Graduate Lame parameter mu = shear modulus derivation (rogue factor of 2)

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The discussion centers on the derivation of the shear modulus G being equal to the Lame parameter μ. The original poster correctly applies the linear, symmetric, isotropic stress-strain formula but mistakenly concludes that G equals 2μ. The key correction involves recognizing that the true shear strain is half of the engineering shear strain, which is crucial for tensor calculations. This adjustment leads to the correct relationship, μ = G. Understanding this distinction is essential for accurate material property analysis.
Twigg
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Hello,

I am trying and failing to derive that the shear modulus ##G## is equal to the Lame parameter ##\mu##. I start with the linear, symmetric, isotropic stress-strain formula: $$\sigma = \lambda \mathrm{tr}(\epsilon) \mathrm{I} + 2\mu \epsilon$$ I then substitute a simple (symmetric) shear strain: $$\epsilon = \epsilon_{xy} (\hat{x} \otimes \hat{y} + \hat{y} \otimes \hat{x} )$$ But then I end up with $$\sigma_{xy} = 2\mu \epsilon_{xy}$$ or equivalently $$G = 2\mu$$ What did I goof up?

Thanks!
 
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