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, WB and WC,...

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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, WB and WC, determine the normal reactions of the wheels D, E, and F on the ground.
Units Used:
kip = 103 lb
Given:
WA = 45000 lb
WB = 8000 lb
WC = 6000 lb
a = 8 ft e = 20 ft
b = 6 ft f = 4 ft
c = 8 ft g = 3 ft
d = 6 ft

Answered Same Day Dec 29, 2021

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David answered on Dec 29 2021

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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, WB and WC,...

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