Parametric study of synthetic jet actuators on a backward facing step

The ability of synthetic jet actuators to leverage natural instabilities in the flow field due to separation is reviewed for applications towards virtual shape change. The separating flow over a backward facing step of height h is studied under the influence of an actuator upstream and downstream of separation. Experimental tests were conducted in a wind tunnel using particle imaging velocimetry and time-averaged static pressure data to measure and analyze the affected flow fields and pressure distribution. By placing a second actuator downstream of separation, the ability to influence the pressure distribution has been shown. The two actuators demonstrated the ability to affect Cp and dCp/dx in the region from 0 - 6h after the step.