Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings (TN)
AIAA journal ; 51 , 9
2013
Article (Journal)
English
MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING
British Library Conference Proceedings | 2011
|Active control of vortex breakdown over delta wings
AIAA | 1994
|