Wind Tunnel Experiments on a NACA0015 Airfoil Equipped with Vectorizable Dielectric Barrier Discharge Plasma Actuators
32nd AIAA Applied Aerodynamics Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2014
|Flow Control of a NACA0015 Airfoil in a Turbulent Wake Using Plasma Actuators
British Library Conference Proceedings | 2012
|