The mid-wing type configuration ion of the USAF F-16c wing (see Figure 1a), can be idealized as a cantilever beam with a uniformly distributed load. that accounts for the weight of the wing as given in Figure 1b. The cantilever deflects under the action of the distributed load, as given in eqn. 1 with a slope given in eqn. 2. USAF F-16c Dimensions and loading conditions of a cantilever beam and its cross-section Deflection and Slope of the cantilever delta(x) = pi_0 x^2/24 EI (6L^2 - 4Lx + x^2) theta(x) = w_0x/6 EI(3L^2 - 3Lx + x^2) where delta(x) and theta(x) are the defection and slope respectively at location x of the cantilever beam of span L_0. w 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 bh^2/12. Develop a C++ program that prompts the user for the input values 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 purpose 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 detection and slope respectively. Format for creating the output display Declare all real variables as "double" in your program. The mid-wing type configuration ion of the USAF F-16c wing (see Figure 1a), can be idealized as a cantilever beam with a uniformly distributed load. that accounts for the weight of the wing as given in Figure 1b. The cantilever deflects under the action of the distributed load, as given in eqn. 1 with a slope given in eqn. 2. USAF F-16c Dimensions and loading conditions of a cantilever beam and its cross-section Deflection and Slope of the cantilever delta(x) = pi_0 x^2/24 EI (6L^2 - 4Lx + x^2) theta(x) = w_0x/6 EI(3L^2 - 3Lx + x^2) where delta(x) and theta(x) are the defection and slope respectively at location x of the cantilever beam of span L_0. w 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 bh^2/12. Develop a C++ program that prompts the user for the input values 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 purpose 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 detection and slope respectively. Format for creating the output display Declare all real variables as "double" in your program