For the beam shown in Figure A2:
(a) Determine the static indeterminacy of the beam.
(b) Using the flexibility method, and taking the support reaction at B as the redundant, express the compatibility condition for the displacement at B.
(c) Using the results of (b), determine the support reaction at B
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For the beam shown in Figure A2:
(a) Determine the static indeterminacy of the beam.
(b)...
For the beam and loading shown in Figure A2: - a. Determine the support reactions b....
For the beam and loading shown in Figure A2: - a. Determine the support reactions b. Draw the shear and bending moment diagrams c. Determine the maximum absolute value of shear force and bending moment P= 100 N P= 140 N w = 30 N/m A B 4 m 7 m 10 m 3 Figure A2.
Q8 (a). For the beam as shown in Figure 8a, determine the reaction forces at A...
Q8 (a). For the beam as shown in Figure 8a, determine the reaction forces at A and B. 5 kN/m 6 m Figure 8a (b). Find all the zero force members in Figure 8b. (c). Find the degree of indeterminacy of the structures in Figure 8c. Figure 8c
Beam ABC as shown in figure 2 is supported as fixed at A, a cable tie...
Beam ABC as shown in figure 2 is supported as fixed at A, a cable tie at B and a spring at C carries a uniformly distributed load of 72 kN/m on member AB and a concentrated load of 54 kN on member BC. Using the flexibility method and neglect the axial effects in the bcam, (a) perform the global flexibility matrix of the beam structure, (b) calculate the rotation at B and displacement at C, (c) draw the deflection,...
Consider the beam shown in (Figure 1). Assume the support at A is a pin and...
Consider the beam shown in (Figure 1). Assume the support at A is a pin and C is a roller. Take E 200 GPa, I 150(106) mm Suppose that w 19 kN/m Figure 1 of 1 TA 2 m 4 m Part B Determine the slope at point B measured clockwise from the positive r axis. Use the method of virtual work Express your answer using three significant figures. rad Part Determine the displacement at point B measured downward. Use...
The continuous beam ABCD shown in Figure Q2(a) has a flexural rigidity EI = 1000 kNm2....
The continuous beam ABCD shown in Figure Q2(a) has a flexural
rigidity EI = 1000 kNm2. The beam is subjected to a concentrated
load at point B and a uniform load from points C to D.
(b) The beam ABCD shown in Figure Q2(b) is identical to that in Figure Q2(a), except that the roller support at point is replaced by a linear spring of stiffness K = 500 kN/m and point D settles (downwards) by 6 cm, calculate the...
KHW 9: force method Force Method of Analysis: Frames 2 of 5> statically indeterminate. Choosing S...
KHW 9: force method Force Method of Analysis: Frames 2 of 5> statically indeterminate. Choosing S and Cy as the redundant forces leads to the superposition shown. The flexibility coefficient Bo relates the deflection at point B to the redundant force at C The compatibility equations are written by requiring the displacements at the redundant locations to be consistent between the real beam and the model formed by the superposition of the statically determinate beams. Part A -Deflection of th...
2.[1251 Determine the support reaction at the roller B using the Force Method. The support at A i...
please I need someone to do it clearly.
2.[1251 Determine the support reaction at the roller B using the Force Method. The support at A is a roller and C is a pin. 500 lb 120 lb/ft 12ft 5 ft 5 ft- a. 130) Write the compatibility condition. Include sketches of the primary structure and redundant condition with the flexibility coefficient. Chose B, as the redundant force b. 160] Solve for ABy using virtual work 130] Draw the shear and...
SAN4701 OCT/NOV 2017 QUESTION 1 The beam shown in Figure 1 is fixed at support A and support C, support B is a roller s...
SAN4701 OCT/NOV 2017 QUESTION 1 The beam shown in Figure 1 is fixed at support A and support C, support B is a roller support. Use the stiffness matrix method to determine the. Member stiffness matrix 11 1.2 Structure and load matrix (10) 13 Displacement matrix Reactions at the support 14 15. Moments at the fixed supports El is constant along the length of the beam 18 kN 10 kN 20 m 10 m 1 15 m15 m Figure 1...
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...
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...
Q5. The cantilever beam, AC, is subjected to the load case shown in Figure 5. For the loading shown, do the following: [10 Marks] a) Calculate the magnitude and direction of the reactions at A b) Usi...
Q5. The cantilever beam, AC, is subjected to the load case shown in Figure 5. For the loading shown, do the following: [10 Marks] a) Calculate the magnitude and direction of the reactions at A b) Using the Macaulay function, determine the displacement in y of the point B of the beam (x 2.4 m from the support at A) [10 Marks] c) Determine the slope at B. [5 Marks] The beam has a Young's modulus of E-200 GPa and...
For the beam and loading shown in Figure A2: - a. Determine the support reactions b. Draw the shear and bending moment diagrams c. Determine the maximum absolute value of shear force and bending moment P= 100 N P= 140 N w = 30 N/m A B 4 m 7 m 10 m 3 Figure A2.
Q8 (a). For the beam as shown in Figure 8a, determine the reaction forces at A and B. 5 kN/m 6 m Figure 8a (b). Find all the zero force members in Figure 8b. (c). Find the degree of indeterminacy of the structures in Figure 8c. Figure 8c
Beam ABC as shown in figure 2 is supported as fixed at A, a cable tie at B and a spring at C carries a uniformly distributed load of 72 kN/m on member AB and a concentrated load of 54 kN on member BC. Using the flexibility method and neglect the axial effects in the bcam, (a) perform the global flexibility matrix of the beam structure, (b) calculate the rotation at B and displacement at C, (c) draw the deflection,...
Consider the beam shown in (Figure 1). Assume the support at A is a pin and C is a roller. Take E 200 GPa, I 150(106) mm Suppose that w 19 kN/m Figure 1 of 1 TA 2 m 4 m Part B Determine the slope at point B measured clockwise from the positive r axis. Use the method of virtual work Express your answer using three significant figures. rad Part Determine the displacement at point B measured downward. Use...
The continuous beam ABCD shown in Figure Q2(a) has a flexural
rigidity EI = 1000 kNm2. The beam is subjected to a concentrated
load at point B and a uniform load from points C to D.
(b) The beam ABCD shown in Figure Q2(b) is identical to that in Figure Q2(a), except that the roller support at point is replaced by a linear spring of stiffness K = 500 kN/m and point D settles (downwards) by 6 cm, calculate the...
KHW 9: force method Force Method of Analysis: Frames 2 of 5> statically indeterminate. Choosing S and Cy as the redundant forces leads to the superposition shown. The flexibility coefficient Bo relates the deflection at point B to the redundant force at C The compatibility equations are written by requiring the displacements at the redundant locations to be consistent between the real beam and the model formed by the superposition of the statically determinate beams. Part A -Deflection of th...
please I need someone to do it clearly.
2.[1251 Determine the support reaction at the roller B using the Force Method. The support at A is a roller and C is a pin. 500 lb 120 lb/ft 12ft 5 ft 5 ft- a. 130) Write the compatibility condition. Include sketches of the primary structure and redundant condition with the flexibility coefficient. Chose B, as the redundant force b. 160] Solve for ABy using virtual work 130] Draw the shear and...
SAN4701 OCT/NOV 2017 QUESTION 1 The beam shown in Figure 1 is fixed at support A and support C, support B is a roller support. Use the stiffness matrix method to determine the. Member stiffness matrix 11 1.2 Structure and load matrix (10) 13 Displacement matrix Reactions at the support 14 15. Moments at the fixed supports El is constant along the length of the beam 18 kN 10 kN 20 m 10 m 1 15 m15 m Figure 1...
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...
Q5. The cantilever beam, AC, is subjected to the load case shown in Figure 5. For the loading shown, do the following: [10 Marks] a) Calculate the magnitude and direction of the reactions at A b) Using the Macaulay function, determine the displacement in y of the point B of the beam (x 2.4 m from the support at A) [10 Marks] c) Determine the slope at B. [5 Marks] The beam has a Young's modulus of E-200 GPa and...
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