激光辐照下有界圆厚板的热弹性弯曲响应分析

考虑板弯曲运动的旋转惯性效应和剪切变形效应，建立了轴对称热能沉积作用下，边界固支或简支圆厚板的热弹性弯曲运动控制方程。利用数学变换和摄动法，导出了各种温度－力学边界条件下板的热弹性弯曲挠度及截面广义转角的解析公式。给出了在空间Ｇａｕｓｓ型分布激光束辐照下，板整体弯曲响应的代表性数值计算结果，直观显示了板弯曲挠度的时空变化规律。     

圆薄板材料性能随温度变化的大挠度弯曲分析

记入材料性能参数随温度的变化，导出了横向力作用下圆薄板轴对称大挠度弯曲的位移型控 制方程，并利用伽辽金方法求出了圆薄板大挠度弯曲的近似位移解；针对一个简例进行了理 论计算和有限元数值模拟，二者结果一致. 在此基础上分析了圆薄板大挠度弯曲的规律及材 料参数随温度变化的热软化效应，给出了相关结果.     

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.     

位移模式对Cross—PLY矩形板热弹性响应的影响

本文建立了以Ｒｅｉｓｓｎｅｒ混合变分原理为基础的迭层板剪切变形理论来求解Ｃｒｏｓｓ－ＰＬＹ矩形板的热弯曲问题，用二种方式来模拟平面位移沿厚度的变化：将一阶剪切变形理论的平面位移叠加一项交错线性函数；设平面位移是分线性连续函数。为保证层间应力的连续性，将横向剪切应力处理成厚度坐标的二次函数，温度沿厚度线性变化。通过对称及反对称Ｃｒｏｓｓ－ＰＬＹ矩形板的热应力及挠度分析比较，指出了位移模式对热弹性响应     

位移模式对Cross－PLY矩形板热弹性响应的影响

本文建立了以Ｒｅｉｓｓｎｅｒ混合变分原理为基础的迭层板剪切变形理论来求解Ｃｒｏｓｓ－ＰＬＹ矩形板的热弯曲问题，用二种方式来模拟平面位移沿厚度的变化：将一阶剪切变形理论的平面位移叠加一项交错线性函数；设平面住移是分段线性连续函数。为保证层间应力的连续性，将横向剪切应力处理成厚度坐标的二次函数，温度沿厚度线性变化。通过对称及反对称Ｃｒｏｓｓ－ＰＬＹ矩形板的热应力及挠度分析比较，指出了位移模式对热弹性响应的影响。     

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。     

考虑地基水平摩阻的Winkler地基上板模型解析

在Winkler地基模型基础上，采用板与地基之间的水平摩阻应力正比于板与地基接触点间水平位移假设，推演了包含板弯曲和轴向拉压效应的非线性地基板微分方程；应用摄动法分析竖向集中力作用下，板与地基水平摩阻应力对板内力（弯曲力、轴向力和剪应力）、位移（挠度、水平位移）的影响规律，实证了板与地基水平摩阻应力对板剪应力的非线性影响可以忽略不计，从而得到了轴对称条件下计入地基水平摩阻的Winkler地基上薄板的线性微分方程．随后通过汉克尔变换得到了轴对称无限大板的解析解，以及包含四项复宗量贝塞尔函数的轴对称圆形板的解析解，给出了板内力、位移的计算式；最后，通过算例分析了板与地基间水平摩阻状况对板挠度、截面弯矩的影响规律．结果表明：地基板挠度与弯矩随着板与地基间水平摩阻的增大而减少；当地基板水平摩阻参数大于0.01时，地基水平摩阻力对板挠度和弯矩影响有可能超过2%，应予考虑；无限大板作用圆形均布荷载时，水平摩阻的存在最大可使板最大挠度（即荷载圆中心点处挠度）下降约50%，板最大截面弯矩（即荷载圆中心点处弯矩）下降约70%.     

热黏弹性梁拟静态弯曲问题的解析分析

基于平面应力假设和热黏弹性材料的积分型本构关系,建立了以位移分量为未知量的热黏弹性梁静动力学分析的二维数学模型。针对拟静态弯曲问题,首先,在Laplace变换域,引入位移势函数,将控制方程解耦;其次,根据给定的平面温度场和边界条件,采用分离变量法,引入热应力函数,得到了热黏弹性梁的热应力分布;最后,利用Laplace逆变换,获得了热黏弹性梁拟静态弯曲热应力响应的解析解,考察了热载荷作用下几何、黏弹性等参数对梁应力和位移的影响。     

横观各向同性三维热弹性力学通解及其势理论法

通过引入两个位移函数，对用位移表达的运动平衡方程作了简化．利用算子理论，严格地导出了横观各向同性非耦合热弹性动力学问题的通解．对于静力学问题，通解的形式可进一步简化成用4个准调和函数来表示．具体考察了横观各向同性体内平面裂纹上下表面有对称分布温度作用的问题，推广了势理论方法，导出了一个积分方程和一个微分-积分方程．针对币状裂纹表面受均布温度作用情形，给出了具体的解。     

基于平面偶应力-Reissner/Mindlin板比拟的偶应力有限元

偶应力理论的有限元列式面临本质性的C1连续性困难. 平面偶应力理论和Reissner/Mindlin板弯曲理论之间的比拟关系表明这两个理论系统的有 限元的同一性，而R/M板有限元并不存在C1连续性困难. 因此，研究将R/M板单元转化为具有一般位移自由度的平面偶应力单元的一般方法. 根据这一方法，将典型的8节点Serendipity型R/M板单元Q8S转化为一个4节点12 自由度的四边形平面偶应力单元，数值结果表明该单元具有良好的精度和收敛性     

Thermal postbuckling analysis of moderately thick plates

A thermal postbuckling analysis is presented for a moderately thick rectangular plate subjected to (1) uniform and non-uniform tent-like temperature loading; and (2) combined axial compression and uniform temperature loading. The initial geometrical imperfection of plate is taken into account. The formulations are based on the Reissner-Mindlin plate theory considering the effects of rotary inertia and transverse shear deformation. The analysis uses a deflection-type perturbation technique to determine the thermal buckling loads and postbuckling equilibrium paths. Numerical examples are presented that relate to the performances of perfect and imperfect, moderately thick rectangular plates and are compared with the results predicted by the thin plate theory.     

Analysis of curved beams using a new differential transformation based curved beam element

Differential transformation method is used to obtain the shape functions for nodal variables of an arbitrarily non-uniform curved beam element including the effects of shear deformation considering axially functionally graded material. The proposed shape functions depend on the variations in cross-sectional area, moment of inertia, curvature and material properties along the axis of the curved beam element. The static and free vibration of axially functionally graded tapered curved beams including shear deformation and rotary inertia are studied through solving several examples. Numerical results are presented for circular, parabolic, catenary, elliptic and sinusoidal beams (both forms—prime and quadratic) with hinged-hinged, hinged-clamped and clamped-clamped and clamped-free end restraints. Three general taper types (depth taper, breadth taper and square taper) for rectangular cross section are studied. Out of plane vibration is studied and the lowest natural frequencies are calculated and compared with the published results. Out of plane buckling is investigated for circular beams due to radial load.     

Stochastic response of an axially loaded composite Timoshenko beam exhibiting bending–torsion coupling

A spectral finite element method is proposed to investigate the stochastic response of an axially loaded composite Timoshenko beam with solid or thin-walled closed section exhibiting bending–torsion materially coupling under the stochastic excitations with stationary and ergodic properties. The effects of axial force, shear deformation (SD) and rotary inertia (RI) as well as bending–torsion coupling are considered in the present study. First, the damped general governing differential equations of motion of an axially loaded composite Timoshenko beam are derived. Then, the spectral finite element formulation is developed in the frequency domain using the dynamic shape functions based on the exact solutions of the governing equations in undamped free vibration, which is used to compute the mean square displacement response of axially loaded composite Timoshenko beams. Finally, the proposed method is illustrated by its application to a specific example to investigate the effects of bending–torsion coupling, axial force, SD and RI on the stochastic response of the composite beam.     

厚圆柱壳的非轴对称振动分析

本文对厚圆柱壳的非轴对称振动进行了分析，其中除包含通常的薄膜和弯曲效应外，还反映了转动惯性，横向剪切变形和横向挤压的影响，数值结果表明：对于厚圆柱壳来说存在着频率密集区，频率位置发生移动，横向挤压的影响必须要考虑。     

点支撑预应力中厚矩形板的弯曲

基于Reissner-Mindlin一阶剪切变形板理论，讨论在预加面内机械荷载或温度场作用下，点支撑中厚矩形板的弯曲问题。温度场假定沿板表面为均布，沿板厚方向为线性分布的。利用考虑剪切变形影响的Timoshenko梁函数，采用Rayleigh-Ritz法给出不同边界条件下点支撑中厚板在横向荷载作用下的挠度和弯矩分布。结果表明，均匀温度场与预加面内压力将使板的挠度和弯矩增加。支撑点位置的变化、边界约束条件和横向剪切变形效应都对板的内力大小和分布有显著影响。     

Shear deformation in thermal bending analysis of laminated plates by the GDQ method

The interlaminar stresses and deflections in a laminated rectangular plate under thermal bending were determined by using the generalized differential quadrature method involving the effect of shear deformation. The approximate stress and deflection solutions are obtained under the bending of sinusoidal temperature of thermal load for layer in cross-ply laminates and angle-ply laminates. Numerical results show that the shear deformation has significant effects on the dominant interlaminar stresses and deflections in the laminated plate of thermal bending analysis.     

Mathematical modelling of the axially moving panels subjected to thermomechanical actions

The paper is devoted to a stability and out-of-plane deformation analysis of an axially moving elastic web modelled as a panel (a plate undergoing cylindrical deformation). The panel is under homogeneous pure mechanical in-plane tension and thermal strains corresponding to the thermal tension and bending. In accordance with the static approach of stability analysis the problem of out-of-plane thermomechanical divergence (buckling) is reduced to an eigenvalue problem which is analytically solved. This problem corresponds to the case of in-plane thermomechanical tension and zero thermal bending. The general case of deformations induced by combined thermomechanical bending and tension is reduced to nonhomogeneous boundary-value problem and analyzed with the help of Fourier series.     

Bending and free vibrational analysis of bi-directional functionally graded beams with circular cross-section

The bending and free vibrational behaviors of functionally graded (FG) cylindrical beams with radially and axially varying material inhomogeneities are investigated. Based on a high-order cylindrical beam model, where the shear deformation and rotary inertia are both considered, the two coupled governing differential motion equations for the deflection and rotation are established. The analytical bending solutions for various boundary conditions are derived. In the vibrational analysis of FG cylindrical beams, the two governing equations are firstly changed to a single equation by means of an auxiliary function, and then the vibration mode is expanded into shifted Chebyshev polynomials. Numerical examples are given to investigate the effects of the material gradient indices on the deflections, the stress distributions, and the eigenfrequencies of the cylindrical beams, respectively. By comparing the obtained numerical results with those obtained by the three-dimensional (3D) elasticity theory and the Timoshenko beam theory, the effectiveness of the present approach is verified.     

Effects of shear stresses and rotary inertia on the stability and vibration of sandwich cylindrical shells with FGM core surrounded by elastic medium

The vibration and stability of axially loaded sandwich cylindrical shells with the functionally graded (FG) core with and without shear stresses and rotary inertia resting Pasternak foundation are investigated. The dynamic stability is derived based on the first order shear deformation theory (FSDT) including shear stresses. The axial load and dimensionless fundamental frequency for FG sandwich shell with shear stresses and rotary inertia and resting on the Pasternak foundation. Finally, the influences of variations of FG core, elastic foundations, shear stresses and rotary inertia on the fundamental frequencies and critical axial loads are investigated.