For the beam and loading shown, and knowing that distance a = 2m, determine the maximum value of the distributed load W so the deflection at midpoint C does not exceed 5 mm Use E = 200 GPa and Ix = 333 x 106 mm4.
For the beam and loading shown, and knowing that distance a = 2m, determine the maximum...
For the beam and loading shown, determine the vertical reaction at the support located at A. The distributed load w = 10kN/m, and the beam W 310 x 52 has a moment of inertia Ix = 119 x 106 mm4 and modulus of elasticity E = 200 GPa ЕВ с 2 m- 4 m
Question 4 (25 marks) For the beam and loading shown in Figure 4, knowing that a GPa, determine (a) the slope at support A, (b) the deflection at point C. (using integration method) 2m, w 50KN/m and E 200 80 w 20 60 Unit: mm A 10 60 В а 20 6 m 80 (a) Beam loading (b) Cross section Figure 4
Question 3 For the simply supported steel beam with cross section and loading shown (see Figure 3a), knowing that uniformly distributed load w=60 kN/m, Young modulus E = 200 GPa, and yield stress Cyield=200 MPa (in both tension and compression). ул 15 mm w=60 kN/m ... 1 B A 15 mm + 300 mm IC - i 2.5m 1 1 15 mm 7.5m 1 150 mm Figure 3a (a) Check if: the beam is safe with respect to yielding (using...
2. The governing differential equation that relates the deflection y of a beam to the load w ia where both y and w are are functions of r. In the above equation, E is the modulus of elasticity and I is the moment of inertia of the beam. For the beam and loading shown in the figure, first de m, E = 200 GPa, 1 = 100 × 106 mm4 and uo 100 kN/m and determine the maximum deflection. Note...
Using Finite Element with a minimum of 3 elements (Penalty Approach). For the beam and loading shown, determine (a) the slope at the end A, (b) the deflection at point C. Use E= 200 GPa And I = 6.83 x 106 mm4 or the beam and loading shown, determine (a) the slope at end A, (6) the deflection at point C. Use E 200 GPa and I -6.83 x 10+6mm4 Use FEM with a minimum of 3 elements(Penalty Approach). 20...
The simply supported beam consists of a W410 × 60 structural steel wide-flange shape [E = 200 GPa; I = 216 × 106 mm4]. For the loading shown, determine the beam deflection at point C. Assume P = 53 kN, w = 91 kN/m, LAB = LBC = 1.7 m, LDE = LCD=1.8 m, MA = 197 kN-m. 200 GPa; I 216 x 100 mm ]. For the loading shown, determine the beam The simply supported beam consists of a...
5. For the beam and loading shown, and wo-1000 N/m, L-3 m, and E-200 GPa. Determine (a) the equation of the elastic curve, and (b) the maximum deflection. Wo 8 mm 300 DT 8 mm ト150mm 〒8mm 150 mm
P10.047 (Multistep) The simply supported beam shown in the figure consists of a W410 x 60 structural steel wide-flange shape [E = 200 GPa; I = 216 x 100 mm"]. For the loading shown, determine the beam deflection at point B. Assume P = 88 kN, w = 94 kN/m, M = 162 kNm, and d= 1.5 m. .PL IIIIIIIIIIIII Part 3 Neglect the concentrated moment M and the concentrated load P and determine the deflection at B due to...
For the cantilever beam and loading shown, use the method of superposition to determine (a) the slope at point A, (b) the deflection at point A. Use E 200 GPa. Hint: Use the expression found in Problem 1 for the tri angular load. 120 kN/m W360 × 64 20 kN 2.1 m
The simply supported beam consists of a W410 × 60 structural steel wide-flange shape [E = 200 GPa; I = 216 × 106 mm4]. For the loading shown, determine the beam deflection at point C. Assume P = 72 kN, w = 60 kN/m, LAB = LBC = 1.4 m, LDE = LCD=1.4 m, MA = 167 kN-m. P10.048 Not Correct 216 x 106 mm41. For the loading shown, determine the beam deflection at point C The simply supported beam...