6 Stress and strain
6.1 Stress
6.1.1 Normal stress
- Normal stress is the resultant normal force over a given area
\[\sigma = \frac{P}{A}\]
6.1.2 Shear stress
- Shear stress is the resultant shear force over a given area
\[\tau = \frac{V}{A}\]
6.1.3 Stresses on arbitrary planes
- Since different “cuts” must yield the same resultant force, the stress depends on your plane of observation
- Each type of stress is simultaneously present13
- A body can fail in shear even when loaded by normal stress
- Ductile materials typically yield due to shear stress
- Brittle materials typically crack due to normal stress
6.1.4 Stress
Note
Stresses result from equilibrium (ie the sum of forces)
It is possible to have stress without strain
Example: thermal expansion/contraction
Exothermic reactions such as bone cement
Cement then adjusts to body temperature
Constrained by bone and implant \(\rightarrow\) stress
6.2 Strain
6.2.1 Normal strain
- Normal strain is the change in length over the original length
\[{\varepsilon}= \frac{\Delta l}{l}\]
6.2.2 Shear strain
- Shear strain (\(\gamma\)) is proportional to the shear angle (\(\alpha\)) \[\gamma = \alpha\]
6.2.3 Strain
Note
- Strain is defined by deformation
- It is possible to have strain without stress
- Tissues expand with moisture content
- PMMA shrinkage during polymerization
6.2.4 A chain of relationships in biomechanics
Constraints |
\(\Updownarrow\) |
Deformation |
\(\Updownarrow\) |
Strain |
\(\Updownarrow\) |
Stress |
\(\Updownarrow\) |
Equilibrium |
\(\Updownarrow\) |
Applied Loads |
- Each arrow represents a relationship that must be understood and properly accounted
except in unusual circumstances↩︎