A new finite element for the analysis of functionally graded shells

被引:6
|
作者
Hernandez, Mirna Teresita Armendariz [1 ]
Diaz, Alberto Diaz [1 ]
Rascon, Carlos Humberto Rubio [2 ]
Balderas, Ruben Castaneda [1 ]
机构
[1] Ctr Invest Mat Avanzados SC, Miguel Cervantes 120,Complejo Ind Chihuahua, Chihuahua 31136, Mexico
[2] Inst Tecnol Chihuahua II, Ave Ind 11101,Complejo Ind Chihuahua, Chihuahua 31130, Mexico
关键词
Shell; Functionally graded material; Stress analysis; Finite element; MECHANICAL-BEHAVIOR; MULTILAYERED PLATES; TRANSVERSE LOAD; PANELS; FORMULATION; MODELS;
D O I
10.1016/j.tws.2023.110659
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents the development of a finite element model for functionally graded shells. The formulation solves the equations of the Stress Approach Model for Functionally Graded shells (SAM-FG) developed and validated by Rubio Rascon et al. (2020). SAM-FG involves only 5 generalized displacements and its equations differ from those of classical first order shear deformation theories mainly in the expressions of the generalized stiffnesses and the approximation of stresses. A 10-node isoparametric triangular element using cubic shape functions and 5 degrees of freedom per node is proposed. The equations of the numerical method were implemented in a program called FESAM-FG. The finite element code enables to calculate and visualize generalized fields on the middle surface of the shell and stress components at a given position across the thickness of the structure. To test the accuracy and convergence of FESAM-FG results, the numerical tool is applied to the structural analysis of four families of functionally graded shells with various distributions of material properties and thickness-to-radius ratios. Results are compared to those obtained by solid finite elements, a higher order shear deformation theory developed by Viola et al. (2014) and two shell models used for laminated composite structures: an equivalent single layer model and a layerwise model, both using 30 fictitious layers.
引用
收藏
页数:18
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