solve by using matlab

A2-1 Figure-a shown below shows a simply supported beam subjected to uniformly distributed load. w=12 kN/m B B A L=6m Figure (1): Simply supported beam The deflection equation for this beam can be computed as; wx Ya = 24E1 (2-2Lx' +x2) Where the modulus of elasticity and I the moment of inertia. KN E = 200 x 106 and I = 300 x 10-6 m2 Part a) Find the maximum deflection in the beam. Part b) Plot deflection ya versus length of beam X (Length on x-axis) Hint: X ranges from 0 to L. (use x = 0 to 6 with intervals of 0.5 and get the maximum value of deflection) Parte) Calculate the maximum shear force V (kN) in the beam. wL 2 Part d) Find the maximum bending moment M (kN-m) in the beam and draw the bending moment diagram with clearly pointing the maximum bending moment value on the figure. M = 36(x) - 6(x2) Hint: X ranges from 0 to L. (use x = 0 to 6 with intervals of 0.5 and get the maximum value of moment). To draw the bending moment diagram, plot (x.M) e) Use subplot command to plot graphs of part b and d together 1 Rearrange distance (x), deflection (y), shear (v), moment (m), in six columns as appropriate using fprintf function