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Investigation of high-speed boundary-layer transition by DNS

  1. Christian Stemmer*,
  2. Nikolaus A. Adams

Article first published online: 13 DEC 2004

DOI: 10.1002/pamm.200410216

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PAMM

PAMM

Volume 4, Issue 1, pages 470–471, December 2004

Additional Information

How to Cite

Stemmer, C. and Adams, N. A. (2004), Investigation of high-speed boundary-layer transition by DNS. Proc. Appl. Math. Mech., 4: 470–471. doi: 10.1002/pamm.200410216

Author Information

  1. Institut für Strömungsmechanik, Technische Universität Dresden, George-Bähr-Str. 3c, 01069 Dresden, Germany

*Phone: +49-351-463-39650 Fax: +49-351-463-35246

Publication History

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

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Abstract

An investigation of hypersonic boundary-layer flow along a flat plate is being presented. The high Mach number investigated calls for the consideration of the chemical reactions and the change in thermodynamical properties for temperatures up to T = 6000 K. For the current investigation a test case at M = 20 and the atmospheric conditions at an altitude of H = 50 Km is chosen. The differences to the ideal-gas result is demonstrated. (© 2004 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)

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