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Derive Lame's constants

Short answer

Lame's constants are λ = νE/[(1+ν)(1-2ν)] and μ = E/[2(1+ν)] = G. They appear in the stress-strain law σ_ij = λ e δ_ij + 2μ ε_ij, derived from Hooke's law by adding normal strains and solving for stresses.

Derive the expression for Lame's constants.

Lame's constants λ\lambda and μ\mu express the isotropic stress-strain law in the compact form

σij=λ e δij+2μ εij,e=εx+εy+εz\sigma_{ij}=\lambda\,e\,\delta_{ij}+2\mu\,\varepsilon_{ij},\qquad e=\varepsilon_x+\varepsilon_y+\varepsilon_z

that is, σx=λe+2μεx\sigma_x=\lambda e+2\mu\varepsilon_x, σy=λe+2μεy\sigma_y=\lambda e+2\mu\varepsilon_y, σz=λe+2μεz\sigma_z=\lambda e+2\mu\varepsilon_z, τxy=μγxy\tau_{xy}=\mu\gamma_{xy} etc.

Derivation

Hooke's law: εx=1E[(1+ν)σx−νΘ]\varepsilon_x=\dfrac{1}{E}[(1+\nu)\sigma_x-\nu\Theta], with Θ=σx+σy+σz\Theta=\sigma_x+\sigma_y+\sigma_z.

Adding the three normal equations: e=1−2νEΘe=\dfrac{1-2\nu}{E}\Theta, so Θ=E1−2νe\Theta=\dfrac{E}{1-2\nu}e.

Solve for σx\sigma_x:

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

Compare with σx=λe+2μεx\sigma_x=\lambda e+2\mu\varepsilon_x:

λ=νE(1+ν)(1−2ν),μ=E2(1+ν)=G\boxed{\lambda=\frac{\nu E}{(1+\nu)(1-2\nu)}},\qquad \boxed{\mu=\frac{E}{2(1+\nu)}=G}

For shear, τxy=Gγxy\tau_{xy}=G\gamma_{xy} with G=E2(1+ν)G=\dfrac{E}{2(1+\nu)}, which confirms μ=G\mu=G (the shear modulus).

Inverse relations: E=μ(3λ+2μ)λ+μE=\dfrac{\mu(3\lambda+2\mu)}{\lambda+\mu}, ν=λ2(λ+μ)\nu=\dfrac{\lambda}{2(\lambda+\mu)}. The bulk modulus is K=λ+23μK=\lambda+\tfrac23\mu.

✓ Answer checked by Claude Opus 5.5 (high effort)

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