Introduction

In the previous lectures we have introduced the concept of CCA model and have derived the expressions for effective axial modulus; Poisson’s ratio; shear modulus and plane strain bulk modulus. Now, only one of the effective properties is left to be determined so that we can get all effective properties of the composite. This property is transverse shear modulus.

In the present lecture, we will derive the expression for effective transverse shear modulus.

The Lecture Contains