聚苯胺体系电流变流体的阻尼机理及阻尼模型研究

对聚苯胺体系电流变流体在正弦信号作用下的阻尼力响应及其频谱特性进行了理论和实验研究.提出电流变流体的非线性阻尼力的频谱是由基频和频率为基频奇数倍的高次谐波分量组成.建立了由粘性阻尼和迟滞阻尼组成的电流变流体阻尼模型,通过对模型的傅立叶变换及数值仿真,验证了理论分析及阻尼模型的正确性.     

低速混合型城市交通的流体力学模型

本文提出了一种新的交通流数学模型，它比目前常用的交通流模型更具有一般性，尤其适用于我国城市现阶段低速混合交通为主的实际状况。讨论了模型的连续形式和离散形式，定解条件的提法，模型参数的测定方法，以及数值解的稳定范围。几个实际的、难度较大的算例，显示这种模型具有良好的数值模拟功能。     

链状柔性多体机器人系统动力学研究

本文基于Ｊｏｕｒｄａｉｎ变分原理建立了具有链状拓扑结构柔性多体机器人系统动力学通用模型，用在一致质量有限单元法及正则模态分析基础上引入的模态坐标描述构件的弹性形，用独立坐标描述相邻板件间的大位移运动，每个铰容许１－６个自由度，组强非线性惯性耦合的封闭形式的系统动力学微分方程组，文末对单弹性臂和双弹性臂机器人操作手进行动力学仿真。     

低Pr数流体非稳态自然对流流动的标度分析

施加了恒定热通量的竖直平板置于静止的均匀或线性分层流体中会在板壁上形成自然对流流 动. 它在达到稳态前将先历经起始和过渡两个阶段. 而表征其瞬时流动特征的主要参数是壁温、热边界层厚度、内层和外层速度边界层厚度、边界层内竖直方向的最大速度、以及层流边界层发展达到稳态所需的时间. 利用标度分析得到了均匀和线性分层低普郎特数(Pr<1)流体沿恒定热通量竖直平板的非稳态自然对流流动在各个发展阶段的标度关系.     

FLUID DAMPING OF AN ELASTIC CYLINDER IN A CROSS-FLOW

Damping characteristics of fluid–structure systems are difficult to measure or calculate. In the past, such data have been rather scarce. This study reports an attempt on the use of a numerical approach to derive damping ratios related to fluid–structure interactions. It is based on an autoregressive moving-average (ARMA) method, which is used to analyse the displacement time series obtained from a numerical simulation of an elastic cylinder in a uniform cross-flow. The damping ratios show a similar trend to those obtained in previous experiments. An alternative way to deduce damping ratios is to decompose the transverse force in the structural dynamics equation into a drag (or out-of-phase) and an inertia (or in-phase) component for analysis. The damping thus deduced is in fair agreement with that obtained from ARMA; however, at or near synchronization, where the natural frequency of the stationary cylinder is close to the vortex shedding frequency, there is a very substantial difference between the two results.     

输液管的非线性振动、分叉与混沌——现状与展望

围绕输液管的非线性振动、分叉与混沌问题，对近几年来的主要研究工作加以综述并提出预测，其中包括运动方程中非线性项的归纳与讨论、非线性动力分析的一些现代计算方法、定常流速下输液管的分叉与混沌行为、振荡流速下输液管的参数共振以及今后值得进一步研究的某些问题．     

INSTABILITY AND CHAOS IN A PIPE CONVEYING FLUID WITH ADDED MASS AT FREE END

This paper shows the mechanism of instability and chaos in a cantilevered pipe conveying steady fluid. The pipe under consideration has added mass or a nozzle at the free end. The Galerkin method is used to transform the original system into a set of ordinary differential equations and the standard methods of analysis of the discrete system are introduced to deal with the instability. With either the nozzle parameter or the flow velocity increasing, a route to chaos can be observed very clearly: the pipe undergoing buckling (pitchfork bifurcation), flutter (Hopf bifurcation), doubling periodic motion (pitchfork bifurcation) and chaotic motion occurring finally. The project supported by the National Key Projects of China under grant No. PD9521907 and Science Foundation of Tongji University under grant No. 1300104010.     

计算流体力学在炼钢中的应用和发展

介绍了计算流体力学应用到炼钢过程中所面临的边界条件和材料物性数据等问题．并着重评述了钢包精炼和连铸结晶器过程中流动及相关现象研究概况,指出炼钢过程中数值模拟的目标不是获得描述某给定过程的精确数值,而是获取过程知识,特别是获取实验无法得到的信息．数值模拟不能代替实验,相反是扩大实验的内容．将来的炼钢过程数值模拟工作将面临更复杂的三维、时间相关的多相反应系统或气金渣等自由表面问题的挑战．      

航天器铰接结构非线性动力学特性研究进展

航天器铰接结构非线性动力特性研究直接关系到航天器动力学模型的建立、航天器姿态控制方案的制定、有效载荷指向稳定度的保持以及部件可靠性的提高, 是航天器设计领域的研究重点之一. 首先介绍航天器铰接结构研究中发现的非线性动力学现象和对该类问题的研究思路, 然后分别对铰链非线性和高维非线性系统动力学研究的最新研究成果进行介绍, 最后对航天器铰接结构非线性动力学特性研究的发展前景进行总结.      

输液管模型及其非线性动力学近期研究进展

综述了输液管系统的各类物理模型及其相应的数学模型,在流体满足基本假设条件下,对于管道内径远远小于管道长度的直管和曲管,详细叙述了梁模型管动力学数学模型的建模过程以及建模方法,针对在水动压力作用下以及管道短而且薄的情形,综述了壳模型的输液管道的动力学方程.在此基础上,概述了近几年来输液管道的非线性振动、稳定性、分岔与混沌、特别是管道控制的研究现状,并对今后的发展趋势作了分析和预测.综观非线性动力学理论的发展历程可以发现选取研究对象和典型的数学模型是至关重要的.对于低维的非线性系统,常常选用van der Pol、Duffing、Mathieu、Lorenz等典型系统来进行研究工作的.通过本文可以看出,对于研究高维非线性系统动力学,流诱发输液管的动力学问题是非常典型的模型之一,它有着容易理解的工程背景、包含了梁和壳的振动问题,并且它的数学模型相对简单,然而却能包含非常复杂的非线性动力学现象,同时容易解释数学方法得到的结果易对应到工程中的实际现象.本文希望通过对输液管动力学模型及其非线性动力学和控制研究现状的综述,建立高维非线性动力学的分析模型,以便发展高维非线性动力学的分岔与混沌理论,同时建立相应的控制理论基础.      

NONLINEAR DYNAMICS AND SYNCHRONIZATION OF TWO COUPLED PIPES CONVEYING PULSATING FLUID

In this paper, the nonlinear dynamical behavior of two coupled pipes conveying pulsating fluid is studied. The connection between the two pipes is considered as a distributed linear spring. Based on this consideration, the equations of motion of the coupled two-pipe system are obtained. The two coupled nonlinear partial differential equations, discretized using the fourth- order Galerkin method, are solved by a fourth-order Runge-Kutta integration algorithm. Results show that the connection stiffness has a significant effect on the dynamical behavior of the coupled system. It is found that for some parameter values the motion types of the two pipes might be synchronous.     

约束层阻尼板动力学问题的半解析解

利用条形传递函数方法(SDTFM)得到了约束层阻尼(CLD)板动力学问题的半解析解.首先对CLD板沿纵向离散成多个条形单元,基于Hamilton原理推导出条形单元的刚度矩阵和质量矩阵,仿照有限元法组集得到系统的总刚度矩阵和总质量矩阵.经Laplace变换后引入状态向量,采用分布参数传递函数方法在状态空间内建立CLD板的控制方程并进行求解.最后以对边固支和悬臂CLD板为例,得到了板的动力学特性和频响曲线,并与NASTRAN或相关文献结果进行了比较,吻合良好,验证了该方法的有效性.从推导过程和算例可以看出,该方法所需的单元数目少,获得的是半解析解,计算效率高且准确可靠.     

计算流体力学中的验证与确认

计算流体力学(CFD)在航空航天等诸多领域的应用越来越广泛.特别是近年来, CFD在实际飞行器的设计中扮演着越来越重要的角色, 许多设计参数直接来源于CFD的计算结果.由此, 飞行器设计师对CFD提供结果的可信度提出了更高的要求.验证(verification)与确认(validation)是评价数值解精度和可信度的主要手段.本文综述了国内外开展CFD验证与确认研究的进展.在引言中论述了开展CFD验证与确认的重要性和必要性, 简述了国内外CFD验证与确认研究的历史和发展现状.第2节中讨论了CFD验证与确认的一些基本概念,以及这些概念定义的形成过程, 并指出了进行CFD验证与确认的基本步骤.第3节和第4节分别讨论了CFD验证与确认的方法, 如CFD验证中的精确解比较方法, 制造解比较方法, 网格收敛性研究;CFD确认中的层次结构, 流动分类法, 确认实验指南.在第5节中我们列举了几个CFD验证与确认的应用实例.最后, 对我国开展CFD验证与确认研究工作提出了若干建议, 包括:(1)开展流动分类法研究,(2)推行软件质量工程方法,(3)开展规范精细的实验, 建立国内的网络数据库.      

三层流体中斜入射波作用下半无限板的水弹性响应

解析地研究了在三层流体中斜入射波浪与半无限弹性板的相互作用引起的波散射和板的水弹性响应. 三层流体在界面处的密度发生阶跃, 各层为一常数. 假设流体不可压缩、无黏、流体运动无旋. 在线性势流理论框架下, 使用本征函数展开法和内积式给出波板相互作用的半解析解. 根据色散关系分析, 得到了表面波模态和界面波模态入射时的临界入射角. 随着物理参数的变化, 临界角将随之发生变化. 临界角决定了当由开阔水域向板覆盖水域传播的表面波或界面波的存在性: (1)板覆盖水域入射界面上, 透射波能否存在; (2)入射界面之上界面中, 板覆盖水域中的透射波以及开阔水域中的反射波能否存在. 当下界面波入射时并且入射角足够大时, 开阔水域中的下界面波模态是整个流体域中唯一存在的模态.      

ON THE ADDED MASS AND DAMPING OF PERIODIC ARRAYS OF FULLY OR PARTIALLY POROUS DISKS

Infinite and periodic arrays of porous disks are considered, in oscillatory flow perpendicular to their planes. This configuration is of interest for the offshore oil industry, for instance to be used as dampers to reduce the heave motion of truss SPAR platforms. The hydrodynamic problem is solved by the method of matched eigenfunction expansions, under the assumptions that losses of head, proportional to the square of the traversing velocities, occur at the disks, and that potential flow theory is applicable. Added mass and damping coefficients are derived, as functions of the relative spacings between the disks, and of the parameter (A/a)(1−τ)/(2 μτ²), where A is the flow motion amplitude, a the disks radii, τ the porosity, or open-area ratio, andμ a discharge coefficient, close to 0.5. Results are also given for disks that are partially porous, from their axis to some radial distance. The practical applicability of the obtained results is discussed.     

MODELING AND DYNAMICS ANALYSIS OF SHELLS OF REVOLUTION BY PARTIALLY ACTIVE CONSTRAINED LAYER DAMPING TREATMENT

A new model for a smart shell of revolution treated with active constrained layer damping （ACLD） is developed, and the damping effects of the ACLD treatment are discussed. The motion and electric analytical formulation of the piezoelectric constrained layer are presented first. Based on the authors~ recent research on shells of revolution treated with passive constrained layer damping （PCLD）, the integrated first-order differential matrix equation of a shell of revolution partially treated with ring ACLD blocks is derived in the frequency domain. By virtue of the extended homogeneous capacity precision integration technology, a stable and simple numerical method is further proposed to solve the above equation. Then, the vibration responses of an ACLD shell of revolution are measured by using the present model and method. The results show that the control performance of the ACLD treatment is complicated and frequency-dependent. In a certain frequency range, the ACLD treatment can achieve better damping characteristics compared with the conventional PCLD treatment.     

MASS PRODUCTION OF NANOPARTICLES BY HIGH GRAVITY REACTIVE PRECIPITATION TECHNOLOGY WITH LOW COST

Mass production of nanoparticles at low cost has attracted much attention from industrial and academic circles. In this paper, a novel method, the high gravity reactive precipitation (HGRP) technology, of manufacturing CaCO3 nanoparticles, presently scaled-up to an annual capacity of 10,000 tons, is presented. This paper describes the process princ/ple, the process design and experiments on the syntheses of 15-30 nm CaCO3, 30-50 nm SiO2,20-30 nm TiO2, 20-60 nm ZnO, 20-30 nm ZnS, 30 nm SrCO3, 40-70 nm BaTiO3, stick-like nano BaCO3 as well as nano-fibrillar aluminum hydroxide measuring 1-10 nm in diameter and 50-300 nm in length, using liquid-liquid,gas-liquid and gas-liquid-solid reactant systems. The advantage of using the HGRP technology is illustrated by comparison to conventional methods.     

结构动力学与运载火箭技术发展

力学作为工程研究的基础学科,在运载火箭的设计中起着至关重要的作用.结构动力学作为分支学科之一在其中扮演着重要角色,其发展水平很大程度上可反映火箭总体设计能力.本文着眼于结构动力学与运载火箭技术的结合点,简述其发展过程,并对其进一步发展方向提出设想.     

CFD模拟方法的发展成就与展望

本文综述了计算流体力学(computational fluid dynamics, CFD),尤其是计算空气动力学的发展概况.从计算方法、网格技术、湍流模型、大涡模拟等方面分别总结了CFD所取得的成就,分析了当前存在的问题、困惑,展望了其发展趋势.在CFD计算方法中,主要介绍了中心格式、迎风格式、TVD格式、WENO格式、紧致格式以及间断Galerkin有限元方法,对不同方法的原理和特性进行了系统阐述.网格技术包括结构网格、非结构网格、混合网格以及重叠网格,重点讨论了重叠网格的若干关键技术.在湍流模型中,对目前的模型进行分类介绍,包括线性涡黏性模型、二阶矩模型、非线性模型等,还介绍了转捩模型、DES方法以及SAS方法等.在大涡模拟方法中,就其中若干相关的研究方向进行了探讨,包括滤波方法、亚格子模型、收敛标准、数值格式等. 文中还包含了作者在相关领域的若干研究成果.