Multi-field coupling static bending of a finite length inhomogeneous double-layered structure with inner hollow cylinder and outer shell

被引:11
|
作者
Dai, Hong-Liang [1 ,2 ,3 ,4 ]
Luo, Wei-Feng [1 ,2 ,3 ,4 ]
Dai, Ting [1 ,2 ,3 ,4 ]
机构
[1] Hunan Univ, State Key Lab Adv Design & Mfg Vehicle Body, Changsha 410082, Hunan, Peoples R China
[2] Tsinghua Univ, Grad Sch Shenzhen, Joint Res Ctr Urban Resource Recycling Technol, Shenzhen 518055, Peoples R China
[3] Shenzhen Green Ecomanufacturer High Tech, Shenzhen 518055, Peoples R China
[4] Hunan Univ, Minist Educ, Key Lab Adv Design & Simulat Technol Special Equi, Changsha 410082, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Multi-field coupling system; Hollow cylinder; Cylindrical shell; FGPM; Inhomogeneous; FGM CYLINDRICAL-SHELL; POSTBUCKLING ANALYSES; VIBRATION ANALYSIS; STRESS; TEMPERATURE; BEHAVIOR; ROUGHNESS; COATINGS;
D O I
10.1016/j.apm.2016.01.040
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study deals with the static bending of a finite length double-layered structure under radially symmetric mechanic and thermal loadings. The double-layered hollow structure is constructed of inner thermal barrier cylinder and outer FGPM(functionally graded piezoelectric material)cylindrical shell. The inner hollow cylinder is subjected to symmetric mechanic and thermal loadings, the outer shell is under an extra electric field. The material parameters of the double-layered structure are assumed to be inhomogeneous, or, rather, follows a power-law distribution. The inner thermal barrier cylinder is solved by the finite difference method, and the outer cylindrical shell is solved by using the analytical method. In the examples, numerical results separately show the effect of material properties, geometric shapes, mechanical and temperature loads on the double-layered structure. The distributions of material properties and the thickness ratio have a great influence on displacement and stress of the double-layered structure. Results in this study may be useful for the optimal design of FGPM cylindrical shell with thermal barrier layer. (C) 2016 Elsevier Inc. All rights reserved.
引用
收藏
页码:6006 / 6025
页数:20
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