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Discussion :: GATE Aeronautical Engineering

  1. An aircraft in trimmed condition has zero pitching moment at
    2. A.
    its aerodynamic centre.
    B.
    its centre of gravity.
    C.
    25% of its mean aerodynamic chord.
    D.
    50% of its wing root chord.

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    Answer : Option B

    Explanation :

    -NA-

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