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Problem 4: The aerodynamic lift of the wing is described by the distributed load w = 300/l 0.0.112 Him. The mass of the wing is
Problem 4: The aerodynamic lift of the wing is described by the distributed load w = 300\\/l 0.0.112 Him. The mass of the wing is 21'kg' and its center of mass is located 2m from the wing root R. (a) Determine the magnitude of the force and the moment about R exerted by the lift of the wing. (in) Determine the reactions on the wing at R. N
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