冲击射流在凹坑壁面通道内的换热特性研究

采用热色液晶瞬态测温技术对航空发动机进气道支板的带凹坑壁面通道内表面开展冲击换热实验。研究了不同射流角度和射流雷诺数下通道内表面的换热特征。结果表明:沿流向在出气缝附近形成换热的高值区,在凹坑尾缘形成局部的高值区。凹坑壁面的换热要强于光滑壁面。随着射流雷诺数的增加,平均努塞尔数增大。当射流倾斜入射时,被冲击一侧换热较高,在驻点区域以及凹坑的尾缘换热最强,另一侧内壁面换热相对弱。射流角度30°时,被冲击面的换热最显著。在射流角度15°时,前缘附近的换热效果最强。     

高效微射流阵列冷却热沉传热特性

微射流阵列冷却热沉是利用射流冲击在驻点区能产生很薄的边界层来提高换热效率,本次研究设计的热沉是5层结构的模块式铜微射流阵列冷却热沉,以去离子水为工质对传热特性进行了实验研究.结果表明,采用微射流阵列冷却不仅能通过增加驻点数目来强化换热,而且能有效地降低换热表面的温差.热沉的热阻会随着泵功的增加而降低;随着泵功的不断提高,热阻变化趋于平缓.     

FC—72圆形射流冲击模拟电子芯片单相局部对流传热的实验研究

以最新微电子设备冷却剂ＦＣ－７２为工质，实验研究了自由和浸没情况下，圆形射流冲击５ｍｍ×５ｍｍ模拟电子芯片的局部对流换热情况。喷嘴直径ｄ＝０．９８７ｍｍ，Ｒｅ数范围为３４８８～４２６４４。测定了自由和侵没情况下驻点换热及换热系数的径向分布，讨论了雷诺数、喷嘴一传热面间距的影响。首次发现ＦＣ—７２自由射流在高Ｒｅ数下，随着喷射间距的增加，驻点换热得到加强，而浸没射流随喷射间距的增大，驻点换热出现非单调性变化；给出了喷射间距ｚ／ｄ＝４时驻点换热系数的关联式，并与其它工质的已有结果进行了比较；对换热系数径向分布的研究表明，与自由射流不同，浸没射流分布曲线上明显出现由层流向湍流过渡所引起的二次峰值。     

脉冲流冲击冷却换热的液晶显示实验研究

采用热色液晶定量测温技术对稳态及脉冲式空气-氮气圆形浸没射流冲击冷却换热进行了实验研究.脉冲射流的实验结果表明,对于喷嘴直径D=3 mm的情形,无论脉冲频率高低,均无强化换热效果;对于D=I0 mm的情形,在较高Re数时出现个别工况的驻点换热强化.脉冲射流表现出换热系数沿径向分布趋于均匀的特点.     

旋转效应下射流冲击速度对换热的影响

采用数值计算方法模拟磨削工件表面的射流冲击对流换热过程,对不同射流冲击速度,考虑旋转盘诱导的气旋卷吸和射流冲击的耦合作用下,研究分析加热壁面的对流换热效果。在转盘诱导的气旋流动影响下,冲击射流向转盘和加热表面之间区域的侵入能力受到抑制,而射流速度的提高能够加强射流冲击的穿透力;在旋转盘诱导的气旋运动和卷吸作用下,空气射流冲击能有效改善磨削弧区的对流换热,且随着射流速度的增加,其强化对流换热的效果更显著。     

冲击角对射流强化换热影响的数值研究

本文介绍了一种新型的冲击冷却型冷板,重点研究了冲击角对强化换热效果的影响以及对驻点位置的影响,并运用场协同理论分析了射流过程中强化换热的机理.     

旋转状态半受限冲射流流动和换热特性研究

利用数值模拟的方法,通过改变冲击雷诺数Rej(20000-35000)、旋转数Ro(0-0．0117)等参数,分析旋转条件下半受限单孔冲击射流的流动和换热特性,讨论了旋转对冲击射流的流场结构和换热特性的影响．研究结果表明:冲击射流在离心力和哥氏力的共同作用下发生弯曲,造成冲击靶面上的冲击斑随着旋转数Ro的增加而不断偏移,显著影响了冲击的冷却效果．冲击靶面的平均Nu数随着冲击雷诺数Rej的增加而增加;当旋转数Ro增加时,冲击靶面的平均Nu数先增加,后减小,然后再增加．计算结果和试验结论基本一致．     

粗糙表面对非定常冲击射流传热的影响

利用在射流驻点周围设置不同高度的圆环来模拟粗糙表面,进行非定常射流冲击换热的实验研究.非定常射流由一个特殊的质量流量控制装置产生,波形和频率可调.采用高度分别为1 mm,2 mm和3 mm的圆环,研究发现环高h=3 mm时,冲击射流流场发生了实质性的改变.对于流动形态没有发生实质改变的粗糙表面,在稳定射流冲击下,传热特性没有质的变化.然而,非定常射流冲击粗糙表面时,与其冲击光滑平板相比,传热特征有很大不同,传热强化系数总体上是削弱了,随着圆环高度的增加更为明显.     

单孔蒸汽射流冲击平板换热的数值研究

对充分发展的过热蒸汽湍流射流冲击平板的流动和换热进行了数值研究,分析了射流温度和射流雷诺数对蒸汽射流冲击换热的影响,并与空气射流冲击换热进行了比较。通过AKN k-ε、V2F和SST k-ω三种湍流模型计算结果的对比可知,SSTk-ω模型模拟冲击射流流动和换热的效果最好。研究表明:在相同条件下蒸汽的冲击换热能力强于空气;射流温度的变化对空气的冲击换热基本没有影响,但是对蒸汽有较大影响;射流雷诺数越大,则蒸汽冲击射流的换热越强。     

阵列射流冲击冷却局部对流换热特性的数值计算与试验验证

本文运用数值计算的方法对具有初始横流的阵列射流在不同的排列方式、冲击间距和横流/射流质量流量比下 的流动换热进行了三维数值研究,并采用热色液晶测试技术对阵列射流冲击的冷却表面温度分布进行了试验研究。获得了 每一股射流的冲击冷却局部对流换热系数分布的特征,研究结果表明本文的计算结果与实验特征是基本吻合的。     

INVESTIGATION INTO METHODS OF ENHANCING HEAT TRANSFER UNDER IMPINGING AIR JETS

Impinging air jets are widely used in industry, for heating, cooling, drying, etc., because of the high heat transfer rates which are developed in the impingement region. In this study, two methods of enhancing jet heat transfer have been investigated, namely, by using turbulence promoters to artificially raise the turbulence level, and by using a loudspeaker to excite the jet acoustically. In both these cases, the increases in heat transfer from enhancement were found to be modest. Some experimental hot-wire anemometry data obtained for free and impinging air jet flows are presented here. The existence of a relationship between turbulence intensity and heat transfer mechanism is also discussed.     

微射流阵列冲击恒热流壁面换热数值模拟

微射流冲击作为一种高热流冷却技术,在大功率激光器、微电子芯片等微型高热流器件冷却方面有广阔应用前景.本文对微射流阵列冲击恒热流表面的换热情况进行数值模拟,详细分析了微射流阵列的换热特点,对比了射流孔顺排和叉排方式的冷却性能,得出射流入口雷诺数、射流孔间距、射流高度等因素对冷却特性的影响规律.     

Heat Transfer and Emission Characteristics of Impinging Rich Methane and Ethylene Jet Flames

Flame impingement heat transfer has widespread industrial and domestic applications and attaining high heat flux as well as low emission of pollutants is the important prerequisite for all such applications. In this article, the heat transfer and emission characteristics of a laminar flame jet impinging on a flat target plate have been investigated experimentally. The effect of reactant jet Reynolds number, equivalence ratio and burner to plate separation distance on the average heat flux, and emissions of CO and NO_x are studied using methane and ethylene fuels. Results indicate that the heat flux is maximized under certain operating conditions of jet Re, equivalence ratio, and separation distance between the burner and the target. Fuel type is found to have an effect on the heat transfer rate because of the varying luminosity of the flame with different fuels. Operating regimes that produce lower emission of pollutants are also identified. Findings of this article have direct industrial relevance to flame impingement heat transfer applications that have small target plate-to-burner port diameter ratios.     

Flat Surface Heat Transfer Enhancement By An Impinging Circular Free Water Jet

Impinging a free water jet onto a heated flat plate was investigated with and without mesh screens. Increasing the jet velocity increased the surface cooling rate via turbulence increase. Lower temperature gradients existed due to the faster wetting front propagation for the water film to advance in shorter times. Decreasing the nozzle-to-block spacing slightly increased the cooling rates by counteracting effects of gravity acceleration and jet momentum dispersion. The turbulence role in the heat transfer enhancement was optimized via opposite changes in the strain rate and largest turbulence scale. Displacing the screens from the impingement zone increased the heat flux.     

Heat transfer and flow characteristics of turbulent slot jet impingement on plane and ribbed surfaces

A computational study is carried out to assess the suitability of various RANS based turbulence models for slot jet impingement on flat and ribbed surfaces with various values of Reynolds number and jet to plate spacing. The com-puted results are compared with the reported experimental data. It was observed that none of the turbulence models considered predicted the heat transfer data accurately. However, some models predicted the experimental data with good trends, e.g., secondary peak and several spikes in Nusselt number for ribbed surface, with a precise computation of the stagnation point Nusselt number. Further, the effects of slot width, rib pitch and jet to ribbed surface spacing were investigated for jet impingement on a ribbed surface. It was observed that the local Nusselt number increased with slot width and rib to plate spacing. It was also observed that increasing Reynolds number had a positive effect on the local heat transfer. With increasing rib pitch the local Nusselt number increased near the stagnation zone but de-creased downstream. The observed flow pattern was different for jet impingement on a ribbed surface than that on a flat surface.     

用速度浓度同步测量系统研究瞬态气体撞壁射流混合过程

用速度浓度同步测量系统研究瞬态气体撞壁射流混合过程谢辉，苏万华，史绍熙，林荣文（天津大学内燃机燃烧学国家重点实验室天津３０００７２）关键词撞壁射流，射流混合，速度浓度同步测量１引言对于中小型直喷式柴油机，燃油喷雾与壁面撞击不可避免，研究喷雾和壁面的相...