Wind tunnel experiments on flow separation control of an Unmanned Air Vehicle by nanosecond discharge plasma aerodynamic actuation
Chen Kang1, Liang Hua2, 3, †,
       

Experimental results at different applied voltages (V∞ = 50 m/s, f = 230 Hz): (a) lift coefficients for different applied voltages, and (b) lift coefficient increments for different applied voltage.