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Compressive failure analysis of unidirectional carbon/epoxy composite based on micro-mechanical models 被引量:6

Compressive failure analysis of unidirectional carbon/epoxy composite based on micro-mechanical models
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摘要 A 2D micro-mechanical model was proposed to study the compressive failure of Uni Directional(UD) carbon/epoxy composite. Considering the initial imperfection and strength distribution of the fiber, the plasticity and ductile damage of the matrix, the failure of T300/914 UD composite under longitudinal compression and in-plane combined loads was simulated by this model. Simulation results show that the longitudinal compressive failure of the UD composite is caused by the plastic yielding of the matrix in kink band, and the fiber initial imperfection is the main reason for it. Under in-plane combined loads, the stress state of the matrix in kink band is changed, which affects the longitudinal compressive failure modes and strength of UD composite.The failure envelope of r_1–s_(12) and r_1–r_2 are obtained by the micro-mechanical model. Meanwhile,the compressive failure mechanism of the UD composite is analyzed. Numerical results agree well with the experimental data, which verifies the validity of the micro-mechanical model. A 2D micro-mechanical model was proposed to study the compressive failure of Uni Directional(UD) carbon/epoxy composite. Considering the initial imperfection and strength distribution of the fiber, the plasticity and ductile damage of the matrix, the failure of T300/914 UD composite under longitudinal compression and in-plane combined loads was simulated by this model. Simulation results show that the longitudinal compressive failure of the UD composite is caused by the plastic yielding of the matrix in kink band, and the fiber initial imperfection is the main reason for it. Under in-plane combined loads, the stress state of the matrix in kink band is changed, which affects the longitudinal compressive failure modes and strength of UD composite.The failure envelope of r_1–s_(12) and r_1–r_2 are obtained by the micro-mechanical model. Meanwhile,the compressive failure mechanism of the UD composite is analyzed. Numerical results agree well with the experimental data, which verifies the validity of the micro-mechanical model.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2017年第6期1907-1918,共12页 中国航空学报(英文版)
关键词 Micro-mechanical model Unidirectional composite Initial imperfection Matrix plasticity Ductile damage Kink band Micro-mechanical model Unidirectional composite Initial imperfection Matrix plasticity Ductile damage Kink band
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