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Distinctive features of the intrachamber instability of combustion in liquid-propellant rocket engines

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Abstract

Self-oscillations and certain of their regularities determined by solution of a degenerate system of differential equations that is used in considering combustion instability in combustion chambers of liquid-propellant rocket engines are modeled mathematically.

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Authors and Affiliations

  1. Zheltye-Vody Enterprise Institute “Strategiya”, 38 Gagarin Str., Zheltye Vody, 52201, Ukraine

    V. V. Gotsulenko

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  1. V. V. Gotsulenko
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 81, No. 5, pp. 897–902, September–October, 2008.

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Gotsulenko, V.V. Distinctive features of the intrachamber instability of combustion in liquid-propellant rocket engines. J Eng Phys Thermophy 81, 935–940 (2008). https://doi.org/10.1007/s10891-009-0121-0

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  • DOI: https://doi.org/10.1007/s10891-009-0121-0

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