基于Galerkin法的旋转薄壁圆柱壳非线性行波振动的数值分析

应用Donnell's简化壳理论,在考虑阻尼和几何非线性的情况下,基于Galerkin方法,对旋转的薄壁悬臂圆柱壳在法向激振力作用下的非线性行波振动进行了数值分析.在研究过程中,首先,考虑阻尼并引入几何非线性项,建立薄壁圆柱壳的非线性波动方程,然后,采用Galerkin方法对波动方程进行转换,选取不同的模态组合,得到相应模态坐标下的非线性微分方程,最后用Runge-Kutta法进行数值计算并对圆柱壳的非线性波动振动特性进行了分析.结果表明,几何非线性使圆柱壳呈现明显的硬特性,其硬特性随激振力幅值的增大而得到加强,共振区存在多值性,多模态分析表明,轴向二阶模态对主模态影响较大,计算时宜采用两个轴向模态.     

薄壁圆柱壳在纯弯曲下的非线性自由振动

分析了薄壁圆柱壳在纯弯曲下的非线性自由振动。基于改良的Brazier简单理论,将圆柱壳的纯弯曲变形简化为以下两个阶段：第一阶段壳体没有弯曲,横截面由圆形变成椭圆形;第二阶段壳体是横力弯矩作用下的变截面梁。通过Brazier简单理论获得壳体的应变能,然后利用拉格朗日方程求得薄壁圆柱壳的几何非线性自由振动方程,最终得到自由振动频率,并对线性解与非线性解进行对比分析。     

薄壁圆柱壳在流体脉动激励下的振动特性分析

摘要：为深入研究薄壁圆柱壳在流体脉动激励下的运动特性,应用Donnell简化壳理论,考虑阻尼、结构非线性和附加质量的影响,建立了薄壁圆柱壳在流体脉动激励下的非线性振动方程。基于Galerkin方法将偏微分方程转化为方便求解的常微分方程,利用多尺度法求解了系统主共振的一次近似解,得到了系统稳态响应的转迁集与分岔图,并通过奇异性分析,得到了系统工作稳定性和可靠性的结构参数区域。对薄壁圆柱壳在流体作用下的振动特性进行了数值模拟和实验研究,考察了阻尼系数、脉动频率、液体深度等对系统动力学特性的影响。研究表明,考虑阻尼、结构非线性和附加质量的非线性振动方程更能体现薄壁圆柱壳在流体脉动激励下完整的动力学特性,同时系统中存在多种分岔行为。     

索力对斜拉索动力特性的影响

针对大跨度斜拉桥拉索大幅振动控制问题,考虑由于索的初始垂度、大位移而引起的几何非线性因素的影响,同时考虑拉索与桥面连接条件和边界条件的影响,建立了拉索在参、强联合激励作用下的面内非线性振动方程。运用多尺度摄动方法,对其进行求解,以目前最长拉索为例,研究拉索初始索力的变化对其大幅振动的影响。研究结果表明:增加斜拉索的初始张拉力,将使索表现出的软弹簧特性变为硬弹簧特性,同时,拉索的振幅最大值对应的激励频率与拉索固有频率比值将由小于2改变为大于2。     

层合薄壁圆柱壳1:1内共振研究

针对一端固定,一端自由的层合薄壁圆柱壳模型,根据Donnell’s非线性简化壳理论建立其非线性振动方程。采用Galerkin方法对非线性振动方程进行离散化,应用平均法对系统包含两个相邻轴向模态的非线性振动响应进行了解析分析,与数值模拟进行了比较,并得到了不同参数对层合薄壁圆柱壳复杂的振动响应的影响。结果表明,1）由于所选的两个相邻轴向模态频率相距较近,能量在两个模态之间相互传递,系统存在1:1内共振现象;2）系统复杂的振动响应受激振力大小和非线性项的影响比较大,而对于阻尼不敏感。     

旋转几何非线性复合材料薄壁梁的自由振动分析

研究具有几何非线性的旋转复合材料薄壁梁的自由振动。梁的变形引入了Von Kármán几何非线性, 基于Hamilton原理和变分渐进法 (Variational-Asymptotical Method -VMA),导出旋转复合材料薄壁梁的非线性振动偏微分方程组。采用Galerkin法将振动方程离散化为常微分方程组。借助于谐波平衡法 (Harmonic Balance Method -HBM) 建立自由振动的振幅-非线性固有频率关系方程。将上述方程化为非线性特征值问题,采用迭代算法进行求解。将所建立的旋转复合材料薄壁梁非线性自由振动分析模型和计算方法,应用于周向均匀刚度配置(Circumferentially Uniform Stiffness –CUS) 构型复合材料薄壁梁,通过数值计算揭示了纤维铺层角、旋转速度对非线性振动固有频率-振幅关系的影响。     

考虑损伤双层扁球面网壳的非线性动力学特性

基于Lematire等效应变损伤理论,计及扁球面网壳各个杆件的损伤影响,应用拟壳法导出了具有损伤的扁球面网壳的动力学非线性控制方程。提出了以中心最大振幅为摄动参数的摄动-变分法的求解方法,对动力非线性控制方程进行了求解,得出了相应的物理量的解析式。据此进行数值分析,得出了相应的特征关系。并用Galerkin方法导出了一个含二次和三次非线性振动微分方程并求解了具有损伤扁球面网壳的的非线性动力学的自由振动方程,给出了准确解。而后利用Melnikov函数法,从理论上给出了考虑损伤的系统发生混沌运动的临界条件,并通过计算机数字仿真证实了考虑损伤的扁球面网壳在非线性强迫振动时存在混沌运动,同时发现损伤使得系统更易发生混沌运动。     

参数激励下碳纳米谐振器的非线性振动研究

该文研究了两端固支情况下的碳纳米管谐振器在直交流电激励作用下的非线性振动响应。考虑外激励频率接近其固有频率的主共振情况下以及几何非线性,忽略静电力的非线性、范德瓦耳斯力和初始静变形的影响,运用欧拉伯努利连续梁理论,通过哈密尔顿原理得到非线性控制方程。然后利用伽略金方法离散得到降阶方程,最后应用摄动分析方法获得其振动响应的幅频曲线。主要分析了阻尼、直交流电荷载、几何三次非线性项对响应的影响。结果表明几何三次非线性项直接影响碳纳米管谐振器在外激励作用的振动响应以及碳纳米管在交流电荷载作用下的振动响应相对于直流电荷载更加敏感,并在一定程度上发生软化行为等。     

反对称正交铺层剪切圆柱壳在外压下的屈曲和后屈曲

给出了反对称正交铺层剪切圆柱壳广义大挠度Donnell 型方程, 并运用位移型摄动技术构造出该圆柱壳在均匀外压作用下的后屈曲渐近级数解。考虑到边界效应对中短圆柱壳的影响及边值问题摄动解的一致性, 详细研究了该圆柱壳端部边界层方程和奇异摄动解, 以便与中部正则摄动解相匹配。文中同时给出一些典型例子并讨论了横向剪切变形、Batdo rf 数、弹性模量比和初始几何缺陷对圆柱壳屈曲与后屈曲性态的影响。比较显示, 横向剪切变形对圆柱壳的屈曲与后屈曲有重要影响。      

基于最小能量原理的矩形平面预应力索网结构大变形自由振动研究

以中关村文化商厦30m×70m平面索网为工程背景,考虑矩形索网结构大变形产生的几何非线性的影响,用最小势能原理推导了非线性振动的微分方程并给出了解法;研究了线性振动频率、大振幅振动频率和大变形后小振幅的振动频率计算方法;结合实例对3个振动频率进行了计算分析。给出的非线性振动方程和解法简单准确,为大跨度平面索网结构抗风抗震设计提供参考。     

径向载荷作用下复合材料圆柱壳的非线性动力屈曲

采用半解析法求解径向阶跃载荷作用下复合材料圆柱壳的非线性动力屈曲。基于一阶剪切变形理论，由Hamilton原理推导出包含横向剪切变形以及几何初缺陷的圆柱壳的非线性动力方程，位移及载荷沿周向采用级数展开，由Galerkin方法得到微分方程组，通过有限差分法求解；根据响应情况，由B—R准则判定屈曲，确定屈曲临界载荷。     

A closed form solution for linear and nonlinear free vibrations of composite and fiber metal laminated rectangular plates

In this paper, the nonlinear equations of motion for laminated composite rectangular plates based on first order shear deformation theory, which include shear deformation and rotary inertia, have been derived. Then, through introducing a force function, these equations reduced to a set of coupled nonlinear partial differential equations and a compatibility equation. By using the Galerkin method, for the first time, a nonlinear ordinary differential equation is obtained, which includes nonlinear inertia and stiffness terms. By using the multiple time scales method, analytical relations for nonlinear frequency and transverse displacement have been obtained. Results are compared with the literature and good agreement is achieved for both linear and nonlinear frequencies. After proving the validity of our work for isotropic rectangular plates and laminated rectangular plates, linear and nonlinear free vibration of a Fiber Metal Laminate panel have been investigated. Also the effects of some system parameters on the nonlinear frequency have been investigated.     

Continuum damage mechanics approach to composite laminated shallow cylindrical/conical panels under static loading

Static response characteristics and failure load of laminated composite shallow cylindrical and conical panels subjected to internal/external lateral pressure are investigated using continuum damage mechanics approach considering geometric nonlinearity and damage evolution. The damage model is based on a generalized macroscopic continuum theory within the framework of irreversible thermodynamics and enables to predict the progressive damage and failure load. Damage variables are introduced for the phenomenological treatment of the state of defects and its implications on the degradation of the stiffness properties. The analysis is carried out using finite element method based on the first order shear deformation theory. The nonlinear governing equations are solved using Newton–Raphson iterative technique coupled with the adaptive displacement control method to efficiently trace the equilibrium path. The detailed parametric study is carried out to investigate the influences of geometric nonlinearity, evolving damage, span-to-thickness ratio, lamination scheme and semi-cone angle on the static response and failure load of laminated cylindrical/conical panels. It is revealed that the membrane forces due to geometric nonlinearity significantly influence the damage distribution and failure load.     

悬索承重梁索耦合结构的垂向运动动力学模型及主共振分析

该文建立了描述结构大变形和主缆初始曲率产生的几何非线性对系统动力学影响的悬索承重梁索耦合结构垂向运动动力学偏微分方程组。通过Galerkin方法一次截断把偏微分方程组化为时域上的两自由度常微分方程组。使用多尺度法得到简谐激励下常微分方程组主共振时的一次近似解。结果显示,当外激励仅激发低频或高频主共振时,系统的振幅随激励的幅值或激励频率的变化出现突然的跳跃。当激励同时激发低频和高频主共振时则有两种情况:1) 若固定高频激励幅值和频率,则系统的低频和高频振动成分的振幅随低频激励参数变化同时增加或减小;2) 若固定低频激励的幅值和频率,则系统的低频和高频振动成分的振幅随高频激励参数变化以相反的趋势变化。即高频振动幅值增大时,低频振幅减小,反之亦然。     

Creep buckling and post-buckling analyses for a hybrid laminated viscoelastic FGM cylindrical shell under in-plane loading

In this paper, creep buckling and post-buckling of a hybrid laminated viscoelastic functionally graded material (FGM) cylindrical shell under in-plane loading are investigated. Considering the high-order transverse shear deformation and geometric nonlinear theory, the von Karman geometric relation of the hybrid laminated viscoelastic FGM cylindrical shell with initial deflection is established. Based on the Donnell theory, elastic piezoelectric theory and Boltzmann superposition principle, nonlinear creep governing equations of the hybrid laminated viscoelastic FGM cylindrical shell under in-plane loading are derived. By means of the finite difference method and the Newton–Newmark method, the problem for creep buckling and post-buckling of the laminated shell’s structure is solved. Numerical results are presented to show effects of geometric parameters, power law index and loading on creep buckling and post-buckling of the hybrid laminated viscoelastic FGM cylindrical shell.     

Nonlinear oscillations of thick asymmetric cross-ply beams

Summary The axial and transverse motion of asymmetrically laminated cross-ply beams is coupled due to (i) the non-coincidence of reference and mid-planes and (ii) finite amplitudes. To derive the equations that govern the nonlinear oscillatory behavior of these laminated beams, a spatial deformation satisfying geometric constraints is substituted in the kinetic potential and Hamilton's principle is employed. This leads to three coupled nonlinear second order ordinary differential equations. These equations have quadratic nonlinear terms in addition to usual linear and cubic terms. The existence of these terms does not allow a straight forward solution in the presence of axial and rotatory inertia for nonlinear frequencies/periods. The objective of the present paper is to propose two possible solution methods for computing nonlinear frequencies/periods of asymmetrically laminated cross-ply beams. In both the methods, energy of positive and negative deflection cycles is maintained equal. A few numerical examples are solved to validate the methods. The effect of axial and rotatory inertia on the large amplitude oscillatory behavior is investigated.     

考虑索间作用的斜拉桥耦合振动研究

为了研究几何非线性条件下斜拉桥索梁耦合振动与索间作用问题,以两条斜拉索与简支梁组合体系为简化模型,利用D’Alembert原理建立考虑初始垂度的索梁体系非线性偏微分方程,设定索的前两阶复合振动模态与梁的基本模态,运用Galerkin方法将其离散为二阶常微分方程,并使用四阶—五阶Runge-Kutta方法对索与梁的振动响应进行了数值分析。结果表明:在双索单梁组合结构中,特定频率条件下一阶模态与主梁强烈耦合,二阶模态与主梁小程度耦合;与单梁单索结构相比,多索导致主梁频率增大,索间作用使得索振幅增大、拍频降低,面内一阶模态对索梁变化更敏感;当索梁频率不变时,索间作用对耦合振动产生的索大幅振动有明显抑制作用,且索梁结构对主梁初位移变化更敏感。     

Accurate approximation to the double sine-Gordon equation

In general, this paper deals with nonlinear double sine-Gordon equation with even potential energy which has arisen in many physical phenomena. The nonlinear dispersion problems without a small perturbation parameter are difficult to be solved analytically. Hence, the main concern is focused on solving the traveling wave of the double sine-Gordon equation. As commonly known, the perturbation method is for solving problems with small parameters, and the analytical representation thus derived has, in most cases, a small range of validity. For some nonlinear problems, although an exact analytical solution can be achieved, they often appear in terms of sophisticated implicit functions, and are not convenient for application. Although a variety of transformation methods has been developed for solving the nonlinear dispersion problems, such transformed equations still include nonlinear terms. To overcome these difficulties, a new approach for Newton-harmonic balance (NHB) method with Fourier–Bessel series is presented here. It is applied to solve the higher-order analytical approximations for dispersion relation in double sine-Gordon equation. The Fourier–Bessel series with the NHB method presents excellent improvement from lower-order to higher-order analytical approximations involving the nonlinear terms in the double sine-Gordon equation. Not restricted by the existence of a small perturbation parameter, the method is suitable for small as well as large amplitudes of wavetrains. Excellent agreement with exact solutions is presented in some practical examples.     

Nonlinear vibration of shear deformable FGM cylindrical shells surrounded by an elastic medium

This paper investigates the large amplitude vibration behavior of a shear deformable FGM cylindrical shell of finite length embedded in a large outer elastic medium and in thermal environments. The surrounding elastic medium is modeled as a Pasternak foundation. Two kinds of micromechanics models, namely, Voigt model and Mori-Tanaka model, are considered. The motion equations are based on a higher order shear deformation shell theory that includes shell-foundation interaction. The thermal effects are also included and the material properties of FGMs are assumed to be temperature-dependent. The equations of motion are solved by a two step perturbation technique to determine the nonlinear frequencies of the FGM shells. Numerical results demonstrate that in most cases the natural frequencies of the FGM shells are increased but the nonlinear to linear frequency ratios of the FGM shells are decreased with increase in foundation stiffness. The results confirm that in most cases Voigt model and Mori-Tanaka model have the same accuracy for predicting the vibration characteristics of FGM shells.     

Postbuckling analysis of axially-loaded functionally graded cylindrical shells in thermal environments

A postbuckling analysis is presented for a functionally graded cylindrical thin shell of finite length subjected to compressive axial loads and in thermal environments. Material properties are assumed to be temperature-dependent, and graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents. The governing equations are based on the classical shell theory with von Kármán–Donnell-type of kinematic nonlinearity. The nonlinear prebuckling deformations and initial geometric imperfections of the shell are both taken into account. A boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, large deflections in the postbuckling range, and initial geometric imperfections of the shell, is extended to the case of functionally graded cylindrical shells. A singular perturbation technique is employed to determine the buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling response of axially-loaded, perfect and imperfect, cylindrical thin shells with two constituent materials and under different sets of thermal environments. The effects played by temperature rise, volume fraction distribution, shell geometric parameter, and initial geometric imperfections are studied.