主支管动量比对T型管道流体混合过程影响

采用大涡模拟(large-eddy simulation,LES)的方法对T型管道内主管与支管不同动量比的流体混合过程的流动情况进行了数值模拟,采用时均值和均方根值来描述速度的平均大小和波动强度。通过改变主管和支管的速度比即动量比,将流体分为三类:碰撞射流、偏射流和壁面射流,研究其对速度的平均值和波动的影响,并研究其所反映的惯性力对流动的影响。该研究揭示了流体混合过程中动量比对波动的影响规律,对预测和校核管壁疲劳失效具有重要的指导意义。     

On the calculation of heat,mass and momentum transport in coaxial jets and mixing layers

This communication deals with the determination of mass, momentum and heat transport in turbulent mixing layers and with the determination of momentum transport in concentric round jets. Mixing length, k/? and k/ω models are employed in the calculations. The constants appearing in these models are evaluated to yield the correct spreading rate, mean axial velocity, concentration and temperature profiles. A single-point probability density function (pdf) has been employed to calculate heat and mass transport in mixing layers. It is shown that the concentric jet mean velocity profiles are accurately predicted if the constants multiplying the production terms in the ?^? and ω^? equation have values of 1.52 and 1.50. These constants have to be taken equal to 1.44 and 3.80 for mixing layers. The calculated turbulent Schmidt/Prandtl number is 0.70 for mixing layers.     

An experimental study on the mixing of inclined heated jets with a cold crossflow

An experimental study is presented for the mixing of one- and dual-line heated jets injected at 60° angle with x-axis into a cold crossflow in a rectangular channel. Measurements of the mean temperature, velocity, and turbulence intensity together with the flow visualization were performed. Self-similar forms for the dimensionless vertical temperature profiles were found. Parametric variations characterizing the mixing processes of the temperature and velocity fields were examined and correlated in terms of the momentum flux ratio and downstream distance. Results show that both the thermal and velocity penetration depths increase with increasing momentum flux ratio and downstream distance. The turbulence intensity is strong within the region of jet half-width, and the maximum value occurs at a point close to the jet velocity trajectory.     

LES analysis of flow and turbulent mixing in an unsteady jet

The flow and mixing process of unsteady jets are fundamentally analyzed by large eddy simulations. The effects of nozzle velocity and turbulence intensity on the turbulent eddy structure and mixing process between the nozzle fluid and ambient fluid were investigated. The results show that a toroidal‐shaped vortex, which emerges around the jet tip, primarily accelerates the entraining flow. Also, increasing the turbulence intensity in the nozzle encourages mixing in the jet without changing the jet‐contour. Furthermore, when the rise‐up time of the initial nozzle velocity is elongated, turbulent mixing is suppressed. © 2007 Wiley Periodicals, Inc. Heat Trans Asian Res, 36(5): 303–313, 2007; Published online in Wiley InterScience ( www.interscience.wiley.com ). DOI 10.1002/htj.20158     

Experimental and numerical investigation of turbulent jets issuing through a realistic pipeline geometry: Asymmetry effects for air,helium, and hydrogen

Experiments and numerical simulations were conducted to investigate the dispersion of turbulent jets issuing from realistic pipe geometries. The effect of jet densities and Reynolds numbers on vertical buoyant jets were investigated, as they emerged from the side wall of a circular pipe, through a round orifice. Particle image velocimetry (PIV) and planar laser-induced fluorescence (PLIF) techniques were employed simultaneously to provide time-averaged flow velocity and concentrations fields. Large eddy simulation (LES) was applied to provide further detail with regards to the three-dimensionality of air, helium, and hydrogen jets. These jets were always asymmetric and found to deflect about the vertical axis. The deflection was influenced by buoyancy, where heavier gases deflected more than lighter gases. Significant turbulent mixing was also observed in the near field. The jets from realistic pipe geometries experienced faster velocity decay and asymmetric jet spreading compared to round jets. These findings indicate that conventional round jet assumptions are, to some extent, inadequate to predict gas concentration, entrainment rates and, consequently, the extent of the flammability envelope of realistic gas leaks.     

支管结构对T型管内流体混合过程热波动影响

通过CFD计算流体软件FLUENT,分别对支管无附加结构及支管有附加结构直管、渐扩管、减缩管四种结构的T型管内冷热流体混合过程进行了大涡模拟,获得了管道内部的瞬时温度。将各结构温度云图与速度矢量图、无量纲时均温度及无量纲均方根温度进行了对比。数值结果表明,附加结构的添加使管内流体流型由冲击射流变为偏转射流,显著减小了T型管壁上的温度波动;缩管结构的无量纲均方根值比其他附加结构更小,表明缩管结构更适合用以减小管壁的温度波动。     

Confined swirling jet impingement onto an adiabatic wall

Impinging swirling jets generate interesting flow fields and depending on the magnitude of the swirl velocity, circulation cells develop in the region close to the solid wall. Moreover, axial momentum of the jet is influenced by the magnitude of the swirl velocity. This, in turn, results in considerable entropy generation in the flow field. In the present study, confined swirling jet impingement onto an adiabatic wall is investigated. The flow and temperature fields are computed numerically for various flow configurations. Different jet exit velocity profiles are considered and their effects on the flow field are examined. The entropy production due to different flow configurations is computed and the irreversibility ratios due to fluid friction and heat transfer are determined. It is found that the jet axis tilts towards the radial direction as swirl velocity increases and reducing the velocity profile number enhances the entropy generation due to heat transfer. The irreversibility ratio variation with the velocity profile number behaves opposite for the fluid friction and heat transfer.     

双平行平面射流输运特性研究

平行射流输运特性研究具有较重要的理论意义和工程价值,对水平浓淡煤粉燃烧也有较重要的意义。本文实验研究了双平行平面射流动量、能量和质量输运,结果表明：速度分布表现为双射流相互吸引并最终汇合成单一射流;温度分布反映了冷射流为加热射流所卷吸;浓度分布反映了惯性力的占优作用。三种变量分布反映了动量、能量和质量输运性质的根本性区别。     

Large-eddy simulations (LES) of temperature fluctuations in a mixing tee with/without a porous medium

Temperature fluctuations in a mixing tee were simulated with and without a porous media in FLUENT using the LES turbulent flow model with the sub-grid scale (SGS) Smagorinsky–Lilly (SL) model with buoyancy. The normalized mean and fluctuating temperatures are used to describe the time-averaged temperatures and the time-averaged temperature fluctuation intensities. For the tee junction without the porous media, the predicted normalized mean temperature and temperature fluctuations compare well with previous experimental data. Comparison of the numerical results with the porous media with both experimental and numerical data without porous media shows that the porous media significantly reduces the temperature fluctuations. Moreover, analysis of the temperature fluctuations and the power spectrum densities (PSD) at the locations having the strongest temperature fluctuations in the tee junction shows that the porous media significantly reduces the thermal fatigue effects and can be useful in various structures such as tee junctions, elbows, piping systems.     

Velocity and temperature profiles in a wall jet

Conditions approximating those of the wall jet have been obtained by operating a system, involving tangential air injection into a turbulent boundary layer, with very low values of the free stream velocity. Under such conditions the flow is essentially produced by the injected air and measurement of the velocity profiles shows correspondence to the theory for the turbulent wall jet. With some alternation of the eddy diffusivity of that theory the measured temperature profiles can also be predicted and these, together with the velocity profiles, are shown to agree generally with the measured values of the adiabatic wall temperature. The measured heat transfer coefficients are related to the hydrodynamic characteristics by a formulation of the Colburn type.     

Étude expérimentale d'une interaction de jets obliques avec un écoulement transversal compressible. I. Effets de la compressibilité en régime subsonique sur les champs aérothermiques

Experimental study of inclined jets cross flow interaction in compressible regime. I. Effect of compressibility in subsonic regime on velocity and temperature fields. The results of the investigation of the interaction of a row of jets with a compressible cross flow are compared with their counterpart obtained in incompressible regime. The comparison reported here focuses on the flow field resulting from the interaction above and at the wall. The velocity and temperature fields are measured respectively by laser Doppler velocimetry and thermocouple probes. The wall temperature distributions are measured using an infrared camera. The experiments are performed for cross flow Mach numbers of 0.72 and 0.1 for respectively the compressible and incompressible regimes with almost the same injection rate (R=0.50 and 0.6). Significant differences are noticed between the two flow fields in particular on the vertical development of the jets in the cross flow and on the turbulent diffusion. The jet penetration is found to be higher in the compressible regime with less interaction between the jets. The comparison also shows that the wall heat transfer modifications induced by the jets are less pronounced in the compressible case as a result of the higher penetration of the jets. These results show that neither the mass flux ratio nor the momentum ratio are good candidates for extrapolation of the cooling efficiency from the incompressible case to the real compressible case as encountered in the practical applications.     

Wall shear stress measurements and parametric analysis of impinging wall jets

This paper investigates the influence of some governing parameters on the near wall characteristics of a circular impinging jet onto a smooth flat plate. Laser Doppler anemometry (LDA) is used to characterize the mean and turbulent fields including the wall shear stress. The experiments were conducted at one nozzle-to-plate space (H/D = 2) and Reynolds number of 47,100. The work makes a parametric analysis of impinging jets based on (i) conventional parameters that include the nozzle diameter, the nozzle-to-plate distance and the bulk velocity of the jet and (ii) gross parameters like the jet momentum flux. Parametrization schemes based on conventional quantities are shown to be very sensitive to the particular choice of reference quantity, resulting in functional behaviours that can be represented through either power law or linear expressions. On the other hand, it is shown that the jet momentum flux and the kinematic viscosity suffice to determine the mean and fluctuating flow parameters, even in the initial region of wall jet development (1 < r/D < 5). With the latter choice, the streamwise variation of the maximum mean velocity and maximum Reynolds longitudinal stress are shown to decay according to power law expressions. A particular near wall parametrization scheme for the mean velocity profile that resorts to a scaling procedure based on the stream-wise evolution of the flow characterized by its maximum velocity is also presented. Higher-order moments of the velocity fluctuations are discussed.     

半封闭狭窄通道内甲烷/空气预混火焰传播不稳定性实验研究

针对贫油预混预蒸发燃烧室主燃级中横喷液雾现象进行研究,综合考虑RP-3航空煤油横喷液雾的雾化、蒸发和自燃过程构建自燃预测模型,基于CH基团随时间的变化规律对自燃延迟时间进行预测。结合试验测试结果对模型进行校验,并进一步分析温度、压力、流速、射流动量比等变量对自燃延迟时间的影响规律。结果表明：对于直射式喷嘴形成的横喷液雾,其下游的油气分布主要受射流动量比和流动速度的影响,射流动量比决定了液雾的总体油气比,流动速度则主要影响液滴的粒径及其蒸发时间;随着压力、射流动量比及气流速度的增加,自燃延迟时间均会缩短,相比于预混燃料液雾的自燃延迟时间受负温度效应的影响较弱。     

Interaction of Two Unequal Turbulent Jets with Different Temperature

This paper examines the control and heat transfer process of the mixing of a strong jet and a weak jet. The control of the jet diffusion may be required in many devices such as cooling systems, combustors, gas turbines, heating or cooling surfaces, cooling problem techniques, mixing flows, etc. A steady three‐dimensional problem is solved by the finite volume method using RANS modeling. The validation confirms that both RSM and k‐ε realizable models predict more accurately this flow configuration than the standard k‐ε model. A parametric study is conducted on the basis of ratios of the momentum of the two jets. Due to the Coanda effect, the deviation of the weak jet has been highlighted for several momentum ratios. In the fully developed flow region, after the confluence point, the structure of a single jet flow is recovered. However, the point of maximum velocity is shifted toward the side of the strong jet. For a given velocities ratio of 0.25, the temperatures ratio between the two jets is checked. The location of maximum temperature of the jet is almost constant for diverse values of 0.8 ≤ λ_T ≤ 1. The location of the point of maximum temperature varies linearly according to λ_T.     

多孔介质对冷热流体横向射流混合过程热波动的影响

运用流固耦合方法建模,应用FLUENT计算软件平台对填充有多孔介质的T型连接方形管道内冷热流体横向射流混合过程的流动和热传递进行大涡模拟,采用了Smagorinsky-Lilly亚格子模型,获得了瞬时速度和温度分布.结果表明,填充多孔介质能够有效减少T型连接管道中冷热流体横向射流混合的温度和速度波动.固体骨架的导热率较...     

Modeling study on the characteristics of laminar and turbulent argon plasma jets impinging normally upon a flat plate in ambient air

Modeling study is performed to compare the flow and heat transfer characteristics of laminar and turbulent argon thermal-plasma jets impinging normally upon a flat plate in ambient air. The combined-diffusion-coefficient method and the turbulence-enhanced combined-diffusion-coefficient method are employed to treat the diffusion of argon in the argon–air mixture for the laminar and the turbulent cases, respectively. Modeling results presented include the flow, temperature and argon concentration fields, the air mass flow-rates entrained into the impinging plasma jets, and the distributions of the heat flux density on the plate surface. It is found that the formation of a radial wall jet on the plate surface appreciably enhances the mass flow rate of the ambient air entrained into the laminar or turbulent plasma impinging-jet. When the plate standoff distance is comparatively small, there exists a significant difference between the laminar and turbulent plasma impinging-jets in their flow fields due to the occurrence of a large closed recirculation vortex in the turbulent plasma impinging-jet, and no appreciable difference is found between the two types of jets in their maximum values and distributions of the heat flux density at the plate surface. At larger plate standoff distances, the effect of the plate on the jet flow fields only appears in the region near the plate, and the axial decaying-rates of the plasma temperature, axial velocity and argon mass fraction along the axis of the laminar plasma impinging-jet become appreciably less than their turbulent counterparts.     

燃气轮机燃烧室液雾自燃延迟时间预测方法

为减少一体化加力燃烧室内支板火焰稳定器高度与进口试验参数较高所导致的昂贵基础试验成本,采用经试验数据验证的数值计算方法,对不同高度的一体化模型加力燃烧室燃烧性能进行数值模拟,分析模型加力燃烧室高度变化和侧壁边界层效应对一体化加力燃烧室回流区、总压恢复系数以及燃烧效率的影响。在保持空间油雾场分布均匀与阻塞比一致的前提下,简化扇形加力燃烧室模型为矩形加力燃烧室模型,其中模型加力燃烧室高度H分别为200,150和100 mm,总长L=1 480 mm,宽B=125 mm。结果表明：模型加力燃烧室高度的降低对燃烧性能影响较小,其中回流率最大降幅为0.16%,总压恢复系数最大降幅为0.15%,燃烧效率的最大降幅为1.9%;模型加力燃烧室侧壁面边界的引入对燃烧性能影响较小,回流率、总压恢复系数最大降幅均小于1%,燃烧效率的最大降幅仅为0.7%;可以采用单支板火焰稳定装置降低高度的方法简化试验件设计。     

Numerical Analysis of Heat Transfer from a Moving Surface Due to Impingement of Slot Jets

Heat transfer from a moving surface with uniform wall temperature due to impingement of series of slot jets has been investigated numerically. In the present paper, transition–shear stress transport model has been used for numerical simulations, which can predict the heat transfer in laminar as well as turbulent flows. This model is adopted here to study the transport phenomenon and predict the transition from laminar to turbulent flow seamlessly under different surface velocities. The present model with stationary surface is validated with the correlation given by Martin for series of slot jets. It has also shown good agreement with existing data for both laminar and turbulent slot jets, and is further studied to understand the heat transfer under wide range of flow conditions and the effect of surface velocity on flow regime. The range of Reynolds number is from 100 to 5,000, whereas surface velocity varied up to six times the jet velocity at the nozzle exit. It has been observed that at high surface velocities the heat transfer from the moving wall is more than stationary case. The transition from laminar to turbulent regime is found to be starting at a Reynolds number of 400 and turns completely turbulent at a Reynolds number of 3,000. Q-criterion is used to confirm the transition zone by observing the breaking of vortices at higher Reynolds number.     

Large eddy simulation of highly turbulent under-expanded hydrogen and methane jets for gaseous-fuelled internal combustion engines

Burning hydrogen in conventional internal combustion (IC) engines is associated with zero carbon-based tailpipe exhaust emissions. In order to obtain high volumetric efficiency and eliminate abnormal combustion modes such as preignition and backfire, in-cylinder direct injection (DI) of hydrogen is considered preferable for a future generation of hydrogen IC engines. However, hydrogen's low density requires high injection pressures for fast hydrogen penetration and sufficient in-cylinder mixing. Such pressures lead to chocked flow conditions during the injection process which result in the formation of turbulent under-expanded hydrogen jets. In this context, fundamental understanding of the under-expansion process and turbulent mixing just after the nozzle exit is necessary for the successful design of an efficient hydrogen injection system and associated injection strategies. The current study used large eddy simulation (LES) to investigate the characteristics of hydrogen under-expanded jets with different nozzle pressure ratios (NPR), namely 8.5, 10, 30 and 70. A test case of methane injection with NPR = 8.5 was also simulated for direct comparison with the hydrogen jetting under the same NPR. The near-nozzle shock structure, the geometry of the Mach disk and reflected shock angle, as well as the turbulent shear layer were all captured in very good agreement with data available in the literature. Direct comparison between hydrogen and methane fuelling showed that the ratio of the specific heats had a noticeable effect on the near-nozzle shock structure and dimensions of the Mach disk. It was observed that with methane, mixing did not occur before the Mach disk, whereas with hydrogen high levels of momentum exchange and mixing appeared at the boundary of the intercepting shock. This was believed to be the effect of the high turbulence fluctuations at the nozzle exit of the hydrogen jet which triggered Gortler vortices. Generally, the primary mixing was observed to occur after the location of the Mach disk and particularly close to the jet boundaries where large-scale turbulence played a dominant role. It was also found that NPR had significant effect on the mixture's local fuel richness. Finally, it was noted that applying higher injection pressure did not essentially increase the penetration length of the hydrogen jets and that there could be an optimum NPR that would introduce more enhanced mixing whilst delivering sufficient fuel in less time. Such an optimum NPR could be in the region of 100 based on the geometry and observations of the current study.     

Experimental investigation of the high-temperature conversion of natural gas in a reactor with swirling jets

The swirling jet, unlike the straight-flow one, has a wide angle of expansion and high ejection capability, causing quick ignition and stable burning of fuel. It has been established that the use of powerful swirling jets strongly increases the pulsating component of the velocity, thereby increasing the speed of flame spreading in a gas flow.Since increasing the tubulence of a flow increases the number of turbulent eddies of smaller size, a remarkable decrease in chemical reaction time is expected in swirling jets as compared to straight-flow ones. In addition, the relative length of the mixing path in a swirling jet is almost three times greater than that in a straight-flow jet, indicating a greater capacity for heat and mass transfer in the swirling jet.To substantiate these considerations, an experimental investigation of the high-temperature partial oxidation of natural gas in a laboratory reactor with swirling jets was conducted without preliminary mixing of the reacting masses. Quite encouraging results have been obtained.