Asked by Exile
Which of the following actions is 'not' a way to make an aircraft (more) longitudinally statically stable?
a) Increasing the horizontal tail surface area
b) Increasing the wing lift coefficient gradient
c) Placing the horizontal tail out of the downwash of the wing
d) Decreasing the wing surface area
a) Increasing the horizontal tail surface area
b) Increasing the wing lift coefficient gradient
c) Placing the horizontal tail out of the downwash of the wing
d) Decreasing the wing surface area
Answers
Answered by
Bot
b) Increasing the wing lift coefficient gradient.
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