Abstract
CXXGYY = specification for camber c (XX%) and h=c (YY%) Cl = airfoil lift coefficient, l=q1c Cd = airfoil drag coefficient, d=q1c c = chord length hc i = oscillatory momentum coefficient F = dimensionless unsteady modulation frequency, fmc=U1 f = plasma actuation frequency fm = plasma modulation frequency h = Gurney flap height normal to surface q1 = dynamic pressure Re = Reynolds number, U1c= U1 = freestream velocity = angle of attack = boundary-layer thickness = aerodynamic efficiency, Cl=Cd
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