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{{continuum mechanics|cTopic=[[Solid mechanics]]}}
[[Image:Hyperelastic.svg|thumb|290px|right|Stress-strain curves for various hyperelastic material models.]]
A '''hyperelastic''' or '''Green elastic''' material<ref name=Ogden>R.W. Ogden, 1984, ''Non-Linear Elastic Deformations'', ISBN 0-486-69648-0, Dover.</ref> is a type of [[Constitutive equation|constitutive model]] for ideally [[elastic (solid mechanics)|elastic]] material for which the stress-strain relationship derives from a [[strain energy density function]]. The hyperelastic material is a special case of a [[Cauchy elastic material]].
For many materials, [[Elasticity (physics)|linear elastic]] models do not accurately describe the observed material behaviour.  The most common example of this kind of material is rubber, whose [[stress (physics)|stress]]-[[strain (physics)|strain]] relationship can be defined as non-linearly elastic, [[isotropic]], [[incompressible]] and generally independent of [[strain rate]].  Hyperelasticity provides a means of modeling the stress-strain behavior of such materials.<ref>Muhr, A. H. (2005). Modeling the stress-strain behavior of rubber. Rubber chemistry and technology, 78(3), 391-425. [http://dx.doi.org/10.5254/1.3547890]</ref>  The behavior of unfilled, [[vulcanized]] [[elastomers]] often conforms closely to the hyperelastic ideal.  Filled elastomers and [[biological tissues]] are also often modeled via the hyperelastic idealization.
 
[[Ronald Rivlin]] and [[Melvin Mooney]] developed the first hyperelastic models, the [[Neo-Hookean solid|Neo-Hookean]] and [[Mooney–Rivlin solid|Mooney–Rivlin]] solids.  Many other hyperelastic models have since been developed.  Other widely used hyperelastic material models include the [[Ogden (hyperelastic model)|Ogden]] model and the [[Arruda–Boyce model]].
 
==Hyperelastic material models==
 
=== Saint Venant–Kirchhoff model ===
The simplest hyperelastic material model is the Saint Venant–Kirchhoff model which is just an extension of the linear elastic material model to the nonlinear regime.  This model has the form
:<math>
\boldsymbol{S} = \lambda~ \text{tr}(\boldsymbol{E})\boldsymbol{\mathit{1}} + 2\mu\boldsymbol{E}
</math>
where <math>\boldsymbol{S}</math> is the second Piola–Kirchhoff stress and <math>\boldsymbol{E}</math> is the Lagrangian Green strain, and <math>\lambda</math> and <math>\mu</math> are the [[Lame constants|Lamé constants]].
 
The strain-energy density function for the St. Venant–Kirchhoff model is
:<math>
W(\boldsymbol{E}) = \frac{\lambda}{2}[\text{tr}(\boldsymbol{E})]^2 + \mu \text{tr}(\boldsymbol{E}^2)
</math>
and the second Piola–Kirchhoff stress can be derived from the relation
:<math>
  \boldsymbol{S} = \cfrac{\partial W}{\partial \boldsymbol{E}} ~.
</math>
 
=== Classification of hyperelastic material models ===
Hyperelastic material models can be classified as:
 
1) [[Phenomenology (science)|phenomenological]] descriptions of observed behavior
*[[Soft tissue#Fung-elastic material|Fung]]
*[[Mooney–Rivlin solid|Mooney–Rivlin]]
*[[Ogden (hyperelastic model)|Ogden]]
*[[Polynomial (hyperelastic model)|Polynomial]]
*Saint Venant–Kirchhoff
*[[Yeoh (hyperelastic model)|Yeoh]]
*[[Marlow (hyperelastic model)|Marlow]]
 
2) [[Rubber elasticity|mechanistic models]] deriving from arguments about underlying structure of the material
*[[Arruda–Boyce model]]
*[[Neo-Hookean solid|Neo-Hookean]]
 
3) hybrids of phenomenological and mechanistic models
*[[Gent (hyperelastic model)|Gent]]
*[[Van der Waals (hyperelatic model)|Van der Waals]]
 
Generally, a hyperelastic model should satisfy the [[Drucker stability]] criterion.
 
== Stress-strain relations ==
 
=== Compressible hyperelastic materials ===
 
==== First Piola–Kirchhoff stress ====
If <math>W(\boldsymbol{F})</math> is the strain energy density function, the [[Piola–Kirchhoff stress tensor|1st Piola–Kirchhoff stress tensor]] can be calculated for a hyperelastic material as
:<math>
  \boldsymbol{P} = \frac{\partial W}{\partial \boldsymbol{F}}  \qquad \text{or} \qquad P_{iK} = \frac{\partial W}{\partial F_{iK}}.
</math>
where <math>\boldsymbol{F}</math> is the [[deformation gradient]].  In terms of the [[Finite_strain_theory#Finite_strain_tensors|Lagrangian Green strain]] (<math>\boldsymbol{E}</math>)
:<math>
  \boldsymbol{P} = \boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{E}} \qquad \text{or} \qquad P_{iK} = F_{iL}~\frac{\partial W}{\partial E_{LK}} ~.
</math>
In terms of the [[finite strain theory|right Cauchy–Green deformation tensor]] (<math>\boldsymbol{C}</math>)
:<math>
  \boldsymbol{P} = 2~\boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{C}} \qquad \text{or} \qquad P_{iK} = 2~F_{iL}~\frac{\partial W}{\partial C_{LK}} ~.
</math>
 
==== Second Piola–Kirchhoff stress ====
If <math>\boldsymbol{S}</math> is the [[Piola–Kirchhoff stress tensor|second Piola–Kirchhoff stress tensor]] then
:<math>
  \boldsymbol{S} = \boldsymbol{F}^{-1}\cdot\frac{\partial W}{\partial \boldsymbol{F}} \qquad \text{or} \qquad S_{IJ} = F^{-1}_{Ik}\frac{\partial W}{\partial F_{kJ}} ~.
</math>
In terms of the [[Finite_strain_theory#Finite_strain_tensors|Lagrangian Green strain]]
:<math>
  \boldsymbol{S} = \frac{\partial W}{\partial \boldsymbol{E}} \qquad \text{or} \qquad
  S_{IJ} = \frac{\partial W}{\partial E_{IJ}} ~.
</math>
In terms of the [[finite strain theory|right Cauchy–Green deformation tensor]]
:<math>
  \boldsymbol{S} = 2~\frac{\partial W}{\partial \boldsymbol{C}} \qquad \text{or} \qquad
  S_{IJ} = 2~\frac{\partial W}{\partial C_{IJ}} ~.
</math>
The above relation is also known as the '''Doyle-Ericksen formula''' in the material configuration.
 
==== Cauchy stress ====
Similarly, the [[stress (physics)|Cauchy stress]] is given by
:<math>
  \boldsymbol{\sigma} = \cfrac{1}{J}~ \cfrac{\partial W}{\partial \boldsymbol{F}}\cdot\boldsymbol{F}^T ~;~~ J := \det\boldsymbol{F} \qquad \text{or} \qquad
  \sigma_{ij} = \cfrac{1}{J}~ \cfrac{\partial W}{\partial F_{iK}}~F_{jK} ~.
</math>
In terms of the [[Finite_strain_theory#Finite_strain_tensors|Lagrangian Green strain]]
:<math>
  \boldsymbol{\sigma} = \cfrac{1}{J}~\boldsymbol{F}\cdot\cfrac{\partial W}{\partial \boldsymbol{E}}\cdot\boldsymbol{F}^T  \qquad \text{or} \qquad
  \sigma_{ij} = \cfrac{1}{J}~F_{iK}~\cfrac{\partial W}{\partial E_{KL}}~F_{jL} ~.
</math>
In terms of the [[finite strain theory|right Cauchy–Green deformation tensor]]
:<math>
  \boldsymbol{\sigma} = \cfrac{2}{J}~\boldsymbol{F}\cdot\cfrac{\partial W}{\partial \boldsymbol{C}}\cdot\boldsymbol{F}^T  \qquad \text{or} \qquad
  \sigma_{ij} = \cfrac{2}{J}~F_{iK}~\cfrac{\partial W}{\partial C_{KL}}~F_{jL} ~.
</math>
The above expression can also be expressed in terms of the ''left'' Cauchy-Green deformation tensor.  In that case <ref name=Basar>Y. Basar, 2000, Nonlinear continuum mechanics of solids, Springer, p. 157.</ref>
:<math>
  \boldsymbol{\sigma} = \cfrac{2}{J}~\boldsymbol{B}\cdot\cfrac{\partial W}{\partial \boldsymbol{B}}  \qquad \text{or} \qquad
  \sigma_{ij} = \cfrac{2}{J}~B_{ik}~\cfrac{\partial W}{\partial B_{kj}} ~.
</math>
 
=== Incompressible hyperelastic materials ===
For an [[incompressible]] material <math>J := \det\boldsymbol{F} = 1</math>.  The incompressibility constraint is therefore <math>J-1= 0</math>.  To ensure incompressibility of a hyperelastic material, the strain-energy function can be written in form:
:<math>
W = W(\boldsymbol{F}) - p~(J-1)
</math>
where the hydrostatic pressure <math>p</math> functions as a [[Lagrange multipliers|Lagrangian multiplier]] to enforce the incompressibility constraint. The 1st Piola–Kirchhoff stress now becomes
:<math>
\boldsymbol{P}=-p~\boldsymbol{F}^{-T}+\frac{\partial W}{\partial \boldsymbol{F}}
  = -p~\boldsymbol{F}^{-T} + \boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{E}}
  = -p~\boldsymbol{F}^{-T} + 2~\boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{C}} ~.
</math>
This stress tensor can subsequently be [[stress (physics)|converted]] into any of the other conventional stress tensors, such as the [[Cauchy stress tensor|Cauchy Stress tensor]] which is given by
:<math>
\boldsymbol{\sigma}=\boldsymbol{P}\cdot\boldsymbol{F}^T=
  -p~\boldsymbol{\mathit{1}} + \frac{\partial W}{\partial \boldsymbol{F}}\cdot\boldsymbol{F}^T
  = -p~\boldsymbol{\mathit{1}} + \boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{E}}\cdot\boldsymbol{F}^T
  = -p~\boldsymbol{\mathit{1}} + 2~\boldsymbol{F}\cdot\frac{\partial W}{\partial \boldsymbol{C}}\cdot\boldsymbol{F}^T ~.
</math>
 
== Expressions for the Cauchy stress ==
 
=== Compressible isotropic hyperelastic materials ===
For [[isotropic]] hyperelastic materials, the Cauchy stress can be expressed in terms of the invariants of the [[Finite strain theory#The_Left_Cauchy–Green_deformation_tensor|left Cauchy–Green deformation tensor]] (or [[Finite strain theory#The_Right_Cauchy-Green_deformation_tensor|right Cauchy–Green deformation tensor]]).  If the [[strain energy density function]] is <math>W(\boldsymbol{F})=\hat{W}(I_1,I_2,I_3) = \bar{W}(\bar{I}_1,\bar{I}_2,J) = \tilde{W}(\lambda_1,\lambda_2,\lambda_3)</math>, then
:<math>
  \begin{align}
  \boldsymbol{\sigma} & =
    \cfrac{2}{\sqrt{I_3}}\left[\left(\cfrac{\partial\hat{W}}{\partial I_1} + I_1~\cfrac{\partial\hat{W}}{\partial I_2}\right)\boldsymbol{B} - \cfrac{\partial\hat{W}}{\partial I_2}~\boldsymbol{B} \cdot\boldsymbol{B} \right] + 2\sqrt{I_3}~\cfrac{\partial\hat{W}}{\partial I_3}~\boldsymbol{\mathit{1}} \\
  & = \cfrac{2}{J}\left[\cfrac{1}{J^{2/3}}\left(\cfrac{\partial\bar{W}}{\partial \bar{I}_1} + \bar{I}_1~\cfrac{\partial\bar{W}}{\partial \bar{I}_2}\right)\boldsymbol{B} -
\cfrac{1}{J^{4/3}}~\cfrac{\partial\bar{W}}{\partial \bar{I}_2}~\boldsymbol{B} \cdot\boldsymbol{B} \right] \\
  & \qquad \qquad + \left[\cfrac{\partial\bar{W}}{\partial J} - \cfrac{2}{3J}\left(\bar{I}_1~\cfrac{\partial\bar{W}}{\partial \bar{I}_1} + 2~\bar{I}_2~\cfrac{\partial\bar{W}}{\partial \bar{I}_2}\right)\right] ~\boldsymbol{\mathit{1}} \\
  & = \cfrac{2}{J}\left[\left(\cfrac{\partial\bar{W}}{\partial \bar{I}_1} + \bar{I}_1~\cfrac{\partial\bar{W}}{\partial \bar{I}_2}\right)\bar{\boldsymbol{B}} -
\cfrac{\partial\bar{W}}{\partial \bar{I}_2}~\bar{\boldsymbol{B}} \cdot\bar{\boldsymbol{B}} \right] + \left[\cfrac{\partial\bar{W}}{\partial J} - \cfrac{2}{3J}\left(\bar{I}_1~\cfrac{\partial\bar{W}}{\partial \bar{I}_1} + 2~\bar{I}_2~\cfrac{\partial\bar{W}}{\partial \bar{I}_2}\right)\right] ~\boldsymbol{\mathit{1}} \\
  & = \cfrac{\lambda_1}{\lambda_1\lambda_2\lambda_3}~\cfrac{\partial\tilde{W}}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 + \cfrac{\lambda_2}{\lambda_1\lambda_2\lambda_3}~\cfrac{\partial\tilde{W}}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 + \cfrac{\lambda_3}{\lambda_1\lambda_2\lambda_3}~\cfrac{\partial\tilde{W}}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3
  \end{align}
</math>
(See the page on [[Finite strain theory#The_Left_Cauchy–Green_deformation_tensor|the left Cauchy–Green deformation tensor]] for the definitions of these symbols).
 
:{| class="toccolours collapsible collapsed" width="80%" style="text-align:left"
!Proof 1:
|-
The [[stress (physics)|second Piola–Kirchhoff stress tensor]] for a hyperelastic material is given by
:<math>
  \boldsymbol{S} = 2~\cfrac{\partial W}{\partial \boldsymbol{C}}
</math>
where <math>\boldsymbol{C} = \boldsymbol{F}^T\cdot\boldsymbol{F}</math> is the [[finite strain theory|right Cauchy–Green deformation tensor]] and <math>\boldsymbol{F}</math> is the [[finite strain theory|deformation gradient]].  The [[stress (physics)|Cauchy stress]] is given by
:<math>
  \boldsymbol{\sigma} = \cfrac{1}{J}~\boldsymbol{F}\cdot\boldsymbol{S}\cdot\boldsymbol{F}^T
    = \cfrac{2}{J}~\boldsymbol{F}\cdot\cfrac{\partial W}{\partial \boldsymbol{C}}\cdot\boldsymbol{F}^T
</math>
where <math>J = \det\boldsymbol{F}</math>.  Let <math>I_1, I_2, I_3</math> be the three principal invariants of <math>\boldsymbol{C}</math>.  Then
:<math>
  \cfrac{\partial W}{\partial \boldsymbol{C}} =
    \cfrac{\partial W}{\partial I_1}~\cfrac{\partial I_1}{\partial \boldsymbol{C}} +
    \cfrac{\partial W}{\partial I_2}~\cfrac{\partial I_2}{\partial \boldsymbol{C}} +
    \cfrac{\partial W}{\partial I_3}~\cfrac{\partial I_3}{\partial \boldsymbol{C}} ~.
</math>
The [[tensor derivative (continuum mechanics)|derivatives of the invariants]] of the symmetric tensor <math>\boldsymbol{C}</math> are
:<math>
    \frac{\partial I_1}{\partial \boldsymbol{C}} = \boldsymbol{\mathit{1}} ~;~~
    \frac{\partial I_2}{\partial \boldsymbol{C}} = I_1~\boldsymbol{\mathit{1}} - \boldsymbol{C} ~;~~
    \frac{\partial I_3}{\partial \boldsymbol{C}} = \det(\boldsymbol{C})~\boldsymbol{C}^{-1} 
</math>
Therefore we can write
:<math>
  \cfrac{\partial W}{\partial \boldsymbol{C}} =
    \cfrac{\partial W}{\partial I_1}~\boldsymbol{\mathit{1}} +
    \cfrac{\partial W}{\partial I_2}~(I_1~\boldsymbol{\mathit{1}} - \boldsymbol{F}^T\cdot\boldsymbol{F}) +
    \cfrac{\partial W}{\partial I_3}~I_3~\boldsymbol{F}^{-1}\cdot\boldsymbol{F}^{-T} ~.
</math>
Plugging into the expression for the Cauchy stress gives
:<math>
  \boldsymbol{\sigma}
    = \cfrac{2}{J}~\left[\cfrac{\partial W}{\partial I_1}~\boldsymbol{F}\cdot\boldsymbol{F}^T+
        \cfrac{\partial W}{\partial I_2}~(I_1~\boldsymbol{F}\cdot\boldsymbol{F}^T - \boldsymbol{F}\cdot\boldsymbol{F}^T\cdot\boldsymbol{F}\cdot\boldsymbol{F}^T) +
\cfrac{\partial W}{\partial I_3}~I_3~\boldsymbol{\mathit{1}}\right]
</math>
Using the [[Finite strain theory#The_Left_Cauchy–Green_deformation_tensor|left Cauchy–Green deformation tensor]] <math>\boldsymbol{B}=\boldsymbol{F}\cdot\boldsymbol{F}^T</math> and noting that <math>I_3 = J^2</math>, we can write
:<math>
  \boldsymbol{\sigma}
    = \cfrac{2}{\sqrt{I_3}}~\left[\left(\cfrac{\partial W}{\partial I_1} +
          I_1~\cfrac{\partial W}{\partial I_2}\right)~\boldsymbol{B} -
        \cfrac{\partial W}{\partial I_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right] +
        2~\sqrt{I_3}~\cfrac{\partial W}{\partial I_3}~\boldsymbol{\mathit{1}}~.
</math>
For an [[incompressible]] material <math>I_3 = 1</math> and hence <math>W = W(I_1,I_2)</math>.Then
:<math>
  \cfrac{\partial W}{\partial \boldsymbol{C}} =
    \cfrac{\partial W}{\partial I_1}~\cfrac{\partial I_1}{\partial \boldsymbol{C}} +
    \cfrac{\partial W}{\partial I_2}~\cfrac{\partial I_2}{\partial \boldsymbol{C}}
    = \cfrac{\partial W}{\partial I_1}~\boldsymbol{\mathit{1}} +
    \cfrac{\partial W}{\partial I_2}~(I_1~\boldsymbol{\mathit{1}} - \boldsymbol{F}^T\cdot\boldsymbol{F})
</math>
Therefore the Cauchy stress is given by
:<math>
  \boldsymbol{\sigma}
    = 2\left[\left(\cfrac{\partial W}{\partial I_1} +
          I_1~\cfrac{\partial W}{\partial I_2}\right)~\boldsymbol{B} -
        \cfrac{\partial W}{\partial I_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right] - p~\boldsymbol{\mathit{1}}~.
</math>
where <math>p</math> is an undetermined pressure which acts as a [[Lagrange multiplier]] to enforce the incompressibility constraint.
 
If, in addition, <math>I_1 = I_2</math>, we have <math> W = W(I_1) </math> and hence
:<math>
  \cfrac{\partial W}{\partial \boldsymbol{C}} =
    \cfrac{\partial W}{\partial I_1}~\cfrac{\partial I_1}{\partial \boldsymbol{C}} = \cfrac{\partial W}{\partial I_1}~\boldsymbol{\mathit{1}}
</math>
In that case the Cauchy stress can be expressed as
:<math>
  \boldsymbol{\sigma} = 2\cfrac{\partial W}{\partial I_1}~\boldsymbol{B} - p~\boldsymbol{\mathit{1}}~.
</math>
|}
 
:{| class="toccolours collapsible collapsed" width="80%" style="text-align:left"
!Proof 2:
|-
|The [[isochoric]] deformation gradient is defined as <math>\bar{\boldsymbol{F}}:=J^{-1/3}\boldsymbol{F}</math>, resulting in the isochoric deformation gradient having a determinant of 1, in other words it is volume stretch free. Using this one can subsequently define the isochoric left Cauchy–Green deformation tensor tensor <math>\bar{\boldsymbol{B}} := \bar{\boldsymbol{F}}\cdot\bar{\boldsymbol{F}}^T=J^{-2/3}\boldsymbol{B}</math>.
The invariants of <math>\bar{\boldsymbol{B}}</math> are
<math>
  \begin{align}
    \bar I_1 &= \text{tr}(\bar{\boldsymbol{B}}) = J^{-2/3}\text{tr}(\boldsymbol{B}) = J^{-2/3} I_1 \\
    \bar I_2 & = \frac{1}{2}\left(\text{tr}(\bar{\boldsymbol{B}})^2 - \text{tr}(\bar{\boldsymbol{B}}^2)\right) =
\frac{1}{2}\left( \left(J^{-2/3}\text{tr}(\boldsymbol{B})\right)^2 - \text{tr}(J^{-4/3}\boldsymbol{B}^2) \right) =
J^{-4/3} I_2 \\
    \bar I_3 &= \det(\bar{\boldsymbol{B}}) = J^{-6/3} \det(\boldsymbol{B}) = J^{-2} I_3 = J^{-2} J^2 = 1
  \end{align}
</math>
The set of invariants which are used to define the distortional behavior are the first two invariants of the isochoric left Cauchy–Green deformation tensor tensor, (which are identical to the ones for the right Cauchy Green stretch tensor), and add <math>J</math> into the fray to describe the volumetric behaviour.
 
To express the Cauchy stress in terms of the invariants <math>\bar{I}_1, \bar{I}_2, J</math> recall that
:<math>
  \bar{I}_1 = J^{-2/3}~I_1 = I_3^{-1/3}~I_1 ~;~~
  \bar{I}_2 = J^{-4/3}~I_2 = I_3^{-2/3}~I_2 ~;~~ J = I_3^{1/2} ~.
</math>
The chain rule of differentiation gives us
:<math>
  \begin{align}
  \cfrac{\partial W}{\partial I_1} & =
    \cfrac{\partial W}{\partial \bar{I}_1}~\cfrac{\partial \bar{I}_1}{\partial I_1} +
    \cfrac{\partial W}{\partial \bar{I}_2}~\cfrac{\partial \bar{I}_2}{\partial I_1} +
    \cfrac{\partial W}{\partial J}~\cfrac{\partial J}{\partial I_1} \\
    & = I_3^{-1/3}~\cfrac{\partial W}{\partial \bar{I}_1}
      = J^{-2/3}~\cfrac{\partial W}{\partial \bar{I}_1} \\
  \cfrac{\partial W}{\partial I_2} & =
    \cfrac{\partial W}{\partial \bar{I}_1}~\cfrac{\partial \bar{I}_1}{\partial I_2} +
    \cfrac{\partial W}{\partial \bar{I}_2}~\cfrac{\partial \bar{I}_2}{\partial I_2} +
    \cfrac{\partial W}{\partial J}~\cfrac{\partial J}{\partial I_2} \\
    & = I_3^{-2/3}~\cfrac{\partial W}{\partial \bar{I}_2}
      = J^{-4/3}~\cfrac{\partial W}{\partial \bar{I}_2} \\
  \cfrac{\partial W}{\partial I_3} & =
    \cfrac{\partial W}{\partial \bar{I}_1}~\cfrac{\partial \bar{I}_1}{\partial I_3} +
    \cfrac{\partial W}{\partial \bar{I}_2}~\cfrac{\partial \bar{I}_2}{\partial I_3} +
    \cfrac{\partial W}{\partial J}~\cfrac{\partial J}{\partial I_3} \\
    & = - \cfrac{1}{3}~I_3^{-4/3}~I_1~\cfrac{\partial W}{\partial \bar{I}_1}
      - \cfrac{2}{3}~I_3^{-5/3}~I_2~\cfrac{\partial W}{\partial \bar{I}_2}
      + \cfrac{1}{2}~I_3^{-1/2}~\cfrac{\partial W}{\partial J}  \\
    & = - \cfrac{1}{3}~J^{-8/3}~J^{2/3}~\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_1}
      - \cfrac{2}{3}~J^{-10/3}~J^{4/3}~\bar{I}_2~\cfrac{\partial W}{\partial \bar{I}_2}
      + \cfrac{1}{2}~J^{-1}~\cfrac{\partial W}{\partial J}  \\
    & = -\cfrac{1}{3}~J^{-2}~\left(\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_1}+
      2~\bar{I}_2~\cfrac{\partial W}{\partial \bar{I}_2}\right) +
      \cfrac{1}{2}~J^{-1}~\cfrac{\partial W}{\partial J}
  \end{align}
</math>
Recall that the Cauchy stress is given by
:<math>
  \boldsymbol{\sigma}
    = \cfrac{2}{\sqrt{I_3}}~\left[\left(\cfrac{\partial W}{\partial I_1} +
          I_1~\cfrac{\partial W}{\partial I_2}\right)~\boldsymbol{B} -
        \cfrac{\partial W}{\partial I_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right] +
        2~\sqrt{I_3}~\cfrac{\partial W}{\partial I_3}~\boldsymbol{\mathit{1}}~.
</math>
In terms of the invariants <math>\bar{I}_1, \bar{I}_2, J</math> we have
:<math>
  \boldsymbol{\sigma}
    = \cfrac{2}{J}~\left[\left(\cfrac{\partial W}{\partial I_1}+
          J^{2/3}~\bar{I}_1~\cfrac{\partial W}{\partial I_2}\right)~\boldsymbol{B} -
        \cfrac{\partial W}{\partial I_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right] +
        2~J~\cfrac{\partial W}{\partial I_3}~\boldsymbol{\mathit{1}}~.
</math>
Plugging in the expressions for the derivatives of <math>W</math> in terms of <math>\bar{I}_1, \bar{I}_2, J</math>, we have
:<math>
  \begin{align}
  \boldsymbol{\sigma}
    & = \cfrac{2}{J}~\left[\left(J^{-2/3}~\cfrac{\partial W}{\partial \bar{I}_1} +
          J^{-2/3}~\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_2}\right)~\boldsymbol{B} -
        J^{-4/3}~\cfrac{\partial W}{\partial \bar{I}_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right]
        + \\
    & \qquad
      2~J~\left[-\cfrac{1}{3}~J^{-2}~\left(\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_1}+
      2~\bar{I}_2~\cfrac{\partial W}{\partial \bar{I}_2}\right) +
      \cfrac{1}{2}~J^{-1}~\cfrac{\partial W}{\partial J}\right]~\boldsymbol{\mathit{1}}
  \end{align}
</math>
or,
:<math>
  \begin{align}
  \boldsymbol{\sigma}
    & = \cfrac{2}{J}~\left[\cfrac{1}{J^{2/3}}~\left(\cfrac{\partial W}{\partial \bar{I}_1} +
          \bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_2}\right)~\boldsymbol{B} -
          \cfrac{1}{J^{4/3}}~
        \cfrac{\partial W}{\partial \bar{I}_2}~\boldsymbol{B}\cdot\boldsymbol{B}\right] \\
    & \qquad + \left[\cfrac{\partial W}{\partial J} -
          \cfrac{2}{3J}\left(\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_1}+
                            2~\bar{I}_2~\cfrac{\partial W}{\partial \bar{I}_2}\right)\right]\boldsymbol{\mathit{1}}
  \end{align}
</math>
In terms of the deviatoric part of <math>\boldsymbol{B}</math>, we can write
:<math>
  \begin{align}
  \boldsymbol{\sigma}
    & = \cfrac{2}{J}~\left[\left(\cfrac{\partial W}{\partial \bar{I}_1} +
          \bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_2}\right)~\bar{\boldsymbol{B}} -
        \cfrac{\partial W}{\partial \bar{I}_2}~\bar{\boldsymbol{B}}\cdot\bar{\boldsymbol{B}}\right] \\
    & \qquad + \left[\cfrac{\partial W}{\partial J} -
          \cfrac{2}{3J}\left(\bar{I}_1~\cfrac{\partial W}{\partial \bar{I}_1}+
                            2~\bar{I}_2~\cfrac{\partial W}{\partial \bar{I}_2}\right)\right]\boldsymbol{\mathit{1}}
  \end{align}
</math>
For an [[incompressible]] material <math>J = 1</math> and hence <math>W = W(\bar{I}_1,\bar{I}_2)</math>.Then
the Cauchy stress is given by
:<math>
  \boldsymbol{\sigma}
    = 2\left[\left(\cfrac{\partial W}{\partial \bar{I}_1} +
          I_1~\cfrac{\partial W}{\partial \bar{I}_2}\right)~\bar{\boldsymbol{B}} -
        \cfrac{\partial W}{\partial \bar{I}_2}~\bar{\boldsymbol{B}}\cdot\bar{\boldsymbol{B}}\right] - p~\boldsymbol{\mathit{1}}~.
</math>
where <math>p</math> is an undetermined pressure-like Lagrange multiplier term.  In addition, if <math>\bar{I}_1 = \bar{I}_2</math>, we have <math> W = W(\bar{I}_1) </math> and hence
the Cauchy stress can be expressed as
:<math>
  \boldsymbol{\sigma} = 2\cfrac{\partial W}{\partial \bar{I}_1}~\bar{\boldsymbol{B}} - p~\boldsymbol{\mathit{1}}~.
</math>
|}
 
:{| class="toccolours collapsible collapsed" width="80%" style="text-align:left"
!Proof 3:
|-
|  To express the Cauchy stress in terms of the [[finite strain theory|stretches]] <math>\lambda_1, \lambda_2, \lambda_3</math> recall that
:<math>
  \cfrac{\partial \lambda_i}{\partial\boldsymbol{C}} = \cfrac{1}{2\lambda_i}~\boldsymbol{R}^T\cdot(\mathbf{n}_i\otimes\mathbf{n}_i)\cdot\boldsymbol{R}~;~~
i = 1,2,3 ~.
</math>
The chain rule gives
:<math>
  \begin{align}
  \cfrac{\partial W}{\partial\boldsymbol{C}} & =
  \cfrac{\partial W}{\partial \lambda_1}~\cfrac{\partial \lambda_1}{\partial\boldsymbol{C}} +
  \cfrac{\partial W}{\partial \lambda_2}~\cfrac{\partial \lambda_2}{\partial\boldsymbol{C}} +
  \cfrac{\partial W}{\partial \lambda_3}~\cfrac{\partial \lambda_3}{\partial\boldsymbol{C}} \\
  & = \boldsymbol{R}^T\cdot\left[\cfrac{1}{2\lambda_1}~\cfrac{\partial W}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 +
  \cfrac{1}{2\lambda_2}~\cfrac{\partial W}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 +
  \cfrac{1}{2\lambda_3}~\cfrac{\partial W}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3\right]\cdot\boldsymbol{R}
  \end{align}
</math>
The Cauchy stress is given by
:<math>
  \boldsymbol{\sigma} = \cfrac{2}{J}~\boldsymbol{F}\cdot
      \cfrac{\partial W}{\partial \boldsymbol{C}}\cdot\boldsymbol{F}^T =
      \cfrac{2}{J}~(\boldsymbol{V}\cdot\boldsymbol{R})\cdot
      \cfrac{\partial W}{\partial \boldsymbol{C}}\cdot(\boldsymbol{R}^T\cdot\boldsymbol{V})
</math>
Plugging in the expression for the derivative of <math>W</math> leads to
:<math>
  \boldsymbol{\sigma} =
      \cfrac{2}{J}~\boldsymbol{V}\cdot
        \left[\cfrac{1}{2\lambda_1}~
                \cfrac{\partial W}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 +
              \cfrac{1}{2\lambda_2}~
                \cfrac{\partial W}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 +
              \cfrac{1}{2\lambda_3}~
                \cfrac{\partial W}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3\right]
    \cdot\boldsymbol{V}
</math>
Using the [[finite strain theory|spectral decomposition]] of <math>\boldsymbol{V}</math> we have
:<math>
  \boldsymbol{V}\cdot(\mathbf{n}_i\otimes\mathbf{n}_i)\cdot\boldsymbol{V} =
    \lambda_i^2~\mathbf{n}_i\otimes\mathbf{n}_i ~;~~ i=1,2,3.
</math>
Also note that
:<math>
  J = \det(\boldsymbol{F}) = \det(\boldsymbol{V})\det(\boldsymbol{R}) = \det(\boldsymbol{V}) = \lambda_1\lambda_2\lambda_3 ~.
</math>
Therefore the expression for the Cauchy stress can be written as
:<math>
  \boldsymbol{\sigma} =
      \cfrac{1}{\lambda_1\lambda_2\lambda_3}~
        \left[\lambda_1~\cfrac{\partial W}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 +
              \lambda_2~\cfrac{\partial W}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 +
              \lambda_3~\cfrac{\partial W}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3
              \right]
</math>
For an [[incompressible]] material <math>\lambda_1\lambda_2\lambda_3 = 1</math> and hence <math>W = W(\lambda_1,\lambda_2)</math>.  Following Ogden<ref name=Ogden/> p.&nbsp;485,  we may write
:<math>
  \boldsymbol{\sigma} =
      \lambda_1~\cfrac{\partial W}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 +
              \lambda_2~\cfrac{\partial W}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 +
              \lambda_3~\cfrac{\partial W}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3
              - p~\boldsymbol{\mathit{1}}~
</math>
Some care is to required at this stage because, when an eigenvalue is repeated, it is in general only [[Gâteaux derivative|Gâteaux differentiable]], but not [[Fréchet differentiable]].<ref>Fox & Kapoor, ''Rates of change of eigenvalues and eigenvectors'', '''AIAA Journal''', 6 (12) 2426–2429 (1968)</ref><ref>Friswell MI. ''The derivatives of repeated eigenvalues and their associated eigenvectors.'' '''Journal of Vibration and Acoustics'''  (ASME) 1996; 118:390–397.</ref>  A rigorous [[tensor derivative (continuum mechanics)|tensor derivative]] can only be found by solving another eigenvalue problem.
 
If we express the stress in terms of differences between components,
:<math>
  \sigma_{11} - \sigma_{33} = \lambda_1~\cfrac{\partial W}{\partial \lambda_1} - \lambda_3~\cfrac{\partial W}{\partial \lambda_3} ~;~~
  \sigma_{22} - \sigma_{33} = \lambda_2~\cfrac{\partial W}{\partial \lambda_2} - \lambda_3~\cfrac{\partial W}{\partial \lambda_3}
</math>
If in addition to incompressibility we have <math>\lambda_1 = \lambda_2</math> then a possible solution to the problem
requires <math>\sigma_{11} = \sigma_{22}</math> and we can write the stress differences as
:<math>
  \sigma_{11} - \sigma_{33} = \sigma_{22} - \sigma_{33} = \lambda_1~\cfrac{\partial W}{\partial \lambda_1} - \lambda_3~\cfrac{\partial W}{\partial \lambda_3}
</math>
|}
 
=== Incompressible isotropic hyperelastic materials ===
For incompressible [[isotropic]] hyperelastic materials, the [[strain energy density function]] is <math>W(\boldsymbol{F})=\hat{W}(I_1,I_2)</math>.  The Cauchy stress is then given by
:<math>
  \begin{align}
  \boldsymbol{\sigma}  & = -p~\boldsymbol{\mathit{1}} +
    2\left[\left(\cfrac{\partial\hat{W}}{\partial I_1} + I_1~\cfrac{\partial\hat{W}}{\partial I_2}\right)\boldsymbol{B} - \cfrac{\partial\hat{W}}{\partial I_2}~\boldsymbol{B} \cdot\boldsymbol{B} \right] \\
    & = - p~\boldsymbol{\mathit{1}} + 2\left[\left(\cfrac{\partial W}{\partial \bar{I}_1} +
          I_1~\cfrac{\partial W}{\partial \bar{I}_2}\right)~\bar{\boldsymbol{B}} -
        \cfrac{\partial W}{\partial \bar{I}_2}~\bar{\boldsymbol{B}}\cdot\bar{\boldsymbol{B}}\right]  \\
    & = - p~\boldsymbol{\mathit{1}} + \lambda_1~\cfrac{\partial W}{\partial \lambda_1}~\mathbf{n}_1\otimes\mathbf{n}_1 +
              \lambda_2~\cfrac{\partial W}{\partial \lambda_2}~\mathbf{n}_2\otimes\mathbf{n}_2 + \lambda_3~\cfrac{\partial W}{\partial \lambda_3}~\mathbf{n}_3\otimes\mathbf{n}_3
             
  \end{align}
</math>
where <math>p</math> is an undetermined pressure. In terms of stress differences
:<math>
  \sigma_{11} - \sigma_{33} = \lambda_1~\cfrac{\partial W}{\partial \lambda_1} - \lambda_3~\cfrac{\partial W}{\partial \lambda_3}~;~~
  \sigma_{22} - \sigma_{33} = \lambda_2~\cfrac{\partial W}{\partial \lambda_2} - \lambda_3~\cfrac{\partial W}{\partial \lambda_3}
</math>
If in addition <math>I_1 = I_2</math>, then
:<math>
  \boldsymbol{\sigma} = 2\cfrac{\partial W}{\partial I_1}~\boldsymbol{B} - p~\boldsymbol{\mathit{1}}~.
</math>
If <math>\lambda_1 = \lambda_2</math>, then
:<math>
  \sigma_{11} - \sigma_{33} = \sigma_{22} - \sigma_{33} = \lambda_1~\cfrac{\partial W}{\partial \lambda_1} -  \lambda_3~\cfrac{\partial W}{\partial \lambda_3}
</math>
 
== Consistency with linear elasticity ==
Consistency with linear elasticity is often used to determine some of the parameters of hyperelastic material models.  These consistency conditions can be found by comparing [[Hooke's law]] with linearized hyperelasticity at small strains.
 
=== Consistency conditions for isotropic hyperelastic models ===
For isotropic hyperelastic materials to be consistent with isotropic [[linear elasticity]], the stress-strain relation should have the following form in the [[infinitesimal strain theory|infinitesimal strain]] limit:
:<math>
  \boldsymbol{\sigma} = \lambda~\mathrm{tr}(\boldsymbol{\varepsilon})~\boldsymbol{\mathit{1}} + 2\mu\boldsymbol{\varepsilon}
</math>
where <math>\lambda, \mu</math> are the [[Lame constants]]. The strain energy density function that corresponds to the above relation is<ref name=Ogden/>
:<math>
  W = \tfrac{1}{2}\lambda~[\mathrm{tr}(\boldsymbol{\varepsilon})]^2 + \mu~\mathrm{tr}(\boldsymbol{\varepsilon}^2)
</math>
For an incompressible material <math>\mathrm{tr}(\boldsymbol{\varepsilon}) = 0</math> and we have
:<math>
  W = \mu~\mathrm{tr}(\boldsymbol{\varepsilon}^2)
</math>
For any strain energy density function <math>W(\lambda_1,\lambda_2,\lambda_3)</math> to reduce to the above forms for small strains the following conditions have to be met<ref name=Ogden/>
:<math>
  \begin{align}
      & W(1,1,1) = 0 ~;~~
      \cfrac{\partial W}{\partial \lambda_i}(1,1,1) = 0 \\
      & \cfrac{\partial^2 W}{\partial \lambda_i \partial \lambda_j}(1,1,1) = \lambda + 2\mu\delta_{ij}
  \end{align}
</math>
 
If the material is '''incompressible''' then the above conditions may be expressed in the following form.
: <math>
  \begin{align}
      & W(1,1,1) = 0 \\
      & \cfrac{\partial W}{\partial \lambda_i}(1,1,1) =  \cfrac{\partial W}{\partial \lambda_j}(1,1,1) ~;~~
        \cfrac{\partial^2 W}{\partial \lambda_i^2}(1,1,1) = \cfrac{\partial^2 W}{\partial \lambda_j^2}(1,1,1) \\
      & \cfrac{\partial^2 W}{\partial \lambda_i \partial \lambda_j}(1,1,1) = \mathrm{independent of}~i,j\ne i \\
      & \cfrac{\partial^2 W}{\partial \lambda_i^2}(1,1,1) - \cfrac{\partial^2 W}{\partial \lambda_i \partial \lambda_j}(1,1,1) + \cfrac{\partial W}{\partial \lambda_i}(1,1,1) = 2\mu ~~(i \ne j)
  \end{align}
</math>
These conditions can be used to find relations between the parameters of a given hyperelastic model and shear and bulk moduli.
 
=== Consistency conditions for incompressible <math>I_1</math> based rubber materials ===
Many elastomers are modeled adequately by a strain energy density function that depends only on <math>I_1</math>.  For such materials we have <math> W = W(I_1) </math>. 
The consistency conditions for incompressible materials for <math>I_1 = 3, \lambda_i = \lambda_j = 1</math> may then be expressed as
:<math>
  W(I_1)\biggr|_{I_1=3} = 0 \quad \text{and} \quad \cfrac{\partial W}{\partial I_1}\biggr|_{I_1=3} = \frac{\mu}{2} \,.
</math>
The second consistency condition above can be derived by noting that
:<math>
  \cfrac{\partial W}{\partial \lambda_i} = \cfrac{\partial W}{\partial I_1}\cfrac{\partial I_1}{\partial \lambda_i} = 2\lambda_i\cfrac{\partial W}{\partial I_1} \quad\text{and}\quad
  \cfrac{\partial^2 W}{\partial \lambda_i \partial \lambda_j}  = 2\delta_{ij}\cfrac{\partial W}{\partial I_1} + 4\lambda_i\lambda_j \cfrac{\partial^2 W}{\partial I_1^2}\,.
</math>
The can then be substituted into the consistency condition for isotropic incompressible hyperelastic materials.
 
== References ==
 
<references/>
 
== See also ==
*[[Cauchy elastic material]]
*[[Continuum mechanics]]
*[[Deformation (mechanics)]]
*[[Finite strain theory]]
*[[Rubber elasticity]]
*[[Stress measures]]
*[[Stress (mechanics)]]
 
{{DEFAULTSORT:Hyperelastic Material}}
[[Category:Continuum mechanics]]
[[Category:Elasticity (physics)]]
[[Category:Rubber properties]]
[[Category:Solid mechanics]]

Revision as of 15:08, 14 August 2013

Template:Continuum mechanics

Stress-strain curves for various hyperelastic material models.

A hyperelastic or Green elastic material[1] is a type of constitutive model for ideally elastic material for which the stress-strain relationship derives from a strain energy density function. The hyperelastic material is a special case of a Cauchy elastic material.

For many materials, linear elastic models do not accurately describe the observed material behaviour. The most common example of this kind of material is rubber, whose stress-strain relationship can be defined as non-linearly elastic, isotropic, incompressible and generally independent of strain rate. Hyperelasticity provides a means of modeling the stress-strain behavior of such materials.[2] The behavior of unfilled, vulcanized elastomers often conforms closely to the hyperelastic ideal. Filled elastomers and biological tissues are also often modeled via the hyperelastic idealization.

Ronald Rivlin and Melvin Mooney developed the first hyperelastic models, the Neo-Hookean and Mooney–Rivlin solids. Many other hyperelastic models have since been developed. Other widely used hyperelastic material models include the Ogden model and the Arruda–Boyce model.

Hyperelastic material models

Saint Venant–Kirchhoff model

The simplest hyperelastic material model is the Saint Venant–Kirchhoff model which is just an extension of the linear elastic material model to the nonlinear regime. This model has the form

𝑺=λtr(𝑬)1+2μ𝑬

where 𝑺 is the second Piola–Kirchhoff stress and 𝑬 is the Lagrangian Green strain, and λ and μ are the Lamé constants.

The strain-energy density function for the St. Venant–Kirchhoff model is

W(𝑬)=λ2[tr(𝑬)]2+μtr(𝑬2)

and the second Piola–Kirchhoff stress can be derived from the relation

𝑺=W𝑬.

Classification of hyperelastic material models

Hyperelastic material models can be classified as:

1) phenomenological descriptions of observed behavior

2) mechanistic models deriving from arguments about underlying structure of the material

3) hybrids of phenomenological and mechanistic models

Generally, a hyperelastic model should satisfy the Drucker stability criterion.

Stress-strain relations

Compressible hyperelastic materials

First Piola–Kirchhoff stress

If W(𝑭) is the strain energy density function, the 1st Piola–Kirchhoff stress tensor can be calculated for a hyperelastic material as

𝑷=W𝑭orPiK=WFiK.

where 𝑭 is the deformation gradient. In terms of the Lagrangian Green strain (𝑬)

𝑷=𝑭W𝑬orPiK=FiLWELK.

In terms of the right Cauchy–Green deformation tensor (𝑪)

𝑷=2𝑭W𝑪orPiK=2FiLWCLK.

Second Piola–Kirchhoff stress

If 𝑺 is the second Piola–Kirchhoff stress tensor then

𝑺=𝑭1W𝑭orSIJ=FIk1WFkJ.

In terms of the Lagrangian Green strain

𝑺=W𝑬orSIJ=WEIJ.

In terms of the right Cauchy–Green deformation tensor

𝑺=2W𝑪orSIJ=2WCIJ.

The above relation is also known as the Doyle-Ericksen formula in the material configuration.

Cauchy stress

Similarly, the Cauchy stress is given by

𝝈=1JW𝑭𝑭T;J:=det𝑭orσij=1JWFiKFjK.

In terms of the Lagrangian Green strain

𝝈=1J𝑭W𝑬𝑭Torσij=1JFiKWEKLFjL.

In terms of the right Cauchy–Green deformation tensor

𝝈=2J𝑭W𝑪𝑭Torσij=2JFiKWCKLFjL.

The above expression can also be expressed in terms of the left Cauchy-Green deformation tensor. In that case [3]

𝝈=2J𝑩W𝑩orσij=2JBikWBkj.

Incompressible hyperelastic materials

For an incompressible material J:=det𝑭=1. The incompressibility constraint is therefore J1=0. To ensure incompressibility of a hyperelastic material, the strain-energy function can be written in form:

W=W(𝑭)p(J1)

where the hydrostatic pressure p functions as a Lagrangian multiplier to enforce the incompressibility constraint. The 1st Piola–Kirchhoff stress now becomes

𝑷=p𝑭T+W𝑭=p𝑭T+𝑭W𝑬=p𝑭T+2𝑭W𝑪.

This stress tensor can subsequently be converted into any of the other conventional stress tensors, such as the Cauchy Stress tensor which is given by

𝝈=𝑷𝑭T=p1+W𝑭𝑭T=p1+𝑭W𝑬𝑭T=p1+2𝑭W𝑪𝑭T.

Expressions for the Cauchy stress

Compressible isotropic hyperelastic materials

For isotropic hyperelastic materials, the Cauchy stress can be expressed in terms of the invariants of the left Cauchy–Green deformation tensor (or right Cauchy–Green deformation tensor). If the strain energy density function is W(𝑭)=Ŵ(I1,I2,I3)=W¯(I¯1,I¯2,J)=W~(λ1,λ2,λ3), then

𝝈=2I3[(ŴI1+I1ŴI2)𝑩ŴI2𝑩𝑩]+2I3ŴI31=2J[1J2/3(W¯I¯1+I¯1W¯I¯2)𝑩1J4/3W¯I¯2𝑩𝑩]+[W¯J23J(I¯1W¯I¯1+2I¯2W¯I¯2)]1=2J[(W¯I¯1+I¯1W¯I¯2)𝑩¯W¯I¯2𝑩¯𝑩¯]+[W¯J23J(I¯1W¯I¯1+2I¯2W¯I¯2)]1=λ1λ1λ2λ3W~λ1𝐧1𝐧1+λ2λ1λ2λ3W~λ2𝐧2𝐧2+λ3λ1λ2λ3W~λ3𝐧3𝐧3

(See the page on the left Cauchy–Green deformation tensor for the definitions of these symbols).

Incompressible isotropic hyperelastic materials

For incompressible isotropic hyperelastic materials, the strain energy density function is W(𝑭)=Ŵ(I1,I2). The Cauchy stress is then given by

𝝈=p1+2[(ŴI1+I1ŴI2)𝑩ŴI2𝑩𝑩]=p1+2[(WI¯1+I1WI¯2)𝑩¯WI¯2𝑩¯𝑩¯]=p1+λ1Wλ1𝐧1𝐧1+λ2Wλ2𝐧2𝐧2+λ3Wλ3𝐧3𝐧3

where p is an undetermined pressure. In terms of stress differences

σ11σ33=λ1Wλ1λ3Wλ3;σ22σ33=λ2Wλ2λ3Wλ3

If in addition I1=I2, then

𝝈=2WI1𝑩p1.

If λ1=λ2, then

σ11σ33=σ22σ33=λ1Wλ1λ3Wλ3

Consistency with linear elasticity

Consistency with linear elasticity is often used to determine some of the parameters of hyperelastic material models. These consistency conditions can be found by comparing Hooke's law with linearized hyperelasticity at small strains.

Consistency conditions for isotropic hyperelastic models

For isotropic hyperelastic materials to be consistent with isotropic linear elasticity, the stress-strain relation should have the following form in the infinitesimal strain limit:

𝝈=λtr(𝜺)1+2μ𝜺

where λ,μ are the Lame constants. The strain energy density function that corresponds to the above relation is[1]

W=12λ[tr(𝜺)]2+μtr(𝜺2)

For an incompressible material tr(𝜺)=0 and we have

W=μtr(𝜺2)

For any strain energy density function W(λ1,λ2,λ3) to reduce to the above forms for small strains the following conditions have to be met[1]

W(1,1,1)=0;Wλi(1,1,1)=02Wλiλj(1,1,1)=λ+2μδij

If the material is incompressible then the above conditions may be expressed in the following form.

W(1,1,1)=0Wλi(1,1,1)=Wλj(1,1,1);2Wλi2(1,1,1)=2Wλj2(1,1,1)2Wλiλj(1,1,1)=independentofi,ji2Wλi2(1,1,1)2Wλiλj(1,1,1)+Wλi(1,1,1)=2μ(ij)

These conditions can be used to find relations between the parameters of a given hyperelastic model and shear and bulk moduli.

Consistency conditions for incompressible I1 based rubber materials

Many elastomers are modeled adequately by a strain energy density function that depends only on I1. For such materials we have W=W(I1). The consistency conditions for incompressible materials for I1=3,λi=λj=1 may then be expressed as

W(I1)|I1=3=0andWI1|I1=3=μ2.

The second consistency condition above can be derived by noting that

Wλi=WI1I1λi=2λiWI1and2Wλiλj=2δijWI1+4λiλj2WI12.

The can then be substituted into the consistency condition for isotropic incompressible hyperelastic materials.

References

  1. 1.0 1.1 1.2 1.3 R.W. Ogden, 1984, Non-Linear Elastic Deformations, ISBN 0-486-69648-0, Dover.
  2. Muhr, A. H. (2005). Modeling the stress-strain behavior of rubber. Rubber chemistry and technology, 78(3), 391-425. [1]
  3. Y. Basar, 2000, Nonlinear continuum mechanics of solids, Springer, p. 157.
  4. Fox & Kapoor, Rates of change of eigenvalues and eigenvectors, AIAA Journal, 6 (12) 2426–2429 (1968)
  5. Friswell MI. The derivatives of repeated eigenvalues and their associated eigenvectors. Journal of Vibration and Acoustics (ASME) 1996; 118:390–397.

See also