AIAA-2019-3492: Lift Enhancement by a Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing
Applied aerodynamics ; 2019 ; Dallas, TX
01.01.2019
15 pages
Aufsatz (Konferenz)
Englisch
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The Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing
British Library Conference Proceedings | 2019
|DataCite | 1912
Vortex Flow Control over a Delta Wing Using Leading-edge Rudder (AIAA 2014-0956)
British Library Conference Proceedings | 2014
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