Engineering Stress increases after yield stress?

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Discussion Overview

The discussion centers on the behavior of engineering stress after reaching the yield stress point, specifically why it continues to increase until the ultimate tensile strength (UTS). Participants explore concepts such as strain hardening and the relationship between applied force and stress in the context of tensile testing of materials like steel, copper, and aluminum.

Discussion Character

  • Technical explanation
  • Homework-related
  • Exploratory

Main Points Raised

  • One participant questions the increase in engineering stress after yield stress, suggesting that strain hardening occurs in this region and asking for a better engineering explanation.
  • Another participant reiterates the question and emphasizes that the increase in applied force leads to an increase in stress, regardless of the calculation method.
  • A later post clarifies that the inquiry is related to a lab report involving tensile tests on multiple materials.
  • One participant references dislocation and work hardening as relevant topics for understanding the phenomenon.
  • Another participant mentions that their instructor indicated the answer involves cold work and strain hardening due to dislocations from plastic deformation.

Areas of Agreement / Disagreement

Participants express a shared understanding of the concepts of strain hardening and dislocations, but the discussion remains exploratory without a definitive consensus on the best explanation for the observed behavior of engineering stress.

Contextual Notes

The discussion does not resolve the complexities of how strain hardening and dislocation mechanisms specifically contribute to the increase in engineering stress, nor does it clarify the assumptions underlying the participants' claims.

Who May Find This Useful

Students and professionals interested in material science, engineering mechanics, and the behavior of materials under tensile testing may find this discussion relevant.

Seth Vogt
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I need to know why the Engineering stress increases after reaching the yield stress point, and continues to increase until reaching the UTS. Am I correct when I remember that there is strain hardening that occurs along the region from Yield stress to the Ultimate tensile stress? Engineering stress equals Force divided by Original cross-sectional area: σ=F/Ao
My first thoughts were that obviously as you increase the force, the stress will increase (from a purely mathematical outlook, this is apparent since stress increases proportionally to force). How could this be explained in better engineering terms?
Thanks
 
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Seth Vogt said:
I need to know why the Engineering stress increases after reaching the yield stress point, and continues to increase until reaching the UTS. Am I correct when I remember that there is strain hardening that occurs along the region from Yield stress to the Ultimate tensile stress? Engineering stress equals Force divided by Original cross-sectional area: σ=F/Ao
My first thoughts were that obviously as you increase the force, the stress will increase (from a purely mathematical outlook, this is apparent since stress increases proportionally to force). How could this be explained in better engineering terms?
Thanks
Does it need a better explanation than the increase in applied force leads to an increase in stress, regardless of how that stress is calculated?
 
The question is: "From the onset of plastic deformation up to the UTS, the engineering stress increases. Discuss in Engineering terms why."
This is for a lab report in which we performed a tensile test on three materials, steel, copper, and aluminum
 
Yes, thank you both for your insight. I asked the instructor also, and the answer he was looking for was regarding the cold work/strain hardening that occurs as a result of dislocations from the plastic deformation.
 

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