Abstract
In this paper, the shear nonlinearity and failure behavior of composite laminates were investigated with experimental and numerical method. A nonlinear shear model that includes progressive stiffness reduction and permanent shear strain was developed to characterize the nonlinear shear behavior. Strain-based failure criteria were combined with a set of stiffness degradation method to predict in-ply damage initiation and evolution of composite laminates. Delamination damage was simulated with cohesive zone model. The progressive damage model was implemented in commercial finite element software ABAQUS by a VUMAT subroutine. The capability of the proposed model was validated by predicting the tensile behavior of open-hole tensile specimen.
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