A feedback control system for mitigating flow separation was developed by using a string-type dielectric-barrier-discharge (DBD)\nplasma actuator and a fiber Bragg grating (FBG) sensor. Tangential jets were induced from the string-type DBD plasma actuator,\nwhich was located at 5% chord from the leading edge of an NACA0024 airfoil.The FBG sensor was attached to the interior surface\nnear the root of the cantilever beam modeled on the pressure surface of the airfoil.The strain at the cantilever root was reflected in\nthe form of Bragg wavelengths (
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