Vibration analysis of laminated composite plates with damage using the perturbation method

被引:35
作者
Wang, Zhen-Xin [1 ,2 ,3 ]
Qiao, Pizhong [1 ,2 ,4 ]
Xu, Jifeng [3 ]
机构
[1] Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai 200240, Peoples R China
[2] Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai 200240, Peoples R China
[3] Beijing Aeronaut Sci & Technol Res Inst, Beijing 100083, Peoples R China
[4] Washington State Univ, Dept Civil & Environm Engn, Pullman, WA 99164 USA
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Laminates; Delamination; Vibration; Analytical modeling; Perturbation methods; FATIGUE DAMAGE; CRACK; MODEL;
D O I
10.1016/j.compositesb.2014.12.005
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The present work focuses on vibration characteristics of damaged laminated composite plates. Damage is considered as a local reduction of anisotropic plate stiffness, and three damage factors (representing the damage severity, damage anisotropy, and damage location/area, respectively) are defined to describe damage status in the laminated composite plates. The analytical solutions are obtained by the perturbation method. A numerical analysis is conducted on the vibration of damaged laminated composited plates, and the effect of damage factors on the vibration characteristics is discussed. Results indicate that three damage factors have different influences on the vibration characteristics. Also, the modal curvatures and strain energy show higher damage sensitivity than the natural frequencies and displacement mode shapes. The perturbation-based vibration analysis developed in this study can be used to effectively evaluate the effect of damage on the vibration behavior of anisotropic plates and potentially identify the damage in the laminated plates. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:160 / 174
页数:15
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