Research related to understanding and modeling aerodynamic loss production in axial-flow compressors was accomplished. Some progress in clarification of loss prediction was attained. Suggestions for incorporating wake interaction effects in axial-flow compressor design calculations are offered. Some of the inherent complications associated with supersonic blade testing are noted. Further study of specific details of loss generation is proposed.


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    Title :

    Aerodynamic Loss Sources in Axial-Flow Compressors


    Contributors:

    Publication date :

    1986


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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