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Calculation of a two-phase flow in an axisymmetric nozzle

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Journal of engineering physics Aims and scope

Abstract

A system of differential equations is presented to describe a two-phase flow through an axisymmetric supersonic nozzle. The results for the solution of this system on a “Minsk-14” computer are given. The theoretical results are compared qualitatively with the experimental data.

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References

  1. L. A. Vulis, DAN SSSR,54, no. 8, 1946.

  2. G. A. Komov, IFZh [Journal of Engineering Physics],10, no. 3, 1966.

  3. Detonation and Two-Phase Flow [Russian translation], ed. S. S. Penner and F. A. Williams, Academic Press, 1966.

  4. Kligel, Voprosy raketnoi tekhniki, no. 10, 1965.

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Authors and Affiliations

  1. All-Union Correspondence Polytechnic Institute, Moscow

    I. M. Kapura, V. I. Serebrennikov & D. G. Chernikov

Authors
  1. I. M. Kapura
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  2. V. I. Serebrennikov
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  3. D. G. Chernikov
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Kapura, I.M., Serebrennikov, V.I. & Chernikov, D.G. Calculation of a two-phase flow in an axisymmetric nozzle. Journal of Engineering Physics 13, 330–334 (1967). https://doi.org/10.1007/BF00832349

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  • DOI: https://doi.org/10.1007/BF00832349

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