# Stress–strain curve

The relationship between the stress and strain that a particular material displays is known as that particular material's stress–strain curve. It is unique for each material and is found by recording the amount of deformation (strain) at distinct intervals of a variety of loadings (stress). These curves reveal many of the properties of a material (including data to establish the Modulus of Elasticity, E).[1]

Generally speaking, curves representing the relationship between stress and strain in any form of deformation can be regarded as stress-strain curves. The stress and strain can be normal, shear, or mixture, also can be uniaxial, biaxial, or multiaxial, even change with time. The form of deformation can be compression, stretching, torsion, rotation, and so on. If not mentioned otherwise, stress–strain curve refers to the relationship between axial normal stress and axial normal strain of materials measured in a tension test.

Consider a bar of original cross sectional area A being subjected to equal and opposite forces F pulling at the ends so the bar is under tension. The material is experiencing a stress defined to be the ratio of the force to the cross sectional area of the bar, as well as an axial elongation:

${\displaystyle \mathrm {\sigma } ={\tfrac {F}{A_{0}}}}$
${\displaystyle \mathrm {\epsilon } ={\tfrac {L-L_{0}}{L_{0}}}={\tfrac {\Delta L}{L_{0}}}}$

Subscript 0 denotes the original dimensions of the sample. The SI unit for stress is newton per square metre, or pascal (1 pascal = 1 Pa = 1 N/m2), and for strain is "1". Stress-strain curve for this material is plotted by elongating the sample and recording the stress variation with strain until the sample fractures. By convention, the strain is set to the horizontal axis and stress is set to vertical axis. Note that for engineering purposes we often assume the cross-section area of the material does not change during the whole deformation process. This is not true since the actual area will decrease while deforming due to elastic and plastic deformation. The curve assuming the cross-section area is fixed is called the “engineering stress-strain curve”, while the curve based on the actual cross-section area is the “true stress-strain curve”. If not mentioned otherwise, the relationship between true stress-strain curve and engineering stress-strain curve will be discussed later.

## Stages

A schematic diagram for the stress-strain curve of low carbon steel at room temperature is shown in figure 2. There are several stages showing different behaviors, which suggests different mechanical properties. To clarify, materials can miss one or more stages shown in figure 2, or have totally different stages.

The first stage is the linear elastic region. The stress is proportional to the strain, that is, obeys the general Hooke's law, and the slope is Young's modulus. In this region, the material undergoes only elastic deformation. The end of the stage is the initiation point of plastic deformation. The stress component of this point is defined as yield strength (or upper yield point, UYP for short).

The second stage is the strain hardening region. This region starts as the strain goes beyond yielding point, and ends at the ultimate strength point, which is the maximal stress shown in the stress-strain curve (tensile strength, T.S., also sometimes referred to as the ultimate tensile strength, D.T.S.). In this region, the stress mainly increases as material elongates, except that there is a nearly flat region at the beginning. The stress of the flat region is defined as the lower yield point (LYP) and results from the formation and propagation of Lüders bands. Explicitly, heterogeneous plastic deformation forms bands at the upper yield strength and these bands carrying with deformation spread along the sample at the lower yield strength. After the sample is again uniformly deformed, the increase of stress with the progress of extension results from work strengthening, that is, dense dislocations induced by plastic deformation hampers the further motion of dislocations. To overcome these obstacles, a higher resolved shear stress should be applied. As the strain accumulates, work strengthening gets reinforced, till the stress reaches the tensile strength.

The third stage is the necking region. Beyond tensile strength, a neck forms where the local cross-sectional area becomes significantly smaller than the average. The necking deformation is heterogenous and will reinforce itself as the stress concentrates more at small section. Such positive feedback leads to quick development of necking and leads to fracture. Note that though the pulling force is decreasing, the work strengthening is still progressing, that is, the true stress keeps growing but the engineering stress decreases because the shrinking section area is not considered. This region ends up with the fracture. After fracture, percent elongation and reduction in section area can be calculated.

## Relationship with true stress and strain

Due to the shrinking of section area and the ignored effect of developed elongation to further elongation, true stress and strain are different from engineering stress and strain.

${\displaystyle \mathrm {\sigma _{t}} ={\tfrac {F}{A}}}$
${\displaystyle \mathrm {\epsilon _{t}} =\int {\tfrac {\delta L}{L}}}$

Here the dimensions are instant values. Assuming volume of the sample conserves and deformation happens uniformly,

${\displaystyle A_{0}L_{0}=AL}$

The true stress and strain can be expressed by engineering stress and strain. For true stress,

${\displaystyle \mathrm {\sigma _{t}} ={\tfrac {F}{A}}={\tfrac {F}{A_{0}}}\cdot {\tfrac {A_{0}}{A}}={\tfrac {F}{A_{0}}}\cdot {\tfrac {L}{L_{0}}}=\sigma \cdot (1+\epsilon )}$

For the strain,

${\displaystyle \mathrm {\delta \epsilon _{t}} ={\tfrac {\delta L}{L}}}$

Integrate both sides and apply the boundary condition,

${\displaystyle \mathrm {\epsilon _{t}} =\ln \left({\tfrac {L}{L_{0}}}\right)=\ln(1+\epsilon )}$

So in a tension test, true stress is larger than engineering stress and true strain is less than engineering strain. Thus, a point defining true stress-strain curve is displaced upwards and to the left to define the equivalent engineering stress-strain curve. The difference between the true and engineering stresses and strains will increase with plastic deformation. At low strains (such as elastic deformation), the differences between the two is negligible. As for the tensile strength point, it is the maximal point in engineering stress-strain curve but is not a special point in ture stress-strain curve. Because engineering stress is proportional to the force applied along the sample, the criterion for necking formation can be set as ${\displaystyle \mathrm {\delta {\textit {F}}} =0}$.

${\displaystyle \mathrm {\delta {\textit {F}}} =0=\sigma _{t}\cdot \delta A+A\cdot \delta \sigma _{t}}$

${\displaystyle \mathrm {-{\tfrac {\delta A}{A}}} =\mathrm {\tfrac {\delta \sigma _{t}}{\sigma _{t}}} }$

This analysis suggests nature of the UTS point. The work strengthening effect is exactly balanced by the shrinking of section area at UTS point.

After the formation of necking, the sample undergoes heterogeneous deformation, so equations above are not valid. The stress and strain at the necking can be expressed as:

${\displaystyle \mathrm {\sigma _{t}} ={\tfrac {F}{A_{neck}}}}$
${\displaystyle \mathrm {\epsilon _{t}} =\ln \left({\tfrac {A_{0}}{A_{neck}}}\right)}$

An empirical equation is commonly used to describe the relationship between true stress and strain.

${\displaystyle \mathrm {\sigma _{t}} =K(\epsilon _{t})^{n}}$

Here, n is strain-hardening coefficient and K is the strength coefficient. n is a measure of material' work hardening behavior. Materials with a higher n has a greater resistance to necking. Typically, metals at room temperature has n ranging from 0.02 to 0.5.[2]

## Classification

It is possible to distinguish some common characteristics among the stress–strain curves of various groups of materials and, on this basis, to divide materials into two broad categories; namely, the ductile materials and the brittle materials.[3]

### Ductile materials

Ductile materials, which includes structural steel and many alloys of other metals, are characterized by their ability to yield at normal temperatures.[4]

Low carbon steel generally exhibits a very linear stress–strain relationship up to a well defined yield point (Fig.2). The linear portion of the curve is the elastic region and the slope is the modulus of elasticity or Young's Modulus . Many ductile materials including some metals, polymers and ceramics exhibit a yield point. Plastic flow initiates at the upper yield point and continues at the lower one. At lower yield point, permanent deformation is heterogeneously distributed along the sample. The deformation band which formed at the upper yield point will propagate along the gauge length at the lower yield point. The band occupies the whole of the gauge at the luders strain. Beyond this point, work hardening commences. The appearance of the yield point is associated with pinning of dislocations in the system. For example, solid solution interacts with dislocations and acts as pin and prevent dislocation from moving. Therefore, the stress needed to initiate the movement will be large. As long as the dislocation escape from the pinning, stress needed to continue it is less.

After the yield point, the curve typically decreases slightly because of dislocations escaping from Cottrell atmospheres. As deformation continues, the stress increases on account of strain hardening until it reaches the ultimate tensile stress. Until this point, the cross-sectional area decreases uniformly because of Poisson contractions. Then it starts necking and finally fractures.

The appearance of necking in ductile materials is associated with geometrical instability in the system. Due to the natural inhomogeneity of the material, it is common to find some regions with small inclusions or porosity within it or surface, where strain will concentrate, leading to a locally smaller area than other regions. For strain less than the ultimate tensile strain, the increase of work-hardening rate in this region will be greater than the area reduction rate, thereby make this region harder to be further deform than others, so that the instability will be removed, i.e. the materials have abilities to weaken the inhomogeneity before reaching ultimate strain. However, as the strain become larger, the work hardening rate will decreases, so that for now the region with smaller area is weaker than other region, therefore reduction in area will concentrate in this region and the neck becomes more and more pronounced until fracture. After the neck has formed in the materials, further plastic deformation is concentrated in the neck while the remainder of the material undergoes elastic contraction owing to the decrease in tensile force.

The stress-strain curve for a ductile material can be approximated using the Ramberg-Osgood equation.[5] This equation is straightforward to implement, and only requires the material's yield strength, ultimate strength, elastic modulus, and percent elongation.

### Brittle materials

Brittle materials, which includes cast iron, glass, and stone, are characterized by the fact that rupture occurs without any noticeable prior change in the rate of elongation,[6] sometimes they fracture before yielding.

Brittle materials such as concrete or carbon fiber do not have a well-defined yield point, and do not strain-harden. Therefore, the ultimate strength and breaking strength are the same. A typical stress–strain curve is shown in Fig.5. Typical brittle materials like glass do not show any plastic deformation but fail while the deformation is elastic. One of the characteristics of a brittle failure is that the two broken parts can be reassembled to produce the same shape as the original component as there will not be a neck formation like in the case of ductile materials. A typical stress–strain curve for a brittle material will be linear. For some materials, such as concrete, tensile strength is negligible compared to the compressive strength and it is assumed zero for many engineering applications. Glass fibers have a tensile strength stronger than steel, but bulk glass usually does not. This is because of the stress intensity factor associated with defects in the material. As the size of the sample gets larger, the size of defects also grows. In general, the tensile strength of a rope is always less than the sum of the tensile strengths of its individual fibers.

## Influencing factors

The stress–strain curves of various materials vary widely, as a result of various intrinsic structures and compositions. Due to extrinsic factors, different tensile tests conducted on the same material yield different results, mainly depending upon the temperature of the specimen and the speed of the loading. The boundary between intrinsic and extrinsic factors is not rigid, if further mechanism is illustrated. Many factors can have an influence on the stress-strain curve by adjusting Young' modulus, strengthening, toughening, as long as they modify the structure and compositions.

Time is often neglected in the stress-strain curve relations, but at higher strain rates, higher stresses will occur according to the relationship

${\displaystyle \mathrm {\sigma _{t}} =K({\dot {\epsilon }}_{T})^{m}}$

where m is the strain rate sensitivity. The higher m is, the greater resistance to necking this material will have, just like the case of work-hardening coefficient.

Another dominant factor is the temperature. Temperature controls the activation of dislocations and diffusions. As the temperature increases, brittle materials can be transformed into ductile materials.