Max. Points: 20 ASSIGNMENT 4 Problem -1: The mid-wing type configuration of the USAF F-16c wing (see Figure la), can be idealized as a cantilever beam with a uniformly distributed load, that accounts for the weight of the wing as given in Figure 1. The cantilever deflects under the action of the distributed load, as given in eqn. 1 with a slope as given in eqn. 2. Figure 1: (a) USAF F-160 (b) Dimensions and loading conditions of a cantilever beam and its cross-section Deflection and Slope of the cantilever 6(r) (6L' (1) 24EI 6(z) 3L (2) 6EI where 5(r) and 6(r) are the deflection and skape respectively at location r of the cantilever beam of span La- is the distributed load. E is the Young's Modulus of the material of the beam and I is the area moment of inertia of the rectangular cross-section given as a. Develop a C++ program that prompts the user for the input val and the output displayed on the screen in a tabular form as given in Table 1. The program should first display information regarding the assignment and its purpoese along with your identity, before prompting the user for the input- The program should also have two functions Beam-Deflection, and Beam-Slope that will calculate the deflection and slope respectively. 12 Points