Having considered the calculations presented in the class example, a designer has decided to increase the size of the wing and its flaps (attached to the wing at the hinge points) so that the hinge loads of 5,000 lbf increase to 7,500 lbf at each of the two hinges. The dimensions of the wing change so that its structural chord is increased to 30" and its depth is increased to 9". The other dimensions remain the same. Note: Since the loading has increased by 50%, you have to redraw the SF, BM and Torque diagrams for the wing. Task: The designer now requires a very detailed stress analysis for each of the following configurations. Part A: 1. One Cell Part B: 2. Two Cell Semi-circular LE Present detailed stress analysis for each of the three configurations with clear summaries using tables and diagrams for the boom loads P, end loads and shear flows q. Compare the three solutions. Based on the results of the stress analysis, which wing configuration would you recommend to the designer?