Lift Enhancement by a Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing
AIAA Aviation 2019 Forum
01.01.2019
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2019-3492: Lift Enhancement by a Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing
British Library Conference Proceedings | 2019
|The Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing
British Library Conference Proceedings | 2019
|