具有连接区的混合子结构模态综合法

本文提出具有连接区的间接对接的混合界面子结构模态综合性，讨论了位移协调和力与位移双协调两种对接模式。     

连结子结构与自由界面模态综合法在非线性动力分析中的应用

本文提出了一种由线性连接元和非线性连接元组成的连接子结构，并将这种连接子结构用于自由界面的模态综合技术。利用非线性振动理论的渐近方法，求得经模态综合法降维后系统方程的近似解析解。从而将具有连接子结构的自由界面的模态综合技术推广应用到具有局部非线性的复杂结构系统的动力分析，为利用非线性振动理论的渐近方法及动力系统理论进一步研究高维非线性动力学系统的振动特性、分岔及混沌行为创造了一种新的途径。算例表明，该方法具有足够的精度。     

具有连接区的混合子结构模态综合法

本文提出具有连接区的间接对接的混合界面子结构模态综合法，讨论了位移协调和力与位移双协调两种对接模式。     

混合界面直接分支模态综合法

在直接分支模态综合法(本质上属自由界面模态综合法)的基础上,提出并深入研究了混合界面直接分支模态综合法。混合界面法将复杂庞大的结构取做主体部件,而将与此主体部件相连的其余部分视为分支部件。对主体部件采用自由界面,分支部件则采用固定界面。各子结构之间完全独立计算,并且通过计入主、从子结构的剩余模态矩阵的办法来补偿所舍去的高阶模态分量,保证了计算精度。本方法从工程应用的实际出发,通过模拟航空发动机机匣管路系统的数值算例,验证了混合界面法的正确性。     

固定界面动态子结构方法研究车内噪声问题

随着社会的发展，降低车内噪声越来越受到人们的重视。由于整车结构复杂，本文采用包括软子结构的动态子结构方法，把整车模型划分为多个子结构，包括动力总成子结构、副车架子结构、车身与车内声场耦合子结构、非簧载质量子结构及多个线性和非线性软子结构等。采用固定界面模态综合法，建立整车结构车内声场流固耦合动力学模型。对于车身与车内声场耦合子结构，由于其总质量和刚度矩阵为非对称矩阵，传统的模态叠加法不能应用到耦合系统中，本文引入了左特征向量的概念，用左特征向量左乘原方程，使耦合系统微分方程得到解耦。在已建立的总系统动力学模型基础上，在时域内对前后轴分别激励时汽车振动和车内噪声特性进行仿真模拟，并通过台架试验对仿真结构进行验证。     

基于键合图法的多个子结构自由界面模态综合法研究和应用

将键合图方法用于动态子结构研究,提出了一种求解多个子结构自由界面模态综合法的新方法。通过一系列物理和数学上的分析,详细推导出多个子结构自由界面模态综合法的计算过程。在本文给出的算例中,基于键合图方法的自由界面模态综合法,通过建立各个子结构的状态空间方程,计算子结构相应的特征值矩阵和振型矩阵;这些子结构在进行模态综合后,获得整体结构的特征值矩阵和振型矩阵,该结果和原来整体结构完全相同,这进一步说明了本文提出的新方法的正确性。运用本文提出的方法建立状态空间方程,在子结构的模态综合过程中,不会产生系统特征值的增失根问题,确保了子结构在综合后其整体结构模态信息的完整性。     

子结构Ritz向量综合法

讨论了在动态子结构法中应用静态Ｒｉｔｚ向量替代模态向量时所应考虑的基本问题，即如何合理地定义荷载空间分布向量｛ｆ（ｓ）｝，以避免在子结构中出现低阶模态不连续分布的情况。文中给出了在自由子结构和约束子结构内进行Ｒｉｔｚ变换的一般形式及修正公式。算例表明：应用子结构Ｒｉｔｚ向量综合技术能有效地提高线性结构模态分析的计算效率     

改进的直接部件模态综合法

Yee和Tsuei提出的直接部件模态综合法将自由界面模态综合法与频响函数相结合 ,简化了计算过程、减少了计算量 ,并便于与实验模态分析相结合。本文在其基础上利用矩阵级数展开的方法将被截断高阶模态的贡献用保留模态和系统物理特性矩阵精确表达 ,结合分块计算方法 ,进一步减少了计算量并有效地提高了计算精度 ,且确定了模态截断准则。数值算例表明其行之有效     

固定界面子结构模态精确综合之非线性特征值问题的迭代解法

本文从模态综合过程出发，构造由于固定界面子结构模态精确综合所致非线性特征值问题的有效迭代格式。能用的Ｃｒａｉｇ固定模态综合结果成为其首次迭代近似。该方法克服了可保留模态数的限制，综合结果能达到指定精度。     

阻尼振动系统存在全实模态的条件

1.引言阻尼矩阵是描述系统运动微分方程的重要物理参数.对于系统的响应分析,阻尼项不可忽略.由于阻尼因素的复杂性,系统运动方程一般难以在对应的实模态空间中解耦.因此需要采用复模态理论进行动力分析,增加了分析计算的复杂性.如何判断阻尼系统能否化为等价的无阻尼系统及相应的形式,十分必要.本文根据矩阵函数的坐标变换关系,将系统化为与之     

The free-interface method of component mode synthesis for systems with viscous damping

This paper presents a new free-interface method of component mode synthesis for linear systems with arbitrary viscous damping. The left and right projection matrices described by slate-variable vectors are first introduced for components with rigid-body freedom. The operator function of projection matrices for state displacement and state force is proved, and then the state residual fiexibility matrix and the state residual inertia-relief attachment mode are defined and employed. The results of three examples demonstrate that the method proposed in this paper leads to very accurate system eigenvalues and high mode-synthesis efficiency     

Contact-impact formulation for multi-body systems using component mode synthesis

The efficiency and accuracy are two most concerned issues in the modeling and simulation of multi-body systems involving contact and impact. This paper proposed a formulation based on the component mode synthesis method for planar contact problems of flexible multi-body systems. A flexible body is divided into two parts： a contact zone and an un-contact zone. For the un-contact zone, by using the fixed-interface substructure method as reference, a few low-order modal coordinates are used to replace the nodal coordinates of the nodes, and meanwhile, the nodal coordinates of the local impact region are kept unchanged, therefore the total degrees of freedom （DOFs） are greatly cut down and the computational cost of the simulation is significantly reduced. By using additional constraint method, the impact constraint equations and kinematic constraint equations are derived, and the Lagrange equations of the first kind of flexible multi-body system are obtained. The impact of an elastic beam with a fixed half disk is simulated to verify the efficiency and accuracy of this method.     

Free vibration analyses by boundary element method using component mode synthesis

The boundary element method for dynamic analysis of two dimensional structures was developed by Nardini and Brebbia in 1983. Free vibration analysis of structures by BEM results in a generalized eigenproblem with coefficient matrices nonsymmetric and full. So, it costs a lot of CPU time to solve the eigenproblem. In order to reduce the cost the improved free interface coupling method has been adopted. By aid of lower eigenvectors and residual modes the degrees of freedom of substructure equaion of dynamic equilibrium can be reduced. By assembling the reduced substructure equations, the system of equations for the whole structure will be obtained. By using the traction and displacement compatibility conditions on the interface, the second transformation matrix has been developed for further reduction of system equations. The technique has been applied to some specific examples which give the evidence that the method is satisfactory and efficient.     

A new matrix perturbation method for analytical solution of the complex modal eigenvalue problem of viscously damped linear vibration systems

A new matrix perturbation analysis method is presented for efficient approximatesolution of the complex modal quadratic generalized eigenvalue problem of viscouslydamped linear vibration systems.First,the damping matrix is decomposed into the sum of aproportional-and a nonproportional-damping parts,and the solutions of the real modaleigenproblem with the proportional dampings are determined,which are a set of initialapproximate solutions of the complex modal eigenproblem.Second,by taking thenonproportional-damping part as a small modification to the proportional one and using thematrix perturbation analysis method,a set of approximate solutions of the complex modaleigenvalue problem can be obtained analytically.The result is quite simple.The new methodis applicable to the systems with viscous dampings-which do not deviate far away from theproportional-damping case.It is particularly important that the solution technique be alsoeffective to the systems with heavy,but not over,dampings.The solution formul     

非比例阻尼线性体系平稳随机地震响应计算的虚拟激励法

应用复振型分解方法,将非比例阻尼线性体系在地震作用下的动力方程求解问题转化为若干个广义复振子的求解与叠加问题。通过假定地震地面运动为一零均值的平稳随机激励,应用虚拟激励法原理,推导得到了广义复振子动力坐标的解析计算公式,进而得到了以复振型为基础的非比例阻尼线性体系随机地震响应计算的一般实数解析解答。算例证实了这种方法的可靠性及高效率。     

Eigenvalue-counting methods for non-proportionally damped systems

This paper presents numerical methods of counting the number of eigenvalues for non-proportionally damped system in some interested regions on the complex plane. Most of the eigenvalue analysis methods for proportionally damped systems use the well-known Sturm sequence property to check the missed eigenvalues when only a set of the lowest modes is used. However, in the case of the non-proportionally damped systems such as the soil–structure interaction system, the structural control system and composite structures, no counterpart of the Sturm sequence property for undamped systems has been established yet. In this study, a numerical method based on argument principle is explained with emphasis on the discretization of the contour and a new method based on Gleyse’s theorem is proposed. To verify the applicability of the methods, two numerical examples are considered.     

复振型导数计算的移位多次模态加速法

本文研究了含粘性阻尼结构的复振型导数计算问题，将导数计算问题看成是一个简谐激振的响应计算问题，采用多次模态加速法和移位法，导出了复振型导数计算的移位多次模态加速法。该方法具有明确的数学和物理意义，可导出已有的各种计算方法。算例表明本方法计算复振型导数只需用很少几个模态即可保证精度，计算量大大减少。