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MMChapter3 6 3D Rigid-Body Equilibrium 2025: Problem 2
(1 point)
Due to the 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 with the following
dimension:
d_(1)=5ft
d_(2)=4ft
d_(3)=17ft
d_(4)=14ft
d_(5)=6ft
d_(6)=7ft
d_(7)=13ft
If these components have weights W_(A)=10000lb,W_(B)=3500lb and W_(C)=3000lb, determine the normal reactions of the wheels D,E, and F on the ground using
the following dimensions: