基于Puck准则的复合材料层压板低速冲击数值分析与试验验证

doi:10.19936/j.cnki.2096-8000.20210628.003

复合材料科学与工程 ›› 2021, Vol. 0 ›› Issue (6): 20-25.DOI: 10.19936/j.cnki.2096-8000.20210628.003

基于Puck准则的复合材料层压板低速冲击数值分析与试验验证

李磊¹, 宋贵宾¹, 郑华勇², 程鹏飞¹, 赵剑^3*

1.中国飞机强度研究所,西安 710065;
2.上海宇航系统工程研究所,上海 201108;
3.同济大学航空航天与力学学院,上海 200092

收稿日期:2021-04-25 出版日期:2021-06-28 发布日期:2021-08-03
通讯作者: 赵剑(1982-),男,博士,助理教授,主要从事先进材料与结构的多尺度力学分析、复合材料结构设计等方面的研究,zhaojian@tongji.edu.cn。
作者简介:李磊(1982-),男,硕士,高级工程师,主要从事复合材料力学性能表征和强度分析技术方面的研究。
基金资助:
上海市自然科学基金(20ZR1462600);航空科学基金(201909038001);上海航天科技创新基金(SAST202020)

NUMERICAL ANALYSIS AND EXPERIMENTAL VERIFICATION OF LOW-VELOCITY IMPACT OFCOMPOSITE LAMINATES BASED ON PUCK′S FAILURE CRITERION

LI Lei¹, SONG Gui-bin¹, ZHENG Hua-yong², CHENG Peng-fei¹, ZHAO Jian^3*

1. China Aircraft Strength Research Institute, Xi′an 710065, China;
2. Shanghai Institute of Aerospace Systems Engineering, Shanghai 201108, China;
3. School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092, China

Received:2021-04-25 Online:2021-06-28 Published:2021-08-03

摘要/Abstract

摘要： 本文发展了一种复合材料层压板冲击损伤数值模拟分析方法,建立了低速冲击问题的分析模型,该模型考虑了纤维损伤、基体损伤以及层间损伤等失效模式,采用基于物理失效模式的Puck失效准则预测损伤起始以及基于断裂应变能的刚度退化方式预测损伤演化过程。开展了T300、T700以及T800等多种纤维和树脂匹配层压板的抗冲击性能试验研究,获得了纤维和树脂性能对层压板抗冲击性能的影响规律。通过仿真结果与试验结果对比,表明所发展的复合材料层压板低速冲击损伤数值分析方法具有较高精度。

关键词: 复合材料层压板, 低速冲击, 失效数据, 渐进损伤, 有限元分析

Abstract: A numerical simulation analysis method for impact damage of composite laminates was developed, and an analysis model for low-velocity impact was established. The failure modes such as fiber damage, matrix damage, and interlayer damage were considered in the model, Puck failure criterion based on physical failure modes was adopted to predict the damage initiation and the stiffness degradation method based on the fracture strain energy was used to predict the damage evolution process. The impact resistance tests of T300, T700 and T800 carbon fiber reinforced laminates were carried out, and the law of the influence of fiber and resin properties on the impact resistance of laminates was obtained. The comparison between simulation results and test results shows that the developed numerical analysis method for low-velocity impact damage analysis of composite laminates has high accuracy.

Key words: composite laminates; low-velocity impact; failure criteria; progressive damage; finite element analysis

中图分类号:

TB332

李磊, 宋贵宾, 郑华勇, 程鹏飞, 赵剑. 基于Puck准则的复合材料层压板低速冲击数值分析与试验验证[J]. 复合材料科学与工程, 2021, 0(6): 20-25.

LI Lei, SONG Gui-bin, ZHENG Hua-yong, CHENG Peng-fei, ZHAO Jian. NUMERICAL ANALYSIS AND EXPERIMENTAL VERIFICATION OF LOW-VELOCITY IMPACT OFCOMPOSITE LAMINATES BASED ON PUCK′S FAILURE CRITERION[J]. COMPOSITES SCIENCE AND ENGINEERING, 2021, 0(6): 20-25.

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基于Puck准则的复合材料层压板低速冲击数值分析与试验验证

NUMERICAL ANALYSIS AND EXPERIMENTAL VERIFICATION OF LOW-VELOCITY IMPACT OFCOMPOSITE LAMINATES BASED ON PUCK′S FAILURE CRITERION

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