Analysis of laminated shells by a sinusoidal shear deformation theory and radial basis functions collocation, accounting for through-the-thickness deformations

被引:161
作者
Ferreira, A. J. M. [1 ]
Carrera, E. [3 ]
Cinefra, M. [3 ]
Roque, C. M. C. [2 ]
Polit, O. [4 ]
机构
[1] Univ Porto, Dept Engn Mecan, Fac Engn, P-4200465 Oporto, Portugal
[2] Univ Porto, INEGI, Fac Engn, P-4200465 Oporto, Portugal
[3] Politecn Torino, Dept Aeronaut & Aerosp Engn, I-10129 Turin, Italy
[4] Univ Paris Ouest Nanterre, F-92410 Ville Davray, France
关键词
Laminates; Vibration; Numerical analysis; FREE-VIBRATION ANALYSIS; FINITE-ELEMENT; MEMBRANE LOCKING; PLATES; FORMULATION; INTERPOLATION;
D O I
10.1016/j.compositesb.2011.01.031
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, the static and free vibration analysis of laminated shells is performed by radial basis functions collocation, according to a sinusoidal shear deformation theory (SSDT). The SSDT theory accounts for through-the-thickness deformation, by considering a sinusoidal evolution of all displacements with the thickness coordinate. The equations of motion and the boundary conditions are obtained by the Carrera's Unified Formulation, and further interpolated by collocation with radial basis functions. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1276 / 1284
页数:9
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