Вестник Нижегородского университета им. Н.И. Лобачевского. Серия: Социальные науки

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Title of Article

AN EXPERIMENTAL STUDY OF EXCITATION AND DEVELOPMENT OF CONTROLLED DISTURBANCES IN SPANWISE MODULATED BOUNDARY LAYERS AT MACH 2

Issue	4
Date	2011

Article type	scientific article	UDC	532.526
Pages	874-876	Keywords

Authors

Kosinov A.D.Institut teoreticheskoy i prikladnoy mekhaniki im. S.A. Khristianovicha SO RAN, Novosibirsk
Panina A.V.Institut teoreticheskoy i prikladnoy mekhaniki im. S.A. Khristianovicha SO RAN, Novosibirsk
Kolosov G.L.Institut teoreticheskoy i prikladnoy mekhaniki im. S.A. Khristianovicha SO RAN, Novosibirsk

Abstract

Experimental data on the receptivity of flat plate and swept wing supersonic boundary layers to controlled disturbances for a smooth model surface as well as in case of periodic roughness are obtained. Spatial and wave characteristics of wave trains are defined in the normal direction of supersonic boundary layer on swept wing.

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