Direct numerical simulation of transition to turbulence in a supersonic boundary layer
A.N. Kudryavtsev and D.V. Khotyanovsky
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
E-mail: khotyanovsky@itam.nsc.ru
Keywords: direct numerical simulation, laminar-turbulent transition, supersonic boundary layer
Pages: 559–568
Abstract
Based on full unsteady compressible Navier–Stokes equations a direct numerical simulation of the linear and nonlinear stages of the laminar-turbulent transition in boundary layer of a flate plate at the freestream Mach number M = 2 is carried out.
DOI: DOI: 10.1134/S0869864315050042
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