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• W2165774518 abstract "We review and expand on the control of separated flows over flat plates and aerofoils at low Reynolds numbers associated with micro air vehicles. Experimental observations of the steady-state and transient lift response to actuation, and its dependence on the actuator, aerofoil geometry and flow conditions, are discussed and an attempt is made to unify them in terms of their excitation of periodic and transient vortex shedding. We also examine strategies for closed-loop flow and flight control using actuation of leading-edge vortices." @default.
• W2165774518 created "2016-06-24" @default.
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• W2165774518 date "2011-04-13" @default.
• W2165774518 modified "2023-09-23" @default.
• W2165774518 title "Control of vortex shedding on two- and three-dimensional aerofoils" @default.
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• W2165774518 doi "https://doi.org/10.1098/rsta.2010.0355" @default.
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