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1.
主被动阻尼层合板结构的自由振动和阻尼特性分析   总被引:3,自引:0,他引:3  
给出了含主被动阻尼非对称复合材料层合板结构的振动微分方程;得到了在压电材料和高粘弹材料作主被动阻尼层情况下,简支层合板结构自由振动的自然频率和损失因子的解析解;分析了正逆向压电效应对自然频率和损失因子的影响  相似文献   

2.
基于径向基点插值函数(RPIM),在Hamilton体系下研究了含弱粘接复合材料层合板的灵敏度分析问题.利用弹簧层模型和修正H-R(Hellinger-Reissner)变分原理,推导了可用于含弱粘接复合材料层合板响应和灵敏度分析的混合控制方程,给出了基于该混合控制方程进行灵敏度分析的解析法(AM)、半解析法(SA)和有限差分法(FD).该混合控制方程的主要优点是可以在进行灵敏度分析过程中避免卷积运算.另外,利用该混合控制方程进行灵敏度分析不仅能够同时得到响应结果和灵敏度系数,而且还考虑了层合板的层间弱粘接问题.  相似文献   

3.
在复合材料层合板静力和动力分析方面,本文提出了一个层合板理论.此理论从板的总挠度中分开了由弯曲所产生的挠度W_b与由剪切产生的挠度W_s,因而使得求控制方程的解变得容易了.而且便于讨论和分析横向剪切变形对层合板弯曲,振动和稳定性的影响.  相似文献   

4.
新型轻质复合材料夹芯结构振动阻尼性能研究进展   总被引:2,自引:1,他引:1       下载免费PDF全文
作为新一代先进轻质超强韧结构材料,复合材料格栅和点阵夹芯结构受到了国内外学者的广泛关注.目前关于该类结构材料的设计制备以及相关力学性能研究已取得了大量的研究成果.然而对该类结构振动阻尼性能的研究则处于起步阶段.该文综述了纤维增强树脂基复合材料简单层合结构以及各类夹芯结构振动阻尼性能的研究现状.首先阐述其阻尼机理, 然后分别概述了复合材料简单层合板的微观和宏观阻尼模型、复合材料粘弹性阻尼夹层结构和新型夹层结构的阻尼预报工作,最后总结归纳现有关于该类结构阻尼特性研究工作中已取得的成果和不足之处,并对其未来发展进行了展望.  相似文献   

5.
被动约束层阻尼圆柱壳振动和阻尼分析的一种新矩阵方法   总被引:4,自引:0,他引:4  
基于线弹性薄壳理论和线粘弹性理论,考虑粘弹性层的剪切耗能作用和各层间的相互作用力,导出了被动约束层阻尼层合圆柱壳在谐激励作用下的一阶常微分矩阵控制方程.然后,借助作者提出的齐次扩容精细积分技术建立了一种新的矩阵方法,并利用该方法研究了层合圆柱壳的振动特性和阻尼特性.该方法与已提出的以位移及其导数作为状态向量的传统传递矩阵法的根本区别在于,控制方程中的状态向量中包含了层合壳的全部位移和整合内力变量,因此,可以方便地适用于各种位移和内力边界条件以及部分环状覆盖约束层阻尼圆柱壳的动态分析.数值算例与解析解和有限元解的结果比较有力说明了该方法的正确性和有效性.  相似文献   

6.
本文讨论了复合材料层合板层间界面处应力和应变的间断性问题,并提出了复合材料层合板的三维理论.本文还以在层合板中全局连续的变量为基础,提出了与传统的势能和余能不同的一种新的弹性能.并得到与复合材料三维理论相应的变分原理.本文得到的三维层合板理论和杂交能变分原理,可以作为校核层合板二维经典理论和确定自由边界附近层间应力的理论基础.  相似文献   

7.
本文针对文献[1]所述复合材料层合板三维模型,在三维线性弹性理论基本方程和经典变分原理的基础上,通过分块矩阵运算和线性Lagrange乘子法,推导出比文献[1]更全面更系统的基本方程和变分原理,使复合材料层合板三维线性理论臻于完整。  相似文献   

8.
本文将分析一个受弯复合材料层合板的计算模型.首先利用无量纲变量将层合板任一层的平衡方程变成以位移表示的摄动型微分方程式;然后利用合成展开法,将求解区域分成内部区域和边界层区域,并推导出求解外部解和内部解的数学模型.为突出边缘效应,最后用边界积分方程表示内部解.  相似文献   

9.
首次把用于动态体系的Hamilton系统引入到静力学中,建立了与原控制方程相对应的Hami-lton方程,可以对全状态向量分离变量,求出解析解和半解析解,特别适合于求解矩形域平面问题和柱形域空间问题.本文建立了一种求解偏微分方程的新方法,并对复合材料力学中的层合板的弯曲和平面应力问题的求解做了详细说明.  相似文献   

10.
层合板的层间粘接模型对整个层合板的结构有重要影响.运用Hamilton正则方程对层合板层间的不同类型的粘接模型进行了分析.结合弹性材料修正后的Hellinger-Reissner变分原理和插值函数,构建了直角坐标系下8节点层合板的每一层的线性方程;考虑到脱层板的连接界面处应力和位移的关系,改进了现有的常用弱粘接模型,建立不同粘接模型的控制方程;最后通过求解整个板的控制方程,得到层合板的层间应力和位移.数值算例验证了该模型的正确性,并研究了层间界面为线性和非线性时的问题.结果表明:应用改进后的弱粘接模型,能够更好地模拟层合板的弱界面失效过程.  相似文献   

11.
约束层阻尼圆柱壳的自由振动   总被引:2,自引:0,他引:2  
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.  相似文献   

12.
This work investigates the active vibration control and vibration characteristics of a sandwich thin cylindrical shell whose intermediate layer is made of the graphene reinforced composite that is bonded with integrated piezoelectric actuator and sensor layers at its outer and inner surfaces. The volume fraction of graphene platelets in the intermediate layer varies continuously in the shell's thickness direction, which generates position-dependent effective material properties. The constitutive relations of the graphene reinforced composite and piezoelectric materials are given by taking one-dimensional steady thermal field into account. Considering Donnell's shell theory, a final equation of motion in terms of the generalized radial displacement is derived by using Hamilton's principle and Galerkin method. Shell's natural frequencies are derived considering influences of the thermo-electro-elastic field. Introducing a constant velocity feedback control algorithm, active vibration control of the sandwich cylindrical shell is presented by employing the Runge-Kutta method. The feedback control gain has a pronounced effect on the damping, as well as the inertia of the system. Comparisons between the present results and those in other papers are done to validate the present solutions. Influences of weight fractions, distribution patterns and geometrical sizes of graphene platelets, temperature variations, thicknesses of layers and the feedback control gain on the vibration characteristics and active vibration control behaviors of the novel sandwich cylindrical shell are discussed.  相似文献   

13.
微曲输流管道振动固有频率分析与仿真北大核心CSCD   总被引:2,自引:2,他引:0  
首次建立了基于Timoshenko梁理论的微曲输流管道横向振动的动力学模型,并分析了流体流动影响下微曲管道横向自由振动的固有特征.采用广义Hamilton原理,导出了考虑流体影响的微曲管道横向振动的控制方程,通过Galerkin截断对控制方程离散化,再由广义本征值问题得到管道横向振动的固有频率,并研究了液体流速和弯曲幅度对管道横向固有振动特征的影响.发展了基于等效刚度和等效阻尼方法的考虑流体影响的微曲管道振动分析的有限元仿真计算方法,并通过有限元软件实现数值仿真,验证了Galerkin截断的分析结果以及所建立的Timoshenko微曲管道动力学模型的有效性.研究表明,流体的流速以及管道的弯曲幅度对管道横向振动固有频率均有显著影响.  相似文献   

14.
The free vibration of laminated composite plates on elastic foundations is examined by using a refined hyperbolic shear deformation theory. This theory is based on the assumption that the transverse displacements consist of bending and shear components where the bending components do not contribute to shear forces, and likewise, the shear components do not contribute to bending moments. The most interesting feature of this theory is that it allows for parabolic distributions of transverse shear stresses across the plate thickness and satisfies the conditions of zero shear stresses at the top and bottom surfaces of the plate without using shear correction factors. The number of independent unknowns in the present theory is four, as against five in other shear deformation theories. In the analysis, the foundation is modeled as a two-parameter Pasternak-type foundation, or as a Winkler-type one if the second foundation parameter is zero. The equation of motion for simply supported thick laminated rectangular plates resting on an elastic foundation is obtained through the use of Hamilton’s principle. The numerical results found in the present analysis for free the vibration of cross-ply laminated plates on elastic foundations are presented and compared with those available in the literature. The theory proposed is not only accurate, but also efficient in predicting the natural frequencies of laminated composite plates.  相似文献   

15.
阻尼复合结构的抑振性能取决于材料布局和阻尼材料特性.该文提出了一种变体积约束的阻尼材料微结构拓扑优化方法,旨在以最小的材料用量获得具有期望性能的阻尼材料微结构.基于均匀化方法,建立阻尼材料三维微结构有限元模型,得到阻尼材料的等效弹性矩阵.逆用Hashin-Shtrikman界限理论,估计对应于期望等效模量的阻尼材料体积分数限,并构建阻尼材料体积约束限的移动准则.将获得阻尼材料微结构期望性能的优化问题转化为体积约束下最大化等效模量的优化问题,建立阻尼材料微结构的拓扑优化模型.利用优化准则法更新设计变量,实现最小材料用量下的阻尼材料微结构最优拓扑设计.通过典型数值算例验证了该方法的可行性和有效性,并讨论了初始微构型、网格依赖性和弹性模量等对阻尼材料微结构的影响.  相似文献   

16.
A formulation is presented for steady-state dynamic responses of rotating bending-torsion coupled composite Timoshenko beams (CTBs) subjected to distributed and/or concentrated harmonic loadings. The separation of cross section's mass center from its shear center and the introduced coupled rigidity of composite material lead to the bending-torsion coupled vibration of the beams. Considering those two coupling factors and based on Hamilton's principle, three partial differential non-homogeneous governing equations of vibration with arbitrary boundary conditions are formulated in terms of the flexural translation, torsional rotation and angle rotation of cross section of the beams. The parameters for the damping, axial load, shear deformation, rotation speed, hub radius and so forth are incorporated into those equations of motion. Subsequently, the Green's function element method (GFEM) is developed to solve these equations in matrix form, and the analytical Green's functions of the beams are given in terms of piecewise functions. Using the superposition principle, the explicit expressions of dynamic responses of the beams under various harmonic loadings are obtained. The present solving procedure for Timoshenko beams can be degenerated to deal with for Rayleigh and Euler beams by specifying the values of shear rigidity and rotational inertia. Cantilevers with bending-torsion coupled vibration are given as examples to verify the present theory and to illustrate the use of the present formulation. The influences of rotation speed, bending-torsion couplings and damping on the natural frequencies and/or shape functions of the beams are performed. The steady-state responses of the beam subjected to external harmonic excitation are given through numerical simulations. Remarkably, the symmetric property of the Green's functions is maintained for rotating bending-torsion coupled CTBs, but there will be a slight deviation in the numerical calculations.  相似文献   

17.
中利用达朗贝(d'Alembert)原理建立了置于温克勒(winkler)弹性地基上具有弹性联系的均质双层矩形截面梁体系的自由振动的微分方程式,利用伽辽金(Galerkin)法推出确定该双层梁体系自由振动频率的行列式,给出特征方程,作为算例,中对弹性地基上的双层均质梁,在简支边界条件下的基频进行了计算,所得结果,在不考虑梁间弹性联系的特殊情况下,与里兹(Ritz)法所确定的单梁自由振动的基频相符合。  相似文献   

18.
Damped free vibrations of multilayered composite cylindrical shells are investigated. Vibration and damping analysis of cylindrical shells is performed by using the first-order shear deformation theory (FOSDT). Based on other researchers' works, two damping models are developed, i.e., the energy method (EM), and the method of complex eigenvalues (MCE). Several numerical examples of the damped free vibration problem of laminated composite cylindrical shells have been solved and comparison has been made with the results of other authors.Published in Mekhanika Kompozitnykh Materialov, Vol. 31, No. 5, pp. 646–659, September–October, 1995.  相似文献   

19.
复合材料层合板的三维非线性分析   总被引:5,自引:1,他引:4  
本文提出了一种研究复合材料层合板壳三维问题的解析方法.该方法采用摄动方法和变分原理来满足三维弹性理论基本微分方程及限制条件,分析了受横向载荷作用的复合材料各向异性单层圆板及层合圆板的三维非线性问题.得到了高精确度的摄动级数解答.大量结果表明横向剪应力和横向正应力在层合板的三维非线性分析中是很重要的.  相似文献   

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