2) For the simply supported beam shown in figure 2 8 marks 4 marks Determine the maximum deflecti...
QUESTION 4 (25 marks) A simply supported beam is loaded by an uniform distributed load, wkN/m, over the span of the beam, L, as shown in Figure Q4. (a) Determine the end reactions at point A and B in terms of w and L. (4 marks) (b) At an arbitrary point, x, express the internal mom (c) Show that the deflection curve of the beam under the loading situation is ent, M(x), in x, w, and L. (5 marks) 24EI...
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...
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 A B 4 m 8 d2v EI dx2 x3 12 *+z*
Q2. A simply supported beam AB (Figure 2) supports a uniformly distributed load of q = 18kN/m and a concentrated load of P = 23kN at the centre. Consider length of the beam, L = 3m, Young's modulus, E = 200GPa and moment of inertial, I = 30 x 10 mm-. Assume the deflection of the beam can be expressed by elastic curve equations of the form: y(x) = Ax4 + Bx3 + Cx2 + Dx + E. 1) Sketch...
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
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
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 A B 4.m x3 EI dx2 = - 2 COM MacBook Air 20 COD F4 FS F6 ►II # $ دیا 4 % 5 6 & 7 8 9
a simply supported beam abcd with arectangular cross section
carries the loading shown in figure. the uniform beam has a mass of
33 kg per meter (m kg/m) and a cross section as shown in the
figure. you may take 10 m/s^2 as acceleration.Question A2 A simply supported beam ABCD with a rectangular cross-section carries the loading shown in Figure QA2. The uniform beam has a mass of m kg per meter of length (m kg/m) and a cross-section as shown...
The simply supported beam shown in Figure 1 is pin-supported at A and roller-supported at D. la) Replace the distributed loads in Figure 1 by an equivalent resultant force and locate its location with respect to A. {2 + 3 marks 1b) Calculate the reactions at supports A and D. {2 marks 1c) Calculate the shear force and bending moment at point C. {4 marks) 15 kN/m 6 kN/m D B q 3.0 m 3.0 m 3.0 m Figure 1
Consider the simply supported beam and loaded as shown in the M figure. Perform the following: 1. Determine the support reactions. 2. Plot SFD and BMD 3. if L=9 m, the beam will fail when the maximum shear force is Vmax= 5 kN or the maximum bending moment is Mmax=22 kN.m. Determine the largest couple moment Mo the beam will support.