压电超声电机的非线性动力学研究进展

压电超声电机 (ultrasonic motor, USM) 是一个具有闭环控制的机电耦合强非线性系统，在大功率情况下，会 表现出明显的非线性现象．其非线性因素主要表现为： (1) 定子与动子之间的接触非线性； (2) 定子材料非线性； (3) 温度、磨损等因素引起的缓变因素； (4) 驱动电网络中的非线 性因素．由于诸多非线性因素的存在，使得 USM 系统具有跳跃、滞后、共振频率漂移、死区 和饱和等非线性现象，同时，给 USM 的非线性动力学建模带来了困难．而 USM 闭环控制要求 有一个合理的动力学模型，因此，研究 USM 的非线性动力学建模是 USM 研究中的一个重要内 容．针对超声电机系统中普遍存在的非线性因素和非线性动力学建模方法进行了归纳， 对已有文献中有关超声电机非线性动力学的研究进行了总结，指出了有关该方面的若干研究 方向．     

空间拦截最优末端导引规律研究的新方法

给出了空间拦截控制的非线性微分方程，并在非线性控制系统引入了结构力学中的多重子结构法，从而求出了空间拦截非线性最优末端导引规律，同时给出了相应的数值仿真。     

非线性碟簧动力吸振器的宽带数值优化设计及其应用

提出了非线性碟簧动力吸振器的宽带数值优化设计，推广了前人在非线性动力吸振顺领域的研究，首先提出了计算耦合非线性动力吸振器的主系统的稳态响应的平均法，然后采用数值优化法详细的研究了非线性动力吸振器的宽带优化设计，系统讨论了质量比、主系统阴尼比、吸振器阴尼比、系统频率比、激励频率比、位移比、吸振器刚度非线性系数和吸振器阻尼非线性系数与抑带宽的关系，最后考虑了非线性动力吸振器的应用实例，指出非线性动力吸     

四边简支矩形板的蠕变损伤非线性弯曲

 基于Kachanov蠕变损伤理论和Von Karman非线性板理论，建立了在横向和面内载荷 共同作用下蠕变损伤四边简支矩形板的非线性弯曲平衡方程，采用有限差分法进行 数值迭代求解，分析了几何非线性、面内荷载等因 素对板非线性蠕变损伤特性的影响.     

一种微静电开关系统的非线性动力学

在微型电子机械（MEMS）中，存在着多种非线性因素，诸如：几何非线性、静电力的非线性以及空气阻力的非线性等，它们严重影响着微机械系统的行为。对于一种具有典型结构的微静电开关，考虑机械、静电、挤压气隙三部分的因素，导出了系统单自由度非线性运动方程（保留到三阶非线性），用数值方法分析了静电激励变化导致的分岔，发现倍周期分岔、逆倍周期分岔广泛存在于该类系统中。     

钢筋混凝土空间杆件精细非线性分析模型

针对现有钢筋混凝土空间杆件非线性分祈模型进行了评还，应用结构力学方法推导得到了沿秆长配筋分布均匀的钢筋混凝土空间杆件的非线性单元刚度矩阵，建立了应用高斯积分点所在截面的非线性性质描述钢筋混凝土空间杆件非线性的计算过程。对于沿杆长配筋分布不均匀的杆件，根据其实际情况，将其细分为两段或三段沿杆长配筋分布均匀的杆段，以沿杆长配筋分布均匀的钢筋混凝土空间杆件非线性分析模型为基础，建立了沿杆长配筋分布不均匀的空间杆件的非线性分析模型。最后，给出了两个算例。就本文方法及程序的计算结果与模型结构振动台试验结果、常规非线性杆件模型的计算结果进行了比较。     

考虑几何与材料及静风荷载的非线性因素的大跨径桥梁静风稳定分析法

针对现有的桥梁静风稳定分析方法中存在的问题，提出了增量与内外两重迭代相结合的新方法，并且考虑了结构几何、材料和静风荷载非线性。在上述方法的基础上，编制了桥梁非线性空气静力稳定分析程序BNAP，并进行了相应的算例分析，所得结果表明该方法具有计算稳定和速度快的优点。最后，以一座主跨1000米的斜拉桥为例，分析了结构几何非线性、材料非线性和静风荷载非线性对大跨径桥梁空气静力稳定性的影响。     

基于渗透率连续变化的低渗透多孔介质非线性渗流模型

基于低渗透多孔介质渗透率的渐变理论，确定了能精确描述低渗透多孔介质渗流特征的非线性运动方程，并通过实验数据拟合．验证了非线性运动方程的有效性。非线性渗流速度关于压力梯度具有连续-阶导数，方便于工程计算；由此建立了低渗透多孔介质的单相非线性径向渗流数学模型，并巧妙采用高效的Douglas-Jones预估一校正有限差分方法求得了其数值解。数值结果分析表明：非线性渗流模型为介于拟线性渗流模型和达西渗流模型之间的一种中间模型或理想模型，非线性渗流模型和拟线性渗流模型均存在动边界；拟线性渗流高估了启动压力梯度的影响，使得动边界的移动速度比实际情况慢得多；非线性越强，地层压力下降的范围越小，地层压力梯度越陡峭，影响地层压力的敏感性减弱，而影响地层压力梯度的敏感性增强。     

斜拉桥拉索-阻尼器系统非线性响应分析

考虑索的抗弯刚度、垂度及几何非线性的影响，得出了索一阻尼器系统的空间非线性振动偏微分方程，用中心差分法将微分方程在空间内离散，导出了系统的非线性振动常微分方程组。结合Newmark法及虚拟力法提出了一种用于求解非线性振动瞬态响应的杂交分析算法。并以典型的斜拉桥拉索为研究对象，给出了数值算例，并与Runge—Kutta直接积分法进行了比较，说明了杂交算法的准确性及有效性。     

空间杆系与叠层板组合结构的非线性稳定分析

本文用非线性有限元法研究一种空间杆系与复合材料叠层板组合结构的非线性稳定问题。将杆系离散成空间梁柱单元，将复合材料叠层板离散成复合材料叠层板单元，并考虑了几何非线性和板的成层正交各向异性性质。为了获得较高的计算效率并顺利通过稳定临界点，求解非线性平衡方程采用了变增量步长和柱面弧长法迭代策略。在考证了程序的正确性之后，具体分析了几个工程模型，得出了于工程设计有益的结论。     

Finite amplitude vibrations of an orthotropic circular plate with an isotropic core

The free and forced non-linear vibrations of a fixed orthotropic circular plate, with a concentric core of isotropic material, are studied. Existence of harmonic vibrations is assumed and thus the time variable is eliminated by a Ritz-Kantorovich method. Hence, the governing non-linear partial equations for the axisymmetric vibration of the composite circular plate are reduced to a set of ordinary differential equations which form a non-linear eigen-value problem. Solutions are obtained by utilizing the related initial-value problems in conjunction with Newton's integration method. The results reveal the effects of finite amplitude and anisotropy of materials upon the dynamic responses. Further, the method developed in this paper, which is used to solve the title problem, is one of some generality. It can be applied to many differential eigenvalue problems with piecewise continuous functions.     

Large amplitude vibration of circular sandwich plates

In this paper, fundamental equations of the axisymmetric large amplitude free vibration for circular sandwich plates are derived by means of Hamilton principle. In most cases, the sandwich plates are composed of very thin faces, then the preceding fundamental equations are simplified considerably. For an illustrative example, a circular sandwich plate with edge clamped but free to slip is considered, and then we got a pure analytic solution of the axisymmetric large amplitude free vibration with the aid of the modified iteration method, and derived an analytic relation for the amplitude-frequency response.     

Large Amplitude Vibration of Circular Sandwich Plate

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Geometrically non-linear free and forced vibrations of simply supported circular cylindrical shells: A semi-analytical approach

The non-linear free and forced vibrations of simply supported thin circular cylindrical shells are investigated using Lagrange's equations and an improved transverse displacement expansion. The purpose of this approach was to provide engineers and designers with an easy method for determining the shell non-linear mode shapes, with their corresponding amplitude dependent non-linear frequencies. The Donnell non-linear shell theory has been used and the flexural deformations at large vibration amplitudes have been taken into account. The transverse displacement expansion has been made using two terms including both the driven and the axisymmetric modes, and satisfying the simply supported boundary conditions. The non-linear dynamic variational problem obtained by applying Lagrange's equations was then transformed into a static case by adopting the harmonic balance method. Minimisation of the energy functional with respect to the basic function contribution coefficients has led to a simple non-linear multi-modal equation, the solution of which gives in the case of a single mode assumption an expression for the non-linear frequencies which is much simpler than that derived from the non-linear partial differential equation obtained previously by several authors. Quantitative results based on the present approach have been computed and compared with experimental data. The good agreement found was very satisfactory, in comparison with previous old and recent theoretical approaches, based on sophisticated numerical methods, such as the finite element method (FEM), the method of normal forms (MNF), and analytical methods, such as the perturbation method.     

NONLINEAR VIBRATION OF CIRCULAR SANDWICH PLATES UNDER CIRCUMJACENT LOAD

Based on von Karman plate theory, the issue about nonlinear vibration for circular sandwich plates under circumjacent load with the loosely clamped boundary condition was researched. Nonlinear differential eigenvalue equations and boundary conditions of the problem were formulated by variational method and then their exact static solution can be got. The solution was derived by modified iteration method, so the analytic relations between amplitude and nonlinear oscillating frequency for circular sandwich plates were obtained. When circumjacent load makes the lowest natural frequency zero, critical load is obtained.     

圆板非线性振动有限元分析的一种迭代方法

同时考虑横向振动和板平面内的运动,用3节点有限元研究均匀圆板的轴对称大振幅非线性振动,构造了一个避免发散加速收敛的平均迭代法,并将计算结果与文献的已有结果做了比较。     

Large deplection of corrugated circular plate with a plane central region under the action of concentrated loads at the center

This paper solves the problem of large deflections for corrugated circular plates with a plane central region under the action of concentrated loads at the center by means of the non-linear bending theory for anisotropic circular plates. Using the modified iteration method, the characteristic relation of the plate is obtained. This formula may be applied directly to design of elastic elements of measuring instruments.     

阶梯圆形和环形薄板的大幅度基本振动

利用修正迭代法求出了具有多个阶梯厚度圆形和环形薄板轴对称大幅度自由振动的一种新的解析解，导出了振幅和非线性振动基频的解析关系式，给出了较完善的数值计算结果，所得结果可供工程设计时参考。     

THE PROBLEM OF THE NON-LINEAR UNSYMMETRICAL BENDING FOR CYLINDRICALLY ORTHOTROPIC CIRCULAR THIN PLATE WITH VARIABLE THICKNESS

I-Intr0ducti0nThebendingproblemofcircularthinplateisimriartantbothintheoryandinengineeringpractice,butbecausethebasicequationsoftheproblemsofnon-linearunsymmetricalbendingf0rcircularthinplate'arenonlineardifferentialequations,itisquitedifficulttoobtainana…     

Non-linear vibrations of imperfect free-edge circular plates and shells

Large-amplitude, geometrically non-linear vibrations of free-edge circular plates with geometric imperfections are addressed in this work. The dynamic analog of the von Kármán equations for thin plates, with a stress-free initial deflection, is used to derive the imperfect plate equations of motion. An expansion onto the eigenmode basis of the perfect plate allows discretization of the equations of motion. The associated non-linear coupling coefficients for the imperfect plate with an arbitrary shape are analytically expressed as functions of the cubic coefficients of a perfect plate. The convergence of the numerical solutions are systematically addressed by comparisons with other models obtained for specific imperfections, showing that the method is accurate to handle shallow shells, which can be viewed as imperfect plate. Finally, comparisons with a real shell are shown, showing good agreement on eigenfrequencies and mode shapes. Frequency-response curves in the non-linear range are compared in a very peculiar regime displayed by the shell with a 1:1:2 internal resonance. An important improvement is obtained compared to a perfect spherical shell model, however some discrepancies subsist and are discussed.