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Constitutive modelling of composite laminates under uniaxial compression 被引量:4
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作者 Hsuan-Teh HU lung-shen ke 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期938-947,共10页
A nonlinear constitutive model for a single lamina is proposed for the failure analysis of composite laminates. In the material model, both fiber and matrix are assumed to behave elasticplastically and the in-plane sh... A nonlinear constitutive model for a single lamina is proposed for the failure analysis of composite laminates. In the material model, both fiber and matrix are assumed to behave elasticplastically and the in-plane shear is assumed to behave nonlinearly with a variable shear parameter.The damage onset for individual lamina is detected by a mixed failure criterion, composed of the Tsai-Wu criterion and the maximum stress criterion. After damage takes place within the lamina,the fiber and in-plane shear are assumed to exhibit brittle behavior, and the matrix is assumed to exhibit degrading behavior. The proposed nonlinear material model is tested against experimental data of composite laminates subjected to uniaxial compressive loads, and good agreement is obtained. 展开更多
关键词 Composite LAMINATES CONSTITUTIVE model FINITE ELEMENT analysis NONLINEARITY UNIAXIAL compression
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