基于简化Zinoviev力学模型的复合材料层压板失效分析

上海交通大学学报（自然版） ›› 2013, Vol. 47 ›› Issue (08): 1210-1216.

基于简化Zinoviev力学模型的复合材料层压板失效分析

史晓辉，陈秀华，汪海

(上海交通大学航空航天学院，上海 200240)

收稿日期:2012-07-08 出版日期:2013-08-29 发布日期:2013-08-29
基金资助:
上海交通大学研究生创新能力培养专项基金项目（Z413008）

Progressive Failure Analysis of Composite Laminates Based on Simplified Zinoviev Model

SHI Xiaohui,CHEN Xiuhua,WANG Hai

(School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai 200240, China)

Received:2012-07-08 Online:2013-08-29 Published:2013-08-29

摘要/Abstract

摘要：

根据Zinoviev对复合材料单层板的力学行为分析，对单层板在横向载荷和剪切载荷作用下的力学模型进行了简化，并提出了形式简单的刚度折减公式.结合二维Hashin准则，采用增量法，编写了复合材料层压板强度预测程序.应用该程序对典型算例进行了强度预测，结果显示，简化后的模型能够在保证原模型计算精度的基础上，使计算过程更加简化，方便应用.

关键词: 复合材料, 渐进失效, 刚度折减, 增量法

Abstract:

A simple stiffness degradation method was proposed based on the model of individual unidirectional ply within the laminated composite. The model simplified Zinoviev’s theory of individual unidirectional ply under transverse loading and shear loading. 2D Hashin criterion was employed to predict the failure of individual ply in laminates. With the help of increment method, a program was complied to analysis the failure behavior of composite laminates. With this program, the failure of composite laminates of various layup and materials were predicted. The results demonstrated that, on the premise of maintaining the high accuracy of Zinoviev’s theory, the proposed model simplified the calculation process and could be easily applied to further study.

Key words: composite, progressive failure, stiffness degradation, increment method

中图分类号:

V 258

史晓辉，陈秀华，汪海. 基于简化Zinoviev力学模型的复合材料层压板失效分析[J]. 上海交通大学学报（自然版）, 2013, 47(08): 1210-1216.

SHI Xiaohui,CHEN Xiuhua,WANG Hai. Progressive Failure Analysis of Composite Laminates Based on Simplified Zinoviev Model[J]. Journal of Shanghai Jiaotong University, 2013, 47(08): 1210-1216.

参考文献

［1］胡祎乐,余音,汪海,等.纤维增强复合材料机翼长桁压缩破坏预测方法［J］.上海交通大学学报,2012,46(9):14711481.

HU Yile, YU Yin, WANG Hai, et al. A failure prediction method of fiberreinforced composite wing stringer subjected to compressive loading ［J］. Journal of Shanghai Jiaotong University,2012,46(9):14711481.

［2］赵丽媛,王戈,张双保,等.双轴向力学性能测试方法及其应用［J］.林业机械与木工设备, 2009,37(12):2831.

ZHAO Liyuan, WANG Ge, ZHANG Shuangbao,et al. Biaxial testing method of mechanical properties and application ［J］. Forestry Machinery & Woodworking Equipment， 2009, 37(12):2831.

［3］Huang Z M. A bridging model prediction of the ultimate strength of composite laminates subjected to biaxial loads ［J］. Composites Science and Technology, 2004, 64: 395448.

［4］张华山,黄争鸣.复合材料层压板低速冲击承载能力的细观力学有限元模型［J］.玻璃钢/复合材料，2008(5):1217.

ZHANG Huashan, HUANG Zhengming. A micromechanics model for predicting strengths in fiber laminated composites plate under lowvelocity impact ［J］.FRP/CM, 2008(5): 1217.

［5］Hahn H T, Tsai S W. Nonlinear elastic behavior of unidirectional composite laminate ［J］. J Comp Mater,1973(7): 257271.

［6］刘勇,陈世健,高鑫,等.基于Hashin准则的单层板渐进失效分析［J］.装备环境工程,2010,7(1): 3439.

LIU Yong, CHEN Shijian, GAO Xin, et al. Progressive failure analysis of monolayer composite based on Hashin criterion［J］. Equipment Environmental Engineering, 2010, 7(1):3439.

［7］Zinoviev P A, Grigoriev S V, Lebedeva O V. The strength of multilayered composites under a planestress state［J］. Composites Science and Technology, 1998, 58: 12091223.

［8］Zinoviev P A, Lebedeva O V, Tairova L P. A coupled analysis of experimental and theoretical results on the deformation and failure of composite laminates under a state of plane stress ［J］. Composites Science and Technology, 2002, 62: 17111723.

［9］伍春波,陈秀华,余音,等.复合材料厚板双轴非线性刚度特性分析［J］.航空学报,2012,33(7):12361244.

WU Chunbo, CHEN Xiuhua, YU Yin, et al. Nonlinear stiffness analysis of thick composite laminate under biaxial load ［J］.Acta Aeronautica et Astronautica Sinica, 2012, 33(7): 12361244.

［10］Martin Knops. Analysis of failure in fiber polymer laminates: The theory of Alfred Puck ［M］. Rendsburg: SpringerVerlag, 2008: 37114.

［11］黄争鸣,张华山.纤维增强复合材料强度理论的研究现状与发展趋势——“破坏分析奥运会”评估综述［J］.力学进展,2007,37(1):8098.

HUANG Zhengming, ZHANG Huashan. Current status and future trend of researches on the strength of fiberreinforced composites-a summary of the results from a “future olympics” ［J］.Advances in Mechanics, 2007, 37(1): 8098.

［12］Soden P D, Hinton M J, Kaddour A S. Biaxial test results for strength and deformation of a range of Eglass and carbon fibre reinforced composite laminates: failure exercise benchmark data ［J］.Composites Science and Technology, 2002, 62: 14891514.

[1]	刘庆升, 薛鸿祥, 袁昱超, 唐文勇. 含复合材料结构的非黏结柔性立管弯曲特性[J]. 上海交通大学学报, 2022, 56(9): 1247-1255.
[2]	杨玲玉, 董顺, 洪长青. 新型低密度树脂裂解碳改性碳纤维复合材料的制备与性能研究[J]. 空天防御, 2022, 5(4): 1-9.
[3]	贾米芝, 徐澧明, 林楠, 南博华, 王坤, 蔡登安, 周光明. 具有回弹复位功能易裂盖的结构设计及力学性能研究[J]. 空天防御, 2022, 5(2): 8-16.
[4]	王烨成, 李洋, 张迪, 杨越, 罗震. 碳纤维增强热塑性复合材料与高强钢的电阻单元焊[J]. 上海交通大学学报, 2022, 56(10): 1349-1358.
[5]	王卓鑫, 赵海涛, 谢月涵, 任翰韬, 袁明清, 张博明, 陈吉安. 反向传播神经网络联合遗传算法对复合材料模量的预测[J]. 上海交通大学学报, 2022, 56(10): 1341-1348.
[6]	陶威, 刘钊, 许灿, 朱平. 三维正交机织复合材料翼子板多尺度可靠性优化设计[J]. 上海交通大学学报, 2021, 55(5): 615-623.
[7]	安庆升, 孙立东, 武秋生. 碳纤维增强复合材料发射筒设计研究[J]. 空天防御, 2021, 4(2): 13-.
[8]	管清宇, 夏品奇, 郑晓玲, 吴光辉. 复合材料层压板冲击后压缩强度拟合模型[J]. 上海交通大学学报, 2021, 55(11): 1459-1466.
[9]	胡济珠, 周俊, 李云云. 基于有机/无机复合材料的航天环境下高效热电转换技术研究 [J]. 空天防御, 2020, 3(2): 72-75.
[10]	栾建泽，那景新，慕文龙，谭伟，陈宏利. 低速加载对铝合金-玄武岩纤维增强树脂复合材料粘接接头失效的影响[J]. 上海交通大学学报, 2020, 54(11): 1200-1208.
[11]	刘海龙，张大旭，祁荷音，伍海辉，郭洪宝，洪智亮，陈超，张毅. 基于X射线CT原位试验的平纹SiC/SiC复合材料拉伸损伤演化[J]. 上海交通大学学报, 2020, 54(10): 1074-1083.
[12]	刘晓东，吴磊，孔谅，王敏，陈一东. 空气等离子处理对碳纤维增强复合材料表面特性及胶接性能的影响[J]. 上海交通大学学报, 2019, 53(8): 971-977.
[13]	李昱霖, 安庆升, 杨坤好, 唐晓峰, 刘龙涛. 防热承载一体化复合材料电缆罩分析及验证[J]. 空天防御, 2019, 2(3): 1-7.
[14]	杜思琦，王继崇，彭雄奇，顾海麟. 可生物降解的黄麻纤维/聚乳酸复合材料的制备和力学性能[J]. 上海交通大学学报, 2019, 53(11): 1335-1341.
[15]	杨万友，王家序，黄彦彦，周青华，杨勇. 热载荷作用下颗粒增强复合材料温升分布数值模拟[J]. 上海交通大学学报, 2019, 53(11): 1342-1351.