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Journal of Engineering Physics and Thermophysics

, Volume 81, Issue 5, pp 935–940 | Cite as

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

  • V. V. Gotsulenko
Article
  • 82 Downloads

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.

Keywords

Combustion Chamber Relaxation Oscillation Rocket Engine Wave Resistance Combustion Instability 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media, Inc. 2008

Authors and Affiliations

  • V. V. Gotsulenko
    • 1
  1. 1.Zheltye-Vody Enterprise Institute “Strategiya”Zheltye VodyUkraine

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