Large eddy simulation of dynamic stall over an airfoil and its control with plasma actuator

The purpose of this study is to investigate deep dynamic stall over a pitching National Advisory Committee for Aeronautics 0015 airfoil and its control with an alternating current dielectric barrier discharge (AC-DBD) plasma actuator by means of large eddy simulation. The airfoil oscillates at a red...

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Veröffentlicht in:	AIP advances 2023-02, Vol.13 (2), p.025218-025218-18
Hauptverfasser:	Zhang, Hengyang, Yu, Haocheng, Zhang, Ao, Zheng, Jianguo
Format:	Artikel
Sprache:	eng
Schlagworte:	Actuation Aeronautics Airfoil oscillations Airfoils Alternating current Angle of attack Computational fluid dynamics Dielectric barrier discharge Drag Drag reduction Eddy currents Flow control Flow separation Fluid flow Hysteresis loops Large eddy simulation Plasma Reynolds number Simulation Stalling Suction
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