用声显微镜技术测量真实接触面积的研究

为了研究表面接触对润滑状态的影响，利用ＴＨＳＡＭ－５超声显微镜配以专门设计的辅助试验装置，测得了铝片－钢球的真实接触面积分别随载荷和加载时间变化的声学像，以及润滑剂的存在对测量结果的影响，发现真实接触面积是随着加载时间的延长而增大，而且载荷越大，真实接触面积越大，这是接触点发生塑性变形的结果。研究表明，声显微镜技术是测量真实接触面积的一种可行方法，但要将其作为一种定量测量手段却还有待于进一步的研究     

真实气体效应试飞器气动布局研究

针对真实气体效应飞行试验的要求对试飞器气动布局开展了设计研究,采用平衡气体模型对真实气体效应进行数值模拟,通过与理想气体状态方程数值模拟结果的比较,分析了真实气体效应对不同试飞器外形气动特性的影响规律,总结出真实气体效应试飞器外形的基本设计要素,给出了适用于真实气体效应飞行试验的试飞器气动布局．     

Generalized and exact solutions for oblique shock waves of real gases with application to real air

Calculation of the oblique shock wave of real gases is a difficult and time consuming problem because it involves numerical solution of a set of 10 equations, two of which (i.e., the equation of state and enthalpy function)—if available—are of a very complicated algebraic form. The present work presents a generalized method for calculating oblique shock waves of real gases, based on the Redlich-Kwong equation of state. Also described is an exact method applicable when the exact equation of state and enthalpy function of a real gas are available. Application of the generalized and the exact methods in the case of real air showed that the former is very accurate and at least twenty times faster than the latter. An additional contribution of the study is the derivation of real gas oblique shock wave equations, which are of the same algebraic form as the well known ideal gas normal shock wave relations.     

昆虫飞行参数测量实验研究进展

在昆虫飞行的实验研究中,可采用活体实验、模型实验和活体模型结合三种方法。活体实验可以客观反映自然界中昆虫的飞行规律,获得真实的实验数据,但可重复性差。模型实验作为机械装置可以重复进行试验,详细描述流场结构并定量各种参数大小,但与真实飞行存在一定差距。单独使用这两种中的任一方法均可对一些现象给出了解释。二者相结合的方法更易于准确描述昆虫的运动特征,通过对比模型与活体的结果来提出机理,尽管需要的实验周期较长,但结论往往更接近真实状态,基于该方法科学家们已提出了几种飞行机理。本文结合近几年文献报道,综述了昆虫飞行参数测量方法,并对以上几种方法在研究昆虫飞行机理中的作用进行了对比分析,认为模型和活体结合的研究方法更容易为一些飞行现象提出合理解释。     

Yeast protein-protein interaction network model based on biological experimental data

Duplication and divergence have been widely recognized as the two dominant evolutionary forces in shaping biological networks, e.g., gene regulatory networks and protein-protein interaction (PPI) networks. It has been shown that the network growth models constructed on the principle of duplication and divergence can recapture the topological properties of real PPI networks. However, such network models only consider the evolution processes. How to select the model parameters with the real biological experimental data has not been presented. Therefore, based on the real PPI network statistical data, a yeast PPI network model is constructed. The simulation results indicate that the topological characteristics of the constructed network model are well consistent with those of real PPI networks, especially on sparseness, scale-free, small-world, hierarchical modularity, and disassortativity.     

金属无润滑磨损过程的原位观察与研究

作者借助于新研制的可以直接观察磨损动态过程的试验装置和扫描电镜原位观察了无润滑条件下金属滑动表面的磨损特征与变化,发现摩擦表面可以划分为真实接触区和过渡磨损区,两者的磨损机理不同,真实接触区发生的是粘着磨损,而且磨粒沿摩擦力方向有明显增大的趋势;随着真实接触区的磨损,过渡磨损区可以逐渐转变为真实接触区,而且由于磨粒增多,非磨损区也可以逐渐转变为过渡磨损区。对磨损过程中摩擦力变化的测试结果表明,当磨损表面发生粘着时的粘着力与Bowden和Tabor粘着理论计算值十分接近。     

真实气体效应对返回舱气动力特性的影响

采用7 组元6 反应化学动力学模型,通过数值方法研究了真实气体效应对阿波罗(Apollo) 返回舱流场及气动力特性的影响. 并利用典型弹道点的飞行和实验数据验证了化学非平衡流计算程序的可靠性. 计算结果表明:真实气体效应主要发生在物面附近很薄的激波层内,真实气体效应使得激波脱体距离减小;真实气体效应使阻力系数和升力系数增加,且在小攻角时增加幅度最大;真实气体效应产生附加的低头力矩,使压心位置后移. 真实气体效应的影响随着马赫数的增加变化不明显.     

摩擦过程中真实接触面积的灰色分析

灰色系统理论是近几年以随机过程为研究对象而形成和发展起来的，在农业和自动控制等方面的研究与应用发展较快．为了使这种理论应用于摩擦学研究领域，从光全反射测量和计算机数值计算两方面，考察了粗糙表面接触时真实接触面积的随机特性，指出摩擦过程中的真实接触面积是一种含有随机成分的变化量，研究目标应当侧重于真实接触面积的变化趋势和范围，而不是它的精确解．在此基础上，首次利用灰色系统理论，分别对静态和动态接触条件下真实接触面积的变化规律进行了灰色分析，建立了精度比较高的预测真实接触面积的灰色模型ＣＭ（１，１）．这种模型对动、静接触面积的计算值与实测值具有良好的一致性，可以用于动态跟踪描述摩擦过程中真实接触面积的变化规律     

原子尺度摩擦行为的分子动力学模拟

应用大规模分子动力学方法,模拟了具有原子级光滑和原子级粗糙形貌的刚性球形探头与弹性平面基体的干摩擦行为,研究了无/有粘附条件下的载荷与摩擦力、载荷与真实接触面积,以及摩擦力与真实接触面积之间的关系,对纳米尺度下的摩擦行为规律进行了分析。几种系统的真实接触面积－载荷关系都与相应的连续力学接触模型定性的一致,它们分别是Hertz光滑表面接触模型、Greenwood-Williamson粗糙表面接触模型和Maugis-Dugdale粘着接触模型。无论是由光滑表面还是粗糙表面构成的摩擦系统,在无粘附条件下摩擦力与载荷成正比,而摩擦力与真实接触面积之间没有一个简单的关系;在粘附条件下摩擦力与真实接触面积成正比,而摩擦力与载荷之间表现为Maugis-Dugdale模型预测的亚线性关系。我们的研究表明,当表面作用从无粘附到粘附时,控制摩擦力的决定因素从载荷转变为接触面积,摩擦行为从载荷控制摩擦转变为粘着控制摩擦。     

Extended graphical representation of polynomials with applications to cybernetics

In this paper,the polynomial of a complex variable s(≡x iy)with realcoefficients K=a_0s~n a_1s~(n-1) …… a_(n-1)s a_n.is graphically represented by three plane curves which are the projections of aspace curve on three coordinate planes of the coordinate system(x,iy.K)inwhich K is confined to be real.The projection on(x,iy)plane is just the rootlocus of the polynomial with K as a real parameter.It is remarkable thatthe equation of the root-locus is m-th degree in y~2,whether n=2m 1 orn=2m 2.In addition to the real curve K.=f(x)in the figure(K,x)thereexists another curve K.which is plotted by the real parts of all complexroots against K.The(K,x)curve is particularly important to determine theabsolute as well as the relative stable interval of K for linear systems.For cybernetics,the(K,iy)curve can be used to show the relation betweenthe nature frequency ω and the gain K.Such three figures are useful forstudying the theory of equation and cybernetics.     

Fast estimation of stable regions in real models

The combined use of periodic orbit computation and Fast Lyapunov Indicator Maps of systems with three degrees of freedom is proposed as a tool for estimating qualitative stability in corresponding real models. Application to spacecraft mission analysis reveals very useful in finding real orbits with very long term stability properties.     

A new fundamental diagram theory with the individual difference of the driver’s perception ability

Based on the driver’s individual difference of the driver’s perception ability, we in this paper develop a new fundamental diagram with the driver’s perceived error and speed deviation difference. The analytical and numerical results show that the speed-density and flow-density data are divided into three prominent regions. In the first region, the speed-density and flow-density data are scattered around the equilibrium speed-density and flow-density curves of the classical fundamental diagram theory, where the widths of these scattered data are very narrow and slightly increase with the real density (i.e., the scattered data appear as two thicker lines); the running speed is approximately equal to the free flow speed and the real flow approximately linearly increases with the real density. In the second region, the speed-density and flow-density data are scattered widely in a two-dimensional region, but the shapes of these widely scattered data are related to the properties of the driver’s perceived error and speed deviation difference. In the third region, the scattered speed-density and flow-density data appear but these scattered data will quickly degenerate into the equilibrium speed-density and flow-density curves with the increase of the real density. Finally, the numerical results illustrate that the new fundamental diagram theory also produces the F-line, U-line, and L-line. The shapes of the scattered data, F-line, U-line, and L-line are relevant to the properties of the driver’s perceived error and speed deviation difference. These results are qualitatively accordant with the real traffic, which shows that the new fundamental diagram theory can better describe some complex traffic phenomena in the real traffic system. In addition, the above results can help us to further explain why the widely scattered speed-density and flow-density data appear in the real traffic system and better understand the effects of the driver’s individual difference on traffic flow.     

Finite-time real combination synchronization of three complex-variable chaotic systems with unknown parameters via sliding mode control

The problem of real combination synchronization between three complex-variable chaotic systems with unknown parameters is investigated by nonsingular terminal sliding mode control in a finite time. Based on the adaptive laws and finite-time stability theory, a nonsingular terminal sliding mode control is designed to ensure the real combination synchronization of three complex-variable chaotic systems in a given finite time. It is theoretically gained that the introduced sliding mode technique has finite-time convergence and stability in both arriving and sliding mode phases. Numerical simulation results are given to show the effectiveness and reliability of the finite-time real combination synchronization.     

Modified projective and modified function projective synchronization of a class of real nonlinear systems and a class of complex nonlinear systems

The modified projective and modified function projective synchronization of a class of chaotic real nonlinear systems, or a class of chaotic complex nonlinear systems, have been widely reported in the previous studies, respectively. In the paper, the modified projective and modified function projective synchronization between a class of chaotic real nonlinear systems and a class of chaotic complex nonlinear systems are first investigated. Based on the Lyapunov stability theory, the drive real system and response complex system can be synchronized up to the desired scaling constants and functions, respectively. The corresponding numerical simulations are performed to verify and demonstrate the validity and feasibility of the presented idea.     

A KIND OF STRUCTURAL MECHANICS TEACHING MODEL1)

基于目前土木工程本科生教学课程结构力学的教学现状,特别是几何体系讲解过于抽象的问题,本文借鉴国外相关经验,提出了基于实物的一种解决方案,即基于计算简图模拟几何体系的结构力学教学模型,并论述其必要性。通过介绍其组成构件、典型用途及使用示例,表明了其具有良好的教学辅助效果,体现了土木工程专业本科重要的专业基础课结构力学教学中,传统授课与创新探索相共存、简化图示和实物呈现相结合的重要作用。     

Mode I fracture analysis of a piezoelectric strip based on real fundamental solutions

In existing papers, mode I crack problems of piezoelectric ceramics are generally solved in complex domain because of the complex fundamental solutions of in-plane piezoelectric governing equations. In fact, these problems can alternatively be analyzed in real number field by recasting the solutions in real form instead. The main purpose of the present work is to develop such real fundamental solutions by detailed eigenvalue and eigenvector analyses. As an example of application, the widely studied fracture problem of a piezoelectric strip with a center-situated crack under mode I loading condition is then revisited based on the real fundamental solutions. Mixed boundary value conditions of the crack are transformed into Cauchy singular integral equations, which are then solved numerically to get fracture parameters including the energy release rate and intensity factors. Convergence behaviors of the kernel functions are surveyed. Theoretical derivation and computation are validated by the exact solution in a special case. The effect of a combined geometrical parameter on the crack is also investigated.     

轮轨三维弹塑性接触应力的算法研究

轮轨三维弹塑性接触应力的计算是研究轮轨接触疲劳的前提,本首次将ＣＯＮＴＡＣＴ程序与有限元方法相结合,考虑钢轨的真实几何形状和边界条件,形成了统一的轮轨滚动接触算法和软件ＣＭＥＦ,快速、有效地计算钢轨中真实的弹塑性应力场。     

四轮客货车安全车速实时监测模型的研究

考虑实际坡度条件下, 提出了基于压力传感器的汽车重心与安全车速实时监测系统的多元力学模型. 建立了考虑车辆重心高度、路面纵横双向坡度及路面半径等因素的车辆安全车速控制力学模型, 并在三维模型分析的基础上提出监测与报警机理, 可为汽车安全系统提供安全车速与重心计算的多维力学模型, 为研制汽车安全车速实时监测系统提供了必要参数与依据.     

飞机进气道流场压力畸变数据采集与处理系统

论述了一个用于飞机进气道出口流场动态压力畸变测试分析的高速数据采集及实时存储处理系统的研制背景、国内外情况、主要技术难题及已完成系统的组成、功能和技术性能，列出了研制中涉及到的若干关键技术     

真实火箭射流冲击流场中激波结构的实验研究

本文采用一种有效的激光-莫瑞光栅干涉系统首次拍摄到真实火箭燃气射流冲击流场的激波结构.解决了长期以来无法拍摄到高温、高速、强火焰光的火箭射流流场图像的问题。利用这一系统,研究了射流冲击流场中激波结构的一些变化规律,发现了一些新的激波结构。较系统地研究了欠膨胀射流冲击各种锥体的激波形态。