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    Title :

    Achieving high parallel performance for an unstructured unsteady turbomachinery CFD code


    Contributors:
    Hills, N. (author)

    Published in:

    The aeronautical journal ; 111 , 1117 ; 185-194


    Publication date :

    2007



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.50 / 55.60
    Local classification TIB:    275/7040




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    Computation of turbomachinery flow with an unstructured CFD code

    Bhale, P. V. / Shembharkar, T. R. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000


    Unsteady Turbomachinery Computations Using Massively Parallel Platforms

    van der Weide, Edwin / Kalitzin, Georgi / Schluter, Jorg et al. | AIAA | 2006


    Solution-adaptive structured-unstructured grid method for unsteady turbomachinery analysis. II - Results

    Mathur, Sanjay R. / Madavan, Nateri K. / NASA, Ames Research Center et al. | AIAA | 1994