN)
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