=11 kN single load, M=22 kN.m moment and w=5 kN/m distributed load act on the beam whose loading condition is given in the figure. The length L is also given as L=5 m. The cross-sectional properties of the beam are; body height yg=218 mm, body thickness xg=18 mm, flange width xf=190 mm, flange height yf=13 mm. Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the B level of the beam. According to this; Question1-A) Find the support response (Dy) at point D. (Write your result in kN.) Question2-B) Find the support response (Ay) at point A. (Write your result in kN.) Question3-C) Find the shear force (VB) at point B. (Write your result in kN.)
F=11 kN single load, M=22 kN.m moment and w=5 kN/m distributed load act on the beam whose loading condition is given in the figure. The length L is also given as L=5 m. The cross-sectional properties of the beam are; body height yg=218 mm, body thickness xg=18 mm, flange width xf=190 mm, flange height yf=13 mm. Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the B level of the beam. According to this;
Question1-A) Find the support response (Dy) at point D. (Write your result in kN.)
Question2-B) Find the support response (Ay) at point A. (Write your result in kN.)
Question3-C) Find the shear force (VB) at point B. (Write your result in kN.)
Question4-D) Find the bending moment (MB) at point B. (Write your result in kN.m.)
Question 5-E) Find the y distance of the section center with respect to the axis passing through the base of the section. (Write your result in mm.)
Question 6-F) Find the moment of inertia of the beam section. (Do your operations by converting the lengths to meters. Take at least 4 digits for the decimal part of your result and use the expression E for the decimal part. Write it as 5E-3 instead of 0.005.)
Question 7-G) For a section taken from the B point of the beam; Find the normal stress at point E on the beam section due to the bending moment. (Write your result in MPa.)
Question 8-H) For a section taken from the B point of the beam; Find the shear stress at point E on the beam section due to the shear force. (Write your result in MPa.)
![w kN/m
F kN
M kN.m
A
D
В
2L
L.
L
E
Yg
Xg](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fd90c4375-6160-4b6f-9c67-7a8789072fc7%2F9ae1a70e-5426-4970-a82c-b3e614604adb%2F9a9h6mg_processed.jpeg&w=3840&q=75)
![](/static/compass_v2/shared-icons/check-mark.png)
Step by step
Solved in 5 steps with 5 images
![Blurred answer](/static/compass_v2/solution-images/blurred-answer.jpg)
![Refrigeration and Air Conditioning Technology (Mi…](https://www.bartleby.com/isbn_cover_images/9781305578296/9781305578296_smallCoverImage.gif)
![Automotive Technology: A Systems Approach (MindTa…](https://www.bartleby.com/isbn_cover_images/9781133612315/9781133612315_smallCoverImage.gif)
![Precision Machining Technology (MindTap Course Li…](https://www.bartleby.com/isbn_cover_images/9781285444543/9781285444543_smallCoverImage.gif)
![Refrigeration and Air Conditioning Technology (Mi…](https://www.bartleby.com/isbn_cover_images/9781305578296/9781305578296_smallCoverImage.gif)
![Automotive Technology: A Systems Approach (MindTa…](https://www.bartleby.com/isbn_cover_images/9781133612315/9781133612315_smallCoverImage.gif)
![Precision Machining Technology (MindTap Course Li…](https://www.bartleby.com/isbn_cover_images/9781285444543/9781285444543_smallCoverImage.gif)