轴对称von Korman位移型方程的打靶法求解

本文采用常微分方程两点边值问题的打靶法，建立了圆薄板轴对称大挠度弯曲ｖｏｎＫáｒｍáｎ位移型方程的自动求解过程．作为例子，分析了圆薄板在均布横向截荷作用下的非线性弯曲问题，给出了载荷参数大范围变化的解曲线     

轴对称von Korman位移型方程的打靶法求解

本文采用常微分方程两点边值问题的打靶法，建立了圆薄板轴对称大挠度弯曲ｖｏｎＫáｒｍáｎ位移型方程的自动求解过程．作为例子，分析了圆薄板在均布横向截荷作用下的非线性弯曲问题，给出了载荷参数大范围变化的解曲线     

损伤弹性薄板的弯曲

通过损伤弹性薄板的变分方法,推导了损伤弹性薄板弯曲的运动控制方程.选取满足边界条件的挠度函数,采用Ritz法和Galerkin法,将原问题转化为线性方程组的求解.通过算例分析,得到y=b/2处挠度和损伤随x的变化曲线,结果表明损伤薄板中任一点的位移总是大于无损薄板中的位移.     

圆薄板轴对称弯曲问题的基本方程讨论

首先通过级数展开和求极限运算的方法,确定了等厚度圆薄板轴对称大/小挠度问题的弯曲微分方程在圆心处的表达式.其次,根据轴对称问题的特点,推导出了实心圆薄板在圆心处应满足边界条件的数学表达式,使圆薄板轴对称大/小挠度问题的弯曲微分方程应满足的边界条件达到了应有的数量.本文工作进一步完善了圆薄板轴对称弯曲问题的微分方程形式和边界条件,从而使我们可以利用成熟的微分方程数值解法,对具有较复杂载荷的实心圆薄板轴对称弯曲微分方程进行数值求解.     

弹性圆板的热过屈曲

基于精确的圆薄板轴对称大挠度变形几何方程，建立了均匀加热圆板轴对称热弹性屈曲问题位移形式的控制方程，采用打靶法和解析延拓法获得了连续依赖于温度载荷的圆板过屈曲状态解，给出了相应的数值结果。     

轴对称圆薄板大挠度微分方程的数值分析方法

根据轴对称问题的特点,利用级数展开和求极限法则,证明了轴对称大挠度圆薄板在圆心处应满足的边界条件,并以圆薄板轴对称大挠度弯曲变形微分方程为基础,建立了圆心处非奇异的轴对称大挠度圆板弯曲微分方程,从而可以方便地利用现有的常微分方程数值求解方法(如变步长龙格-库塔法)对实心圆板的轴对称问题进行数值求解,又不必像摄动法那样推导复杂的公式。在数值求解轴对称圆板大挠度弯曲变形微分方程时,将非线性微分方程的求解主要归结为迭代求解圆心处三个未知边界条件的问题,即圆心处的径向膜力、圆心处的挠度、圆心处挠度的二阶导数,并提出了相应的求解方法。实例中,对于圆薄板受均布横向荷载的问题,分析了周边固支边界条件下的非线性弯曲问题,给出了中心挠度参数大范围变化时的荷载和部分边界值变化曲线,并与经典摄动解进行了对比。对比结果可见,本文方法和摄动法的解非常接近,在量纲归一化中心挠度不超过4.0时,两种方法解的相对误差均小于5.0%。另外,本文还分析了与挠度有关的液体压力作用下和集中荷载作用下周边固支圆板的非线性弯曲问题。通过算例可见:本文方法可以灵活处理不同的荷载问题;对于不同的问题,计算过程相似,不必推导复杂的计算公式,计算精度容易控制。     

热力联合作用下不同材料参数圆薄板的大挠度弯曲

采用由Berger方法和伽辽金方法导出的圆板大挠度弯曲的挠度解析解和ANSYS程序，对均布横向力和均匀温升作用下板中心挠度wc随温度升及横向力的变化规律进行了解析和有限元计算，讨论了板材弹性模量和热膨胀系数不同时，板中温度膜力NT和材料参数（弹性模量E，泊松比μ和热膨胀系数σ）的温度相关性对板大挠度弯曲变形的不同影响规律及温升与横向力联合对圆板大挠度弯曲的不同作用机制。     

正交各向异性圆薄板非线性弯曲

本文取板中点挠度为摄动参数,采用Von—Kármán型大挠度方程组,分析了均布载荷作用下边缘可移夹支正交各向异性圆薄扳的非线性弯曲问题。本文特例与各向同性圆薄板结果很吻合。文中还讨论了有关参数对板挠度和内力的影响,所得结果可供工程应用参考。     

弹性梁式薄板在横向绕流中的大变形

采用相容拉格朗日-欧拉(ULE)法,给出了弹性薄板理想流体横向绕流条件下变形与应力的理论算法,其中:对固体采用拉格朗日法;对流体采用欧拉法;对相互接触面采用拉格朗日法和欧拉法.建立了不问断横向绕流条件下弹性梁式薄板的大弯曲变形的非线性微分方程.求解该方程时,将纵向位移分量和曲率的改变量用挠度表示.通过具体算例分析了各参数对悬臂梁式薄板挠度、纵向位移及应力大小的影响.理论解与数值解进行比较,验证了理论解的可靠性.     

薄板小挠度问题刚度随机时的随机解析分析

将二维随机场视为可分空间，对薄板小挠度问题进行随机分析，给出当薄板刚度随机时板上各点位移数字特征的解析解．为薄板小挠度问题的随机分析提供了准确解，也可用于检验其它各种近似分析方法的准确程度．最后以四边简支薄板为例，对其位移的统计特性进行了计算．     

Buckling of imperfect functionally graded cylindrical shells under axial compression

Buckling behaviors of axially compressed functionally graded cylindrical shells with geometrical imperfections are investigated in this paper using Donnell shell theory and the nonlinear strain-displacement relations of large deformation. The analysis is based on the nonlinear prebuckling consistent theory. Both the prebuckling effects and the temperature-dependent material properties are taken into account. The buckling condition for imperfect functionally graded cylindrical shells is obtained by using the Galerkin method. Numerical results show various effects of imperfection, structural type, power law exponent, temperature and dimensional parameters on buckling. The present theoretical results are verified by those in literature.     

Bénard-Marangoni convection in a rotating fluid with and without surface deformation

This paper deals with Bénard-Marangoni convection in a thin horizontal layer heated from below and rotating uniformly about a vertical axis. The analysis is linear and its objective is to determine the critical temperature drop and the critical wavenumber at the onset of convection. The lower surface of the layer is in contact with an uniformly heated rigid plate and the upper face is deformed and subjected to a temperature-dependent surface tension. Exchange of stability and Boussinesq's approximation are taken for granted. It is shown that rotation has a stabilizing effect while surface deflection plays a stabilizing role at large angular velocity and has an opposite influence at low angular velocity. By increasing the angular velocity, one reinforces the stability, whatever the surface deformation.     

Stochastic nonlinear bending response of laminated composite plates with system randomness under lateral pressure and thermal loading

In this paper, the effect of sensitivity of randomness in system parameters on the nonlinear transverse central deflection response of laminated composite plates subjected to transverse uniform lateral pressure and thermal loading is examined. System parameters such as the lamina material properties, expansion of thermal coefficients, lamina plate thickness and lateral load are modelled as basic random variables. A higher order shear deformation theory in the von-Karman sense is used to model the system behavior of the laminated plate. A direct iterative-based C ⁰ nonlinear finite element method in conjunction with the first-order perturbation technique developed by the authors is extended for thermal problem to obtain the second-order response statistics, i.e., mean and variance of the nonlinear transverse deflection of the plate. Typical numerical results of composite plates with temperature independent and dependent material properties subjected to uniform temperature and combination of uniform and transverse temperature are obtained for various combinations of geometric parameters, uniform lateral pressures, staking sequences and boundary conditions. The results have been compared with those available in the literature and an independent Monte Carlo simulation.     

Resonant flexural vibrations and dissipative heating of a piezoceramic ring plate with nonuniformly electroded surfaces

The forced flexural vibrations and dissipative heating of a bimorph ring plate are studied. The plate is made of viscoelastic piezoceramics and is polarized across the thickness. The outer surfaces of the plate are nonuniformly electroded, and harmonic electric excitation is applied to the electrodes. The viscoelastic behavior of the material is described using the concept of temperature-dependent complex moduli. The coupled nonlinear problem of thermoviscoelasticity is solved by time iteration using, at each iteration, the discrete-orthogonalization method to integrate the mechanics equations and the explicit finite-difference method to solve the heat-conduction equation with a nonlinear heat source. Numerical calculations demonstrate that by changing the size of the ring electrode we can influence the natural frequency, stress and displacement distributions, dissipative-heating temperature, and amplitude-and temperature-frequency characteristics. With certain boundary conditions, there is an optimal electrode configuration that produces deflections of maximum amplitudes when an electric excitation is applied __________ Translated from Prikladnaya Mekhanika, Vol. 42, No. 3, pp. 102–109, March 2006.     

Kantorovich solution for the problem of bending of a ladder plate

Based on the Kantorovich approximation solution for a rectangular plate in bending, this paper deals with the solutions for the ladder plate with various boundary conditions. The deflection of the plate is expressed in a first-order displacement function w(x,y)=u(x,y)v(y) where the u(x,y) in x direction is the generalized beam function. By making use of the principle of least potential energy, the variable coefficients differential equations for v(y) may be established. By solving is, these differential eugations and making use of the boundary conditions, the accurate solutions of v(y) in y direction may be obtained. Then the displacement function w(x,y) is the solution for the problem of the bending of the ladder plate with a better degree of approximation.     

NONLINEAR BUCKLING BEHAVIOR OF DAMAGED COMPOSITE SANDWICH PLATES CONSIDERING THE EFFECT OF TEMPERATURE-DEPENDENT THERMAL AND MECHANICAL PROPERTIES

On the basis of the first-order shear deformation plate theory and the zig-zag deformation assumption, an incremental finite element formulation for nonlinear buckling analysis of the composite sandwich plate is deduced and the temperature-dependent thermal and mechanical properties of composite is considered. A finite element method for thermal or thermo-mechanical coupling nonlinear buckling analysis of the composite sandwich plate with an interfacial crack damage between face and core is also developed. Numerical results and discussions concerning some typical examples show that the effects of the variation of the thermal and mechanical properties with temperature, external compressive loading, size of the damage zone and ply angle of the faces on the thermal buckling behavior are significant. Project supported by the National Natural Science Foundation of China (No. 59975013).     

Bending analyses of 1D orthorhombic quasicrystal plates

The meshless Petrov–Galerkin method (MLPG) is applied to plate bending analysis in 1D orthorhombic quasicrystals (QCs) under static and transient dynamic loads. The Bak and elasto-hydrodynamic models are applied for phason governing equation in the elastodynamic case. The phason displacement for the orthorhombic QC in the first-order shear deformation plate theory depends only on the in-plane coordinates on the mean plate surface. Nodal points are randomly distributed over the mean surface of the considered plate. Each node is the center of a circle surrounding this node. The coupled governing partial differential equations are satisfied in a weak-form on small fictitious subdomains. The spatial variations of the phonon and phason displacements are approximated by the moving least-squares (MLS) scheme. After performing the spatial MLS approximation, a system of ordinary differential equations (ODEs) for nodal unknowns is obtained. The system of the ODEs of the second order is solved by the Houbolt finite-difference scheme. Our numerical examples demonstrate clearly the effect of the coupling parameter on both static and dynamic phonon/phason deflections.     

黏弹性板的大挠度蠕变屈曲

研究了具有初始小挠度受轴向压载黏弹性板的蠕变屈曲问题，在建立控制方程时，利用了von Karman非线性应变-位移关系，并考虑了初始挠度，用标准线性固体模型描述材料的黏弹性特性，在求解非线性积分方程时，利用梯形公式计算记忆积分式，将非线性积分方程化为非线性代数方程进行数值求解，得到了结构的蠕变变形过程，又将问题退化到小挠度情况进行研究，得到了挠度随时间扩展的解析解，分析了瞬时失稳临界载荷、持久临界载荷的物理意义，讨论了考虑几何非线性对黏弹性板蠕变屈曲的影响。     

Thermomechanical Postbuckling of Imperfect Moderately Thick Plates on Nonlinear Elastic Foundations*

ABSTRACT

A postbuckling analysis is presented for a moderately thick rectangular plate subjected to combined axial compression and uniform temperature loading, and resting on a softening nonlinear elastic foundation. The cases of (1) thermal postbuckling of initially compressed plates and (2) compressive post-buckling of initially heated plates are considered. The initial geometrical imperfections of the plates are taken into account. Formulations are based on Reissner-Mindlin plate theory, considering first-order shear deformation effects, and including plate-foundation interaction and thermal effects. The analysis uses a deflection-type perturbation technique to determine buckling loads and postbuckling equilibrium paths. Numerical examples include the performance of perfect and imperfect, moderately thick plates resting on softening nonlinear elastic foundations. Typical results are presented in dimensionless graphical form.