A drawing of a scale model aircraft flying at constant velocity in level flight is shown.
Assume that the lift acts as a point load only on each wing and is located as shown in the drawing.
- In the box below, draw the free body diagram of the forces acting on the aircraft. (1 mark)
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- Draw both a shear force diagram and a bending moment diagram of the aircraft as the forces act across the wingspan of the aircraft. (5 marks)
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