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Aerodynamics and Basic Flight Mechanics

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If the origin, o, is located at the wing tip and the leading & trailing edge curve is given above, find the constant c at the wing root and then calculate the chord of the wing at position 2 and position 3 as indicated in figure 1. (Marks Breakdown: find constant c [2 marks], chord pos. 2 [2], chord pos. 3 [2], workings shown [4]) [10 marks] (b) (i) Develop expressions for the shear force and bending moment distribution along the length of the wing as a function of distance, x, measured from ...


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