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Numerical methods for simulating supersonic combustion

  • J. Groenner
  • E. von Lavante
  • M. Hilgenstock
3. Numerical Methods and Algorithms d) Euler/Navier-Stokes Equations
Part of the Lecture Notes in Physics book series (LNP, volume 453)

Abstract

An efficient computer program was developed for the computation of supersonic combustion problems. Several test cases showed the capabilities of implementations of different upwind schemes in calculating chemical reactions. The FAS multigrid procedure accelerated in some cases the convergence to steady state. The numerical results were validated by the corresponding experiments for the more demanding cases. A reasonable qualitative as well as quantitative agreement was achieved.

Keywords

Mach Number Pressure Contour Separation Shock Supersonic Combustion Hypersonic Flight 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag 1995

Authors and Affiliations

  • J. Groenner
    • 1
  • E. von Lavante
    • 1
  • M. Hilgenstock
    • 1
  1. 1.University of EssenEssenGermany

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