Abstract
A feasibility study of feedback control for mitigating periodic flow separation on NACA0024 airfoil was constructed by using dielectric barrier discharge plasma actuator(DBD-PA) and fiber Bragg grating flow sensor(FBG-FS).Towards applying these devices to small wind turbines,transmission of Bragg wavelengths detected by FBG-FS are tested by using a fiber optic rotary joint(FORJ) from rotor to stationary location Non-contact power transmissions for driving DBD-PAs were also tried by using opposed ferrite pot-cores from stationary location to rotor adversely.
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