Stress and Strain (Finding the thickness of truss members)

AI Thread Summary
The discussion focuses on understanding how to calculate the thickness of truss members using stress and strain concepts. The main formula highlighted is axial stress, expressed as stress = P/A, where P is the axial load and A is the cross-sectional area. The conversation emphasizes that the compression case is critical since it involves the highest load and lowest allowable stress. Participants suggest starting by solving for the required cross-sectional area using the formula and then determining the wall thickness based on the tube's diameter. Clarity on unit management and showing work is also encouraged for better understanding.
D0m
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Hi guys i have a exam coming up soon and stress is starting to kick in. I am good with stress and strain, but I am just confused on this question and don't understand what i need to be doing. I've tried every formula and i just can't seem to get question 5 out. The answears for this question is underneath the question.

Please have a look at it and tell me what you think, it will also be much appriciated if can write down a solution for them. The question is in the attachment.

Thanks, Dom
 

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What is the formula for determining axial stress in a member?
 
stress= P/A
 
D0m said:
axial [/color]stress= P/A
Yes.
The controlling case for stress and axial load is the compression case, since the load is the greatest and the allowable stress is the smallest. So you know P and and you know the allowable stress. Solve for the required cross sectional area of the hollow tube, A, and from that you can determine the required wall thickness from the given data of the tube's diameter.
 
I understand what you mean but i just don't know how to get started
 
A = P/s. Solve for A. Watch units. What do you get for the area ? Show your work.
 
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