Deformation (physics)

Deformation is the change in the metric properties of a continuous body, meaning that a curve drawn in the initial body placement changes its length when displaced to a curve in the final placement. If none of the curves changes length, it is said that a rigid body displacement occurred. It is convenient to identify a reference configuration or initial geometric state of the continuum body which all subsequent configurations are referenced from. The reference configuration need not be one the body actually will ever occupy. Often, the configuration at is considered the reference configuration, . The configuration at the current time is the current configuration. For deformation analysis, the reference configuration is identified as undeformed configuration, and the current configuration as deformed configuration. Additionally, time is not considered when analyzing deformation, thus the sequence of configurations between the undeformed and deformed configurations are of no interest. The components of the position vector of a particle in the reference configuration, taken with respect to the reference coordinate system, are called the material or reference coordinates. On the other hand, the components of the position vector of a particle in the deformed configuration, taken with respect to the spatial coordinate system of reference, are called the spatial coordinates There are two methods for analysing the deformation of a continuum. One description is made in terms of the material or referential coordinates, called material description or Lagrangian description. A second description of deformation is made in terms of the spatial coordinates it is called the spatial description or Eulerian description. There is continuity during deformation of a continuum body in the sense that: • The material points forming a closed curve at any instant will always form a closed curve at any subsequent time. • The material points forming a closed surface at any instant will always form a closed surface at any subsequent time and the matter within the closed surface will always remain within. Affine deformation An affine deformation is a deformation that can be completely described by an affine transformation. Such a transformation is composed of a linear transformation (such as rotation, shear, extension and compression) and a rigid body translation. Affine deformations are also called homogeneous deformations. Therefore, an affine deformation has the form \mathbf{x}(\mathbf{X},t) = \boldsymbol{F}(t) \cdot \mathbf{X} + \mathbf{c}(t) where is the position of a point in the deformed configuration, is the position in a reference configuration, is a time-like parameter, is the linear transformer and is the translation. In matrix form, where the components are with respect to an orthonormal basis, \begin{bmatrix} x_1(X_1, X_2, X_3, t) \\ x_2(X_1, X_2, X_3, t) \\ x_3(X_1, X_2, X_3, t) \end{bmatrix} = \begin{bmatrix} F_{11}(t) & F_{12}(t) & F_{13}(t) \\ F_{21}(t) & F_{22}(t) & F_{23}(t) \\ F_{31}(t) & F_{32}(t) & F_{33}(t) \end{bmatrix} \begin{bmatrix} X_1 \\ X_2 \\ X_3 \end{bmatrix} + \begin{bmatrix} c_1(t) \\ c_2(t) \\ c_3(t) \end{bmatrix} The above deformation becomes non-affine or inhomogeneous if or . Rigid body motion A rigid body motion is a special affine deformation that does not involve any shear, extension or compression. The transformation matrix is proper orthogonal in order to allow rotations but no reflections. A rigid body motion can be described by \mathbf{x}(\mathbf{X},t) = \boldsymbol{Q}(t)\cdot\mathbf{X} + \mathbf{c}(t) where \boldsymbol{Q}\cdot\boldsymbol{Q}^T = \boldsymbol{Q}^T \cdot \boldsymbol{Q} = \boldsymbol{\mathit{1}} In matrix form, \begin{bmatrix} x_1(X_1, X_2, X_3, t) \\ x_2(X_1, X_2, X_3, t) \\ x_3(X_1, X_2, X_3, t) \end{bmatrix} = \begin{bmatrix} Q_{11}(t) & Q_{12}(t) & Q_{13}(t) \\ Q_{21}(t) & Q_{22}(t) & Q_{23}(t) \\ Q_{31}(t) & Q_{32}(t) & Q_{33}(t) \end{bmatrix} \begin{bmatrix} X_1 \\ X_2 \\ X_3 \end{bmatrix} + \begin{bmatrix} c_1(t) \\ c_2(t) \\ c_3(t) \end{bmatrix} ==Background: displacement==

A change in the configuration of a continuum body results in a displacement. The displacement of a body has two components: a rigid-body displacement and a deformation. A rigid-body displacement consists of a simultaneous translation and rotation of the body without changing its shape or size. Deformation implies the change in shape and/or size of the body from an initial or undeformed configuration to a current or deformed configuration (Figure 1). If after a displacement of the continuum there is a relative displacement between particles, a deformation has occurred. On the other hand, if after displacement of the continuum the relative displacement between particles in the current configuration is zero, then there is no deformation and a rigid-body displacement is said to have occurred. The vector joining the positions of a particle P in the undeformed configuration and deformed configuration is called the displacement vector in the Lagrangian description, or in the Eulerian description. A displacement field is a vector field of all displacement vectors for all particles in the body, which relates the deformed configuration with the undeformed configuration. It is convenient to do the analysis of deformation or motion of a continuum body in terms of the displacement field. In general, the displacement field is expressed in terms of the material coordinates as \mathbf u(\mathbf X, t) = \mathbf b(\mathbf X,t) + \mathbf x(\mathbf X,t) - \mathbf X \qquad \text{or}\qquad u_i = \alpha_{iJ}b_J + x_i - \alpha_{iJ} X_J or in terms of the spatial coordinates as \mathbf U(\mathbf x, t) = \mathbf b(\mathbf x, t) + \mathbf x - \mathbf X(\mathbf x, t) \qquad \text{or}\qquad U_J = b_J + \alpha_{Ji} x_i - X_J where are the direction cosines between the material and spatial coordinate systems with unit vectors and , respectively. Thus \mathbf E_J \cdot \mathbf e_i = \alpha_{Ji} = \alpha_{iJ} and the relationship between and is then given by u_i = \alpha_{iJ} U_J \qquad \text{or} \qquad U_J = \alpha_{Ji} u_i Knowing that \mathbf e_i = \alpha_{iJ} \mathbf E_J then \mathbf u(\mathbf X, t) = u_i \mathbf e_i = u_i (\alpha_{iJ}\mathbf E_J) = U_J \mathbf E_J = \mathbf U(\mathbf x, t) It is common to superimpose the coordinate systems for the undeformed and deformed configurations, which results in , and the direction cosines become Kronecker deltas: \mathbf E_J \cdot \mathbf e_i = \delta_{Ji} = \delta_{iJ} Thus, we have \mathbf u(\mathbf X, t) = \mathbf x(\mathbf X, t) - \mathbf X \qquad \text{or} \qquad u_i = x_i - \delta_{iJ} X_J = x_i - X_i or in terms of the spatial coordinates as \mathbf U(\mathbf x, t) = \mathbf x - \mathbf X(\mathbf x, t) \qquad \text{or} \qquad U_J = \delta_{Ji} x_i - X_J = x_J - X_J Displacement gradient tensor The partial differentiation of the displacement vector with respect to the material coordinates yields the material displacement gradient tensor . Thus we have: \begin{align} \mathbf{u}(\mathbf{X},t) & = \mathbf{x}(\mathbf{X},t) - \mathbf{X} \\ \nabla_\mathbf{X}\mathbf{u} & = \nabla_\mathbf{X} \mathbf{x} - \mathbf{I} \\ \nabla_\mathbf{X}\mathbf{u} & = \mathbf{F} - \mathbf{I} \end{align} or \begin{align} u_i & = x_i - \delta_{iJ} X_J = x_i - X_i\\ \frac{\partial u_i}{\partial X_K} & = \frac{\partial x_i}{\partial X_K} - \delta_{iK} \end{align} where is the deformation gradient tensor. Similarly, the partial differentiation of the displacement vector with respect to the spatial coordinates yields the spatial displacement gradient tensor . Thus we have, \begin{align} \mathbf U(\mathbf x,t) &= \mathbf x - \mathbf X(\mathbf x,t) \\ \nabla_{\mathbf x} \mathbf U &= \mathbf I - \nabla_{\mathbf x} \mathbf X \\ \nabla_{\mathbf x} \mathbf U &= \mathbf I -\mathbf F^{-1} \end{align} or \begin{align} U_J& = \delta_{Ji}x_i-X_J =x_J - X_J\\ \frac{\partial U_J}{\partial x_k} &= \delta_{Jk} - \frac{\partial X_J}{\partial x_k} \end{align} ==Examples==

Homogeneous (or affine) deformations are useful in elucidating the behavior of materials. Some homogeneous deformations of interest are • uniform extension • pure dilation • equibiaxial tension • simple shear • pure shear Linear or longitudinal deformations of long objects, such as beams and fibers, are called elongation or shortening; derived quantities are the relative elongation and the stretch ratio. Plane deformations are also of interest, particularly in the experimental context. Volume deformation is a uniform scaling due to isotropic compression; the relative volume deformation is called volumetric strain. Plane deformation A plane deformation, also called plane strain, is one where the deformation is restricted to one of the planes in the reference configuration. If the deformation is restricted to the plane described by the basis vectors , , the deformation gradient has the form \boldsymbol{F} = F_{11} \mathbf{e}_1 \otimes \mathbf{e}_1 + F_{12} \mathbf{e}_1 \otimes \mathbf{e}_2 + F_{21} \mathbf{e}_2 \otimes \mathbf{e}_1 + F_{22} \mathbf{e}_2 \otimes \mathbf{e}_2 + \mathbf{e}_3 \otimes \mathbf{e}_3 In matrix form, \boldsymbol{F} = \begin{bmatrix} F_{11} & F_{12} & 0 \\ F_{21} & F_{22} & 0 \\ 0 & 0 & 1 \end{bmatrix} From the polar decomposition theorem, the deformation gradient, up to a change of coordinates, can be decomposed into a stretch and a rotation. Since all the deformation is in a plane, we can write \boldsymbol{F} = \boldsymbol{R}\cdot\boldsymbol{U} = \begin{bmatrix} \cos\theta & \sin\theta & 0 \\ -\sin\theta & \cos\theta & 0 \\ 0 & 0 & 1 \end{bmatrix} \begin{bmatrix} \lambda_1 & 0 & 0 \\ 0 & \lambda_2 & 0 \\ 0 & 0 & 1 \end{bmatrix} where is the angle of rotation and , are the principal stretches. Isochoric plane deformation If the deformation is isochoric (volume preserving) then and we have F_{11} F_{22} - F_{12} F_{21} = 1 Alternatively, \lambda_1 \lambda_2 = 1 Simple shear A simple shear deformation is defined as an isochoric plane deformation in which there is a set of line elements with a given reference orientation that do not change length and orientation during the deformation. If is the fixed reference orientation in which line elements do not deform during the deformation then and . Therefore, F_{11}\mathbf{e}_1 + F_{21}\mathbf{e}_2 = \mathbf{e}_1 \quad \implies \quad F_{11} = 1 ~;~~ F_{21} = 0 Since the deformation is isochoric, F_{11} F_{22} - F_{12} F_{21} = 1 \quad \implies \quad F_{22} = 1 Define \gamma := F_{12} Then, the deformation gradient in simple shear can be expressed as \boldsymbol{F} = \begin{bmatrix} 1 & \gamma & 0 \\ 0 & 1 & 0 \\ 0 & 0 & 1 \end{bmatrix} Now, \boldsymbol{F}\cdot\mathbf{e}_2 = F_{12}\mathbf{e}_1 + F_{22}\mathbf{e}_2 = \gamma\mathbf{e}_1 + \mathbf{e}_2 \quad \implies \quad \boldsymbol{F} \cdot (\mathbf{e}_2 \otimes \mathbf{e}_2) = \gamma \mathbf{e}_1\otimes \mathbf{e}_2 + \mathbf{e}_2 \otimes\mathbf{e}_2 Since \mathbf{e}_i \otimes \mathbf{e}_i = \boldsymbol{\mathit{1}} we can also write the deformation gradient as \boldsymbol{F} = \boldsymbol{\mathit{1}} + \gamma\mathbf{e}_1 \otimes \mathbf{e}_2 ==See also==