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Direct numerical simulation of transition to turbulence in a supersonic boundary layer

Direct numerical simulation of transition to turbulence in a supersonic boundary layer 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. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Thermophysics and Aeromechanics Springer Journals

Direct numerical simulation of transition to turbulence in a supersonic boundary layer

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Publisher
Springer Journals
Copyright
2015 Pleiades Publishing, Ltd.
ISSN
0869-8643
eISSN
1531-8699
DOI
10.1134/S0869864315050042
Publisher site
See Article on Publisher Site

Abstract

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.

Journal

Thermophysics and AeromechanicsSpringer Journals

Published: Sep 1, 2015

References