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Constitutive relations for 3D elastic solid

Short answer

The 3D constitutive matrix for isotropic linear elasticity is [D] = (E/[(1+ν)(1-2ν)]) × a 6×6 matrix with diagonal entries (1-ν, 1-ν, 1-ν, (1-2ν)/2, (1-2ν)/2, (1-2ν)/2) and off-diagonal ν for normal stress components, relating {σ} = [D]{ε}.

Derive the constitutive relations for the 3D state of a solid (i.e. {σ}=[D]{ε}\{\sigma\} = [D]\{\varepsilon\} for an elastic isotropic material).

The constitutive relation links stress and strain. For a linear elastic isotropic material the stresses are related to strains by Hooke's law with two constants, EE and ν\nu.

Strains from stresses

By superposition of the effect of each normal stress (a stress σx\sigma_x gives εx=σx/E\varepsilon_x=\sigma_x/E and lateral strains −νσx/E-\nu\sigma_x/E):

εx=1E[σx−ν(σy+σz)]εy=1E[σy−ν(σx+σz)]εz=1E[σz−ν(σx+σy)]\begin{aligned} \varepsilon_x&=\frac{1}{E}[\sigma_x-\nu(\sigma_y+\sigma_z)]\\ \varepsilon_y&=\frac{1}{E}[\sigma_y-\nu(\sigma_x+\sigma_z)]\\ \varepsilon_z&=\frac{1}{E}[\sigma_z-\nu(\sigma_x+\sigma_y)] \end{aligned}

and shear strains γxy=τxyG, γyz=τyzG, γzx=τzxG\gamma_{xy}=\dfrac{\tau_{xy}}{G},\ \gamma_{yz}=\dfrac{\tau_{yz}}{G},\ \gamma_{zx}=\dfrac{\tau_{zx}}{G} with G=E2(1+ν)G=\dfrac{E}{2(1+\nu)}.

Stresses from strains

Add the three normal strain equations. With e=εx+εy+εze=\varepsilon_x+\varepsilon_y+\varepsilon_z and Θ=σx+σy+σz\Theta=\sigma_x+\sigma_y+\sigma_z:

e=1−2νEΘ ⇒ Θ=E1−2νee=\frac{1-2\nu}{E}\Theta\ \Rightarrow\ \Theta=\frac{E}{1-2\nu}e

Write the first equation as Eεx=(1+ν)σx−νΘE\varepsilon_x=(1+\nu)\sigma_x-\nu\Theta, so

σx=E1+νεx+ν1+νΘ=E1+νεx+νE(1+ν)(1−2ν)e\sigma_x=\frac{E}{1+\nu}\varepsilon_x+\frac{\nu}{1+\nu}\Theta=\frac{E}{1+\nu}\varepsilon_x+\frac{\nu E}{(1+\nu)(1-2\nu)}e

Substituting ee and collecting terms gives σx=E(1+ν)(1−2ν)[(1−ν)εx+νεy+νεz]\sigma_x=\dfrac{E}{(1+\nu)(1-2\nu)}[(1-\nu)\varepsilon_x+\nu\varepsilon_y+\nu\varepsilon_z], and similarly for σy,σz\sigma_y,\sigma_z.

Matrix form {σ}=[D]{ε}\{\sigma\}=[D]\{\varepsilon\}

{σxσyσzτxyτyzτzx}=E(1+ν)(1−2ν)[1−ννν000ν1−νν000νν1−ν0000001−2ν20000001−2ν20000001−2ν2]{εxεyεzγxyγyzγzx}\begin{Bmatrix}\sigma_x\\\sigma_y\\\sigma_z\\\tau_{xy}\\\tau_{yz}\\\tau_{zx}\end{Bmatrix}=\frac{E}{(1+\nu)(1-2\nu)}\begin{bmatrix}1-\nu&\nu&\nu&0&0&0\\\nu&1-\nu&\nu&0&0&0\\\nu&\nu&1-\nu&0&0&0\\0&0&0&\frac{1-2\nu}{2}&0&0\\0&0&0&0&\frac{1-2\nu}{2}&0\\0&0&0&0&0&\frac{1-2\nu}{2}\end{bmatrix}\begin{Bmatrix}\varepsilon_x\\\varepsilon_y\\\varepsilon_z\\\gamma_{xy}\\\gamma_{yz}\\\gamma_{zx}\end{Bmatrix}

The matrix [D][D] is symmetric. In terms of Lame's constants, σx=λe+2μεx\sigma_x=\lambda e+2\mu\varepsilon_x and τxy=μγxy\tau_{xy}=\mu\gamma_{xy} with λ=νE(1+ν)(1−2ν)\lambda=\dfrac{\nu E}{(1+\nu)(1-2\nu)}, μ=G\mu=G.

✓ Answer checked by Claude Opus 5.5 (high effort)

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