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Possible mechanism of nonsteady-state erosion combustion of composite solid propellants

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Abstract

It has been demonstrated that in the combustion of composite solid propellants the instantaneous mass burning rate can depend on variations in the velocity of cross-flow of gases even if in the steady-state regime the combustion is insentitive to cross-flow velocity. A method has been proposed for studying the nonsteady-state erosion combustion in experiments with composite systems.

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Authors
  1. L. K. Gusachenko
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  2. V. E. Zarko
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Additional information

Institute of Chemical Kinetics and Combustion, Novosibirsk 630090. Translated from Fizika Goreniya i Vzryva, Vol. 31, No. 4, pp. 40–43, July–August, 1995.

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Gusachenko, L.K., Zarko, V.E. Possible mechanism of nonsteady-state erosion combustion of composite solid propellants. Combust Explos Shock Waves 31, 437–440 (1995). https://doi.org/10.1007/BF00789363

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  • DOI: https://doi.org/10.1007/BF00789363

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