Shock models to be incorporated in an off-design performance prediction method for transonic axial flow compressor stages for more accurate flow prediction were developed. The improvement of shock models used for evaluating the shock losses, especially at supercritical subsonic, but also at supersonic inflow conditions, is emphasized. The methods were verified by calculating, investigating, and analyzing the losses of compressor cascades, as well as a transonic axial flow compressor.


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    Title :

    Theoretical and Experimental Investigations on Shocks Losses in Transonic Axial Flow Compressors


    Contributors:
    R. Dunker (author)

    Publication date :

    1988


    Size :

    231 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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