How to derive plane strain bulk modulus?

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SUMMARY

The discussion focuses on deriving the plane strain bulk modulus, K23, for transversely isotropic materials. It establishes that under specific stress conditions (σ2 = σ3 = σ) and strain conditions (ε1 = 0, ε2 = ε3 = ε), the stress-strain relationship can be expressed as σ = 2 * ε * K23. Additionally, it explores the relationship among K23, E1, E2, G23, and μ12 (Poisson's ratio), emphasizing the importance of these parameters in materials science.

PREREQUISITES
  • Understanding of transversely isotropic materials
  • Familiarity with stress-strain relationships in materials science
  • Knowledge of stiffness matrices and their applications
  • Basic concepts of Poisson's ratio (μ12)
NEXT STEPS
  • Study the derivation of the stiffness matrix for transversely isotropic materials
  • Research the implications of Poisson's ratio (μ12) on material behavior
  • Explore the relationship between bulk modulus and Young's modulus (E1, E2)
  • Learn about the application of G23 in the context of isotropic and anisotropic materials
USEFUL FOR

Materials scientists, engineering students, and professionals involved in the study of mechanical properties of materials, particularly those focusing on transversely isotropic materials and their stress-strain behavior.

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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