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. %3D

International Edition---engineering Mechanics: Statics, 4th Edition
4th Edition
ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
Publisher:Andrew Pytel And Jaan Kiusalaas
Chapter10: Virtual Work And Potential Energy
Section: Chapter Questions
Problem 10.9P: The four-bar linkage supports the homogeneous box of weight W. Neglecting the weight of the linkage,...
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4 of 4
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, WR = 8000 lb,
and Wc = 6000 lb, determine the normal reactions of the
wheels D, E, and F on the ground.
8 ft
4 ft
6 ft
8 ft
6 ft
20 ft
3 ft
Transcribed Image Text:4 of 4 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, WR = 8000 lb, and Wc = 6000 lb, determine the normal reactions of the wheels D, E, and F on the ground. 8 ft 4 ft 6 ft 8 ft 6 ft 20 ft 3 ft
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