对称层合折板结构自由振动分析的移动最小二乘无网格法

提出了一种求解对称层合折板结构自由振动问题的移动最小二乘无网格法。以作者提出的折板无网格模型为基础,将对称层合折板结构视为由不同平面上对称层合板组成的复合结构。先基于一阶剪切变形理论,由移动最小二乘近似推导出各对称层合板的刚度和质量矩阵,再利用板与板间的位移协调条件,将各板的刚度和质量矩阵叠加得到整个结构的刚度和质量矩阵,推导出描述层合折板结构自由振动行为的控制方程。文末算例表明由本文方法得到的解与采用壳单元得到的ANSYS有限元解吻合良好,证明了本文方法的准确性。     

平行四边形加肋板自由振动分析的无网格法

基于一阶剪切理论,提出一种求解平行四边形加肋板自由振动问题的无网格法,通过用一系列点来离散平板及肋条,得到加肋板的无网格模型。基于一阶剪切理论及移动最小二乘近似求出位移场,以梁模拟肋条,求出平行四边形加肋板总动能及总势能。再由Hamilton原理导出加肋板自由振动的控制方程,采用完全转换法引入边界条件,求解方程得出结构自振频率。以不同参数的加肋板为例,将该文解与ABAQUS有限元解进行比较分析。研究表明,该方法能有效地分析平行四边形加肋板自由振动问题,在肋条位置改变时,又避免了网格重构。     

基于一阶剪切变形理论和移动最小二乘近似的加肋板屈曲临界荷载求解

针对加肋板屈曲临界荷载的求解,提出了一种基于一阶剪切变形理论和移动最小二乘近似的无网格方法。该方法将加肋板的肋条和平板分开考虑,肋条用梁模型来模拟,按照一阶剪切变形理论和移动最小二乘近似给出平板和肋条的无网格近似位移场,再利用板和肋条交界上的位移协调条件推导出将肋条的节点参数转换成板节点参数的公式,最后通过转换公式,将板和肋条的势能叠加,由最小势能原理得到描述整个加肋板线性屈曲行为的控制方程。该文方法相对有限元的优势在于加肋板肋条不必沿网格线布置,即使肋条位置改变也不需要网格重构。文末通过几个算例比较了该文方法解和采用实体单元的ANSYS 有限元解,两者较为接近,证明了该文方法的准确性。     

任意壳线性弯曲与自由振动分析的最小二乘无网格法

提出了一种求解任意壳结构线性弯曲与自由振动的最小二乘无网格法。利用映射技术并结合Mindlin板壳理论将三维任意壳参数化曲面转换成二维无网格模型。基于移动最小二乘法近似和一阶剪切变形理论求出其位移场,利用最小势能原理及Hamilton原理分别得到其弯曲及自由振动控制方程。由于该方法不能直接施加本质边界条件,故采用完全转换方法引入本质边界条件。文末以几种典型的不同形状壳结构算例表明,该研究的解与理论解或ABAQUS有限元解吻合良好,证明了该方法在计算任意壳的线性弯曲与自由振动的有效性及准确性。     

弹性地基圆形加肋板静力弯曲及弯曲自由振动分析的无网格法

基于一阶剪切理论和移动最小二乘法,提出分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题的无网格方法.对弹性地基采用Winkler地基模型,对圆形加肋板则将平板和肋条分开考虑,通过位移协调条件建立两者的参数转换方程.平板和肋条均采用一系列点来离散,用移动最小二乘法建立的形函数来分别描述两者的位移场,再分别通过最小势能原...     

折板结构非线性弯曲分析的移动最小二乘无网格法

提出了一种研究折板结构非线性弯曲行为的移动最小二乘无网格法。先将折板结构模拟成不同平面上平板的集合体,再基于冯·卡门的大挠度理论,使用一阶剪切变形理论和移动最小二乘近似先分析各平板的几何非线性行为,最后将通过修正的各板的非线性刚度矩阵叠加得到整个折板结构的非线性刚度矩阵,研究整个结构的几何非线性行为。由于摆脱了网格的束缚,该文方法可以避免网格扭曲引起的网格重构问题。文末通过几个算例将该文方法与使用壳单元的ANSYS 有限元非线性分析进行对比,发现两者的计算结果接近。     

任意壳线性弯曲与自由振动分析的最小二乘无网格法EI北大核心CSCD

提出了一种求解任意壳结构线性弯曲与自由振动的最小二乘无网格法。利用映射技术并结合Mindlin板壳理论将三维任意壳参数化曲面转换成二维无网格模型。基于移动最小二乘法近似和一阶剪切变形理论求出其位移场,利用最小势能原理及Hamilton原理分别得到其弯曲及自由振动控制方程。由于该方法不能直接施加本质边界条件,故采用完全转换方法引入本质边界条件。文末以几种典型的不同形状壳结构算例表明,该研究的解与理论解或ABAQUS有限元解吻合良好,证明了该方法在计算任意壳的线性弯曲与自由振动的有效性及准确性。     

弹性地基圆形加肋板静力弯曲及弯曲自由振动分析的无网格法EI北大核心CSCD

基于一阶剪切理论和移动最小二乘法,提出分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题的无网格方法。对弹性地基采用Winkler地基模型,对圆形加肋板则将平板和肋条分开考虑,通过位移协调条件建立两者的参数转换方程。平板和肋条均采用一系列点来离散,用移动最小二乘法建立的形函数来分别描述两者的位移场,再分别通过最小势能原理和Hamilton原理导出弹性地基的静力弯曲和弯曲自由振动控制方程,最后采用完全转换法处理边界条件。以一系列不同基床系数、荷载、边界、肋条布置方式的弹性地基圆形加肋板为例,研究所提出方法的收敛性和稳定性,并将计算结果与有限元、文献结果对比。研究表明该方法可以有效分析弹性地基圆形加肋板线性弯曲的静力和自由振动问题,且肋条位置改变时,可避免网格重构。     

波纹夹层板线性弯曲分析的无网格伽辽金法

提出了一种求解波纹夹层板结构线性弯曲问题的无网格模型。将波纹夹层板看成两侧平板和中间波纹板核的复合结构,用正交各向异性板等效近似波纹板核。先基于一阶剪切变形理论,由无网格伽辽金法建立各板的刚度方程,再通过位移协调条件将各板刚度方程叠加,以得到整体刚度方程。采用全转换法处理位移边界。算例表明：该文所提出的无网格模型分析波...     

改进的移动最小二乘插值法研究

本文首先从内积的角度给出了移动最小二乘逼近法的新的推导方法,然后对Lancaster等提出的移动最小二乘插值法进行了重新推导,取在插值节点奇异的权函数,并对基函数进行部分正交化,建立了改进的移动最小二乘插值法,并证明了其形函数的插值性质。本文提出的改进移动最小二乘插值法的公式比Lancaster的公式更为简单,并可提高形函数的计算效率。本文为工程问题的插值型无网格方法提供了建立形函数的基本方法。     

DSC‐Ritz method for the free vibration analysis of Mindlin plates

This paper introduces a novel method for the free vibration analysis of Mindlin plates. The proposed method takes the advantage of both the local bases of the discrete singular convolution (DSC) algorithm and the pb‐2 Ritz boundary functions to arrive at a new approach, called DSC‐Ritz method. Two basis functions are constructed by using DSC delta sequence kernels of the positive type. The energy functional of the Mindlin plate is represented by the newly constructed basis functions and is minimized under the Ritz variational principle. Extensive numerical experiments are considered by different combinations of boundary conditions of Mindlin plates of rectangular and triangular shapes. The performance of the proposed method is carefully validated by convergence analysis. The frequency parameters agree very well with those in the literature. Numerical experiments indicate that the proposed DSC‐Ritz method is a very promising new method for vibration analysis of Mindlin plates. Copyright © 2004 John Wiley & Sons, Ltd.     

Application of a new differential quadrature methodology for free vibration analysis of plates

A new methodology is introduced in the differential quadrature (DQ) analysis of plate problems. The proposed approach is distinct from other DQ methods by employing the multiple boundary conditions in a different manner. For structural and plate problems, the methodology employs the displacement within the domain as the only degree of freedom, whereas along the boundaries the displacements as well as the second derivatives of the displacements with respect to the co‐ordinate variable normal to the boundary in the computational domain are considered as the degrees of freedom for the problem. Employing such a procedure would facilitate the boundary conditions to be implemented exactly and conveniently. In order to demonstrate the capability of the new methodology, all cases of free vibration analysis of rectangular isotropic plates, in which the conventional DQ methods have had some sort of difficulty to arrive at a converged or accurate solution, are carried out. Excellent convergence behaviour and accuracy in comparison with exact results and/or results obtained by other approximate methods were obtained. The analogous DQ formulation for a general rectangular plate is derived and for each individual boundary condition the general format for imposing the given conditions is devised. It must be emphasized that the computational efforts of this new methodology are not more than for the conventional differential quadrature methods. Copyright © 2002 John Wiley & Sons, Ltd.     

A meshless local radial point collocation method for free vibration analysis of laminated composite plates

In this paper, a meshless local radial point collocation method based on multiquadric radial basis function is proposed to analyze the free vibration of laminated composite plates. This method approximates the governing equations based on first-order shear deformation theory using the nodes in the support domain of any data center. Natural frequencies of the laminated composite plates with various boundary conditions, side-to-thickness ratios, and material properties are computed by present method. The choice of shape parameter, effect of dimensionless sizes of the support domain on accuracy, convergence characteristics are studied by several numerical examples. The results are compared with available published results which demonstrate the accuracy and efficiency of present method.     

热过屈曲正交异性圆(环)板的自由振动响应

基于vonKármán薄板几何非线性理论,建立了以中面位移为基本未知量的加热极正交异性圆板轴对称大挠度动力学控制方程。然后,将控制方程的响应分解为热过屈曲静态解和振动解两部分,并在小振幅振动假设下得到了板在热过屈曲静平衡构形附近自由振动的线性微分方程。最后,采用打靶法获得了板在热过屈曲前后的固有频率与升温参数之间的特征关系曲线。结果表明,周边面内约束板的前两阶固有频率在热屈曲前随着温度升高而降低,而一旦板进入过屈曲平衡状态,前两阶频率都随着升温而单调增加。     

Geometrically nonlinear static and free vibration analysis of functionally graded piezoelectric plates

In this paper, nonlinear static and free vibration analysis of functionally graded piezoelectric plates has been carried out using finite element method under different sets of mechanical and electrical loadings. The plate with functionally graded piezoelectric material (FGPM) is assumed to be graded through the thickness by a simple power law distribution in terms of the volume fractions of the constituents. Only the geometrical nonlinearity has been taken into account and electric potential is assumed to be quadratic across the FGPM plate thickness. The governing equations are obtained using potential energy and Hamilton’s principle that includes elastic and piezoelectric effects. The finite element model is derived based on constitutive equation of piezoelectric material accounting for coupling between elasticity and electric effect using higher order plate elements. The present finite element is modeled with displacement components and electric potential as nodal degrees of freedom. Results are presented for two constituent FGPM plate under different mechanical boundary conditions. Numerical results for PZT-4/PZT-5H plate are given in dimensionless graphical forms. Effects of material composition and boundary conditions on nonlinear response are also studied. The numerical results obtained by the present model are in good agreement with the available solutions reported in the literature.     

热环境中功能梯度材料圆板的自由振动

基于von Kaman经典板理论,建立了功能梯度材料圆板在升温场内的大挠度动力学控制方程.将控制方程的响应分解为热过屈曲静态解和振动解两部分,得到了功能梯度材料圆板在热过屈曲平衡构形附近小振幅线性自由振动的微分方程.采用打靶法同时求热过屈曲和振动问题的控制方程,得到了随温度载荷变化的热过屈曲平衡路径以及前三阶固有频率的数值解.分析和讨论了板的材料梯度参数、温度场分布参数、边界条件等因素对过屈曲变形和振动响应的影响.分析中考虑了功能梯度板的组份材料的物性参数对温度的依赖性.     

A new analysis of nonlinear free vibration behavior of bi-functionally graded sandwich plates using the p-version of the finite element method

Geometrically nonlinear vibration of bi-functionally graded material (FGM) sandwich plates has been carried out by the p-version of the finite element method (FEM). The bi-FGM sandwich plate is made up of two face-sheet layers of two different FGM and one layer of homogeneous core. The nonlinear equations of motion of bi-FGM sandwich plates are establish using the harmonic balance method and solved iteratively by the linearized updated mode method. The effects of amplitude vibration, mechanical properties, geometrical parameters, thickness ratio of bi-FGM layers, and volume fraction exponent on the nonlinear vibration behavior of bi-FGM sandwich plates are plotted and investigated.     

Static and free vibration analyses of rectangular plates by the new version of the differential quadrature element method

A new version of the differential quadrature method is presented in this paper to overcome the difficulty existing in the ordinary differential quadrature method for applying multi‐boundary conditions in two‐dimensional problems. Since the weighting coefficients of the first derivative are the same as for the ordinary differential quadrature method even with the introduction of multi‐degree‐of‐freedom at the boundary points, the method is easier to extend to two‐ or three‐dimensional problems. A new version of the differential quadrature plate element has been established for demonstration. The essential difference from the existing old version of the differential quadrature plate element is the way the weighting coefficients are determined. The methodology is worked out in detail and some numerical examples are given to show the efficiency of the present method. Copyright © 2004 John Wiley & Sons, Ltd.