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Viscous and Inviscid Hypersonic Flow About a Double Ellipsoid

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Book cover Hypersonic Flows for Reentry Problems

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Abstract

The steady hypersonic flow over a double ellipsoid is numerically investigated for two nonreacting inviscid cases at Ma = 8.15, one reacting inviscid case at Ma = 25 with the freestream conditions taken from standard atmosphere at 75km and one nonreacting viscous case at Ma = 8.15 and Re = 1.27 × 106. For the last two cases an error estimation is performed by means of global mesh refinement.

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References

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Author information

Authors and Affiliations

  1. Dornier Luftfahrt GmbH, Postfach 1303, 7990, Friedrichshafen, Germany

    Klaus Dortmann

Authors
  1. Klaus Dortmann
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Editor information

Editors and Affiliations

  1. Centre de Sophia Antipolis, INRIA, 2004 Route des Lucioles, F-06561, Valbonne Cedex, France

    Jean-Antoine Désidéri

  2. Department of Mathematics, University of Houston, Texas, 4800 Calhoun Road, University Park, 77004, Houston, TX, USA

    Roland Glowinski

  3. Aerodynamics Department, Dassault Aviation, 78 Quai Marcel Dassault, F-92214, Saint Cloud, France

    Jacques Périaux

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© 1991 Springer-Verlag Berlin Heidelberg

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Dortmann, K. (1991). Viscous and Inviscid Hypersonic Flow About a Double Ellipsoid. In: Désidéri, JA., Glowinski, R., Périaux, J. (eds) Hypersonic Flows for Reentry Problems. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-76527-8_42

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  • DOI: https://doi.org/10.1007/978-3-642-76527-8_42

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-76529-2

  • Online ISBN: 978-3-642-76527-8

  • eBook Packages: Springer Book Archive

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