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Fluid Dynamics

, Volume 2, Issue 2, pp 82–84 | Cite as

Study of supersonic flow past axisymmetric bodies of different form

  • Z. D. Zapryanov
Article
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Abstract

A method is proposed in [1] for calculating supersonic flow past smooth bodies. The present article presents a computational scheme and calculational formulas for determining the gasdynamic functions at the nodes of the linesϕ=const. A comparison is made of certain of the results obtained with the results of other studies [2, 3]. Results are also presented of the calculation of the flow of a perfect gas past ellipsoids of revolution (δ=2.3) and inverted cones with spherical and ellipsoidal blunting.

Keywords

Present Article Supersonic Flow Computational Scheme Axisymmetric Body Inverted Cone 
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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References

  1. 1.
    Z. D. Zapryanov and V. B. Minostsev, “Method of calculating three-dimensional supersonic gas flow past bodies”, Izv. AN SSSR, Mekhanika i mashinostroenie, no. 5, 1964.Google Scholar
  2. 2.
    P. I. Chushkin and N. P. Shulishnina, Tables of Supersonic Flow Past Blunt Cones [in Russian], VTs AN SSSR, 1961.Google Scholar
  3. 3.
    Yu. N. D'yakonov and N. A. Zaitseva, “Supersonic ideal gas flow past a blunt body”, Izv. AN SSSR, Mekhanika i mashinostroenie, no. 1, 1963.Google Scholar
  4. 4.
    S. M. Gilinskii, G. F. Telenin, and G. P. Tinyakov, “Method of calculating supersonic flow past blunt bodies with detached shock wave”, Izv. AN SSSR, Mekhanika i mashinostroenie, no. 4, 1964.Google Scholar
  5. 5.
    S. M. Gilinskii and M. G. Lebedev, “Study of slightly supersonic flow past plane and axisymmetric bodies with detached shock wave”, Izv. AN SSSR, Mekhanika, no. 1, 1965.Google Scholar

Copyright information

© The Faraday Press, Inc. 1971

Authors and Affiliations

  • Z. D. Zapryanov
    • 1
  1. 1.Moscow

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