Confined Submerged Jet Impingement Boiling of Subcooled FC-72 over Micro-Pin-Finned Surfaces

Heat transfer characteristics of confined submerged jet impingement boiling of air-dissolved FC-72 on heated micro-pin-finned surfaces are presented. The dimension of the silicon chips is 10 × 10 × 0.5 mm³ (length × width × thickness) on micro-pin-fins with the four dimensions of 30 × 30 × 60 μm³, 50 × 50 × 60 μm³, 30 × 30 × 120 μm³, and 50 × 50 × 120 μm³ fabricated by using the dry etching technique. For comparison, experiments of jet impinging on a smooth surface were also conducted. The results have shown that submerged jet impingement boiling gives a large heat transfer enhancement compared with pool boiling, and all micro-pin-fins showed better heat transfer performance than a smooth surface. The effects of jet Reynolds number, jet inlet subcooling, micro-pin-fins, and nozzle-to-surface distance on jet impingement boiling heat transfer were explored. For micro-pin-fins, the maximum allowable heat flux increases with jet Reynolds number and subcooling. The largest value of the maximum allowable heat flux of micro-pin-fins by submerged jet impingement boiling is 157 W/cm², which is about 8.3 times as large as that for the smooth surface in pool boiling. Also, Nusselt number has a strong dependence on Reynolds number.     

Numerical Analysis of Jet Impingement Heat Transfer at High Jet Reynolds Number and Large Temperature Difference

Jet impingement heat transfer from a round gas jet to a flat wall was investigated numerically for a ratio of 2 between the jet inlet to wall distance and the jet inlet diameter. The influence of turbulence intensity at the jet inlet and choice of turbulence model on the wall heat transfer was investigated at a jet Reynolds number of 1.66 × 10⁵ and a temperature difference between jet inlet and wall of 1600 K. The focus was on the convective heat transfer contribution as thermal radiation was not included in the investigation. A considerable influence of the turbulence intensity at the jet inlet was observed in the stagnation region, where the wall heat flux increased by a factor of almost 3 when increasing the turbulence intensity from 1.5% to 10%. The choice of turbulence model also influenced the heat transfer predictions significantly, especially in the stagnation region, where differences of up to about 100% were observed. Furthermore, the variation in stagnation point heat transfer was examined for jet Reynolds numbers in the range from 1.10 × 10⁵ to 6.64 × 10⁵. Based on the investigations, a correlation is suggested between the stagnation point Nusselt number, the jet Reynolds number, and the turbulence intensity at the jet inlet for impinging jet flows at high jet Reynolds numbers.     

Experimental Study on Jet Impingement Boiling Heat Transfer in Brass Beads Packed Porous Layer

Jet impingement boiling has been widely used in industrial facilities as its higher heat transfer coefficient(HTC) and critical heat flux(CHF) can be achieved in comparison with the pool boiling. By covering beads packed porous layer on the heated wall surface, the enlarged heat transfer area and rise of nucleation sites for boiling occur, thus, the heat transfer performance of boiling can be enhanced. For the jet impingement boiling with brass bead packed porous layers, the heat transfer perfor...     

液体射流泵喷嘴长径比的数值分析

液体射流泵的工作喷嘴一般采用锥直形喷嘴,锥直形喷嘴出口直段的长度与喷嘴出口直径之比即喷嘴长径比,是射流泵的重要几何参数。为了研究喷嘴长径比对液体射流泵性能的影响,采用Realizableκ-ε模型对不同长径比的射流泵内部流动进行三维数值模拟。结果表明,在射流泵的流量比小于0.5时,不同喷嘴长径比所对应的射流泵效率曲线差别不大;在流量比大于0.5时,以射流泵效率为判据,喷嘴长径比范围为0.250～1.000的射流泵性能较好;不同喷嘴长径比对应的射流泵壁面剪切应力相差不大。从湍流耗散率、喷嘴出口断面收缩、核心区长度等方面考虑,喷嘴长径比范围为0.250～1.000的射流泵性能较好。     

液滴撞击液膜动力学特性的FTM模拟

采用界面追踪法(front-tracking method)对液滴撞击液膜动力学特性进行数值模拟,通过撞击后的形态演变及内部物理场信息分析,研究了韦伯数和无量纲液膜厚度对界面运动过程的影响,并阐述了撞击过程中形成卷吸现象的机理。研究表明,液滴撞击之后,会在颈部区域产生小射流,该射流是后期水花形成的基础;水平方向上,在撞击影响不到的区域压力不变化,而在射流形成处的颈部附近存在局部压差;液滴撞击液膜时其间的气体层被压缩,在流体黏性和剪切力的作用下,压力高的气层中的气体逃逸速度减慢,从而形成卷吸现象。     

阵列射流冲击冷却换热特性的数值研究

运用数值计算的方法对不同流动取向的多排孔冲击射流冷却特性进行了三维模拟,并对有初始横向流的多排孔冲击射流冷却特性进行了数值研究,揭示出射流雷诺数、流动方向、初始横向流对冲击冷却传热特性的影响规律。结果表明:研究范围内,射流雷诺数越大,冲击靶面换热效果越好;冲击腔室两端都设为出口时努赛尔数峰值所对应的射流驻点区向下游偏移最小且换热效果最好;当横流雷诺数与射流雷诺数之比大于0.5之后,有横流时的冲击射流冷却局部努赛尔数比无横流时有较为显著下降。     

Confined Boiling Heat Transfer,Two-Phase Flow Patterns,and Jet Impingement in a Hele-Shaw Cell

ABSTRACT

Experiments were carried out to study heat transfer and two-phase flow patterns during boiling in a Hele-Shaw cell filled with pure water vapor at atmospheric pressure and with a central inlet of a liquid jet. The Hele-Shaw cell was based on a circular copper rod surface and a polycarbonate plate permitting optical access and thus high-speed cinematography. The diameter of the heated copper rod was 10 mm, the jet diameters were 0.5 and 1 mm, and spacing was varied between 50, 100, and 200 μm. The heat was applied through 4 cartridge heaters with a maximum heat flux of 327 W/cm². Results showed how high-volume flow rates for the liquid jet led to jet impingement heat transfer while low flow rates led to a Hele-Shaw flow boiling system. The relationship between the volume flow rate and the temperature difference differed significantly between these two regimes. Different flow patterns and evaporation fronts were observed using high-speed cinematography. They strongly depended on jet properties, applied heat flux, and gap spacing. The efficiency of the Hele-Shaw flow boiling system during high heat flux levels was attributed to high interface velocities, combined with viscous fingering at the interface. This combination led to high wetting rates with substantial microlayer evaporation. Good results regarding the heat transfer and the pressure drop were obtained with the final configuration of a 10-mm copper rod diameter, a jet diameter of 1 mm, and a spacing of 0.1 mm. A rather surprising observation was the existence of a stable rotation of an evaporating liquid jet in the Hele-Shaw boiling chamber. The driving mechanism for the rotation with a frequency of 105 Hz was the rapid microlayer evaporation at the rear side of the rotating liquid jet.     

Free Liquid Jet Impingement from a Slot Nozzle to a Curved Plate

This article explores the heat transfer characteristics of a free liquid jet discharging from a slot nozzle and impinging vertically on a curved cylindrical shaped plate of finite thickness. Computations were done for Re = 500–1800, β = 0.75–3, R _i /d _n  = 4.16–16.66, b/d _n  = 0.08–1.5, and d _n  = 0.3–2.4 mm. Results are presented for dimensionless solid–fluid interface temperature, dimensionless maximum temperature in the solid, and local and average Nusselt numbers. The local Nusselt number increases with Reynolds number. Decreasing the nozzle width increases the local heat transfer coefficient. Decreasing the nozzle to target spacing or plate thickness or plate inner radius of curvature all enhances the Nusselt number.     

动力锂电池组非稳态射流强化换热数值模拟

为动力锂电池组设计了通风冷却系统,在控制总通风量的前提下,研究了非稳态射流对动力锂电池组的冷却效果,针对26650型锂电池组射流冲击方案进行数值模拟分析,揭示非稳态射流送风周期、送风变化量对电池组温升和温度均匀性的影响。研究结果表明:冲击射流的非稳态特性改善了电池组温度场的均匀性,对电池组总温升影响不明显。     

Convective Heat Transfer from a Thick Hemispherical Plate during Free Liquid Jet Impingement

Convective heat transfer during free liquid jet impingement on a hemispherical solid plate of finite thickness has been examined. The model included the entire fluid region (impinging jet and flow spreading out over the hemispherical surface) and solid plate as a conjugate problem. Solution was done for both isothermal and constant heat flux boundary conditions at the inner surface of the hemispherical plate. Computations were done for jet Reynolds number (Re _j ) ranging from 500 to 2,000, dimensionless nozzle-to-target spacing ratio (β) from 0.75 to 3, and for various dimensionless plate thicknesse-to-nozzle diameter ratios (b/d _n ) from 0.08 to 1.5. Results are presented for local Nusselt number using water (H₂O), flouroinert (FC-77), and oil (MIL-7808) as working fluids, and aluminum, Constantan, copper, silicon, and silver as solid materials. It was observed that plate materials with higher thermal conductivity maintained a more uniform temperature distribution at the solid–fluid interface. A higher Reynolds number increased the Nusselt number over the entire solid–fluid interface.     

阵列射流冲击冷却流场与温度场的数值模拟

采用数值模拟方法对冲击冷却的流动和传热过程进行了三维数值研究。特别研究了在冲击孔叉排方式下,相邻孔间距、冲击距离以及射流入口雷诺数对冲击表面冷却流动传热特性的影响规律。     

喷嘴距离和喷嘴角度对油膜附壁的影响

为研究进气道燃油喷射汽油机内喷嘴距离和喷嘴角度对燃油碰壁形成的附壁油膜的影响,采用激光诱导荧光法,研究了不同喷嘴距离和喷嘴角度下的附壁油膜厚度二维分布规律.结果表明,喷嘴角度越小,附壁油膜厚度较大的区域越向下游移动,油膜较厚区域的范围越大,油膜的最大厚度越小.喷嘴距离越大,附壁油膜的厚度越薄.     

平板滞止区内饱和液体喷流沸腾的临界热流密度

对高温平板滞止区内饱和液体的圆形喷流冲击沸腾的临界热流密度进行了系统的稳态实验研究。考察了不同液体、流速和喷流直径等系统条件对喷流沸腾临界热流密度的影响。建立了一个预示临界热流密度的半理论半经验型方程,其基本形式采用过去的研究结果,方程系数由本研究的实验数据拟合得到。研究结果证明,饱和液体喷流冲击沸腾的临界热流密度取决于液体物性、滞止冲击速度和喷流直径。本研究得到的半理论半经验公式在广泛的实验范围内能很好的预示喷流沸腾的临界热流密度。     

Numerical Investigation of Jet Impingement Cooling of a Flat Plate with Carbon Dioxide at Supercritical Pressures

Confined round jet impingement cooling of a flat plate at constant heat flux with carbon dioxide at supercritical pressures was investigated numerically. The pressure ranged from 7.8 to 10.0 MPa, which is greater than the critical pressure of carbon dioxide, 7.38 MPa. The inlet temperature varied from 270 to 320 K and the heat flux ranged from 0.6 to 1.6 MW/m². The shear-stress transport turbulence model was used and the numerical model was validated by comparison with experimental results for jet impingement heating with hot water at supercritical pressures. Radial conduction in the jet impingement plate was also considered. The sharp variations of the thermal-physical properties of the fluid near the pseudocritical point significantly influence heat transfer on the target wall. For a given heat flux, the high specific heat near the wall for the proper inlet temperature and pressure maximizes the average heat transfer coefficient. For a given inlet temperature, the heat transfer coefficient remains almost unchanged with increasing surface heat flux at first and then decreases rapidly as the heat flux becomes higher due to the combined effects of the thinner high specific heat layer and the smaller thermal conductivity at higher temperature.     

脉冲液体射流泵能量平衡的数值研究

运用能量平衡分析原理,根据脉冲液体射流泵主要流动部件的能量损失压力比公式,利用脉冲液体射流泵性能数值计算模块,对脉冲液体射流泵能量平衡进行了数值研究,分析了主要流动部件的能量损失变化及其对脉冲液体射流泵性能的影响,并与恒定液体射流泵的能量损失压力比、性能及效率进行了对比。结果表明,脉冲射流是提高射流泵传能、传质效率的有效途径。     

Recent Trends in Computation of Turbulent Jet Impingement Heat Transfer

A review of the current status of computation of turbulent impinging jet heat transfer is presented. It starts with a brief introduction to flow and heat transfer characteristics of jet impinging flows considering the simplest jet impinging geometry: normal impingement of a single jet into a flat surface. Subsequently, a review of recent computational studies related to the same geometry is presented. The effects of different subgrid scale models, boundary conditions, numerical schemes, grid distribution, and size of the computational domain adopted in various large eddy simulations of this flow configuration are reviewed in detail. A review of direct numerical simulation of the same geometry is also presented. Further, some recent attempts in Reynolds-averaged Navier–Stokes modeling of impinging flows are also reviewed. A review of computation of other complex impinging flows is also presented. The review concludes with a listing of some important findings and future directions in the computation of impinging flows.     

三维横向紊动射流流场结构的数值分析

对横向紊动射流流场结构、流动机理的研究具有重要的学术意义．同时对解决工程应用中存在的许多问题具有指导作用。利用RNG模型对横流中单股紊动射流流场的流动特性进行了数值模拟。运用SIMPLEC算法求解了适体坐标系下的控制方程．壁面函数法处理近壁区流动。得到了射流与主气流速度比为2和4的流场。结果表明：较大的射流速度对主气流流场影响大；射流内部已形成明显的反向涡旋对(CVP)；射流喷孔上游处出现了主气流向喷孔内部流动的趋势；射流喷孔背风侧存在尾迹区。图7表1参10     

Numerical Simulation of Liquid Film Evaporation in Circular and Square Microcavities

Numerical simulations are performed for liquid film evaporation in circular and square microcavities, which occurs frequently in ink-jet fabrication. The conservation equations of mass, momentum, energy, and mass fraction in the liquid and gas phases are solved using a sharp-interface level-set method, which is modified to include the effects of evaporation and dynamic contact angles. Three-dimensional computations for a square cavity are efficiently carried out in a reduced domain by introducing an effective mass transfer length for the truncated region. The liquid film evaporation pattern is observed to depend strongly on the dynamic contact angles and cavity geometry.     

带扩张段构型超声速气流中横向射流数值模拟

针对带扩张段构型的发动机燃烧室,采用欧拉-拉格朗日仿真方法研究喷注方式、喷孔参数及隔离段燃烧室构型的改变对于射流雾化效果的影响,用以更好地指导发动机设计.结果表明,在保证发动机总体流量不变的条件下,喷孔孔径减小或者喷孔总数量减少使得液气动量通量比增大,有利于同时增大单孔射流穿透深度以及液滴展向宽度.贫燃工况下如当量比为...     

Direct and Inverse Methods for an Air Jet Impingement

The reconstruction of the distribution of the heat transfer coefficient (HTC) for the air jet impinging of a solid object is discussed. After an optimal turbulence model is selected, computational fluid dynamics is used to obtain detailed information about the HTC produced by a jet and to validate its invariability in time. Two inverse models of the temperature field in the solid impinged by the jet are derived as a linear combination of known, constant, or linear auxiliary fields. Simultaneous minimization of the discrepancies between the temperatures measured by an infrared camera and both inverse models produces the distribution of the HTC for various jets configurations.