The aerodynamic lift of the wing is described by the distributed load w = -3001-0.04x N/m....

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The aerodynamic lift of the wing is described by the distributed load w = -300√1-0.04x² N/m. The mass of the wing is 27kg, 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. (b) Determine the reactions on the wing at R. -2 m- 5 m 1 The aerodynamic lift of the wing is described by the distributed load w = -300√1-0.04x² N/m. The mass of the wing is 27kg, 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. (b) Determine the reactions on the wing at R. -2 m- 5 m 1 The aerodynamic lift of the wing is described by the distributed load w = -300√1-0.04x² N/m. The mass of the wing is 27kg, 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. (b) Determine the reactions on the wing at R. -2 m- 5 m 1 The aerodynamic lift of the wing is described by the distributed load w = -300√1-0.04x² N/m. The mass of the wing is 27kg, 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. (b) Determine the reactions on the wing at R. -2 m- 5 m 1