高瓦斯煤层冲击地压发生条件与影响因素

针对高瓦斯煤层冲击地压问题,用解析方法得到冲击地压发生条件,分析了主要影响因素对满足冲击地压发生条件的临界塑性区半径和临界应力的影响规律.结合五龙矿开采实际情况对影响高瓦斯煤层冲击地压的煤的模量比、煤层瓦斯孔隙压力、支护应力和内摩擦角4个因素做了对比分析.研究发现:高瓦斯煤层在巷道掘进面附近由于存在开挖面空间效应,掘进面前方尚未开挖的煤体对巷道变形起到了限制作用,减少了冲击地压的发生,随着掘进面向前推进,后方一定距离范围内的巷道支护应力增大.随着瓦斯解吸渗流的进行,巷道壁处孔隙压力降低,巷道冲击地压危险性明显提高,此时提高支护应力,冲击危险性有所降低.高瓦斯煤层巷道发生冲击地压的临界塑性区半径和临界应力随模量比、瓦斯孔隙压力的增大而快速减小,随支护应力的增大而增大,临界塑性区半径随内摩擦角的增大而增大,临界应力与内摩擦角不是单调函数关系,存在一个极小值点,当内摩擦角小于此极小值时,临界应力随内摩擦角增大而减小;当内摩擦角大于此极小值时,临界应力随内摩擦角增大而增大.     

含空心球涂层粒子复合材料界面的脱粘应力分析

在球对称拉伸载荷作用下针对空心球涂层复合材料分析了空心球涂层粒子增强复合材料的局部应力场，得到了界面临界脱粘应力的解析表达式．讨论了各相几何参数对非均匀涂层空心球粒子临界脱粘应力的影响，比较了均匀涂层和非均匀涂层的脱粘应力．结果表明：在球对称拉伸下界面脱粘更容易发生在涂层相与基体相界面间，空心球的壁厚和涂层厚度是影响界面临界脱粘应力的重要因素，因而选择适当的空心球、涂层厚度和提高界面粘结能将有利于提高界面的临界脱粘应力．     

高速铁路CRTS Ⅱ型板式无砟轨道结构临界荷位和最不利位置分析

为了研究高速铁路CRTS Ⅱ型板式无砟轨道结构的临界荷位和最不利位置,以京沪高速铁路CRTS Ⅱ型板式无砟轨道结构为例,选取轨道板板底的纵向弯拉应力作为确定轨道结构临界荷位的指标,计算得到了列车轴载位于板端位置为临界荷位;计算了轴载在临界荷位时的钢轨竖向位移、轨道板板底水平拉应力、CA砂浆层竖向压应力、底座(或支承层)板底水平拉应力,分析了车辆荷载在不同位置处的无砟轨道结构产生的应力大小,得出路基和桥梁上CRTS Ⅱ型无砟轨道结构的最不利位置。     

切应力协同下受热过冷层流液膜的破断特性

针对界面切应力协同下受热过冷层流液膜流动的破断过程, 建立了不同气液流向下的临界液膜厚度和最小润湿量的理论模型, 分析了不同驱动力作用下, 接触角、流体温度、界面切应力和壁面热流密度对液膜破断特性的影响. 研究表明: 临界液膜厚度和最小润湿量均随壁面热流密度的增加而增大; 重力驱动下的接触角影响在不同热流密度下有所不同, 流体温度在不同驱动力下对最小润湿量的影响截然相反; 同向切应力驱动下临界液膜厚度和最小润湿量随切应力增加而减小; 在重力和切应力协同驱动下, 同向切应力对最小润湿量的影响与重力和切应力所起作用的相对大小有关, 反向切应力使得临界液膜厚度和最小润湿量有所增大.      

多轴载荷下缺口试件疲劳寿命预测研究

基于临界平面法,在分析光滑薄壁圆管试件疲劳寿命预测模型的基础上,借助有限元应力应变分析,进一步将模型推广应用到了缺口试件的多轴疲劳寿命预测中,并利用坐标变换原理,明确了临界平面及有效循环变量的确定方法.在存在平均应力的情况下,分析了平均应力对疲劳寿命的影响,并对所建模型进行了平均应力修正.     

多轴载荷下缺口试件疲劳寿命预测研究

基于临界平面法,在分析光滑薄壁圆管试件疲劳寿命预测模型的基础上,借助有限元应力应变分析,进一步将模型推广应用到了缺口试件的多轴疲劳寿命预测中,并利用坐标变换原理,明确了临界平面及有效循环变量的确定方法.在存在平均应力的情况下,分析了平均应力对疲劳寿命的影响,并对所建模型进行了平均应力修正.     

拉扭复合加载下循环应力应变关系的研究

以拉扭簿壁管试件为研究对象,根据多轴临界面上的应力应变特性及多轴疲劳临界面法的结果,结合单轴循环应力应变关系,研究了多轴比例与非比例加载下的循环应力应变关系,推导出多应力应变关系模型,经拉扭复合比例与非比例物载试验难证,其预测结果与实测值相符合。     

一个可区分破坏模式的新应力三轴度参数

三轴应力状态对破坏模式影响很大,但是根据应力三轴度的传统定义难以定量地判断破坏模式。本文根据准脆性断裂和塑性屈服的发生条件,从二者被满足的先后顺序角度,提出了一个新的应力三轴度定义以及临界三轴度这一材料常数。区分破坏模式的判据可简单地表示为:当应力三轴度大于材料的临界三轴度时,则发生准脆性断裂;当应力三轴度小于临界三轴度时,则先发生屈服和塑性变形。通过对平面应力和平面应变状态下椭圆孔孔边应力三轴度的理论分析,提出了有限厚度板中裂尖应力三轴度的数值计算方法,考察了不同板厚下单边裂纹裂尖应力三轴度沿板厚方向的分布特点,并给出了相应的经验公式。     

自紧身管临界裂纹尺寸的概率断裂力学研究

基于概率断裂力学理论和Mome Caflo模拟方法，本文进行了自紧身管临界裂纹尺寸的可靠性研究。自紧身管内表面的疲劳裂纹考虑为半椭圆形式。裂纹尖端处的应力强度因子由内压和自紧残余应力共同产生。自紧残余应力采用了符合身管材料具有强化和包辛格效应性能推导的公式计算，它产生的应力强度因子通过权函数方法得到。根据断裂准则，可计算出自紧身管的临界裂纹尺寸。实例分析表明，对数正态分布为临界裂纹尺寸的最佳分布，同时给出了在各种置信度和可靠度下自紧身管的临界裂纹尺寸。     

正交各向异性薄板的弹塑性屈曲分析

本文应用混合硬化正交各向异性塑性理论和屈曲的能量法则，推导了正交各向异性薄板在面内压缩情况下的弹塑性稳定方程，计算了相应的临界荷载，并讨论几何形状、边界条件及诱导荷载比等对临界应力的影响。分析表明材料的各向异性性质对弹塑性临界应力的有较大的影响。     

Motion stability of high-speed maglev systems in consideration of aerodynamic effects: a study of a single magnetic suspension system

In this study, the intrinsic mechanism of aerodynamic effects on the motion stability of a high-speed maglev system was investigated. The concept of a critical speed for maglev vehicles considering the aerodynamic effect is proposed. The study was carried out based on a single magnetic suspension system, which is convenient for proposing relevant concepts and obtaining explicit expressions. This study shows that the motion stability of the suspension system is closely related to the vehicle speed when aerodynamic effects are considered. With increases of the vehicle speed, the stability behavior of the system changes. At a certain vehicle speed, the stability of the system reaches a critical state, followed by instability. The speed corresponding to the critical state is the critical speed. Analysis reveals that when the system reaches the critical state, it takes two forms, with two critical speeds, and thus two expressions for the critical speed are obtained. The conditions of the existence of the critical speed were determined, and the effects of the control parameters and the lift coefficient on the critical speed were analyzed by numerical analysis. The results show that the first critical speed appears when the aerodynamic force is upward, and the second critical speed appears when the aerodynamic force is downward. Moreover, both critical speeds decrease with the increase of the lift coefficient.     

Slip yield stress effects in start-up Newtonian Poiseuille flows

Analytical solutions are derived for various start-up Newtonian Poiseuille flows assuming that slip at the wall occurs when the wall shear stress exceeds a critical value, known as the slip yield stress. Two distinct regimes characterise the steady axisymmetric and planar flows, which are defined by a critical value of the pressure gradient. If the imposed pressure gradient is below this critical value, the classical no-slip, start-up solution holds. Otherwise, no-slip flow occurs only initially, for a finite time interval determined by a critical time, after which slip does occur. For the annular case, there is an additional intermediate (steady) flow regime where slip occurs only at the inner wall, and hence, there exist two critical values of the pressure gradient. If the applied pressure gradient exceeds both critical values, the velocity evolves initially with no-slip at both walls up to the first critical time, then with slip only along the inner wall up to the second critical time and finally with slip at both walls.     

THE DETERMINATION OF BUCKLING POINT AND CRITICAL LOAD OF COMPRESSIVE MEMBER

为了分析压杆失稳的临界力与失稳后杆件屈服形态的关系,在理论推导和试验研究的基础上,提出了通过捕捉细长压杆失稳时的失稳点来确定压杆临界力的分析方法,通过测量细长压杆失稳时微弯状态下杆端的纵向位移,求得临界压力的大小. 文中将该方法的实验结果与直接用欧拉公式计算的临界压力进行了比较,结果表明,考虑细长压杆微弯状态时杆端的纵向位移所得到的失稳的临界压力值大于利用欧拉公式计算的临界压力值.     

A fundamental study of a variable critical nozzle flow

Critical nozzle is defined as a device to measure the mass flow rate with only the nozzle supply conditions, making use of the flow choke phenomenon at the nozzle throat. Recently, such critical nozzles have been extensively utilized to measure the mass flow rate in a variety of industrial applications. For the measurement of mass flow rates in a wide range of operation conditions, the critical nozzle is required to be designed with different diameters. The objective of the present study is to investigate the effectiveness of a variable critical nozzle. A rod with a small diameter is inserted into the critical nozzle to change the effective cross-sectional area of the critical nozzle. Experimental work is performed to measure the mass flow rate of the critical nozzle with rod. Computational work is carried out using the two-dimensional, axisymmetric, compressible Navier–Stokes equations which are discretized using a fully implicit finite volume method. The diameter of the rod is varied to obtain different mass flow rates through the variable critical nozzle. Computational results predict well the measured mass flow rates. The boundary layer displacement and momentum thickness at the throat of the critical nozzle are given as a function of Reynolds number. The discharge coefficient of the critical nozzle is given as an empirical equation.     

网链缠结对凝胶薄膜起皱的影响

凝胶薄膜在变形时易发生屈曲、起皱等失稳现象,这在凝胶薄膜的应用中是非常重要的．近年来,针对凝胶薄膜的屈曲、起皱失稳行为,越来越多的科研人员尝试从力学角度进行分析．但是大多数的研究是基于Flory-Rehner弹性凝胶理论,未考虑凝胶网链缠结引起的物理交联对凝胶自由能的影响,模型精度不高．本文采用Edwards-Vilgis所提出的Slip-link模型对平面内起皱的凝胶薄膜进行分析,研究了不伸展参数、滑移参数对聚合物凝胶增量模量的影响以及不伸展参数、滑移参数、基底材料泊松比对凝胶薄膜起皱时的临界波长和临界应力的影响．结果表明：化学势在一定范围内变化时,随着化学势的增加,增量模量、临界波长、临界应力减小;不可伸长参数越大,增量模量、临界波长及临界应力越大;滑移参数越大,增量模量、临界波长及临界应力越小．     

计算气动弹性若干研究进展

郭永怀和钱学森先生早在1946年提出了上临界马赫数的概念,即对于亚声速的二维无旋流 动,当来流速度达到下临界马赫数时开始出现声速. 稍增加来流速度,光滑无旋的亚、超声 速混合流动可以继续存在,理论上只有当来流速度达到上临界马赫数出现激波后, 光滑无旋流动才被破坏. 随后, 航空工程界先驱们为提高阻力发散马赫数,降低马赫数1附近的飞机 阻力, 为突破声障, 提出了超临界翼型设计技术,引进了后掠翼设计概念, 提出了跨声速面 积律理论,导致了20世纪军民用航空飞行器的大规模发展.随着计算机技术和计算方法的 进步,不同程度地简化流体控制方程的求解方法得到大发展.基于雷诺平均Navier-Stokes方程的计算流体力学已广泛应用于飞机性能评估、复杂流动机理分析.目前, 气动外形优化设计、气动/结构耦合干扰、气动噪声等多学科问题成为空气动力学的研究热点.该文介绍作者的团队近年来在计算气动弹性研究方面的若干进展,作为对郭永怀先生诞辰100周年的怀 念.      

Calculating the Critical Parameters Characterizing the Thermal Instability of a Viscoelastic Prism with a Stress Concentrator under Harmonic Compression

The paper proposes simplified schemes for analyzing critical thermal states of a notched rectangular viscoelastic prism under harmonic loading. The influence of the problem parameters on the critical stress amplitude is analyzed. The notch does not decrease the critical stress. Varying the problem parameters hardly affects the critical level of temperature. This level corresponds to the glass-transition temperature of an amorphous polymer     

STUDY ON AMPLIFICATION FACTOR OF FLEXURAL BUCKLING CRITICAL LOAD OF AXIAL COMPRESSION BARS1)

为了建立一般条件下轴压构件屈曲临界载荷的计算理论,首先对轴心受压构件发生屈曲时的总势能方程进行了推导,然后采用Rayleigh-Ritz法并基于势能驻值原理得到了4种不同端部约束条件下轴压构件的屈曲临界载荷,对比欧拉临界载荷,给出了临界载荷放大系数 的计算式,全面考虑了构件长细比、压缩变形、剪切变形以及截面形状系数对临界载荷的影响,推导的计算式可用于较小长细比轴压构件发生屈曲时临界载荷的计算.圆截面和双轴对称工字形截面轴压构件屈曲临界载荷的分析表明构件长细比是影响放大系数的主导因素。     

Influences of aerodynamic loads on hunting stability of high-speed railway vehicles and parameter studies

The influences of steady aerodynamic loads on hunting stability of high-speed railway vehicles were investigated in this study.A mechanism is suggested to explain the change of hunting behavior due to actions of aerodynamic loads：the aerodynamic loads can change the position of vehicle system（consequently the contact relations）,the wheel/rail normal contact forces,the gravitational restoring forces/moments and the creep forces/moments.A mathematical model for hunting stability incorporating such influences was developed.A computer program capable of incorporating the effects of aerodynamic loads based on the model was written,and the critical speeds were calculated using this program.The dependences of linear and nonlinear critical speeds on suspension parameters considering aerodynamic loads were analyzed by using the orthogonal test method,the results were also compared with the situations without aerodynamic loads.It is shown that the most dominant factors a ff ecting linear and nonlinear critical speeds are different whether the aerodynamic loads considered or not.The damping of yaw damper is the most dominant influencing factor for linear critical speeds,while the damping of lateral damper is most dominant for nonlinear ones.When the influences of aerodynamic loads are considered,the linear critical speeds decrease with the rise of cross wind velocity,whereas it is not the case for the nonlinear critical speeds.The variation trends of critical speeds with suspension parameters can be significantly changed by aerodynamic loads.Combined actions of aerodynamic loads and suspension parameters also a ff ect the critical speeds.The effects of such joint action are more obvious for nonlinear critical speeds.     

子午线轮胎驻波现象和临界速度的有限元分析

利用ABAQUS软件建立了较完整系统的轮胎驻波现象的有限元模型和分析方法,包括充气、加载、匀速滚动和加速滚动过程的有限元分析以及确定轮胎驻波临界速度的Euler描述和表征的方法.由此得到的轮胎驻波临界速度与试验值吻合较好.着重分析了载荷、充气压力对临界速度的影响,结果表明,增大充气压力会显著提高临界速度,而载荷的影响则可以忽略不计.