# 1.4 Constitutive Models, Stiffness and Flexibility

A *constitutive model* is the link between the stresses and strains of a structure. Of course, stresses are linked to forces and strains are linked to deformations. If we apply a certain set of forces to a structure, how will it elongate, compress, bend or move? It depends on the shape of the structure, but it also depends on what the structure is made of. Different materials deform in different ways in different directions. A constitutive model describes the behaviour of an individual material under load.

The simplest type of constitutive relationship is for the linear axial deformation of a uniform bar:

\begin{align}

\sigma &= E \epsilon

\end{align}

where $\sigma$ is stress, $E$ is the Young's Modulus, and $\epsilon$ is strain. In this relationship, $E$ is the constitutive model that links axial stress $\sigma$ (related to force) and the axial strain $\epsilon$. Of course, things get considerably more complex if we have to consider more than one direction of deformation, for example, if you have a beam (which can bend as well as deform axially), or if you have a plate or block that deforms. For these systems, it is typically convenient to represent the constitutive model as a matrix of values instead of the single value $E$. For example, for a isotropic thin plate (i.e. the material behaves the same in all directions and there is no stress out of plane), the constitutive relationship may look like:

\begin{equation}

\begin{Bmatrix}

\sigma_{11} \\

\sigma_{22} \\

\sigma_{12}

\end{Bmatrix}

= \frac{E}{1-\nu^2}

\begin{bmatrix}

1 & \nu & 0 \\[6pt]

\nu & 1 & 0 \\[6pt]

0 & 0 & \dfrac{1-\nu}{2}

\end{bmatrix}

\begin{Bmatrix}

\epsilon_{11} \\

\epsilon_{22} \\

2\epsilon_{12}

\end{Bmatrix}

\end{equation}

where $\sigma_{11}$, $\sigma_{22}$, $\epsilon_{11}$, and $\epsilon_{22}$ are axial stresses and strains in two dimensions, $\sigma_{12}$ and $\epsilon_{12}$ are shear stresses and strains, and $\nu$ is Poisson's ratio for the material. As you would imagine, the situation is considerably more complex in 3D.

If we stick with a uniform bar for now and assume a constant cross-sectional area $A$ and a length of $L$, then we can expand this relationship to force ($P$) and deformation ($\Delta$). We can do this by using the mechanics relationships that stress is equal to force divided by area and strain, and strain is change in elongation ($\Delta$) divided by initial length:

\begin{equation}

\sigma = \frac{P}{A} \quad \text{,} \quad \epsilon = \frac{\delta}{L}

\end{equation}

Therefore,

\begin{align}

\frac{P}{A} &= E \left( \frac{\delta}{L} \right) \\

\delta &= \frac{PL}{EA} \label{eq:PLEA}

\end{align}

The relationship in equation \eqref{eq:PLEA} can be rewritten in terms of a Hooke's Law relationship:

\begin{equation}

P = k \delta

\end{equation}

where

\begin{equation} \label{eq:Stiffness}

k = \frac{EA}{L}

\end{equation}

In these equations, $k$ is the *stiffness*, which is the relationship between force and deformation (or force and displacement). The stiffness is the amount of force that must be applied in order to get a single unit of deformation. Therefore, the units for stiffness are force per unit distance. For example, if the stiffness is 20 kN\textbackslash m then this means that 20 kN must be applied to deform the structure by a unit of deformation, which in this case is 1 m. It also means that it would take 40 kN to deform by 2 m. A structure that is more *stiff* takes more force to move a given distance. It is also possible to have rotational stiffness for a structure that can bend, which is the relationship between moment and rotation.

The inverse of stiffness is called *flexibility*. Flexibility is given in units of distance per unit force. For the example in equation \eqref{eq:Stiffness}, the flexibility would be:

\begin{align}

f &= \frac{1}{k} \\

f &= \frac{L}{EA}

\end{align}

A structure that is more *flexible* takes less force to move a given distance.