The inadequacy of axisymmetric theory in modeling the structure of the shock system in a transonic compressor rotor is shown with a simple model. A more accurate model for the flow near the sonic radius is proposed, which is supported by some flow visualization data and three-dimensional computations.


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    Title :

    Shock structure in transonic compressor rotors


    Contributors:

    Published in:

    Publication date :

    1979-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Shock Structure in Transonic Compressor Rotors

    A. H. Epstein / J. L. Kerrebrock / W. T. Thompkins | AIAA | 1979


    Tip shock structures in transonic compressor rotors

    SELLIN, M. / PUTERBAUGH, STEVEN / COPENHAVER, WILLIAM | AIAA | 1993