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Accurate nonlinear material models must include both material and damage related nonlinearities. Even at the specimen level macromechanical boundary conditions and specimen geometry can significantly affect the measured response. In this study two experimental techniques for determining shear stress strain response are compared and a micromechanical finite element analysis is used to determine the effect of failure theory on predicted nonlinear response.

The influence of Material Nonlinearity and Microstructural Damage on the Inplane Shear response of Carbon/Epoxy Composites