Experimental study of vortex breakdown over nonslender flying wing at high angle of attack
AIAA AVIATION 2021 FORUM
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Vortex Flows on a Rolling Nonslender Delta Wing
AIAA | 2004
|The effect of angle of attack on the flow structure over the nonslender lambda wing
Online Contents | 2013
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