5-67. 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 Fon the ground. 8 ft 6 ft 8 ft 6 ft 4 ft 20 ft 3 ft

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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5-67. 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 W = 45 000 lb, WR = 8000 lb,
and Wc = 6000 lb, determine the normal reactions of the
wheels D, E, and Fon the ground.
B.
8 ft
4 ft
6 ft
8 ft
6 ft
20 ft
3 ft
Transcribed Image Text:5-67. 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 W = 45 000 lb, WR = 8000 lb, and Wc = 6000 lb, determine the normal reactions of the wheels D, E, and Fon the ground. B. 8 ft 4 ft 6 ft 8 ft 6 ft 20 ft 3 ft
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