Case 1: Uniform beam under distributed load.
In the shown Figure, a uniform beam subject to a linearly increasing distributed load. The deflection y (m) can be expressed by
y=w_o/120EIL (-x^5+2L^2 x^3-L^4 x)
Where E is the modulus of elasticity and I is the moment of inertia (m4), L length of beam. Use the following parameters L=600 cm, E=50,000 kN/cm2, I= 30.000 cm4, wo=2.5 kN/cm, to find the requirements
Develop MATLAB code to determine the point of maximum deflection by using numerical method (bisection, false position method,….). Hint(The value of x where dy/dx=0). Plot the point of maximum deflection versus iteration number. Plot the values of the relative approximate error of the point of maximum deflection (ϵ_(a,x)) versus iteration number.
Plot the following quantities versus distance along the beam Displacement (y). Slope θ(x)=dy/dx. Moment M(x)=EId^2 y/dx^2. Shear V(x)=EId^3 y/dx^3. Loading w(x)=-EId^4 y/dx^4.
