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A 2-Dimensional column is subjected to two forces as shown. Sketch the normal stress distribution acting...
A 2-D L-beam is subjected to an axial and a shear forces as shown. The L-beam...
A 2-D L-beam is subjected to an axial and a shear forces as shown. The L-beam is fixed at base AB. The member has a rectangular cross section of b = 12 in wide and 2 in deep a. Determine all the stresses acting at base AB. b. Sketch diagrams of the combined stress distribution acting over base AB. lok G 12 in • ok 12 in (2 เห 36 in lin zin Crors-sécnion TAT BATE AB)
A column is subjected to eccentric forces of P and 2P as shown in figure 5a. Calculate the maximum normal stress developed on the cross section of the column if P 60kN. (a) [10 marks] 2P 15 mm 1...
A column is subjected to eccentric forces of P and 2P as shown in figure 5a. Calculate the maximum normal stress developed on the cross section of the column if P 60kN. (a) [10 marks] 2P 15 mm 15 mm 150 m 150 mm 15 mmi 100 m 100 mm 75 mm 100 mm
A column is subjected to eccentric forces of P and 2P as shown in figure 5a. Calculate the maximum normal stress developed on the cross section...
A circular column segment, shown in Figure 2, is subjected to a concentric 1,000 kN compression...
A circular column segment, shown in Figure 2, is subjected to a concentric 1,000 kN compression force, and 100 kNm torsional forces. For this column segment: a Calculate the normal stress at point A, due to the axial load b) Calculate the shear stress at point A, due to the applied torque c Determine the major and minor principal stresses, the maximum shear stress, and the angle to the principal axes at point A. d) Draw a diagram illustrating the...
The beam is made from three boards nailed together as shown. If the moment acting on the cross section is M = 1 kip·ft, determine the maximum bending stress in the beam.
6-58 The beam is made from three boards nailed together as shown. If the moment acting on the cross section is M = 1 kip·ft, determine the maximum bending stress in the beam. Sketch a three-dimensional view of the stress distribution acting over the cross section. 6-59 If M = 1 kip·ft, determine the resultant force the bending stresses produce on the top board A of the beam.
Problem 5.1. Axial stress in a reinforced box beamm Figure 5. 12 depicts an aluminum rectangular...
Problem 5.1. Axial stress in a reinforced box beamm Figure 5. 12 depicts an aluminum rectangular box beam of height ћ-0.30 m, width b-0.15 m, flange thickness ta-12 mm, and web thickness tw-5 mm. The beam is reinforced by two layers of unidirectional composite material of thickness te - 4 mm. The section is subjected to an axial load i - 600 kN. The Young's moduli for the aluminum and unidirec- tional composite are Ea - 73 GPa and Ec140...
For the joint and loading shown, determine the stress states at points A and B on...
For the joint and loading shown, determine the stress states at
points A and B on section-aa, and the principle stresses at point
A. The free-body diagram including section-aa is given below for
your convenience. Section-aa has a rectangular cross-section area
of thickness 12 mm (shown) and width 18 mm. a) Sketch each stress
state using a square stress element. b) Determine the principle
stresses at point A (no need to sketch the stress
element).
Problem 1: (25%) For the...
Problem 5. (20 pts) The joint is subjected to forces of F and P. The member...
Problem 5. (20 pts) The joint is subjected to forces of F and P. The member has a rectangular cross-sectional area of width w 50 mm and thickness t 20 mm. [a 42 cm, b-5 cm, P- 275 N, F 190 N] a) Determine the stress at A. Include sign. b) Determine the magnitude of shear stress at A c) Determine the stress at B. Include sign. d) Determine the magnitude of shear stress at B.
The beam having a cross-section as shown is subjected to the distributed load w (1) Calculate...
The beam having a cross-section as shown is subjected to the distributed load w (1) Calculate the moment of inertia, I (2) If the allowable maximum normal stress ơmax-20 MPa, determine the largest distributed load 5. w. (3) If w 1.5 kN/m, determine the maximum bending stress in the beam. Sketch the stress distribution acting over the cross-section. 100 mm 50mm 120 mm 3 m50 mm 3 m
0 Q c) 28125000 1 Question 4 2 the shown column subjected to the shown forces...
0 Q c) 28125000 1 Question 4 2 the shown column subjected to the shown forces Answer the following questions 100 O F c) 42187500 150 c) 204.44444 F, [kN] F; [kN] [kN] 300 500 400 c) 44.444444 5) moment of inertia about x-axis Ix (mm) a) 83333333 b) 42187500 6) moment of inertia about y-axis ly a) 83333333 b) 28125000 7) Normal stress at point A[Mpa) a) 186.66667 b) 44.4444444 8) Normal stress at point B [Mpa) a) 62...
The beam has the rectangular cross section shown. If w 1 kN/m
The beam has the rectangular cross section shown. If w 1 kN/m, determine the maximum bending stress in the beam. Sketch the stress distribution acting over the cross section.
A 2-D L-beam is subjected to an axial and a shear forces as shown. The L-beam is fixed at base AB. The member has a rectangular cross section of b = 12 in wide and 2 in deep a. Determine all the stresses acting at base AB. b. Sketch diagrams of the combined stress distribution acting over base AB. lok G 12 in • ok 12 in (2 เห 36 in lin zin Crors-sécnion TAT BATE AB)
A column is subjected to eccentric forces of P and 2P as shown in figure 5a. Calculate the maximum normal stress developed on the cross section of the column if P 60kN. (a) [10 marks] 2P 15 mm 15 mm 150 m 150 mm 15 mmi 100 m 100 mm 75 mm 100 mm
A column is subjected to eccentric forces of P and 2P as shown in figure 5a. Calculate the maximum normal stress developed on the cross section...
A circular column segment, shown in Figure 2, is subjected to a concentric 1,000 kN compression force, and 100 kNm torsional forces. For this column segment: a Calculate the normal stress at point A, due to the axial load b) Calculate the shear stress at point A, due to the applied torque c Determine the major and minor principal stresses, the maximum shear stress, and the angle to the principal axes at point A. d) Draw a diagram illustrating the...
Problem 5.1. Axial stress in a reinforced box beamm Figure 5. 12 depicts an aluminum rectangular box beam of height ћ-0.30 m, width b-0.15 m, flange thickness ta-12 mm, and web thickness tw-5 mm. The beam is reinforced by two layers of unidirectional composite material of thickness te - 4 mm. The section is subjected to an axial load i - 600 kN. The Young's moduli for the aluminum and unidirec- tional composite are Ea - 73 GPa and Ec140...
For the joint and loading shown, determine the stress states at
points A and B on section-aa, and the principle stresses at point
A. The free-body diagram including section-aa is given below for
your convenience. Section-aa has a rectangular cross-section area
of thickness 12 mm (shown) and width 18 mm. a) Sketch each stress
state using a square stress element. b) Determine the principle
stresses at point A (no need to sketch the stress
element).
Problem 1: (25%) For the...
Problem 5. (20 pts) The joint is subjected to forces of F and P. The member has a rectangular cross-sectional area of width w 50 mm and thickness t 20 mm. [a 42 cm, b-5 cm, P- 275 N, F 190 N] a) Determine the stress at A. Include sign. b) Determine the magnitude of shear stress at A c) Determine the stress at B. Include sign. d) Determine the magnitude of shear stress at B.
The beam having a cross-section as shown is subjected to the distributed load w (1) Calculate the moment of inertia, I (2) If the allowable maximum normal stress ơmax-20 MPa, determine the largest distributed load 5. w. (3) If w 1.5 kN/m, determine the maximum bending stress in the beam. Sketch the stress distribution acting over the cross-section. 100 mm 50mm 120 mm 3 m50 mm 3 m
0 Q c) 28125000 1 Question 4 2 the shown column subjected to the shown forces Answer the following questions 100 O F c) 42187500 150 c) 204.44444 F, [kN] F; [kN] [kN] 300 500 400 c) 44.444444 5) moment of inertia about x-axis Ix (mm) a) 83333333 b) 42187500 6) moment of inertia about y-axis ly a) 83333333 b) 28125000 7) Normal stress at point A[Mpa) a) 186.66667 b) 44.4444444 8) Normal stress at point B [Mpa) a) 62...
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**86 at 40 not 88. please show how got Tr in calculations thank
you
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