弹性边界约束旋转功能梯度圆柱壳结构自由振动行波特性分析

对旋转功能梯度圆柱壳自由振动行波特性及边界约束影响进行了分析研究.将功能梯度材料的物理特性表示成沿壳体厚度方向指数变化的函数,基于Love壳体理论,将圆柱壳3个方向的振动位移场采用改进Fourier(傅立叶)级数方法展开, 进而改善位移函数在边界位置求导连续性,结合旋转圆柱壳结构能量原理描述与Rayleigh Ritz法,推导旋转功能梯度圆柱壳自由振动特征方程.通过将计算结果与现有文献结果对比验证了该文模型的正确性与收敛性.随后,通过算例讨论分析了功能梯度材料特性参数、几何参数、边界条件及约束弹簧刚度对旋转功能梯度圆柱壳自由振动行波振动特性的影响.结果表明:边界条件在环向波数n较小或长径比L/R较小的情况下对行波特性影响较为明显;随着厚径比H/R的增大,边界条件的影响逐渐减小;边界约束弹簧对行波特性影响程度取决于模态阶数情况;功能梯度材料特性参数对前后行波频率的影响随着模态序数的增大而逐渐增大.     

环向加筋圆柱壳自由振动的摄动解

本文采用奇异摄动中的PLK方法和作者在[13]中所提出的广义Hale定理,讨论研究了带有环向加强肋圆柱壳的自由振动,由此并给出了一个计算环向加筋圆柱壳固有频率的一般计算表达式。为了验证本文解的精确性,文中还采用数值方法对此作了对比,比较结果表明,摄动一阶近似解已达到较好的精度。     

厚壳理论及其在圆柱壳中的应用

本文从Hellinger-Reissner广义变分原理出发,以位移和应力的假设为基础,建立了厚壳理论.文中把壳体的位移展开为其厚度方向的幂级数,对平行和垂直于中面的位移分别保留其级数的前四项和前三项.并假定壳体的法向挤压和横向剪切应力沿壳厚为三次曲线,使其满足上下壳面上的应力条件,利用变分原理推导出分析厚壳所需的物理方程,平衡方程和边界条件.文中对圆柱壳的情况作了实例计算,并作了光弹性实验,结果表明理论和实验符合良好.     

约束层阻尼圆柱壳的自由振动

给出了被动约束层阻尼圆柱壳(PCLD)的自由振动特性．波传播法被用来求解两端简支的PCLD圆柱壳的振动,而不是用有限元法、传递矩阵法和Rayleigh-Ritz法．基于Sanders薄壳理论,导出了PCLD正交各向异性圆柱壳的控制方程．数值结果表明当前的方法要比目前其它方法有效．讨论了粘弹性层和约束层的厚度,正交各向异性约束层的弹性模量比率和粘弹性层的复剪切模量对频率参数和损失因子的影响．     

环向和纵向加肋非均匀大变形圆柱壳的自由振动*

环向和纵向加肋非均匀圆柱壳在航空,宇航等工业广泛运用,本文使用阶梯折算法得到了环向和纵向加肋非均匀大变形圆柱壳在任意边界条件下自由振动的一般解.问题最后归结为求解一个超越代数方程,这个方程可以用一个具体的解析表达式表示出来.文中还给出了收敛性证明和算例.算例表明,利用本文的方法,可得到满意的结果.     

正交各向异性旋转扁壳的非线性振动*

本文提出一种时间模态假设,由此导出描述圆柱正交各向异性薄扁球壳和锥壳非线性轴对称自由振动的非线性耦合的代数和微分特征值方程组.我们求出了该方程组的近似解析解,并获得壳体振动的幅频响应关系的渐近展开式.文中还讨论了壳体的几何及材料参量对其振动性态的影响.     

圆柱壳开孔的应力集中──非圆孔问题的一般解

本文从Donnell型圆柱壳的基本方程出发,利用复变函数方法和保角映射技术,对圆柱壳开非圆形孔的问题进行了研究.首先给出了逼近具有非圆形孔的圆柱壳开孔问题一般解的完备函数序列,构造出了问题的一般解;其次利用有关圆柱壳开小孔的假设概念,给出了圆柱壳开非圆孔时边界条件的一般表达式.进而利用正交函数展开的方法,将待解的问题归结为一组无穷代数方程组的求解问题,并进行直接求解.在本文最后,对圆柱壳开圆孔.椭圆孔附近的应力集中问题进行了数值计算,给出了分析结果.     

基于扭转模态的角振动压电俘能器研究

以线性压电理论为基础,分析了压电陶瓷圆柱壳的扭转振动问题.由于压电陶瓷柱壳的扭转振动使得覆盖于柱壳两端的电极之间出现电势差,通过导线连接两电极与外负载,则圆柱壳在振动过程中所捕获的能量能有效地供给微电子器件工作.得到了输出电压、电流、能量、效率以及输出功率密度的解析表达式,并数值分析了这类压电俘能器的基本性能.结果表明,这种结构能够用作压电俘能器,将旋转机械能转化成为电能.     

弹性圆柱壳扭转屈曲研究

本文给出两端固支的弹性圆柱壳扭转屈曲实验与理论计算结果.实验发现,对于较长的壳,其屈曲后的变形并不占据整个壳体的长度.另外在计算中仅考虑壳体的法向边界条件,而不考虑其周向和轴向边界条件,结果和Yamaki精确解以及本文实验结果相符较好,说明周向和轴向边界条件对圆柱壳的扭转屈曲影响较小.     

厚壁圆柱壳开孔应力集中问题的复变函数解法

本文基于考虑横向剪切变形影响的厚壳理论建立了求解圆柱壳开孔应力集中问题的复变函数方法，得到了此种问题的一般解和满足任意形开孔边界条件的表达式·该应力集中问题可以简化为求解无穷代数方程组的问题·用复变函数方法可以规范地求解应力集中问题·文中给出了圆柱壳开小圆孔和椭圆孔时应力集中系数的数值结果·     

Numerical analysis of free vibrations of laminated composite conical and cylindrical shells: Discrete singular convolution (DSC) approach

A numerical study on the free vibration analysis for laminated conical and cylindrical shell is presented. The analysis is carried out using Love's first approximation thin shell theory and solved using discrete singular convolution (DSC) method. Numerical results in free vibrations of laminated conical and cylindrical shells are presented graphically for different geometric and material parameters. Free vibrations of isotropic cylindrical shells and annular plates are treated as special cases. The effects of circumferential wave number, number of layers on frequencies characteristics are also discussed. The numerical results show that the present method is quite easy to implement, accurate and efficient for the problems considered.     

Buckling and free vibration analysis of high speed rotating carbon nanotube reinforced cylindrical piezoelectric shell

In this paper, buckling and free vibration behavior of a piezoelectric rotating cylindrical carbon nanotube-reinforced (CNTRC) shell is investigated. Both cases of uniform distribution (UD) and FG distribution patterns of reinforcements are studied. The accuracy of the presented model is verified with previous studies and also with those obtained by Navier analytical method. The novelty of this study is investigating the effects of critical voltage and CNT reinforcement as well as satisfying various boundary conditions implemented on the piezoelectric rotating cylindrical CNTRC shell. The governing equations and boundary conditions have been developed using Hamilton's principle and are solved with the aid of Navier and generalized differential quadrature (GDQ) methods. In this research, the buckling phenomena in the piezoelectric rotating cylindrical CNTRC shell occur as the natural frequency is equal to zero. The results show that, various types of CNT reinforcement, length to radius ratio, external voltage, angular velocity, initial hoop tension and boundary conditions play important roles on critical voltage and natural frequency of piezoelectric rotating cylindrical CNTRC shell.     

密封容器组合壳自由振动的精确解

给出了一类密封容器组合壳自由振动问题的精确解,基于Love经典薄壳理论,导出了具有任意经线形状的旋转壳体在轴对称振动时的基本方程,组合壳结构中球壳与柱壳的连接条件是通过连接处的变形连续性和内力平衡关系得出的。问题的数学模型被归结为常微分方程组在球壳和 壳两个区间上的特征值问题。振动模态函数是由Legendre和三角函数构造出来,并且得到了精确的频率方程。所有的计算都是在Maple程序下运行的,无论是精确的符号运算还是具有所需有效数学精度的数值计算,都表明该文所编译的Maple程序是简单而有效的。固有频率的数值结果同文献中有限元法和其它数值方法的结果作了比较。作为一个标准,该文给出的精确解对于检验各种近似方法的精密度是有价值的。     

Free nonlinear vibrations of statically loaded long cylindrical shells

Summary Large-amplitude global free vibration of a long cylindrical shell resting on an elastic foundations is considered. The shell is initially loaded by uniform static transverse forces.Both the static deflections of the shell and the nonlinear vibrations superimposed on static equilibrium are considered using nonlinear theory. Numerical analysis elucidates the effect of different parameters on vibrations.The version of this paper was presented at the Twentieth Midwestern Mechanics Conference, Purdue University, West Lafayette, Indiana, USA, August 31–Sept. 2, 1987.     

Free edge stress prediction in thick laminated cylindrical shell panel subjected to bending moment

A thick composite cylindrical shell panel with general layer stacking is studied to investigate the free edge and 3D stresses in the panel which is subjected to pure bending moment. To this aim, a Galerkin based layerwise formulation is presented to discretize the governing equation of the panel to ordinary differential equations. Employing a reduced displacement field for the cylindrical panel, the governing equations for thick panel are developed in terms of displacements and a set of coupled ordinary differential equations is obtained. The governing equations are solved analytically for free edge boundary conditions and applied pure bending moment. The accuracy of numerical results is examined and the distribution of interlaminar and in-plane stresses is studied. The free edge stresses are studied and the effect of radius to thickness ratio, width to thickness ratio and layer stacking on the distribution of stresses is investigated. The focus of numerical results is on the prediction of boundary layer and free edge stress distribution.     

A novel matrix method for coupled vibration and damping effect analyses of liquid-filled circular cylindrical shells with partially constrained layer damping under harmonic excitation

A novel matrix method is further developed for a liquid-filled circular cylindrical shell with partially constrained layer damping (CLD), which consists of treating liquid domain with Bessel function approach, and shell domain with transfer matrix equation based on a new set of first order matrix differential equation. In order to indicate its advantage to the finite element method (FEM), free vibration analysis on such an empty shell under clamped–clamped boundary are carried out by using the present method together with FEM. Meanwhile, coincident result is yielded for the liquid-filled shell by adopting the present method with by other transfer matrix method. Finally, a series of valuable numerical results are obtained by this method.     

Free vibration analysis of two-dimensional functionally graded cylindrical shells

In this paper, the free vibration of a two-dimensional functionally graded circular cylindrical shell is analyzed. The equations of motion are based on the Love’s first approximation classical shell theory. The spatial derivatives of the equations of motion and boundary conditions are discretized by the methods of generalized differential quadrature (GDQ) and generalized integral quadrature (GIQ). Two kinds of micromechanics models, viz. Voigt and Mori–Tanaka models are used to describe the material properties. To validate the results, comparisons are made with the solutions for FG cylindrical shells available in the literature. The results of this study show that the natural frequency of the material can be modified in order to meet the expected results through manipulation of the constituent volume fractions. A comprehensive comparison is then drawn between ordinary and 2-D FG cylindrical shells.