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    Title :

    Computational Method in the Throughflow Simulation of Aeroengine Compressor


    Contributors:
    Tao, Qitian (author) / Jin, Hailiang (author) / Liu, Xiaohua (author)

    Conference:

    International Conference on Aerospace System Science and Engineering ; 4. ; 2020 ; Online



    Publication date :

    2021



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik
    DDC:    629.1



    Computational Method in the Throughflow Simulation of Aeroengine Compressor

    Tao, Qitian / Jin, Hailiang / Liu, Xiaohua | Springer Verlag | 2021


    Coupling-Optimization Method for Aeroengine Performance Simulation

    Wang, X. / Zhang, S. / Du, H. et al. | British Library Conference Proceedings | 1999



    Throughflow Theory

    Oates, Gordon C. | AIAA | 1997


    A ROBUST DESIGN METHODOLOGY FOR HIGH-PRESSURE COMPRESSOR THROUGHFLOW OPTIMIZATION

    Lecerf, N. / Jeannel, D. / Laude, A. et al. | British Library Conference Proceedings | 2003