This is part of the reason i am confused. i believe the negative sign is to...
Question 2 Simply supported beam ABC is subject to a point load and the patch loads as indicated in Figure Q2. Assume the beam has a uniform cross-section size. The Modulus of Elasticity E = 210x106 kN/m2, second moment of area l=5x105 m. Determine the deflection of beam ABC at the middle point using MacCaulay's Method. Total (15) marks. -30 KN -6 kN/m -3 kN/m B 3 m 4 m * Figure Q2: Simply supported beam ABC
getting a few different answers and not sure what is correct. greatly appriciate the help Question 2 Simply supported beam ABC is subject to a point load and the patch loads as indicated in Figure Q2. Assume the beam has a uniform cross-section size. The Modulus of Elasticity E = 210x106 kN/m2, second moment of area l=5x105 m. Determine the deflection of beam ABC at the middle point using MacCaulay's Method. Total (15) marks. -30 KN -3 kN/m -6 kN/m...
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature equation is shown (from the left). The (El-constant) 1. Determine the deflection at middle beam. 2. Determine the rotation at middle beam. 2 kN/m B 4 m 8 EI 12 MacBook Air DOO 008 A tA % A - 5 & 7 6 I 0 * 8 9 R T
The simply supported beam consists of a w530 x 66 structural steel wide-flange shape [E-200 GPa; I -351 x 106 mm]. Determine (a) the beam deflection at point C. (b) the beam deflection at point E. Assume P = 35 kN, w = 80 kN/m, LAB = LBC = LCD = 4 m, LDE = 2 m LAB BC Answers: (a) vc=T-190.693 (b) VE178.156 The simply supported beam consists of a w530 x 66 structural steel wide-flange shape [E-200 GPa;...
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...
2. a. An edge beam with sectional dimensions is shown in Fig.3. i. Determine the location of its centriod from point 0. ii. Determine its moment of inertia in x-x direction about centriod. A y 150mm 40mm 35mm 300mm V --> X Fig. 3 2. b. Determine the mid-span deflection of a 3m long simply supported R.C. beam which is subject to a gravity UDL of 10 kN/m with a cross section as shown in Fig. 3 (E = 35kN/mm²).
Data are given-see 2 pictures attached I am not sure if these answers are correct. I have used Micro stran to solve them. I need manual calculation by using Mc Cauley's Method(double integration) to compare them. Deflection at B = -2.073mm C=-2.045 mm D=-1.876mm F= +2.033mm = 40 kN All dic tances in m-enhart it to meter 4.9a x100 mm sin 1150! 150, 675ーーーヒーー600 --イ 975 2550 Simply-supported beam with cantilever overhang and a single vertical point load = 40...
Q2 The 10 m long simply supported beam is subjected to a uniformly distributed load w = 10 kN/m throughout and a point load P =10 kN at the midspan of the beam, as shown in Figure Q2 (a). The cross section of this beam is depicted in Figure Q2 (b), which consists of three equal rectangular steel members. Self-weight of the beam is neglected. 30 mm P= 10 KN W = 10 kN/m 200 mm 5 m 5 m...
Figure 1 shows a beam is supported by a pin at A and a roller at C. The beam is subjected to point loads 30 kN and 60 kN and a uniformly distributed load of 24 kN/m. Modulus of elasticity, E and moment of inertia, I for all members are 205 kN/mm2 and 195 x 106 mm4, respectively. By using Virtual Work method, (a) determine the slope at B. (1.801 mrad) (b) determine the deflection at B and D. (2.4...
Problem 2 Consider a simply supported symmetric I beam ABCD carrying a uniformly distributed load w and a concentrated load F as shown in Figure 2. Young's modulus of the beam is 200 GPa. F 8 kN 8cm 3cm 3cm 7 m 5 m 3 m 2cm W= 6 kN/m 6cm A D B 2cm 7TITT TITIT Figure 2 1) Replace the support C with the reaction force Rc, and using static equilibrium find the reactions at point A and...