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Fizika Goreniya i Vzryva, 2012, Volume 48, Issue 1, Pages 71–79 (Mi fgv978)  

This article is cited in 2 scientific papers (total in 2 papers)

Method of the model equation in the theory of unsteady combustion of a solid propellant

S. A. Rashkovskiya, Yu. M. Miloekhinb, A. N. Kluchnikovb, A. V. Fedorychevb

a Ishlinskii Institute for Problems in Mechanics, Russian Academy of Sciences, Moscow, 119526, Russia
b Federal Center for Dual-Use Technologies "Soyuz", Dzerzhinskii, 140090, Russia
Citations (2)
Abstract: A model equation for the unsteady burning rate of a solid propellant is proposed and justified. In the frequency range of interest for practice, the proposed model agrees with the phenomenological theory of unsteady combustion, but it is even more convenient for applications because it reduces to an ordinary differential equation of the second order with respect to the burning rate. A parametric study of the transitional process in the solid-propellant rocket motor is performed with variations of the nozzle throat area in a wide range of solid propellant parameters. The model predicts oscillatory combustion regimes and propellant extinction in the case of a decrease in pressure. The boundary of stability of the transitional process in the coordinates “sensitivity of the burning rate to changes in pressure–sensitivity of the burning rate to changes in initial temperature”. It is demonstrated that the calculations performed with the use of this model are in qualitative and quantitative agreement with experimental data for a full-scale solidpropellant rocket motor.
Keywords: solid propellant, combustion, low-frequency instability, extinction, modeling.
Received: 16.02.2011
English version:
Combustion, Explosion and Shock Waves, 2012, Volume 48, Issue 1, Pages 64–72
DOI: https://doi.org/10.1134/S0010508212010091
Bibliographic databases:
Document Type: Article
UDC: 536.46
Language: Russian
Citation: S. A. Rashkovskiy, Yu. M. Miloekhin, A. N. Kluchnikov, A. V. Fedorychev, “Method of the model equation in the theory of unsteady combustion of a solid propellant”, Fizika Goreniya i Vzryva, 48:1 (2012), 71–79; Combustion, Explosion and Shock Waves, 48:1 (2012), 64–72
Citation in format AMSBIB
\Bibitem{RasMilKlu12}
\by S.~A.~Rashkovskiy, Yu.~M.~Miloekhin, A.~N.~Kluchnikov, A.~V.~Fedorychev
\paper Method of the model equation in the theory of unsteady combustion of a solid propellant
\jour Fizika Goreniya i Vzryva
\yr 2012
\vol 48
\issue 1
\pages 71--79
\mathnet{http://mi.mathnet.ru/fgv978}
\elib{https://elibrary.ru/item.asp?id=17706491}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2012
\vol 48
\issue 1
\pages 64--72
\crossref{https://doi.org/10.1134/S0010508212010091}
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  • https://www.mathnet.ru/eng/fgv/v48/i1/p71
  • This publication is cited in the following 2 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
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