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. Draw a free-body diagram of the airplane. If these components have weights W_A = 43000lb , W_B = 8000 lb, and W_C = 6000 lb determine the normal reactions of the wheels D, E, and F on the ground.

Respuesta :

The normal reactions of the wheel is determined as 13222.22 lb at point F and 21888.89 lb for point E and D.

Free body diagram of the plane is drawn by removing all the supports and replacing with forces. Equilibrium of moment of forces about x-axis is considered and relation between the reaction forces at point D and E is determined. Equilibrium of moment of forces about y-axis is considered and value of the reaction force at point F is determined. Moment of axis (line) is considered to eliminate an unknown force and get equation with other two variables.

After drawing the free body diagram, apply force balance about x-axis:

= ∑Mₓ = 0

= - (R₄ X 14) + (R₅ X14) + (W₂ X 6) - (W₃ X 8) = 0

= (R₅ - R₄) X 14 =  (W₃ X 8) - (W₂ X 6)

= R₅ = R₄

Apply moment balance about y axis,

= ∑Mₙ = 0

= - (R₆ X 27 ) + (W₁ X 7) + (W₂ X 4) + (W₃ X 4) = 0

= R₆ = 13222.22 lb

Next, consider force equilibrium equation.

Write the force equilibrium equation along vertical axis, z-axis;

= ∑F = 0

= R₆ + R₅ + R₄ - (W₁ + W₂ + W₃) = 0

where, R represents reaction and W represents load.

= R₆ + R₅ + R₄ - (W₁ + W₂ + W₃) = 0

= R₅ = R₄ = 21888.89 lb

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