This article describes and graphical clarify the air flow through the labyrinth seals of aircraft turbine engine. Evaluates the air flow data from the calculation and define the high temperature gradient in labyrinth seal.


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    Title :

    3D CFD Research of Labyrinth Seal Cavities of Aircraft Turbine Engine


    Contributors:
    Cizek, M. (author)


    Publication date :

    2019-09-01


    Size :

    591632 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English






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