Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the airplane fuselage A and wings B and C are located as shown. If these components have weights WA = 45 000 lb, Wg = 8000 lb, and Wc = 6000 Ib, determine the normal reactions of the wheels D, E, and F on the ground.
Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the airplane fuselage A and wings B and C are located as shown. If these components have weights WA = 45 000 lb, Wg = 8000 lb, and Wc = 6000 Ib, determine the normal reactions of the wheels D, E, and F on the ground.
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
Transcribed Image Text:Due to an unequal distribution of fuel in the wing tanks, the
centers of gravity for the airplane fuselage A and wings B
and C are located as shown. If these components have
weights WA = 45 000 lb, Wg = 8000 lb, and Wc = 6000 lb,
determine the normal reactions of the wheels D, E, and F
on the ground.
Bo
8 ft
4 ft
6 ft
8 ft
6 ft
20 ft
3 ft
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