JonOl
Structural
- Aug 23, 2021
- 5
Hi!
I have made a stress-strain curve for 245SMO material (S31254), which has S_y = 310MPa and S_u = 670MPa according to ASME II part D. My material datasheet tells me that the elongation at failure is 35% (engineering strain). Now, using the formulas in AMSE VIII Annex 3-D, I calculate true ultimate tensile stress to be 1042MPa, with a true ultimate strain of 41,8%. This corresponds to an engineering ultimate strain of 52%, way higher than my strain at failure!
If my calculations are correct, can anyone help me understand how this is conservative in any way?
Note: I'm using ASME VIII div 2 2019
I have made a stress-strain curve for 245SMO material (S31254), which has S_y = 310MPa and S_u = 670MPa according to ASME II part D. My material datasheet tells me that the elongation at failure is 35% (engineering strain). Now, using the formulas in AMSE VIII Annex 3-D, I calculate true ultimate tensile stress to be 1042MPa, with a true ultimate strain of 41,8%. This corresponds to an engineering ultimate strain of 52%, way higher than my strain at failure!
If my calculations are correct, can anyone help me understand how this is conservative in any way?
Note: I'm using ASME VIII div 2 2019