The description of the structural features of the working shoulder blade with the inflow in the root portion and the results of the comparative numerical simulation of the three-dimensional flow of ordinary and proposed work blades designed for the transonic level of the compressor


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    Title :

    Workbench for the first stages of gas turbine engine compressors




    Publication date :

    2002




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown





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