基于解析试函数的广义协调四边形厚板元

本文构造两个广义协调四边形厚板元ATF-PQ4a和ATF-PQ4b。根据Mindlin-Reissner厚板理论的控制方程，首先求出其基本解析解，然后用其作为试函数来构造单元。数值算例表明，这两个单元不出现剪切闭锁，显示出良好的性能。     

任意一点作用集中荷载与简支矩形厚板的弯曲

本文基于Reissner理论求解矩形厚板的弯曲问题，给出在任意一点作用集中荷载与矩形厚板弯曲问题的解析解，并给出了具有实际价值的计算结果。     

弹性地基上四边自由矩形薄板的自由振动

将弹性地基用Winkler模型来代替。首先把弹性地基上矩形薄板的动力学方程表示成为Hamilton正则方程，然后采用辛几何方法对全状态相变量进行分离变量，并利用得到的共扼辛正交归一关系，求出弹性地基上四边自由矩形薄板的固有频率和振型的解析解表达式。由于在求解过程中不需要事先人为的选取挠度函数，而是从弹性地基上矩形薄板的动力学基本方程出发，直接利用数学的方法求出可以满足四边自由边界条件的固有频率和振型的解析解表达式，使得问题的求解更加合理化。文中的最后还给出了计算实例来验证本文所采用的方法以及所推导出公式的正确性。     

一类非线性广义强阻尼时滞扰动Sine-Gordon方程初值问题

本文讨论了一类非线性广义Sine-Gordon扰动方程,基于渐近理论得到对应方程的时滞初值问题并求出渐近解析解．首先,利用Fourier变换方法得出外部解．其次,按时滞变量展开扰动函数,再根据摄动方法和理论求出强阻尼时滞扰动广义Sine-Gordon方程初值问题的的渐近解．根据本文的理论和方法得到的渐近解是解析的表示式,能够进行解析运算,从而可得到相关的物理量的性状,扩大了问题的讨论范围．     

基于解析试函数的广义协调超基膜元

利用解析试函数法构造一个带旋转自由度广义协调超基膜元。根据弹性力学平面问题的控制方程和艾雷应力函数,求出问题完备的基本解析解,然后用其作为试函数并采用广义协调条件来构造单元:ATF-SCQ4θ。数值算例表明,该类单元精度高、对网格畸变不敏感,显示出良好的性能。     

Kirchhoff型裂纹板的边界元法

本文用的复变函数理论,导出了含裂板弯曲问题的基本解。该基本解满足自由裂纹的边界条件。将其引入直接或间接积分方程中,只要对板的外边界进行离散,就可计算有限尺寸裂纹板的弯曲问题。算例表明,本文所得到的基本解用以求解裂纹板弯曲问题划分的单元较少,精度较高。本文的方法还可用以求解含有形状比较复杂的裂纹或孔洞板弯曲问题的基本解。     

考虑流固耦合的典型管段结构振动特性分析

研究了两种最常见的流体管段结构模型与计算。对于直管,利用拉氏变换把时域方程变换到频域,对频域方程进行推导求解,得到了直管的频域解析解;对于弯管,直接对方程模型进行整体求解,同样求得了其频域解析解。然后以Davidson单弯管模型为例,说明典型管段结构组合的管道系统的求解方法,并验证直管以及弯管模型和求解方法的正确性。最后,通过改变弯管的弯曲半径以及角度来对管道的流固耦合振动特性的影响因素进行分析。结果表明,弯曲角度以及弯曲半径越小,频谱曲线密集程度越低,耦合振动越弱,反之越强。     

基于哈密顿解法的厚板边界效应典型算例分析

在平板弯曲问题中存在边界效应现象。这个现象用Reissner厚板理论可以论证,而经典薄板理论则无法解释。边界效应现象在板的自由边界附近表现最为典型。该文首先选取均载作用下的三边简支,一边自由的矩形厚板作为典型问题,采用哈密顿解法求出解析解。然后结合这个典型问题,对边界效应现象进行分析,对其影响因素和影响范围进行讨论。     

正交各向异性矩形板的自由振动特性分析

采用改进Fourier级数方法,建立了正交各向异性矩形薄板的弯曲振动模型,推导出与振动控制方程等价的矩阵方程,得到控制方程在任意边界条件下的解析解。弯曲振动的位移函数表示为标准的二维Fourier余弦级数和辅助Fourier级数之和,通过辅助级数的引入,解决了振动位移函数的偏导数在各边界处潜在不连续的问题。矩形板的振动模态信息能够通过求解一个标准的矩阵特征值而得到。最后进行数值计算并与现有的文献结果进行比较,验证了该方法的快速收敛性和计算精确性。     

正交各向异性厚板振动分析的边界积分方程法

本文采用正交各向异性厚板静力问题的基本解作为边界积分方程的核函数,利用加权残数法建立了正交各向异性厚板振动分析的边界积分方程。文中详细地讨论了边界积分方程的数值处理过程并给出了若干数值算例以论证本文方法的正确性。      

Buckling behavior of standing laminated Mindlin plates subjected to body force and vertical loading

In this article, an exact analytical solution for stability analysis of vertical moderately thick laminated rectangular plates subjected to selfweight and top load on the basis of the first-order shear deformation plate theory is presented. It is assumed that the symmetric laminated rectangular plate is composed of transversely isotropic layers. Employing an analytical approach, the coupled governing stability equations of the laminated plate are converted into two uncoupled partial differential equations in terms of transverse displacement and an auxiliary function. It is considered that the vertical sides of the laminated plate are simply supported. Using Levy-type solution, the decoupled equations are reduced to two ordinary differential equations. One of these equations has variable coefficients, for which an exact analytical solution is obtained in the form of power series method of Frobenius. After appropriate convergence study, the present analysis is validated by comparing the results with the existing data reported in the literature. Furthermore, the effects of aspect ratio, plate thickness, boundary conditions, weight of plate and top load on the stability of laminated rectangular plates are investigated and discussed in details. The presented formulations and results can be used as benchmark for future research studies.     

Nonlinear dynamics of composite laminated cantilever rectangular plate subject to third-order piston aerodynamics

This paper presents the analysis of the nonlinear dynamics for a composite laminated cantilever rectangular plate subjected to the supersonic gas flows and the in-plane excitations. The aerodynamic pressure is modeled by using the third-order piston theory. Based on Reddy’s third-order plate theory and the von Kármán-type equation for the geometric nonlinearity, the nonlinear partial differential equations of motion for the composite laminated cantilever rectangular plate under combined aerodynamic pressure and in-plane excitation are derived by using Hamilton’s principle. The Galerkin’s approach is used to transform the nonlinear partial differential equations of motion for the composite laminated cantilever rectangular plate to a two-degree-of-freedom nonlinear system under combined external and parametric excitations. The method of multiple scales is employed to obtain the four-dimensional averaged equation of the non-automatic nonlinear system. The case of 1:2 internal resonance and primary parametric resonance is taken into account. A numerical method is utilized to study the bifurcations and chaotic dynamics of the composite laminated cantilever rectangular plate. The frequency–response curves, bifurcation diagram, phase portrait and frequency spectra are obtained to analyze the nonlinear dynamic behavior of the composite laminated cantilever rectangular plate, which includes the periodic and chaotic motions.     

On a new symplectic geometry method for exact bending solutions of orthotropic rectangular plates with two opposite sides clamped

A novel symplectic geometry method is presented for exact bending solutions of orthotropic rectangular thin plates with two opposite sides clamped. In the proposed mathematical method, it starts with the basic governing equations for the bending of orthotropic plates, and there are no predetermined functions, which overcome the deficiency of conventional semi-inverse methods; therefore, the straightforward implementation procedure serves as a completely rational model in plate bending analysis. The proposed method can be extended to more problems of plates such as buckling and vibration. Tabulated accurate results are included in this paper, which are expected to be valuable for future comparison.     

固支三维弹性矩形厚板的精确解

采用有限积分变换和状态空间理论相结合的方法推导出了固支三维弹性矩形厚板的精确解.在分析过程中摒弃以往薄板和中厚板理论中有关应力和位移函数的各种人为假定,完全从三维弹性力学基本方程出发,经过变量代换将关于应力和位移分量的六阶偏微分方程组化为2 个彼此独立的四阶、二阶矩阵微分方程,再利用有限积分变换的方法得到空间状态方程,并由Cayley-Hamilton定理求得应力和位移分量沿板厚度z 方向的传递矩阵,最后利用边界条件定解出待定常数,经过有限积分逆变换解得了固支三维厚板的精确解.通过计算实例验证了该文方法的正确性.     

Finite difference solution of a system of first-order partial differential equations

A finite difference solution of a system of first-order partial differential equations, using a central difference scheme, is presented. The equations describe the linear elastic behaviour of a thick rectangular plate resting on an elastic foundation and carrying an arbitrary transverse load. The lateral edges of the plate are unstressed. The main deflections and stresses predicted by the method for a particular case are given, together for purposes of comparison, with results from a finite element analysis.     

弹性力学求解体系的研究与进展 第十三届全国结构工程学术会议特邀报告

本文介绍弹性力学对偶求解体系的近期研究和进展:(1)提出一种新的正交关系。不用辛几何的概念,直接导出对偶微分方程组;(2)基于新正交关系,建立二维弹性力学特征函数展开直接解法,求得含可对角化边界条件下的显式封闭解:(3)将对偶求解体系推广到多坐标方向,建立多坐标方向的对偶微分方程和求解体系。(4)采用偏微分方程的算子解法,建立了板状弹性体的弯曲理论,把它的解分解为弯曲齐次解、特解、和衰减解:(5)将对偶求解体系推广应用于厚板和薄板问题,建立了有关的对偶微分方程,正交关系和变分原理。     

Fourier series solution for a rectangular thick plate with free edges on an elastic foundation

A Fourier series solution is presented for a system of first-order partial differential equations which describe the linear elastic behaviour of a thick rectangular plate resting on an elastic foundation and carrying an arbitrary transverse load. The lateral edges of the plate are unstressed. A central step in the method for solving the system of equations is to combine a complementary function with a particular solution of the system in order to satisfy the boundary conditions. The complementary function is the sum of two series. The terms of the first series are products of a Fourier term in one space variable with the solution of an eigenvalue problem in the other space variable. The second series is similar and comes from reversing the roles of the space variables.     

带有加强筋的Mindlin板动态刚度阵法

以加筋中厚矩形板为研究对象，推导了加筋板的动态刚度阵，为动态刚度阵法提供一种新单元。板的运动微分方程由Mindlin厚板理论给出，同时还考虑了板平面内的振动。对于板上加强筋的处理，则通过Hamilton原理对板的运动方程作相应的修正，最终得到加筋板的运动微分方程。而方程的解析解直接用于单元刚度阵的推导，所得加筋板单元的动态刚度阵结合传统有限元方法的单元组装和求解方法即可用于计算整个结构的动力响应。此外，还给出了加筋板单元的均方响应计算公式，可用来计算结构的平均振动能量。最后通过数值算例验证本文方法，计算结果与传统有限元方法进行分析比较。     

On new symplectic elasticity approach for exact free vibration solutions of rectangular Kirchhoff plates

In the classical approach, it has been common to treat free vibration of rectangular Kirchhoff or thin plates in the Euclidian space using the Lagrange system such as the Timoshenko’s method or Lévy’s method and such methods are the semi-inverse methods. Because of various shortcomings of the classical approach leading to unavailability of analytical solutions in certain basic plate vibration problems, it is now proposed here a new symplectic elasticity approach based on the conservative energy principle and constructed within a new symplectic space. Employing the Hamiltonian variational principle with Legendre’s transformation, exact analytical solutions within the framework of the classical Kirchhoff plate theory are established here by eigenvalue analysis and expansion of eigenfunctions in both perpendicular in-plane directions. Unlike the classical semi-inverse methods where a trial shape function required to satisfy the geometric boundary conditions is pre-determined at the outset, this symplectic approach proceeds without any shape functions and it is rigorously rational to facilitate analytical solutions which are not completely covered by the semi-inverse counterparts. Exact frequency equations for Lévy-type thin plates are presented as a special case. Numerical results are calculated and excellent agreement with the classical solutions is presented. As derivation of the formulation is independent on the assumption of displacement field, the present method is applicable not only for other types of boundary conditions, but also for thick plates based on various higher-order plate theories, as well as buckling, wave propagation, and forced vibration, etc.