Discrete particle simulation of particle–fluid flow model formulations and their applicability
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第 54 卷第 4 期2023 年 4 月中南大学学报(自然科学版)Journal of Central South University (Science and Technology)V ol.54 No.4Apr. 2023离散颗粒抑制热喷流红外辐射的大涡模拟胡峰1,孙文静1, 2,张靖周1,单勇1(1. 南京航空航天大学 能源与动力学院,江苏 南京,210016;2. 中国航天科工飞航技术研究院 北京动力机械研究所,北京,100074)摘要:为了探究气溶胶离散颗粒对飞行器排气喷管热喷流3~5 μm 波段的红外辐射的抑制效果,设计地面状态下气溶胶颗粒投射的仿真环境,采用大涡模拟和颗粒离散相模型对含气溶胶颗粒的飞行器排气喷管尾部气固两相剪切流进行数值模拟研究,系统地分析颗粒的质量流量、粒径和喷射速度对离散颗粒空间分布形态以及热喷流红外辐射抑制的影响规律。
研究结果表明:颗粒的质量流量和粒径对于红外抑制效率的影响较为明显,增加颗粒质量流量对颗粒的空间分布形态影响较小,但能够显著提升红外抑制效率;当颗粒粒径大于1.0 μm 时,颗粒空间分布均匀,红外抑制效率最高;颗粒的喷射速度对于颗粒的空间分布以及红外抑制效率的影响较小。
关键词:红外抑制;高速剪切流;大涡模拟;气溶胶颗粒分布;气固相互作用中图分类号:V231.1 文献标志码:A 开放科学(资源服务)标识码(OSID)文章编号:1672-7207(2023)04-1576-16Large eddy simulation of discrete particles suppressing infraredradiation from thermal jetsHU Feng 1, SUN Wenjing 1, 2, ZHANG Jingzhou 1, SHAN Yong 1(1. College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2. Beijing Power Machinery Institute, China Aerospace Institute of Science and Technology, Beijing 100074, China)Abstract: To investigate the effect of aerosol discrete particles on the infrared radiation suppression in the 3~5 μm band of thermal jets of aircraft exhaust nozzles, the simulation environment of aerosol particle projection under ground conditions was designed. The large eddy simulation(LES) and particle discrete phase model(DPM) were used to numerically simulate the gas-solid two-phase shear flow at the tail of the aircraft exhaust nozzle containing aerosol particles, and the effect law of particle mass flow, size and jet speed on the spatial distribution of discreteparticles and the suppression of infrared radiation of thermal jets was systematically analyzed. The results show收稿日期: 2022 −05 −14; 修回日期: 2022 −07 −23基金项目(Foundation item):中国博士后科学基金特别资助(站前)项目(2020TQ0143);江苏省自然科学基金青年基金资助项目(BK20200448) (Project(2020TQ0143) supported by the Postdoctoral Science Foundation of China; Project(BK20200448) supported by the Youth Fund of Jiangsu Natural Science Foundation)通信作者:孙文静,博士,讲师,从事气固两相湍流、湍流燃烧、流动强化传热研究;E-mail :**************.cnDOI: 10.11817/j.issn.1672-7207.2023.04.033引用格式: 胡峰, 孙文静, 张靖周, 等. 离散颗粒抑制热喷流红外辐射的大涡模拟[J]. 中南大学学报(自然科学版), 2023, 54(4): 1576−1591.Citation: HU Feng, SUN Wenjing, ZHANG Jingzhou, et al. Large eddy simulation of discrete particles suppressing infrared radiation from thermal jets[J]. Journal of Central South University(Science and Technology), 2023, 54(4): 1576−1591.第 4 期胡峰,等:离散颗粒抑制热喷流红外辐射的大涡模拟that the effect of particle mass flow and size on infrared radiation suppression rate is obvious. With the increase of particle mass flow, its effect on the spatial distribution of particles is small, but the infrared suppression efficiency is significantly improved. When the particle diameter is 1.0 μm, the particle space distribution is uniform and the highest infrared suppression rate is achieved. However, the particle injection speed has less effect on the spatial distribution of particles and infrared radiation suppression efficiency.Key words: infrared suppressing; high-speed shear flow; large eddy simulation; aerosol particle distribution; gas-solid interactions气溶胶红外隐身技术是一种主动型应急红外对抗技术,该技术利用附加的机载引气装置,将细微颗粒喷射在发动机热喷流周围形成气溶胶云,借此对排气喷管热内腔和热喷流的强红外辐射进行遮蔽和散射。
考虑组构演化的散粒体各向异性力学特性数值分析与本构模拟摘要:散粒体材料是一种具有重要应用价值的材料,其力学特性与材料内部结构的组构演化密切相关。
本文从组构演化的角度出发,研究了散粒体材料的各向异性力学特性,采用数值分析和本构模拟的方法对其力学行为进行了研究。
首先介绍了散粒体力学特性的研究现状和存在的问题,然后重点阐述了组构演化与材料力学特性之间的关系。
接着,通过建立数学模型和仿真模拟,探究了散粒体材料的各向异性力学特性变化规律和组构演化的影响。
最后,对本文的研究结果和对散粒体材料力学性质的认识加以分析和总结,提出了未来研究的方向和展望。
关键词:散粒体;组构演化;力学特性;数值分析;本构模拟Abstract: Granular material is a kind of material with important application value. Its mechanical properties are closely related to the structural evolution of the material. Starting from the perspective of structural evolution, this paper studies the anisotropic mechanical properties of granular materials, and uses numerical analysis and constitutive simulation tostudy their mechanical behavior. First, the research status and existing problems of granular material mechanics are introduced, and then the relationship between structural evolution and material mechanicalproperties is elaborated. Then, through the establishment of mathematical models and simulation, the change law of anisotropic mechanical properties of granular materials and the influence of structural evolution are explored. Finally, the research results of this paper and the understanding of the mechanical properties of granular materials are analyzed and summarized, and the future research directions and prospects are put forward.Keywords: granular material; structural evolution; mechanical properties; numerical analysis;constitutive simulationGranular materials are materials made up of small, discrete particles, such as sand, gravel, or powders. They are widely used in many fields, including civil engineering, chemical engineering, and geotechnical engineering, among others. Understanding the mechanical properties of granular materials is a fundamental problem in many applications, such as the design of foundations, embankments, and tunnels.The mechanical properties of granular materials are strongly influenced by their microstructure, which changes continuously during deformation. The structure of a granular material is defined by the packingarrangement of its particles, which depends on the particle size, shape, and the forces acting between them. When a granular material is subjected toexternal forces, such as compression or shear, its particles rearrange and its structure evolves.The structural evolution of granular materials has a significant impact on their mechanical behavior, such as their deformation, strength, and stiffness. For example, under compression, a granular material undergoes densification, accompanied by a decrease in its porosity and an increase in its stiffness. However, this process is not a simple isotropic compaction, but rather involves significant anisotropy in the packing structure, particle orientation, and stress transmission. Similarly, under shear, a granular material experiences strain localization, which isalso influenced by the anisotropic particle arrangements and the development of shear bands.To understand the mechanical properties of granular materials and their structural evolution, numerical analysis and constitutive simulation are widely used. Numerical models, such as the discrete element method (DEM), are used to simulate the behavior of granular materials at the particle scale. Constitutive models, such as the Mohr-Coulomb model and the critical statemodel, are used to describe the macroscopic behaviorof granular materials in terms of their stress-strain relationships and failure criteria.Through numerical analysis and constitutive simulation, researchers have made significant progress in understanding the mechanical properties of granular materials and their structural evolution. For example, the anisotropic mechanical properties of granular materials have been characterized and quantified, and the impact of the packing structure and particle interactions on these properties has been explored. Moreover, the effect of structural evolution on the mechanical behavior of granular materials has been investigated, and new constitutive models that takeinto account this effect have been proposed.In summary, the mechanical properties of granular materials are strongly influenced by their microstructure, which evolves continuously during deformation. Numerical analysis and constitutive simulation are powerful tools for studying thebehavior of granular materials and their structural evolution. The research in this field has important implications for many applications, and future studies should focus on developing more accurate and robustmodels for predicting the mechanical behavior of granular materials in different conditionsContinued:One important application of granular materials is geotechnical engineering, where soil and rock are the primary materials utilized. In order to prevent landslides, control erosion, design foundations and tunnels, and excavate deep underground facilities, an accurate prediction of the mechanical behavior of granular materials is essential. Therefore, researchers in this field need to systematically investigate the influence of various factors on the mechanical behavior of granular materials, such as strain rate, temperature, moisture content, particle size distribution, and confining pressure.Another area where granular materials play an important role is in the manufacturing industry, where powders and granules are used to produce a wide range of products, such as pharmaceuticals, chemicals, ceramics, and food products. In order to optimize the manufacturing process and ensure the quality of the end product, it is crucial to understand the mechanisms underlying the deformation and failure of granular materials during processing. Therefore,researchers in this field need to develop new methods for characterizing the microstructure of granular materials, such as X-ray tomography and micromechanical testing, and integrate these methods into numerical simulations to predict the mechanical behavior of granular materials in different processing conditions.In addition, granular materials are also used in the energy industry, where they play a critical role inoil and gas extraction and storage, carbon capture and storage, and nuclear waste disposal. In these applications, the mechanical behavior of granular materials under extreme conditions is of great significance, such as high pressure, high temperature, high radiation dose, and aggressive chemical environment. Therefore, researchers in this field need to develop new testing techniques and modeling approaches that can capture the effects of these extreme conditions on the structural evolution and mechanical behavior of granular materials.Finally, granular materials are also widely used in natural phenomena, such as landslides, avalanches, and earthquakes. In order to understand and predict the behavior of these phenomena, it is essential to develop new experimental techniques and numericalmodels that can accurately describe the deformation and failure of granular materials under dynamic loading conditions. Therefore, researchers in this field need to conduct experiments with advanced visualization techniques and data acquisition methods and develop new computational methods that can capture the complex interactions between particles and the surrounding environment.In conclusion, the mechanical behavior of granular materials is governed by the microstructure of the material, which continuously evolves during deformation. The research in this field has important implications for various applications, including geotechnical engineering, manufacturing, energy, and natural hazards. Future studies should focus on developing more accurate and robust models for predicting the mechanical behavior of granular materials under a wide range of conditions and investigating the influence of various factors on the microstructure and mechanical behavior of granular materialsIn addition to improving our understanding of the mechanical behavior of granular materials, future research should also focus on developing new techniques for characterizing their microstructure andproperties. Accurate quantification of grain size distribution, shape, and orientation can provide valuable insights into the behavior of granular materials and aid in the development of more realistic models. Techniques such as X-ray tomography, confocal microscopy, and laser scanning can provide three-dimensional information on the microstructure of granular materials, while acoustic and ultrasonic imaging can be used to infer properties such as density, porosity, and elastic moduli.Another important area of research is the study of granular materials under extreme conditions, such as high pressures, temperatures, and strain rates. Such conditions are encountered in many industrial processes, such as metal forging and welding, and in natural disasters, such as earthquakes and landslides. Understanding how granular materials behave under such conditions is essential for the development of safe and efficient manufacturing processes and for the prediction and mitigation of natural hazards.Finally, much can be gained by investigating the role of environmental factors on the mechanical behavior of granular materials. Factors such as moisture, temperature, and chemical composition can alter the mechanical properties of granular materials and theirresponse to external stimuli. For example, the presence of water can cause soils to become more plastic and increase their shear strength, while exposure to certain chemicals can lead to changes in bonding and surface tension of granular particles. Research into the effects of environmental factors on granular materials can provide valuable insights into their behavior in natural and industrial settings.In conclusion, granular materials are ubiquitous in nature and industry, and the study of their mechanical behavior offers many important insights into their properties and response to external stimuli. While our understanding of granular materials has advanced significantly in recent years, much remains to be learned about their microstructure and mechanical properties, particularly under extreme conditions and in the presence of environmental factors. Continued research in this field will have importantimplications for a wide range of applications, including geotechnical engineering, manufacturing, energy, and natural hazardsIn conclusion, granular materials are ubiquitous in nature and technology, and their macroscopic behavior is strongly influenced by their microstructure and response to external stimuli. Research in this fieldhas advanced in recent years, but there is still much to be learned about their mechanical properties and behavior under extreme conditions and in the presence of environmental factors. Further research in thisarea will have important implications for various applications, particularly in geotechnical engineering, manufacturing, energy, and natural hazards。
专利名称:PARTICLE SIMULATION SYSTEM 发明人:MATSUZAWA KAZUYA申请号:JP25489289申请日:19890929公开号:JPH03116385A公开日:19910517专利内容由知识产权出版社提供摘要:PURPOSE:To attain analysis with physically high accuracy while sufficiently utilizing the feature of particle simulation by arranging super-particles in an analysis area where particle simulation is executed, and afterwards, handling the transportation of particles, which are remained in the area without being distributed to the super- particles, according to the transient analysis method of fluid simulation. CONSTITUTION:When the transportation of the plural particles is analyzed, the super- particles are arranged in the analysis area, to which the particle simulation is executed, and afterwards, the transportation of the particles, which are remained in the area without being distributed to the super-particles, is handled according to the transient analysis method of the fluid simulation. When the analysis is executed by using a window method, the transportation for the small number of the particles, which are remained in a window without being distributed to the super-particles, and the particles out of the window is handled by the transient analysis method of the fluid simulation and when the supplying source of the particles such as an ohmic electrode, etc., is included in the analysis area, the transient analysis is executed under a contour condition that the number of the particles is fixed in a contour with the supplying source. Thus, while effectively utilizing the feature of the particle simulation, the simulation can be executed with physically high accuracy.申请人:TOSHIBA CORP 更多信息请下载全文后查看。
COREX熔化气化炉风口回旋区CFD+DEM数值模拟孙俊杰;周恒;罗志国;邹宗树【摘要】COREX熔化气化炉风口回旋区是炉况顺行的基础,在冶炼过程中起着十分重要的作用,为了描述其形状和大小,建立了CFD+ DEM(Computational Fluid Dynamics and Discrete Element Method)耦合模型,对回旋区形成过程及大小进行了颗粒尺度的分析.得到床层高度为0.4m,气体速度11.74 m/s的条件下回旋区颗粒空隙度分布,当吹气时间为0.13s时,气体人口附近有颗粒被吹开,随着时间的推进,气体动能吹开的颗粒增多,0.19~0.21 s时,形成的回旋区开始稳定.对入口处不同气体速度条件下回旋区及其附近颗粒速度进行了计算模拟.模拟结果显示,风口附近颗粒在做回旋运动,并且随着入口气体速度的增大,吹开的颗粒增多,回旋区空腔增大,当入口气体速度为11.74 m/s和16.83 m/s时形成的回旋区较稳定,当入口气体速度大于21.90 m/s时形成的回旋区不太稳定.【期刊名称】《东北大学学报(自然科学版)》【年(卷),期】2013(034)006【总页数】5页(P824-827,844)【关键词】熔化气化炉;风口回旋区;DEM;CFD;回旋区颗粒速度【作者】孙俊杰;周恒;罗志国;邹宗树【作者单位】东北大学材料与冶金学院,辽宁沈阳110819;东北大学材料与冶金学院,辽宁沈阳110819;东北大学材料与冶金学院,辽宁沈阳110819;东北大学材料与冶金学院,辽宁沈阳110819【正文语种】中文【中图分类】TF557风口回旋区的形状和大小决定了高炉及COREX熔化气化炉中煤气的一次分布,反映了焦炭的燃烧状态,是炉况顺行的基础,在冶炼过程中起着十分重要的作用. COREX熔化气化炉风口回旋区的物理化学过程与高炉具有相似之处.关于COREX 熔化气化炉风口回旋区的研究较少,研究COREX时可以借鉴高炉风口回旋区的一些研究成果.Sarkar[1]把焦炭和球团矿简化为连续相,用双欧拉方法对高炉回旋区建模计算,此种方法未能准确描述颗粒的运动情况.Natsui[2]利用DEM,对高炉回旋区区域模拟计算,得到料层高度和风口间隔对死料柱高度的影响,此模型得到较精确的三维高炉回旋区部分参数,因其提前设置了回旋区的边界,但模型没有考虑气体流场对离散颗粒的影响,未实现CFD和DEM的耦合.罗志国等[3-4]建立了熔化气化炉物理模型,通过跟踪示踪颗粒的运动信息,得到观察面板处风口回旋区域的颗粒速度场,利用图像处理手段和分形理论,提供了一种确定熔化气化炉回旋区大小的方法.CFD+DEM耦合模型能够模拟工业中大部分同时存在颗粒和流体的流程,此种方法的最大优势是能够得到详细的单个颗粒信息(轨迹、相间力),而这些正好是阐明复杂流体行为控制机理的关键信息[5].前人使用CFD+DEM方法对回旋区的研究都是针对高炉,未见有人用这种方法对COREX熔化气化炉的回旋区进行模拟计算.文献[6]建立了CFD+DEM耦合模型对高炉复杂的瞬变现象做了初步的模拟,分析了鼓风气体流量对回旋区处颗粒速度和所受力的影响(其计算相间力时仅考虑了曳力).回旋区内存在鼓风气体和焦炭颗粒,气体和焦炭颗粒的运动参数都会对回旋区形状和大小产生影响.本文以商业软件FLUENT为平台,用CFD+DEM方法对风口回旋区进行研究.利用UDF(user defined function)将DEM程序编译进FLUENT,从而实现了DEM与CFD的耦合,对回旋区内颗粒的运动分布规律模拟研究.1 数学模型描述1.1 颗粒相控制方程COREX熔化气化炉回旋区附近焦炭视为离散相,采用DEM模型计算,颗粒的平动和转动用牛顿第二运动定律描述[7-9]如下.(1)(2)式中:mi,Ii,vi和ωi分别代表颗粒i的质量(kg),转动惯量(kg·m2),平动速度(m/s)和转动速度(r/s);fg代表i颗粒的重力(N);fc,ij,fd,ij和Ti,j分别为颗粒i和j间的接触力(N),阻尼力(N)以及转矩(N·m);t为时间(s).当颗粒i与ki个颗粒同时接触时,其所受颗粒间的作用力和力矩矢量需要叠加在一起,fp-f,i是颗粒和流体的相间力,是颗粒相和流体相互作用力的合力,包括曳力、压力梯度力、虚假质量力、Basset加速度力、Magnus力、Saffman升力、滑移-剪切升力[5,10].1.2 气相控制方程风口处的鼓风气体视为连续相,采用类似于传统双流体模型方法进行描述.气相控制方程为计算单元上局部平均变量的质量和动量守恒形式,其表达式如下. +·(ρfεu)=0,(3)+·(ρfεuu)= -p+·(ετ)+ρfεg-fp-f,i.(4)式中:ρf,u分别代表气体密度(kg/m3),气体速度(m/s);τ为气体的应力张量(N/m2);ε为颗粒孔隙度;p为气体压力(Pa).1.3 颗粒和气相的耦合在整个模型计算中,DEM用来计算每个颗粒的运动,气相流动的模拟在远大于颗粒尺寸的计算网格中进行,利用FLUENT提供的用户自定义函数UDF实现颗粒相与气相的耦合.具体耦合步骤如下.1) 使用DEM将颗粒堆积到模拟所需高度,用FLUENT初始化气体流场;2) 通过DEFINE_ON_DEMOND(name)将计算的颗粒初始结构调入,同时根据式(5)和图1计算网格空隙度:(5)式中:Vi表示颗粒i的体积;V表示单元格体积.图1 气相网格空隙度计算方法Fig.1 Calculation method of grid porosity3) 根据DEM得到的颗粒运动速度、位置和流体速度场计算出每个颗粒所受相间力,通过DEFINE_ADJUST(name,d)更新颗粒所受的力、颗粒速度、位置、转矩等的变化,完成DEM的颗粒计算;4) 通过DEFINE_PROPERTY(name,c,t)将密度ρf,黏度μ变为与空隙度ε有关的ε·ρf和ε·μ来实现对密度和黏度的修正;5) 将每个流体单元内所有颗粒所受相间力求和,得到此单元内的颗粒与流体相间力,将该相间力加到气相动量方程的源项中,进行流体运动计算,得出每个计算单元的速度值,根据网格单元中流体速度、颗粒速度更新流体与颗粒的相间力;6) 将每个颗粒所受相间力加入到DEM中就可以计算下一个时间步长内颗粒运动信息,如此迭代计算就可实现颗粒相和气相的持续耦合计算,计算流程如图2所示.图2 颗粒和气相耦合计算流程图Fig.2 Coupled calculation flow chart forparticle phase and gas phase2 模型建立及参数选择在实际物理实验中颗粒粒径0.002 5 m左右,床层高度0.4 m,一个风口所在区域的颗粒数已达到600 000个,受计算条件的限制,本模型简化为一个0.23m×0.005 m×1.0 m的矩形床,右侧墙壁上有一个0.025 m(5个颗粒厚度)×0.005 m的气体入口,入口中心距底部0.11 m.模型在x方向的网格尺寸为0.023 m,y方向的网格尺寸为0.005 m,z方向的网格尺寸为0.005 m.边界条件设置入口为速度入口,出口为outflow,壁面为无滑移边界条件.颗粒相模型中,颗粒-墙之间的碰撞与颗粒-颗粒之间的碰撞一致,只是墙不会产生位移.模拟参数如表1所示.表1 模拟参数Table 1 Simulation parameters颗粒相流体相颗粒形状球形μ1.8×10-5Pa·s颗粒密度950kg/m3ρf1.205kg/m3弹性模量216kPa11.74m/s 摩擦因数0.3入口速度16.83m/s阻尼因数0.1221.90m/s3 结果与分析3.1 回旋区的形成过程图3为气体喷吹倾角为4°,颗粒直径为0.005 m,床层填充高度为0.4 m,颗粒个数为5 700,气体速度为11.74 m/s条件下不同时刻回旋区颗粒运动及空隙度. 图3 床高0.4 m,气体速度11.74 m/s时回旋区形成过程Fig.3 The formation of raceway with bed height of 0.4 m and gas blowing velocity of 11.74m/s(a)—0.13 s时颗粒分布和空隙度; (b)—0.19 s时颗粒分布和空隙度; (c)—0.21 s时颗粒分布和空隙度.从图上可以看出,0.13 s时,气体入口附近开始有颗粒被吹开,空隙度变大,对比两张图可以看出空隙度变大的范围比颗粒吹开的范围大,这是因为空隙度的计算是以网格为基础,没有颗粒的位置及其附近同属于一个单元网格,导致没有颗粒的位置空隙度不等于1,且其附近位置的空隙度变大.随着时间的推进,气体动能吹开的颗粒增多.0.19~0.21 s时,形成的回旋区开始稳定.3.2 回旋区颗粒速度图4为气体喷吹倾角为4°,颗粒直径为0.005 m,床层填充高度为0.4 m,颗粒个数为5 700,回旋区基本稳定条件下不同气体速度时回旋区及其附近颗粒位置及速度.图4 不同气体速度下回旋区及附近颗粒位置及速度值Fig.4 Particle position and velocity in and around raceway with different gas blowing velocity(a)—11.74 m/s; (b)—16.83 m/s; (c)—21.90 m/s.从图中可以看出,在重力、颗粒间摩擦力和气体动能的共同作用下,风口附近颗粒在做回旋运动,且随着入口气体速度的增大,吹开的颗粒增多,回旋区空腔增大;回旋区内部无颗粒,外围颗粒速度基本为0;当入口气体速度为11.74 m/s和16.83 m/s时形成的回旋区较稳定,当入口气体速度大于21.90 m/s时,床层中的大部分颗粒有向上的速度,形成的回旋区不太稳定,有形成流化床的趋势.4 结论本文通过CFD+DEM耦合方法对风口回旋区的形成进行模拟研究,利用UDF将DEM程序编译进FLUENT,从而实现了DEM与CFD的耦合.对回旋区内颗粒的分布运动规律进行了模拟,得到床层高度为0.4 m,气体速度11.74 m/s的条件下回旋区颗粒的空隙度分布.0.13 s时,气体入口附近开始有颗粒被吹开,随着时间的推进,气体动能吹开的颗粒增多,0.19~0.21 s时,形成的回旋区开始稳定;对入口处不同气体速度条件下回旋区及其附近颗粒速度进行了计算模拟.结果显示,在重力、颗粒间摩擦力和相间力的共同作用下,风口附近颗粒在做回旋运动,且随着入口气体速度的增大,吹开的颗粒增多,回旋区空腔增大;当入口气体速度为11.74 m/s和16.83 m/s时形成的回旋区较稳定,当入口气体速度大于21.90m/s时形成的回旋区不太稳定.参考文献:[1] Sarkar S,Gupta G S,Kitamura S.Prediction of raceway shape and size[J].ISIJ International,2007,47(12):1738-1744.[2] Natsui S, Ueda S, Oikawa M, et al.Optimization of physical parameters of discrete element method for blast furnace and its application to the analysis on solid motion around raceway[J].ISIJ International,2009,49(9):1308-1315.[3] 罗志国,孙俊杰,狄瞻霞,等.COREX熔化气化炉风口回旋区内表面积研究[J].东北大学学报:自然科学版,2012,33(6):840-843.(Luo Zhi-guo,Sun Jun-jie,Di Zhan-xia,et al.Study on surface area of raceway in COREX melter-gasifier[J].Journal of Northeastern University:Natural Science,2012,33(6):840-843.)[4] Luo Z G, Di Z X, Zou Z S, et al.Application of fractal theory on raceway boundary in COREX melter-gasifier model[J].Ironmaking and Steelmaking,2011,38(6):417-421.[5] Zhou Z Y,Kuang S B,Chu K W,et al.Discrete particle simulation of particle-fluid flow:model formulations and their applicability[J].Journal of Fluid Mechanics,2010,661:482-510.[6] Zhou Z Y,Zhu H P,Yu A B,et al.Numerical investigation of the transient multiphase flow in an ironmaking blast furnace[J].ISIJInternational,2010,50(4):515-523.[7] 宋伟刚,陈洪亮,李勤良,等.散状物料转载冲击载荷的DEM仿真[J].东北大学学报:自然科学版,2011,32(11):1631-1634.(Song Wei-gang,Chen Hong-liang,Li Qin-liang,et al.Simulation of handling impact load of bulk material by DEM method[J].Journal of Northeastern University:Natural Science,2011,32(11):1631-1634.) [8] Luo Z G,Li H F.Mathematical simulation of burden distribution in COREX melter gasifier by discrete element method[J].Journal of Iron and Steel Research International,2012,19(9):36-42.[9] Wang X,You C F.Evaluation of drag force on a nonuniform particle distribution with a meshless method[J].Particuology,2011,9(3):288-297.[10]Zhu H P,Zhou Z Y,Yang R Y,et al.Discrete particle simulation of particulate systems:theoretical developments[J].Chemical Engineering Science,2007,62(13):3378-3396.。
专利名称:Discrete particle electrolyzer cathode andmethod of making same发明人:Stuart I. Smedley,Martin De TezanosPinto,Stephen R. des Jardins,Donald JamesNovkov,Ronald Gulino申请号:US10424539申请日:20030424公开号:US20040168922A1公开日:20040902专利内容由知识产权出版社提供专利附图:摘要:A system for producing metal particles using a discrete particle electrolyzercathode, a discrete particle electrolyzer cathode, and methods for manufacturing the cathode. The cathode has a plurality of active zones on a surface thereof at least partially immersed in a reaction solution. The active zones are spaced from one another by between about 0.1 mm and about 10 mm, and each has a surface area no less than about 0.02 square mm. The cathode is spaced from an anode also at least partially immersed in the reaction solution. A voltage potential is applied between the anode and cathode. Metal particles form on the active zones of the cathode. The particles may be dislodged from the cathode after they have achieved a desired size. The geometry and composition of the active zones are specified to promote the growth of high quality particles suitable for use in metal/air fuel cells. Cathodes may be formed from bundled wire, machined metal, chemical etching, or chemical vapor deposition techniques.申请人:SMEDLEY STUART I.,PINTO MARTIN DE TEZANOS,JARDINS STEPHEN R. DES,NOVKOV DONALD JAMES,GULINO RONALD更多信息请下载全文后查看。
J.Fluid Mech.(2010),vol.661,pp.482–510.c Cambridge University Press2010doi:10.1017/S002211201000306XDiscrete particle simulation of particle–fluid flow:model formulations and their applicability Z.Y.Z H O U,S.B.K U A N G,K.W.C H UA N D A.B.Y U†Laboratory for Simulation and Modelling of Particulate Systems,School of Materials Science and Engineering,The University of New South Wales,Sydney NSW2052,Australia(Received3September2009;revised28May2010;accepted28May2010;first published online25August2010)The approach of combining computationalfluid dynamics(CFD)for continuumfluid and the discrete element method(DEM)for discrete particles has been increasingly used to study the fundamentals of coupled particle–fluidflows.Different CFD–DEM models have been used.However,the origin and the applicability of these models are not clearly understood.In this paper,the origin of different model formulations is discussedfirst.It shows that,in connection with the continuum approach,three sets of formulations exist in the CFD–DEM approach:an original format set I, and subsequent derivations of set II and set III,respectively,corresponding to the so-called model A and model B in the literature.A comparison and the applicability of the three models are assessed theoretically and then verified from the study of three representative particle–fluidflow systems:fluidization,pneumatic conveying and hydrocyclones.It is demonstrated that sets I and II are essentially the same,with small differences resulting from different mathematical or numerical treatments of a few terms in the original equation.Set III is however a simplified version of set I. The testing cases show that all the three models are applicable to gasfluidization and,to a large extent,pneumatic conveying.However,the application of set III is conditional,as demonstrated in the case of hydrocyclones.Strictly speaking,set III is only valid whenfluidflow is steady and uniform.Set II and,in particular,set I,which is somehow forgotten in the literature,are recommended for the future CFD–DEM modelling of complex particle–fluidflow.Key words:fluidized beds,granular media,particle–fluidflows1.IntroductionCoupled particle–fluidflow can be observed in almost all types of particulate processes which are widely used in industry.Understanding the fundamentals governing theflow and formulating suitable governing equations and constitutive relationships are of paramount importance to the formulation of strategies for process development and control.This necessitates a multi-scale approach to understanding the phenomena at different time and length scales(see e.g.Villermaux1996;Xu& Yu1997;Li2000;Tsuji2007;Zhu et al.2007).The existing approaches to modelling particleflow can generally be classified into two categories:the continuum approach at a macroscopic level and the discrete approach at a microscopic level.In the †Email address for correspondence:a.yu@.auDiscrete particle simulation of particle–fluidflow483 continuum approach,the macroscopic behaviour is described by balance equations, e.g.mass and momentum,closed with constitutive relations together with initial and boundary conditions(see e.g.Anderson&Jackson1967;Ishii1975;Gidaspow 1994;Enwald,Peirano&Almstedt1996).The discrete approach is based on the analysis of the motion of individual particles,i.e.typically by means of the discrete element method(DEM)(Cundall&Strack1979).The method considers afinite number of discrete particles interacting by means of contact and non-contact forces, and every particle in a considered system is described by Newton’s equations of motion.On the other hand,fluidflow can be modelled at different time and length scales from discrete(e.g.molecular dynamic simulation,lattice Boltzman,pseudo-particle method)to continuum(direct numerical simulation,large-eddy simulation and other conventional computationalfluid dynamics(CFD)techniques).Different combinations of models for the particle phase andfluid phase can be made,and their relative merits in describing particle–fluidflow have been discussed(see e.g.Yu2005; Zhu et al.2007).Two popular combinations are widely used to describe particle–fluidflow:the two-fluid model(TFM)and CFD–DEM.In TFM,bothfluid and solid phases are treated as interpenetrating continuum media in a computational cell which is much larger than individual particles but still small compared with the size of process equipment(Anderson&Jackson1967).However,its effective use heavily depends on the constitutive or closure relations for the solid phase and the momentum exchange between phases,which are often difficult to obtain within its framework; this is particularly true when dealing with different types of particles that should be treated as different phases.In CFD–DEM,the motion of discrete particles is obtained by solving Newton’s second law of motion as used in DEM,and theflow of continuumfluid by solving the Navier–Stokes equations based on the concept of local average as used in CFD,with the coupling of CFD and DEM through particle–fluid interaction forces(Xu&Yu1997).The main advantage of CFD–DEM is that it can generate detailed particle-scale information,such as the trajectories of and forces acting on individual particles,which is key to elucidating the mechanisms governing the complicatedflow behaviour.With the rapid development of computer technology, the CFD–DEM approach has been increasingly used by various investigators to study various particle–fluidflow systems as,for example,reviewed by Zhu et al.(2007,2008). The implementation of a CFD–DEM model,as pointed out by Feng&Yu(2004a), lies in three aspects:the formulation of governing equations,the coupling scheme for numerical computation and the calculation of particle–fluid interaction forces.The latter two have been well discussed,particularly for monosized particles(Feng&Yu 2004a;Zhu et al.2007).However,thefirst aspect is not well established.In fact, two models,called model A and model B,have been used by different investigators, and there are conflicting views regarding their applications(Hoomans et al.1998; Xu&Yu1998;Kafui,Thornton&Adams2002,2004;Feng&Yu2004a,b;Di Renzo&Di Maio2007).Xu&Yu(1998)pointed out that the interpretation of the fluid–particle interaction force is different for both models,but both the methods can meet the requirement that the bed pressure drop balances the bed weight at minimum fluidization and hence are valid forfluidization.Kafui et al.(2002)discussed model A and model B,and summarized the models used by different research groups. Nevertheless,their claim that model A best captures the essential features of a fixed/fluidized bed was questionable,as noted by Feng&Yu(2004b)and Kafui et al.(2004).It is now clear that the two models have little significant difference when applied to gasfluidization of monosized particles.It is not clear which is484Z.Y.Zhou,S.B.Kuang,K.W.Chu and A.B.Yubetter when applied to the modelling offluidization of particle mixtures,but thisproblem is related to the calculation of particle–fluid interaction forces.In fact,howto calculate thefluid drag force acting on a particle in a mixture is still an openproblem(Feng&Yu2004a;Beetstra,van der Hoef&Kuipers2007).More recently,the two models were further discussed by Di Renzo&Di Maio(2007).These authorsclaimed that model B is only valid at the minimumfluidization condition,contraryto those by other investigators(Kafui et al.2004;Feng&Yu2004b).Therefore,although the CFD–DEM approach is now widely used,its theoretical backgroundis not fully established.In fact,to date,there are still some basic questions whichneed to be answered.For example,what are the origins of different models such asmodel A and model B?What are the exact differences between those models?Whatis the applicability or limitation of a particular model,and which model is the mostappropriate for modelling different particle–fluidflow systems?This paper provides our answers to those questions.Firstly,the origins of differentformulations in the continuum approach are explored.It is argued that three models,rather than two,exist in the continuum approach.Then,it is demonstrated thatcorresponding to the continuum approach,there are three models in the CFD–DEM approach.The relationships between the three models are discussed,andtheir applicability is analysed theoretically and verified in a comparative study ofthree representative particle–fluidflow systems:fluidization,pneumatic conveyingand hydrocyclones.2.Theoretical treatments2.1.Origin of different model formulations in the continuum approachThe model formulation in the continuum approach to describing particle–fluidflow,focused on gas–solidflow influidization,has been proposed since the1960s,includingthose,for example,by Anderson&Jackson(1967),Ishii(1975),Gidaspow(1994),Enwald et al.(1996)and Jackson(1997).In practice,different sets of governingequations from different resources have been used(e.g.Arastoopour&Gidaspow1979;Lee&Lyczkowski2000;van Wachem et al.2001).However,the area hasbeen well established,as recently summarized by Prosperetti&Tryggvason(2007).Unfortunately,this is not the case in the CFD–DEM approach,as described in §1.On the other hand,the derivation of CFD–DEM models is closely related to the continuum approach due to the fact thatfluidflow is still modelled at themacroscopic local average level.Thus,it is helpful to start our discussion with theTFM approach.In the continuum approach,bothfluid and solid phases are treated as continuousmedia.Anderson&Jackson(1967)used the local average method to directly derivethefluid governing equation on the basis of the point equation of motion of thefluid,and the solid phase governing equation on the basis of the equation of motion for thecentre of mass of a single particle.They obtained thefirst set of governing equations(set I):ρfεf[∂(u)/∂t+∇·(uu)]=∇·ξ−n f i+ρfεf g(fluid phase),(2.1)ρsεs[∂(v)/∂t+∇·(vv)]=nΦ−∇·S+n f i+ρsεs g(solid phase),(2.2) whereεf andεs(=1−εf)are,respectively,volume fractions offluid and particles.ξisfluid stress tensor,Φis the local mean value of particle–particle interaction force,S is the tensor representing‘Reynolds stresses’for the particle phase,f i isDiscrete particle simulation of particle–fluidflow485 the local mean value of the force on particle i by its surroundingfluid and n is the number of particles per unit volume.This cannot be used unless the undetermined terms or dependency ofξ,Φ,S and f i on the voidage,the local mean velocities and the pressure are known.In order to solve the problem,Anderson&Jackson(1967) derived some constitutive equations,including:(i)combination of nΦand−∇·S into −∇·ξs which represents the solid stress tensor;(ii)ξandξs are analogous to thatfor the stress tensor in a Newtonianfluid,and written intoξ=−pδk+f(λ,µ,u), where p is the local meanfluid pressure andλ,µare,respectively,the effective bulk and shear viscosities;and(iii)decomposition of n f i into two components,namely,a component due to‘macroscopic’variations in thefluid stress tensor on a large scale compared with the particle spacing,together with the other component representing the effect of detailed variations of the point stress tensor as thefluidflows around a particle.That is,n f i=n(V p∇·ξ)/ V+n f i=εs∇·ξ+n f i,(2.3) where V p is the volume of the particle and n f i represents the part of the totalfluid–particle interaction force per unit bed volume arising from the detailed variations in the stress tensor induced byfluctuations in velocity as thefluid passes around individual particles and through the interstices between particles.It mainly includes the drag force in the direction of the relative velocity(u i−v i),and virtual mass force proportional to the mass offluid displaced by a particle.Other forces such as the lift force can also be included.Thus,the interaction force n f i in(2.1)and(2.2)is replaced by(2.3)together with the consideration of nΦ−∇·S=−∇·ξs,giving the second set of equations(set II):ρfεf[∂(u)/∂t+∇·(uu)]=εf∇·ξ−n f i+ρfεf g(fluid phase),(2.4)ρsεs[∂(v)/∂t+∇·(vv)]=εs∇·ξ+n f i+ρsεs g+∇·ξs(solid phase).(2.5) On comparing the governing equations in sets I and II,it can be seen that the difference is caused by the introduction of those constitutive equations.Anderson& Jackson(1967)commented that set I is derived directly from the basic equations of fluid mechanics for the system,the subsequent set II reflects their own opinion of the most appropriate form for the undermined terms in set I.Based on set II,particle–fluid interaction force can be further written in another format(Jackson1963;Anderson&Jackson1967).In particular,to eliminate thefluid stress tensor term,an equation is obtained by multiplying(2.5)by(1−εf)/εf and subtracting from(2.4),givingρsεs[∂(v)/∂t+∇·(vv)]=n f i/εf−ρfεs g+ρfεs[∂(u)/∂t+∇·(uu)]+ρsεs g+∇·ξs.(2.6) This is an equation of motion for particles which does not contain thefluid stress tensorξ.When compared with(2.5),it can be seen that the elimination offluid stress tensorξhas introduced a buoyancy term(−ρfεs g)and a termρfεs[∂(u)/∂t+∇·(uu)] which represents thefluid acceleration into the particle equation of motion.The magnitude of thefluid acceleration term depends onflow conditions.If this term approaches zero or much smaller than(n f i/εf−ρfεs g),according to(2.6),the total particle–fluid interaction force acting on particles can be written asn f i=n f i/εf−ρfεs g.(2.7)486Z.Y.Zhou,S.B.Kuang,K.W.Chu and A.B.YuIncorporating(2.7)into(2.1)and(2.2)and considering nΦ−∇·S=−∇·ξs give the third set of governing equations(set III):ρfεf[∂(u)/∂t+∇·(uu)]=∇·ξ−[n f i/εf−ρfεs g]+ρfεf g(fluid phase),(2.8)ρsεs[∂(v)/∂t+∇·(vv)]=∇·ξs+[n f i/εf−ρfεs g]+ρsεs g(solid phase).(2.9) However,it should be pointed out that the derivation of this set of equations is conditional.Strictly speaking,the following conditions for thefluid phase should be satisfied:ρfεs[∂(u)/∂t+∇·(uu)]=0.(2.10) This indicates that thefluidflow through the particle phase should be steady and uniform(Anderson&Jackson1967;Gidaspow1994).On the other hand,hydrodynamics models with concepts of the so-called models A and B have been widely used for the particle–fluidflow,as discussed by Bouillard, Lyczkowski&Gidaspow(1989),and later by Gidaspow(1994)and Enwald et al. (1996).The difference between models A and B depends on the treatment of the pressure source term in the governing equations.Generally speaking,if the pressure is attributed to thefluid phase alone,it is referred to as model B.If the pressure is shared by both thefluid and solid phases,it is referred to as model A.Bouillard et al.(1989)attributed the origin of model A to Nakamura&Capes(1973)and Lee&Lyczkowski(1981),and that of model B to Rudinger&Chang(1964)and Lyczkowski(1978).The drag coefficientsβA andβB are,respectively,defined in models A and B to calculate the particle–fluid interaction force.The applications of those two sets of governing equations and their comparison have been assessed for pneumatic conveying(Arastoopour&Gidaspow1979)andfluidization process(Bouillard et al. 1989),showing insignificant difference between the two models.Bouillard et al.(1989) commented that the main problem with model A is its stability,and being conditional on the absence of all viscous stresses and without the solid elastic modulus g(εf), while model B,which possesses all real characteristics,makes the set of equations well-posed.But Enwald et al.(1996)later clarified that nobody has yet proved well-posedness for a multi-dimensional initial-boundary value problem.To date,most researchers prefer model A,as reflected by the fact that commercial software packages FLUENT and CFX both use model A.On comparing the three formulations(sets I,II and III)with those hydrodynamics models A and B,it can be seen that in principle,model A is consistent with set II, and model B with set III.However,sets II and III are more general than models A and B but less detailed,which is another reason why the concepts of models A and B are more popular in TFM modelling.Mathematically,sets I and II(model A)are identical,as seen from the derivation of set II.Set III(or model B)is a simplified form of set I with the assumption of(2.10).It should be noted that,according to the definition of model B,set I is also in a form of model B.Thus,model B has two types: an original model B(set I)and a simplified model B.The deficiency of simplified model B has been realized by some investigators(e.g.Anderson&Jackson1967; Gidaspow1994).However,the difference between original model B and simplified model B has not been fully recognized,and the original model B(set I)is somehow forgotten.The two models are mixed up,and only simplified model B is commonly used.This has created some conceptual problems.For example,although model B or its treatment is argued to be well-posed,model A,which may be ill-posed,is more widely used due to its convenience in numerical implementation.When applied to CFD–DEM modelling,some investigators feel that the model B treatment isDiscrete particle simulation of particle–fluidflow487 better than model A.However,because a simplified model B was used,the treatment experiences problems,as discussed in§2.3.Nevertheless,the governing equations in the continuum approach have been well established,particularly if the expressions for different source terms are ignored.The challenge remaining is to develop closure laws to determine solidflow parameters including dynamic/bulk viscosities and particle pressure,and interfacial momentum transfer in multi-sized system(Bouillard et al.1989;Enwald et al.1996;Arastoopour 2001;van Wachem et al.2001).Two approaches are commonly used to achieve this goal.One is to formulate empirical models mainly based on particle properties and(local)voidage.However,those models vary significantly,depending on the conditions,as reviewed by Enwald et al.(1996).The other way is to use the so-called kinetic theory(e.g.Gidaspow1994;Iddir,Arastoopour&Hrenya2005).However, its general application is still questioned(see e.g.Campbell2006;Goldhirsch2008). Particles exhibit threeflow regimes:quasi-static,fast and in-between;to date,the success of TFM is largely limited to the fastflow regime.This difficulty does not exist in the CFD–DEM approach,as discussed below.2.2.Model formulations in the computationalfluid dynamics–discrete elementmethod approachCorresponding to the three set models in the continuum approach,CFD–DEM also has three models.However,the CFD–DEM approach is quite different from the traditional TFM.In CFD–DEM,one has to consider the coupling between DEM at the particle scale and CFD at the computational cell scale.The main difference between the CFD–DEM and TFM approaches lies in the treatment of the particle phase.In CFD–DEM,for the particle phase,based on the soft sphere model originally proposed by Cundall&Strack(1979),a particle in a particle–fluidflow system can have two types of motion:translational and rotational.The governing equations for the translational and rotational motion of particle i with radius R i,mass m i and moment of inertia I i can be written asm i d v id t=f pf,i+k cj=1(f c,ij+f d,ij)+m i g,(2.11)I i dωid t=k cj=1(M t,ij+M r,ij),(2.12)where v i andωi are,respectively,the translational and angular velocities of the particle,and k c is the number of particles in interaction with the particle.The forces involved are:the particle–fluid interaction force f pf,i,the gravitational force m i g, and inter-particle forces between particles which include the elastic force f c,ij and viscous damping force f d,ij.The torque acting on particle i by particle j includes two components:M t,ij,generated by the tangential force,and M r,ij,commonly known as the rolling friction torque.The equations used to calculate the particle–particle interaction forces and torques have been well established in the literature(Zhu et al. 2007).Many of these have been used in our previous studies of particle–fluidflow (Xu&Yu1997;Zhou et al.1999;Xu et al.2000;Feng&Yu2004a;Feng et al. 2004;Feng&Yu2007;Chu&Yu2008;Kuang et al.2008;Zhou,Yu&Zulli2009). The particle–fluid interaction force f pf,similar to f i in the continuum approach,is the sum of all types of particle–fluid interaction forces acting on individual particles488Z.Y.Zhou,S.B.Kuang,K.W.Chu and A.B.Yubyfluid,including the so-called drag force f d,pressure gradient force f∇p,viscous force f∇·τdue to thefluid shear stress or deviatoric stress tensor,virtual mass force f vm,Basset force f B and lift forces such as the Saffman force f Saffand Magnus force f Mag(Crowe,Sommerfeld&Tsuji1998).Unless otherwise specified in later discussion, the buoyancy force is included in the pressure gradient force f∇p.Therefore,the total particle–fluid interaction force on an individual particle i can be written asf pf,i=f d,i+f∇p,i+f∇·τ,i+f vm,i+f B,i+f Saff,i+f Mag,i.(2.13) Many correlations have been proposed to calculate the particle–fluid interaction forces,particularly the drag force which can be based on the equation of Ergun (1952)and Wen&Yu(1966)equations,and correlation of Di Felice(1994)or others. Details of those correlations can be found elsewhere(e.g.Crowe et al.1998;Zhu et al.2007).For thefluid phase,itsflow is essentially governed by the Navier–Stokes equation to be satisfied at every point of thefluid.As discussed earlier,the present interest is more focused on the particle behaviour,notfluid phase.Theflow offluid can thus be determined at a large scale,such as a CFD cell,which may contain many particles. Consequently,the governing equations forfluid phase are obtained based on the local averaged method as used in TFM.Thefluid governing equations corresponding to sets I,II and III are summarized in table1.Note that the equations to calculate the volumetric particle–fluid interaction force F pf differ for different sets,although they are all related to the particle–fluid interaction force f pf.It should be noted thatτ=µ[∇u+(∇u)−1]−(2/3)µ(∇·u)δk for Newtonianfluids. Corresponding to the volumetric particle–fluid interaction force terms in sets I,II and III,those force terms in(2.15)–(2.17)are respectively written by F set Ipf(=n f i),F set IIpf (=n f i)and F set IIIpf(=n f i/εf−ρfεs g).The definitions of n f i and n f i can befound in§2.1,and their determination in CFD–DEM is described below.The coupling of CFD and DEM is achieved mainly through the particle–fluid interaction force,which is at the computational cell level for thefluid phase(F pf in (2.15)–(2.17))and at the individual particle level for the solid phase(f pf in(2.13)). Three coupling schemes have been identified(Feng&Yu2004a).In scheme1,the force on thefluid phase from particles is calculated by a local-average method as used in the TFM,whereas the force on a particle from thefluid phase is calculated separately according to individual particle velocity.In scheme2,the force on thefluid phase from particles isfirst calculated at a local-average scale as used in scheme1, then this force is distributed among individual particles according to a certain average rule.In scheme3,at each time step,the particle–fluid interaction forces on individual particles in a computational cell are calculatedfirst,and the values are then summed to produce the particle–fluid interaction force at the cell scale.Theoretically,scheme 1is problematic because Newton’s third law of motion may not hold in describing the particle–fluid interaction.This problem is not there for schemes2and3,but the implementation of scheme2needs to introduce an extra assumption or numerical treatment at a CFD cell level to distribute the particle–fluid forces among the particles in the cell.Because scheme3represents the basic features of CFD–DEM modelling from particle scale to computational cell scale,it is more reasonable and logical.In fact,it has been widely used since its introduction by Xu&Yu(1997).Thus,the total volumetric particle–fluid interaction force n f i in a computational cell of volume VDiscrete particle simulation of particle–fluidflow489Mass conservation:∂(εf)/∂t+∇·(εf u)=0.(2.14) Momentum conservation(and corresponding particle–fluid interaction force).Set I:∂(ρfεf u)/∂t+∇·(ρfεf uu)=−∇p−F set Ipf+∇·τ+ρfεf g,(2.15a)where F set Ipf =1Vni=1f d,i+f∇p,i+f∇·τ,i+f i,and f pf,i=f d,i+f∇p,i+f∇·τ,i+f .(2.15b) Set II:∂(ρfεf u)/∂t+∇·(ρfεf uu)=−εf∇p−F set IIpf+εf∇·τ+ρfεf g,(2.16a)where F set IIpf =1Vni=1f d,i+f i,and f pf,i=f d,i+f∇p,i+f∇·τ,i+f .(2.16b)Set III:∂(ρfεf u)/∂t+∇·(ρfεf uu)=−∇p−F set IIIpf+∇·τ+ρfεf g,(2.17a)where F set IIIpf =1εf Vni=1f d,i+f i−1Vni=1ρf V p,i g,and f pf,i=(f d,i+f i)/εf−ρf V p,i g.(2.17b) Notes.(1)The governing equations for particle phase are given by(2.11)and(2.12).(2)f i=f vm,i+f B,i+f Saff,i+f Mag,i is the sum of particle–fluid interaction forces on particle i, other than the drag,pressure gradient and viscous forces which are often regarded as the dominant forces in particle–fluidflow.Table1.Formulations of different models in the CFD–DEM approach.can be determined byn f i=1Vni=1(f pf,i)=1Vni=1(f∇p,i+f∇·τ,i+f d,i+f vm,i+f B,i+f Saff,i+f Mag,i).(2.18)Equation(2.18)represents the total particle–fluid interaction force in a cell determined at a particle scale.According to(2.3),the total force in a cell in the continuum approach can be further rewritten asn f i=−εs∇p+εs∇·τ+n f i.(2.19) Equations(2.18)and(2.19)should be consistent.Thenn fi =n f i−(−εs∇p+εs∇·τ)=1Vni=1(f d,i+f vm,i+f B,i+f Saff,i+f Mag,i).(2.20)Thus,the volumetric particle–fluid interaction force in each model can be written asF set Ipf =n f i=1Vni=1(f∇p,i+f∇·τ,i+f d,i+f vm,i+f B,i+f Saff,i+f Mag,i),(2.21)490Z.Y.Zhou,S.B.Kuang,K.W.Chu and A.B.YuF set IIpf =n f i=1Vni=1(f d,i+f vm,i+f B,i+f Saff,i+f Mag,i),(2.22)F set IIIpf =n f i/εf−ρfεs g=1εf Vni=1(f d,i+f vm,i+f B,i+f Saff,i+f Mag,i)−1Vni=1(ρf V p,i g).(2.23)When coupling CFD with DEM,or vice versa,the governing equations should be consistent,as noted by Xu&Yu(1998).Generally speaking,for all the three models, the governing equations for particles can be the same,shown in(2.11)–(2.13).However, in order to satisfy the Newton’s third law of motion,for set III,the particle–fluid interaction force acting on particles,instead of(2.13),can be obtained from(2.23), and written asf pf,i=1εff d,i+f vm,i+f B,i+f Saff,i+f Mag,i−ρf V p,i g.(2.24)ments on different computationalfluid dynamics–discrete element methodmodelsClearly,from the above discussion,there are three sets of governing equations in the CFD–DEM modelling of particle–fluidflow.They correspond to those in TFM. By reference to the discussion presented in§2.1,the relationship and applicability of these models in the CFD–DEM approach can be obtained as discussed below. Firstly,set II is derived from set I mainly with the decomposition of particle–fluid interaction force n f i as shown in(2.3).Physically speaking,in set II,the pressure gradient force and viscous force on particles are separated from the volumetric particle–fluid interaction force F pf,while set I does not.However,such a treatment will not cause any significant difference in the simulated results because they are mathematically the same,which will be verified in§3.Secondly,set III is a simplified form of set I under the assumption of(2.10).In thefluid governing equations,F set Ipf and F set IIIpfrepresent the total volumetric particle–fluidinteraction force.The difference between them is that F set Ipf is explicit while F set IIIpfisimplicit and lumps the drag force and pressure gradient force(excluding those causedby buoyancy)together,as seen in table1.Both models are identical only when(2.10)is satisfied.Thirdly,when comparing set III with model B in the literature,a slight differencerelated to the viscous part exists(Xu et al.2000;Kafui et al.2002;Feng&Yu2004a).In the literature,the particle–fluid interaction force F pf and f pf in model B includesa component of the viscous forceεs∇·τ,but it has been excluded in the present set III.From its derivation as shown in(2.6)–(2.9),it can be seen that the viscous parttogether with the pressure has been hidden in the expression of(n f /ε-ρεs g)in(2.8)and(2.9).Most importantly,it should be noted that set III is not a general model,andits application is conditional.Strictly speaking,it can be used only when(2.10)issatisfied.Alternatively,from the viewpoint of forces,the following condition obtainedfrom(2.4)and(2.10)should be satisfied in a CFD cell:F resid=εs∇·ξ−n f εs/εf+ρfεs g=0.(2.25a)。