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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:

    Aerospace system science and engineering (4th international conference)



    Publication date :

    2021-01-01


    Size :

    14 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Computational Method in the Throughflow Simulation of Aeroengine Compressor

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


    Computational Method in the Throughflow Simulation of Aeroengine Compressor

    Tao, Qitian / Jin, Hailiang / Liu, Xiaohua | TIBKAT | 2021



    A ROBUST DESIGN METHODOLOGY FOR HIGH-PRESSURE COMPRESSOR THROUGHFLOW OPTIMIZATION

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