An experimental investigation of deep dynamic stall control using plasma actuators

The effect of active control by a nanosecond pulsed dielectric-barrier discharge plasma actuator was studied on a NACA 0012 airfoil, with a 7-inch chord (with 13-inch endplates) and a 14-inch span, for a sinusoidal motion profile from α  = 0° to 20° at Re c  = 300,000 and k  = 0.075. Characterizatio...

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