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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    Titel :

    Aerodynamic Loss Sources in Axial-Flow Compressors


    Beteiligte:
    T. H. Okiishi (Autor:in) / G. K. Serovy (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    38 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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