Effects of unsteady flow interactions on the aerodynamic performance of a highly-loaded transonic axial compressor are investigated in the present study. The primary focus of the study is to investigate how unsteady flow interactions between blade rows affect the aerodynamic performance of a highly-loaded transonic axial compressor. Recent experimental and numerical studies of current highly-loaded axial compressor performance indicated that predicting calculating the loss generation is very challenging with various analysis tools. In the present study, the effects of generation and transport of shock induced vortices on the compressor performance is investigated in detail.


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    Title :

    Effects of Unsteady Flow Interactions on the Performance of a Highly-Loaded Transonic Compressor Stage


    Contributors:
    C. Hah (author)

    Publication date :

    2015


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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