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Discussion :: Compressors,Gas Dynamics and Gas Turbines

  1. In axial flow compressor, exit flow angle deviation from the blade angle is a function of

    2. A.
    blade camber
    B.
    blade camber and incidence angle
    C.
    space-chord ratio
    D.
    blade camber and space-chord ratio

    View Answer

    Workspace

    View Answer

    Answer : Option B

    Explanation :

    No answer description available for this question.

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