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

• Autorzy: Lysenko V. I. , Kosinov A. D. , Yermolaev Yu. G.
• Języki publikacji: EN

Abstrakty

EN

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.

Słowa kluczowe

EN

supersonic flow; boundary layer; artificial wake disturbance; flate plate

PL

przepływ naddźwiękowy; warstwa brzegowa

• Wydawca: Instytut Podstawowych Problemów Techniki PAN
• Czasopismo: Archives of Mechanics
• Rocznik: 2003
• Tom: Vol. 55, nr 3
• Strony: 243--256
• Opis fizyczny: Bibliogr. 24 poz.

Twórcy

autor

Lysenko V. I.

• Russian Academy of Sciences, Institute of Theoretical and Applied Mechanics, Novosibirsk 630090, Russia

autor

Kosinov A. D.

• Russian Academy of Sciences, Institute of Theoretical and Applied Mechanics, Novosibirsk 630090, Russia

autor

Yermolaev Yu. G.

• Russian Academy of Sciences, Institute of Theoretical and Applied Mechanics, Novosibirsk 630090, Russia

Bibliografia

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