中厚矩形板的非线性动力屈曲分叉

建立考虑横向剪切与转动惯量影响的矩形板的动力控制方程，应用Ｇａｌｅｒｋｉｎ方法将其化为Ｍａｔｈｉｅｕ方程，然后根据Ｌｙａｐｕｎｏｖ－Ｓｃｈｍｉｄｔ方法得到了系统在参数激励下的１／２亚谐分叉特性，并给出了四边简支与四边固支弹性薄板的非线性动力屈曲分叉条件。     

Hamilton体系下矩形薄板受抛物线压力载荷的屈曲分析

针对四边简支矩形薄板在两对边相向的非线性分布压力下的面内应力分布以及屈曲问题,应用弹性力学的Hamilton体系和Galerkin法进行了研究.基于弹性力学的平面矩形域Hamilton体系,根据辛本征向量展开解法,得到了对应于零本征值和非零本征值的含待定常数的实数型面内应力分布通解.依据必须满足的应力边界条件,导出了矩形薄板在抛物线分布载荷下的面内应力分布.考虑到应力分布表达式的复杂性,用完全的解析方法得到屈曲载荷是不可能的.因此,运用基于虚功原理的Galerkin法,根据四边简支矩形薄板弯曲的位移边界条件,给出了不同长宽比矩形薄板受抛物线分布载荷的屈曲临界载荷.通过与已有文献中DQ法给出的数值计算结果比较,表明了本文求解方法的有效性和正确性.基于所给出的结果,可望为解决矩形薄板在非线性分布载荷下的面内应力分布以及屈曲问题提供一种新的研究方法.     

基于物理信息的深度学习求解矩形薄板力学正反问题

建立基于物理信息的神经网络框架,利用深度学习求解矩形薄板力学正反问题.力学正问题为已知矩形薄板的基本参数、边界条件和受力情况,求薄板各点挠度;反问题为已知薄板部分点的挠度、基本参数和受力情况等,识别边界条件.基于物理信息的神经网络模型中,损失函数除基于数据驱动模型的挠度数据拟合部分以外,还引入薄板弯曲基本方程和应力应变...     

分数阶微分型双参数黏弹性地基矩形板受荷响应

基于考虑水平剪切变形和竖向压缩变形的双参数地基模型,利用分数阶微分建立了黏弹性地基上矩形薄板荷载作用下的挠度方程;根据弹性-黏弹性对应原理,通过Laplace变换将四边简支矩形板弹性问题的解推广求解分数阶微分黏弹性问题;通过算例表明分数阶微分型黏弹性模型比经典黏弹性模型的适应性,并分析了模型参数对挠度-时间关系的影响.     

矩形薄板屈曲分析的高阶有限条传递矩阵法

针对矩形薄板屈曲,基于基尔霍夫板理论,采用半解析有限条法和含有中间节线的高阶有限条法推导条元的控制方程。在此基础上,根据传递矩阵形成单元传递方程和系统传递矩阵,形成了分析薄板屈曲临界力和屈曲模态的矩形薄板屈曲分析的高阶有限条传递矩阵法。采用该方法分析了两种边界条件下四边受压矩形板的屈曲临界力,并与理论解和有限元解比较,实例证明该方法有效。此方法在有限条传递矩阵法的基础上可进一步提高计算精度。     

四边固定载流矩形薄板的磁弹性稳定性分析

本文针对四边固定载流矩形薄板,利用Mathieu方程解的稳定性,研究其在电磁场与机械荷载共同作用下的磁弹性稳定性问题。首先在载流薄板的磁弹性非线性运动方程、物理方程、几何方程、洛仑兹力表达式及电动力学方程的基础上,导出了载流薄板在电磁场与机械荷载共同作用下的磁弹性动力稳定方程,然后应用Galer-kin方法将稳定方程整理为Mathieu方程的标准形式,并将薄板的动力稳定性问题归结为对Mathieu方程的求解。利用Mathieu方程的稳定解区域与非稳定解区域的分界,即方程系数λ和η的本征值关系,得出了磁弹性问题失稳临界状态的判别方程。通过具体算例,给出了四边固定载流矩形薄板的磁弹性动力失稳临界状态与相关参量之间的关系曲线,并对计算结果及其变化规律进行了分析讨论。     

横观各向同性弹性半空间地基上四边自由各向异性矩形薄板弯曲解析解

选用更具广泛性的横观各向同性弹性半空间地基模型,来分析四边自由各向异性矩形地基板的弯曲解析解．将异性薄板的弯曲控制方程,与基于横观各向同性弹性半空间地基位移解建立的板与地基变形协调方程相结合,先按对称性分解,然后用三角级数法,得出横观各向同性弹性半空间地基上四边自由各向异性矩形薄板的弯曲解析解,包括地基反力、板的挠度及内力的解析表达式．该解析解克服了数值法的弊端,取消了对地基反力的假设,板的内力及地基反力求解更切实际．算例结果与文献结果吻合良好,证明本文方法的可行性．     

四角点支承四边自由矩形薄板屈曲问题的新解析解

角点支承矩形薄板的屈曲问题是板壳力学的一类重要课题，控制方程和边界条件的复杂性导致寻求该类问题的解析解十分困难。虽然各类近似/数值方法可用于解决此类难题，但作为基准的精确解析解在公开文献中鲜有报道。本文基于近年来提出的辛叠加方法，解析求解了四角点支承四边自由矩形薄板的屈曲问题。首先将问题拆分为两个子问题，接着利用分离变量与辛本征展开推导出子问题的解析解，最后通过叠加获得原问题的解。由于求解过程从基本控制方程出发，逐步严格推导，无需假定解的形式，因此本文解法是一种理性的解析方法。数值算例给出了不同长宽比和不同面内载荷比情况下，四角点支承四边自由矩形薄板的屈曲载荷和典型屈曲模态，并经有限元方法验证，确认了解析解的正确性。     

任意变厚度矩形薄板的屈曲和振动

本文采用两步级数展开法获得了任意变厚度矩形薄板的屈曲和振动问题的一般解,并详细研究了四边简支变厚度矩形板的屈曲和振动问题的解.针对两种变厚度板,计算了失稳临界荷载、失稳波形以及基频,并与前人的结果做了比较,分析结果表明本文方法简单收敛快。     

板下地基位移分布规律及参数确定

将弹性半空间地基受任意竖向荷载作用下的静力位移积分变换解与弹性半空间地基上四边自由矩形板受任意竖向荷载作用下的弯曲解析解相结合,建立了求解板下地基位移的一般方法.对一些算例,进行大量数值计算分析,得出弹性半空间地基上四边自由矩形板下地基水平位移和竖向位移的分布规律,地基影响深度,并由此分布规律确定了其相应的简化模型-双参数地基模型的两个参数.     

The Effect of Multiple Buckling Modes on the Postbuckling Behavior of Plane Elastic Frames. Part II. Asymmetric Frames

The postbuckling behavior of an asymmetric one-bay, two-storey frame with clamped edges is analyzed. Columns have different bending stiffnesses and are pairwise of the same length. By assuming columns to be inextensible and shear undeformable, and beams to be rigid, two buckling modes are possible which are described by the sidesway of the lower floor with a rigid horizontal displacement of the upper floor and a sidesway of the upper floor, the lower floor undergoing no displacement. By properly selecting the ratios EI/h² (EI being the bending stiffness of a column and h its length) the two buckling modes may occur simultaneously. A third buckling mode is also possible which is characterized by no displacement of the horizontal beams and local deflection of one or more columns in the shape of a beam with fixed edges. This third case will not be considered in this paper. The Koiter general nonlinear theory of elastic stability recast in a form convenient for the development of finite elment models along lines similar to the recent presentation by Budiansky has been employed in the analysis. Nonlinear constraints on the field variable φ (φ being the cross-section rotation) are accounted for by means of Lagrangian multipliers. Results show that the postbuckling behavior of a single buckling mode is always asymmetric unstable and depends both on the degree of asymmetry of the structure and on the ratio h/l, l being the frame span. The occurrence of simultaneous buckling modes exacerbates the imperfection sensitivity of the structure.     

圆截面弹性细杆的平面振动

基于Kirchhoff理论讨论圆截面弹性细杆的平面振动．以杆中心线的Frenet坐标系为参考系建立动力学方程．杆作平面运动时，其扭转振动与弯曲振动解耦．讨论任意形状杆的扭转振动和轴向受压直杆在无扭转条件下的弯曲振动，证明直杆平衡的静态Lyapunov稳定性与欧拉稳定性条件为动态稳定性的必要条件．考虑轴向力和截面转动惯性效应的影响，导出弯曲振动的固有频率．     

矩形夹层板稳定性分析

本文在Reissner 理论基础上，应用功的互等定理推导了夹层矩形板稳定问题的基本解，在已推导出的夹层板基本解的基础上，利用功的互等法求解了两对边固定一边简支一边自由、两邻边简支另两邻边自由且角点支承、两邻边简支另两邻边自由且角点悬空三种不同边界条件下夹层板的稳定问题，给出了挠曲面方程及其对应的执行方程；进行了数值计算，并与有限元结果进行对照分析．结果表明：本文方法求解过程更简单，提供了一种求解夹层板稳定问题的新方法，计算结果对解决工程实际问题具有一定的参考价值．     

Stability of bars with variable rigidity

A variable cross-section bar is considered. The bar is not uniform in length. The bar axis through the mass centers of all cross sections is a straight line. The bar is compressed by a longitudinal force applied to the mass center of the boundary cross section. The stability loss of the straight-line shape of the bar’s equilibrium is discussed when a curved shape is also possible. Approximate analytical formulas are obtained for the critical compressive force when four types of end fixing are used for a periodically nonuniform bar. The numerical results obtained by these formulas are compared with the known exact solutions to the stability equation for a bar whose cross section is stepwise variable and whose nonuniformity consists of only one period (the limiting case).     

Vibrations of nonhomogeneous orthotropic rectangular plates with bilinear thickness variation resting on Winkler foundation

Free transverse vibrations of nonhomogeneous orthotropic rectangular plates with bilinear thickness variation resting on Winkler foundation are presented here using two dimensional boundary characteristic orthogonal polynomials in the Rayleigh-Ritz method on the basis of classical plate theory. Gram-Schmidt process has been used to generate orthogonal polynomials. The nonhomogeneity of the plate is assumed to arise due to linear variations in elastic properties and density of the plate material with the in-plane coordinates. The two dimensional thickness variation is taken as the Cartesian product of linear variations along the two concurrent edges of the plate. Effect of nonhomogeneity parameters, aspect ratio and thickness variation together with foundation parameter on the natural frequencies has been illustrated for the first three modes of vibration for four different combinations of clamped, simply supported and free edges correct to four decimal places. Three dimensional mode shapes for specified plate for all the four boundary conditions have been plotted. A comparison of results in special cases with published one has been presented.     

Nonlinear sway-buckling of an eccentrically loaded frame of two timoshenko-bars

Summary A variational method for investigating the nonlinear lateral stability is applied to a rectangular, geometrically perfect, two-bar frame which is loaded eccentrically to the center line of one of the bars. The frame loses its stability through a limit point. The individual, and primarily the coupling effects on the nonlinear sway-buckling load are fully assessed for a variety of parameters such as transverse shear deformation, cross-sectional shape, loading eccentricity, slenderness ratio and moment of inertia ratio of the two bars. The conclusions presented herein give a better insight into the actual response of the frame.

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Übersicht In dieser Arbeit wird ein Variationsverfahren für die Untersuchung der nichtlinearen Stabilität eines rechteckigen, geometrisch perfekten, Zwei-Stab-Rahmens vorgestellt, der exzentrisch bezüglich eines der Stäbe belastet ist. Der Rahmen verliert Scine Stabilität bei einer Grenzlast. Der Einfluß einzelner, vor allem aber die Wirkung von kombiniert auftretenden Parametern — wie Querkraftbiegung, Querschnittsform, Lastexzentrizität, Schlankheitsgrad und Trägheitsmoment der Stäbe — auf die nichtlineare Knicklast werden untersucht. Die in dieser Arbeit mitgeteilten Ergebnisse lassen das wirkliche Verhalten des Rahmens gut erkennen.

     

Some exact plane elasticity solutions for nonhomogeneous,orthotropic sheets

Exact plane stress solutions are presented for composite material sheets made of parallel fibers embedded in matrix materials. The fibers have variable spacing, and the resulting material is macroscopically orthotropic and nonhomogeneous. Formulas for the variable elastic coefficients are presented for arbitrary fiber spacing. Exact solutions for the stress, strain and displacement fields are presented for four types of problems with arbitrary fiber spacing: (1) Uniform normal stress on the edges parallel to the fibers (i.e., the longitudinal edges), zero normal displacement on the transverse edges; (2) zero normal stress on the longitudinal edges, uniform normal displacement on the transverse edges; (3) zero normal displacement in the longitudinal edges, uniform normal displacement on the transverse edges; and (4) zero normal displacement on the longitudinal edges, uniform shear stress on all edges. For the first three problems, the shear stresses on all boundaries are zero. For the last one, the normal stress on the transverse edge is zero.     

An analytical solution for buckling of moderately thick functionally graded sector and annular sector plates

In this article, an analytical solution for buckling of moderately thick functionally graded (FG) sectorial plates is presented. It is assumed that the material properties of the FG plate vary through the thickness of the plate as a power function. The stability equations are derived according to the Mindlin plate theory. By introducing four new functions, the stability equations are decoupled. The decoupled stability equations are solved analytically for both sector and annular sector plates with two simply supported radial edges. Satisfying the edges conditions along the circular edges of the plate, an eigenvalue problem for finding the critical buckling load is obtained. Solving the eigenvalue problem, the numerical results for the critical buckling load and mode shapes are obtained for both sector and annular sector plates. Finally, the effects of boundary conditions, volume fraction, inner to outer radius ratio (annularity) and plate thickness are studied. The results for critical buckling load of functionally graded sectorial plates are reported for the first time and can be used as benchmark.     

Nonlinear dynamical stability analysis of the circular three-dimensional frame

The three-dimensional frame is simplified into flat plate by the method of quasiplate. The nonlinear relationships between the surface strain and the midst plane displacement are established. According to the thin plate nonlinear dynamical theory, the nonlinear dynamical equations of three-dimensional frame in the orthogonal coordinates system are obtained. Then the equations are translated into the axial symmetry nonlinear dynamical equations in the polar coordinates system. Some dimensionless quantities different from the plate of uniform thickness are introduced under the boundary conditions of fixed edges, then these fundamental equations are simplified with these dimensionless quantities. A cubic nonlinear vibration equation is obtained with the method of Galerkin. The stability and bifurcation of the circular three-dimensional frame are studied under the condition of without outer motivation. The contingent chaotic vibration of the three-dimensional frame is studied with the method of Melnikov. Some phase figures of contingent chaotic vibration are plotted with digital artificial method.