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Railways NTPC (Technical Ability) Turbomachinery Question Bank Turbomachinery

  • question_answer
    The Mach number at inlet of gas turbine diffuser is 0.3. The shape of the diffuser would be:

    A) Converging                    

    B) diverging I

    C) Stagnation enthalpy

    D) stagnation pressure

    Correct Answer: B

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