Title: Control of unsteady separated flow associated with the dynamic stall of airfoils
Subjects: Unsteady flow, Wind tunnel tests, Leading edges, Aerodynamic stalling, Boundary layer control, Unsteady flow (Aerodynamics), Separated flow, Boundary layer separation, Reynolds number, Supercritical airfoils, Airfoil oscillations, Airfoil profiles, Airfoils, Mach number, Active control