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Experimental investigation and numerical simulation of three-point bending fatigue of 3D orthogonal woven composite

机译:3D正交编织复合材料三点弯曲疲劳试验研究与数值模拟

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This paper reports the three-point bending fatigue behavior of three-dimensional (3D) orthogonal woven composite (3DOWC) in experimental and finite element analysis (FEA) approach. In experimental, the S-N curve was obtained to illustrate the relationship between applied stress levels and number of cycles to failure. The stiffness variation was recorded to present the degradation of mechanical properties of the 3D0WC during the process of fatigue loading. Furthermore, the fatigue damage morphologies of the tested 3D0WC coupons were given to indicate the damage modes of different parts (resin, yarns, and their interface) of the composite under the range of stress levels. In FEA approach, a user-defined material subroutine UMAT which characterizes the stiffness matrix and fatigue damage evolution of the 3DOWC was developed and incorporated with a finite element code ABAQUS/Standard to calculate the maximum deflection of the 3DOWC during each loading cycle. The bending deformation at different loading cycles was also calculated. From the comparisons between FEA and experimental approaches, it is indicated that the proposed model is reasonable for calculating the fatigue bending deformation.
机译:本文报告了三维(3D)正交编织复合材料(3DOWC)在实验和有限元分析(FEA)方法中的三点弯曲疲劳行为。在实验中,获得了S-N曲线以说明所施加的应力水平与失效循环次数之间的关系。记录了刚度变化,以显示3D0WC在疲劳载荷过程中机械性能的下降。此外,给出了测试的3D0WC试样的疲劳损伤形态,以表明在应力水平范围内复合材料不同部分(树脂,纱线及其界面)的损伤模式。在FEA方法中,开发了可定义3DOWC刚度矩阵和疲劳损伤演变的用户定义材料子程序UMAT,并将其与有限元代码ABAQUS / Standard结合使用,以计算每个加载周期中3DOWC的最大挠度。还计算了不同加载周期下的弯曲变形。通过有限元分析和实验方法的比较,表明该模型对于计算疲劳弯曲变形是合理的。

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