基于计算流体动力学软件的气旋浮流场分析

气旋浮高效油水分离技术是江汉机械研究所新开发的新一代用于油田采出液油水分离的技术。将气旋浮技术应用于油水分离,到目前为止仅江汉机械研究所正在研究,同时基于FLUENT的气旋浮流场分析,国内外尚很少见。本文首先对气旋浮高效油水分离器模型的网格划分和定义边界条件进行研究,其次,对气旋浮流场模拟结果进行分析,实践表明:基于计算流体动力学软件的气旋浮流场分析与现场实测结果比较吻合。因此,采用计算流体动力学软件技术研究气旋浮流场规律是可行的。

计算流体动力学(CFD)软件在提高发电技术经济效益研究中的应用

介绍英国Durhan 大学工程学院利用计算流体动力学(CFD)软件解决汽轮机和锅炉等发电设备改进设计中遇到的流体流量和热传递问题的情况,其中涉及采用CFD软件对汽轮机轴向和径向流量的各项特性进行模拟试验,及对锅炉烟气流量分布进行研究。

CFX仿真软件在天线设计中的应用

通过采用计算流体动力学仿真软件CFX对天线建立数学模型和仿真分析,将仿真结果数据与天线风洞实验数据进行归纳对比,发现结果能够反映出实际天线的风载状况,能为天线结构风载荷计算提供理论依据。

基于FLUENT超声振动流场的数值模拟

超声振动辅助加工技术具有高效、高精度、高可靠性、环保等优点,对提高加工质量和效率具有重要意义。为研究在超声振动辅助下工件的两种装夹方案的流场特性,首先,本文在ICEM CFD建立了二维模型并进行了网格划分。然后,将其导入计算流体动力学软件FLUENT进行模型相关参数设置,从而进行数值模拟分析,对工件不同装夹方案流场的气含率进行了详细分析及讨论。最后,对比两种不同安装方式的流场内气含率的分布及大小,从而选择更优的工件装夹方案,为超声振动辅助加工技术发展提供参考。

矿井主要通风机扩散弯道合理流型的研究

扩散弯道是矿井主要通风机装置的重要辅属装置,其性能的优劣直接影响通风机装置的运行效率。文章在应用计算流体动力学软件对不同流型的扩散弯道内部流动进行了计算分析的基础上,提出了一种新型扩散弯道结构,并进行了模型对比试验。模型试验结果表明,新设计的扩散弯道可以有效地提高静压回收能力。

PS/超临界CO_2微孔塑料挤出成型中温度对气泡成核的影响

通过计算流体动力学软件对聚苯乙烯(PS)/超临界CO2均相熔体在快速降压口模中流动状态的数值模拟,研究了口模温度对PS/CO2均相熔体气泡成核的影响。结果表明,当其它工艺条件不变、口模温度在微孔塑料发泡温度以上时,口模温度越低,越有利于微孔发泡,即形成小尺寸、大密度的泡孔。

超临界CO_2磨料射流流场影响因素的模拟分析

为了揭示超临界CO2磨料射流流场特性,利用计算流体动力学模拟软件,对超临界CO2磨料射流结构及不同因素对射流流场的影响规律进行了研究。结果表明：超临界CO2磨料射流轴向速度和冲击力随着喷距的增大,先增大后减小,即存在最优喷距,喷射压差为10~30 MPa时最优喷距为3~6倍喷嘴直径;喷射压差一定时,围压由10 MPa增至30 MPa对射流速度场及液相冲击力会造成较小的负面影响。通过超临界CO2射流破岩实验对上述2因素进行了辅助对比验证;流体温度由333K增至413K,固液两相轴向速度增大,而流体密度降低,导致液相冲击力减弱;磨料浓度由3.0%连续增至11.0%,射流固液两相轴向速度逐渐降低,降幅逐渐减小。

POLYFLOW在塑料制造机械混炼设备研究中的应用

通过数值仿真的方法，应用计算流体动力学软件POLYFLOW分析不同塑料机械混炼元件的混炼性能，来分析POLYFLOW在密炼机、注塑机、挤出机等成型设备混炼研究设计中的应用，为塑料机械塑化设备研究及提高塑化质量提供借鉴和参考。

过量空气系数和水蒸气对管式加热炉燃烧特性的影响研究

文章分别在过量空气系数α为1.05、1.10、1.15、1.20、1.25、1.30的6种工况下和氧化剂中添加的水蒸气体积分数φ_(H2)O为0、0.03、0.05、0.08、0.10、0.15的6种工况下,利用计算流体动力学(computational fluid dynamics,CFD)软件对燃气分级燃烧的管式加热炉进行了研究,分析了炉膛内的温度分布、NO密度分布以及NO排放情况。结果表明,α=1.10时,低氮燃烧效果较好;φ_(H2)

连续推钢式轧钢加热炉的数值模拟

运用流体动力学计算软件(CFD)FLUENT,对湘潭钢铁公司第二高速线材厂轧钢加热炉的三维流场进行了数值模拟,获得该轧钢加热炉内的气体流动、流速和压力的分布规律。通过与加热炉内的结构特点和实际操作状况对照分析,表明该加热炉的局部结构与操作不相适应,尤其是压力分布不适应加热炉的操作要求,造成炉内供热调节的灵活性降低,从而影响到加热质量。分析结果与加热炉的实际运行状况相符,为加热炉的进一步结构改造提供依据。

Experimental and CFD Heat Transfer Studies of Al2Oa-Water Nanofluid in a Coiled Agitated Vessel Equipped with Propeller

This paper presents the heat transfer characteristics of A1203-water nanofluid in a coiled agitated vessel with propeller agitator. The experimental study was conducted using 0.10%, 0.20% and 0.30% volume concentra tion of A1203-water nanofluids. The results showed considerable enhancement of convective heat transfer using the nanofluids. The empirical correlations developed for Nusselt number in terms of Reynolds number, Prandtl number, viscosity ratio and volume concentration fit with the experimental data within ±10%. The heat transfer characteris tics were also simulated using computational fluid dynamics using FLUENT software with the standard ke model and multiple reference frame were adopted. The computational fluid dynamics （CFD） predicted Nusselt number agrees well with the experimental value and the discrepancy is found to be less than ＋8%.

Experimental and numerical study of fence effects on dust emission into atmosphere from open storage piles

The results obtained from the research on the behaviour of fences (solid and porous) in the protection against particulated material emission to the atmosphere from open storage piles,are presented. This research was carried out through computational fluid dynamics (CFD) simulation by software Ansys CFX-10.0 in 3D,with K-epsilon being considered in the turbulence model. The efficiency of the use of porous fences as a protection against the wind flow,which interacts with an open storage pile,is shown. The use of these fences (when porosity is ε=30%) allows the reduction of wind flow velocity which interacts with the pile in comparison with the case of no use of fences (when porosity is 100%). In addition,the use of porous fences makes the velocity vortex,which is formed between the solid fence (ε=0%) and the pile,disappear,reducing the particle emission to the atmosphere by 78%.

Effects of static aeroelasticity on composite wing characteristics under different flight attitudes

Composite wing static aeroelasticity was analyzed through a loosely coupled method and the effects on composite wing characteristics under different flight attitudes were presented. Structural analysis and aerodynamic analysis were carried out through finite element method (FEM) software NASTRAN and computational fluid dynamics (CFD) software FLUENT, respectively. Correlative data transfer and mesh regenerate procedure were applied to couple the results of computational structure dynamics (CSD) and CFD. After static aeroelasticity analysis under different flight attitudes, it can be seen that lift increases with the increase of flight speed and the incremental value enlarges gradually in both rigid and elastic wings. Lift presents a linear increment relationship with the increase of attack angle when the flight speed is 0.4Ma or 0.6Ma, but nonlinear increment in elastic wing when flight speed is 0.8Ma. On the effect of aeroelasticity, the maximum of deformation increases with the increase of flight speed and attack angle, and the incremental value decreases with the increase of flight speed while uniform with different attack angles. The results provide a reference for engineering applications.

直线压缩机气体轴承的性能分析

针对直线压缩机的应用,给出了静压式小孔节流气体轴承的分析模型,运用Fluent流体数值计算软件,分析了气体轴承的几何参数和进出口压力对其承载力及质量流量的影响,并对静态和动态出口压力条件下的气体轴承特性进行了研究和比较,确定了合适的气体轴承特性参数.研究结果可用于气体轴承的设计和直线压缩机间隙密封的改善.

Velocity Profiles between Two Baffles in a Shell and Tube Heat Exchanger

Heat exchangers are extensively utilized for waste heat recovery,oil refining,chemical processing,and steam generation.In this study,velocity profiles are measured using a 3D particle image velocimetry(PIV)system between two baffles in a shell and tube heat exchanger for parallel and counter flows.The PIV and computational fluid dynamics results show the occurrence of some strong vectors near the bottom.These vectors are assumed due to the clearance between the inner tubes and the front baffle.Therefore,the major parts of the vectors are moved out through the bottom opening of the rear baffle,and other vectors produce a large circle between the two baffles.Numerical simulations are conducted to investigate the effects of the baffle on the heat exchanger using the Fluent software.The k-εturbulence model is employed to calculate the flows along the heat exchanger.

Multi-Physics CFD Simulations in Engineering

Nowadays Computational Fluid Dynamics （CFD） software is adopted as a design and analysis tool in a great number of engineering fields. We can say that single-physics CFD has been suffciently matured in the practical point of view. The main target of existing CFD software is single-phase flows such as water and air. However, many multi-physics problems exist in engineering. Most of them consist of flow and other physics, and the interactions between different physics are very important. Obviously, multi-physics phenomena are critical in devel- oping machines and processes. A multi-physics phenomenon seems to be very complex, and it is so difficult to be predicted by adding other physics to flow phenomenon. Therefore, multi-physics CFD techniques are still under research and development. This would be caused from the facts that processing speed of current computers is not fast enough for conducting a multi-physics simulation, and furthermore physical models except for flow physics have not been suitably established. Therefore, in near future, we have to develop various physical models and ef- ficient CFD techniques, in order to success multi-physics simulations in engineering. In the present paper, I will describe the present states of multi-physics CFD simulations, and then show some numerical results such as ice accretion and electro-chemical machining process of a three-dimensional compressor blade which were obtained in my laboratory. Multi-physics CFD simulations would be a key technology in near future.

Exploring the intention of Using Aspirated Cascade to Replace Tandem Cascades

In the present paper,computational fluid dynamics(CFD) simulations were executed to exploring the intent of using aspirated cascade to replace tandem cascades.Firstly,the ONERA tandem cascades were investigated,and the performance of the cascades at the design point were listed,such as diffusion factor,total pressure loss coefficient,deviation angle etc.For replacing the ONERA tandem cascades,a new cascade was designed with the codes BLADEGEN developed by the authors.The quasi 3-D calculations were carried out using the collection of programs for cascade analysis and design,MISES.The cascade was analyzed and designed by using this code.And the cascade was simulated and analyzed by commercial CFD software.It is found there is an obvious separation on the suction side.Based on the 3D CFD simulation results of the cascade without aspiration,an aspirated cascade was designed by introducing a slot on the suction side.The performance of the aspirated cascade was investigated and compared with the tandem cascades,indicated that under the same inlet condition,the total pressure loss of the single row aspirated cascade was less than that of the tandem cascades,and the outlet static pressure is higher than that of the tandem cascades.Meanwhile,the different suction slot location,suction width and suction mass flow are studied for the aspirated cascade.