Draw shear and moment diagrams for the fuselage structure

The fuselage loads is shown below. The wing structure with fuel included weighs a total of 45,000 Ib and is assumed to act at station 400 . The horizontal tail weighs a total of $5000 lb$ and acts at station 900 . The fuselage weighs a total of $100, 000 lb$ , and its weight is assumed to be evenly distributed along the length of the structure. The wing lift $L_{W}$ is assumed to carry 90 percent of the total load, and the tail surface lift $L_{T}$ is assumed to carry the remaining 10 percent of the load.

Question

Draw shear and moment diagrams for the fuselage structure

The fuselage loads is shown below. The wing structure with fuel included weighs a total of 45,000 Ib and is assumed to act at station 400 . The horizontal tail weighs a total of

5000 lb

and acts at station 900 . The fuselage weighs a total of

100, 000 lb

, and its weight is assumed to be evenly distributed along the length of the structure. The wing lift

L_{W}

is assumed to carry 90 percent of the total load, and the tail surface lift

L_{T}

is assumed to carry the remaining 10 percent of the load.

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