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Problem 4: Shown below is a crank with 5 kN load. Calculate the vertical deflection at...
Problem 4: Shown below is a crank with 5 kN load. Calculate the vertical deflection at...
Problem 4: Shown below is a crank with 5 kN load. Calculate the vertical deflection at the point of the load. The material properties are E = 2003 MPa, G= 80e3 MPa. Show which segment is going through bending and which bending + torsion. (Hint: Total external strain energy = 72 PS) Z 5 kN Y Uim M² dx 400 mm С X ZEI 500 mm UiT aco ST dx 10 mm x 40 mm Section B. 40 mm dia.
Shown below is a crank with 5 kN load. Calculate the vertical deflection at the point...
Shown below is a crank with 5 kN load. Calculate the vertical deflection at the point of the load. The material properties are E = 2003 MPa, G= 80e3 MPa. Show which segment is going through bending and which bending + torsion. (Hint: Total external strain energy = 72 PS) 5 kN Uim= att S m² dx 400 mm с 500 mm UiT J ST² dx 10 mm x 40 mm Section B 40 mm dia.
The attachment shown carries a static bending load of 12 kN. The length of attachment,...
The attachment shown carries a static bending load of 12 kN. The
length of attachment, l1 = 225 mm. The other
dimensions are as shown on figure Q-2 below. Allowable shear stress
on weldment is tall = 120 MPa. Both column and
attachment are made of AISI 1030 HR steel. A minimum factor of
safety for the joint n = 1.5 is required. Among several possible
weld patterns, we are asked to decide on one of the two patterns...
The beam is shown in the figure below. Use the slope-deflection method. The support Ais pinned,...
The beam is shown in the figure below. Use the slope-deflection method. The support Ais pinned, support B is a roller, and support C is fixed. Assume El = 21537 kNm2. The support at B settles by 73 mm (downwards). The segment AB is subjected to a uniformly distributed load w= 11 kN/m. The segment BC is subjected to a point load P = 91 KN. Enter the digit one in the answer box. The link will be provided on...
Design the cantilever beam below to take the maximum load. Calculate the load in KN to...
Design the cantilever beam below to take the maximum load. Calculate the load in KN to 2 decimal places, if the allowable bending stress is allow = 162 MPa and the allowable shear stress is Tallow = 95 MPa. Also I = 11.918 x 10-6 m4 and the y_bar = 0.04875 m from the top of the t-beam. 150 mm 15 mm T150 mm Hi 15 mm P P 2 m 2 m
As shown in Figure 8, the structural member (beam) is 7m long, carries a 2 kN point load, a 1.2 kN/m uniformly distribu...
As shown in Figure 8, the structural member (beam) is 7m long, carries a 2 kN point load, a 1.2 kN/m uniformly distributed load and is supported at points A and B. The beam is constructed from two pieces of steel plate (2 at 80mm x 8mm) that are welded together with 3mm welds. Section properties for the beam are also listed. Given the support reactions as RAv 5.8 kN and RBv 2.2 kN, as well as the shear force...
A 3 m rigid bar AB is supported with a vertical translational spring at A and a pin at B The bar is subjected to a linearly varying distributed load with maximum intensity g Calculate the ver...
A 3 m rigid bar AB is supported with a vertical translational spring at A and a pin at B The bar is subjected to a linearly varying distributed load with maximum intensity g Calculate the vertical deformation of the spring if the spring constant is 700 kN/m. (ans: 21.43 mm) 2. A steel cable with a nominal diameter of 25 mm is used in a construction yard to lift a bridge section weighing 38 kN. The cable has an...
Problem 3: One way solid slab (10 pts) The slab shown in Figure 2 is 200...
Problem 3: One way solid slab (10 pts) The slab shown in Figure 2 is 200 mm thick. All beams/girders have 400 x 600 mm sections. All columns have 400 x 400 mm sections. Superimposed dead load = 3 kN/m, live load = 4 kN/mº. No walls used. a) Check the slab thickness for deflection control. b) Determine the ultimate uniform load on a l-m wide typical slab strip. c) Determine the ultimate uniform load transferred to beam 2. d)...
post only Group#7 Problem 5 (6 marks) For the beam and loading shown, a) Draw the...
post
only Group#7
Problem 5 (6 marks) For the beam and loading shown, a) Draw the shear and bending-moment diagrams. b) Determine the maximum absolute value of the shear and bending moment. c) Determine the minimum required depth h of the beam. Knowing that the material used has an ultimate normal and shear stresses, use the given factor of safety in each loading case in the following table. P A LLL Dimensions, material properties and load values are presented in...
The simply supported beam carries a uniform load. of 30 kN/m is shown in Figure 3. Due to a certain requi...
The simply supported beam carries a uniform load. of 30 kN/m is shown in Figure 3. Due to a certain requirement, maximum deflection should not be more than 1/360 of the span length. If the allowable bending stress, Ơalkw-168 MPa and allowable shear stress. llo 110 MPa, choose the lightest wide flange beam from Appendix. Given data E-225 GPa, p 7850 kg/m3. Assume A is a pin and B a roller support Rasuk yang dsokong mudah Disebabkan sebuah keperluan tertentu,...
Problem 4: Shown below is a crank with 5 kN load. Calculate the vertical deflection at the point of the load. The material properties are E = 2003 MPa, G= 80e3 MPa. Show which segment is going through bending and which bending + torsion. (Hint: Total external strain energy = 72 PS) Z 5 kN Y Uim M² dx 400 mm С X ZEI 500 mm UiT aco ST dx 10 mm x 40 mm Section B. 40 mm dia.
Shown below is a crank with 5 kN load. Calculate the vertical deflection at the point of the load. The material properties are E = 2003 MPa, G= 80e3 MPa. Show which segment is going through bending and which bending + torsion. (Hint: Total external strain energy = 72 PS) 5 kN Uim= att S m² dx 400 mm с 500 mm UiT J ST² dx 10 mm x 40 mm Section B 40 mm dia.
The attachment shown carries a static bending load of 12 kN. The
length of attachment, l1 = 225 mm. The other
dimensions are as shown on figure Q-2 below. Allowable shear stress
on weldment is tall = 120 MPa. Both column and
attachment are made of AISI 1030 HR steel. A minimum factor of
safety for the joint n = 1.5 is required. Among several possible
weld patterns, we are asked to decide on one of the two patterns...
The beam is shown in the figure below. Use the slope-deflection method. The support Ais pinned, support B is a roller, and support C is fixed. Assume El = 21537 kNm2. The support at B settles by 73 mm (downwards). The segment AB is subjected to a uniformly distributed load w= 11 kN/m. The segment BC is subjected to a point load P = 91 KN. Enter the digit one in the answer box. The link will be provided on...
Design the cantilever beam below to take the maximum load. Calculate the load in KN to 2 decimal places, if the allowable bending stress is allow = 162 MPa and the allowable shear stress is Tallow = 95 MPa. Also I = 11.918 x 10-6 m4 and the y_bar = 0.04875 m from the top of the t-beam. 150 mm 15 mm T150 mm Hi 15 mm P P 2 m 2 m
As shown in Figure 8, the structural member (beam) is 7m long, carries a 2 kN point load, a 1.2 kN/m uniformly distributed load and is supported at points A and B. The beam is constructed from two pieces of steel plate (2 at 80mm x 8mm) that are welded together with 3mm welds. Section properties for the beam are also listed. Given the support reactions as RAv 5.8 kN and RBv 2.2 kN, as well as the shear force...
A 3 m rigid bar AB is supported with a vertical translational spring at A and a pin at B The bar is subjected to a linearly varying distributed load with maximum intensity g Calculate the vertical deformation of the spring if the spring constant is 700 kN/m. (ans: 21.43 mm) 2. A steel cable with a nominal diameter of 25 mm is used in a construction yard to lift a bridge section weighing 38 kN. The cable has an...
Problem 3: One way solid slab (10 pts) The slab shown in Figure 2 is 200 mm thick. All beams/girders have 400 x 600 mm sections. All columns have 400 x 400 mm sections. Superimposed dead load = 3 kN/m, live load = 4 kN/mº. No walls used. a) Check the slab thickness for deflection control. b) Determine the ultimate uniform load on a l-m wide typical slab strip. c) Determine the ultimate uniform load transferred to beam 2. d)...
post
only Group#7
Problem 5 (6 marks) For the beam and loading shown, a) Draw the shear and bending-moment diagrams. b) Determine the maximum absolute value of the shear and bending moment. c) Determine the minimum required depth h of the beam. Knowing that the material used has an ultimate normal and shear stresses, use the given factor of safety in each loading case in the following table. P A LLL Dimensions, material properties and load values are presented in...
The simply supported beam carries a uniform load. of 30 kN/m is shown in Figure 3. Due to a certain requirement, maximum deflection should not be more than 1/360 of the span length. If the allowable bending stress, Ơalkw-168 MPa and allowable shear stress. llo 110 MPa, choose the lightest wide flange beam from Appendix. Given data E-225 GPa, p 7850 kg/m3. Assume A is a pin and B a roller support Rasuk yang dsokong mudah Disebabkan sebuah keperluan tertentu,...
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