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Numerical analyses of bending fatigue of four-step three-dimensional rectangular-braided composite materials from unit cell approach

机译:基于单元格的四步三维矩形编织复合材料弯曲疲劳数值分析

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摘要

This paper reports the numerical analyses of three-point bending fatigue behavior of four-step three-dimensional braided composite with three types of representative unit cell (RUC) model. The three types of unit cell models are the unit cell model for the interior, surface, and corner regions of the three-dimensional braided composite. A user-defined material subroutine was developed to characterize the stiffness matrix and fatigue damage evolution of the unit cells and furthermore the braided composite. The fatigue bending behaviors were calculated from the unit cell model with finite element method. It is found that the stress concentration and large deflection located at the middle of the braided composite specimen and both the ends of the bottom areas. As the increase of the stress level, the braided composite is subjected to larger deformation and faster damage accumulation, resulting in a fast fatigue failure. The RUC model could be extended to predict and design the bending fatigue performance of other three-dimensional braided composite structures.
机译:本文用三种代表单元模型(RUC)对四步三维编织复合材料的三点弯曲疲劳行为进行了数值分析。三种类型的晶胞模型是三维编织复合材料内部,表面和拐角区域的晶胞模型。开发了用户定义的材料子例程,以描述单元格以及编织复合材料的刚度矩阵和疲劳损伤演变。用有限元方法从晶胞模型中计算出疲劳弯曲行为。发现应力集中和大挠度位于编织复合材料试样的中部和底部的两端。随着应力水平的增加,编织复合材料会经受更大的变形和更快的损伤积累,从而导致快速的疲劳破坏。 RUC模型可以扩展为预测和设计其他三维编织复合结构的弯曲疲劳性能。

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