Operating range of turbomachinery for which stability calculated extended. TIPS (Two In-Passage Shocks) calculates unsteady lifts and moments on compressor blade if relative mach number supersonic and if two shock waves in blade passage. Written in FORTRAN IV and run on IBM 3033 with 370TSS operating system.


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    Title :

    Unsteady Flow In A Supersonic Cascade With Shocks


    Contributors:

    Published in:

    Publication date :

    1988-05-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Unsteady Supersonic Cascade in Subsonic Axial Flow

    JOSEPH M. VERDON AND JAMES E. McCUNE | AIAA | 1975



    The unsteady supersonic cascade in subsonic axial flow

    VERDON, J. / MCCUNE, J. | AIAA | 1975


    Unsteady flow in a supersonic cascade with subsonic leading-edge locus

    Adamczyk, J. J. / Goldstein, M. E. | NTRS | 1978