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Figure 3b() shows a step beam with different moment of inertia in member 1 and 2. Assemble the structure stiffnes...
A two-member beam structure is given in the figure. The load, P, is set to be 1000 N. Find the displacements at node 1 in terms of the global coordinate system. The sectional areas of Member 1 and Member 2 are 100 mm- and 144 mm², respectively and their moment of inertias are 833 mm+ and 1728 mm4. The Young's modulus is given as E=200 GPa Additional Question: for those MAE 540 Students: Find the displacements and the bending stress...
Consider the cantilever beam shown in (Figure 1). Suppose that I AB = 800(106) mm4, IBC = 150(106) mm4. Take E = 200 GPa. Figure < 1 of 1 > 12 kN/m 8 kN/m 1AB 2 m B BC lm Part B Determine the displacement at point C measured downward. Use Castigliano's theorem. Express your answer to three significant figures and include the appropriate units. Enter positive value if the displacement is downward and negative value if the displacement is...
Problem 3: For the beam shown find the slope and deflection at point B and C 100 KN 300 kN-m 6 m E = constant = 70 GPa 1 = 500 (106) mm Problem 4: For the beam shown find the deflection at point B and the slope at point A 80 KN 12 m 12 m E = constant = 200 GPa I = 600 (106) mm
Consider the beam shown in (Figure 1). Solve this problem using the moment-area theorems. Take E = 200 GPa, I = 310(106) mm4. Determine the slope at B measured counterclockwise from the positive x axis.Determine the maximum displacement of the beam measured upward.
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...
a w310 x 129 I-beam, made of a36 steel, is shown in the figure. this I-beam is 4 m long and has a distributed load and a concentrated load as shown in the figure. determine the slope at point b and deflection at point c. the modulus of elasticity of A-36 steel is E = 200GPA. the answers should contain no variables 15 kN/m 20 kN 2 m im Wide-Flange Sections or W Shapes SI Units Flange Web x-x axis...
Figure 1 shows A fully symmetrical I beam of area A1 = 5472 mm?, and second moment of areal = 59.9 x 10 mm' that is strengthened by attaching a plate of 10 mm thickness and 100 mm breadth at the top as shown in Figure 2. Pairs of 12 mm diameter steel bolts are used at regular 200 mm spacing along the beam to connect the plate to the I beam in an arrangement as shown in Figure 3....
Figure Q3 shows a simply supported beam carrying a point load. The beam hasa rectangular hollow steel section as shown in Figure Q3. a. Calculate the second moment of area of the section about the horizontal (10 marks) centroidal axis. Calculate the maximum allowable value of the point load Wif the elastic bending (15 marks) b. stress in the beam is to be limited to 250 MPa. c. Calculate the maximum shear stress at q-q in the beam when the...
16-5. Determine the structure stiffness matrix K for the 200 GPa, are fixed. Take E and frame. Assume 1-300 105) mm,A 10(10) mm2 for each member. 16-6. Determine the support reactions at the fixed supports D and . Take E-200 GPa,1 300 (10) mm, A 10(10) mm2 for each member. 12 kN/m 2 m 4 m 12 2 m Probs. 16-5/6 16-5. Determine the structure stiffness matrix K for the 200 GPa, are fixed. Take E and frame. Assume 1-300...
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...