Abstract The paper reports the results of experimental studies and numerical calculations of the flame stabilization process in the model gas turbine combustor. The mathematical model of the process in the combustor is presented. Using this model, the main parameters of combustors with different ratios of total area of the holes in the combustion zone to total area of all holes, are determined.


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    Titel :

    Study of flame stabilization in a model gas turbine combustor


    Beteiligte:
    Mingazov, B. G. (Autor:in) / Baklanov, A. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2016-07-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Study of flame stabilization in a model gas turbine combustor

    Mingazov, B. G. / Baklanov, A. V. | Online Contents | 2016


    Gas Turbine Combustor Stabilization by Heat Recirculation

    A. J. Ganji / J. Short / M. C. Branch et al. | AIAA | 1976


    Gas turbine combustor stabilization by heat recirculation

    GANJI, A. / SHORT, J. / BRANCH, M. et al. | AIAA | 1975


    Gas turbine combustor stabilization by heat recirculation

    Ganji, A. / Short, J. / Branch, M. | Tema Archiv | 1975


    Flame radiation in a gas turbine combustor

    Cummings,W.G. / Sojka,P.E. Lefebvre,A.H. / Purdue Univ.,US | Kraftfahrwesen | 1985