Investigation of Micro-Scale Architectural Effects on Damage of Composites

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

This paper presents a three-dimensional, energy based, anisotropic, stiffness reduction, progressive damage model for composite materials and composite material constituents. The model has been implemented as a user-defined constitutive model within the Abaqus finite element software package and applied to simulate the nonlinear behavior of a damaging epoxy matrix within a unidirectional composite material. Three different composite microstructures were considered as finite element repeating unit cells, with appropriate periodicity conditions applied at the boundaries. Results representing predicted transverse tensile, longitudinal shear, and transverse shear stress-strain curves are presented, along with plots of the local fields indicating the damage progression within the microstructure. It is demonstrated that the damage model functions appropriately at the matrix scale, enabling localization of the damage to simulate failure of the composite material. The influence of the repeating unit cell geometry and the effect of the directionality of the applied loading are investigated and discussed.

Authors

• Stier, Bertram Technische Hochschule
• Bednarcyk, Brett A. NASA Glenn Research Center
• Simon, Jaan W. Technische Hochschule
• Reese, Stefanie Technische Hochschule

Keywords

• damage
• composite materials
• finite element method