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一种用于复合材料冲击损伤分析的具有基体塑性的基于键的近场动力学模型。

A Bond-Based Peridynamic Model with Matrix Plasticity for Impact Damage Analysis of Composite Materials.

作者信息

Sun Mingwei, Liu Lisheng, Mei Hai, Lai Xin, Liu Xiang, Zhang Jing

机构信息

Hubei Key Laboratory of Theory and Application of Advanced Materials Mechanics, Wuhan University of Technology, Wuhan 430070, China.

Department of Engineering Structure and Mechanics, Wuhan University of Technology, Wuhan 430070, China.

出版信息

Materials (Basel). 2023 Apr 4;16(7):2884. doi: 10.3390/ma16072884.

Abstract

The prediction of damage and failure to fiber-reinforced polymer composites in extreme environments, particularly when subjected to impact loading, is a crucial issue for the application and design of protective structures. In this paper, based on the prototype microelastic brittle (PMB) model and the LaRC05 composite materials failure model, we proposed a bond-based peridynamic (BB-PD) model with the introduction of plastic hardening of the resin matrix for fiber-reinforced polymer composites. The PD constitutive relationships of the matrix bond and interlayer bond under compressive loading are considered to include two stages of linear elasticity and plastic hardening, according to the stress-strain relationship of the resin matrix in the LaRC05 failure model. The proposed PD model is employed to simulate the damage behaviors of laminated composites subjected to impact loading. The corresponding ballistic impact tests of composite laminates were carried out to observe their damage behaviors. The PD prediction results are in good agreement with the ballistic experimental results, which can verify the correctness and accuracy of the PD model developed in this study in describing the impact damage behaviors of composite materials. In addition, the characteristics and degree of damage in composite laminates are analyzed and discussed based on this PD model. The difference in the impact resistance of composite laminates with different stacking sequences is also studied using the numerical simulation results.

摘要

预测纤维增强聚合物复合材料在极端环境下,特别是承受冲击载荷时的损伤和失效,对于防护结构的应用和设计而言是一个关键问题。本文基于原型微弹性脆性(PMB)模型和LaRC05复合材料失效模型,通过引入树脂基体的塑性硬化,针对纤维增强聚合物复合材料提出了一种基于键的近场动力学(BB-PD)模型。根据LaRC05失效模型中树脂基体的应力-应变关系,考虑了基体键和层间键在压缩载荷下的近场动力学本构关系包括线弹性和塑性硬化两个阶段。采用所提出的近场动力学模型模拟层合复合材料承受冲击载荷时的损伤行为。对复合层合板进行了相应的弹道冲击试验以观察其损伤行为。近场动力学预测结果与弹道试验结果吻合良好,这可以验证本研究中所建立的近场动力学模型在描述复合材料冲击损伤行为方面的正确性和准确性。此外,基于该近场动力学模型对复合层合板中的损伤特征和程度进行了分析和讨论。还利用数值模拟结果研究了不同铺层顺序的复合层合板在抗冲击性方面的差异。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/68fa/10096160/d5063703ff0e/materials-16-02884-g001.jpg

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