超临界CO_2在内螺纹管内换热特性研究

建立了外径为3 mm的内螺纹管三维实体模型,使用Fluent软件研究了在不同的进口雷诺数和操作压力下超临界二氧化碳在水平内螺纹管内的流动与传热特性。研究表明:不同截面局部换热系数和相同流体局部平均温度下的局部换热系数均随着冷却压力的增大而增大;相同流体局部平均温度下的局部换热系数随着进口雷诺数的增加而增大;不同冷却压力和进口雷诺数下,流体局部平均温度越接近超临界二氧化碳的临界点温度,局部换热系数也就越大。     

ZrO2纳米流体的对流换热系数测定及机理浅析

建立了测量圆管内纳米流体流动与传热性能的实验系统,测量了不同粒子浓度的ZrO2/水纳米流体在雷诺数为3 000～18 000范围内的管内对流换热系数以及不同位置处纳米流体对流换热系数的变化情况.实验结果显示,在液体中添加纳米粒子显著增大了液体的管内对流换热系数,例如,在相同雷诺数时,与纯水相比,如果纳米粒子的质量浓度从1.6%增大到4.1%,则纳米流体的对流换热系数增加的比例从1.09增大到1.2.此外,从颗粒的浓度、粒径两方面分析纳米流体强化传热的机理.     

水平微细圆管内膜状凝结换热特性的研究

实验研究了微细圆管内凝结换热特性,实验中采用四种不锈钢管,其内径范围为289-997μm。基于实验结果, 分析了换热温差、蒸汽进口雷诺数Rein和管径对管内膜状凝结换热系数的影响,发现温差对管内膜状凝结换热的影响很小, Nu随蒸汽进口雷诺数Rein增加而增大,随管径减小而降低,而对流换热系数随管径减小而显著增大。     

纳米流体对流换热的实验研究

建立了测量纳米流体对流换热系数的实验系统,测量了不同粒子体积份额的水-Cu纳米流体在层流与湍流状态下的管内对流换热系数,实验结果表明,在液体中添加纳米粒子增大了液体的管内对流换热系数,粒子的体积份额是影响纳米流体对流换热系数的因素之一。综合考虑影响纳米流体对流换热的多种因素,提出了计算纳米流体对流换热系数的关联式。     

波纹管管内层流流动和换热规律的实验研究及数值模拟

波纹管是近几年来被广泛采用的一种强化换热元件,对其管内的流动和换热规律进行研究具有十分重要的意义。本文通过实验和数值模拟的方法,对三种不同尺寸(φ=19 mm、25 mm、32 mm)的波纹管层流流动和换热进行了研究,发现存在一个临界的Re数,当Re数小于临界值时波纹管的换热性能不及对应的光管,随着Re数的增加,波纹管换热性能逐渐改善。     

微细管内超临界二氧化碳冷却换热研究

本文对超临界二氧化碳在微细管内冷却对流换热进行数值模拟研究,分析不同流动方向和管径大小对超临界二氧化碳对流换热的影响,考察管内局部流体温度、管壁温度以及无量纲温度分布的变化。湍流模型采用低雷诺数YS模型。研究表明,在LPV范围比较大的截面,超临界二氧化碳局部换热系数达到最大值,同时管内传热受流动方向和管径的影响均较大。     

微细管碳纳米管悬浮液强制对流换热实验研究

测量了水平微细圆管内蒸馏水和不同质量浓度的水基多壁碳纳米管纳米流体在低雷诺数下的强制对流换热特性。实验结果表明,与蒸馏水相比,纳米流体的对流换热系数显著提高,且随质量浓度和管内雷诺数的增大而增大;并且研究了流体管内流动阻力特性,得到的泊肃叶数f·Re值随着雷诺数的变化不明显,但纳米流体的f·Re值要明显小于纯水。     

波纹曲面气膜冷却特性数值模拟

本文对波纹曲面的气膜冷却特性进行数值模拟,主要研究了吹风比和主流雷诺数对有效温比和主流侧换热系数的影响.研究结果表明:波谷区域的冷却效果要明显优于波峰区域;有效温比受吹风比的影响较大,并随着吹风比的增大而增大;主流侧换热系数受主流雷诺数的影响较大,并随着主流雷诺数的增大而增大.     

电动汽车空调室外换热器空气侧流动换热模拟研究

采用数值模拟方法对室外微通道换热器翅片侧空气流动换热性能进行仿真计算, 探讨了在制冷工况下,不同百叶窗结构对微通道换热器空气侧传热及流动特性的影响. 结果表明j 因子的模拟结果与实验关联式之间的平均偏差在7.8% 以内,f 因子的平均误差在7.35 % 以内, 符合工程应用要求. 雷诺数较低时, 传热因子j 和阻力因子f 都随Fp 的增大而减小, 雷诺数较高时,Fp 对两者的影响不明显; 随着开窗角度增加换热器换热系数会呈现先增加后减小的趋势, 同时压降会随开窗角度的增大而有所升高.     

基于纳米磁流体微通道内流动换热性能研究

为探究磁场强度和肋片高度对微通道内Fe₃O₄-H₂O纳米磁流体流动换热性能的影响,采用数值模拟的方法,以开放式间断微通道热沉为研究对象,在雷诺数为200到500之间展开数值模拟研究,模拟微通道内流体工质流动换热过程。结果表明：进出口压降随雷诺数的增大而增大,且随着磁场强度的增大,压降的增大趋势愈显著;微通道的换热性能随着磁场强度的增大,呈现出先增大后减小的趋势;通过增加肋片高度,可以有效的提高热沉的传热性能。研究发现,开放型微通道综合换热性能优于封闭型,在所研究的参数范围内,微通道肋片高度达到0.9 mm时,综合换热性能和均温性最佳。     

波纹内翅片管换热与阻力特性的实验研究

本文研究了三组内翅片管的湍流流动与换热特性,拟合出所测参数范围内阻力和换热的实验关联式,并运用相同质量流量、相同泵功率、相同压降三种准则比较了不同组翅片管之间的强化传热效果。     

周期性波纹通道内换热与流动的数值研究

采用曲线坐标系下压力与速度耦合的SIMPLER算法,数值研究了一种紧凑换热器中波纹通道内周期性充分发展的层流流动与换热情况,流动Re数的范围为100~1100,Pr数为0.7.计算考察了不同波纹高度、波纹间距对流动与换热的影响,并对模型参数进行了性能评价.计算结果表明,整体Nu数及fRe数随着流动Re数的增加而增加.随着波纹高度的增加或波纹间距的减小,换热增强,特别是在高Re数下波纹高度的增加更加强化换热.最佳波纹高度和间距分别为1.15 mm和13 mm.     

高雷诺数下降液膜流动换热分析

本文分析了降液膜高雷诺数区域换热系数随液膜长度变化趋势,引出临界长度的概念。在较高雷诺数的湍流区,回流区的存在以及表面波的影响能有效地减少局部薄膜厚度并增加对流换热,流速的增加进一步强化换热,增加降膜整体传热系数。在高雷诺数区域,厚度形成的热阻超过回流的增强作用,而使换热削弱。液膜小于临界长度L换热系数随长度增长而增加,大于L换热系数随液膜增长而减小。     

EXPERIMENTAL STUDY OF HEAT TRANSFER FROM A DISCRETE SOURCE TO A CIRCULAR LIQUID JET WITH ANNULAR COLLECTION OF THE SPENT FLUID

This study reports an experimental investigation of evaporative heat transfer and pressure drop of R-134a flowing downward inside vertical corrugated tubes with different corrugation pitches. The double tube test section is 0.5 m long with refrigerant flowing in the inner tube and hot water flowing in the annulus. The inner tubes are comprised of one smooth tube and three corrugated tubes with different corrugation pitches of 6.35, 8.46, and 12.7 mm. The test runs are performed at evaporating temperatures of 10°C, 15°C, and 20°C; heat fluxes of 20, 25, and 30 kW/m²; and mass fluxes of 200, 300, and 400 kg/m²s. The experimental data obtained from the smooth tube are plotted with flow pattern map for vertical flow. Comparisons between smooth and corrugated tubes on the heat transfer and pressure drop are also discussed. It is observed that the heat transfer coefficient and frictional pressure drop obtained from the corrugated tubes are higher than those from the smooth tube. Furthermore, the heat transfer coefficient and frictional pressure drop increase as the corrugation pitch decreases. The maximum heat transfer enhancement factor and penalty factor are up to 1.22 and 4.0, respectively.     

格芯夹层结构散热性能的数值计算评估

为评估格芯夹层结构的传热性能以及代替传统的板式肋片结构应用于汽车散热系统中的可能性,文章对几种典型的格芯夹层结构（如kagome lattice,tetrahedral lattice和pyramidal lattice）和板式肋片（corrugated plate）结构实施了一系列的三维数值计算评估.通过对比相同Reynolds数下的传热系数和相同泵功率下的局部Nusselt数来评估各组结构的传热性能.结果显示,相同Reynolds数条件下,各组格芯夹层结构的传热系数较板式肋片结构均有提高,同时摩擦阻力也大幅度增大.在相同泵功率条件下,由于板式肋片结构所受形阻基本可以忽略,因此在较低泵功率范围内（< 1 500 W）,板式肋片的局部Nusselt数最大.随着泵功率的增长,当泵功率提高到3 000 W,tetrahedral的Nusselt数与板式肋片持平并进一步增大,显示出了格芯夹层结构的应用潜力.高传热性能而低摩擦阻力的格芯夹层结构完全有潜力代替传统的板式肋片结构应用于新型高效紧凑的散热系统中.      

Influence of T-semi attached rib on turbulent flow and heat transfer parameters of a silver-water nanofluid with different volume fractions in a three-dimensional trapezoidal microchannel

This study aimed at exploring influence of T-semi attached rib on the turbulent flow and heat transfer parameters of a silver-water nanofluid with different volume fractions in a three-dimensional trapezoidal microchannel. For this purpose, convection heat transfer of the silver-water nanofluid in a ribbed microchannel was numerically studied under a constant heat flux on upper and lower walls as well as isolated side walls. Calculations were done for a range of Reynolds numbers between 10,000 and 16,000, and in four different sorts of serrations with proportion of rib width to hole of serration width (R/W). The results of this research are presented as the coefficient of friction, Nusselt number, heat transfer coefficient and thermal efficiency, four different R/W microchannels. The results of numerical modeling showed that the fluid's convection heat transfer coefficient is increased as the Reynolds number and volume fraction of solid nanoparticle are increased. For R/W=0.5, it was also maximum for all the volume fractions of nanoparticle and different Reynolds numbers in comparison to other similar R/W situations. That's while friction coefficient, pressure drop and pumping power is maximum for serration with R/W=0 compared to other serration ratios which lead to decreased fluid-heat transfer performance.     

EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER AND PRESSURE DROP CHARACTERISTICS OF W-TYPE SPIRALLY FLUTED TUBES

A new w-type spirally fluted tube with enhanced heat transfer characteristics was developed and manufactured. The heat transfer and pressure drop characteristics of tubes with various geometric parameters were measured over a range of Reynolds numbers from 8,000 to 30,000 for water flowing horizontally through the tube with steam condensing on the outside surface. Experimental correlations for the pressure drop and the heat transfer coefficient were developed from a large amount of data using multivariable linear regression analysis. Factors influencing the heat transfer and flow were analyzed. The experiments showed that heat transfer coefficient can be increased by 3–8% with the pressure drop reduced by 5–10% compared with an ordinary spirally fluted tube.     

HEAT TRANSFER CHARACTERISTICS OF AN IMPINGING BUTANE/AIR FLAME JET OF LOW REYNOLDS NUMBER

An experimental study was performed to determine the heat transfer characteristics of a premixed butane/air round flame jet, of low Reynolds number, impinging upwards normally on a flat rectangular plate. The effects of the exit Reynolds number and equivalence ratio of the flame jet, and the distance between the nozzle and the impingement plate, on the thermal performance of the jet were examined. The range of Reynolds numbers was selected to cover the laminar to the transitional flow conditions. The investigations were conducted with equivalence ratios corresponding to the fuel-rich, stoichiometric, and fuel-lean conditions. The nozzle-plate distance was varied from 1d to 8d. Within the range of Reynolds numbers investigated, the highest Nusselt numbers were obtained at the equivalence ratio of φ = 0.85 when the nozzle-plate distance was maintained at 5d. At the stoichiometric condition, the highest Nusselt number was obtained at the nozzle- plate distance of 6d. Nondimensional correlations were obtained from the experimental results and presented to predict the maximum Nusselt number and average Nusselt number for laminar flame jets as a function of the nozzle-plate distance, Reynolds number, and equivalence ratio.