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Question 1 of 10
Fex
easy
The leading edge slats and trailing edge flaps extend the aircraft's usable speed range by:
A
Increasing wing sweep to delay compressibility effects at low speeds
B
Increasing wing camber and area, raising maximum lift coefficient (CLmax) for lower stall speed
C
Increasing wing dihedral to improve lateral stability at low speeds
D
Reducing induced drag at low speeds for better climb performance
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