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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2013-10-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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