矩形薄板面内非线性分布载荷下的辛弹性力学解

用辛弹性力学理论,根据平面矩形域本征向量展开解法,得到了对应于零本征值和非零本征值的本征向量解,以及含待定常数的面内应力分布通解,依据必须满足的应力边界条件,利用符号运算软件Maple,导出了矩形薄板在半余弦分布载荷作用下的面内应力表达式。为了验证方法的有效性和所得到的公式的正确性,具体分析了正方形薄板在两种非线性形式载荷——半余弦和抛物线分布载荷作用下的例子。算例结果与微分求积法及其有限元法得到的数值结果极其相近。基于所给出的结果,可望为工程应用中的屈曲分析提供合理的前期准备。     

多跨弹性支承连续矩形薄板屈曲分析

针对钢箱梁和混凝土薄壁箱梁受压翼缘的稳定问题,基于状态-空间向量法,提出了一种用于弹性支承连续矩形薄板弹性屈曲分析的计算方法。与有限条法结果对比,验证了该方法的可靠性。分析了跨间弹性支承刚度和布置以及荷载参数对屈曲的影响,结果表明：跨间弹性支承对连续矩形薄板屈曲影响明显,屈曲系数随着弹性支承刚度的增大呈非线性增长;等间距、等刚度布置弹性支承有利于板的稳定性,弹性支承的刚度或间距差别越大,对板的稳定性越不利;不同荷载工况下,弹性支承刚度-屈曲系数关系曲线的变化规律基本相同,弹性支承刚度较小时,荷载参数对屈曲系数影响显著,单向受压的屈曲系数可达双向等值受压的两倍。     

弹性支承上边界转动约束矩形板屈曲分析

随着工程结构的轻型化、薄壁化,薄板结构稳定问题越来越受到重视,针对不同条件下薄板屈曲问题开展了大量研究。弹性支承上的薄板屈曲、边界弹性转动约束的薄板屈曲和刚性支承上边界转动约束的薄板屈曲问题已有相关文献,关于非加载边弹性转动约束、弹性支承上薄板屈曲问题的研究尚不充分。该文研究了非加载边弹性转动约束、均匀受压弹性支承矩形薄板弹性屈曲问题。由Ritz能量变分法得到了临界载荷计算公式,应用有限元分析证实了理论解的适用性。得到了屈曲半波数与板的纵横比、边界转动约束系数及支承刚度之间的关系式,支承刚度增加使屈曲半波数和屈曲系数增大。     

变刚度Winkler地基上受压非均质矩形板的自由振动与屈曲特性

基于经典薄板理论,利用Hamilton原理建立变刚度Winkler地基上受压非均质矩形板自由振动与屈曲问题的控制微分方程并进行无量纲化。通过一种半解析方法-微分变换法(DTM)研究其无量纲固有频率和屈曲临界载荷特性。采用DTM将其无量纲控制微分方程及边界条件变换为等价的代数方程,得到含有频率和屈曲载荷的特征方程。将该问题退化为面内变刚度矩形板情形,其DTM解与精确解进行对比,结果表明DTM具有非常高的精度和很强的适用性。计算出在不同边界条件下屈曲临界载荷并分析地基刚度变化参数、弹性模量变化参数、密度变化参数、面内载荷和长宽比对矩形板无量纲固有频率的影响,给出了不同边界条件下变刚度Winkler地基上受压非均质矩形板的前三阶振型。     

受边缘非线性分布荷载作用矩形薄板的面内应力分析

矩形薄板边缘受非线性分布面内载荷作用的情况在工程中经常遇到,精确的应力分析也是薄板稳定性分析的基础,由于问题的复杂性目前还没有精确解.该文根据弹性力学理论,采用里兹法求解矩形薄板边缘受非线性分布载荷作用的面内应力,应力函数采用切比雪夫多项式并满足所有应力边界条件.结合数学计算软件Mathematica,分析了不同长宽比...     

粘弹性地基上弹性板受刚体撞击的动力响应分析

本文针对工程实际中所遇到的撞击问题,在事先仅知撞击体初始速度的情况下.研究分析了半无限粘弹性Winkler地基上的矩形弹性薄板受刚体撞击的动力响应问题,推导出了关于撞击力F(t)的非线性Volterra积分方程,给出了薄板位移响应W(x,y,t)的一般表达式,并给出了求解计算的数值方法。作为应用实例,本文对弹性方薄板受刚球撞击问题进行了分析计算,并与无粘性支承时的结果进行了对比讨论.     

弹性地基上受压矩形纳米板的自由振动与屈曲特性

基于Eringen非局部弹性理论和经典薄板理论,利用Hamilton原理推导Winkler-Pasternak弹性地基上面内受压正交各向异性矩形纳米板自由振动的控制微分方程并进行无量纲化。采用一种半解析方法—微分变换法(DTM)将无量纲控制微分方程及边界条件变换为等价的代数方程,得到含有无量纲固有频率和屈曲载荷的特征方程。数值给出了不同边界条件下无量纲地基刚度系数、压力强度、载荷参数、长宽比和纳米尺度对正交各向异性矩形纳米板无量纲固有频率的影响以及不同无量纲地基刚度系数、载荷参数和纳米尺度下的屈曲临界载荷值。结果表明:正交各向异性矩形纳米板的无量纲固有频率随无量纲地基刚度系数、载荷参数和长宽比的增大而增大,随纳米尺度的增大而趋向减小;屈曲临界载荷也随无量纲地基刚度系数的增大而增大,随纳米尺度的增大而减小。     

弹性压应力波作用下矩形薄板动力屈曲解析解

根据板的非线性动力平衡方程和压缩波前附加约束方程,基于双特征参数法和应力波理论,求解了矩形薄板在面内轴向冲击载荷作用下动力屈曲位移的解析解。揭示了矩形薄板动力屈曲过程中板的厚宽比、屈曲模态、冲击载荷大小和临界屈曲长度之间的关系。求得的屈曲模态与之前文献中用差分解得出的结果吻合良好。     

四边简支钢筋混凝土矩形薄板的热屈曲

基于刚性板和小挠度理论,考虑混凝土的材料非线性,推导了热载作用下钢筋混凝土矩形薄板的平衡方程和稳定方程。给出了四边简支钢筋混凝土矩形薄板在横向变温和温度均匀变化时临界屈曲温度变化的封闭解,并对工程中常见的钢筋混凝土矩形薄板在温度均匀变化时的临界屈曲温度变化进行了计算,讨论了板的材料常数、长宽比和相对厚度对临界屈曲温度变化的影响,从而为工程结构中钢筋混凝土矩形薄板的临界屈曲温度变化的计算提供了理论计算依据。     

横向磁场中对边简支对边固支矩形薄板的分岔与混沌

研究了力磁耦合作用下对边简支对边固支矩形薄板的分岔与混沌问题。在给出横向稳恒磁场和载荷共同作用下的矩形薄板的非线性磁弹性耦合运动学方程的基础上,得到了对边简支对边固支的矩形薄板的磁弹性振动方程。用Melnikov函数法给出该系统发生混沌运动的条件,并用数值方法求解该系统振动方程。通过具体算例,得到了系统的分岔图、Lyapunov指数图,并给出了相应位移波形图、相平面轨迹图、庞伽莱截面图。分析了电磁场参量及外载荷对系统运动状态的影响。     

Buckling analysis of rectangular composite plates with rectangular cutout subjected to linearly varying in-plane loading using fem

A numerical study is carried out using finite element method, to examine the effects of square and rectangular cutout on the buckling behavior of a sixteen ply quasi-isotropic graphite/epoxy symmetrically laminated rectangular composite plate [0°/+45°/-45°/90°]_2s, subjected to various linearly varying in-plane compressive loads. Further, this paper addresses the effects of size of square/rectangular cutout, orientation of square/rectangular cutout, plate aspect ratio(a/b), plate length/thickness ratio(a/t), boundary conditions on the buckling bahaviour of symmetrically laminated rectangular composite plates subjected to various linearly varying in-plane compressive loading. It is observed that the various linearly varying in-plane loads and boundary conditions have a substantial influence on buckling strength of rectangular composite plate with square/rectangular cutout.     

Levy Solution for Buckling Analysis of Functionally Graded Rectangular Plates

In this article, an analytical method for buckling analysis of thin functionally graded (FG) rectangular plates is presented. It is assumed that the material properties of the plate vary through the thickness of the plate as a power function. Based on the classical plate theory (Kirchhoff theory), the governing equations are obtained for functionally graded rectangular plates using the principle of minimum total potential energy. The resulting equations are decoupled and solved for rectangular plate with different loading conditions. It is assumed that the plate is simply supported along two opposite edges and has arbitrary boundary conditions along the other edges. The critical buckling loads are presented for a rectangular plate with different boundary conditions, various powers of FGM and some aspect ratios.     

Buckling analysis of orthotropic thin rectangular plates subjected to nonlinear in-plane distributed loads using generalized differential quadrature method

In the present work, buckling analysis of orthotropic thin rectangular plates with uniform thickness resting on Pasternak foundation are investigated for eight types of boundary conditions: SSSS, CCCC, SCSC, SSSC, SSCC, CCCF, SSFC, and CFCF. Based on classical plate theory, governing differential equation in buckling are solved numerically using generalized differential quadrature method (GDQM) to obtain critical buckling loads and corresponding modes. The kinds of nonlinear loading are presented in six cases including symmetrical and unsymmetrical distribution. In addition, the effects of aspect ratio, orthotropic moduli ratio and coefficients of foundation on the buckling load are illustrated. The present work is the first attempt to consider the influence of the nonlinearity of distributed in-plane bi-directional loading in determination of buckling load and representation of the corresponding shape modes. Some numerical examples are provided to demonstrate good accuracy of the GDQ method to evaluate the critical buckling load in case of nonlinear distributed bi-directional compressive loads. As shown, profile of distributed in-plane loading plays an important role on buckling behavior of the rectangular plate.     

Experimental study of dynamic buckling of plates under fluid–solid slamming

This paper describes the experimental investigation of the elastic–plastic dynamic buckling properties of rectangular plates under in-plane fluid–solid slamming. Based on the observation of elastic–plastic dynamic response characteristics of the plates, a dynamic buckling criterion and a dynamic yielding criterion are defined. The corresponding critical impulse are determined from the experimental results for each tested plate. The effect of different boundary conditions on the elastic–plastic dynamic buckling properties of plates is also examined. The results indicate that dynamic buckling always takes place elastically for the types of rectangular plates tested under fluid–solid slamming. The dynamic buckling modes of the plates are governed by the plate fundamental transverse free vibration mode. It is also found that boundary conditions strongly affect the dynamic buckling properties of plates subjected to fluid–solid slamming loads. Strengthening plate boundary constraint is a very effective way to enhance the plates’ ability to resist dynamic buckling.     

Differential quadrature analysis of functionally graded circular and annular sector plates on elastic foundation

The main purpose of this study is to investigate buckling and free vibration behaviors of radially functionally graded circular and annular sector thin plates subjected to uniform in-plane compressive loads and resting on the Pasternak elastic foundation. In-plane compressive loads may be applied to either radial, circumferential, or all edges of circular/annular sector plates. Based on the classical plate theory (CPT), critical buckling loads and fundamental frequencies of the circular/annular sector plates under simply-supported and clamped boundary conditions are obtained by using differential quadrature method (DQM). The inhomogeneity of the plate is characterized by taking exponential variation of Young’s modulus and mass density of the material along the radial direction whereas Poisson’s ratio is considered to be constant. Convergence study is carried out to demonstrate the stability of the present method. To confirm the excellent accuracy of the present approach, a few comparisons are made for limited cases between the present results and those available in literature. Critical buckling load and fundamental frequency parameters of the circular/annular sector thin plates are computed for different boundary conditions, various values of the material inhomogeneity constants, sector angles, and inner to outer radius ratios.     

三边简支一边固支矩形薄板动力屈曲解析解

根据板的动力平衡方程和压缩波前附加约束方程,基于双特征参数法和应力波理论,求解了三边简支一边固支矩形薄板在面内轴向冲击载荷作用下动力屈曲位移的解析解。揭示了矩形薄板动力屈曲过程中板的厚宽比、屈曲模态、冲击载荷大小和临界屈曲长度之间的关系。计算结果表明,由于横向惯性效应的存在,动力屈曲的临界载荷要比静力屈曲的大得多。     

Effect of in-plane boundary restraints on optimal design of skew laminates under buckling loads

Symmetrically laminated cross-ply and angle-ply skew plates subject to uniaxial buckling loads and various combinations of in-plane boundary restraints are studied using a shear deformable theory. For this purpose a finite element code is developed and applied to a couple of verification problems. The formulation of the parabolic iso-parametric plate element is briefly given and numerical results obtained for the verification problems related to stability analysis and stress diffusion are presented. The effect of in-plane restraints on the non-uniform distribution of in-plane stresses is studied by means of contour graphs. Next the buckling loads are maximized with respect to layer thicknesses in the case of cross-ply laminates and with respect to fiber orientations in the case of angle-ply laminates. The optimization results show that the exclusion of the in-plane restraints, which arise in several engineering applications, may lead to errors in the stability analysis and consequently in the design of laminated plates against buckling.