81-04. Stability
All questions: 154
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1. In what way is the longitudinal stability affected by the degree of positive camber of the aerofoil?
2. Where must the CG be located?
3. In relation to the manoeuvre point, the aft CG limit is:
4. The effect of a ventral fin on the static stability of an aero plane is as follows: (1 = longitudinal, 2 = lateral, 3 = directional)
5. The effects of CG position on longitudinal static stability and control response will be:
