考虑多种失效模式耦合的复合材料损伤分析OACSTPCD
Damage Analysis of Composites by Coupling Multiple Failure Mode
复合材料的损伤失效形式是多样的,其损伤失效形式包括层合板损伤、胶体裂纹扩展和界面脱黏.为了探讨层合板损伤、胶体裂纹扩展、界面脱黏 3 种损伤失效之间的内在联系,先利用ABAQUS/Explicit软件建立混合型弯曲(MMB)断裂有限元模型,通过数值仿真结果与实验结果的比较,从而证明MMB模型的准确性.然后结合Hashin失效准则、扩展有限元法(XFEM)和内聚力模型(CZM)来研究3 种失效模式的内在联系.结果表明:层合板损伤不仅可以影响界面脱黏失效发生时间,同时也能影响胶体中裂纹扩展路径,为复合材料损伤问题数值分析提供了一定的参考.
Composite damage failure form is various,the damage failure forms including laminated plate damage,colloid crack extension and interface debonding.To investigate damage of laminates,colloid crack propagation,interface delamination inherent relations among the three kinds of damage failure,the hybrid bending(MMB)fracture finite element model is firstly established by using ABAQUS/Explicit software,by comparing the simulation and experimental results,which proves the accuracy of MMB model.Then,the internal relationship among the three failure modes was studied by combining the Hashin failure criterion,extended finite Element method(XFEM)and cohesive force model(CZM).The results show that the damage of laminates can not only affect the time of interface viscous separation failure,but also affect the crack propagation path in colloid,which provides a certain reference for numerical analysis of the damage problem of composites.
何易周;张凝;尹硕辉
湘潭大学 机械工程学院,湖南湘潭 411105
层合板损伤胶体裂纹扩展界面脱黏Hashin失效准则XFEMCZM
damage of laminatescolloid crack propagationinterface delaminationHashin failure criterionXFEMCZM
《机械科学与技术》 2024 (001)
166-172 / 7
湖南省教育厅优秀青年项目(20B565)
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