Experimental research on development of the controllable disturbances in the wake at supersonic flow around the plate

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Authors

  • V.I. Lysenko Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Russia
  • A.D. Kosinov Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Russia
  • Yu.G. Yermolaev Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Russia

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.

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