Efficient analysis on buckling of FG-CNT reinforced composite joined conical-cylindrical laminated shells based on GDQ method under multiple loading conditions

被引:8
|
作者
You, Qingquan [1 ,2 ]
Hua, Fenfei [1 ,2 ]
Huang, Qingyang [1 ,2 ]
Zhou, Xiaoqiang [1 ,2 ]
机构
[1] Huazhong Univ Sci & Technol, Sch Aerosp Engn, Dept Mech, Wuhan 430074, Peoples R China
[2] Hubei Key Lab Engn Struct Anal & Safety Assessment, Wuhan, Peoples R China
基金
中国国家自然科学基金;
关键词
Functionally graded carbon nanotube; joined conical-cylindrical shell; generalized differential quadrature method; buckling; FREE-VIBRATION ANALYSIS; ELASTIC FOUNDATIONS; DIFFERENTIAL QUADRATURE; THERMAL ENVIRONMENT; SANDWICH PLATES; AGGLOMERATION;
D O I
10.1080/15376494.2024.2302327
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This work presents an efficient analysis of buckling for functionally graded carbon nanotube reinforced composite (FG-CNTRC) joined conical-cylindrical laminated shells with lateral pressure and axial compressive load considering thermal effect. The governing equilibrium equation of the joined conical-cylindrical shell (CO-CYL) is determined using the first-order shear deformation theory (FSDT), Donnell kinematic assumptions, von-Karman geometrical nonlinearity, and considering thermal effect. A semi-analytical solution, generalized differential quadrature (GDQ) method, and artificial springs are applied during the solution procedure. The comparison studies have demonstrated a remarkable 97% reduction in running time compared to the finite element method (FEM).
引用
收藏
页码:11173 / 11190
页数:18
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