Using the cut method, draw the shear and moment diagrams for the beam, and calculate the shear and moment throughout the beam as functions of x. 2 N/m 6m 10 N m- 8 N 40 Nm

Beam AC is in equilibrium with loading 100 N at B shown in the figure when β = 45. Determine the unknown forces Ax and Ay at A in x and y direction and Rc perpendicular to the beam AC in y’ direction at C by using the equilibrium equations: ∑ ???= 0 ; ∑ ??y= 0; and ∑ ???= 0 where o is an arbitrary point. (you have three equations to solve three unknowns)

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

sketch the deflected structure of this frame (just shape no exact values for how much deflection). This is linear analysis so only looking at the displacement of the nodes. Note that D is a hinge support, E is fixed and C is a roller

Q.2) (a) Calculate the support reactions of the loaded beam shown below. (b) Write equations for w(x), V(x) and M(x) of the beam using singularity functions. (c) Sketch the shear-force and bending moment diagrams for the beam for the beam using the Graphical method. Label the values of shear-force and bending-moment at all key points. 350 N.m G 0.5 m4 2m 95 N/m, 200 N 250 N.m 80 N/m 2m 300 N 0.5 m