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Russian Aeronautics

, Volume 61, Issue 3, pp 460–466 | Cite as

Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber

  • W. M. YousefEmail author
  • V. A. Sychenkov
  • N. V. Davydov
  • Yu. B. Aleksandrov
Aircraft and Rocket Engine Theory
  • 4 Downloads

Abstract

This paper presents the calculation results by a reactor model, numerical simulation in ANSYS Fluent CFD software, and the results of studying the flow structure and the burn-up fuel in the reverse-flow combustion chamber. These results are intended to create a methodology for further refinement of a combustion process in a combustion chamber.

Keywords

reverse-flow combustion chamber computational grid reactor model excess air coefficient temperature fields completeness of fuel combustion 

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References

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    Longwell, J.P. and Weiss, M.A., High Temperature Reaction Rates in Hydrocarbon Combustion, Industrial and Engineering Chemistry, 1955, vol. 47, no. 8, pp. 1634–1643.CrossRefGoogle Scholar
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    Doroshenko, V.E., On Combustion Process in the GTE Chambers, Trudy TsIAM, 1959, no. 354, p. 25–28.Google Scholar
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    Yankovskii, V.M., Modeling the Combustion Zone of GTE Combustors, Izv. Vuz. Av. Tekhnika, 1986, vol. 29, no.1, p. 73–76 [Soviet Aeronautics (Engl. Trans.), vol. 29, no. 1, pp. 85–90].Google Scholar

Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • W. M. Yousef
    • 1
    Email author
  • V. A. Sychenkov
    • 1
  • N. V. Davydov
    • 1
  • Yu. B. Aleksandrov
    • 1
  1. 1.Tupolev Kazan National Research Technical UniversityKazanRussia

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