基于渐进损伤理论的复合材料开孔拉伸失效分析
TB33; 为研究碳纤维复合材料在受载情况下损伤的萌生、扩展及材料失效行为,采用三维Hashin失效准则预测材料的初始失效,基于渐进损伤理论提出了一种用于材料损伤后的刚度折减方案.利用编写的UMAT用户子程序对碳纤维复合材料板开孔拉伸进行数值分析,并将数值计算结果与碳纤维复合材料板开孔拉伸实验结果进行对比分析,结果表明数值分析对极限载荷的预测和失效过程的预测结果与实验结果吻合较好....
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Published in | 航空材料学报 Vol. 38; no. 5; pp. 138 - 146 |
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Main Authors | , , , , |
Format | Journal Article |
Language | Chinese |
Published |
上海飞机制造有限公司,上海,200436%大连理工大学 汽车工程学院,辽宁 大连,116024%大连理工大学 机械工程学院,辽宁 大连,116024
01.10.2018
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Subjects | |
Online Access | Get full text |
ISSN | 1005-5053 |
DOI | 10.11868/j.issn.1005-5053.2017.000133 |
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Abstract | TB33; 为研究碳纤维复合材料在受载情况下损伤的萌生、扩展及材料失效行为,采用三维Hashin失效准则预测材料的初始失效,基于渐进损伤理论提出了一种用于材料损伤后的刚度折减方案.利用编写的UMAT用户子程序对碳纤维复合材料板开孔拉伸进行数值分析,并将数值计算结果与碳纤维复合材料板开孔拉伸实验结果进行对比分析,结果表明数值分析对极限载荷的预测和失效过程的预测结果与实验结果吻合较好. |
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AbstractList | TB33; 为研究碳纤维复合材料在受载情况下损伤的萌生、扩展及材料失效行为,采用三维Hashin失效准则预测材料的初始失效,基于渐进损伤理论提出了一种用于材料损伤后的刚度折减方案.利用编写的UMAT用户子程序对碳纤维复合材料板开孔拉伸进行数值分析,并将数值计算结果与碳纤维复合材料板开孔拉伸实验结果进行对比分析,结果表明数值分析对极限载荷的预测和失效过程的预测结果与实验结果吻合较好. |
Author | 陈磊 李汝鹏 高航 曾祥钱 刘学术 |
AuthorAffiliation | 上海飞机制造有限公司,上海,200436%大连理工大学 汽车工程学院,辽宁 大连,116024%大连理工大学 机械工程学院,辽宁 大连,116024 |
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Author_FL | GAO Hang ZENG Xiangqian LI Rupeng CHEN Lei LIU Xueshu |
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Keywords | 渐进损伤 失效分析 碳纤维复合材料 刚度折减 |
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Publisher | 上海飞机制造有限公司,上海,200436%大连理工大学 汽车工程学院,辽宁 大连,116024%大连理工大学 机械工程学院,辽宁 大连,116024 |
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Title | 基于渐进损伤理论的复合材料开孔拉伸失效分析 |
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