Accurate transverse stress evaluation in composite/sandwich thick laminates using a C0 HSDT and a novel post-processing technique

被引:18
作者
Bhar, A. [1 ]
Satsangi, S. K. [2 ]
机构
[1] Motilal Nehru Natl Inst Technol, Dept Appl Mech, Allahabad 211004, Uttar Pradesh, India
[2] Indian Inst Technol, Dept Ocean Engn & Naval Architecture, Kharagpur 721302, W Bengal, India
关键词
Composite/sandwich thick laminate; Transverse shear stress; C-0; HSDT; LSE post-processing; HIGHER-ORDER THEORY; FINITE-ELEMENT FORMULATION; PLATE DEFORMATION;
D O I
10.1016/j.euromechsol.2010.09.003
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An efficient method for accurate evaluation of through-the-thickness distribution of transverse stresses in thick composite and sandwich laminates, using a displacement-based C-0 higher-order shear deformation theory (HSDT), is presented. The technique involves a least square of error (LSE) method applied to the 3D equilibrium equations at the post-processing phase, after a primary finite element analysis is performed using the HSDT. This is distinctly different from the conventional method of integrating the 3D equilibrium equations, for transverse stress recovery in composite laminates during post-processing. Competence of the technique is demonstrated in the numerical examples through comparison with results from first-order shear deformation theory (FSDT), another HSDT and those from analytical and 3D elasticity solutions available in literature. (C) 2010 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:46 / 53
页数:8
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