How to derive plane strain bulk modulus?

AI Thread Summary
The discussion focuses on deriving the stress-strain relationship for a transversely isotropic material under specific conditions. It highlights the definition of the "plane strain bulk modulus," K23, and the corresponding stress and strain conditions. The user attempts to apply the stiffness matrix relationship but encounters difficulties, particularly with the implications of setting epsilon1 to zero. The conversation emphasizes the need to clarify how these conditions affect the stress components and the relationships among K23, E1, E2, G23, and Mu12. Ultimately, the problem illustrates the complexities involved in materials science when dealing with isotropic and anisotropic properties.
lou_skywalker
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This is a homework problem and I thought about putting it in the homework section bu since its very materials science specific I decided to put it here:

For a transversely isotropic material, the “plane strain bulk modulus”, K23, is an
engineering constant that is defined by the stress condition (sigma)2 =(sigma)3=(sigma)
and the strain conditions (epsilon)1=0, (epsilon)2=(epsilon)3=(epsilon)
Show that these conditions lead to the stress-strain relationship (sigma)=2*(epsilon)*K23, and find the relationship among K23, E1, E2, G23, Mu12 (poisson's ratio).

I tried using the relationship Epsilon= stiffness matrix x stress, plugging in all the given relationships (and sigma1 is zero because epsilon1 is zero) but just got stuck at
sigma=(epsilon)*E2/(1-Mu23)
 
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if epsilon 1 =0 then sigma 1 won't be 0 because if you limit the deformation you will hava a stress
 
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