How Do I Correctly Calculate and Plot Stress-Strain for a Physics Test?

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To calculate and plot the stress-strain graph, the maximum tensile stress has been correctly calculated as 541.5 MPa using the formula 42700/78.85. The engineering stress-strain curve is typically used, which does not account for necking, while the true stress-strain curve does. The final extension of 10 mm corresponds to a total length of 60 mm after breaking. With the available data, the engineering stress at the break point is 394.4 MPa, and the engineering strain at the break point is 0.2. Limited information restricts the ability to plot a comprehensive stress-strain curve beyond the break point.
MCooltA
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I need to draw a stress and strain graph. New to physics, so would like to know if i am on the right line and require a bit of help for the last few questions

These are the values I have:

Diameter - 10.02mm
Original Length - 50mm
Extension -10mm
Diameter After Test - 6.76mm
Max Load - 42.7 kN
Break Point - 31 kN

Found the cross sectional area to be - 78.85

So for the maximum tensile stress, i done

42700/78.85 = 541.5 MPa ... Is this correct?

How do i go about calculating the strain for this value so i can plot it on my graph. I know the formulas, but wasnt given a extension at the Max Load?

Thanks
 
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There is a differenve between the engineering stress-strain curve and the true stress-strain curve. The engineering stress-strain curve does not take into account the 'necking down' of the cross sectional area, whereas the true stess -strain curve does. The engineering curve is most often used. Your calc for the max stress is correct. if you weren't given any intermediate extension values as a function of stress, you can't do much with a plot of the curve. Was the the 10 mm extension at the break point, or max load point, or other point?
 
10mm was the final extension, so a total of 60mm, after it had broken.

And i am trying to calculate the engineering stress and engineering strain. Thanks
 
Last edited:
MCooltA said:
10mm was the final extension, so a total of 60mm, after it had broken.
If that's all the info you have, you can compute the stress-strain only at the break point (engineering stress at break point = 31000/78.85 MPa, and strain at break point = 10/50). You don't have much else to work with.
 
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