Characterization of a helical vortex, generated behind a rotating blade, using the Actuator Line Method
31st AIAA Applied Aerodynamics Conference
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Vortex Wake Generated Behind a Forward Swept Wing
AIAA | 2009
|Vortex Wake Generated Behind a Forward Swept Wing
Online Contents | 2009
|Aerodynamics and Acoustics of Blade-Vortex Interaction Using an Independently Generated Vortex
British Library Conference Proceedings | 1994
|Aerodynamics and Acoustics of Blade-Vortex Interaction Using an Independently Generated Vortex
British Library Conference Proceedings | 1993
|