Experimental research on development of the controllable disturbances in the wake at supersonic flow around the plate
Arch. Mech. 55 (3), 243-256, 2003
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Abstract
The development of the artificial disturbances in the boundary layer on the flat part of a plate, the boundary layer on the opposite wedge (model stern) behind a fan of expansion waves and the wake was investigated at Mach number 2.