User:Eas4200c.f08.carbon.orear/HW5/MATLABMotivation

=MATLAB Motivation=

This homework adds T-brackets to the previous assignments and exams how it affects the airfoil. Given cross-sectional areas, the new centroid, area, inertia, highest bending moment and highest bending stress will be computed. For the second part, the same is computed but now including bending moment effects (given). Then the highest bending moments are observed in the stringers (not the skin) and the ultimate bending moment is found and compared. 

contribution by carbon.w