Learning Goal: To calculate the normal and shear stresses at a point on the cross section of a column. A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness ty =9 mm , and flange thickness t, = 14 mm (Figure 1). Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and bending moment M = 3 kN - m as shown (Figure 2). The state of stress at a point is a description of the normal and shear stresses at that point. The normal stresses are generally due to both internal normal force and intenal bending moment. The net result can be obtained using the principle of superposition as long as the deflections remain small and the response is elastic. Part A - Normal stress Calculate the normal stress at the point due to the internal normal force on the section. Express your answer with appropriate units three significant figures. > View Available Hint(s) Onormal = 0.222 MPa Previous Answers v Correct Part B - Shear stress Calculate the magnitude of the shear stress at the point due to the internal shear on the section. Express your answer with appropriate units three significant figures. > View Available Hint(s) Figure O 2 of 2 > ? 7= 2.36 MPa Submit Previous Answers X Incorrect; Try Again; 4 attempts remaining
Learning Goal: To calculate the normal and shear stresses at a point on the cross section of a column. A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness ty =9 mm , and flange thickness t, = 14 mm (Figure 1). Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and bending moment M = 3 kN - m as shown (Figure 2). The state of stress at a point is a description of the normal and shear stresses at that point. The normal stresses are generally due to both internal normal force and intenal bending moment. The net result can be obtained using the principle of superposition as long as the deflections remain small and the response is elastic. Part A - Normal stress Calculate the normal stress at the point due to the internal normal force on the section. Express your answer with appropriate units three significant figures. > View Available Hint(s) Onormal = 0.222 MPa Previous Answers v Correct Part B - Shear stress Calculate the magnitude of the shear stress at the point due to the internal shear on the section. Express your answer with appropriate units three significant figures. > View Available Hint(s) Figure O 2 of 2 > ? 7= 2.36 MPa Submit Previous Answers X Incorrect; Try Again; 4 attempts remaining
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Question
What is the T ?
![Learning Goal:
To calculate the normal and shear stresses at a point on the cross
section of a column.
A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness t, = 9 mm , and flange thickness t = 14 mm (Figure 1).
Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and
bending moment M = 3 kN - m as shown (Figure 2).
The state of stress at a point is a description of the normal and shear
stresses at that point. The normal stresses are generally due to both
internal normal force and internal bending moment. The net result can
be obtained using the principle of superposition as long as the
deflections remain small and the response is elastic.
Part A - Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
• View Available Hintís)
Onormal = 0.222 MPa
Submit
Previous Answers
v Correct
Part B - Shear stress
Calculate the magnitude of the shear stress at the point due to the internal shear on the section.
Express your answer with appropriate units to three significant figures.
• View Available Hint(s)
Figure
< 2 of 2 >
HA
?
T= 2.36
MPа
Submit
Previous Answers
N
X Incorrect; Try Again; 4 attempts remaining
M](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa7be627d-a430-4dbe-8b99-b087a651acc0%2F64aaeb0d-7866-43f6-8b3c-fcb45b57ec15%2Fslw7kch_processed.png&w=3840&q=75)
Transcribed Image Text:Learning Goal:
To calculate the normal and shear stresses at a point on the cross
section of a column.
A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness t, = 9 mm , and flange thickness t = 14 mm (Figure 1).
Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and
bending moment M = 3 kN - m as shown (Figure 2).
The state of stress at a point is a description of the normal and shear
stresses at that point. The normal stresses are generally due to both
internal normal force and internal bending moment. The net result can
be obtained using the principle of superposition as long as the
deflections remain small and the response is elastic.
Part A - Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
• View Available Hintís)
Onormal = 0.222 MPa
Submit
Previous Answers
v Correct
Part B - Shear stress
Calculate the magnitude of the shear stress at the point due to the internal shear on the section.
Express your answer with appropriate units to three significant figures.
• View Available Hint(s)
Figure
< 2 of 2 >
HA
?
T= 2.36
MPа
Submit
Previous Answers
N
X Incorrect; Try Again; 4 attempts remaining
M
![Learning Goal:
To calculate the normal and shear stresses at a point on the cross
section of a column.
A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness t = 9 mm , and flange thickness t = 14 mm (Figure 1).
Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and
bending moment M = 3 kN - m as shown (Figure 2).
The state of stress at a point is a description of the normal and shear
stresses at that point. The normal stresses are generally due to both
internal normal force and internal bending moment. The net result can
be obtained using the principle of superposition as long as the
deflections remain small and the response is elastic.
Part A- Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
> View Available Hintís)
Onormal = 0.222 MPa
Submit
Previous Answers
Correct
Part B - Shear stress
Calculate the magnitude of the shear stress at the point due to the internal shear on the section.
Express your answer with appropriate units to three significant figures.
> View Available Hintís)
Figure
< 1 of 2 >
HA
T= 2.36
MPа
Submit
Previous Answers
X Incorrect; Try Again; 4 attempts remaining](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa7be627d-a430-4dbe-8b99-b087a651acc0%2F64aaeb0d-7866-43f6-8b3c-fcb45b57ec15%2F1tvxowd_processed.png&w=3840&q=75)
Transcribed Image Text:Learning Goal:
To calculate the normal and shear stresses at a point on the cross
section of a column.
A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness t = 9 mm , and flange thickness t = 14 mm (Figure 1).
Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and
bending moment M = 3 kN - m as shown (Figure 2).
The state of stress at a point is a description of the normal and shear
stresses at that point. The normal stresses are generally due to both
internal normal force and internal bending moment. The net result can
be obtained using the principle of superposition as long as the
deflections remain small and the response is elastic.
Part A- Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
> View Available Hintís)
Onormal = 0.222 MPa
Submit
Previous Answers
Correct
Part B - Shear stress
Calculate the magnitude of the shear stress at the point due to the internal shear on the section.
Express your answer with appropriate units to three significant figures.
> View Available Hintís)
Figure
< 1 of 2 >
HA
T= 2.36
MPа
Submit
Previous Answers
X Incorrect; Try Again; 4 attempts remaining
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