吸气槽道形状对扩压叶栅性能的影响

数值模拟了低速条件下吸气槽道宽度、角度变化对采用附面层吸除技术的大转角扩压叶栅气动性能影响。结果表明,附面层抽吸具有显著降低叶栅损失,改善流动,增加负荷及扩压能力等优点;吸气量相同时,槽道宽度增加可进一步改善角区流动并减小叶栅两端部损失,吸气角度变化则对吸气槽道出口压力有较大影响,为非均匀槽道宽度设计及工况变化时有效控制吸气量提供了设计自由度。     

压气机抽气级静叶吸力面抽气方式的研究

本文提出了将压气机系统性抽气与改善流道内部边界层流动相结合的方法,以提高压气机抽气级的性能.以某多级轴流压气机为例,采用数值模拟的方式讨论了压气机静叶吸力面抽气的可行性.通过不同抽气流量下3个算例计算结果的比较分析,证明了通过静叶吸力面抽气改善叶片性能和流动状况是可行的.     

MHD Double-Diffusive Carreau Fluid Flow through a Porous Medium with Variable Thermal Conductivity and Suction/Injection

In this article, we consider the effects of double diffusion on magnetohydrodynamics (MHD) Carreau fluid flow through a porous medium along a stretching sheet. Variable thermal conductivity and suction/injection parameter effects are also taken into the consideration. Similarity transformations are utilized to transform the equations governing the Carreau fluid flow model to dimensionless non-linear ordinary differential equations. Maple software is utilized for the numerical solution. These solutions are then presented through graphs. The velocity, concentration, temperature profile, skin friction coefficient, and the Nusselt and Sherwood numbers under the impact of different parameters are studied. The fluid flow is analyzed for both suction and injection cases. From the analysis carried out, it is observed that the velocity profile reduces by increasing the porosity parameter while it enhances both the temperature and concentration profile. The temperature field enhances with increasing the variable thermal conductivity and the Nusselt number exhibits opposite behavior.     

负压抽液分装的数学模型

本文介绍了负压抽液分装的数学模型 .由于考虑到所讨论液态物质的渗透性及污染性大等特点 ,采用负压抽液的原理 ,根据能量守恒理论确定抽液所需的负压 (真空度 ) ;根据克拉珀龙方程、分子流运动论的 Knudsen公式等理论 ,确定达到额定压力 (真空度 )所需的时间 (即装置的起动时间 ) .据此设计了一套含有不完全真空保护系统的分装装置 ,用这套装置进行的实验和实际操作 ,其真空度、时间数据与确定值 (计算值 )基本相符 .表明所建立的数学模型正确 ,据此设计的这套装置已成功用于液态物质的分装 .     

Thermal and magnetic characterisation of (Co0.402Fe0.201Ni0.067B0.227Si0.053Nb0.05)100–xCux bulk metallic glasses

Abstract

In this work, Co-based (Co_0.402Fe_0.201Ni_0.067B_0.227Si_0.053Nb_0.05)_100–xCu_x bulk glassy alloys (BMG) with 2 mm diameters were formed by suction-casting method and effect of Cu in this system’s thermal stability, glass forming ability and magnetic properties were also investigated. The curves of thermal analysis, obtained using differential scanning calorimetry, show that (Co_0.402Fe_0.201Ni_0.067B_0.227Si_0.053Nb_0.05)_100-xCu_x (x = 0–2) has supercooled liquid region (?T_x) of about 45 K, and reduced glass transition temperature (T_g/T_l) lies in the range from 0.663 to 0.678. The saturation magnetisation (J_s) and coercivity (H_c) for as-cast BMG were in the range of 0.46 T–0.65 T and 13 A/m, respectively.     

速度-涡量法数值求解具有表面吹吸圆柱的绕流问题

用速度-涡量法数值求解了具有表面吹吸圆柱的绕流问题.所得高阶隐式差分方程,采用以修正的不完全LU分解作预处理器的共轭梯度法(MILU-CG),高效解出.研究了雷诺数Re=100时,各种吹吸位置、吹吸强度对圆柱尾流涡旋结构和阻力、升力系数的影响规律.指出,在圆柱肩部的吸气和在圆柱尾部的吹气,可有效地抑制尾流涡旋结构在垂直来流方向上的非对称性,达到减小升力的目的.对在圆柱肩部吸气的情形,合适选择吸气强度,还可有效减小圆柱在来流方向上所受的阻力.     

一种检定辅助系统对气体分析仪检定结果的影响

对自行研制的气体分析仪检定用辅助系统进行性能评定。选择多种不同测量原理及进气方式的气体分析仪,分别利用仪器自带标定罩及自行研制的检定辅助系统对仪器进行计量检定。根据试验结果,使用该系统进行检定时,6种扩散式气体分析仪的响应时间比使用标定罩时平均增加了67.2%,而示值误差平均减小了9.2%,重复性(RSD)平均减小了19.6%;4种吸入式气体分析仪的响应时间平均减小了9.3%,示值误差平均减小了0.1%,重复性平均增加了4.7%。实验结果表明该系统对准确反映扩散式气体分析仪的计量性能有明显帮助。     

MHD free convective flow past semi-infinite vertical permeable wall

In this paper,the basic equations governing the flow and heat transfer of an incompressible viscous and electrically conducting fluid past a semi-infinite vertical permeable plate in the form of partial differential equations are reduced to a set of non-linear ordinary differential equations by applying a suitable similarity transformation.Approximate solutions of the transformed equations are obtained by employing the perturbation method for two cases,i.e.,small and large values of the suction parameter.From the numerical evaluations of the solution,it can be seen that the velocity field at any point decreases as the values of the magnetic and suction parameters increase.The effect of the magnetic parameter is to increase the thermal boundary layer.It is also found that the velocity and temperature fields decrease with the increase in the sink parameter.     

Injection/suction boundary conditions for fluid–structure interaction simulations in incompressible flow

This paper presents the analysis of injection/suction boundary conditions in the context of the fluid–structure interactions simulation of the incompressible turbulent flow. First, the equations used in the modelling of the fluid and the structure are presented, as well as the numerical methods used in the corresponding solvers. Injection/suction boundary conditions are then presented with details of different implementation alternatives. Arbitrary Lagrangian–Eulerian (ALE) approach was also implemented in order to test the injection/suction boundary conditions. Numerical tests are performed where injection/suction boundary conditions are compared to ALE simulations. These tests include forced movement of the structure and two‐degrees‐of‐freedom structure model simulations. Copyright © 2002 John Wiley & Sons, Ltd.     

Controlling the Turbulent Flow Past a Thick Airfoil by Means of Flow Enhancement in Vortex Cells Using Suction from Central Body Surfaces

On the basis of a numerical simulation of the turbulent steady-state flow past a thick airfoil with vortex cells built into the body contour, an unconventional technique for controlling flow separation by means of distributed suction from central bodies embedded in the cells is analyzed over a wide range of Reynolds numbers and suction velocities.