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    Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection

    Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection


    The paper presents the results of determining the temperature of gas turbine plant shell. The total heat transfer from the engine is calculated. The thermal protection scheme by blowing air through the porous screen is proposed to reduce the temperature of the gas turbine plant shell as well as to reduce the total heat transfer from the engine to the surrounding compartment space.

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    Titel :

    Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection

    Weitere Titelangaben:

    Russ. Aeronaut.

    Beteiligte:
    Baklanov, A. V. (Autor:in) / Gimbitskii, A. V. (Autor:in)
    Erschienen in:

    Russian Aeronautics ; 62 , 3 ; 463-468

    Erscheinungsdatum :

    2019-07-01

    Format / Umfang :

    6 pages

    ISSN :

    1934-7901 , 1068-7998

    DOI :

    https://doi.org/10.3103/S1068799819030140

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    heat transfer , shell , gas turbine plant , thermal protection , air curtain , porous screen Engineering , Automotive Engineering

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