Nonlinear buckling of eccentrically stiffened nanocomposite cylindrical panels in thermal environments

被引:38
作者
Nguyen Dinh Duc [1 ,2 ,3 ]
Kim, Seung-Eock [3 ]
Tran Quoc Quan [1 ]
Duong Tuan Manh [1 ]
Nguyen Huy Cuong [1 ]
机构
[1] Hanoi Univ Engn & Technol, VNU, Dept Construct & Transportat Engn, 144 Xuan Thuy, Hanoi, Vietnam
[2] Nguyen Tat Thanh Univ, NTT Inst High Technol, Disctr 4, Ho Chi Minh City, Vietnam
[3] Sejong Univ, Dept Civil & Environm Engn, Natl Res Lab, 209 Neungdong Ro, Seoul 05006, South Korea
关键词
Analytical solutions; Nonlinear buckling; Imperfect nanocomposite cylindrical panels; Reddy's third order shear deformation shell theory; Eccentrically stiffeners; Thermal environment; DYNAMIC-RESPONSE; VIBRATION; BEHAVIOR; SHELLS; COMPRESSION; STABILITY;
D O I
10.1016/j.tws.2019.106428
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Based on Reddy's third order shear deformation shell theory and Galerkin method, this paper introduces analytical solutions to study nonlinear buckling behaviors of imperfect carbon nanotube reinforced composite cylindrical panels on elastic foundations in thermal environments. The panels are reinforced by single-walled carbon nanotubes and the eccentrically longitudinal and transversal stiffeners. The effects of geometrical parameters, eccentrically stiffeners, elastic foundations, initial imperfection, temperature increment and nanotube volume fraction on the mechanical behaviors of the nanocomposite cylindrical panels are also examined in numerical results. Some comparisons with results of other authors show the accuracy of the present theory and approach.
引用
收藏
页数:17
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