线性分布载荷作用下双模量圆板的计算分析

双模量圆板在线性载荷作用下,会形成各向同性的拉伸区和压缩区.可将双模量圆板看成两种各向同性材料组成的层合板,采用弹性理论建立双模量圆板在外载荷作用下的静力平衡方程,利用此静力平衡方程即可确定双模量圆板的中性面位置.建立双模量圆板在外载荷作用下的弯曲微分方程,求得双模量圆板在线性分布载荷作用下的挠度方程.通过算例讨论分析双模量对圆板弯曲变形的影响,得到圆板材料拉压弹性模量相差较大时,其挠度计算不宜采用相同弹性模量经典薄板理论,而应该采用双模量薄板理论的结论.     

用单自由度弹性系统研究双模量圆板的冲击问题

在考虑双模量圆板质量的基础上,研究了重物对双模量圆板的冲击问题。把被冲击的双模量圆板简化为一集中质量与无重量弹簧相连接的单自由度弹性系统,使重物对双模量圆板的冲击问题转化为重物对具有集中质量单自由度弹性系统的冲击问题,然后采用动力学方程推导出了重物对双模量圆板的冲击力、冲击时间、动载荷系数的函数表达式,解决了能量法仅能给出动载荷系数的缺陷,指出有关板壳理论专著给出的动载荷系数公式,仅是动力学方程推导出的动载荷系数公式的特例。当拉压弹性模量相差较大时,不能把重物对双模量圆板的冲击问题简单处理为重物对单弹性模量圆板的冲击问题,必须考虑拉压弹性模量不同的因素对圆板冲击问题的影响。     

非线性变厚度圆薄板轴对称弯曲问题的变分解答

基于能量原理,推导出均布载荷作用下变厚度圆薄板轴对称弯曲的变分列式,应用计算代数系统Mathematica编制程序,计算得到不同板厚参数下的挠度方程和最大挠度因子。结果表明,里茨法的计算过程易于实现程序化,计算精度高,在求解变厚度圆薄板小挠度弯曲问题时是有效的。与等厚度板相比较,变厚度板在弯曲刚度、抗屈曲和振动的性能等方面都有明显提高,因而在工程中得到广泛应用。变厚度圆薄板的厚度通常仅是半径的函数,并且受到的载荷关于板轴线对称,求解板的变形、内力、应力等即形成变厚度圆薄板轴对称弯曲问题。     

横向磁场中载流薄板模态截断问题研究

根据板壳理论与磁弹性理论,在不考虑感应电场,仅考虑机械场与磁场的相互耦合作用情况下,在薄板非线性运动方程、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,建立在横向磁场和机械载荷共同作用下的大挠度载流矩形薄板的非线性运动方程.以三边简支一边自由矩形薄板为例,给出板的单模态运动方程和双模态运动方程.利用数学计算软件,采用四阶Ronger-Kuta数值方法,模拟非线性系统在单、双模态位移模式下的时程图、庞加莱截面图、相轨迹图.讨论电磁参数和外载荷参数对板在单、双模态位移模式下的非线性行为的影响及差异.结果表明,这些参数对薄板的运动有较大的影响,通过调整电磁参数可控制系统的混沌运动,以实现对系统运动特性的控制.     

圆锯片受辊压适张度作用时固有频率的变化规律

基于弹塑性板弯曲自由振动微分方程,建立了考虑面内膜应力作用下圆薄板有限元动力平衡方程。从理论上探讨了圆锯片受适张度应力作用时固有频率的变化规律,提出了合理的圆锯片辊压适张度评价准则。试验验证了理论方法的正确性。     

基于大挠度理论的减振器阀片精确变形模拟和研究

为获得筒式减振器环形阀片弯曲变形的大挠度表达式与半径的关系,基于圆薄板大挠度理论,提出了薄板变形问题表达式内在统一的表示,结合针对环板外边缘挠度的大挠曲变形解析式与小挠曲变形方程,推导出环形阀片大挠曲变形与半径相关的混合解法解析式与变形修正系数。利用ABAQUS有限元软件对环形阀片进行了仿真分析,验证了混合解法解析式的精确度。分析了基于混合解法的叠加阀片弯曲变形,对叠加阀片的等效厚度与弯曲变形刚度进行了研究,得出的解析式与结论可用于减振器阀片的设计、调校与仿真分析。     

柱形杜瓦容器圆端板的结构设计与分析

杜瓦瓶是射电望远镜上接收机系统的前端。文中针对一种柱形杜瓦容器的结构特点，应用经典板壳力学理论，分析计算了在两种实验工况下．即大气压力单独作用、及大气压力与横向外力同时作用时，圆端板的结构尺寸。推导出了均布载荷及横向载荷共同作用下的中心开孔圆板挠度公式。并在ANSYS上，建立了模拟真实载荷条件下杜瓦容器的有限元模型．计算了变形场，逆向检验了结构的可靠性。     

光学检测下气浮支承的玻璃薄板变形

液晶玻璃基板在线检测过程中对玻璃板在垂直方向上的变形量有严格的要求,为了确定在指标要求光学检测精度下的喷嘴间距。本文基于弹性薄板的小挠度弯曲理论对气浮支承下的液晶玻璃板进行理论分析,推导出液晶玻璃薄板在吹吸喷嘴作用下的最大挠度计算公式,分析得出最大挠度与通孔间距的二次方、载荷集度成正比;通过Fluent对液晶玻璃基板气浮支承系统进行仿真,得到了不同的喷嘴孔间距下的载荷分布以及玻璃基板最大位移处受到载荷的准确值,从满足玻璃板最大位移要求、气膜面的压力分布状况及经济性方面综合考虑得到气膜单元的通孔横向间距范围,给出了采用气浮支承传输的液晶玻璃基板光学检测仪器的喷嘴布置参数,即喷嘴的合理间距应处于20~25mm之间。     

耦合场中弹性圆形薄板在混沌状态下的应力分析

在给出圆薄板的非线性电磁弹性耦合运动基本方程及电磁力表达式的基础上,得到在横向稳恒磁场、环向电流和机械载荷共同作用下简支圆薄板的振动方程,并采用四阶Runge-Kutta法求解方程,得出圆板的弹性变形及应力状态.通过变化磁感应强度和电流密度,使系统由周期状态进入混沌状态;由分岔图与最大Lyaponov指数图判定系统是否进入混沌状态;并讨论磁场与电流对系统应力状态的影响.     

机械载荷作用下梯度多孔材料圆板非线性力学行为的研究

基于一阶剪切变形圆板理论,应用最小势能原理,推导了梯度多孔材料圆板在径向载荷与横向载荷共同作用时的控制微分方程及边界条件,并将其退化为经典板理论下的结果。利用打靶法求解圆板非线性力学行为的数值解,并根据结果分析了梯度多孔材料的性质、机械载荷及边界条件等因素对圆板非线性力学行为的影响。     

Nonlinear resonance of the rotating circular plate under static loads in magnetic field

The rotating circular plate is widely used in mechanical engineering, meanwhile the plates are often in the electromagnetic field in modern industry with complex loads. In order to study the resonance of a rotating circular plate under static loads in magnetic field, the nonlinear vibration equation about the spinning circular plate is derived according to Hamilton principle. The algebraic expression of the initial deflection and the magneto elastic forced disturbance differential equation are obtained through the application of Galerkin integral method. By mean of modified Multiple scale method, the strongly nonlinear amplitude-frequency response equation in steady state is established. The amplitude frequency characteristic curve and the relationship curve of amplitude changing with the static loads and the excitation force of the plate are obtained according to the numerical calculation. The influence of magnetic induction intensity, the speed of rotation and the static loads on the amplitude and the nonlinear characteristics of the spinning plate are analyzed. The proposed research provides the theory reference for the research of nonlinear resonance of rotating plates in engineering.     

NON-LINEAR DYNAMIC BEHAVIOR OF THERMOELASTIC CIRCULAR PLATE WITH VARYING THICKNESS SUBJECTED TO NON- CONSERVATIVE LOADING

The non-linear dynamic behaviors of thermoelastic circular plate with varying thickness subjected to radially uniformly distributed follower forces are considered. Two coupled non-linear differential equations of motion for this problem are derived in terms of the transverse deflection and radial displacement component of the mid-plane of the plate. Using the Kantorovich averaging method, the differential equation of mode shape of the plate is derived, and the eigenvalue problem is solved by using shooting method. The eigencurves for frequencies and critical loads of the circular plate with unmovable simply supported edge and clamped edge are obtained. The effects of the variation of thickness and temperature on the frequencies and critical loads of the thermoelastic circular plate subjected to radially uniformly distributed follower forces are then discussed.     

Ultimate state of a plate with a regular system of stringers and cracks issuing from a circular hole

A fracture mechanics problem on crack development in a stiffened plate with a round hole is considered. A crack model with domains in which crack borders interact is used. This interaction in the end domain is simulated by introducing bonds (cohesive forces) between the crack borders. A boundary problem on the equilibrium of cracks issuing from the surface around the circular hole and exposed to external tensile loads is reduced to a nonlinear singular integral equation. From solving this equation, stresses in bonds are found. The condition of crack development is formulated taking into account a criterion of ultimate opening of interparticle bonds of material.     

Post-buckling stability of orthotropic, linear elastic, rectangular plates under biaxial loads

The potential energy function in a neighborhood of the buckling point for a biaxially loaded, linear elastic, orthotropic, simply supported, rectangular plate is obtained from a perturbation analysis. The perfect system has two independent bifurcation parameters, the loads. The postbuckling behavior is stable, and a good estimate is found for the post-buckling deflection of the plate in terms of the loads. The orthotropic constitutive equation interacts with the biaxial loading to cause a bimodal buckling point for certain combinations of loads; this point is also stable. Away from the bimodal point, the equilibrium surface is described as a cusp cylinder. At the bimodal point, the equilibrium surface is a double cusp.     

An exact solution for buckling of functionally graded circular plates based on higher order shear deformation plate theory under uniform radial compression

In this research, mechanical buckling of circular plates composed of functionally graded materials (FGMs) is considered. Equilibrium and stability equations of a FGM circular plate under uniform radial compression are derived, based on the higher order shear deformation plate theory (HSDT). Assuming that the material properties vary as a power form of the thickness coordinate variable z and using the variational method, the system of fundamental partial differential equations are established. A buckling analysis of a functionally graded circular plate (FGCP) under uniform radial compression is carried out and the results are given in closed-form solutions. The results are compared with the buckling loads of plates obtained for FGCP based on the first order shear deformation plate theory (FSDT) and classical plate theory (CPT) given in the literature. The study concludes that HSDT accurately predicts the behavior of FGCP, whereas the FSDT and CPT overestimates buckling loads.     

Free vibration analysis of a thin rectangular plate with multiple circular and rectangular cut-outs

The present work is to investigate the variation in the natural frequency of a rectangular plate with the change in position of cut outs of different sizes along its diagonal and major axis line by considering different aspect ratios of plates. In this regard the free vibration analysis of an isotropic rectangular plate of various aspect ratios with different sizes of multiple circular and rectangular cut-outs is carried out by using an Independent coordinate coupling method (ICCM) under simply supported boundary condition. The ICCM utilizes independent coordinates separately for plate domain and hole domain, in which the reduced mass and stiffness matrices can be derived, by matching the deflection conditions for each hole imposed on the expressions. The resulting equation is useful for the calculation of the Eigen values. The position, size, and number of cutouts have been varied in all the possible ways to investigate their effects on the natural frequency of the rectangular plate.     

Buckling analysis of circular plates of functionally graded materials under uniform radial compression

This study presents the buckling analysis of radially loaded solid circular plate made of functionally graded material. The edge of the plate is either simply supported or clamped and the plate is assumed to be geometrically perfect. The equilibrium and stability equations, derived through variational formulation, are used to determine the prebuckling forces and critical buckling loads. The equations are based on Love–Kirchhoff hypothesis and the Sander's non-linear strain-displacement relation. The results are verified with the known results in the literature.     

Dynamic buckling of isotropic and orthotropic shallow spherical cap with circular hole

The axisymmetric dynamic behaviour of clamped isotropic and orthotropic spherical cap with central circular hole under a uniform step pressure of infinite duration is investigated. The critical loads are determined by using the rapidly converging Chebyshev series in a space domain and a Houbolt numerical integration scheme in time domain. Three different cases of openings are investigated and detailed numerical results have been obtained for the isotropic case and two different cases of orthotrophy, which may be useful for design engineers.     

Bending and extension of a multilayered plate with body forces and thermal loading

A multilayered plate composed of thin layers of isotropic materials is analyzed. The problem for the multilayered plate with body forces is formulated by using the lamination theory in which displacement fields are expressed in terms of in-plane displacements on a main plane and transverse displacement. Placing the main plane at an appropriate distance from the lower surface of the plate, a set of equilibrium equations is shown to be written in uncoupled forms, which are identical to those for an uncoupled plate such as a single layer plate. It is proved that the complete solutions of the multilayered plates subject to the specified in-plane resultant tractions or in-plane displacements on its whole boundary can be obtained from the sum of solutions for uncoupled plates. Closed form solutions are obtained for a circular laminate clamped or simply supported on its the boundary as well as for a rotating disk with a constant angular velocity. The calculations of thermoelastic stresses and displacements in multilayered plates are also discussed. Closed form solutions are obtained for a circular laminate with distributed temperature varying in the radial direction and through the thickness.