Numerical Study on Azimuthal Partition Combined Plasma Control for Rotor Airfoil Deep Dynamic Stall at High Advance Ratio
To address the challenge of effectively suppressing deep dynamic stall on the retreating side of rotor blades at high advance ratios, an azimuthal-zone plasma combined control strategy is proposed. This strategy is grounded in the complementary physical mechanisms of AC-DBD and NS-DBD actuators—AC-DBD delays separation...