Aerospace Engineering > GATE 2012 > Aircraft Stability
An aircraft in trimmed condition has zero pitching moment at
A
its aerodynamic centre.
B
its centre of gravity.
C
25% of its mean aerodynamic chord.
D
50% of its wing root chord.

Correct : b

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Related Topics

aerospace engineering GATE 2012 aircraft trimmed condition zero pitching moment aerodynamic centre centre of gravity aircraft stability pitching moment at trim

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