混合能量原理求解矩形板在静水压力作用下的弯曲

本文从能量原理出发,以混合变量的最小势能原理为理论指导,对其进行进一步的研究。求解出了静水压力作用下三边简支一边固定、两邻边固定两邻边简支、三边固定一边简支三种不同边界条件下矩形板弹性阶段的挠曲面方程,并通过应用数值分析软件对方程组求解,将所求得的数值解与有限元的模拟值进行数值分析。对于矩形板在静水压力作用下的弯曲问题已经有很多相关研究,但本文方法是一个新的方法。结果表明：本文研究方法对于工程实际中各种相关问题拥有良好的实用性,计算方法为工程实际问题提供了一个新的途径。     

角点悬空弯曲厚矩形板的边界积分法

在边界积分法中引用了拟基本系统矩形板,在该拟基本系统与实际系统之间应用功的互等定理,得到一挠曲面方程的积分表达式,只要对此表达式进行极简单的积分便可得到该挠曲面方程,这比直接求解Reissner挠度控制方程要简单,边界积分法的求解过程概念清晰,计算伊始便给出了挠曲面方程的总体表达式.以Reissner厚板理论为基础,应用边界积分法研究了角点悬空厚矩形板的弯曲问题,给出了在集中荷载作用下两邻边固定另两邻边自由且角点悬空弯曲厚矩形板的封闭解析解,并给出了相应的数据和图表以供工程上的应用和参考.     

功的互等法在简谐分布力矩下矩形板受迫振动问题的应用

从功的互等法出发,研究了薄板在简谐分布力矩作用下的受迫振动问题.给出了三条边固定另一条边简支、三条边固定另一条自由矩形板受迫振动的挠曲线方程,并进行了数值运算,得到了一系列数据.通过与给出的Ansys值对比,其误差小于5％,表明了给出的挠曲线方程和计算结果的正确性.给出的计算矩形板受迫振动问题的方法,避免了传统方法庞大的高阶偏微分方程组和复杂的求解过程,不仅具有一定的理论价值,而且可以直接用于工程实际.     

求解弯曲矩形板受迫振动的混合变量法

应用混合变量最小作用量原理,求解了两邻边固定、另两邻边自由弯曲矩形板在均匀谐载作用下的受迫振动问题,得到其受迫振动的稳态解．所获得的计算结果,跟现有文献进行比较,证明其给出的方法是正确的,因此不仅具有重要的理论价值,而且可以为工程实际直接采用．     

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.     

任意边界条件下双模量矩形薄板的弯曲

将双模量板等效为两个各向同性小矩形板组成的层合板,假定该层合板的中性面即为两个小矩形板的交界面。根据中性面上应力为零且薄板全厚度上应力的代数和为零,推导了双模量矩形薄板的中性面位置。本文采用严宗达提出的带补充项的双重正弦傅里叶级数通解,该通解可以适用于任意边界条件的矩形薄板且不需要叠加或者重新构造。联立边界条件和控制方程,求得通解中的待定系数并代入到通解中,即可得到任意边界条件下双模量矩形薄板的弯曲解析解。与有限元结果比较,本文结果符合工程精度要求。     

求解矩形夹层板在集中载荷下的稳定问题

在考虑了横向切应力和横向正应力对夹层板稳定影响的情况下,给出了矩形夹层板结构屈曲失稳的控制方程、基本解以及边界条件。应用功的互等定理求解了在均布载荷作用下的矩形夹层板的屈曲失稳问题。     

应用混合变量余能原理求解不同载荷作用下四边简支矩形板的弯曲

由功的互等定理导出了弯曲矩形板混合变量的总余能,应用混合变量余能原理求解四边简支矩形板弯曲问题,给出了四边简支矩形板的混合变量余能表达式,求解了不同载荷作用下四边简支矩形板的弯曲问题,并将计算的不同载荷作用下的挠度和弯矩值与ANSYS有限元的计算值比较,给出了一种求解四边简支矩形板的新方法。     

不同边界条件下波动方程解的对应关系研究

同一结构在两种不同边界条件下的声振结果存在某种联系,这种联系可用来研究飞行器地面模拟试验环境与空中飞行环境下的状态关系。对此从一般的弹性体波动方程出发,基于载荷等效原则,应用变分原理和偏微分方程理论,对同一结构在不同边界条件下的内在联系进行了研究,证明了这种内在联系的存在性。研究结果表明:响应变化与边界扰动间存在的平方关系;响应变化幅度估计与精确解相比在一个数量级上。     

冲击载荷作用下矩形薄板的弹性动力屈曲

为了研究冲击载荷作用下考虑应力波效应弹性矩形薄板的动力屈曲,根据动力屈曲发生瞬间的能量转换和守恒准则,导出板的屈曲控制方程和波阵面上的补充约束条件,真实的屈曲位移应同时满足控制方程和波阵面上的附加约束条件。满足上述条件,建立了该问题的完整数值解法,对屈曲过程中冲击载荷、屈曲模态和临界屈曲长度之间的关系进行研究,定量计算了横向惯性效应对提高薄板动力屈曲临界应力的贡献。研究表明：板的厚宽比一定时,临界屈曲长度随冲击载荷的增大而减小;由于屈曲时的横向惯性效应,应力波作用下薄板一阶临界力参数是相应边界板的静力失稳临界力参数的1.5倍;随着边界约束逐渐减弱,板临界力参数逐渐减小,动力特征参数逐渐增大。

     

THE METHOD OF THE RECIPROCAL THEOREM OF FORCED VIBRATION FOR THE ELASTIC THIN RECTANGULAR PLATES (III)—CANTILEVER RECTANGULAR PLATES

In this paper, applying the method of the reciprocal theorem, we give the stationary solutions of the forced vibration of cantilever rectangular plates under uniformly distributed harmonic load and concentrated harmonic load acting at any point of the plates, the figures and tables of number value of bending moment and the deflection amplitudes as well.     

Fluctuation strength of modulated sound radiated from rectangular plates with mixed boundary conditions

A generalized differential quadrature method is developed for solving the sound radiated from the forced vibrating rectangular plates with mixed boundary conditions in this paper. The fluctuation strength of the radiated sound, which is modulated by another sound near the plates, is studied. The effects of the modulation frequency and the modulation degree on fluctuation strength are revealed. The effects of the radiated sound frequency and the structural modal density are also studied and compared. The numerical results are presented to show the characteristics of the fluctuation strength of the modulated sound radiated from rectangular plates with mixed boundary conditions.     

中厚板统计分析的随机边界元法

本文建立了分析含随机材料参数并具厚度不均匀性的中厚板问题的随机边界元法,基于Taylor级数展开技术,分析和到广义位移的均值和一阶偏差的积分方程,其中将材料参数的随机性和厚度的不均匀性作为等效荷载处理,从而得到广义边界位移或面力的均值和协方差,并进一步求出部点广义位移和内力的均值和协方差,最后用本文方法计算了两个数例,并对所得结果进行了分析,探讨。     

The vibration and stability analysis of moderate thick plates by the method of lines

The method of lines based on Hu Hai-chang's theory for the vibration and stability of moderate thick plates is developed. The standard nonlinear ordinary differential equation (ODE) system for natural frequencies and critical load is given by use of ODE techniques, and then any indicated eigenvalue could be obtained directly from ODE solver by employing the so-called initial eigenfunction technique instead of the mode orthogonality condition.Numerical examples show that the present method is very effective and reliable.     

混合边界各向异性矩形板的静力分析

采用一般解析解和配点法相结合的方法,求解混合边界各向异性矩形板的弯曲问题.先由弯曲挠度的微分方程求出各种类型的齐次解和特解,然后组成一般解析解,再将板的每个边等分 为很多微小的段,仅对每一微段的中点建立应满足的边界条件,由全部边界条件方程式即可求得全部积分常数.以每边一半边界为平夹、另一半边界为简支或自由的方板为例进行了计算,并与四边均为简支的方板进行了对比,表明理论简单,结果实用.     

Numerical solution of the unsteady Euler equations for airfoils using approximate boundary conditions

This paper presents an efficient numerical method for solving the unsteady Euler equations on stationary rectilinear grids. Boundary conditions on the surface of an airfoil are implemented by using their first-order expansions on the mean chord line. The method is not restricted to flows with small disturbances since there are no restrictions on the mean angle of attack of the airfoil. The mathematical formulation and the numerical implementation of the wall boundary conditions in a fully implicit time-accurate finite-volume Euler scheme are described. Unsteady transonic flows about an oscillating NACA 0012 airfoil are calculated. Computational results compare well with Euler solutions by the full boundary conditions on a body-fitted curvilinear grid and published experimental data. This study establishes the feasibility for computing unsteady fluid-structure interaction problems, where the use of a stationary rectilinear grid offers substantial advantages in saving computer time and program design since it does not require the generation and implementation of time-dependent body-fitted grids.     

A theoretical and experimental investigation of a primary resonance of a three circular plates torsion vibration system

I.IntroductionRotor-shaftingiswidelyusedinengineering,androtor-shaftingtorsionvibrationisgainingattentionwidespreadly.Inthispaper,themodeloftherotor-shaftingtorsionvibrationofa200MWturbogenerationsetisdesignedandathreecircularplatestorsionvibrationsystemwithcubicnonlinearitiestoasimple-harmonicexcitationisstudied.TheobjectiveofthepaperistostudythedynamicsphenomenaofthesystemwhileQ=co2.Themethodofaveragingisusedandthesteadystateresponsebifurcationequationanditssingularityanalysisaregiven.Thet…     

Transfer matrix method for free and forced vibrations of multi-level functionally graded material stepped beams with different boundary conditions

Functionally graded materials(FGMs) are a novel class of composite materials that have attracted significant attention in the field of engineering due to their unique mechanical properties. This study aims to explore the dynamic behaviors of an FGM stepped beam with different boundary conditions based on an efficient solving method.Under the assumptions of the Euler-Bernoulli beam theory, the governing differential equations of an individual FGM beam are derived with Hamilton's principle and decoupled via the separation-of-variable approach. Then, the free and forced vibrations of the FGM stepped beam are solved with the transfer matrix method(TMM). Two models,i.e., a three-level FGM stepped beam and a five-level FGM stepped beam, are considered,and their natural frequencies and mode shapes are presented. To demonstrate the validity of the method in this paper, the simulation results by ABAQUS are also given. On this basis, the detailed parametric analyses on the frequencies and dynamic responses of the three-level FGM stepped beam are carried out. The results show the accuracy and efficiency of the TMM.