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The static margin is the distance between

  • A.The neutral point and the wing leading edge
  • B.The neutral point and the centre of gravity
  • C.The wing and tail aerodynamic centres
  • D.The forward and aft centre of gravity limits

Answer: B

Correct answer: The neutral point and the centre of gravity

The static margin is

\[ K_n = \frac{x_{np} - x_{cg}}{\bar{c}} \]

expressed as a fraction of the mean aerodynamic chord. It is positive, and the aircraft statically stable, when the centre of gravity lies forward of the neutral point.

The neutral point is a property of the aerodynamic configuration; the centre of gravity moves with loading. So the aft centre of gravity limit is set by the minimum margin the design requires, typically around 5 per cent for a transport, and the fourth option confuses that limit with the margin itself.

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