变截面压电层合梁自由振动分析

考虑压电材料的质量效应和刚度效应,将表面粘贴或埋入式压电悬臂梁看作变截面梁,研究压电材料对智能结构固有特性的影响。基于一阶剪切变形理论导出压电层合梁的抗弯刚度和横向剪切刚度,计及梁的剪切变形和转动惯量,采用Timoshenko理论推导变截面压电层合梁的频率方程。给出了T300/970压电层合梁和硬铝压电层合梁的前3阶固有频率,并和有限元结果、等截面梁的计算结果进行比较。计算表明,压电材料对压电结构固有频率和固有振型的影响显著,在以振动控制为目标的压电结构动力学建模过程中,有必要考虑压电材料的质量和刚度。     

基于压弯耦合效应下预应力梁的竖向自由振动研究

基于大位移广义变分原理,考虑梁的压弯耦合、剪切应变能和转动惯量的影响,建立了预应力梁的不完全广义势能泛函,通过对位移变分,推导出预应力梁自由振动微分方程。并以预应力混凝土简支梁和悬臂梁为例,通过引入边界条件,求出了自由振动频率的解答。对比Bernoulli-Eular梁和Timoshenko梁,详细分析了轴向荷载、剪切效应和转动惯量对自振频率的影响,研究发现,轴向压力荷载可使梁的自振频率降低,反之增大。剪切变形的影响约为转动惯量的3倍,随着主模态阶数的增加和长细比L/r的减小,轴向荷载、剪切变形和转动惯量的影响非常显著。因此,对于预应力混凝土梁,当跨高比L/h≤8,或长细比L/r≤28时,必须考虑轴向荷载、剪切变形和转动惯量的影响,通过与Bernoulli-Eular梁和Timoshenko梁的精确解相比较,证明该文的解答是正确的。     

功能梯度材料Timoshenko型剪切梁的自由振动分析

基于Timoshenko梁理论,研究各向异性功能梯度材料梁的自由振动。假设材料参数沿梁厚度方向按同一函数规律变化,建立了功能梯度材料梁的振动方程,求得简支条件下其自振频率表达式。通过算例,给出指数函数梯度变化Timoshenko梁的自振频率和模态图,结果表明不同梯度变化对材料结构动力响应有较大影响。该方法为发展功能梯度材料梁的设计与数值计算提供了理论依据。     

弹性半空间地基上两端自由梁稳态振动研究

基础梁是一种基本的工程受力构件,广泛应用于交通工程和工业民用建筑中,因而受到广泛重视和研究.弹性基础梁稳态振动的关键是要确定梁下地基反力分布函数。现有关于地基反力的稳态振动方法大致分为两类：Winkler地基模型或双参数地基模型以及弹性理论方法。然而Winkler地基模型或双参数地基模型忽略了地基的连续性。而按弹性半空间理论计算弹性地基梁的问题实际上是解决接触问题。     

一类变截面梁横向自由振动的精确解析解

本文研究了一类变截面梁的横向自由振动问题，半径按抛物线变化的圆形变截面梁以及高度按抛物线变化而宽度接任意次幂函数变化的矩形变截面梁是这类梁的两个典型特例。求得了其横向自由振动的精确解析解。解的形式与楔形梁完全不同，是一以幂函数表示的初等函数。本文最后给出了两个算例。     

黏弹性三参数地基上Timoshenko梁横向自由振动

运用复模态分析方法研究了黏弹性三参数地基上Timoshenko梁的横向振动特征,得到简支边界条件下的频率方程以及模态函数表达式。通过具体算例，分析了各项地基参数对固有频率和模态函数的影响，比较了相同地基上作用的Timoshenko梁和Euler-Bernoulli梁的振动特征。结果表明，随着地基刚度、剪切参数的增大以及黏性系数的减小，各阶固有频率值均增大；Timoshenko梁的固有频率略低于Euler-Bernoulli梁。     

热载荷作用下嵌入SMA丝复合材料梁的横向自由振动

基于形状记忆合金Brinson一维热力学本构方程,采用复合材料细观力学分析方法,建立了热载荷作用下嵌入SMA丝复合材料梁的一维热弹性本构关系。其次利用Euler-Bernoulli梁的轴线可伸长几何非线性理论和自由振动理论,建立了嵌入SMA丝复合材料梁在均匀升温场内自由振动的动力学控制方程,导出了热过屈曲构形附近嵌入SMA丝复合材料梁微幅横向自由振动的模型。最后通过打靶法求解了两端固定约束条件下嵌入形状记忆合金丝复合材料梁在加热过程中的振动响应,获得了梁的前四阶固有频率在不同SMA相对体积含量时随温度变化的特征关系曲线。数值结果表明,SMA丝相变过程中的回复应力和弹性模量变化对梁在过屈曲前后的各阶固有频率均有影响,是实现梁自振频率主动控制的一种有效方法。     

一类Timoshenko梁振动系统的渐近稳定性与极点配置

利用了算子半群理论、无条件基理论和（Ｄ）类算子理论讨论了一类Ｔｉｍｏｓｈｅｎｋｏ梁振动系统,给出了闭环系统渐近稳定与极点配置的条件。     

车载作用下多跨变截面损伤梁的振动特性

将车辆视为7自由度的整车模型,桥梁为多跨变截面的混凝土梁,裂缝分成开口裂缝和呼吸裂缝两种类型,建立了多跨变截面的损伤混凝土梁的车桥耦合方程;编制了相应的计算程序,结果表明了本方法的正确性.数值分析表明:相同条件下.呼吸裂缝所对应DFC的绝对值约为开口裂缝对应绝对值的1.55倍,故忽略呼吸裂缝随载荷张开与闭合的特性是不可取的;裂缝参数、裂缝位置等对耦合系统振动特性影响很大,如当裂缝参数a值从0.2变化到0.4时,对应的DFC绝对值增大1.95倍,且随着裂缝区域出现越多,各阶振动频率减小越快.     

黏弹性Pasternak地基上两跨连续Timoshenko梁横向自振特性分析

以黏弹性Pasternak地基上的Timoshenko梁为研究对象，研究其在两端简支、两端固支、简支-固支边界条件下的单跨地基梁及两跨连续地基梁(等跨和不等跨两种工况)的自振频率、衰减系数和模态。基于回传射线矩阵法，根据各种约束条件下的节点耦合条件，推导横向振动频率方程，通过观察两跨连续地基梁与单跨地基梁的频率方程，并通过具体算例，研究两跨连续地基梁与单跨地基梁自振频率之间的联系与区别，进一步给出前三阶模态。结果表明：两等跨连续地基梁自振频率方程可分为两个部分，且这两部分分别与两端简支和简支-固支边界条件下单跨地基梁的频率方程形式类同；其奇数阶自振频率与两端简支边界条件下单跨地基梁的偶数阶自振频率相等，而其偶数阶自振频率则与两端固支边界条件下单跨地基梁的偶数阶自振频率相同；不等跨的两跨连续Timoshenko地基梁的模态函数曲线幅值随阶数的增加降低最快。     

Nonlinear free vibration of functionally graded carbon nanotube-reinforced composite beams

This paper investigates the nonlinear free vibration of functionally graded nanocomposite beams reinforced by single-walled carbon nanotubes (SWCNTs) based on Timoshenko beam theory and von Kármán geometric nonlinearity. The material properties of functionally graded carbon nanotube-reinforced composites (FG-CNTRCs) are assumed to be graded in the thickness direction and estimated though the rule of mixture. The Ritz method is employed to derive the governing eigenvalue equation which is then solved by a direct iterative method to obtain the nonlinear vibration frequencies of FG-CNTRC beams with different end supports. A detailed parametric study is conducted to study the influences of nanotube volume fraction, vibration amplitude, slenderness ratio and end supports on the nonlinear free vibration characteristics of FG-CNTRC beams. The results for uniformly distributed carbon nanotube-reinforced composite (UD-CNTRC) beams are also provided for comparison. Numerical results are presented in both tabular and graphical forms to investigate the effects of nanotube volume fraction, vibration amplitude, slenderness ratio, end supports and CNT distribution on the nonlinear free vibration characteristics of FG-CNTRC beams.     

热冲击下轴向运动FGM梁的自由振动分析

基于Timoshenko梁理论研究两端夹紧、一端夹紧一端简支、两端简支三种不同边界条件下的轴向运动功能梯度材料(FGM)梁在热冲击载荷作用下的自由振动响应。利用Hamilton原理推导热冲击下轴向运动FGM梁的自由振动控制微分方程,并采用分离变量法求解一维热传导方程。通过微分求积法(DQM)在梁的长度方向进行离散,将原方程转化为四阶广义特征值问题,求解FGM梁自由振动的无量纲固有频率并进行特性分析。考虑了不同热冲击载荷,不同梯度指数和不同轴向运动无量纲速度对FGM梁自振频率的影响。结果表明:热冲击载荷越大,对降低FGM梁的固有频率的效果越明显;在轴向运动速度和热流输入不改变的情况下,逐渐增大材料梯度指数会使FGM梁的固有频率随之减小;FGM梁对热冲击短时间内有减缓作用,相对于均匀材料一阶失稳所需时间更长,受到热冲击的FGM梁在轴向运动时也更快达到失稳状态。     

多跨覆冰导线脱冰振动模型风洞试验研究

覆冰导线脱冰可能造成金具、导线和杆塔等构件受力破坏,也可能会引起导线闪络、烧断等电力事故。设计了1∶50的三跨覆冰导线的缩尺模型,采用熔断集中荷载的方法模拟导线脱冰,共七种工况研究三跨导线中脱冰量、脱冰跨位置、覆冰厚度和风速等参数不同时,导线的冰跳高度、导线张力和绝缘子轴力变化规律。结果表明:边跨脱冰将引起比中间跨脱冰更大的竖向振动,跳跃高度增大了近7%,导线张力也有明显增大;在风荷载作用时,导线脱冰振动会受气动阻尼影响,跳跃高度和振动周期都有所减小,导线张力和悬垂绝缘子的轴力随着风荷载增大而增大。     

An analytical method for free vibration analysis of Timoshenko beam theory applied to cracked nanobeams using a nonlocal elasticity model

This paper is concerned with the free transverse vibration of cracked nanobeams modeled after Eringen's nonlocal elasticity theory and Timoshenko beam theory. The cracked beam is modeled as two segments connected by a rotational spring located at the cracked section. This model promotes discontinuities in rotational displacement due to bending which is proportional to bending moment transmitted by the cracked section. The governing equations of cracked nanobeams with two symmetric and asymmetric boundary conditions are derived; then these equations are solved analytically based on concerning basic standard trigonometric and hyperbolic functions. Besides, the frequency parameters and the vibration modes of cracked nanobeams for variant crack positions, crack ratio, and small scale effect parameters are calculated. The vibration solutions obtained provide a better representation of the vibration behavior of short, stubby, micro/nanobeams where the effects of small scale, transverse shear deformation and rotary inertia are significant.     

弹性螺旋桨-轴系建模及振动特性的解析方法研究

为考虑螺旋桨自身弹性对桨-轴系统振动特性的影响,建立了一套基于Timoshenko梁理论的解析方法。将螺旋桨、轴系均用Timoshenko梁建模,结合桨叶与轴系连接处的协调条件及其边界条件,给出系统横向、纵向自由振动的控制方程;在同有限元结果对比表明本方法具有良好精度基础上,分析了桨叶弹性对系统模态的影响及桨-轴系统的力传递特性。研究表明:桨-轴系统的模态振型中螺旋桨叶片和轴系的弹性变形同时发生且相互影响,叶片弯曲模态会加剧轴系振动;作用于桨叶的激励引起的桨-轴系统轴承处的纵向传递力被桨叶弯曲和轴系纵振两阶模态显著放大,而横向传递力主要由桨叶及轴系的弯曲模态控制。     

DQEM for free vibration analysis of Timoshenko beams on elastic foundations

 A differential quadrature element method (DQEM) based on first order shear deformation theory is developed for free vibration analysis of non-uniform beams on elastic foundations. By decomposing the system into a series of sub-domains or elements, any discontinuity in loading, geometry, material properties, and even elastic foundations can be considered conveniently. Using this method, the vibration analysis of general beam-like structures is to be studied. The governing equations of each element, natural compatibility conditions at the interface of two adjacent elements and the external boundary conditions are developed in a systematic manner, using Hamilton's principle. The present DQEM is to be implemented to Timoshenko beams resting on partially supported elastic foundations with various types of boundary conditions under the action of axial loading. The general versality, accuracy, and efficiency of the presented DQEM are demonstrated having solved different examples and compared to the exact or other numerical procedure solutions. Received: 11 October 2002/Accepted: 26 November 2002     

Free vibrations of a multi-span Timoshenko beam carrying multiple spring-mass systems

Structural elements supporting motors or engines are frequently seen in technological applications. The operation of a machine may introduce additional dynamic stresses on the beam. It is important, then, to know the natural frequencies of the coupled beam-mass system, in order to obtain a proper design of the structural elements. The literature regarding the free vibration analysis of Bernoulli-Euler single-span beams carrying a number of spring-mass system and Bernoulli-Euler multi-span beams carrying multiple spring-mass systems are plenty, but on Timoshenko multi-span beams carrying multiple spring-mass systems is fewer. This paper aims at determining the natural frequencies and mode shapes of a Timoshenko multi-span beam. The model allows to analyse the influence of the shear effect and spring-mass systems on the dynamic behaviour of the beams by using Timoshenko Beam Theory (TBT). The effects of attached spring-mass systems on the free vibration characteristics of the 1–4 span beams are studied. The natural frequencies of Timoshenko multi-span beam calculated by using secant method for non-trivial solution are compared with the natural frequencies of multi-span beam calculated by using Bernoulli-Euler Beam Theory (EBT) in literature; the mode shapes are presented in graphs.     

Nonlinear non-classical microscale beams: Static bending, postbuckling and free vibration

This paper initiates the theoretical analysis of nonlinear microbeams and investigates the static bending, postbuckling and free vibration. The nonlinear model is conducted within the context of non-classical continuum mechanics, by introducing a material length scale parameter. The nonlinear equation of motion, in which the nonlinear term is associated with the mean axial extension of the beam, is derived by using a combination of the modified couple stress theory and Hamilton’s principle. Based on this newly developed model, calculations have been performed for microbeams simply supported between two immobile supports. The static deflections of a bending beam subjected to transverse force, the critical buckling loads and buckled configurations of an axially loaded beam, and the nonlinear frequencies of a beam with initial lateral displacement are discussed. It is shown that the size effect is significant when the ratio of characteristic thickness to internal material length scale parameter is approximately equal to one, but is diminishing with the increase of the ratio. Our results also indicate that the nonlinearity has a great effect on the static and dynamic behaviors of microscale beams. To attain accurate and reliable characterization of the static and dynamic properties of microscale beams, therefore, both the microstructure-dependent parameters and the nonlinearities have to be incorporated in the design of microscale beam devices and systems.     

圆形薄膜自由振动的理论解

本文研究圆形薄膜的自由振动。首先根据哈密顿原理建立薄膜横向振动的动力学方程,然后采用分离变量法,导出时间t\、径向坐标r和环向坐标 变量分离的2个二阶常微分方程和1个贝塞尔方程并分别求解,求得周边固定圆形薄膜、扇形薄膜自由振动的理论解,从而得到固有频率及其振型的解析表达式。最后,应用ANSYS有限元计算软件计算上述几种类型自由振动的频率及其模态并与理论解比较。ANSYS有限元数值解与理论解二者十分接近,理论解是有限元数值解的下限。