功能梯度开孔矩形板的动力特性解

对于功能梯度平板结构,采用与矩形板两对边边界条件相应的梁函数组合级数来求解开孔板动力特性问题,得到板件各阶固有频率与振型解的一般表达式,适用于具有任意孔洞的四边为任意简单（包括36种）边界条件的功能梯度矩形板动力特性分析,为各类功能梯度开孔板件的动力计算与设计打下理论基础。     

复杂形状功能梯度板件的三维动力特性分析

从细观力学角度出发根据材料细观组分分布对具有不同复杂形状功能梯度材料构件进行三维动力特性分析,并相应给出其三维固有频率及其基频对应的位移振型和应力振型沿厚度方向的三维分布。结果发现对同样材料细观组分分布的不同功能梯度结构,其固有频率和相应的振型分布均有很大差异。此结果为建立专门的功能梯度板壳理论提供定量的资料依据。     

功能梯度板的振动功率流特性分析

根据功能梯度复合材料矩形板的基本动力方程,基于模态叠加法求出简谐激励载荷作用下功能梯度板横向振动位移,结合结构振动功率流方程,研究功能梯度材料矩形板的振动及输入和传播功率流特性。算例中,首先计算功能梯度板固有频率,并与数值解进行对比分析,验证了算法的准确性。然后研究了功能梯度板输入功率流特性,讨论了不同梯度指数对输入功率流特性的影响。并通过可视化方法计算得到了功率流在板中的传播特性,通过功率流矢量图和流线图描述了功能梯度板。     

混合边界矩形板的自由振动分析

应用一块板的一般解析解来求解混合边界矩形板的自由振动问题。一块板的一般解析解适用于求解任意边界条件矩形板的振动问题。混合边界矩形板的求解过程是将整块板分解为若干块板,每块板仅有均匀的边界,每两块相连的板边则具有连续性条件。利用全部边界条件和连续性条件即可求解各阶固有频率和振型。对几种具有简支边、平夹边或自由边混合边界的板做了计算,并与其它文献结果进行了对比。     

沿板平面变异功能梯度板件的三维动力特性

功能梯度材料具有复杂的细部结构,其内部构造远比匀质材料复杂,因此其构件动力分析很难求得其解析解。文中建议一种新颖的功能梯度构件动力分析的细观元法。细观力学研究的目的在于建立材料的宏观性能同其组分材料性能及细观结构之间的定量关系,它可揭示不同的材料组合具有不同的宏观性能的内在机制。目前功能梯度板件分析只能处理材料特性沿厚度方向梯度变化,而细观元法则直接从制备时给定的材料组分分布出发计算构件宏观三维动力特性,并给出了沿板平面方向材料特性梯度变化的功能梯度板件三维固有频率及振型的三维分布。     

具有中等组分不同网状结构功能梯度构件的三维动力特性分析

功能梯度材料具有复杂的细部结构,其内部构造远比匀质材料复杂,因此其构件动力分析很难求得其解析解。该文建议一种新颖的功能梯度构件动力分析的细观元法。细观力学研究的目的在于建立材料的宏观性能同其组分材料性能及细观结构之间的定量关系,它可揭示不同的材料组合具有不同的宏观性能的内在机制。此法可实现材料细观结构到构件宏观响应的直接过渡分析,而计算单元与自由度又等同一般常规有限元,却使得组成功能梯度材料构件的各种材料细观构造得到反映。通过细观元技术,对具有中等组分不同网状结构功能梯度构件进行三维动力特性分析,并给出其三维固有频率及振型的三维分布,特别是给出了不同网格结构功能梯度板件应力振型的平面等值线图差异。结果表明:不同细观网格结构对功能梯度材料结构三维动力响应有较明显影响。     

弹性边界约束矩形板的振动特性分析：理论、有限元和实验

提出一种有效的理论方法研究弹性边界约束矩形板的振动特性,并设计实验测试不同边界矩形板的固有频率。矩形板的弹性边界约束采用一系列的均布线性弹簧模拟,用特征正交多项式来表示矩形板的位移容许函数,并采用瑞利?里茨法获得弹性边界约束矩形板的固有频率和固有振型。通过改变边界弹簧的刚度即可模拟矩形板不同的边界条件,提高计算效率。基于理论方法计算获得结构固有频率并和有限元及实验结果进行对比,验证所提理论方法的正确性。此外,通过实验测试的方法分析弹性?简支、弹性?固支等不同边界组合条件下矩形板的振动特性,分析调整不同边界弹簧刚度对矩形板振动特性的影响。     

变刚度Winkler地基上受压非均质矩形板的自由振动与屈曲特性

基于经典薄板理论,利用Hamilton原理建立变刚度Winkler地基上受压非均质矩形板自由振动与屈曲问题的控制微分方程并进行无量纲化。通过一种半解析方法-微分变换法(DTM)研究其无量纲固有频率和屈曲临界载荷特性。采用DTM将其无量纲控制微分方程及边界条件变换为等价的代数方程,得到含有频率和屈曲载荷的特征方程。将该问题退化为面内变刚度矩形板情形,其DTM解与精确解进行对比,结果表明DTM具有非常高的精度和很强的适用性。计算出在不同边界条件下屈曲临界载荷并分析地基刚度变化参数、弹性模量变化参数、密度变化参数、面内载荷和长宽比对矩形板无量纲固有频率的影响,给出了不同边界条件下变刚度Winkler地基上受压非均质矩形板的前三阶振型。     

矩形薄板自由振动的一般解析解

本文求得了矩形薄板弹性横向自由振动位型函数微分方程的一般解。可以求解任意边界矩形薄板的固有频率。以四边固定矩形板为例求解了板的基频及其位型。     

转动弹性支承矩形板自由振动的一般解析解法

转动弹性支承边与简支边,平夹边均有不同,一方面板边均能防止上下移动,即其挠度均为零。而转动弹性支承边,由于在边界装有均匀分布的转动弹簧使边界弯矩受到斜度的制约而与板边的斜度成正比。采用矩形薄板自由振动横向位移函数的微分方程建立了一般性的解析解,该一般解包括三角函数和双曲线函数组成的解,它能满足4个边为任意边界条件的问题。解中的待定常数可由4边的边界条件来确定,由此得出的齐次线性代数方程系数矩阵行列式等于零可以精确地求得各阶固有频率及其振型。由于矩形板对中间轴具有对称性,利用对称和反对称条件可使求解大大简化。对于正方形板还可利用对角线的对称性而毫无遗漏地找出最低的各阶频率及其振型。以四边均为转动弹性支承方板为例进行计算和讨论。     

温度影响下Winkler-Pasternak弹性地基上多孔FGM矩形板的自由振动分析

基于经典薄板理论和Hamilton原理研究温度影响下Winkler-Pasternak弹性地基上多孔功能梯度材料(FGM)矩形板的自由振动特性。采用Voigt混合幂率模型和孔隙任意分布模型来表征多孔FGM矩形板的材料属性,并考虑多孔FGM矩形板内部均匀温升和材料具有温度依赖特性;应用物理中面推导弹性地基上多孔FGM矩形板自由振动的控制微分方程并进行无量纲化;采用微分变换法(DTM)对无量纲控制微分方程及其边界条件进行变换,引入典型的六种边界在MATLAB统一编程且保证计算精度一致,经过迭代收敛,求解出无量纲固有频率;通过算例研究了边界条件、梯度指数、升温、孔隙率、长宽比、边厚比、无量纲弹性刚度系数和无量纲剪切刚度系数对多孔FGM矩形板振动特性的影响。     

A meshfree radial point interpolation method for analysis of functionally graded material (FGM) plates

A meshfree model is presented for the static and dynamic analyses of functionally graded material (FGM) plates based on the radial point interpolation method (PIM). In the present method, the mid-plane of an FGM plate is represented by a set of distributed nodes while the material properties in its thickness direction are computed analytically to take into account their continuous variations from one surface to another. Several examples are successfully analyzed for static deflections, natural frequencies and dynamic responses of FGM plates with different volume fraction exponents and boundary conditions. The convergence rate and accuracy are studied and compared with the finite element method (FEM). The effects of the constituent fraction exponent on static deflection as well as natural frequency are also investigated in detail using different FGM models. Based on the current material gradient, it is found that as the volume fraction exponent increases, the mechanical characteristics of the FGM plate approach those of the pure metal plate blended in the FGM.     

An RMVT-Based Finite Rectangular Prism Method for the 3D Analysis of Sandwich FGM Plates with Various Boundary Conditions

A Reissner's mixed variational theorem (RMVT)-based finite rectangular prism method (FRPM) is developed for the three-dimensional (3D) analysis of sandwich functionally graded material (FGM) plates subjected to mechanical loads, in which the edge conditions of the plates are such that one pair of opposite edges is simply supported and the other pair may be combinations of free, clamped or simply supported edges. The sandwich FGM plate considered consists of two thin and stiff homogeneous material face sheets combined with an embedded thick and soft FGM core, the material properties of which are assumed to obey the powerlaw distributions of the volume fractions of the constituents. In this formulation, the plate is divided into a number of finite rectangular prisms, in which the trigonometric functions and Lagrange polynomials are used to interpolate the y-direction and x-ζ plane variations of the primary field variables of each individual prism, respectively. Because an h-refinement process is adopted to yield the convergent solutions in this analysis, the prism-wise either linear or quadratic function distribution through the x-ζ plane is assumed for the related field variables. A unified formulation of these FRPMs with freely-chosen orders for assorted field variables is presented. It is shown that these quadratic FRPM solutions of simply supported, multilayered composite plates and sandwich FGM ones are in excellent agreement with the exact 3D solutions available in the literature, and those of multilayered composite plates with various boundary conditions closely agree with the solutions obtained using the ANSYS commercial software.     

具有中间支承的正交异性矩形板自由振动分析

应用一般解析解来求解具有中间支承的正交异性矩形板的自由振动问题。一般解析解能求解任意边界条件矩形板的振动问题。求解过程是将整块板看成是沿中间支承分开的两块板。沿支承边两块板的挠度均等于零;斜度和弯矩均相等。由全部边界条件和连续性条件可以求解各阶频率和振型。对几种具有简支边、平夹边或自由边的板进行了计算。     

复合材料层合板在非保守力作用下的动力稳定性

利用弹性非保守系统自激振动的拟固有频率变分原理,推导出复合材料矩形板受非保守随从力作用的变分方程,进而导出此问题的有限元基本方程及求解临界力和固有频率的特征方程。用载荷增量法计算了在多种边界条件下不同边长比的复合材料矩形板在面内受随从力作用的临界载荷,分析了不同角铺设方向及两种材料组合板的临界载荷。计算结果表明,边界条件对层合板的动力稳定性有较大影响,复合材料层合板的角铺设方向对临界载荷有较大影响。     

Levy Solution for Buckling Analysis of Functionally Graded Rectangular Plates

In this article, an analytical method for buckling analysis of thin functionally graded (FG) rectangular plates is presented. It is assumed that the material properties of the plate vary through the thickness of the plate as a power function. Based on the classical plate theory (Kirchhoff theory), the governing equations are obtained for functionally graded rectangular plates using the principle of minimum total potential energy. The resulting equations are decoupled and solved for rectangular plate with different loading conditions. It is assumed that the plate is simply supported along two opposite edges and has arbitrary boundary conditions along the other edges. The critical buckling loads are presented for a rectangular plate with different boundary conditions, various powers of FGM and some aspect ratios.     

一边支承三边自由矩形板振形曲线及其正交性

本文提出主振方向排序法的思想 ,建立了一边支承三边自由矩形板统一的振形函数表达式。该振形曲线基本符合板边界条件所限定的变形曲线形态 ,可以满足全部边界条件 ,又具有振形的正交性。本文阐明了主振方向排序法的物理含义 ,推导了 2种矩形板自由振动频率方程 ,计算了各 2 5个自振频率及相应的振形。     

具有局部分层的对称铺设层合板在非保守力作用下的屈曲分析

利用弹性非保守系统自激振动的拟固有频率变分原理,推导出复合材料矩形板受非保守随从力作用的变分方程,进而导出复合材料层合板含分层损伤的有限元基本方程及求解临界荷载力和固有频率的特征方程。用载荷增量法计算了不同边长比的复合材料矩形板在面内受随从力作用且含有分层的临界载荷,分析了不同角铺设方向对临界载荷的影响。分析表明,分层对临界载荷有一定影响,复合材料层合板的角铺设方向对临界载荷有较大影响。     

Free vibration analysis of thin isotropic and anisotropic rectangular plates by the discrete singular convolution algorithm

This paper presents the free vibration analysis of thin isotropic and anisotropic rectangular plates with various boundary conditions by using the discrete singular convolution (DSC) algorithm. Based on Taylor's series expansion, a unique scheme is proposed to handle various boundary conditions, including the simply supported (S), clamped (C) and free (F) edge. To validate the proposed method, the non‐dimensional frequency parameters of isotropic, orthotropic and angle‐ply symmetric laminated rectangular plates with various combinations of boundary conditions are obtained by using the DSC algorithm and compared with the analytical and/or numerical solutions. Comparisons reveal that the proposed method can handle the zero bending moment and zero shear force conditions for the isotropic as well as anisotropic plates. The proposed method provides an alternative way for applying the simply supported boundary conditions in applications of the DSC algorithm to plate structures. This investigation extends the application range of the DSC algorithm to vibration analysis of anisotropic plates with various combinations of boundary conditions. Copyright © 2010 John Wiley & Sons, Ltd.