Question: Problem 1 Under cruising conditions, the distributed load acting on the wing of a small airplane has the idealized variation shown in figure. a .

Problem 1
Under cruising conditions, the distributed load acting on the wing of a small airplane has the idealized variation shown in figure.
a. Find the shear force V and bending moment M for each section of the wing.
b. Determine the maximum deflection at the tip of the beam.
Assume that the shape of the load is as the following:
 Problem 1 Under cruising conditions, the distributed load acting on the

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