轴向运动粘弹性夹层梁的横向振动

研究了小扰度下轴向匀速运动粘弹性夹层梁的振动模态和固有频率.基于Kelvin粘弹性本构方程,建立了轴向运动粘弹性夹层梁横向振动控制方程.分别采用Galerkin截断和复模态分析方法,研究两端简支的粘弹性夹层梁的固有频率和模态函数,讨论了轴向运动速度、夹心层与约束层厚度比、初始轴力等参数对夹层梁固有频率、临界速度及稳定性的影响.     

双层圆柱壳振动传递及声辐射试验研究

对有限长的敷设阻尼材料的加筋双层圆柱壳进行振动和声辐射试验,测量了壳体的结构响应和水中的辐射声压。对全部敷设隔声去耦材料、内壳全部敷设隔声去耦材料、外壳全部敷设以及外壳部分敷设4种工况下的近场声压进行了对比,分析了单频激振时内外壳间的振动传递特性。结果表明:托板在内外壳的振动传递中起着较大的作用;且内外壳全部敷设隔声去耦材料对抑制振动和声辐射很有效。     

Chaotic oscillations of a shallow cylindrical shell with a concentrated mass under periodic excitation

This paper presents effects of a concentrated mass on chaotic oscillations of a shallow cylindrical shell under gravity and periodic acceleration. The rectangular shell is simply supported and is elastically in-plane constrained. Assuming mode functions, the Donnell equation with inertia force is reduced to non-linear coupled differential equations by the Galerkin method. The chaotic response is calculated numerically and is examined by the maximum Lyapunov exponent. Dominant chaotic responses are generated within restricted frequency regions of sub-harmonic resonance of 1/2 order. As the concentrated mass increases, the chaotic response is shifted to the lower frequency region. The increment of the concentrated mass decreases the maximum Lyapunov exponent.     

Parametric instability of a circular cylindrical shell with geometric imperfections

The static and dynamic behavior of a compressed circular cylindrical shell having geometric imperfections is analyzed. The analysis is mainly performed by means of the Donnell’s nonlinear shallow-shell theory. However, the refined Sanders shell theory is also used for comparison. A suitable expansion of the radial displacement, able to describe both buckling and dynamic behaviors is developed; the effect of geometric imperfections is accounted for by means of a modal representation. The response of the shell subjected to a sinusoidal axial excitation at its ends, giving rise to a parametric excitation, is considered. The effect of imperfections on the critical value of the dynamic load, that causes the loss of stability of the system, is analyzed. Interesting nonlinear dynamic phenomena are observed: direct resonance with softening behavior and parametric instability with period doubling response.     

金字塔型点阵夹芯梁振动特性分析

研究了金字塔芯层点阵夹芯梁的自由振动和非线性受迫振动特性.基于折线理论推导出两端简支金字塔型点阵夹芯梁的非线性动力学方程.计算点阵夹芯梁固有频率并进行了验证.分析了杆件半径、杆件倾斜角度和芯层高度对点阵夹芯梁固有频率的影响.研究了点阵夹芯梁在不同激励幅值和不同结构参数下的非线性幅频响应特性.结果表明,随着各结构参数的增大,夹芯梁的固有频率均呈先增大后减小的变化规律,并且芯层结构参数对点阵夹芯梁的非线性响应存在复杂影响.     

磁约束阻尼悬臂壳的轴对称振动分析

提出了一种新型有效的方法来降低悬臂壳的轴对称振动．该方法的原理是在约束层端部上及固定端分别设置引力排列的永磁体,振动时磁体间的动态磁力可使阻尼层获得比传统约束阻尼处理方法更高的剪应变,阻尼层耗能增加,从而降低结构的共振峰．从夹层单元微元体受力分析出发,建立了局部磁约束悬臂壳的轴对称振动分析模型,得到分别用约束层纵向位移u30、积分常数c和径向位移w表示的夹层壳体单元的纵向和周向力平衡方程．在此模型中,考虑了振动时因u30引起动态磁力的变化,使得此模型能描述MCLD结构的动态及阻尼性能．此外,通过比较MCLD处理与传统的约束阻尼处理对磁约束悬臂壳的轴对称振动的控制效果,分析表明：磁约束处理可同时控制悬臂壳前几阶模态的振动．     

非线性地基上正交异性矩形板的非线性热振动

研究了非线性地基上正交异性矩形板的非线性固有热振动.采用常规的L-P法分析非线性地基上正交异性矩形板的非线性热振动难以得到高精度的近似解,为此,先对该强非线性振动系统进行参数变换,将该强非线性振动系统转化为弱非线性振动系统.然后采用改进的L-P法进行求解,得到了强非线性振动系统的高精度近似解.此外,讨论了温度、地基特征参数、长宽比等因素对非线性地基上正交异性矩形板非线性热振动固有频率的影响,得到了非线性地基上正交异性矩形板热振动频率随温度下降、地基特征参数变大、长宽比变大而增大的结论.     

具有损伤扁球面网壳非线性稳定性

基于Lematire等效应变损伤原理,计及扁球面网壳各个杆件的损伤影响,根据薄壳非线性动力学理论推导出含有损伤扁球面网壳非线性动力学方程和协凋方程,在固定夹紧边界条件下,用Galerkin方法得到一个含二次和三次非线性振动微分方程,并对具有损伤扁球面网壳的非线性自由振动方程求解．用Floquet指数法研究系统分叉问题给出了平衡点的状态．并通过数字仿真绘出了不同损伤状态下系统的分叉图和平衡点的相对位置图,发现损伤对系统的平衡点的状态影响较大．     

粘弹性夹层圆板自由振动的理论解

研究了粘弹性夹层圆板的自由振动特性.基于经典弹性薄板理论和Kelvin-Voigt粘弹性本构方程,建立了粘弹性夹层圆板振动控制方程.采用分离变量法导出了粘弹性夹层圆板的自然频率及振型解析表达式,计算了固支和简支粘弹性夹层圆板的自然频率,并与有限元计算结果进行比较;讨论了粘弹性夹层圆板的夹心层比率对自然频率及衰减系数的影响.研究表明：（1）随着夹心层厚度的增大,系统频率先增大后减小,高阶时该趋势表现更为明显;（2）随着夹心层厚度的增大,衰减系数一直增大,高阶时该趋势表现更为明显.     

恒定磁场中简支圆柱壳的磁弹性振动分析

依据电磁场方程及相应的电磁本构关系,给出了作用于圆柱壳体上的电磁力及力矩表达式.在此基础上,分别推得了纵向和横向磁场中圆柱壳体的磁弹性轴对称振动方程.针对两端简支约束条件,通过位移函数的设定,得到了相应的有阻尼振动微分方程.通过算例,给出了系统衰减振动的响应曲线图和相图,分析了磁感应强度和壳体厚度对系统振幅衰减速度的影响.结果表明,通过改变磁感应强度可以达到控制系统振动的目的.     

Nonlinear topology optimization of layered shell structures

Topology stiffness (compliance) design of linear and geometrically nonlinear shell structures is solved using the SIMP approach together with a filtering scheme. A general anisotropic multi-layer shell model is employed to allow the formation of through-the-thickness holes or stiffening zones. The finite element analysis is performed using nine-node Mindlin-type shell elements based on the degenerated shell approach, which are capable of modeling both single and multi-layered structures exhibiting anisotropic or isotropic behavior. The optimization problem is solved using analytical compliance and constraint sensitivities together with the Method of Moving Asymptotes (MMA). Geometrically nonlinear problems are solved using iterative Newton–Raphson methods and an adjoint variable approach is used for the sensitivity analysis. Several benchmark tests are presented in order to illustrate the difference in optimal topologies between linear and geometrically nonlinear shell structures.     

轴向覆盖磁约束阻尼条对悬臂壳非轴对称振动的影响

应用Rayleigh-Ritz方法建立了局部磁约束阻尼壳的振动分析模型.选取约束层的横向振动模态和面内振动模态作假设模态,形成横向位移和面内位移.调查了不同约束阻尼层配置下,轴向覆盖磁约束阻尼条对悬臂壳非轴对称振动模态(m=1,n=1)损耗因子的影响.研究表明:当阻尼层远离该模态的节线(θ=±π/2),磁约束阻尼处理的阻尼改进效果越明显.阻尼层设置在θ=0,π处,该模态的损耗因子最大,MCLD处理的阻尼改进效果也最显著,损耗因子提高约40%.可以通过改变阻尼层的长度及宽度可增加损耗因子,但随二者的增加,磁约束处理对阻尼的改进作用减小.     

沿轴向飞行粘弹性夹层梁热弹耦合振动响应分析

研究了沿轴向飞行粘弹性夹层梁的热弹耦合振动响应.考虑材料变形与传热的相互影响,建立了轴向运动粘弹性夹层梁的热弹耦合振动控制方程;将方程中激励项(温度函数与外激力)拟合为时间的函数,采用伽辽金法得到方程的位移解,并在每一个微小的时间段内采用迭代收敛的数值方法对热传导方程进行求解得到温度场.使用数值方法讨论了轴向飞行运动速度和热载荷持续时间对其振动响应的影响.研究表明:稳定振动时飞行速度对位移影响较大,对温度影响较小;热冲击对振动位移响应有较大影响,并改变振动特性.     

格栅夹层板抑振性能研究

为了有效降低铺板与圆柱壳体耦合结构中因铺板振动而引起的壳体振动,提出了以格栅夹层板作为一种铺板结构.以格栅夹层板安装于带有端板的圆柱壳体上作为研究模型,采用有限元软件对格栅夹层板的抑振性能展开了仿真分析,讨论了格栅结构参数对其抑振效果的影响,并实验验证了格栅夹层板的抑振效果.仿真和实验结果一致表明：格栅夹层板能有效降低圆柱壳体的振动响应,尤其是在中高频段抑振效果显著；格栅的结构参数对抑振效果影响规律比较复杂,格栅夹层的上层面板采用阻尼较大的材料利于提高其抑振效果.     

悬臂式蜂窝夹层板的非线性动力学建模及分析

蜂窝夹层结构因其良好的力学特性,在众多工程领域具有非常广泛的应用.本文建立了悬臂边界条件下,蜂窝夹层板的动力学模型并研究其非线性动力学行为.选取文献中更加接近实体有限元解的等效弹性参数公式对蜂窝芯层进行等效简化,得到六角形蜂窝芯的等效弹性参数.基于Reddy高阶剪切变形理论,应用Hamilton原理建立悬臂式蜂窝夹层板在受到面内激励和横向激励联合作用下的偏微分运动方程.然后利用Galerkin方法得到两自由度非自治常微分形式运动方程.在此基础上,通过对悬臂式蜂窝夹层板进行数值模拟分析系统的非线性动力学.结果表明面内激励和横向激励对系统的动力学特性有着重要影响,在不同激励作用下系统会出现周期运动、概周期运动以及混沌运动等复杂的非线性动力学响应.     

Optimum weight design of sandwich cylinders with orthotropic facings and core under combined loads

The minimum weight of a honeycomb sandwich cylinder with the facings in composite material is obtained by an optimization method with the ply angles and the thicknesses of the ply and honeycomb as the design variables. The cylinder is under the combined loads of axial compression, bending moment and transverse shear. The structural analyses verify the stability and the material strength. The stability analyses are done with the simply supported boundary conditions for the orthotropic case. Three stability modes have been studied: general buckling, dimpling and wrinkling. In all cases, the initial imperfections and the prebuckling distortions are not taken into account. This problem is treated with the knock-down factors. For the optimization, we have used a variable metric method for constrained optimization (subroutine VMCON, method of M.J.D. Powell). From an arbitrary design point (feasible or non-feasible), the program searches for an optimal design by the iterative procedure. To verify that the obtained optima are not local, the program has been initiated from several different starting points. Having compared the results, global alternative optima as well as local optima have been found.     

去耦瓦敷设方式对双层壳声特性影响试验研究

对有限长敷设隔声去耦材料的加筋双层圆柱壳进行了振动和声辐射试验,测量了壳体的结构响应和水中的辐射声压,对内外壳全部敷设、内壳全部敷设、外壳全部敷设以及外壳部分敷设隔声去耦材料4种敷设方式进行了对比.结果表明:内外壳全部敷设隔声去耦材料对抑制振动和声辐射最有效,而且,部分敷设隔声去耦材料对水下航行器敷设隔声材料的位置选择具有一定的参考价值.     

Robustness of Nonlinear Delay Equations with Respect to Input Perturbations: a Trajectory-Based Approach

 The effect of input perturbations on the stability properties of nonlinear time-varying delay differential equations is studied from a trajectory-based point of view. Thereby the semi-global stability results from [MSR2], where a Lyapunov approach is taken, are broadened to a much larger class of delay differential equations. Applications to the stabilization of partially linear cascade systems with delay using partial state feedback are briefly outlined. Date received: January 9, 2001. Date revised: April 15, 2002. RID="*" ID="*"This paper presents research results of the Belgian programme on Interuniversity Poles of Attraction, initiated by the Belgian State, Prime Minister's Office for Science, Technology and Culture (IUAP P4/02). The scientific responsibility rests with its authors. Luc Moreau is a Postdoctoral Fellow of the Fund for Scientific Research—Flanders (Belgium) (F.W.O.-Vlaanderen) and a recipient of an Honorary Fellowship of the Belgian American Educational Foundation. Part of this work was done while Luc Moreau was supported by a BOF grant of the Ghent University.     

动力吸振器对转子系统气流激振稳定性影响分析

针对气流激振引起离心压缩机转子振动失稳的问题,提出了采用动力吸振方法提高转子系统的稳定性.首先建立流体激励作用下转子 吸振系统动力学模型;其次采用Lyapunov理论研究附加吸振器后流体激励作用下转子系统的稳定性;分析了吸振器参数变化对转子系统稳定性的影响;最后采用数值方法进行验证.结果表明,动力吸振方法能够有效地提高转子系统失稳转速,吸振器固有频率和阻尼比对转子稳定性有较大的影响.     

Nonlinear forced vibration of damped plates by an asymptotic numerical method

This work deals with damped nonlinear forced vibrations of thin elastic rectangular plates subjected to harmonic excitation by an asymptotic numerical method. Using the harmonic balance method and Hamilton’s principle, the governing equation is converted into a static formulation. A mixed formulation is used to transform the problem from cubic nonlinearity to quadratic one sequence. Displacement, stress and frequency are represented by power series with respect to a path parameter. Equating the like powers of this parameter, the nonlinear governing equation is transformed into a sequence of linear problems with the same stiffness matrix. Through a single matrix inversion, a considerable number of terms of the perturbation series can easily be computed with a limited computation time. The starting point, corresponding to a regular solution, is obtained by the Newton–Raphson method. In order to increase the step length, Padé approximants are used. Numerical tests are presented and compared with numerical and analytical results in the literature, for different boundary conditions, excitations and damping coefficients.