NUMERICAL INVESTIGATION OF FLOW CONTROL OVER AN AIRFOIL - Akcayöz, Eray
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The synthetic jet is applied over an airfoil to control the flow separation. Response Surface Methodology is employed for the optimization of synthetic jet parameters at various angles of attack. The synthetic jet parameters; the jet velocity, the jet location, the jet angle and the jet frequency are optimized to maximize the lift to drag ratio. The jet power coefficient is kept constant in the optimization. The lift to drag ratio increased significantly especially at post stall angles of attack.

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Produktbeschreibung
The synthetic jet is applied over an airfoil to control the flow separation. Response Surface Methodology is employed for the optimization of synthetic jet parameters at various angles of attack. The synthetic jet parameters; the jet velocity, the jet location, the jet angle and the jet frequency are optimized to maximize the lift to drag ratio. The jet power coefficient is kept constant in the optimization. The lift to drag ratio increased significantly especially at post stall angles of attack.
Autorenporträt
Eray Akçayöz was born in 1982 in Kars, Turkey. He received the B.S. and M.S. degrees in aerospace engineering from METU, Turkey. He has worked over 4 years in aerospace defense industry as aerodynamics engineer. He is currently working towards the Ph.D. in mechanical engineering from École Polytechnique de Montréal.