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

Transcribed Image Text:

B.