求解多跨连续梁固有振动精确解的一种方法

本文将多跨连续梁按单跨梁来处理,而将中间支座的支反力看作作用在梁上的未知外力,对于具有任意有限个中间支座的多跨连续梁,其横向振动的频率方程和振型函数可分别用一个统一的解析式来表示.     

两对边简支厚度按指数规律变化矩形板横向自振频率的渐近解法

本文提供了一个求解两对边简支、厚度按指数规律变化的变厚度矩形板横向自振频率的渐近解法,求得了其横向自振的一级渐近解。作为算例,给出了二对边简支、另两对边固支的变厚度矩形板一级近似自振频率的计算公式.自振频率的计算非常简单,且精度可满足工程需要。     

矩形板受边缘荷载的若干格林函数及其应用

本文求得了两对边简支,两对边自由的矩形板及四边简支矩形板受单位边缘剪力或弯矩作用下的若干格林函数。通过叠加原理和力法,可用于解决在横向载作用下具有各种非连续边界条件的矩形板的弯曲问题。文中给出了具体应用的方法和算例。     

Maxwell模型薄板的自由振动

本文利用Ｍａｘｗｅｌ粘弹性模型建立了粘弹性薄板的振动微分方程，给出四边简支粘弹性矩形薄板的固有频率解析解．对粘弹性矩形薄板的振动特性进行了讨论     

线性变厚度矩形薄板自由振动的精确解

基于小挠度薄板理论，采用Ｌｅｒｙ法结合Ｆｒｏｂｅｎｉｕｓ法构造的幂级数解，得到了两对边简支另两对边为ＳＳ、ＣＳ、ＦＦ支承的三种线性变厚度矩形薄板的自振频率随板的边长比及厚度比变化的精确解及其振型函数的解析表达式。     

附着了任意个弹性质量的任意形状的膜的振动

本文提供了一个精确求解附着了任意个弹性质量的任意形状膜的振动的新方法。将弹性质量对膜的作用反力视为作用于膜上的未知外力,求出了包含有未知反力的膜的运动方程的精确解,利用附加弹性质量的运动方程导出频率方程。最后以附着了任意个弹性质量的圆膜为例给出了其频率方程的具体计算公式,并用数值计算了对称附着两个刚性质量的圆膜的固有振动频率。     

具有高阶剪切效应的粘弹性板准静态分析的DQ法

本文对基于Reddy的高阶剪切理论及线性粘弹性材料的Boltzmann本构定律建立的高阶剪切粘弹性板准静态分析的数学模型，在空域上应用推广的DQ技术对模型进行简化，求得了问题的DQ近似解析解；得到了横向阶跃载荷作用下的粘弹性简支板的准静态响应；考察了几何、材料参数及横向剪切效应对粘弹性板拟静态弯曲行为的影响。为说明该方法的可靠性和有效性，将考虑剪切变形及不计剪切变形的DQ数值结果与粘弹性薄板精确解进行了比较，同时研究了数值结果的收敛性。结果表明该方法具有收敛性好，计算精度高，计算量少等优点。     

横向磁场中对边简支对边固支矩形薄板的几何非线性因素忽略的条件

在横向稳恒磁场和载荷共同作用下，以磁弹性薄板的振动方程为基础，利用谐波平衡法研究了对边简支对边固支矩形薄板的非线性振动特性；推导出了频率响应方程，并分析了其频率响应特性；讨论了矩形薄板的非线性因素的影响，得出了在对横向稳恒磁场和载荷共同作用下的矩形薄板进行设计、计算分析时其几何非线性因素忽略的条件。只有在各参数满足此条件时才可以不考虑横向稳恒磁场和载荷共同作用下该矩形薄板的几何非线性因素的影响。     

角支及多点支承矩形板的弯曲

本文取两对边简支另两对边自由的板为初始解,用迭加法在两边简支板上迭代消去板边上的剪力。为了简化消去板边剪力的复杂迭代过程,作者提出了高精度的简化方法,将无限迭代简化为一次计算,将角支板的求解化为计算两个对边简支矩形板的简单问题。对于多点支承矩形板,则可取角点支承板为基本结构用力法求解。文中还提出了一些实用经验公式,列出了典型算例,验证了方法的适用性和高精度。     

弹性半空间地基与四边自由异性矩形板相互作用的研究

选用弹性半空间地基模型分析四边自由各向异性矩形地基板的弯曲和稳态振动解析解。将异性薄板控制微分方程与基于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,然后采用三角级数法得出了弹性半空间地基上四边自由各向异性矩形薄板的弯曲和稳态振动解析解,包括地基反力(幅值)、板的挠度(幅值)、板的内力(幅值)的解析表达式。克服了数值法的弊端,取消了对地基反力的假设,得到了板的内力(幅值)及地基反力(幅值)更切实际的分布规律。算例结果不但与文献结果吻合良好,而且表明对于异形板,对称载荷能引起反对称的内力和变形。该方法使得半空间地基上各向异性矩形薄板这一复杂的接触问题的求解统一化、简单化、规律化。     

AN ANALYTICAL SOLUTION OF TRANSVERSE VIBRATION OF RECTANGULAR PLATES SIMPLY SUPPORTED AT TWO OPPOSITE EDGES WITH ARBITRARY NUMBER OF ELASTIC LINE SUPPORTS IN ONE WAY

ＡＮＡＮＡＬＹＴＩＣＡＬＳＯＬＵＴＩＯＮＯＦＴＲＡＮＳＶＥＲＳＥＶＩＢＲＡＴＩＯＮＯＦＲＥＣＴＡＮＧＵＬＡＲＰＬＡＴＥＳＳＩＭＰＬＹＳＵＰＰＯＲＴＥＤＡＴＴＷＯＯＰＰＯＳＩＴＥＥＤＧＥＳＷＩＴＨＡＲＢＩＴＲＡＲＹＮＵＭＢＥＲＯＦＥＬＡＳＴＩＣＬＩＮＥ...     

Vibration of open circular cylindrical shells with intermediate ring supports

This paper is concerned with the free vibration of open circular cylindrical shells with intermediate ring supports. An analytical procedure for determining the free vibration frequencies of such shells is developed based on the Flügge thin shell theory. An open circular cylindrical shell is assumed to be simply supported along the two straight edges and the remaining two opposite curved edges may have any combinations of support conditions. The shell is divided into multiple segments along the locations of the intermediate ring supports. The state-space technique is employed to derive the exact solutions for each shell segment and the domain decomposition method is applied to enforce the geometric and natural boundary/interface conditions along the interfaces of the shell segments and the curved edges of the shell. Comparison studies are carried out to verify the correctness of the proposed method. Exact vibration frequencies are obtained for open circular cylindrical shells with multiple intermediate ring supports.The influence of the number of intermediate ring supports, the locations of the ring supports, the boundary conditions and the variation of the included angle of the shells on the natural frequencies are examined. The exact vibration solutions can be used as important benchmark values for researchers to check their numerical methods and for engineers to design such shell structures.     

具有自由边的复合材料层合板的解析解

从三维弹性力学基本方程出发,通过假设自由边的边界位移函数,建立了正交异性层合板的状态方程,给出了对边自由,对边简支矩形板的解析解.此解满足层合板的基本方程和层间连续条件.用本文的方法比较容易处理层合板的自由边.算例表明,数值结果具有较高的精度.     

Vibration of arbitrarily shaped membranes with elastical supports at points

This paper presents a new method for solving the vibration of arbitrarily shaped membranes with elastical supports at points. The reaction forces of elastical supports at points are regarded as unknown external forces acting on the membranes. The exact solution of the equation of motion is given which includes terms representing the unknown reaction forces. The frequency equation is derived by the use of the linear relationship of the displacements with the reaction forces of elastical supports at points. Finally the calculating formulae of the frequency equation of circular membranes are analytically performed as examples and the inherent frequencies of circular membranes with symmetric elastical supports at two points are numerically calculated.     

Exact characteristic equations for some of classical boundary conditions of vibrating moderately thick rectangular plates

The dimensionless equations of motion are derived based on the Mindlin plate theory to study the transverse vibration of thick rectangular plates without further usage of any approximate method. The exact closed form characteristic equations are given within the validity of the Mindlin plate theory for plates having two opposite sides simply supported. The six distinct cases considered involve all possible combinations of classical boundary conditions at the other two sides of rectangular plates. Accurate eigenfrequency parameters are presented for a wide range of aspect ratio η and thickness ratio δ for each case. The three dimensional deformed mode shapes together with their associated contour plots obtained from the exact closed form eigenfunctions are also presented. Finally, the effect of boundary conditions, aspect ratios and thickness ratios on the eigenfrequency parameters and vibratory behavior of each distinct cases are studied in detail. It is believed that in the present work, the exact closed form characteristic equations and their associated eigenfunctions, except for the plates with four edges simply supported, for the rest of considered six cases are obtained for the first time.     

Transverse vibration of rectangular plates elastically supported at points on edges

This paper studies transverse vibration of rectangular plates with two opposite edges simply supported, other two edges arbitrarily supported and free edges elastically supported at points. A highly accurate solution is presented for calculating inherent frequencies and mode shape of rectangular plates elastically supported at points. The number and location of these points on free edges may be completely arbitrary. This paper uses impulse function to represent reaction and moment at points. Fourier series is used to expand the impulse function along the edges. Characteristic equations satisfying all boundary conditions are given. Inherent frequencies and mode shape with any accuracy can be gained.     

Transverse vibration characteristics of axially moving viscoelastic plate

The dynamic characteristics and stability of axially moving viscoelastic rect- angular thin plate are investigated.Based on the two dimensional viscoelastic differential constitutive relation,the differential equations of motion of the axially moving viscoelastic plate are established.Dimensionless complex frequencies of an axially moving viscoelastic plate with four edges simply supported,two opposite edges simply supported and other two edges clamped are calculated by the differential quadrature method.The effects of the aspect ratio,moving speed and dimensionless delay time of the material on the trans- verse vibration and stability of the axially moving viscoelastic plate are analyzed.     

Bending of uniformly loaded rectangular plates with two adjacent edges clamped, one edge simply supported and the other edge free

ＩｎｔｒｏｄｕｃｔｉｏｎＤｕｒｉｎｇｔｈｅｌａｔｅｓｅｖｅｎｔｉｅｓ,ＺｈａｎｇＦｕｆａｎｏｂｔａｉｎｅｄｔｈｅｅｘａｃｔｓｏｌｕｔｉｏｎｓｔｏｔｈｅｂｅｎｄｉｎｇｐｒｏｂｌｅｍｏｆｒｅｃｔａｎｇｕｌａｒｃａｎｔｉｌｅｖｅｒｐｌａｔｅｓａｎｄｒｅｃｔ...     

Winkler地基上四边自由正交各向异性矩形薄板弯曲问题的辛叠加解

研究Winkler地基上正交各向异性矩形薄板弯曲方程所对应的Hamilton正则方程, 计算出其对边滑支条件下相应Hamilton算子的本征值和本征函数系, 证明该本征函数系的辛正交性以及在Cauchy主值意义下的完备性, 进而给出对边滑支边界条件下Hamilton正则方程的通解, 之后利用辛叠加方法求出Winkler地基上四边自由正交各向异性矩形薄板弯曲问题的解析解. 最后通过两个具体算例验证了所得解析解的正确性.     

EXACT SOLUTIONS FOR FREE IN-PLANE VIBRATIONS OF RECTANGULAR PLATES

All possible exact solutions are successfully obtained in terms of 10 sets of distinct eigensolutions for the free in-plane vibration of isotropic rectangular plates. The plates have simply supported condition at two opposite edges and any combination of classical boundary conditions at the other two edges. The exact solutions are validated through both mathematical proof and comparisons with the solutions of differential quadrature method. Some unusual phenomena are revealed in free in-plane vibrations of rectangular plates due to one of the eigenvalues being zero. This work constitutes an improved version of very recent corresponding work by the same authors [Int. J. Mech. Sci., 2009, 51: 246-255]. Both the solution forms and solving procedures in the previous work are substantially simplified. Some new results are also given, which are useful for validation purpose in future.