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。     

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。     

有正阻尼时强非线性振动问题的插值摄动解法

有正阻尼的非线性振动问题，无论是弱非线性或强非线性的情形，均不能用L－P法或改进的L－P法求解，本文用插值摄动法求解了有正阻尼的强非线性自由振动问题，运算简单，精度好。     

考虑固体域几何非线性的固液耦合系统瞬态有限元分析

本文基于理想可压缩流体压力传输方程及增量型ＴｏｔａＩＬａｇｒａｎｇｉａｎ列式，建立了考虑固体域几何非线性的固液耦合系统有限元方程，并开展了非线性分析工作。本文的方法可用于流体域远大于固体域，从而可仅仅研究固体域非线性响应的情况。由于流体域每个节点仅有一个未知量（压力），故流体域的计算规模得以大大减缩。同时，因为本文方法仅需对固体域进行非线性分析，故显著地简化了固液耦合非线性问题的求解工作。本文的方法亦可用于三维分析。     

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。     

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。     

杆系结构非线性损伤随机演化分析

通过研究结构非线性构形状态转移过程考察结构非线性损伤随机演化的思路，建立了作为Markov链的非线性构形状态转移过程的转移速率与屈服应变风险率函数之间的关系。进而，通过力学分析与非线性构形状态的逻辑分析得到转移速率矩阵，从而将一个结构非线性损伤随机演化问题转化为一个非时齐Markov链的分析问题，以三杆桁架结构为例，给出了数值分析结果。     

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

ＬＡＲＧＥＡＭＰＬＩＴＵＤＥＶＩＢＲＡＴＩＯＮＯＦＣＩＲＣＵＬＡＲＳＡＮＤＷＩＣＨＰＬＡＴＥＳＤｕＧｕｏ－ｊｕｎ（杜国君）（ＮｏｒｉｈｅａｓｉＩｎｓｔｉｔｕｔｅｏｆＨｅａｖｙＭａｃｈｉｎｅｒｙ,Ｑｉｑｉｈａｒ）（ＲｅｃｅｉｖｅｄＪａｎ．２,１９９２,...     

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.