TURBULENT SEPARATED REATTACHED FLOW IN A TWO-DIMENSIONAL CURVED-WALL DIFFUSER

A turbulent separation-rcattachment flow in a two-dimensional asymmetrical curved-wall diffuser is studied by a two-dimensional laser doppler velocimeter.The turbulent boundary layer separates on the lower curved wall under strong pressure gradient and then reattaches on a parallel channel.At the inlet of the diffuser,Reynolds number based on the diffuser height is 1.2×10~5 and the velocity is 25.2m/s.The re- sults of experiments are presented and analyzed in new defined streamline-aligned coordinates.The experiment shows that after Transitory Detachment Reynolds shear stress is negative in the near-wall backflow region. Their characteristics are approximately the same as in simple turbulent shear layers near the maximum Reynolds shear stress.A scale is formed using the maximum Reynolds shear stresses.It is found that a Reynolds shear stress similarity exists from separation to reattachment and the Schofield-Perry velocity law ex- ists in the forward shear flow.Both profiles are used in the experimental work that leads to the design of a new eddy-viscosity model.The length scale is taken from that developed by Schofield and Perry.The composite velocity scale is formed by the maximum Reynolds shear stress and the Schofield Perry velocity scale as well as the edge velocity of the boundary layer.The results of these experiments are presented in this paper

NUMERICAL SIMULATION OF THREE DIMENSIONAL TURBULENT FLOW IN SUDDENLY EXPANDED RECTANGULAR DUCT

In this paper,to simulate the three dimensional turbulent flow in suddenly expanded rectangular duct numerically,the SIMPLEC algorithm is employed to solve the incompressible Navier-Stckes equation with k-εturbulence model.The numerical resulis show well the three dimensional turbulent flow field in the rectangular duct behind the sudden expansion cross-section. and agree.fairly well with the experimental result of the length of the main circumfluence.The numerical method of this paper can be applied to numerical analysis of this kind of turbulent flow.

ALGEBRAIC TURBUL ENCE MODEL WITH MEM ORY FOR COMPUTATION OF 3-D TURBULENT BOUNDARY LAYERS WITH VALIDATION

Additional equations were found based on experiments for an algebraic turbulence model to improve the prediction of the behavior of three dimensional turbulent boundary layers by taking account of the effects of pressure gradient and the historical variation of eddy viscosity, so the model is with memory. Numerical calculation by solving boundary layer equations was carried out for the five pressure driven three dimensional turbulent boundary layers developed on flat plates, swept wing, and prolate spheroid in symmetrical plane. Comparing the computational results with the experimental data, it is obvious that the prediction will be more accurate if the proposed closure equations are used, especially for the turbulent shear stresses.

Stress-Blended Eddy Simulation of the Turbulent Flow Around Circular Cylinder with Dynamic Hybrid RANS/LES Model

In order to verify the effectiveness and superiority of the dynamic hybrid RANS/LES(DHRL)model,the flow around a cylinder with sinusoidal fluctuating velocity at the inlet was used as the test case.The latest computational fluid dynamics(CFD)model can flexibly choose any existing large-eddy simulation(LES)method combined with RANS method to calculate the flow field.In addition,the DLES model and DDES model are selected as typical representatives of the turbulence model to compare the capture ability of the flow field mechanism.The internal flow field including the y+value,velocity distribution,turbulent kinetic energy and vortex structures is comprehensively analyzed.Finally,the results show that the new model has enough sensitivity to capture the information of the flow field and has more consistent velocity distribution with the experimental value,which shows its potential in practical engineering applications to some extent.

Numerical Simulation of Turbulent Flow of Hydraulic Oil through 90° Circular-sectional Bend

Oil flow through pipe bends is found in many engineering applications. However, up to now, the studies of oil flow field in the pipe bend appear to be relatively sparse, although the oil flow field and the associated losses of pipe bend are very important in practice. In this paper, the relationships between the turbulent flow of hydraulic oil in a bend and the Reynolds number Re and the curvature ratio δare studied by using computational fluid dynamics （CFD）. A particular emphasis is put on hydraulic oil, which differs from air or water, flowing through 90° circular-sectional bend, with the purpose of determining the turbulent flow characteristics as well as losses. Three turbulence models, namely, RNG κ-ε model, realizable k-ε model, and Reynolds stress model （RSM）, are used respectively. The simulation results in the form of contour and vector plots for all the three turbulence models for pipe bends having curvature ratio of δ=0.5, and the detailed pressure fields and total pressure losses for different Re and δ for RSM are presented. The RSM can predict the stronger secondary flow in the bend better than other models. As Re increases, the pressure gradient changes rapidly, and the pressure magnitude increases at inner and outer wall of the bend. When δ decreases, two transition points or transition zones of pressure gradient arise at inner wall, meanwhile, the transition point moves towards the inlet at outer wall of the bend. Owing to secondary flow, the total pressure loss factor k increases as the bend tightens, on the contrary, as Re increases, factor k decreases due to higher velocity heads, and the rapid change of pressure gradient on the surface of the bend leads to increasing of friction and separation effects, and magnified swirl intensity of secondary flow. A new mathematical model is proposed for predicting pressure loss in terms of Re and δ in order to provide support to the one-dimensional simulation software. The proposed research provides reference for the analysis of oil flow with higher Re in the large bends.

NumericaI Computation of Flow over a Train in Cross-Winds

A finite different method is developed to predict the side force on a high speedtrain in a cross-wind at low yaw anglee. The k-εturbulence model with wallfunctions is employed. the solution algorithm is based on curvilinearnonorthogonal coordinates,covariant velocity components ,and staggered gridarrangement. The convective fluxes are described by the Power tow Scheme.A highly deformed grid generated with an elliptic grid generator is used aroundthe comero of the cross-section of the train. The results obtained comparepositively with wind tunnel experinients.

Thermal Radiation Effect on the MHD Turbulent Compressible Boundary Layer Flow with Adverse Pressure Gradient, Heat Transfer and Local Suction

The combined effect of magnetic field, thermal radiation and local suction on the steady turbulent compressible boundary layer flow with adverse pressure gradient is numerically studied. The magnetic field is constant and applied transversely to the direction of the flow. The fluid is subjected to a localized suction and is considered as a radiative optically thin gray fluid. The Reynolds Averaged Boundary Layer (RABL) equations with appropriate boundary conditions are transformed using the compressible Falkner Skan transformation. The nonlinear and coupled system of partial differential equations (PDEs) is solved using the Keller box method. For the eddy-kinematic viscosity the Baldwin Lomax turbulent model and for the turbulent Prandtl number the extended Kays Crawford model are used. The numerical results show that the flow field can be controlled by the combined effect of the applied magnetic field, thermal radiation, and localized suction, moving the separation point, xs , downstream towards the plate’s end, and increasing total drag, D . The combined effect of thermal radiation and magnetic field has a cooling effect on the fluid at the wall vicinity. The combined effect has a greater influence in the case of high free-stream temperature.

Analysis of three-dimensional vortexes below the free surface in a continuous casting mold

To study fluctuations of the free surface of liquid steel in the mold,two different models with the same casting conditions but different thicknesses were employed to analyze the hydrodynamic behavior at the top of the mold.The first model was a standard thickness slab,and the second had a thickness three times wider.It is found with the second model that above the plane formed by the steel jets,it is possible to observe four three-dimensional vortexes that interact with the submerged entry nozzle（SEN）and mold walls.By using a biphasic model to simulate the interface between the liquid and air inside the mold,the flow asymmetry and the fluctuations of the free surface can be clearly observed.

Three-Dimensional Water-Quality Simulation for River Based on VOF Method

In the present study, considering the transport and transformation processes of variables, a threedimensional water quality model for the river system was established, which coupled the volume of fluid(VOF) method with the k-ε turbulence mathematical model. Then, the water hydrodynamic characteristics and transport processes for BOD_5, NH_(3^-)N and TP were analyzed. The results showed that the water surface of convex bank was a little lower than that of concave bank due to the centrifugal force near the bend, and most concentrations were inferior to the type Ⅴ standard indexes of surface water environmental quality. The model validation indicated that the errors between the simulated and monitored values were comparatively small, satisfying the application demands and providing scientific basis and decision support for the restoration and protection of water quality.

High performance parallel computing of large eddy simulation of the flow in a curved duct with square cross section

Large eddy simulation(LES) cooperated with a high performance parallel computing method is applied to simulate the flow in a curved duct with square cross section in the paper. The method consists of parallel domain decomposition of grids, creation of virtual diagonal bordered matrix, assembling of boundary matrix, parallel LDL^T decomposition, parallel solving of Poisson Equation, parallel estimation of convergence and so on. The parallel computing method can solve the problems that are difficult to solve using traditional serial computing. Furthermore, existing microcomputers can be fully used to resolve some large-scale problems of complex turbulent flow.

4D Flow MRI在肥厚型心肌病中的应用研究进展

四维血流磁共振成像(four-dimensional flow magnetic resonance imaging,4D Flow MRI)是近年快速发展的一种在体无创血流定量成像技术,应用于心脏大血管,头颈部及周围血管等血流动力学研究。肥厚型心肌病(hypertrophic cardiomyopathy,HCM)是临床常见的原发性、遗传性心脏病。本文主要介绍4D Flow MRI的成像原理及目前其在HCM中的应用研究相关文献,拟总结利用4D Flow MRI技术获得的HCM血流动力学参数特征,为HCM患者进行早期干预和治疗提供影像学证据。

FAST SOLUTION OF TURBULENT SEPARATION BY STRAWN'S METHOD

A quasi-simultaneous viscous/inviscid interaction model and a new integral method are tried to predict twodimensional incompressible turbulent boundary-layer separating flows. The results are compared with experiments and other prediction.

Assessment of Turbulence Models on Bridge-Pier Scour Using Flow-3D

The main purpose of this paper is to analyze the influence of different turbulence flow models on scouring pit of bridge-pier. Flow-3D software is applied in line with the purpose. The key motivation for this study is to contribute to the Flow-3D software by means of some modification and adjustment in the sediment scour model and shallow water model. An assessment of turbulence model adopted with the parameters of the Melville experiment to estimate the maximum scour-depth was performed. In the simulation results, the alternate eddy formation and shedding were repeated while the Karman vortex street formed behind the pier for the large eddy simulation LES turbulence model is more realistic in the flow phenomenon. The results of the scour development of large eddy simulation (LES) turbulence model were found to be more satisfied than the Renormalized group (RNG) turbulence model and close to the prior experiment results. The simulated scour results were significantly different with the observed data collected from previous literature in the reason of some unsuitability of meshing method in Flow-3D software.

NUMERICAL SIMULATION OF UNSTEADY TURBULENT FLOW INDUCED BY TWO-DIMENSIONAL ELEVATOR CAR AND COUNTER WEIGHT SYSTEM

A two-dimensional model of unsteady turbulent flow induced by high-speed elevator system was established in the present study. The research was focused on the instantaneous variation of the aerodynamic force on the car structure during traversing motion of the counter weight in the hoistway. A dynamic meshing method was employed to treat the multi-body motion system to avoid poor distortion of meshes. A comprehensive understanding of this significant aspect was obtained by varying the horizontal gap （δ =0.1m, 0.2m, and 0.3m） between the elevator car and the counter weight, and the moving speed （ U 0= 2m/s, 6m/s, and 10m/s） of the elevator system. A pulsed intensification of the aerodynamic force on the elevator car and subsequent appearance of large valley with negative aerodynamic force were clearly observed in the numerical results. In parameters studied （ δ =0.1m, U 0= 2m/s, 6m/s, 10m/s）, the peaked horizontal and vertical forces are respectively 7-11 and 4.3-5.65 times of that when the counter weight is far from the car. These results demonstrated the prominent influence of the traversing counter weight on aerodynamic force on the elevator car, which is of great significance to designers of high-speed elevator system.

大雷诺数下对称翼型的转捩判断与规律研究

围绕翼型的转捩问题,以NACA0012、NACA0015、NACA0018三种不同厚度的对称翼型为研究对象,基于TSST湍流模型的数值模拟方法,提出基于湍流强度的转捩判断方法并研究在5种大雷诺数条件下翼型表面流动的转捩规律,以期为风力机叶片设计提供新的参考思路。研究表明,基于湍流强度的转捩判断方法是有效、可行的,使用翼型表面湍流强度曲线的阶跃现象观测转捩,可有效避免转捩前流动扰动带来的影响。同时利用湍流强度的变化情况可为风力机叶片设计寻找最佳设计参数。研究发现,增大攻角和雷诺数使得翼型上翼面转捩位置前移、下翼面转捩位置后移。此外,随着攻角的减小、雷诺数的增大、翼型表面厚度的增加,在翼型转捩前的流动逐渐稳定。

THE EXPERIMENTAL RESULTS OF 2-D FREE SHEAR TURBULENT FLOWS AND THE COMPARISON WITH THE THEORETICAL COMPUTATION

An extensive set of measurements in 2-D turbulent mixing layer, wake and jet flow by the hot-wire technique and data sampling are presented. The measured quantities, i. e. the mean velocity, the turbulence intensity, the Reynolds stress and higher-order correlations of the fluctuating velocity in the self-preserving region of the above free shear flows are compared with the computational results based on Zhou's theory for the shear turbulence of in- compressible fluid. The experimental and computational results are in good agreement.

NUMERICAL COMPUTATION OF 3-D TURBULENT FLOW IN TURBINE CASCADE

Ⅰ. INTRODUCTIONThe flow phenomena that exist in the advanced turbomachinery are extremely complex and propose a challenge to the engineers and scientists to improve the design procedure. The rapid progress of high speed and large capacity computers has encouraged the development of computational fluid dynamics that has had an increasingly important influence on turbomachinery blade design and analysis. Compared with the inviscid solver, the N.S.

歧管式射流微通道液冷散热性能

随着信息技术进步,芯片向大面积、高功率方向发展,对热管理提出了严峻挑战。微通道液冷能够解决高功率芯片散热难题,但传统平直微通道热沉流阻大、温度均匀性差。提出了一种耦合歧管式进出液结构、分布式射流和微针翅的新型歧管式微通道散热器,在平均热通量高于330 W/cm^(2)、总功率达到2500 W时,芯片平均温度低于70℃,实现了高效散热。通过数值模拟发现:降低散热器射流腔高度可显著强化传热,但整体压降也随之陡升,存在一个最佳射流腔高度;散热器底板的微针翅尺寸及其与射流腔的相对尺寸是新型歧管式微通道散热器的重要结构参数,微针翅的存在并不是绝对有益于传热强化。定义了微针翅与射流腔之间相对高度的无量纲参数——翅占比,存在临界翅占比使得阻碍效应和强化效应相抵消,当翅占比高于这一临界值时才能达到强化换热效果。本研究为新型歧管式微通道散热器的设计提供了指导。

基于一维计算模型的斜盘式柱塞泵流动特性分析

斜盘式柱塞泵广泛应用在直升机疲劳试验的液压系统中,其流动特性对液压系统稳定性有着至关重要的作用。文中使用立体几何方法分析了斜盘式柱塞泵柱塞运动轨迹,基于图形解析法推导了过流面积公式,并编写相应Matlab程序实现吸排油过流面积自动化计算;构建了考虑流量倒灌及泄漏的单柱塞流动模型,结合AMESim软件实现柱塞泵三维计算模型向一维计算模型的转变;依据初始工况计算结果分析了柱塞泵的流动特性及其产生流量脉动的原因,并使用基于计算流体力学(CFD)方法的三维模型所获得的流量脉动计算结果验证了一维计算模型的准确性。在此基础上分析了不同运行工况(包含运行温度、工作压力及柱塞泵调节参数)对出口流量脉动率的影响,从降低流量脉动率进而提高直升机疲劳试验精度的角度分析了试验中柱塞泵调节控制要点。文中提出的一维计算模型可显著提高柱塞泵仿真计算速率,便于后续柱塞泵的改进设计以及将其作为子系统添加到虚拟数字试验平台中。

秸秆还田下土壤孔隙演化及其对溶质穿透特征的影响机理分析

为揭示秸秆粉碎还田后,不同腐解进程下土壤孔隙演化及其对水分和溶质穿透特征的影响机理,设置不同秸秆还田量(0、5、10、15 t/hm^(2))和还田时间(0、30、60 d)处理,采用CT断层扫描技术,视觉量化了土壤孔隙结构特征演变,并基于溶质穿透试验,分析了水分-溶质迁移优先流规律。结果表明,秸秆还田引起土壤孔隙/喉道特征变化,抑制水分-溶质迁移过程,田间持水率和土壤含水率上升,溶质穿透变慢,优先流现象减少,土壤水肥有效持留;随秸秆腐解至60 d,孔隙/喉道特征改变,优先流开始发育,但土壤水肥持留能力增强。秸秆还田5、10、15 t/hm^(2)初期,和CK组相比大孔隙体积占比分别减少7%、14%、50%,连通孔隙减少11%、39%、66%,表层含水率增加1%、3%、6%。腐解60 d后,和0 d相比大孔隙体积占比分别增加331%、200%、357%,连通孔隙增加33%、84%、195%,表层含水率增加6%、5%、5%,完全穿透试样所需溶质减少55%、76%、67%。基于Green-Ampt模型和指数衰减模型估算了不同秸秆初始投入量在不同腐解时间下的导水特征,发现饱和导水率在秸秆还田后减小,且随秸秆腐解增大。研究可为控制大孔隙流和无效灌溉提供依据,进一步为秸秆科学还田提供实践指导。