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).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Unsteady Euler cascade analysis


    Weitere Titelangaben:

    Analyse von instationaeren Euler-Kaskaden


    Beteiligte:
    Lin, J. (Autor:in) / Sockol, P. (Autor:in)

    Erschienen in:

    AIAA-Papers ; Jan ; 1-7


    Erscheinungsdatum :

    1989


    Format / Umfang :

    7 Seiten, 11 Bilder, 10 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Unsteady Euler cascade analysis

    LIU, JONG-SHANG / SOCKOL, PETER | AIAA | 1989


    Euler Analysis of Oscillating Cascade Unsteady Aerodynamics Using Embedded Composite Grids

    Wolff, J. M. / Fleeter, S. / AIAA | British Library Conference Proceedings | 1994



    Finite element Euler calculations of unsteady transonic cascade flows

    HSIAO, CHINGTENG / BENDIKSEN, ODDVAR | AIAA | 1992