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The beam shown in the figure consists of a W360 79 structural steel wide-flange shape [E...
P11.046 (Multistep) A W530 X 66 structural steel [E = 200 GPa) wide-flange shape is loaded and supported as shown in the figure. A uniformly distributed load of w = 66 kN/m is applied to the beam, causing the roller support at B to settle downward (i.e., displace downward) by d = 8 mm. Determine: (a) the reactions at supports A and B. (b) the maximum bending stress in the beam. Assume a = 5.5 m and b = 1.3...
The beam shown in the figure consists of a W360x19 structural steel wide-flange shape [E = 200 GPa; = 225 ×106 mm": Mo-210 kN·m; w-90 kN/m, a _ 4 m, and b-5ml Me Determine the deformation at B due to the distributed load if the roller support at B is removed. 0.0972 m 0.1324 m 0.1444 m 0.1682 m 0.1599 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 = 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...
The simply supported beam consists of a W460 × 82 structural steel wide-flange shape [E = 200 GPa; I = 370 × 106 mm4]. For the loading shown, determine the beam deflection vC at point C. Assume P = 62 kN, w = 36 kN/m, LAB = LBC = 3.9 m, LCD = 1.9 m. Chapter 10, Supplemental Question 053 Not Correct The samply supported beam cons sts o a W460 × 82 structural steel wide flange shape E :...
Problem 2 Problem Statement A W310x33 wide-flange A36 steel beam is used for the application shown below. 10 kN 20 kN 20 KN 10 KN B --Im-eIm-e-Im -Im -Im-- Using beam theory, determine the maximum tensile and compressive bending stress you would expect in this problem and determine where those stresses would occur. Using the theory of elasticity finite element model available here, create a plot which verifies the stress distribution and the values predicted by beam theory at the...
P10.023 The simply supported beam consists of a W410 x 85 structural steel wide-flange shape [E - 200 GPa? - 316 x 10 mm. For the loading shown, use discontinuity functions to computer (a) the slope of the beam at A, and (b) the deflection of the beam at midspan. Assume LA - LCD - 2.1 m, lec-3.0 m, w = 64 kN/m. Answers: (a) 0 L (b) ...The number of significant digits is set to estion Open Show Work
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...
A column with a wide-flange section has a flange width b = 400 mm , height h = 400 mm , web thickness tw = 13 mm , and flange thickness tf = 21 mm (Figure 1). Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 3 kN at the centroid, shear force V = 7.4 kN , and bending moment M = 4 kN⋅m as shown...
The beam shown will be constructed from a standard steel W-shape using an allowable bending stress of 150 MPa. Assume L=3.4 m, wA-44 kN/m and P-11 kN (a) Develop a list of four acceptable shapes that could be used for this beam. Include the most economical W310, W360, W410, and W460 shapes on the list of possibilities. (b) Select the most economical W shape for this beam. WA
For the Wide-Flange I-beam with distributed load as in figure below calculate: 1) the shear force V(x) and the bending moment M(x) and plot the shear and bending moment diagrams 2) the maximum bending moment MMAX For the section of the beam with Mwax calculate for each of the points A and B shown in the figure: (a) the flexural stress og (b) the principal stresses 01, 02, 03 c) the principal stress angle Upi (d) the absolute maximum shear...