Refined beam elements with arbitrary cross-section geometries

被引:204
作者
Carrera, E. [1 ]
Giunta, G. [2 ]
Nali, P. [1 ]
Petrolo, M. [1 ]
机构
[1] Politecn Torino, Dept Aeronaut & Space Engn, I-10129 Turin, Italy
[2] Ctr Rech Publ Henri Tudor, Dept Adv Mat & Struct, L-1855 Luxembourg, Luxembourg
关键词
Refined beam elements; Unified formulation; Higher order modeling; THICKNESS LOCKING; FINITE-ELEMENTS; LAMINATED BEAMS; COMPOSITE; PLATES; BEHAVIOR;
D O I
10.1016/j.compstruc.2009.11.002
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper presents hierarchical beam elements on the basis of the Carrera Unified Formulation. The displacement components are expanded in terms of the section coordinates. (x,y), using a set of I-D generalized displacement variables. N-Order Taylor type expansions are employed. N is a free parameter of the formulation. Linear, quadratic and cubic approximations along the beam axis, (z), are introduced to develop finite element matrices. These are obtained in terms of a few fundamental nuclei whose form is independent of both N and the number of element nodes. Convergence and assessment with available results is first made. Additional analyses consider different beam sections (square and airfoil-shaped) as well as loading conditions (bending and torsion). It has mainly been concluded that the proposed model is capable of furnishing 3-D stress states in the considered beams with conventional (rectangular) and unconventional (thin-walled airfoil) sections. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:283 / 293
页数:11
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