(3) The aerodynamic loads on an airplane wing can be approximated by the following figure below....

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(3) The aerodynamic loads on an airplane wing can be approximated by the following figure below. 22kN-m A 2.5-m 6kN-m B 5.5-m 3-kN a) Find the shear force and bending moment in the wing at 1.0-m intervals along the span starting from the free end using the integral method discussed in class. b) Find the maximum shear and bending moment in the wing (30 points) (3) The aerodynamic loads on an airplane wing can be approximated by the following figure below. 22kN-m A 2.5-m 6kN-m B 5.5-m 3-kN a) Find the shear force and bending moment in the wing at 1.0-m intervals along the span starting from the free end using the integral method discussed in class. b) Find the maximum shear and bending moment in the wing (30 points)