A Hybrid Model for Lift Response to Dynamic Actuation on a Stalled Airfoil
A Hybrid Model for Lift Response to Dynamic Actuation on a Stalled Airfoil
The current research focuses on modeling the lift response due to dynamic (time-varying) “burst-type” actuation on a stalled airfoil. Here, the “burst-type” actuation refers to the synthetic jet (generated from the actuator) that is used for flow separation mitigation. Dynamic “burst-type” actuation exhibits two different characteristic dynamic behaviors within the …