The results of an investigation of the rotor-stator interaction phenomena in turbomachines are presented. Numerical study was carried out by solving the unsteady Euler equations in the blade-to-blade direction for a variety of cascade geometries. The problem of uneven rotor and stator blades is addressed by adopting the tilted time domain technique. Computed solutions are presented and discussed for a NACA 0012 type cascade and the first stage fuel turbopump of the Space Shuttle Main Engine (SSME).


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    Title :

    Unsteady Euler cascade analysis


    Additional title:

    Analyse von instationaeren Euler-Kaskaden


    Contributors:
    Lin, J. (author) / Sockol, P. (author)

    Published in:

    AIAA-Papers ; Jan ; 1-7


    Publication date :

    1989


    Size :

    7 Seiten, 11 Bilder, 10 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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