This chapter describes the mechanics of analyzing carbon-carbon composite materials from the structural analyst’s point of view. The peculiarities of CC material as well as their influences upon the material behavior are discussed. Many assumptions must be made regarding some of the material parameters; an intelligent approach to making those assumptions is presented.
Material models for evaluating thermoelastic properties of fiber composite materials having a spatial distribution of fiber orientations are discussed. The approach is to construct a material model with a finite number of fiber orientations in a repeating unit cell. This basic material model is a mini-mechanical model based upon the concept that a material system can be regarded as an assemblage of unit cells.
Symbols:
EA modulus in axial fiber direction, Msi
ET modulus in transverse fiber direction, Msi
Ez composite modulus in a fiber z direction, Msi
GA fiber axial shear modulus, Msi
△l/lA thermal expansion in axial fiber direction
△l/lT thermal expansion in transverse direction
vAT Poisson’s ratio in axial direction
vTT Poisson’s ratio in transverse direction