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2) A 10-ft long rigid wing is modeled as the cantilevered beam AB in the figure. The lift of the wing is modeled as

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2) A 10-ft long rigid wing is modeled as the cantilevered beam AB in the figure. The lift of the wing is modeled as w(x) = 3x lb/ft, with x = 0 at the left end (A). Ignoring the weight of the wing: w(x) - 3xx 109 a) Draw the free-body-diagram. b) Calculate the reactions at the fuselage (point B) which is fixed. c) Calculate the centroid of the load w(x). B

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