![QUESTION 34 The simply supported beam shown in the figure below is subjected to a 3 kN concentrated force. The beam has modulus of elasticity of E-70 GPa and area moment of inertia equals to l-126x10-6 m4 Question 34- Question 38] 3 kN 5](http://img.homeworklib.com/questions/677ae580-b4c2-11ea-b3a0-eb2489ad79c3.png?x-oss-process=image/resize,w_560)
![QUESTION 36 C2 - 0 2 3 QUESTION 37 C1- 1.33 1.5 2.3 QUESTION 38 Deflection at x-2m [mm] 0.00123 -0.00595 -0.0147 0 -0.1512](http://img.homeworklib.com/questions/68d8a050-b4c2-11ea-9459-bb0f8d53c4ab.png?x-oss-process=image/resize,w_560)
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QUESTION 34 The simply supported beam shown in the figure below is subjected to a 3...
QUESTION 33 The simply supported beam shown in the figure (18) below is subjected to a...
QUESTION 33 The simply supported beam shown in the figure (18) below is subjected to a 3 kN/m uniformally distributed load. The beam has modulus of elasticity of E-200 GPa) and area moment of inertia equals to (/ 12.5 x 10 mm).Answer [Question 33-Question 361 3 kN/m 4 m Figure (18) The support reaction at point A in the y-direction (RAJ: (CLO6) (1 Point) 6.3 kN 48 kN 2 kN 6 kN
QUESTION 33 A simply supported steel beam with two eccentric loads as shown in the figure...
QUESTION 33 A simply supported steel beam with two eccentric loads as shown in the figure (17) below. The second moment of area of the beam section about the neutral axis is ( 1-0.201 x 10 mm). And the modulus of elasticity (E 207 GPa) Al dimensions in mm), Answer (Question 33-Question 361 3.5 kN 2.1 kN E 207 x 10" Pa 300. Figure (17) The support reaction at point A in the y direction (RAy):(CLO6) (a Point) 2.71 KN...
QUESTION 1 [15] For the simply supported beam subjected to the loading shown in the figure,...
QUESTION 1 [15] For the simply supported beam subjected to the loading shown in the figure, a) Derive equations for the shear force V and the bending moment M for any location in the beam. (Place the origin at point A.) b) Report the maximum positive bending moment, the maximum negative bending moment, and their respective locations. 36 KN 180 KN-m X B C D 4 m 5 m 3 m Figure 1
Question 3 For the simply supported steel beam with cross section and loading shown (see Figure...
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...
The simply supported bearm is made of A-36 steel and is subjected to the loading shown...
The simply supported bearm is made of A-36 steel and is subjected to the loading shown in (Figure 1. Suppose that P 18 kN. E 200 GPa and I - 0.1457(10 Part A Determine the deflection of the beam at its center C Express your answer to three signiticant tigures and include the appropriate units. Enter positive value If the deflection is upward and negative value If the deflection is downward. Ac= Value Units Figure 1 of 1 Submit Request...
P10.047 (Multistep) The simply supported beam shown in the figure consists of a W410 x 60...
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...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform t...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to determine the deflection and stress of bottom surface. (2.) Using elementary beam theory to determine the deflection and stress of bottom surface
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to...
(a) A cantilever beam shown in Figure 6 is subjected to a concentrated load P. Deflection...
(a) A cantilever beam shown in Figure 6 is subjected to a concentrated load P. Deflection of the beam at each point can be defined by the following equations: 6EI Pa 6EI F3x-a) for axx<l The following MATLAB code calculates and plots the deflection diagram for a beam with 1-4 m, d1 = 3 m, b = 1 m,E>210 x 10, Pa, 1 = 285 x 10-6 m4 and P = 20 kN. Find at least FOUR errors in the...
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature...
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 d2v x3 ΕΙ = dx? 12 -x2+1
A simply supported beam AB is subjected to a triangle loading (see figure). The moment curvature...
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*
QUESTION 33 The simply supported beam shown in the figure (18) below is subjected to a 3 kN/m uniformally distributed load. The beam has modulus of elasticity of E-200 GPa) and area moment of inertia equals to (/ 12.5 x 10 mm).Answer [Question 33-Question 361 3 kN/m 4 m Figure (18) The support reaction at point A in the y-direction (RAJ: (CLO6) (1 Point) 6.3 kN 48 kN 2 kN 6 kN
QUESTION 33 A simply supported steel beam with two eccentric loads as shown in the figure (17) below. The second moment of area of the beam section about the neutral axis is ( 1-0.201 x 10 mm). And the modulus of elasticity (E 207 GPa) Al dimensions in mm), Answer (Question 33-Question 361 3.5 kN 2.1 kN E 207 x 10" Pa 300. Figure (17) The support reaction at point A in the y direction (RAy):(CLO6) (a Point) 2.71 KN...
QUESTION 1 [15] For the simply supported beam subjected to the loading shown in the figure, a) Derive equations for the shear force V and the bending moment M for any location in the beam. (Place the origin at point A.) b) Report the maximum positive bending moment, the maximum negative bending moment, and their respective locations. 36 KN 180 KN-m X B C D 4 m 5 m 3 m Figure 1
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...
The simply supported bearm is made of A-36 steel and is subjected to the loading shown in (Figure 1. Suppose that P 18 kN. E 200 GPa and I - 0.1457(10 Part A Determine the deflection of the beam at its center C Express your answer to three signiticant tigures and include the appropriate units. Enter positive value If the deflection is upward and negative value If the deflection is downward. Ac= Value Units Figure 1 of 1 Submit Request...
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...
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to determine the deflection and stress of bottom surface. (2.) Using elementary beam theory to determine the deflection and stress of bottom surface
(1)20points 0.12m 0.05m The simply supported beam shown in the figure is subjected to a uniform transverse load and a concentrated load. (1.) Using two equal-length elements (FEM) to...
(a) A cantilever beam shown in Figure 6 is subjected to a concentrated load P. Deflection of the beam at each point can be defined by the following equations: 6EI Pa 6EI F3x-a) for axx<l The following MATLAB code calculates and plots the deflection diagram for a beam with 1-4 m, d1 = 3 m, b = 1 m,E>210 x 10, Pa, 1 = 285 x 10-6 m4 and P = 20 kN. Find at least FOUR errors in the...
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 d2v x3 ΕΙ = dx? 12 -x2+1
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*
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