再循环重力供液蒸发器管内换热性能预测

为了找出适用于再循环重力供液蒸发器管内强制对流沸腾换热系数的关系式,通过对以R404A为制冷剂的重力供液实验台的研究,编程计算出J.Chawla关系式及Shah关联式对重力供液沸腾换热系数进行预测值。与实验结果比较可知:J.Chawla关系式在较低温度下较接近于实验值,Shah关联式在较高的温度下可以对实验值进行预测,两种关系式相结合的方法就可以较好对重力供液蒸发器管内沸腾换热进行预测。     

小温差喷雾碰壁蒸发过渡段换热特性分析

本文对小温差下水平面的喷雾碰壁蒸发传热特性进行了实验研究.通过对实验数据的分析发现,喷雾碰壁蒸发换热过程可分为三个阶段,即雾化工质单相冲击对流换热段、过渡换热段、充分沸腾换热段.在喷雾碰壁蒸发换热过程中,总的热流密度由单相冲击对流换热的热流密度和沸腾换热的热流密度两部分组成.据此,提出并改进了喷雾碰壁蒸发换热过程中过渡段换热系数的处理方法,将有利于对喷雾碰壁换热的进一步研究.     

汽车尾气催化转化器内的对流换热

为了建立汽车尾气催化转化器冷启动过程温度场变化的数学模型,必须正确地选取对流换热系数关联式。本文选用三个典型的对流换热系数关联式,对无化学反应条件下催化剂载体的温升过程分别进行了数值模拟。同时建立实验台,测量不同工况下载体温升过程中温度场的变化。数值模拟与实验结果的对比表明,在催化转化器冷启动过程的不同阶段,应使用不同的对流换热系数关联式进行描述。     

中等雷诺数下高水分烟气横流圆管对流换热实验研究

在中等雷诺数（３０００～７０００）下的广泛温度范围内（３００～７００℃）水测量了水蒸汽和干空气的混合介质（ｒＨ２Ｏ＝ ０．２５～ ０．４５）横流单管和管排的对流换热系数,并与经典的Ｚｈｕｋａｕｓｋａｓ方法计算结果进行了比较,实验结果表明,高水分烟气横流圆管对流换热系数伴随烟气水分浓度的增大和温度的升高而加强,这种加强的趋势比使用Ｚｈｕｋａｕｓｋａｓ关联式计算得到的结果更为显著,本文使用烟气水分含量作为修正因子,通过修正的Ｚｈｕｋａｕｓｋａｓ关联式,给出了高水分烟气横流圆管对流换热计算关联式。     

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。     

冷却条件下管内超临界压力CO2对流换热研究

本文用数值计算和实验测量结合的实验方法对冷却条件下超临界压力二氧化碳在细圆管内(Din=2 mm)的局部对流换热进行了实验研究.结果表明,冷却条件下超临界二氧化碳局部对流换热系数在流体温度略高于准临界温度时达到峰值.本文还对该过程进行了数值模拟,比较了不同湍流模型的计算结果,根据数值模拟提供的信息分析了影响冷却条件下超临界压力二氧化碳换热的主要因素和物性变化对换热的影响.     

无沸腾喷雾冷却技术的研究进展

文中简述了无沸腾喷雾冷却技术近年来国内外的研究进展。着重介绍了关于影响无沸腾区换热各参数的实验研究,如壁面温度、介质体积通量、喷雾流量、喷雾倾角和喷雾高度等,为寻求最佳换热提供了指导。并对无沸腾区的理论研究内容进行了归纳,主要是模拟不同喷雾条件下的换热过程及特性参数(如液膜厚度)的大小和分布,并将理论值与实验数据进行比较分析;总结了影响无沸腾区换热的喷雾特性参数和外部特性。     

润滑油对超临界压力CO_2对流换热特性影响

本文对含有少量润滑油对冷却条件下水平细圆管中超临界压力二氧化碳的对流换热特性进行了实验研究,并与相应不含润滑油的工况及已有经验关联式进行对比。实验结果表明,润滑油会使冷却工况下超临界压力二氧化碳的对流换热恶化,尤其是二氧化碳温度在准临界温度附近时,恶化现象更显著。本文提出了用于计算含润滑油时冷却工况下超临界压力二氧化碳对流换热的经验关联式,其计算结果与90%以上实验数据的偏差在25%以内。     

微通道中液氮单相流动和换热实验研究

对直径为0.531,0.834,1.042和1.931 mm的圆形微通道内液氮的单相流动和传热进行了实验研究.在10,000～90,000的高雷诺数范围内,测量了流动摩擦系数、局部和平均对流换热系数.结果表明,流动摩擦系数随微通道壁面粗糙度的增加而变大.微通道中局部对流换热系数受到液氮导热系数变化的影响沿管程逐渐下降约12.5%.传统的Gnielinski换热关联式经过流动摩擦系数的修正后与实验换热系数符合较好.     

甲烷的池内核态沸腾传热研究

本文针对0.15 MPa、0.2 MPa以及0.3 MPa三个压力下甲烷的池内核态沸腾进行了系统实验研究,得到了相应的甲烷核态沸腾传热数据,并将实验结果和现有的核态沸腾传热关联式进行对比,分析各个关联式对甲烷沸腾数据的拟合偏差和影响因素,结果表明McNelly和Labuntsov关联式的拟合结果最好,偏差均在5%以内。同时所有由制冷剂数据得到的沸腾关联式均可较好的拟合出甲烷沸腾换热系数的变化趋势,除Nishikawa关联式外其余偏差均小于30%,而对于Nishikawa关联式,仅仅改变其常数项即可得到较好的拟合结果。从传热关联式的拟合情况来看,甲烷与常规制冷剂的沸腾传热特性没有本质差异。     

喷雾冷却相变传热的建模与模拟计算

喷雾冷却是一种高效的热控技术,为了探索形成完善的喷雾冷却技术设计流程,文章开展了喷雾冷却传热过程的建模研究.针对喷雾冷却传热过程的模拟计算,基于喷雾冷却相变传热的4个传热机制:液膜对流传热、池沸腾传热、二次气泡沸腾传热、二次气泡高频化机制,利用Monte Carlo方法描述了不同粒径与速率分布的液滴撞击液膜并生成二次气泡的过程,通过液态介质中气泡生长速率的解析计算模型考虑了气泡的生长过程,并结合模化气泡与气泡之间、液滴与气泡之间、气泡与液膜之间的干涉行为描述了气泡的演化过程,通过综合液膜单相对流与气泡相变传热,发展了喷雾冷却相变传热模拟计算方法.基于喷雾冷却实验台开展了稳态喷雾冷却实验,实验校核结果表明,计算方法能够较好地模拟喷雾冷却相变传热性能.另外还分析了影响本方法计算精度的两类因素.      

A Study on Nucleate Boiling Heat Transfer Characteristics of Acetone on Smooth and Indented Surfaces

This article presents the nucleate boiling heat transfer characteristics of acetone at one bar on smooth and enhanced circular stainless steel surfaces (SS 316) of 20 mm diameter for heat flux between 1 and 4 W cm^? 2, which mimic the operating condition of a typical immersion electronic cooling system. The experimental heat transfer coefficient from the smooth surface is validated against Borishanski correlation [1] within acceptable limits of ± 5%. The steel smooth surface is enhanced by providing 100 equally spaced indents of 0.5 mm diameter and 0.05 mm depth. The experimental results indicate that the enhanced surface shows a good shift in the boiling curve and thus, enhancing the nucleate boiling heat transfer at a lesser wall super heat when compared to the smooth surface by around 35% for tested condition. The effect of subcooling on nucleate boiling in enhanced surface reveal that the heat transfer coefficient degrade by 40 to 55% for a sub cooling of 5 to 10 K. The influence of material is studied by a similar enhanced surface made of brass and compared for the same working condition. The brass enhanced surface showed an improved of around 50% against the steel-enhanced surface. Also, the influence of fluid is studied by comparing acetone and n-pentane, which showed that the latter an enhancement in heat transfer coefficient of 50% over the former.     

Interpreting the influence of fuel spray impact on mixture preparation for HCCI combustion with port-fuel injection

This paper addresses the influence of fuel spray impact on fuel/air mixture for combustion in port-fuel injection engines. The experiments include time resolved measurements of surface temperature synchronized with PDA measurements of droplet dynamics at impact and were conducted to quantify the effects of interactions between successive injections on the mixture preparation for combustion in homogeneous charge compression ignition (HCCI) engines. Analysis shows that, during engine warm up, the heat transfer over the entire valve surface occurs within the vaporization-nucleate-boiling regime and the local instantaneous surface temperature correlates with the dynamics of droplets impacting at the same point. A functional relation is found for the heat transfer coefficient, which also describes other experiments reported in the literature. Similarity does not hold after the engine warms up because heat transfer and droplet vaporization at the surface are dominated by multiple interactions between droplets arisen from diverse heat transfer regimes. However, results evidence the existence of a critical surface temperature which sets a transition between overall heat transfer regimes dominated by local nucleate boiling at lower temperatures and by local intermittent transition regimes at higher temperatures. The heat transfer within the overall nucleate boiling regime is shown to be due to a thin film boiling mechanism leading to breakdown of the liquid-film at a nearly constant surface temperature, regardless of injection frequency or any other spray conditions. While at low frequencies this regime is not limited neither by the delivery of liquid to the surface, nor by the removal of vapour from the surface, at higher frequencies it is triggered by enhanced vaporization induced by piercing and mixing the liquid film. The results further evidence the important role of spray impingement for mixture preparation as required for HCCI.     

微通道内超临界二氧化碳的压降与传热特性

进行了微通道内超临界CO2的局部和平均传热与压降特性实验研究。结果表明,临界点附近物性参数的剧烈变 化使压降增大,但传热被大大强化。同时也发现,系统压力、质量流速及CO2温度对流动与传热特性有重要影响。在大 量实验数据的基础上,得出了冷却条件下水平微通道内超临界CO2强制对流换热关联式。     

低温流体在多孔表面的池沸腾研究综述

低温流体尤其是液氮在航天、电子冷却、低温生物医疗与超导磁体与电缆等领域有着广泛的应用.文中对光滑与多孔表面上的流体核态沸腾换热与临界热流密度的研究进行了归纳；总结了低温流体池沸腾的研究现状；比较了低温流体与常见制冷剂以及水在物性上的主要差异；综合分析了加热表面材料、多孔层厚度、孔隙率、烧结颗粒直径、平均孔隙直径与压力等...     

水喷射淬冷高温壁面的传热实验研究

本文采用直接表面温度测量的方法对水喷射高温壁面的传热过程进行实验研究．系统地研究了射流出口速度、冷却水过冷度、喷嘴至加热面的间距、初始壁温以及水喷雾的流量密度等参数对淬冷表面的膜态沸腾、最小临界点、过渡沸腾、最大临界点等传热过程的影响，给出了有关实验结果，分析了它们的特点。     

雾化喷射冷却的机理及模型研究

雾化喷射冷却的换热机理十分复杂,目前其研究还很不成熟。本文从喷射雾滴的特性参数出发,以被冷却表面上形成的喷射液膜为对象,考虑了冷却液体向环境的散热,建立质量、能量守恒方程,得到半经验半解析的雾化喷射换热模型。其中,本文提出真换热系数和显换热系数的概念,认为显换热系数受空间散热影响,而真换热系数只与喷雾动量有关。最后设计了雾化喷射局部换热实验,对模型进行检验,结果表明,该模型能够较好地符合实验所得的换热系数及加热面表面温度沿喷射半径的分布趋势。     

液氮流动沸腾换热研究综述

作为一种优良的低温冷却剂,液氮在航天、电子工业、超导磁体和超导电缆冷却及低温生物医疗等领域应用广泛。在这些应用中,准确预测液氮的流动沸腾换热特性对于系统设计和安全运行十分重要。该文主要介绍了液氮流动沸腾换热的特点,对已有的实验和数值模拟结果进行了归纳;并比较了四个液氮流动沸腾换热计算关联式的预测情况,以及关联式中干度、质量流量、热流密度和压力对换热系数的影响;指出了有待进一步研究的课题。     

喷雾冷却的热逆转现象及其传热强化特性

针对高热流密度激光介质散热问题,利用实验方法研究了以十二烷基硫酸钠水溶液作为工质的喷雾冷却传热特性。结果表明,在特定的热流密度范围内,随着热流密度的增加,加热面温度不升反降,称之为热逆转。热逆转现象对对流换热系数的提升作用可高达94.0%,提升大小与热流密度有关。热逆转对应的热流密度区间为80～130 W/cm2,与浓度关系较小。热逆转现象与实验过程有关,该现象仅在热流密度逐渐升高的过程中出现,降低和任调热流密度过程中未发现此现象。热逆转具体原因还有待研究。     

Influence of nucleation on the flow boiling heat transfer coefficient of a refrigerant mixture under varied heat flux conditions

The influence of nucleation on the flow boiling heat transfer coefficient of R-134a/R-290/R-600a refrigerant mixture is experimentally studied in a smooth horizontal tube of 12.7 mm diameter. The heat transfer coefficients are experimentally measured for stratified flow patterns under a varied heat flux condition; a condition found in the evaporator of refrigerators and deep freezers. The experiments are conducted in a counter-current heat exchanger test section. By regulating the flow rate and inlet temperature of acetone, which is the heating fluid flowing in the outer tube, a varied heat flux is provided to the refrigerant flowing in the inner tube. The refrigerant mass flow rate is fixed between 3 and 5 g s⁻¹ and its inlet temperature between −8.59 and 5.33°C, which corresponds to a pressure of 3.2 to 5 bar. The significance of nucleate boiling prevailing in the above-mentioned evaporators is highlighted. The experimental heat transfer coefficients are also compared with well known heat transfer correlations.