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RISActive Control of a Stalled Airfoil Through Steady or Unsteady Actuation Jets
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The active control of the leadingedge (LE) separation on the suction surface of a stalled airfoil (NACA 0012) at a Reynolds number of 106 based on the chord length is investigated through a computational study. The actuator ...