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W 1. The aerodynamic lift of the wing is described by the distributed load of w = -3001-0.04x2 N/m. The mass of the wing
W 1. The aerodynamic lift of the wing is described by the distributed load of w = -3001-0.04x2 N/m. The mass of the wing is 27 Kg, and its center of mass is located 2 m from the wing root K. Cb = 2m from Root M - R C6 2 m 5 m a. Determine the magnitude of the lift force. b. Determine the reaction force and the moment about R. X
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