Railways NTPC (Technical Ability) Turbomachinery Question Bank Turbomachinery

  • question_answer
    In axial flow compressor, exit flow angle deviation from the blade angle is a function of:

    A) Blade camber

    B) space-chord ratio

    C) Both blade camber and space-chord ratio       

    D) Blade camber and incidence angle 

    Correct Answer: C


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