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RISNumerical Investigation of a Pitching NACA 0012 Wing with Plasma-Based Flow Control Using Prediction–Correction Direct-Forcing Immersed Boundary Method
Publisher: ASCE
Abstract: Dynamic stall is a nonlinear fluid phenomenon. It is caused by the vortex generation and motion of the leading edge of the wing. When the angle of attack (AOA) changes rapidly, it causes the vortex to delay and shed. ...