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Journal of engineering physics

, Volume 44, Issue 5, pp 509–513 | Cite as

Thermal mechanism of destruction of the barrier of a transonic jet of combustion products of rocket fuel

  • V. G. Zabotin
  • A. I. Kosenko
  • A. I. Osipov
  • A. N. Pervyshin
Article
  • 15 Downloads

Abstract

The work concerns the combined theoretical and experimental investigation of the cutting speed of thermally highly conducting alloys by a jet of combustion products flowing at supercritical pressure gradient from the transonic jet of oxygen-hydrogen and oxygen-propane gas generators.

Keywords

Combustion Statistical Physic Pressure Gradient Experimental Investigation Combustion Product 
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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Literature cited

  1. 1.
    I. I. Sokolov, Gas Welding and Gas Cutting of Metals [in Russian], Vysshaya Shkola, Moscow (1981).Google Scholar
  2. 2.
    B. N. Yudaev, M. S. Mikhailov, and V. K. Savin, Heat Exchange in Interaction of Jets with Barriers [in Russian], Mashinostroenie, Moscow (1977).Google Scholar
  3. 3.
    A. V. Antsupov, “Investigation of the parameters of an underexpanded supersonic gas jet,” Zh. Tekh. Fiz.,44, 372–379 (1974).Google Scholar

Copyright information

© Plenum Publishing Corporation 1983

Authors and Affiliations

  • V. G. Zabotin
    • 1
  • A. I. Kosenko
    • 1
  • A. I. Osipov
    • 1
  • A. N. Pervyshin
    • 1
  1. 1.Academician S. P. Korolev Kuibyshev Aviation InstituteUSSR

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