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The Flame Stabilization and Calculation of the Stall Characteristics of Gas Turbine Engine Combustion Chamber

  • AIRCRAFT AND ROCKET ENGINE THEORY
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Abstract

The results are presented of the experimental and computational studies of the flame stabilization behind a swirler in an open flow and in a model compartment of the combustion chamber. Using the thermal theory, the calculation model of the flame stabilization in the combustion chamber is developed. Using this model, the calculation is carried out and the calculated and experimental data are compared.

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REFERENCES

  1. Kosterin, V.A., et al., Generalization of Experimental Data on Flame Stabilization in Jets, Izv. Vuz. Av. Tekhnika, 1968, vol. 11, no. 3, pp. 59–66.

    Google Scholar 

  2. Matveev, S.G., Orlov, M.Yu., Abrashkin, V.Yu., Zubrilin, I.A., and Matveev, S.S., Simulation of Aerodynamic Structure of the Flow in the Combustion Chamber of a Small-Size Gas Turbine Engine with the Help of CAE-Systems, Vestnik SGAU, 2011, no. 5 (29), pp. 179–187.

    Google Scholar 

  3. Mingazov, B.G., Kamery sgoraniya gazoturbinnykh dvigatelei: konstruktsiya, modelirovanie protsessov i raschet (Combustion Chambers of Gas Turbine Engines: Design, Simulation of Processes, and Calculation), Kazan: Izd. Kazan. Gos. Tekhn. Univ., 2006.

    Google Scholar 

  4. Mingazov, B.G. and Baklanov, A.V., Calculation of Main Parameters in a Burning Swirl Jet, Vestnik KGTU im. A.N. Tupoleva, 2013, no. 1, pp. 35–39.

    Google Scholar 

  5. Pomerantsev, V.V., Aref’ev, K.M., Akhmedov, D.B., et al., Osnovy prakticheskoi teorii goreniya (Fundamentals of Practical Combustion Theory), Leningrad: Energoatomizdat, 1986.

    Google Scholar 

  6. Bortnikov, M.T., Stabilization of the Combustion Process in Combustion Chambers, Trudy TsIAM, 1974, no. 613, pp. 48–53.

    Google Scholar 

  7. Baklanov, A.V., Investigation of Processes in the Combustion Chamber of a Converted Aircraft GTE in Order to Improve its Environmental Performance, Cand. Sci. (Tech.) Dissertation, Kazan, 2011.

  8. Mingazov, B.G. and Baklanov, A.V., Study of Flame Stabilization in a Model Gas Turbine Combustor, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 3, pp. 106–110 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 3, pp. 408–413].

    Google Scholar 

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, 420111, Kazan, Tatarstan, Russia

    B. G. Mingazov & A. V. Baklanov

Authors
  1. B. G. Mingazov
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  2. A. V. Baklanov
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Correspondence to A. V. Baklanov.

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Mingazov, B.G., Baklanov, A.V. The Flame Stabilization and Calculation of the Stall Characteristics of Gas Turbine Engine Combustion Chamber. Russ. Aeronaut. 63, 469–475 (2020). https://doi.org/10.3103/S1068799820030137

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  • DOI: https://doi.org/10.3103/S1068799820030137

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