[1]郭文辉,李成.采用流固耦合方法的复合材料层合板鸟撞分析[J].郑州大学学报(工学版),2015,36(06):76.[doi:10.3969 / j. issn.1671 -6833.2015.06.015]
　LI Cheng,GUo Wenhui,TIE Ying.Analysis of bird impact on composite laminates by fluid-solid coupling method[J].Journal of Zhengzhou University (Engineering Science),2015,36(06):76.[doi:10.3969 / j. issn.1671 -6833.2015.06.015]
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采用流固耦合方法的复合材料层合板鸟撞分析()
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《郑州大学学报(工学版)》[ISSN:1671-6833/CN:41-1339/T]

卷:
36卷
期数:
2015年06期
页码:
76
栏目:
出版日期:
2015-12-25

文章信息/Info

Title:
Analysis of bird impact on composite laminates by fluid-solid coupling method
作者:
郭文辉; 李成
郑州大学机械工程学院,河南郑州450001
Author(s):
LI Cheng; GUo Wenhui; TIE Ying
School of Mechanical Engineering，Zhengzhou University，Zhengzhou 450001，China
关键词:
流固耦合; 复合材料; 鸟撞; 动响应; 损伤分析
Keywords:
fluid-solid coupling;  composite;  bird impact;  dynamic response;  damage analysis
分类号:
V215
DOI:
10.3969 / j. issn.1671 -6833.2015.06.015
文献标志码:
A
摘要:
基于流固耦合的方法,利用ANSYS/LS - DYNA软件构建了复合材料层合板鸟撞损伤模型,通过分析层合板鸟撞后的动响应验证了鸟撞过程的4个阶段,探讨了鸟撞过程中冲击波在层合板中的传递情况;分析了层合板在鸟撞时先后出现的基体压缩、基体开裂以及纤维断裂这一损伤过程;研究了铺层方式对鸟撞后鸟体的剩余能的影响.结果表明:合理的设计铺层方式可以有效提升层合板抗撞能力.
Abstract:
With the fluid-solid coupling method,damage model of the composite laminates under bird impact isbuilt by using the software IS-DYNA; through analyzing the dynamic response of the laminates，four stages ofthe bird impact process are verified，and spreading of the impact wave in the laminates is discussed. The pro-gressive damage process of matrix compression，matrix cracking， and fiber fracture during the bird impact is an-alyzed. The effect of different layer styles on residual energy of the bind after impact is studied,and the resultproves that properly designed layer style can improve the anti-impact capacity of the laminates effectively.

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