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Motion of a gas behind a plane detonation wave passing through a cylinder of explosive

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Combustion, Explosion and Shock Waves Aims and scope

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Literature Cited

  1. K. P. Stanyukovich, Nonsteady Motion of a Continuous Medium [in Russian], Nauka, Moscow (1971).

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  2. V. A. Dvornikov, “Nonsteady two-dimensional flow of gas in the vicinity of a break of the line of flow,” in: Transactions of the Scientific-Research Institute of Applied Mathematics and Mechanics, Tomsk State University [in Russian], Vol. 4, Izd. Tomsk. Gos. Univ., Tomsk (1974).

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  3. R. Sauer, Nonsteady-State Problems of Gasdynamics [Russian translation], Mir, Moscow (1969).

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  4. P. I. Chushkin, Method of Characteristic Curves for Three-Dimensional Supersonic Gas Flows [in Russian], Izd. Vychisl. Tsentr. Akad. Nauk SSSR, Moscow (1968).

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Authors
  1. V. A. Dvornikov
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  2. L. V. Komarovskii
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Additional information

Scientific-Research Institute of Applied Mathematics and Mechanics, Tomsk State University. Translated from Fizika Goreniya i Vzryva, Vol. 12, No. 6, pp. 930–935, November–December, 1976.

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Dvornikov, V.A., Komarovskii, L.V. Motion of a gas behind a plane detonation wave passing through a cylinder of explosive. Combust Explos Shock Waves 12, 815–819 (1976). https://doi.org/10.1007/BF00740758

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  • DOI: https://doi.org/10.1007/BF00740758

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