Discussion
The free-elevator factor in the stick-free tail contribution depends on
Answer: C
The factor is built from \( \tau C_{h_\alpha}/C_{h_\delta} \), so it combines the float tendency with how much moment a degree of elevator produces. Area enters through those derivatives rather than on its own. Elevator mass and its balance weight matter for flutter and for inertia effects in manoeuvres, not for the steady float. Stick gearing scales the force the pilot feels but cannot change where the surface floats to, since floating happens with the stick free.
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