Nonlinear finite element analysis of laminated composite doubly curved shells in hygrothermal environment

被引:15
|
作者
Kundu, C. K. [1 ]
Maiti, D. K. [1 ]
Sinha, P. K. [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Kharagpur 721302, W Bengal, India
关键词
geometric nonlinearity; finite element method; composite shells; curvilinear coordinates; hygrothermal;
D O I
10.1177/0731684407079751
中图分类号
TB33 [复合材料];
学科分类号
摘要
In the present investigation, the geometrically nonlinear analysis of laminated doubly curved shells in a hygrothermal environment is presented using the finite element method. The laminated composite shells may be exposed to moisture and temperature during their service life. Hygrothermal effects induce residual stresses and the laminated shell may undergo large bending deformation. The shell geometry used in the formulation is derived using the orthogonal curvilinear coordinate system. Based on the principle of virtual work the nonlinear finite element equations are derived. A total Lagrangian approach associated to the arc-length method is implemented to solve the equilibrium equations. The present results are found to compare well with those available in the open literature and parametric studies are performed to analyze the nonlinear deflections of [0 degrees/45 degrees/90 degrees](s) laminated spherical, cylindrical and conoidal shell panels under hygrothermal condition.
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页码:1461 / 1478
页数:18
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