When Does the Nonlinear Stress-Strain Equation Apply?

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Homework Help Overview

The discussion revolves around the application of nonlinear stress-strain equations in material mechanics, specifically comparing a linear equation to a nonlinear one as stress levels increase. Participants are exploring when the nonlinear equation becomes more applicable than the linear representation.

Discussion Character

  • Exploratory, Conceptual clarification, Assumption checking

Approaches and Questions Raised

  • Participants discuss the conditions under which the nonlinear equation may be more appropriate, with references to material behavior beyond the elastic limit and the transition to plasticity. There are questions about the specific stress levels that trigger this transition.

Discussion Status

Some participants have provided insights into the regions of material behavior, such as the non-linear elastic and plastic regions, while others suggest alternative equations commonly used in practice. The discussion reflects a range of interpretations regarding the applicability of the equations presented.

Contextual Notes

There is mention of material-specific behavior, such as that of aluminium alloys, and the implications of exceeding the elastic limit, which may affect the applicability of the equations discussed.

tandoorichicken
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My statics text says the following:

The relationship between axial stress and strain can be represented by the equation
[tex]\sigma = E\epsilon[/tex]

"At higher levels of stress, the following nonlinear equation may be a better fit to describe the correlation between axial stress and strain:
[tex]\sigma = E e^{\epsilon-1}[/tex]
"

Where [itex]\sigma[/itex] is force per unit area, [itex]\epsilon[/itex] is axial strain and E is Young's modulus.

Out of curiosity, at what level of stress does the second equation begin to better represent the situation than the first?
 
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More than likely in the non-linear elastic region.
 
First equation is valid below the material's elastic limit. Below the elastic limit, when the stress is removed the material comes back to it's original length. If you apply sufficiently large stress, then you can pass the elastic limit. Meaning, that upon the removal of the stress the object does not return to its original length.
 
I haven't seen that equation before, but for non-linear behaviour the equations most used are Ramberg-Osgood, especially for materials that have a gradual transition between the elastic linear region to the plasticity. Some examples are aluminium-alloys. Mostly high-strength alloys in aircrafts.
 
cyrusabdollahi said:
More than likely in the non-linear elastic region.
You mean the non-linear plastic region.
 

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