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

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Title of Article

DIRECT NUMERICAL SIMULATION OF THE TRANSITIONAL SUPERSONIC BOUNDARY LAYER ON A FLAT PLATE

Issue	4
Date	2011

Article type	scientific article	UDC	532.51;519.8
Pages	1235-1236	Keywords

Authors

Khotyanovskiy D.V.Institut teoreticheskoy i prikladnoy mekhaniki im. S.A. Khristianovicha SO RAN, Novosibirsk
Kudryavtsev A.N.Institut teoreticheskoy i prikladnoy mekhaniki im. S.A. Khristianovicha SO RAN, Novosibirsk

Abstract

On the basis of full unsteady Navier-Stokes equations of compressible gas the direct numerical simulation of linear and non- linear stages of laminar-turbulent transition in the flat-plate boundary layer is performed at flow Mach number M = 2.

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