Mesh-free radial basis function method for static, free vibration and buckling analysis of shear deformable composite laminates

被引:81
作者
Liu, L. [1 ]
Chua, L. P. [1 ]
Ghista, D. N. [1 ]
机构
[1] Nanyang Technol Univ, Sch Mech & Aerosp Engn, Singapore 639798, Singapore
关键词
mesh-free method; radial point interpolation method; free vibration; buckling; laminated composite plates; third-order shear deformation plate theory;
D O I
10.1016/j.compstruct.2005.08.010
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A mesh-free radial basis function method is presented to analyze the static deflection, free vibration and buckling analysis of laminated composite plates using third-order shear deformation plate theory. The problem domain represented by a set of scattered nodes in its support domain based on the radial basis functions with polynomial reproduction. Based on the third-order shear deformation plate theory, variation forms of the static, free vibration and buckling system equations are formulated in terms of displacements and are discretized. The shape function thus constructed possesses a delta function property, and hence the essential boundary conditions can be implemented with ease as in the conventional finite element method. Several numerical examples are presented to demonstrate the convergence, accuracy and validity of the proposed method. Comparison of results with the exact solution as well as finite element method in the literature suggests that the mesh free radial basis function method yields an effective solution method for laminated composite plates. The effects of the modulus ratio, side-to-thickness ratio, shear correction factor and boundary conditions are discussed. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:58 / 69
页数:12
相关论文
共 50 条
[21]   Free vibration of skew fiber-reinforced composite and sandwich laminates using a shear deformable finite element model [J].
Garg, AK .
JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2006, 8 (01) :33-53
[22]   Static and free vibration analysis of delaminated composite plates using secant function based shear deformation theory [J].
Bhardwaj, Nitin ;
Sinha, Abhiraj ;
Abhijeet, Babar ;
Sahoo, Rosalin .
JOURNAL OF STRAIN ANALYSIS FOR ENGINEERING DESIGN, 2024, 59 (03) :178-193
[23]   Free vibration analysis of symmetric laminated composite plates by FSDT and radial basis functions [J].
Ferreira, AJM ;
Roque, CMC ;
Jorge, RMN .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2005, 194 (39-41) :4265-4278
[24]   Free vibrations and buckling analysis of laminated plates by oscillatory radial basis functions [J].
Neves, A. M. A. ;
Ferreira, A. J. M. .
CURVED AND LAYERED STRUCTURES, 2016, 3 (01) :17-21
[25]   Free vibration and buckling analysis of laminated composites and sandwich microbeams using a transverse shear-normal deformable beam theory [J].
Karamanli, Armagan ;
Aydogdu, Metin .
JOURNAL OF VIBRATION AND CONTROL, 2020, 26 (3-4) :214-228
[26]   Morphing of Plane Element to Beam Element for Static, Buckling, and Free Vibration Analysis [J].
Yaghoobi, Majid ;
Sedaghatjo, Mohsen ;
Alizadeh, Reyhaneh .
IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY-TRANSACTIONS OF CIVIL ENGINEERING, 2021, 45 (04) :2425-2435
[27]   A mesh-free analysis of the ship structures based on daubechies wavelet basis theory [J].
Chen, Jianping ;
Tang, Wenyong ;
Xu, Manping .
Journal of Information and Computational Science, 2015, 12 (05) :1675-1684
[28]   Nonlinear analyses of FGM plates in bending by using a modified radial point interpolation mesh-free method [J].
Vuong Nguyen Van Do ;
Lee, Chin-Hyung .
APPLIED MATHEMATICAL MODELLING, 2018, 57 :1-20
[29]   Morphing of Plane Element to Beam Element for Static, Buckling, and Free Vibration Analysis [J].
Majid Yaghoobi ;
Mohsen Sedaghatjo ;
Reyhaneh Alizadeh .
Iranian Journal of Science and Technology, Transactions of Civil Engineering, 2021, 45 :2425-2435
[30]   Vibration analysis of a strain gradient plate model via a mesh-free moving Kriging Interpolation Method [J].
Hou, Dongchang ;
Wang, Lifeng ;
Yan, Jianwei ;
Liew, Kim Meow .
ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS, 2022, 135 :156-166