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Nonstationary processes during quenching of condensed systems in a half-closed volume by a combination method

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Combustion, Explosion and Shock Waves Aims and scope

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Literature Cited

  1. B. T. Erokhin and Yu. I. Fedorov, Fiz. Goren. i Vzryva,7, No. 4 (1971).

  2. B. A. Raizberg, B. T. Erokhin, and K. P. Samsonov, Principles of the Theory of Working Processes in Solid Propellant Rocket Systems [in Russian], Mashinostroenie, Moscow (1972).

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  4. Horton et al., Raketn. Tekhn. i Kosmonav.,6, No. 2 (1968).

  5. G. Von Elbe, Theory of Solid Propellant Ignition and Response to Pressure Transients, Interagency Solid Propulsion Meeting, No. 3 (1963), p. 95.

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Authors
  1. V. T. Erokhin
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  2. Yu. I. Fedorov
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  3. A. V. Sindyukov
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Additional information

Kaliningrad. Translated from Fizika Goreniya i Vzryva, Vol. 11, No. 2, pp. 208–213, March–April, 1975.

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Erokhin, V.T., Fedorov, Y.I. & Sindyukov, A.V. Nonstationary processes during quenching of condensed systems in a half-closed volume by a combination method. Combust Explos Shock Waves 11, 180–184 (1975). https://doi.org/10.1007/BF00756714

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  • DOI: https://doi.org/10.1007/BF00756714

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