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Journal of engineering physics

, Volume 16, Issue 6, pp 683–688 | Cite as

The approximate solution of the equation for the supersonic flow of a gas

  • P. M. Kolesnikov
Article
  • 28 Downloads

Abstract

A new approximation of the Chaplygin function is proposed in this paper, one that is suitable at 1 < M < 3, making it possible to find analytical solutions for the equations of supersonic gas flow. An explicit form of the Riemann function has been derived for the potential equation and the stream function, and the limit transitions to the Tricomi equation or to the Euler-Poisson-Darboux equation are examined.

Keywords

Statistical Physic Approximate Solution Explicit Form Stream Function Supersonic Flow 
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

© Consultants Bureau 1972

Authors and Affiliations

  • P. M. Kolesnikov
    • 1
  1. 1.Institute of Heat and Mass TransferAcademy of Sciences of the Belorussian SSRMinsk

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