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Erosive burning of a propellant in the field of a traveling acoustic wave

  • Combustion and Explosion
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Abstract

The response of the propellant burning rate to periodically varied pressure and the tangential mass flow of the combustion products is examined within the framework of the phenomenological theory of unsteady combustion. The effect of an elementary acoustic disturbance, a plane monochromatic traveling acoustic wave, is examined. The analytical and numerical results are obtained for the simplest propellant model with a minimum number of parameters. The roles of the steady and unsteady components of erosion at low and high values of the erosion ratio are established.

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Authors and Affiliations

  1. Semenov Institute of Chemical Physics, Russian Academy of Sciences, ul. Kosygin 4, Moscow, 119991, Russia

    B. V. Novozhilov, Z. I. Kaganova & A. A. Belyaev

Authors
  1. B. V. Novozhilov
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  2. Z. I. Kaganova
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  3. A. A. Belyaev
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Additional information

Original Russian Text © B.V. Novozhilov, Z.I. Kaganova, A.A. Beylaev, 2007, published in Khimicheskaya Fizika, 2007, Vol. 26, No. 3, pp. 34–41.

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Novozhilov, B.V., Kaganova, Z.I. & Belyaev, A.A. Erosive burning of a propellant in the field of a traveling acoustic wave. Russ. J. Phys. Chem. B 1, 94–101 (2007). https://doi.org/10.1134/S1990793107020030

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  • DOI: https://doi.org/10.1134/S1990793107020030

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