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Stability of supersonic boundary layer on permeable surface

Gaponov S. A., Ermolaev Yu. G., Kosinov A. D., Lysenko V. I., Semionov N. V., Smorodsky B. V.

Archives of Mechanics

2014

Vol. 66, nr 6

453--466

In the present study we have performed combined theoretical and experimental investigation of the surface permeability influence on the linear stability of the supersonic flat-plate boundary layer at free-stream Mach number M = 2. Good quantitative agreement was obtained between the data calculated by the linear theory of stability and the data obtained in experiments with artificially generated disturbances performed on models with various porous inserts.

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

Lysenko V. I., Kosinov A. D., Yermolaev Yu. G.

Archives of Mechanics

2003

Vol. 55, nr 3

243-256

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.