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Discussion :: Compressors, Gas Turbines and Jet Engines

  1. Propulsive efficiency is defined as ratio of

    2. A.

     Thrust power and fuel energy
    B.

     Engine output and propulsive power
    C.

     Propulsive power and fuel input
    D.

     Thrust power and propulsive power

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    Answer : Option D

    Explanation :

    Propulsive efficiency is defined as ratio of Thrust power and propulsive power

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