following characteristics: The loading profile acting on the wing of a Spitfire MK XVI has the The wing weighs 800 lbf and is uniformly distributed (i.e., 40 lbf/ft) The is also subjected to inertial forces of 7,200 lbf also uniformly distributed (i.e., 360 lbf/ft) The wing is 20 feet in length. 1. Make a cut and draw a free body diagram (FBD) with all the external forces acting on the body. 2. Determine the reaction forces using the equations of equilibrium and calculate the normal for N, the shear force V, and bending moment M at the wing root, in red (i.e., the part of the wing that is closest or connect to the fuselage). 3. Draw shear and bending moment diagram and calculate the maximum moment and shear force.