大锻件内部疏松缺陷锻造压实过程FEM分析

通过分析大型铸钢锭内部疏松缺陷的物理性质和变形特征,将疏松缺陷视为多孔可压缩材料,利用多孔可压缩材料的刚塑性有限元方法,建立了Cr5型支承辊钢锻件内部疏松缺陷锻造压实过程的非线性有限元模型。通过数值模拟,研究了上下V型砧锻造工艺下,疏松体缺陷的初始孔隙率、砧宽比、接触摩擦系数和压下量等因素对其致密压实效果的影响。在Gl...     

Finite element modelling of saturated porous media at finite strains under dynamic conditions with compressible constituents

Two finite element formulations are proposed to analyse the dynamic conditions of saturated porous media at large strains with compressible solid and fluid constituents. Unlike similar works published in the literature, the proposed formulations are based on a recently proposed hyperelastic framework in which the compressibility of the solid and fluid constituents is fully taken into account when geometrical non‐linear effects are relevant on both micro‐ and macroscales. The first formulation leads to a three‐field finite element method (FEM), which is suitable for analysing high‐frequency dynamic problems, whereas the second is a simplification of the first, leading to a two‐field FEM, in which some inertial effects of the pore fluid are disregarded, hence the second formulation is suitable for studying low‐frequency problems. A fully Lagrangian approach is considered, hence all terms are expressed with reference to the material setting; the balance equations for the pore fluid are also expressed in terms of the chemical potential and the mass flux of the pore fluid in order to take the compressibility of the fluid into account. To improve the numerical response in the case of wave propagation, a discontinuous Galerkin FEM in the time domain is applied to the three‐field formulation. The results are compared with analytical and semi‐analytical solutions, highlighting the different effects of the discontinuous Galerkin method on the longitudinal waves of the first and second kind. Copyright © 2010 John Wiley & Sons, Ltd.     

最晚截止期优先带宽转让算法

基于最早截止期优先调度的实时系统，针对有新任务插入(与/或)现行任务加速但系统带宽不足的问题，提出一种最晚截止期优先(LDF)算法，用于系统在运行时选择现行任务转让带宽。采用从最晚作业截止期任务开始判断的方法，经过尽可能少的比较次数，找到合适的受压任务，平滑地完成带宽转让。算法需要的最多比较次数为2n。仿真结果表明，该算法在大多情况下只需要比较1~2次即可完成压缩任务。     

可压缩粘弹性材料Ⅰ型动态扩展裂纹尖端场

为了研究粘性效应作用下的动态扩展裂纹尖端渐近场,建立了可压缩粘弹性材料Ⅰ型动态扩展裂纹的力学模型,推导了可压缩材料Ⅰ型动态扩展裂纹的本构方程.在稳态蠕变阶段,弹性变形和粘性变形同时在裂纹尖端场中占主导地位,应力和应变具有相同的奇异量级.通过渐近分析求得了裂纹尖端应力、应变和位移分离变量形式的渐近解,并采用打靶法求得了裂纹尖端应力、应变和位移的数值结果,给出了应力、应变和位移随各种参数的变化曲线.数值计算表明,弹性可压缩变形对Ⅰ型裂纹尖端应力场影响甚微,而对应变场和位移场影响较大.裂纹尖端场主要受材料的蠕变指数n和马赫数M控制.当泊松比v=0.5时,可以退化为不可压缩粘弹性材料Ⅰ型动态扩展裂纹.     

饱和土中流体对压缩波传播特性影响

为了进一步分析流体性质对饱和土中压缩波传播的影响,基于Biot两相介质波动理论,推导了压缩波平面波动解,并得到了孔隙流体自由流动和流体无渗流时的压缩波速度公式.通过数值算例分析了水饱和、准饱和及气饱和三种饱和情况下土中压缩波的传播及衰减特性.结果表明,在水饱和至准饱和土中,两种压缩波的速度和弥散性均随含气量的增加而降低,衰减则随含气量的增加而增加.气饱和土中,P1波速度比水饱和时显著降低且基本无弥散和衰减;P2波速度比水饱和时有很大提高,同时弥散和衰减加强,且特征频率向高频漂移.完全水饱和时P1波主要在流体中传播,含气量超过一定值(1%)时主要受土骨架中控制,P2波则刚好与此相反.     

高阶间断Galerkin方法求解三维欧拉方程的研究

在三维非结构网格上,对高阶间断Galerkin方法求解定常三维欧拉方程进行研究.文中使用Roe格式通量函数计算网格单元边界上的数值通量;时间方向采用显式Runge-Kutta方法推进;并引入激波探测器和斜率限制器技术,成功地抑制流场解在间断处的数值振荡.对M6机翼跨音速无粘流场进行数值模拟,结果表明:计算结果和实验值吻...     

The time dependent strain potential function for a polymeric glass

Torsion and normal force measurements were made during single step stress relaxation experiments on a polymeric glass (PMMA). Isochronal data were analysed using an approach adapted from that developed by Penn and Kearsley¹ (for incompressible elastic materials) to determine the derivatives $\text{?W}\text{?I}{}_1$, and $\text{?W}\text{?I}{}_2$ of the time dependent strain potential function. $\text{?W}\text{?I}{}_1$ and $\text{?W}\text{?I}{}_2$ are determined from existing solution to the torsion of an incompressible cylinder. A special solution to the torsion of a compressible cylinder is presented and it is shown that the values of $\text{?W}\text{?I}{}_1$ and $\text{?W}\text{?I}{}_2$ obtained using this solution to analyse the data do not differ greatly from those obtained using the incompressible solution. It is found from both solutions that $\text{?W}\text{?I}{}_1$ is negative and increases towards zero with increasing time and deformation while $\text{?W}\text{?I}{}_2$ is positive, greater in magnitude than $\text{?W}\text{?I}{}_1$ and decreases towards zero with increasing time and deformation. These results were unexpected and a full understanding of their meaning has yet to be reached.     

Modeling Abrasion Forces in a Pneumatically Powered Grinding Tool Using Compressible Large Eddy Simulation

This paper describes the design of a new kind of miniature abrading sphere, which is magnetically mounted inside a spherical gap and set in rotation pneumatically with air. Large eddy simulation is performed in conjunction with the compressible Smagorinsky model. Minimal temperature variation allows for the assumption of adiabatic walls. Fluid-solid interaction is modeled using the law of the wall for compressible turbulent flow. A parametric study is done to determine optimal geometric layout while taking physical restrictions into account. The resulting optimal configuration is then examined in detail in order to determine demands to be met by the computerized control of the magnetic bearing as well as to quantify the force available to the abrasion process. Finally, a mathematical relation is given that determines available abrasion force depending on standard volumetric flow rate and rotation frequency. The findings presented here provide a basis for further development of smaller versions of the tool.     

Effect of Duct Geometry on Shock Wave Discharge

This paper describes computational work to understand the unsteady flow-field of a shock wave discharging froman exit of a duct and impinging upon a flat plate.A flat plate is located downstream, and normal to the axis of theduct.The distance between the exit of the duct and fiat plate is changed.In the present study,two different ductgeometries(i.e.,square and cross section)are simulated to investigate the effect of duct geometry on theun-steady flows of a shock wave.In computation,the total variation diminishing(TVD)scheme is employed tosolve three-dimensional,unsteady,compressible,Euler equations.Computations are performed over the range ofshock Mach number from 1.05 to 1.75.Computational results can predict the three-dimensional dynamic behav-iour of the shock wave impinging upon the flat plate.The results obtained show that the pressure increase gener-ated on the plate by the shock impingement depends on the duct geometry and the distance between the duct exitand plate,as well as the shock Mach number.It is also found that for the duct with cross-section,the unsteadyloads acting on the flat plate are less,compared with the square duct.     

Numerical Simulation on Supersonic Flow in High-Velocity Oxy-Fuel Thermal Spray Gun

This paper analyzes the behaviour of coating particles as well as the gas flow both inside and outside of the High-Velocity Oxy-Fuel (HVOF) thermal spray gun by using a quasi-one-dimensional analysis and a numerical simulation. The HVOF gun in the present analysis is an axially symmetric convergent-divergent nozzle with the design Mach number of 2.0. From the present analysis, the distributions of velocity and temperature of the coating particles flying inside and outside of the HVOF gun are predicted. The velocity and temperature of the coating particles at the exit of the gun calculated by the present method agree well with the previous experimental results. Therefore, the present method of calculation is considered to be useful for predicting the HVOF gas and particle flows.