Numerical simulation of the evolution of unstable disturbances of various modes and initial stages of the laminar-turbulent transition in the boundary layer at the freestream Mach number М = 6


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Abstract

Direct numerical simulations of linear and nonlinear stages of the evolution of unstable disturbances of various modes and initial stages of the laminar-turbulent transition in the boundary layer on a flat plate at the freestream Mach number M = 6 are performed on the basis of full unsteady Navier–Stokes equations for a compressible gas. A considerable effect of three-dimensional unstable disturbances on initiation of the laminar-turbulent transition is demonstrated.

About the authors

D. V. Khotyanovsky

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Author for correspondence.
Email: khotyanovsky@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk

A. N. Kudryavtsev

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Email: khotyanovsky@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk

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