微通道人工泡状流的Lattice Boltzmann数值模拟

采用高频电控热激发汽泡的方式构造微通道人工泡状流,可以有效抑制微通道沸腾流动的不稳定性和强化传热。本文基于Lattice Boltzmann大密度比多相流复合模型,数值研究了通道内人工泡状流的流动和传热,通过比较分析不同发泡频率的泡状流,量化分析了汽泡运动和增长对微通道流动与传热的相互影响。一方面着重分析了汽泡运动对微通道运动边界层以及汽泡相变增长对热边界层的影响,另一方面也研究了边界层对汽泡动力行为的影响,所得结论对研究抑制微通道沸腾流动不稳定性和强化传热有参考意义。     

用格子Boltzmann方程模拟浅水波问题

提出了用格子Ｂｏｌｔｚｍａｎｎ方程（ＬＢＥ）模拟浅水波问题的方法．通过无粘气体运动方程与浅水波方程的比较,确定了ＬＢＥ方法中平衡态的形式,使宏观方程与浅水波方程一致．计算了二维浅水波的一个问题,数值结果与精确解做了比较．     

A novel incompressible finite-difference lattice Boltzmann equation for particle-laden flow

In this paper, we propose a novel incompressible finite-difference lattice Boltzmann Equation (FDLBE). Because source terms that reflect the interaction between phases can be accurately described, the new model is suitable for simulating two-way coupling incompressible multiphase flow. The 2-D particle-laden flow over a backward-facing step is chosen as a test case to validate the present method. Favorable results are obtained and the present scheme is shown to have good prospects in practical applications. The project supported by the National Natural Science Foundation of China (60073044), and the State Key Development Programme for Basic Research of China (G1999022207). The English text was polished by Guowei Yang and Yunming Chen.     

正则化相场格子玻尔兹曼两相流模型

目前, 基于相场理论的格子玻尔兹曼 (lattice Boltzmann, LB)模型已经被广泛应用于气-液两相流流动问题中. 为了提高已有相场LB模型的数值稳定性, 提出了一种新型的正则化相场格子玻尔兹曼模型(regularized lattice Boltzmann model, RLBM)用于模拟大密度比和大黏度比的气液两相流动. 该模型由界面追踪和流场求解两个核心模块构成, 其中界面变化采用守恒型Allen-Cahn (A-C)相场方程控制, 流场演化则通过不可压Navier-Stokes (N-S)方程控制. 首先, 构建了两个正则化格子玻尔兹曼方程(lattice Boltzmann equation, LBE)分别获取流场信息和相场信息. 与标准的单松弛模型不同的是, 提出的模型在演化方程的碰撞项中引入了非平衡态的预前碰撞函数, 且该预前碰撞项仅与宏观量有关. 通过Chapman-Enskog (C-E)多尺度展开分析, 证实了所提出的模型能够准确地恢复到宏观流场控制方程和相场控制方程. 进一步地, 为了验证本模型的有效性, 模拟了4个两相流典型算例, 包括静态液滴、Rayleigh-Taylor (R-T)不稳定性问题、气泡上升和单个液滴撞击液膜. 数值结果证实了提出的模型能够准确地模拟大密度比、大黏度比、大雷诺数下的气液两相流流动问题. 更重要的是, 相较于传统的相场单松弛模型在小的迁移率$( {theta _M} < 2.0 times {10^{ - 2}}) $下就会诱发数值方法不收敛的问题, 提出的模型在模拟迁移率较小$( {theta _M} = 1.0 times {10^{ - 6}} )$的复杂两相流动时表现出更好的稳定性, 能够更准确地刻画界面流动, 捕捉界面形态.     

盐度对甲烷水合物分解特性影响的LBM模拟

海洋甲烷水合物在分解过程中会受到海水盐度的影响,本文基于格子玻尔兹曼方法建立了孔隙尺度下甲烷水合物在盐水中分解的数值模型。该模型综合考虑了甲烷水合物分解动力学、甲烷和盐的传质以及气液两相流动和传热过程,并通过引入附加源项描述盐度对于甲烷水合物分解的影响。在此基础上,本文分析了盐度对甲烷水合物分解特性及传热特性的影响。结果表明,甲烷水合物在盐溶液中的分解速率明显快于纯水中的分解速率,并且随着盐度的增加,水合物分解得越快,分解持续的时间越短。计算域内平均温度在水合物分解的初始阶段急剧下降,然后逐渐升高到初始入口温度,并且最低平均温度随着盐度的增加而升高。因此,盐度的增加可以加快甲烷水合物的分解速率,降低水合物分解的吸热量。     

ON THE MECHANISM OF TURBULENT COHERENT STRUCTURE (III)──A STATISTICAL AND DYNAMICALMODEL OF COHERENT STRUCTURE AND ITSHEAT TRANSFER MECHANISM

I.IntroductionItisaveryinlportulltdiscoveryofcoherentstrLICturcinshetlrturbulellt11owsbyexperimentinthelate1950s,whichleadsustoseekthenaturall,ropertiesofturbulcllcefromthenewideaandilladifferentway.ThestudyofthecoherclltstrLlcttlrcisofgreatimportallcetounderstandthegeneration,developmentanddecayof'tLlrbulellce,allditlsoconstructsInorerealisticturbulencemodeltheory.Meanwhile,itwillbeor11elpIYomengineerillgpoint,suchaslllassandheattrallslbr,dl'agI.eductiolland11oisecontrolproblems.Soinlnlel…     

ON THE MECHANISM OF TURBULENT COHERENT STRUCTURE (III)──A STATISTICAL AND DYNAMICAL MODEL OF COHERENT STRUCTURE AND ITS HEAT TRANSFER MECHANISM

Following Tsai & Ma^[1] and Tsai & Liu^[2], a statistical and dynamical near-wall turbulent coherent structural model with separate consideration of two different portions: locally generated and upstream-transported large eddies has been established. With this model, heat transfer in a fully developed open channel in the absence of pressure gradient is numerically simulated. Database of fluctuations of velocity and temperature has also been set. Numerical analysis shows the existence of high-low temperature streak caused by near-wall coherent structure and its swing in the lateral direction. Numerical results are in accordance with the computations and experimental results of other researchers.     

Coherent contribution to turbulent mixing of a jet in cross flow

In this work, an experimental study of a jet issuing in cross flow is reported. Support is offered to a theory on the origin of Karman-like vortices, in the wake of jets issuing in boundary layers. Further, a coherent structure with strong contribution to the energetics of the flow field is identified here. This structure has not been reported earlier, according to the present authors' knowledge, and it is shown to be related to engulfment of external fluid at the bottom of the jet, and to interesting stochastic and spectral characteristics of the flow field. Three-dimensional plots of the coherent quantities, based on experimental data, reveal a double-helical morphology of the coherent structure. The same morphology has recently been proposed for the far field of jets issuing in stagnant fluid (i.e., without cross flow). The results of this study are expected to support theoretical and numerical work on jets issuing in cross flow.     

具有壁面射流激励的圆管内气相流动大涡模拟

采用大涡模拟方法和单方程亚格子模式对小尺度量进行模拟。研究了不同强度壁面射流激励对圆管内气相流动的影响,模拟结果给出了射流对瞬态拟序结构发展、时平均流向速度分布的影响。随着射流强度的增加,射流入口附近流体的回流现象增强。射流强度足够大时可以减小管壁处的切应力值,同时会减小壁面附近流动速度,这种速度分布会导致气体夹带颗粒的能力下降,从而在实际两相流动中容易造成壁面附近的气粒返混现象。     

模拟MKDV方程的格子BGK模型

目前,格子Boltzmann方法已被广泛应用于模拟各种非线性方程.文中用D1Q4模型给出MKDV方程的带修正项的BGK型格子Boltzmann法.数值模拟与理论结果吻合很好.     

建筑物周围流场格子Boltzmann仿真

基于格子BGK方程的三维15点格子Boltz-mann模型,对建筑物周围流场进行了数值仿真,对其流场的划分进行了分析,并对不同雷诺数下建筑物周围的流场进行了数值模拟计算,得到了比较满意的结果,为环境质量的评估提供了新的途径.     

Experimental study of heat transfer characteristics due to confined impinging two-dimensional jets

Experimental results are presented for characteristics of impingement heat transfer caused by three slot jets. Experimental values were obtained for the dimensionless distance H = 0.5−3, dimensionless pitch P = 6−16, and Reynolds number Re = 500−8000. For laminar impinging flow, they were compared with numerical results. For turbulent impinging flow, two peaks of the local Nusselt number were obtained behind the second nozzle. The position of the second peak approached the nozzle as the space between nozzle and impinged surface decreased. The average Nusselt number between the central and second nozzles was determined from the ratio P/H and the Reynolds number based on the pitch of the nozzles.