Deformation (engineering)

The study of temporary or elastic deformation in the case of engineering strain is applied to materials used in mechanical and structural engineering, such as concrete and steel, which are subjected to very small deformations. Engineering strain is modeled by infinitesimal strain theory, also called small strain theory, small deformation theory, small displacement theory, or small displacement-gradient theory where strains and rotations are both small.

For some materials, e.g. elastomers and polymers, subjected to large deformations, the engineering definition of strain is not applicable, e.g. typical engineering strains greater than 1%,[1] thus other more complex definitions of strain are required, such as stretch, logarithmic strain, Green strain, and Almansi strain. Elastomers and shape memory metals such as Nitinol exhibit large elastic deformation ranges, as does rubber. However, elasticity is nonlinear in these materials.

Normal metals, ceramics and most crystals show linear elasticity and a smaller elastic range.

Linear elastic deformation is governed by Hooke's law, which states:

${\displaystyle \sigma =E\varepsilon }$

Where ${\displaystyle \sigma }$ is the applied stress, ${\displaystyle E}$ is a material constant called Young's modulus or elastic modulus, and ε is the resulting strain. This relationship only applies in the elastic range and indicates that the slope of the stress vs. strain curve can be used to find Young's modulus (${\displaystyle E}$). Engineers often use this calculation in tensile tests.

Note that not all elastic materials undergo linear elastic deformation; some, such as concrete, gray cast iron, and many polymers, respond in a nonlinear fashion. For these materials Hooke's law is inapplicable.[2]

Since we disregard the change of area during deformation above, the true stress and strain curve should be re-derived. For deriving the stress strain curve, we can assume that the volume change is 0 even if we deformed the materials. We can assume that:

${\displaystyle A_{i}\times \varepsilon _{i}=A_{f}\times \varepsilon _{f}}$

Then, the true stress can be expressed as below:

${\displaystyle \sigma _{T}=F/A_{f}=F/A_{i}\times A_{i}/A_{f}=\sigma _{e}\times l_{f}/l_{i}=\sigma _{E}\times {\frac {l_{i}+\delta l}{l_{i}}}=\sigma _{E}(1+\varepsilon _{E})}$

Additionally, the true strain ε_T can be express as below:

${\displaystyle \varepsilon _{T}={\frac {dl}{l_{0}}}+{\frac {dl}{l_{1}}}+{\frac {dl}{l_{2}}}+\cdots =\sum _{i}{\frac {dl}{l_{i}}}}$

Then, we can express the value as

${\displaystyle \int _{l_{0}}^{l_{i}}{\frac {dl}{l}}\,dx=\ln \left({\frac {l_{i}}{l_{0}}}\right)=\ln(1+\varepsilon _{E})}$

Thus, we can induce the plot in terms of ${\displaystyle \sigma _{T}}$ and ${\displaystyle \varepsilon _{E}}$ as right figure.

Additionally, based on the true stress-strain curve, we can estimate the region where necking starts to happen. Since necking starts to appear after ultimate tensile stress where the maximum force applied, we can express this situation as below:

${\displaystyle dF=0=\sigma _{T}dA_{i}+A_{i}d\sigma _{T}}$

so this form can be expressed as below:

${\displaystyle {\frac {d\sigma _{T}}{\sigma _{T}}}=-{\frac {dA_{i}}{A_{i}}}}$

It indicates that the necking starts to appear where reduction of area becomes much significant compared to the stress change. Then the stress will be localized to specific area where the necking appears.

Additionally, we can induce various relation based on true stress-strain curve.

1) True strain and stress curve can be expressed by the approximate linear relationship by taking a log on true stress and strain. The relation can be expressed as below:

${\displaystyle \sigma _{T}=K\times (\varepsilon _{T})^{n}}$

Where ${\displaystyle K}$ is stress coefficient and ${\displaystyle n}$ is strain-hardening coefficient. Usually, the value of ${\displaystyle n}$ has range around 0.02 to 0.5 at room temperature. If ${\displaystyle n}$ is 1, we can express this material as perfect elastic material.[3][4]

2) In reality, stress is also highly dependent on the rate of strain variation. Thus, we can induce the empirical equation based on the strain rate variation.

${\displaystyle \sigma _{T}=K'\times ({\dot {\varepsilon _{T}}})^{m}}$

True stress-strain curve of FCC metal and its derivative form[3]

Where ${\displaystyle K'}$ is constant related to the material flow stress. ${\displaystyle {\dot {\varepsilon _{T}}}}$ indicates the derivative of strain by the time, which is also known as strain rate. ${\displaystyle m}$ is the strain-rate sensitivity. Moreover, value of ${\displaystyle m}$ is related to the resistance toward the necking. Usually, the value of ${\displaystyle m}$ is at the range of 0-0.1 at room temperature and as high as 0.8 when the temperature is increased.

By combining the 1) and 2), we can create the ultimate relation as below:

${\displaystyle \sigma _{T}=K''\times (\varepsilon _{T})^{n}({\dot {\varepsilon _{T}}})^{m}}$

Where ${\displaystyle K''}$ is the global constant for relating strain, strain rate and stress.

3) Based on the true stress-strain curve and its derivative form, we can estimate the strain necessary to start necking. This can be calculated based on the intersection between true stress-strain curve as shown in right.

This figure also shows the dependency of the necking strain at different temperature. In case of FCC metals, both of the stress-strain curve at its derivative are highly dependent on temperature. Therefore, at higher temperature, necking starts to appear even under lower strain value.

All of these properties indicate the importance of calculating the true stress-strain curve for further analyzing the behavior of materials in sudden environment.

4) A graphical method, so-called "Considere construction", can help determine the behavior of stress-strain curve whether necking or drawing happens on the sample. By setting ${\displaystyle \lambda =L/L_{0}}$as determinant, the true stress and strain can be expressed with engineering stress and strain as below:

${\displaystyle \sigma _{T}=\sigma _{e}\times \lambda ,\qquad \varepsilon _{T}=\ln \lambda .}$

Therefore, the value of engineering stress can be expressed by the secant line from made by true stress and ${\displaystyle \lambda }$ value where ${\displaystyle \lambda =0}$ to ${\displaystyle \lambda =1}$. By analyzing the shape of ${\displaystyle \sigma _{T}-\lambda }$ diagram and secant line, we can determine whether the materials show drawing or necking.

Considere Plot. (a) True stress-strain curve without tangents. There is neither necking nor drawing. (b) With one tangent. There is only necking. (c) With two tangents. There are both necking and drawing.[5]

On the figure (a), there is only concave upward Considere plot. It indicates that there is no yield drop so the material will be suffered from fracture before it yields. On the figure (b), there is specific point where the tangent matches with secant line at point where ${\displaystyle \lambda =\lambda _{Y}}$. After this value, the slope becomes smaller than the secant line where necking starts to appear. On the figure (c), there is point where yielding starts to appear but when ${\displaystyle \lambda =\lambda _{d}}$, the drawing happens. After drawing, all the material will stretch and eventually show fracture. Between ${\displaystyle \lambda _{Y}}$ and ${\displaystyle \lambda _{d}}$, the material itself does not stretch but rather, only the neck starts to stretch out.

Swebor-brand high-strength low alloy steel plate, showing both sides, after plastic deformation from defeating projectiles in ballistics testing. Note: When exposed to fire, steel first expands and then loses its strength, exceeding critical temperature at 538°C or 1000°F per ASTM E119 unless treated with fireproofing.

This type of deformation is not undone simply by removing the applied force. An object in the plastic deformation range, however, will first have undergone elastic deformation, which is undone simply be removing the applied force, so the object will return part way to its original shape. Soft thermoplastics have a rather large plastic deformation range as do ductile metals such as copper, silver, and gold. Steel does, too, but not cast iron. Hard thermosetting plastics, rubber, crystals, and ceramics have minimal plastic deformation ranges. An example of a material with a large plastic deformation range is wet chewing gum, which can be stretched to dozens of times its original length.

Under tensile stress, plastic deformation is characterized by a strain hardening region and a necking region and finally, fracture (also called rupture). During strain hardening the material becomes stronger through the movement of atomic dislocations. The necking phase is indicated by a reduction in cross-sectional area of the specimen. Necking begins after the ultimate strength is reached. During necking, the material can no longer withstand the maximum stress and the strain in the specimen rapidly increases. Plastic deformation ends with the fracture of the material.

Diagram of a stress–strain curve, showing the relationship between stress (force applied) and strain (deformation) of a ductile metal.

Usually, compressive stress applied to bars, columns, etc. leads to shortening.

Loading a structural element or specimen will increase the compressive stress until it reaches its compressive strength. According to the properties of the material, failure modes are yielding for materials with ductile behavior (most metals, some soils and plastics) or rupturing for brittle behavior (geomaterials, cast iron, glass, etc.).

In long, slender structural elements — such as columns or truss bars — an increase of compressive force F leads to structural failure due to buckling at lower stress than the compressive strength.

This type of deformation is also irreversible. A break occurs after the material has reached the end of the elastic, and then plastic, deformation ranges. At this point forces accumulate until they are sufficient to cause a fracture. All materials will eventually fracture, if sufficient forces are applied.