弹性半空间地基上预应力中厚矩形板的弯曲

基于Reissner-Mindlin一阶剪切变形理论,讨论在预加面内机械荷载或预加温度场作用下,弹性半空间地基上四边自由中厚矩形板的弯曲问题。把地基看作三维弹性半空间体,考虑地基变形的衰减。用一组数学上完备的二元多项式作为位形函数,采用pb-2 Rayleigh-Ritz法求得四边自由中厚矩形板的挠度和弯矩,并讨论了初应力对板的挠度和弯矩的影响。     

弹性半空间地基上预应力中厚矩形板的横向振动

基于Reissner-Mindlin一阶剪切变形理论,讨论在预加面内机械荷载作用下,弹性半空间地基上四边自由中厚矩形板的横向振动问题。把地基看作三维弹性半空间体,考虑地基变形的衰减。用一组数学上完备的二元多项式作为位形函数,采用pb-2 Rayleigh-Ritz法求得四边自由中厚矩形板的自振频率和在横向简谐荷载作用下的动力响应。讨论了板的长宽比、宽厚比及弹性地基和板的相对刚度对板的自振频率的影响。     

面内预应力功能梯度材料矩形板的横向弯曲

功能梯度材料（FGM)是一类具有广阔应用前景的新型复合材料。本文考虑材料物性参数随坐标和温度变化的特性，研究横向荷载和面内预加荷载作用下FGM矩形板在各种边界条件下的弯曲问题。给出了基于一维微分求积格式的Galerkin技术的半解析方法，并以ZrO2/Ti-6Al-4V板为例考察了材料组分，温度相关性，面内预加荷载，边界约束条件等对FGM板弯曲行为的影响。结果表明，FGM板的弯曲变形介于各向同性陶瓷板与各向同性金属板之间，且随板抗弯刚度的增大而逐步减小，在高温下条件下必须考虑材料物性和温度的相关性。     

功能梯度材料矩形中厚板的受压/热致屈曲

考虑材料组份沿板厚度方向按幂律变化的情形,研究了温度均匀变化时固支功能梯度材料(FGM)矩形中厚板的受压屈曲、热致屈曲和考虑热／机械预应力时的屈曲问题,给出了基于Reddy高阶剪切理论研究板屈曲荷载和屈曲临界温度的半解析数值方法．并以Si3N4／SUS304板为例考虑了材料组份、预加应力、横向剪切变形及面内位移约束条件等对FGM板屈曲承载能力的影响．     

两相邻边固定两相邻边自由的矩形板

本文给出两相邻边自由、两相邻边固定的矩形板的精确解.所解的两个问题为:均布荷重作用及有一集中力作用在自由角点.本文对一正方形板作了数字计算,其中包括自由角点的挠度,沿自由边的挠度以及沿固定边的弯矩.板的其他各点的挠度、弯矩、扭矩和剪力均可由叠加法得到.这种方法,可以很容易推广到沿自由边作用任何荷载或包括有扭矩作用的情况.     

考虑横向拉伸影响的FGM夹层板动不稳定性分析

以受多种形式面内载荷作用下的功能梯度夹层矩形板为研究对象,夹层板的功能梯度层组分材料沿厚度方向按幂律分布,考虑组分材料物性参数的温度相关性.研究中所用的位移场在Reddy高阶剪切变形理论基础上考虑了横向拉伸的影响.利用能量原理和Galerkin法得到四边简支功能梯度材料夹层矩形板的动力学模型.运用Bolotin法求得了...     

双参数地基圆(环)形板的边界剪力及其力学响应

针对目前考量双参数地基上圆形或环形板边界剪力中存在的一些不足,应用Hankel变换法求得双参数地基的解析解,研究了任意环状线荷载作用下双参数地基的挠度、转角及地基反力间的关系。指出双参数地基在线荷载处的转角差与表示横向联系的地基参数之乘积等于线荷载集度;环内的分布荷载仅影响环内侧转角,而环外分布荷载也仅影响环外侧转角;进而又给出了适用于双参数地基圆形或环形板的内/外边界剪力的简明表达式。最后分别给出了双参数地基上自由边界圆形薄板中点承受集中力、圆形均布荷载作用时边界剪力对板中点挠度、弯矩的影响规律;双参数地基边界剪力对板挠度、弯矩有较明显影响,尤其是板的相对半径ρ_04或是荷载距板边界较近时这种影响更为明显。     

弹性地基上四边自由矩形厚板非线性大挠度弯曲

基于Ｒｅｉｓｓｎｅｒ－Ｍｉｎｄｌｉｎ一阶剪切变形板理论,采用摄动－Ｇａｌｅｒｋｉｎ混合法,给出双参数弹性地基上四边自由矩形中厚板在对称分布局部荷载作用下的大挠度弯曲渐近解,满足全部自由边界条件和控制方程,同时讨论弹性地基刚度系数对自由矩形厚板大挠度弯曲的影响。     

考虑接触效应的具脱层轴对称层合圆板的非线性动力响应

基于von Karman板理论,利用三分区模型,建立了在面内压力和横向荷载联合作用下具脱层的轴对称正交层合圆板的非线性运动微分方程,其中,考虑了横向剪切效应和脱层接触效应.在此基础上,利用正交配点法进行了求解,并着重讨论了脱层之间的接触效应对结构非线性动力响应的影响.     

功能梯度压电材料板的有限元解

本文利用变分原理和功能梯度压电材料的本构关系、几何关系、板的边界条件等,推导出功能梯度板的有限元方程。其中考虑了横向剪切变形的影响,采用了板变形问题的Mindlin假设,板内电势设为声：Ф=ψ0（x,y）＋ψ1（x,y）z＋ψ2（x,y）z^2＋ψ1（x,y）g（z）,并假设材料的力学和电学常数均沿板厚度z方向按同一函数规律K=K^0f（z）变化,其中f（z）为任意的函数形式。为了验证本文方法的正确性,以功能梯度压电材料正方形板为例,使板所受的机械荷载和电荷载以及函数f（z）的形式与参考文献中所给出的相同,利用本文中提出有限元法计算了功能梯度板的电势和位移,所得结果与参考文献中的几乎一致。最后用此法计算四边简支,接地,线性梯度的PZT-4正方形板受均布荷载作用下的挠度和电势分布。     

热/机械载荷下功能梯度材料矩形厚板的弯曲行为

采用Reddy高阶剪切板理论，考虑材料物性参数随坐标和温度变化的特性，研究在均匀变化的温度场内功能梯度材料矩形板在面内与横向载荷共同作用下的横向弯曲问题，基于一维DQ法和Galerkin技术，给出了一对边固支，另对边任意约束时板弯曲问题的半解析解，以Si3N4/SUS304板为例考察了材料组份，温度场，面内载荷及边界约束条件等对功能梯度材料板弯曲行为的影响。     

功能梯度中厚圆/环板轴对称弯曲问题的解析解

基于一阶剪切变形板理论，导出了热/机载荷作用下，位移形式的功能梯度 中厚圆/环板轴对称弯曲问题的控制方程，获得了问题的位移和内力的一般解析解. 作为特 例，分别研究了边缘径向固定和可动的夹紧和简支的4种实心功能梯度圆板，给出了它们的 解，并分析了热/机载荷作用下解的形态，讨论了横向剪切变形、材料梯度常数和边界条件， 对板的轴对称弯曲行为的影响.     

Kármán-type equations for a higher-order shear deformation plate theory and its use in the thermal postbuckling analysis

Kármán-type nonlinear large deflection equations are derived occnrding to the Reddy’s higher-order shear deformation plate theory and used in the thermal postbuckling analysis The effects of initial geometric imperfections of the plate areincluded in the present study which also includes th thermal effects.Simply supported,symmetric cross-ply laminated plates subjected to uniform or nomuniform parabolictemperature distribution are considered. The analysis uses a mixed GalerkinGolerkinperlurbation technique to determine thermal buckling louds and postbucklingequilibrium paths.The effects played by transverse shear deformation plate aspeclraio, total number of plies thermal load ratio and initial geometric imperfections arealso studied.     

A new trigonometric shear deformation theory for isotropic,laminated composite and sandwich plates

A new trigonometric shear deformation theory for isotropic and composite laminated and sandwich plates, is developed. The new displacement field depends on a parameter “m”, whose value is determined so as to give results closest to the 3D elasticity bending solutions. The theory accounts for adequate distribution of the transverse shear strains through the plate thickness and tangential stress-free boundary conditions on the plate boundary surface, thus a shear correction factor is not required. Plate governing equations and boundary conditions are derived by employing the principle of virtual work. The Navier-type exact solutions for static bending analysis are presented for sinusoidally and uniformly distributed loads. The accuracy of the present theory is ascertained by comparing it with various available results in the literature. The results show that the present model performs as good as the Reddy’s and Touratier’s shear deformation theories for analyzing the static behavior of isotropic and composite laminated and sandwich plates.     

Postbuckling of FGM plates with piezoelectric actuators under thermo-electro-mechanical loadings

A postbuckling analysis is presented for a simply supported, shear deformable functionally graded plate with piezoelectric actuators subjected to the combined action of mechanical, electrical and thermal loads. The temperature field considered is assumed to be of uniform distribution over the plate surface and through the plate thickness and the electric field considered only has non-zero-valued component E_Z. The material properties of functionally graded materials (FGMs) are assumed to be graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents, and the material properties of both FGM and piezoelectric layers are assumed to be temperature-dependent. The governing equations are based on a higher order shear deformation plate theory that includes thermo-piezoelectric effects. The initial geometric imperfection of the plate is taken into account. Two cases of the in-plane boundary conditions are considered. A two step perturbation technique is employed to determine buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling behavior of perfect and imperfect, geometrically mid-plane symmetric FGM plates with fully covered or embedded piezoelectric actuators under different sets of thermal and electric loading conditions. The effects played by temperature rise, volume fraction distribution, applied voltage, the character of in-plane boundary conditions, as well as initial geometric imperfections are studied.     

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基于形状记忆合金Brinson一维热力学本构关系和von K\'{a}rm\'{a}n几何非线性薄板理论,研究了径向嵌入SMA丝复合材料加热圆板在横向均布 机械载荷作用下的弯曲响应, 获得了周边不可移简支和夹紧圆板的中心最大挠度与升温之间的关系曲线. 结果表明,形状 记忆合金丝在从马氏体向奥氏体的逆相变过程中所产生的相变回复力对板的弯曲变形具有明 显的调整作用. 通过嵌入SMA纤维丝和施加升温载荷可以主动而有效地调节受机 械载荷作用圆板的弯曲变形.     

轴对称热载作用厚板的热弹性运动效应分析

对板的上下表面存在一般温度边界条件的情况，解出了板表面受轴对称热辐射作用时，板内轴对称二维瞬态温度场的一般表达式；导出了厚板的热弯曲运动和热平面运动的位移型动力学方程，得出了板的挠度、转角和平面径向位移的无穷积分型公式；提出了一个求解弯曲波传播速度的方法；然后完成了一个代表性算例分析，给出了弯曲波传播规律的直观图象，得出了热加载和热卸载过程中，板内热弯曲波的时空变化特点；找出了剪切变形和旋转惯性对弯曲波传播速度的影响规律；最后，将理论结果与相应的实验结果进行了比较，两者吻合良好。     

Axisymmetric static and dynamics snap-through phenomena in a thermally postbuckled temperature-dependent FGM circular plate

Thermal postbuckling analysis and the axisymmetric static and dynamic snap-through phenomena due to static/sudden uniform lateral pressure in a thermally postbuckled functionally graded material circular plate are performed in this research. Plate is formulated using the first order shear deformation plate theory. Thermo-mechanical properties of the plate are assumed to be temperature dependent where dependency is described according to the higher order Touloukian representation. Two types of temperature loading are considered. Uniform temperature rise and heat conduction across the thickness direction. The one dimensional heat conduction equation in the thickness direction is obtained and discreted via the central finite difference method. The obtained system of equations is nonlinear since the thermal conductivity itself is a function of the unknown nodal temperatures. Using the von-Kármán assumptions, the governing equations of the plate are obtained in a matrix representation with the aid of the conventional Ritz method whose shape functions are developed using the Gram-Schmidt process. At first thermal postbuckling analysis is performed which is a nonlinear problem with respect to both temperature and displacements. Afterwards, response of the bulged thermally postbuckled plate is obtained under the static and dynamic uniform pressure. Snap-through phenomenon may be observed in both static and dynamic loading cases, due to the immovability of the edge of the plate and the initial deflection caused by postbuckling deflection. To capture the snapping phenomenon and trace the path beyond the limit loads, cylindrical arch-length technique is used. In dynamic snap-through analysis, the effect of structural damping is also included. Numerical results of this study reveal that the structure is sensitive to the initial deflection caused by thermal postbuckling load. Increasing the temperature prior to mechanical loads enhances the snap-through intensity and also increases both the upper and lower limit loads. As shown, dynamic snap-through loads are lower than the static ones, however dynamic snap-through intensity is more than the static snap-though intensity. Furthermore, structural damping enhances the dynamic buckling loads of the plate and decreases the dynamic postbuckling deflection of the plate.     

Axisymmetric bending analysis of thick functionally graded circular plates using fourth-order shear deformation theory

In the present article, axisymmetric bending and stretching of functionally graded (FG) circular plates subjected to uniform transverse loading based on fourth-order shear deformation plate theory (FOST) have been studied. Using a fourth-order shear deformation theory, the solutions for deflection and rotation functions of FG plates are presented in terms of the corresponding quantities for a homogeneous plate using the classical plate theory (CPT), from which solutions one can easily obtain the FOST solutions for axisymmetric bending of FG circular plates. It is assumed that the effective mechanical properties of the functionally graded plates through the thickness are continuous functions of the volume fractions of the constituent parts which are themselves defined by a power-law function. Numerical results for maximum deflection and shear stress are presented for various percentages of ceramic–metal volume fractions. These results are also compared with those obtained from the first-order shear deformation plate theory of Mindlin (FST), the third-order shear deformation plate theory of Reddy (TST) as well as the exact three-dimensional elasticity solution. It is found that although the maximum deflections obtained using FOST and TST are close to each other, the through-thickness shear stress is predicted more accurately by the FOST formulation than by the TST.     

A new simple third-order shear deformation theory of plates

An improved simple third-order shear deformation theory for the analysis of shear flexible plates is presented in this paper. This new plate theory is composed of three parts: the simple third-order kinematics of displacements reduced from the higher-order displacement field derived previously by the author; a system of 10th-order differential equilibrium equations in terms of the three generalized displacements of bending plates; five boundary conditions at each edge of plate boundaries. Although the resulting displacement field is the same as that proposed by Murthy, the variational consistent governing equations and the associated proper boundary conditions are derived and identified in this work for the first time in the literature. The applications and accuracy of the present shear deformation theory of plates are demonstrated by analytically solving the differential governing equations of a twisting plate, a bending beam and two bending plates to which the 3-D elasticity solutions are available, and excellent agreements are achieved even for the torsion of a plate with square cross-section as well the local effects of stresses at plate boundaries can be characterized accurately. These analytical solutions clearly show that the simple third-order shear deformation theory developed in this work indeed gives better results than the first-order shear deformation theories and other simple higher-order shear deformation theories, since the present third-order shear flexible theory is based on a more rigorous kinematics of displacements and consists of not only a system of variational consistent differential equations, but also a group of consistent boundary conditions associated with the differential equations. The present simple third-order shear deformation theory can easily be applied to the static and dynamic finite element analysis of laminated plates just like the applications of other popular shear flexible plate theories, and improved results could be obtained from the present simple third-order shear deformable theories of plates.