An analysis yields a model for energy transfer in compressor stages operating in the closed-throttle condition. The derivation indicates that three geometry parameters (hub/tip ration, aspect ration, and rotor blade setting angle) influence the values of pressure coefficient when the compressor flow is close to zero.


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    Title :

    Analysis of Fully Stalled Compressor


    Contributors:

    Publication date :

    1986


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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