Abstract The finite-difference method acceptable for on-board computers is applied to analyze the thermo-stressed state for the thermal-barrier coating of a perforated turbine blade and its wall at transient and stationary conditions of air-breathing jet engine operation during a flight.


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    Titel :

    Thermostressed state in turbine rotor blades with thermal barrier coating at transient conditions of air breathing jet engine operation


    Beteiligte:
    Trushin, V. A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2013-10-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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