碳纤维三维机织整体中空复合材料屈曲与后屈曲行为研究

Study on Buckling and Post-buckling Behaviors of Carbon Fiber Integrated Woven Spacer Composites

  • 摘要: 为研究碳纤维三维机织整体中空复合材料在面外轴压载荷下的屈曲及后屈曲行为,本研究对该材料进行了试验与有限元仿真分析。研究了在压缩载荷下材料的屈曲载荷以及绒经的屈曲破坏模式;基于不同绒经高度试验件的试验结果,分析了绒经高度对屈曲载荷以及破坏模式的影响;基于用户自定义子程序引入Hashin失效准则以及刚度退化准则对材料进行非线性屈曲仿真分析。结果表明,屈曲载荷仿真值与试验值的误差范围在10.9%以内,且破坏模式一致,表明该方法可预测碳纤维三维机织整体中空复合材料的屈曲行为。

     

    Abstract: Experimental studies and finite element simulations are conducted to investigate the buckling and post buckling behaviors of carbon fiber 3D integrated woven spacer composites under out-of-plane axial compression loads. Firstly, the buckling loads of the material and the buckling failure modes of the pile warp under compression loads are studied. Then, based on the experimental results of specimens with different heights of pile warp, the influences of height of pile warp on buckling loads and failure modes are studied. Finally, based on a user-defined subroutine, a finite element model employing the Hashin failure criterion and a stiffness degradation criterion is established to conduct nonlinear buckling analysis of the material. Compared with the experimental results, the error ranges of the buckling loads are within 0.0%-10.9%, and the failure modes are basically coincident, which indicates that the proposed method can predict the buckling behaviors of carbon fiber 3D integrated woven spacer composites.

     

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