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The wing of a small plane is represented by a simplified prismatic cantilever beam model acted on by the distributed loads shown in the figure.

The wing of a small plane is represented by a simplified prismatic cantilever beam model acted on by the distributed loads shown in the figure. Assume constant EI = 1200 kN*m 2 . Find the tip deflection and rotation at B.

-1600 N/m 900 N/m 1.0 m 2.6 m - 2.6 m- 1600 N/m 900 N/m

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