EXPERIMENTAL STUDY OF VORTEX BREAKDOWN OVER NONSLENDER FLYING WING AT HIGH ANGLE OF ATTACK
AIAA Aviation Forum ; 2021 ; Online
2021
Conference paper
English
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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