We investigate the fluid-structure interactions from distributed bleed flow control over a semispan wing. Multi-scale, constitutive models are developed to incorporate bleed-effected terms in both the stiffness and inertia terms. Extensive wind tunnel experiments investigate the behavior of the system under the presence of bleed in a variety of forms, such as the dynamic behavior from the natural forcing of the flow to different forms of bleed actuation and their effects on the dynamic response of the wing. As a result, we utilize this form of flow control to suppress undesired vibrations in open loop feedback form, as well as to define flutter control authority.
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