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The Finite Pointset Method for hypersonic flows in the rarefied gas regime

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Advances in Hypersonics

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Abstract

There seems to be no doubt any longer, that it is not recommendable to use the Navier-Stokes equation for the description of the flow around aspace vehicle in altitudes above 80 km. One has to go one step up in the hierarchy and use a kinetic equation, which holds even if the gas is far away from the thermodynamic equilibrium.

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Authors and Affiliations

  1. Department of Mathematics, University of Kaiserslautern, Germany

    H. Neunzert & J. Struckmeier

Authors
  1. H. Neunzert
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  2. J. Struckmeier
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Editor information

Editors and Affiliations

  1. Sandia National Laboratories, Albuquerque, NM 87111, USA

    John J. Bertin

  2. Dept. of Aerodynamic Theory Avions Marcel Dassault-Brequet Aviation, 92214 Saint Cloud, France

    Jacques Periaux

  3. Lehr-Und Forschungsbiet für Mechanik der Rheinisch-Westfälischen, Technischen Hochschule Aachen, Templergraben 64, Germany

    Josef Ballmann

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© 1992 Springer Science+Business Media New York

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Neunzert, H., Struckmeier, J. (1992). The Finite Pointset Method for hypersonic flows in the rarefied gas regime. In: Bertin, J.J., Periaux, J., Ballmann, J. (eds) Advances in Hypersonics. Birkhäuser, Boston, MA. https://doi.org/10.1007/978-1-4612-0375-9_7

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  • DOI: https://doi.org/10.1007/978-1-4612-0375-9_7

  • Publisher Name: Birkhäuser, Boston, MA

  • Print ISBN: 978-1-4612-6732-4

  • Online ISBN: 978-1-4612-0375-9

  • eBook Packages: Springer Book Archive

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