Combustion, Explosion and Shock Waves

, Volume 9, Issue 6, pp 687–690 | Cite as

High-speed flow of a mixture of hydrogen and oxygen over blunt bodies

  • S. Yu. Chernyavskii
  • N. N. Baulin
  • A. S. Mkrtumov
Article

Keywords

Detonation Wave Adiabatic Shock Model Speed Mixture Pressure Detonation Speed 

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Literature Cited

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    G. G. Chernyi, Astron. Acta,13, 5 (1968).Google Scholar
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    “A technique for studying supersonic combustion in the vicinity of a hypersonic missile,” Nat. Bur. Stand. Tech. News Bull.,44 (1960).Google Scholar
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    H. Behrens, W. Struth, and F. Wecken, Tenth (International) Symp. on Combustion (1965).Google Scholar
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    R. L. Alpert and T.-Y. Toog, Astron. Acta,17, 4 (1972).Google Scholar
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    H. F. Lehr, Astron. Acta,17, 4 (1972).Google Scholar
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    I. Vagner, in: Basic Results of Experiments in Shock Tubes [in Russian], Moscow (1963).Google Scholar

Copyright information

© Plenum Publishing Corporation 1975

Authors and Affiliations

  • S. Yu. Chernyavskii
  • N. N. Baulin
  • A. S. Mkrtumov

There are no affiliations available

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