For the frame shown, compute and trace the shear and moment diagrams via: (a) Method of Sections (brutal force method),

Please help me with solution to Item 4 (Sub question No- 4) For the beam below: Draw the approximate deflected shape from the bending moment diagram. Develop the piecewise functions of θ(x) and v(x) using double integration. Assume EI is constant. Take x to be references from the farthest left point on the beam If w = 2 k/ft and L = 5 ft, locate the point of maximum deflection between supports A and B. Develop a variable based excel program that allows you to plot both the slope and displacement functions with x.  In other words, your program should be able to take any value of w, L, E, I and x and automatically calculate deflection and slope.  Print x-y scatter plots connected by smooth lines for both the deflection and slope using values of x ranging from 0 to 2L in increments of 0.5 ft.  Plot the displacement in inches and slope in radians for the following cases using your program: i) w = 2 k/ft, L = 5 ft, E = 4,176,000 ksf, I = 0.073784 ft4 ii) w = 10 k/ft, L = 6 ft, E =…

Please solve fully with diagrams as needed and for all parts of the question. Question:  a) What is deflected shape of the beam? b) Find dispacement of beam at point B using moment-area method. c) Find displacement of beam at point B using Castiglianos theorem. Assume EI is constant for all

Solve the problem by the moment-area method. The beam has constant flexural rigidity EI. A simple beam AB supports two concentrated loads P at the positions shown in the figure. B C 4. 4 A support C at the midpoint of the beam is positioned at distance d below the beam before the loads are applied. Assuming that d = 12 mm, L = 5.4 m, E = 200 GPa, and I = 193 x 10° mm, calculate the magnitude of the loads P (in kN) so that the beam just touches the support at C. 163.87 x kN