Dynamic Stall Control around Practical Airfoil Using Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators
The flow control effects of a nanosecond-pulse-driven dielectric barrier discharge plasma actuator (ns-DBDPA) in dynamic stall flow were experimentally investigated.The ns-DBDPA mozelle riesling was installed on the leading edge of an airfoil model designed in the form of a helicopter blade.The model was oscillated periodically around 25% of the ch