The basic differential equation of the elastic curve for a simply supported, uniformly loaded beam, as shown in the Figure below, is given as:
wLx - Wx^2 EI dx^2 = 0
where E is the modulus of elasticity and I is the moment of inertia. The boundary conditions are y(0) = y(L) = 0. Solve for the deflection y of the beam using the Finite-Difference Method with x = 1m manually (but use MATLAB as your computational aid is permitted). The following parameter values apply: E = 200 GPa, I = 30,000 cm^4, w = 15 kN/m, and L = 6m. Show your work! Please upload MATLAB commands you used, calculation results, and plot (copy and paste to a Word or PDF file on Brightspace under Exams category in Assessments/Assignments).