INVESTIGATION OF A DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATOR TO CONTROL TURBULENT BOUNDARY LAYER SEPARATION

Investigation of a Dielectric Barrier Discharge Plasma Actuator to Control Turbulent Boundary Layer Separation

A numerical investigation was carried out to explore the effects of a dielectric barrier discharge (DBD) plasma actuator on a three-dimensional incompressible, separated flow.The test article selected for the simulations was the National Aeronautical and Space Administration (NASA) wall-mounted hump model.The simulations were run at a Reynolds numb

read more