Problem 2: For the rectangular element shown determine the strain c., at the center of the elemen...
(0, 2) (4,2) (Coordinates in inch units) (4,0) (0, 0) 3. (5 point) For the element shown in Figure above (Problem 2), determine the stress matrix at s = 0.5773, t = 0.5773 using isoparametric formulation. The nodal displacements are given as Uj = 0) Vj = 0 U2 = 0.005 in. v2 = 0.0025 in. Uz = 0.0025 in. v3 = -0.0025 in. U4 = 0 04 = 0
Problem 2: For the beam shown in below figure, determine the nodal displacements and slopes, the forces in each element, and the reactions. 4 kN/ Im E 70 GPa 13 x 10-4 m4 4 m
structural analysis
Figure Q() Question 2 For the bar assemblages shown in Figure Q(2), determine the nodal displacements, the forces in each element and the reactions. Use the direct stiffness method (25 marks) 35 kN E-210 GPa 2 A4 x 10m2 1 m im
Figure Q() Question 2 For the bar assemblages shown in Figure Q(2), determine the nodal displacements, the forces in each element and the reactions. Use the direct stiffness method (25 marks) 35 kN E-210 GPa 2...
Problem No-3: The coordinates are shown in units of inches. Assume plane stress conditions. Let E 45x1 displacements have been determined to be u 1-0, v1 0.0025 in., u2 = 0.0012 in, v2 0.0001 in, u3 0, and v3 0.0025 in. Determine: (a) the stiffness matrix for the element shown [k] (b) the element stresses: ??, dy, and ? y and the principal stresses 06 psi, v = 0.25, and thickness t 1 in. The element nodal (15p) (20p) (0....
Problem 2: a. For the plane truss shown in Figure 2, determine the nodal displacements, the element forces and stresses, and the support reactions. All elements have E-70 GPa and A-25 cm 100 kN 50 kN 50 kN 4 4 6 Figure 2. Plane Truss
Problem 2: a. For the plane truss shown in Figure 2, determine the nodal displacements, the element forces and stresses, and the support reactions. All elements have E-70 GPa and A-25 cm 100 kN 50...
3.24 Determine the nodal displacements and the element forces for the truss shown in Figure P3-24. Assume all elements have the same AE 4 15 m 4 2 20 m Figure P3-24
3.24 Determine the nodal displacements and the element forces for the truss shown in Figure P3-24. Assume all elements have the same AE
4 15 m 4 2 20 m Figure P3-24
Part C - Average normal strain in the differential element of material Determine the average normal strain in the differential element of material. Express your answer to four significant figures. View Available Hint(s) IPO AQ 1 vec R o 2 ? Eaug in/in Submit Part B - Maximum in-plane shear strain and its orientation Determine the magnitude of the maximum in-plane shear strain, marame, and its orientation relative to the differential element of material. Express your answers to four significant...
For the spring assemblage shown in Figure 2-13, obtain (a) the global stiffness matrix, (b) the displacements of nodes 2-4, (c) the global nodal forces, and (d) the local element forces. Node l is fixed while node 5 is given a fixed, known displacement δ= 20.0 mm. The spring constants are all equal to k = 200 kN/m.
2. For the spring assemblages shown in Figures 2a through 2e, determine the nodal displacements, the forces in each element, and the reactions. k = 3000 lb/in. k =3000 lb/in. k = 3000 lb/in. 2000 lb 1000 lb 4 Figure 2a. k= 500 lb/in. a 3000 lb/in. 2000 lb V 4 Rigid bar_ k =500 lb/in. Figure 2b.