Program developed for computing aerodynamic design of multistage axialflow compressor and associated blading geometry input for internal flow analysis. Aerodynamic solution gives velocity diagrams on selected streamlines of revolution at blade row edges. Program written in FORTRAN IV.


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    Title :

    Design of Multistage Axial-Flow Compressors


    Contributors:

    Published in:

    Publication date :

    1983-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Reverse flow in multistage axial compressors

    GAMACHE, R. / GREITZER, E. | AIAA | 1986


    Reverse flow in multistage axial compressors

    GAMACHE, R. N. / GREITZER, E. M. | AIAA | 1990



    Parametric study of advanced multistage axial-flow compressors

    Miller, M. L. / Bryans, A. C. | TIBKAT | 1967