Trailing Vortex Strength Attenuation via Chipped Wingtip Shapes
31st AIAA Applied Aerodynamics Conference
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Trailing Vortex Strength Attenuation via Chipped Wingtip Shapes
British Library Conference Proceedings | 2013
|Wingtip Vortex Attenuation by Plasma Actuator
AIAA | 2012
|NTIS | 1984
|Wingtip vortex dissipator for aircraft
NTRS | 1976
|Adaptive control of wingtip vortex
AIAA | 1998
|