Two-volume report describes experimental study of flow of air around double-circular-arc turbine blade in cascade of such blades. Provides well-documented, somewhat-complicated flow field used to develop or test future computer codes for simulation of such viscous-flow fields.


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    Title :

    Measurements Of Boundary Layers On A Compressor Blade


    Contributors:

    Published in:

    Publication date :

    1991-04-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



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