Static and dynamic analysis of the composite laminated stiffened plates via the MLS meshless method

被引:11
|
作者
Peng, L. X. [1 ,2 ,3 ]
Huang, Z. M. [1 ]
Wei, D. Y. [4 ]
He, X. C. [1 ]
机构
[1] Guangxi Univ, Coll Civil Engn & Architecture, Nanning, Peoples R China
[2] Guangxi Univ, Key Lab Disaster Prevent & Struct Safety, Minist Educ, Nanning, Peoples R China
[3] Guangxi Univ, Guangxi Key Lab Disaster Prevent & Struct Safety, Nanning, Peoples R China
[4] Guangxi Technol Coll Machinery & Elect, Fac Civil Engn, Nanning, Peoples R China
基金
中国国家自然科学基金;
关键词
Meshless method; Moving least -squares; Composite laminated stiffened plates; Bending; Free vibration; FREE-VIBRATION ANALYSIS; FINITE-ELEMENT-ANALYSIS; POINT INTERPOLATION METHOD; LARGE-DEFORMATION ANALYSIS; FREE GALERKIN METHOD; BUCKLING ANALYSIS; COLLOCATION; MODEL;
D O I
10.1016/j.enganabound.2023.03.008
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A meshfree method combined the first-order shear deformation (FSDT) theory to moving least-squares (MLS) approximation for static and dynamic investigations of composite laminated stiffened plates is presented. The novelty is that the resultant meshfree model presented in this paper considers the coupling effects in laminated plates and torsional effects and out-of-plane deformations for laminated ribs. The composite laminated stiffened plate is viewed as a composite structure of a laminated plate and ribs. MLS and FSDT are employed to establish the displacement fields, and the transformation equation of the nodal parameters between laminated rib and laminated plate is proposed. After superposing the potential and kinetic energy of the plate and stiffeners and introducing the displacement compatibility condition, the equations governing the bending and free vibration of the stiffened plates are obtained according to the principle of Minimum Potential Energy and Hamilton's Prin-ciple, respectively. Thereafter, several stiffened plate examples with different numbers and heights of ribs, different laminated arrangements and boundary conditions are calculated. The comparison of the present results with those given by ABAQUS and the literature. The results show the effectiveness and accuracy of the present method in analyzing the bending and free vibration properties of composite laminated stiffened plates.
引用
收藏
页码:309 / 327
页数:19
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