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Large-Eddy Simulation of Shock Wave/Turbulent Boundary Layer Interaction at High Reynols Number

  1. M. S. Loginov1,2,*,
  2. N. A. Adams1,
  3. A. A. Zheltovodov2

Article first published online: 13 DEC 2004

DOI: 10.1002/pamm.200410213

Issue

PAMM

PAMM

Volume 4, Issue 1, pages 464–465, December 2004

Additional Information

How to Cite

Loginov, M. S., Adams, N. A. and Zheltovodov, A. A. (2004), Large-Eddy Simulation of Shock Wave/Turbulent Boundary Layer Interaction at High Reynols Number. Proc. Appl. Math. Mech., 4: 464–465. doi: 10.1002/pamm.200410213

Author Information

  1. 1

    Institute of Fluid Mechanics, Dresden University of Technology, George-Bähr Str. 3c, 01062 Dresden, Germany

  2. 2

    Institute of Theoretical and Applied Mechanics, Institutskaya Str. 4/1, 630090 Novosibirsk, Russia

*Phone: +49 351 463 34910

Publication History

  1. Issue published online: 13 DEC 2004
  2. Article first published online: 13 DEC 2004

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References

  • [1]
    N. A. Adams. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Re = 1685. J. Fluid Mech. 429:187–216, 2000.
  • [2]
    A. A. Zheltovodov, V. M. Trofimov, E. Schülein, V. N. Yakovlev. An experimental documentation of supersonic turbulent flows in the vicinity of forward- and backward-facing ramps. Report N 2030. Institute of Theoretical and Applied Mechanics, USSR Academy of Sciences, Novosibirsk, 1990.
  • [3]
    S. Stolz, N. A. Adams, L. Kleiser. The approximate deconvolution model for large eddy simulation of compressible flows and its application to shock-turbulent-boundary-layer interaction. Phys. Fluids 13:2985–3001, 2001
  • [4]
    D. S. Dolling and M. T. Murphy. Unsteadiness of the separation shock wave structure in supersonic compression ramp flowfield. AIAA Journal, 21:1628–1634, 1983.
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