EXPERIMENTAL STUDY ON THE VORTEX FORMATION AND ENTRAINMENT CHARACTERISTICS FOR A ROUND TRANSVERSE JET IN SHALLOW WATER

The vortex formation and entrainment characteristics for a round transverse jet in shallow water were experimentally investigated by means of a combination of LIF flow visualization and PIV measurement. A scarf vortex wrapped around the main body of the jet is formed in the near-wall region due to the interaction between the resulting wall jet and sufficiently shallow crossflow, with some more or less unsteady flow properties and with spreading ranges as functions of both the velocity ratio and the water depth within the near field. The entrainment of the ambient crossflow fluid into the jet main body is closely associated with the time-evolving features of the shear layer between the jet and surrounding fluid as well as the induced vortical structures near the wall. In the case of slight impingement upon the wall, the interaction between the jet shear layer and the weak, unstable scarf vortex gives rise to an appreciable local entrainment enhancement, confined in the near-wall region in the vicinity of the stagnation point. While in the case of intense impingement upon the wall, the well-organized and stable scarf vortex gives rise to a greatly enhanced entrainment and a greatly increased lateral spreading rate nearly throughout the overall near field as compared to the conventional wall jet. In addition, the entrainment of the ambient crossflow fluid by the scarf vortex in this case occurs largely on the surface of the unique spiral roller structure by itself due to the presence of smaller and unorganized eddies, and accordingly the scarf vortex is likely to keep its spiral roller structure steadily to a relatively great downstream distance within the near field.     

LARGE-EDDY SIMULATION OF THREE-DIMENSIONAL VORTICAL STRUCTURES FOR AN IMPINGING TRANSVERSE JET IN THE NEAR REGION

The three-dimensional vortical structures for an impinging transverse jet in the near region were numerically investigated by means of Large-Eddy Simulation (LES). The LES results reproduced the skewed jet shear layer vortices close to the jet nozzle and the scarf vortex in the near-wall zone, in good agreement with the experimental observations. Different vortical modes in the skewed jet shear layer close to the jet nozzle were identified depending upon the velocity ratio between jet and crossflow, namely changing from an approximately axisymmetric mode to a helical one with the velocity ratios varying from 20 to 8. Moreover, the scarf vortex wrapped around the impinging jet in the near-wall zone showed distinct asymmetry with regard to its bilateral spiral legs within the near region. And the entrainment of the ambient crossflow fluids by the scarf vortex in the near-wall zone was appreciably influenced by its asymmetry and in a large part occurred on the surface of the spiral roller structures in the course of spreading downstream.     

ON THE SELF-SIMILARITY OF A JET IN CROSSFLOW

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EXPERIMENTAL STUDY ON THE EFFECTS OF AIR ENTRAINMENT ON A PLANE JET DIFFUSION IN A PLUNGE POOL

l'mTRODUrmNThisworkwasmotivatedbythepotentialapplicationOftheerosionofplungepoolsdownstreamofdamscausedbysubmergedwaterjets.TheerosionorscourofplungepoolsoccursatthePointofajetimpact.Thescourprocesshasbeeninvestigatedformanyyears.Thescourdepthestimatedfromformulasdevelopedoveryears,however,indicatesawidevariation(MasonandArumugam,l985)-Mostoftheseformulasinvolveanexpressioninwhichscourdepthisafunctionofthedischargeperunitwidth,theheaddropandthechar-acteristicsizeofthebedmaterial.Arecentin…     

平面掺气散裂射流特性

本文根据部分掺气散裂射流的特性，提出了相应的物理模式与数学模式，并通过简化与相似分析得到了掺气散裂射流的半宽，水挟气泡区的半宽，水核区的半宽和射流掺混区与水挟气泡区边界处的含气浓度随射流初始条件的变化，并将计算结果与实验结果进行了比较，结果表明，两者甚为一致。     

Large eddy simulations of 45° and 60° inclined dense jets with bottom impact

In the present study, we performed a numerical study with the Large Eddy Simulations (LES) approach to simulate inclined dense jets with 45° and 60° inclinations in a stagnant ambient, including the bottom impact and subsequent spreading on the wall boundary. The objective was to evaluate the performance of LES on the predictions of both the kinematic and mixing behavior of the inclined dense jet with bottom boundary in the near field region. The Dynamic Smagorinsky sub-grid model was adopted with near-wall modeling for the bottom boundary. The results showed that LES can reasonably predict the jet trajectory with the present mesh scheme, including the locations of the return point and impact point at the boundary. The localized concentration build-up at the impact point reported by Abessi and Roberts (2015) was also reproduced. The impact dilution was however underestimated by ∼20% in general corresponding to the grid resolution adopted in the present study, which demonstrated the challenge to simulate accurately the dynamics of the mixing behaviour as well as the wall interaction processes. The spreading layer was examined to the end of the near field region as defined by Roberts et al. (1997). The profiles of the mean concentration and concentration fluctuation along the spreading layer were found to be similar to previous experimental results with self-similar behaviour. The dilution was however also under-predicted within the spreading layer.     

不同动力环境下孔间距对双孔射流特性的影响

为研究孔间距对双孔射流运动和稀释特性的影响,采用粒子图像测速技术(PIV)和激光诱导荧光技术(PLIF)分别对静水、横流和波浪环境下双孔射流的速度场和浓度场进行测量,对比分析了孔间距为5倍、10倍和15倍射流孔直径时双孔射流的轴向速度、横断面垂向速度、轨迹线及浓度场分布情况。结果表明:在静水环境下,孔间距较小时双孔射流的轴向速度衰减较单孔射流慢,随着孔间距的增大双孔射流轴向速度衰减的程度逐渐趋近于单孔射流。在横流环境下,随着孔间距的增大,前方射流对后方射流的遮掩作用不断减小,而后方对前方射流的卷吸作用也有所减弱,导致前方射流弯曲程度的增大和后方射流上升高度的降低。在波浪环境下,孔间距较小时,两孔中间存在一个独立的高浓度区;孔间距增大后,浓度等值线逐渐呈"凸"形分布。为降低双孔射流相互作用对射流初始稀释的影响,建议在波浪和横流环境下双孔射流的孔间距不宜小于射流孔直径的10倍。     

NUMERICAL SIMULATION OF THE FORMATION OF NANOPARTICLES IN AN IMPINGING TWIN-JET

The Large Eddy Simulation (LES) method has been used to solve the fluid momentum equations coupled with a convection-diffusion equation to study the formation of pollutant nanoparticles in a vehicular exhaust with impinging twin-jet. The functions of the space (S) between the two jets and the distance (H) from the exit of nozzle to the impingement plane are evaluated according to the distributions of pollutant nanoparticles. The results show that the nucleation produces a large number of nanoparticles, and gas-to-nanoparticle conversion mostly takes place in the interface region of the two jets, the circumambience of the jets, and region near the plane. The maximal particle size and maximal number concentration produced by both nucleation and coagulation appear around the region of free jet and the region near the plane, respectively. The significant differences for various spaces between the two jets are the number concentration and size distributions in the interface region of the two jets. For the case with larger space, more nanoparticles are produced by nucleation and coagulation. The more the distance from the exit of nozzle to the impingement plane, the lower is the number concentration and the fewer the particles distribute near the plane. Increasing the distance from nozzle to plane is beneficial to the reduction of nanoparticle formation.     

多孔射流扩散器在宽浅型江河中排放特性研究

多孔射流扩散器排放城市污水是充分利用天然水体环境容量和自净能力的有效途径，本文以水槽试验资料为基础，分析了流动水体中多孔射流扩散器排污下游流场和浓度场的主要影响参数，根据多孔射流与环境水体的掺混稀释特性，采用虚拟扰动源的处理方法，给出了描述扩散器排放下游流速与浓度的分布公式，该公布公式的计算结果与实测值吻合较好。     

NUMERICAL SIMULATION OF TURBULENT JETS WITH LATERAL INJECTION INTO A CROSSFLOW

1. INTRODUCTION The interaction of jets with crossflow generates complex flow fields which exist in a variety of industrial applications, e.g. internal film cooling of turbine blades, dilution air jets in combustion chambers, jet from V/STOL aircraft in transition flight. Systematic experimental, theoretical and numerical investigations of the flow fields began several decades ago, where the parameters studied include the jet injection angel, the jet-to-crossflow velocity ratio, the jet …     

STABILITY AND MIXING CHARACTER FOR BUOYANT JETS IN QUIESCENT SHALLOW WATER

BRIEFINTRODUCTIONOFTHEPAPER:Inthe firstpart,thecharactersforthe3Dthermalbuoy antjetsintheflowingenvironmentareanalyzed experimentally.UsingtheMicroADVandtem peraturemeasuringsystem,thevelocityfieldand temperaturefieldoftheheatedbuoyantjetsatdif ferentcross to jetvelocityratiosaremeasured.Thetestdatarevealedthecharacteristicsofthose meanflowparametersandturbulentflowparame tersaregaveout.Furthermore,theexperimental runsarenumericallysimulatedusingthebuoyancy extendedkεturbulencemo…     

射流冲沙研究

作者通过实验和分析，研究了横流中加入平面冲击射流对防止局部泥沙淤积的影响。水槽实验中观测了水射流局部紊动强度变化、射流冲沙范围内局部紊动剪应力分布、泥沙不淤积临界断面的底部垂向紊动强度和射流强度与泥沙防淤尺度的关系。得出了射流影响区水流紊动能随距离的衰减规律和保持泥沙不淤积所需的水流临界紊动强度。统计分析了射流强度与紊动能的变化关系。根据泥沙悬浮理论和射流紊动输沙机理，建立了水射流局部无泥沙淤积长度经验计算式，并以不同特性泥沙的射流输沙实验资料对所建立的计算公式进行了验证，二者吻合良好。     

横流中射流及其温度标量输运大涡模拟

将动力拟序涡黏性亚格子应力模型拓展到温度标量亚格子模型中,数值模拟了横流条件下有、无温度标量场作用的射流,得到的横流条件下浮力射流的温度和速度分布与Anwar的试验值吻合一致。在此基础上,分析了有、无温度标量场作用下射流回流区域大小和射流轨迹线特性,对比分析了回流区域内涡心和分离点处湍动能和耗散率、拟涡能以及边界层处拟序结构等湍流特性。计算结果表明:温度场的作用使射流的回流区域增大,射流速度轨迹线高度增加,回流区域内湍流的湍动能增加,边界处拟序结构的周期性不如无温度场时明显。     

EXPERIMENTAL MEASUREMENT AND NUMERICAL SIMULATION FOR FLOW FIELD AND FILM COOLING EFFECTIVENESS IN FILM-COOLED TURBINE

Numerical simulation of three-dimensional flow field and film cooling effectiveness in film-cooled turbine rotor and stationary turbine cascade were carried out by using the k - ε turbulence model, and the predictions of the three-dimensional velocities were compared with the measured results by Laser-Doppler Velocimetry (LDV). Results reveal the secondary flow near the blade surface in the wake region behind the jet hole. Compared with the stationary cascade, there are the centrifugal force and Coriolis force existing in the flow field of the turbine rotor, and these forces make the three-dimensional flow field change in the turbine rotor, especially for the radial velocity. The effect of rotation on the flow field and the film cooling effectiveness on the pressure side is more apparent than that on the suction side as is shown in the computational and measured results, and the low film cooling effectiveness appears on the pressure surface of the turbine rotor blade compared with that of the stationary cascade.     

THEORETICAL AND EXPERIMENTAL INVESTIGATIONS OF ENTRAINED AND TRANSPORTED CHARACTERISTICS OF SUBMERGED JET

This paper presents entrainment mechanism, and transported and diffusion characteristics at the point of entry of submerged jet. The profiles of both velocity and concentration within the air water mixing layer were theoretically deduced. And the comparisons between theoretical values and measured data were made. Results show that the velocity profile within the air water mixing layer exhibits a form of error function. The concentrations of air entrainment in the internal and external regions of ai~water mixing layer correspond to Gaussian distribution.     

CHARACTERISTICS OF CORRELATION AND SPECTRUM BETWEEN WALL FLUCTUATING PRESSURE AND FLUCTUATING VELOCITY OF IMPINGING JET

The correlation, the spectrum and the turbu-lent scale between wall fluctuating pressure and fluctuating ve-locity, on the bed of plunging pool under the action of single and twin impinging jet, are investigated in the paper by using 2-D LDA and the dynamic pressure scanning system of multi-ple points. It is found that the cross correlation between the horizontal fluctuating velocity and the fluctuating pressure of twin jet is bigger than that of sinlge jet, and the spectrum be-tween horizontal fluctuating velocity and fluctuating pressure obviously has approximately dominant frequency. The rela-tionship between the fluctuation pressure coefficient on wall and the turbulent intensity near the wall can be described with logarithmic curve.     

静止环境中垂直平面浮力射流稳定性与混合特性数值研究

针对不同的射流参数和环境流体参数下的有限深平面垂直射流，采用混合有限分析法对近区以稳定浮力表面层形式排放和由于近区漩涡产生二次吸附的非稳定排放两种流动形态的混合流体的流速场和温度场进行了数值模拟。结果表明近区排放稳定性主要取决于排放佛汝德数和相对淹没度，而与受纳水体的远区几何形状无关；受纳水体的远区几何形状只对排放水体的混合性质产生影响，这一点对非稳定排放尤其显著。所得结果与Jirka和Harleman的理论分析和试验结果十分吻合，说明所采用数值方法可对平面浮力射流的流动现象进行完整的预报。     

Large eddy simulation of turbulent flow structure and characteristics in an annular jet pump

The large eddy simulation(LES) of the flow characteristics in an annular jet pump(AJP) is conducted, and the flow characteristics are systematically analyzed from both time-averaged and instantaneous aspects. The jet expansion, the velocity distribution and the energy are considered to analyze the time-averaged evolution of the flow field in the AJP. The transient flow characteristics can also be acquired from the analysis of the turbulence intensity and the Reynolds stress. The simulation demonstrates that in the time-averaged characteristics, the potential cores increase linearly with the increase of the flow ratio. With the flow development, the jet half-width gradually increases and the residual energy coefficient decreases. Compared with the distribution of the time-averaged axial velocity, that of the instantaneous velocity is more complex and disorderly. The high intensity of the axial turbulence mainly occurs in the mixing layer and the near-wall regions of the diffuser. The annular distribution of the Reynolds stress is mainly in the mixing layer and the recirculation region. There is a low-stress zone between the mixing layer and the high-stress region in the wall-boundary layer. The intensity of the spanwise vortexes is larger than that of the streamwise vortexes, and therefore, the former make greater contribution to the total vorticity. This research provides a better understanding of the flow characteristics in the AJP.     

NUMERICAL SIMULATION OF 3-D TURBULENT FLOWS OF PLUNGE POOL AND ENERGY DISSIPATION ANALYSIS

A 3-D numerical model for simulating the complicated turbulent flows was developed and the code was made. A numerical calculation of the plunge pool of Laxiwa project in China was carried on. Those 3-D distributions of velocity,pressure on bottom wall,turbulence kinetic energy and turbulence energy dissipation rate are revealed in detail and the detailed flow patterns of plunge pool were shown. By studying on the characteristics of turbulent diffusion and energy dissipation,the calculated results show that the major turbulence and energy dissipation are taken place near the axis of water jet. The calculated results also indicated that the calculated maximum impact pressures on the bottom wall of the plunge pool have a good agreement with those obtained by physical hydraulic model test.     

NUMERICAL STUDY ON TURBULENT COUNTER-GRADIENT-TRANSPORT PHENOMENA IN ASYMMETRIC TURBULENT CHANNEL FLOW

1 .　BRIEFINTRODUCTIONTOCGTPHENOME NAINTURBULENCETurbulence ,prevalentinnature ,isofgreatimportanceinengineeringprojects .Asathree di mensionalunsteadynonlinearrandommotion ,oneofbasiccharacteristicsofturbulentflowisitsstrongerdiffusingeffectthanlaminarflow ,bywhichtheotherturbulentcharacteristicsaredeter mined .AccordingtoFourier’stheory ,turbulenttransportiscommonlyinthesamedirectionasgra dient .However ,thereareCGTphenomenaoccur ringincertainregionsofcomplexflows ,suchas…