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首页> 外文期刊>Mechanics of composite materials >A Numerical and Experimental Study on the Impact Behavior of a Carbon-Fiber-Reinforced Thermoplastic Poly (Methyl Methacrylate) Composite
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A Numerical and Experimental Study on the Impact Behavior of a Carbon-Fiber-Reinforced Thermoplastic Poly (Methyl Methacrylate) Composite

机译:碳纤维增强热塑性聚(甲基丙烯酸甲酯)复合材料冲击性能的数值和实验研究

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摘要

The goal of the present study was to investigate the low-speed impact behavior and damage patterns of carbonfiber-reinforced methyl methacrylate composites. The process of low-speed impact damage in the composites was simulated using the finite-element method and verified experimentally. Orthotropic plane stress conditions of a homogenized lamina were used to model the composite structures. The evolution of damage was simulated, using the LS-DYNA finite-element code, by material models MAT58 based on the Matzenmiller damage mechanics model with four Hashin failure criteria and MAT54 based on four Chang-Chang failure criteria. The damage variables were determined calibrating the numerical model according to the experimental data of three-pointbending and impact tests. Detailed quantitative comparisons were carried out between the delaminated areas simulated by the model and those characterized experimentally by the ultrasonic C-Scan method. Results of the numerical analyses demonstrated their good agreement with experimental data in terms of contact force histories, peak forces, absorbed energy, and projected damage area.
机译:本研究的目的是研究碳纤维增强甲基丙烯酸甲酯复合材料的低速冲击行为和损伤模式。使用有限元方法模拟复合材料中的低速冲击损伤的过程,并通过实验验证。使用均质薄层的正交平面应力条件来模拟复合结构。根据Matzenmiller损伤力学模型,使用基于四个Chang-Chang失败标准的Matzenmiller损伤标准和MAT54,使用LS-DYNA有限元码模拟损坏的进化。确定根据三点和冲击试验的实验数据确定校准数值模型的损伤变量。在模型模拟的分层区域和通过超声C扫描方法实验表征的分层区域之间进行了详细的定量比较。数值分析的结果证明了与接触力历史,峰值力,吸收能量和投影损伤区域的实验数据良好的一致性。

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