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三维编织复合材料的压缩损伤模拟
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摘要
三维编织复合材料的强度分析仍然处于初始阶段,而其压缩性能的研究成果目前多来自实验。本文采用细观有限元法,基于线弹性力学对碳/环氧三维四向矩形编织复合材料进行了压缩渐进损伤模拟。参照文献建立了材料内胞的细观有限元分析模型,通过对基体和纤维束采用不同的失效判据及相应材料性能折减方案实现损伤模拟,利用有限元软件ABAQUS的用户材料子程序编写包含组分材料损伤非线性的材料属性,分别对大、小编织角试件采用了几种不同破坏准则判定纤维束单元失效,通过实验对比证明了模型的正确性,同时比较了各准则的模拟结果以确定其适用性,分析了材料压缩损伤起始和演变过程,总结了大、小编织角试件的材料主要破坏模式;在此模拟分析基础上讨论了编织角和纤维体积分数对编织复合材料压缩性能的影响;最后基于假设建立了同已有内胞模型相适应的面胞模型,并对包含面胞的细观模型进行压缩渐进失效模拟,分析了面胞的损伤特点并讨论其对材料性能的影响,为深入研究编织复合材料的破坏及强度提供一些参考。
The strength analysis of 3-D braided composites is still in the initial stage, and the compressive property research results of this material mainly come from experiments. This thesis adopts the microscopic finite element method to conduct progressive damage simulation for carbon/epoxy 3-D four-directional rectangular braided composites on the basis of linear elastic mechanics. Based on the interior unit cell model provided in literature, the finite element analysis model is firstly constructed. Then different damage initiation criteria and corresponding material degradation models are set for matrix and yarn to model different type of damage in comprising materials, and the non-linear material constitutive caused by damage is compiled by the user material subroutine UMAT in finite element software ABAQUS. Progressive damage analysis is conducted for typical large and small braiding angle specimens individually using five different failure criteria for yarns; strength results are compared with experimental data to verify that the analysis model is correct and to determine the applicability of the criteria. Damage initiation and evolution are analyzed and different failure modes are concluded for both large and small braiding angle specimens. The influence of braiding angle and fiber volume fraction on the material compressive property is then investigated. In the last part, the surface cell model is built on hypothesizes in accordance with the interior cell model, and the progressive damage analysis under compression is conducted for the cell model with surface part, then the damage feature of the surface cell as well as its effect on the material property are analyzed for further study on failure and strength of 3-D braided composites.
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