Effective plasma buffet and drag control for laminar transonic aerofoil
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DOI: 10.1177/0954410018795542
Abstract: The effect of plasma actuators on shock wave–laminar boundary layer interaction was studied experimentally on transonic laminar aerofoil. The unsteady characteristics of the separation zone including the transonic buffet were measured. Two kinds of electrical… read more here.
Keywords: plasma; control; plasma actuators; laminar ... See more keywords