NONLINEAR DYNAMIC ANALYSIS OF FLEXIBLE MULTIBODY SYSTEM

The nonlinear dynamic equations of a multibody system composed of ?exible beams are derived by using the Lagrange multiplier method. The nonlinear Euler beam theory with inclusion of axial deformation e?ect is employed and its deformation ?eld is …     

NUMERICAL STUDY OF PARTICLE DISTRIBUTION IN WAKE OF LIQUID-PARTICLE FLOWS PAST A CIRCULAR CYLINDER USING DISCRETE VORTEX METHOD

Particle-laden water flows past a circular cylinder were numerically investigated. The discrete vortex method (DVM) was employed to evaluate the unsteady water flow fields and a Lagrangian approach was applied for tracking individual solid particles. A dispersion function was defined to represent the dispersion scale of the particle. The wake vortex patterns, the distributions and the time series of dispersion functions of particles with different Stokes numbers were obtained. Numerical results show that the particle distribution in the wake of the circular cylinder is closely related to the particle's Stokes number and the structure of wake vortices: (1) the intermediate sized particles with Stokes numbers, St, of 0.25, 1.0 and 4.0 can not enter the vortex cores and concentrate near the peripheries of the vortex structures, (2) in the circular cylinder wake, the dispersion intensity of particles decreases as St is increased from 0.25 to 4.0.     

ON THE DYNAMICAL STRUCTURE OF THE WIND FIELD OF JUPITER''''S GREAT RED SPOT

Based on the geographic approximation the two-dimensional dynamical structure of the wind fields of Jupiterls Great Red Spot and White Oval BC is obtained. The results of calculation are in good agreement with the observations. Thus, an explanation of the observed dispersion of the velocities along the horizontal streamline is given. The major physical mechanism of this dispersion is as follwos: The distance between two adjacent elliptical streamlines varies along the elliptical streamline; leading to the variance of the normal pressure gradient. Thus, the horizontal velocity V_T has to vary correspondingly so that the Coriolis force can approximately balance the normal pressure gradient Another less important factor, i.e., the change of the Coriolis force parameter with the latitude, is also taken into account. The distributions of the vorticities of GRS and White Oval BC are also calculated.     

NONLINEAR STABILITY OF BALANCED ROTOR DUE TO EFFECT OF BALL BEARING INTERNAL CLEARANCE

Stability and dynamic characteristics of a ball bearing-rotor system are investigated under the effect of the clearance in the ball bearing. Different clearance values are assumed to calculate the nonlinear stability of periodic solution with the aid of the Floquet theory. Bifurcation and chaos behavior are analyzed with variation of the clearance and rotational speed. It is found that there are three routes to unstable periodic solution. The period-doubling bifurcation and the secondary Hopf bifurcation are two usual routes to instability. The third route is the boundary crisis, a chaotic attractor occurs suddenly as the speed passes through its critical value. At last, the instable ranges for different internal clearance values are described. It is useful to investigate the stability property of ball bearing rotor system.     

Surface wave transference in a piezoelectric cylinder coated with reinforced material

The present study deals with the propagation of a polarized shear horizontal(SH)wave in a pre-stressed piezoelectric cylinder circumscribed by a self-reinforced cylinder.The interface of the two media is assumed mechanically imperfect.For obtaining the dispersion relation,the mathematical formulation has been developed and solved by an analytical treatment.The effects of various parameters,i.e.,the thickness ratio,the imperfect interface,the initial stress,the reinforcement,and the piezoelectric and dielectric constants,on the dispersion curve are observed prominently.The dispersion curves for different modes have been also plotted.The consequences of the study may be used for achieving optimum efficiency of acoustic wave devices.     

Theoretical research on rotational dispersion coefficient of fiber in turbulent shear flow of fiber suspension

The rotational dispersion coefficient of the fiber in the turbulent shear flow of fiber suspension was studied theoretically. The function of correlation moment between the different fluctuating velocity gradients of the flow was built firstly. Then the expression, dependent on the characteristic length, time, velocity and a dimensionless parameter related to the effect of wall, of rotational dispersion coefficient is derived. The derived expression of rotational dispersion coefficient can be employed to the inhomogeneous and non-isotropic turbulent flows. Furthermore it can be expanded to three-dimensional turbulent flows and serves the theoretical basis for solving the turbulent flow of fiber suspension.     

Controllable wave propagation in a weakly nonlinear monoatomic lattice chain with nonlocal interaction and active control

The one-dimensional monoatomic lattice chain connected by nonlinear springs is investigated, and the asymptotic solution is obtained through the Lindstedt-Poincar′e perturbation method. The dispersion relation is derived with the consideration of both the nonlocal and the active control effects. The numerical results show that the nonlocal effect can effectively enhance the frequency in the middle part of the dispersion curve.When the nonlocal effect is strong enough, zero and negative group velocities will be evoked at different points along the dispersion curve, which will provide different ways of transporting energy including the forward-propagation, localization, and backwardpropagation of wavepackets related to the phase velocity. Both the nonlinear effect and the active control can enhance the frequency, but neither of them is able to produce zero or negative group velocities. Specifically, the active control enhances the frequency of the dispersion curve including the point at which the reduced wave number equals zero, and therefore gives birth to a nonzero cutoff frequency and a band gap in the low frequency range. With a combinational adjustment of all these effects, the wave propagation behaviors can be comprehensively controlled, and energy transferring can be readily manipulated in various ways.     

THE SIZE EFFECT ON THE DISPERSION OF A PARTICLE IN A HOMOGENEOUS ISOTROPIC TURBULENCE

The mechanism of the response motion of a suspended particle to turbulent motion ofits,surrounding fluid is different according to size of turbulent eddies.The particle isdragged by the viscous force of large eddies.and meanwhile driven randomly by smalleddies.Based on this understanding,the dispersion of a particle with finite size in ahomogeneous isotropic turbulence is calculated in this study.Results show that there aretwo competing effects:when enhanced by the inertia of a particle,the long-term particlediffusivity is reduced by the finite size of the particle.     

Generalized flyby trajectories around elongated minor celestial bodies as a rotating mass dipole

The aim of this paper is to understand the com-mon characteristics of the generalized flyby trajectory around natural elongated bodies. Such flyby trajectories provide a short-term mechanism to clear away vicinal objects or temporally capture ejecta into circling orbits. The gravita-tional potential of elongated bodies is described by a unified approximate model, i.e., the rotating mass dipole which is two point masses connected with a constant massless rod. The energy power is used to illustrate the flyby effect in terms of the instantaneous orbital energy. The essential of the single flyby trajectory is studied analytically, and the relationship between the flyby trajectory and its Jacobi integral is also illustrated. Sample trajectories are given to show the varia-tional trend of the energy increment with respect to different orbital periapsides. The distribution of natural ejecting orbits is presented by varying the parameters of the approximate model.     

FUNCTION OF REGION

The purpose of this paper is to extend points function and interval functions theoreticsto an arbitrary region.For this,the new theory.the contraction of a region,and theretraction of a region;the extension of a region,and the kernel-preserving extension of aregion are established by the author.Starting from these concepts,the new definitions of aregion function is given.And a kernel (i.e.fixed point) of a region function is connectedwith a stable centre of defining region of such a region function.Thereby,the regiontheoretics and algorithms are established.In applications,to find a stable centre of a region,the author has utilized the measuretheoretics of matrice defined by Hartfiel and other authors.The measure problems ofcoefficient matrice of system of equations of linear algebra associated with some region arediscussed.     

新型立式动平衡机的设计与分析

在分析传统的双面立式动平衡机的振动结构的基础上，设计了一种新的立式动平衡机的振动结构(即摆架)，采用新摆架结构的动平衡机可以实现静不平衡和偶不平衡的有效分离。文中详细分析了新摆架结构的特点，并在ANSYS7．0平台上对摆架进行了有限元模态分析和谐响应分析。由于新的摆架结构采用多块簧板，在多个部位刚度匹配，且采用多个传感器安装于测量点处，这样新的动平衡机可以直接测量静不平衡和偶不平衡，且相互影响极小。实践证明：采用新摆架结构的动平衡机特别适合于飞行物体的惯性测量，且克服了传统的双面立式动平衡机长期以来平面分离不佳的缺点，具有很高的推广价值。     

The identification of the vibration control system parameters designed for continuous miner machines

The Continuous Miner machines are exposed to time dependent loads during normal operation of the rock cutting process. These loads cause vibrations, which have a negative influence on the whole structure of the machine. This phenomenon can be eliminated by applying passive or active vibration control systems (VCS). Generally these systems are coupled with additional elements, which provide dispersion or transfer energy. The energy thus acquired can also reinforce the intended function such as rock cutting operation in the case of mining machines. The objective of this paper is to present the method of numerical identification of VCS parameters for Continuous Miner machines. The main function of the presented system is to reduce displacement of cutting drum by using elastic element joined to machine chassis and applying appropriate algorithm of control of the angular velocity of cutting drum. The method described improves efficiency of mining and increases durability of machine. In order to determine mechanical and control parameters of VCS the genetic algorithm optimisation method conjugated with numerical modal analysis was used. Finally the transient dynamic analysis was performed for the full-scale model of Continuous Miner in order to verify VCS in normal working condition.     

考虑人体耦合作用的结构竖向隔振研究

结构在环境振动或地震作用下的竖向振动不容忽略,有必要采取竖向隔振装置进行减振控制。考虑人体与结构耦合作用后不仅使隔振动力模型更加真实,还可以直接获得人体的动力响应。采用碟形弹簧支座对结构进行基础竖向隔振,并根据国际标准ISO5982规定的不同姿势下的人体动力模型,建立了考虑具有非经典阻尼的人与隔振结构耦合运动方程,利用复模态分析实现了方程的解耦,通过算例分析了竖向隔振以及人体作用对结构响应的影响。结果表明:对于一般的质量和刚度分布均匀的结构,人体对结构具有微弱的减振作用。碟形弹簧支座可以显著地降低结构的竖向振动并改善居住舒适度。     

CAE技术在井架设计中的应用

应用GAE技术，针对ZJ30／1700CZ钻机井架分别进行了静态分析及在自然状态和有钩载情况下的模态分析，为合理设计钻机井架结构提供了理论依据。通过分析计算，可以看出：所设计的井架的静态强度满足要求；经动力再设计后的井架固有频率与钻机的设计工作转速相差较大，达到工程要求，表明修改后的井架设计方案合理。     

按叠加于静态悬垂位形上小变形理论分析索的微幅振动

采用叠加于初应力位形上小变形问题的理论框架,分析叠加于索的静态悬垂位形上的微幅振动;给出了附加于静态位形上微幅振动的微分方程。在小拉伸柔度和附加于静态悬垂位形上的变形为微小变形的条件下,利用解析方法得出了悬垂面外与面内的微幅振动无耦合、悬垂面内竖向振动和水平振动可以解耦算出的结论。算例将微分方程的数值解法与ABAQUS有限元算法的计算结果进行了比较,误差小于4％,且前种算法得到的计算结果随时间衰减较快,计算精度和效率较高。     

张拉整体结构的动力学等效建模与实验验证

为了实现张拉整体结构高效动力学计算, 并考虑其大范围运动中柔性杆局部动态屈曲, 提出了一种受压细长杆动力学降阶模型, 采用五节点弹/扭簧集中质量离散模型等效连续杆的静力学和动力学特性. 首先, 通过静力学等效分析推导了弹簧拉压刚度和扭簧弯曲刚度表达式, 可准确预测杆件受压屈曲和近似预测其后屈曲行为. 第二, 通过动能等效分析推导了集中质量表达式, 可准确预测杆在线速度场下的运动. 第三, 通过弯曲振动固有模态等效分析确定弯曲刚度和节点质量的分布参数, 合适的分布参数取值组合可将降阶模型前两阶固有频率相对误差均降低至1%以内. 第四, 在全局坐标系下建立张拉整体结构瞬态动力学方程, 并利用静力凝聚法实现方程高效迭代求解. 最后, 分别对球形张拉整体结构准静态压缩、模态分析和碰撞动力学进行仿真和实验对比分析, 证明了提出的动力学降阶模型可有效预测张拉整体结构的静力学行为、固有振动特性及瞬态动力学响应, 并分析了结构参数变化对其力学特性的影响规律. 本文提出的动力学等效建模与计算方法, 可望用于软着陆行星探测器、大型可展开空间结构及点阵材料等复杂张拉整体系统的动力学分析与控制.      

模态分析和有限元法结合识别机械结构结合面动力学参数的研究

本文探讨了一种将实验模态分析和有限元法相结合，识别机械结构结合面动力学参数的新方法，以解决大型复杂机装拆不例，难于用实验方法识别部件间结合面动力学参数的问题。用些方法识别了一台遥臂钻床的接触度和接触阻尼。     

航天器与运载火箭耦合分析相关技术研究进展

本文以载荷分析为主要内容, 概述航天飞行器结构动力学研究的一些进展. 首先介绍航箭(航天器/运载火箭简称为航箭) 耦合系统载荷分析基本思想. 然后介绍以下3 个方面的载荷分析方法: (1) 采用基础激励理论初始载荷分析的近似方法; (2) 考虑航箭耦合影响的航天器/运载耦合系统分支模态综合法. 导出采用约束模态质量界面加速度的航天器载荷计算方法; 当仅考虑静定约束特殊情况时, 退化的方程与Chen 采用有限元法导出的方程相同. 给出新航天器载荷瞬态分析技术, 即一个以前的航天器/运载耦合系统载荷结果可以用来获得相同运载火箭发射一个新航天器结构的必要的载荷信息. (3) 考虑航箭耦合影响的航天器/运载耦合系统模态综合法. 包括: 固定界面模态综合法, 以及航天器/运载耦合的界面综合动态响应计算新方法. 最后, 介绍验证载荷分析技术. 简要讨论验证技术的重要性, 提出了采用试验与理论相结合的结构动态试验仿真技术,该方法包括了一套修正数学模型的新技术, 称之为子结构试验建模综合技术. 该方法已应用于复杂的结构建模. 在进行CZ-2E 运载火箭实尺模态试验之前, 用建议的模态试验仿真技术给出CZ-2E 模态参数的预示结果, 并与随后获得的实际模态试验结果相比, 两个结果彼此之间高度一致. 这个结果证明了模态试验仿真技术已成功地预示了CZ-2E 运载火箭的模态参数, 验证了建议的模态试验仿真技术的可靠性. 讨论了振动台振动试验仿真技术. 介绍了振动台振动试验仿真的几个关键技术. 包括: 有限元模型修正技术, 40 t 振动台系统台面控制仿真方法和D 卫星振动台振动试验仿真.      

Research on coupled thermo-hydro-mechanical dynamic response characteristics of saturated porous deep-sea sediments under vibration of mining vehicle

The excessive deformation of deep-sea sediments caused by the vibration of the mining machine will adversely affect the efficiency and safety of mining. Combined with the deep-sea environment, the coupled thermo-hydro-mechanical problem for saturated porous deep-sea sediments subject to the vibration of the mining vehicle is investigated. Based on the Green-Lindsay(G-L) generalized thermoelastic theory and Darcy's law, the model of thermo-hydro-mechanical dynamic responses for saturated porous deep-sea sediments under the vibration of the mining vehicle is established. We obtain the analytical solutions of non-dimensional vertical displacement, excess pore water pressure, vertical stress, temperature, and change in the volume fraction field with the normal mode analysis method, and depict them graphically. The normal mode analysis method uses the canonical coordinate transformation to solve the equation, which can quickly decouple the equation by ignoring the modal coupling effect on the basis of the canonical mode. The results indicate that the vibration frequency has obvious influence on the vertical displacement, excess pore water pressure, vertical stress, and change in volume fraction field. The loading amplitude has a great effect on the physical quantities in the foundation, and the changes of the physical quantities increase with the increase in loading amplitude.     

Seismic Evaluation of Multi-Storey RC Frame Using Modal Pushover Analysis

The recently developed pushover analysis procedure has led a new dimension to performance-based design in structural engineering practices. With the increase in the magnitude of monotonic loading, weak links and failure modes in the multi-storey RC frames are usually formed. The force distribution and storey displacements are evaluated using static pushover analysis based on the assumption that the response is controlled by fundamental mode and no mode shift takes place. Himalayan-Nagalushai region, Indo-Gangetic plain, Western India, Kutch and Kathiawar regions are geologically unstable parts of India and some devastating earthquakes of remarkable intensity have occurred here. In view of the intensive construction activity in India, where even a medium intensity tremor can cause a calamity, the authors feel that a completely up-to-date, versatile method of aseismic analysis and design of structures are essential. A detailed dynamic analysis of a 10-storey RC frame building is therefore performed using response spectrum method based on Indian Standard Codal Provisions and base shear, storey shear and storey drifts are computed. A modal pushover analysis (MPA) is also carried out to determine the structural response of the same model for the same acceleration spectra used in the earlier case. The major focus of study is to bring out the superiority of pushover analysis method over the conventional dynamic analysis method recommended by the code. The results obtained from the numerical studies show that the response spectrum method underestimates the response of the model in comparison with modal pushover analysis. It is also seen that modal participation of higher modes contributes to better results of the response distribution along the height of the building. Also pushover curves are plotted to illustrate the displacement as a function of base shear.