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1.
航空煤油在微通道中传热性能的实验研究   总被引:1,自引:0,他引:1       下载免费PDF全文
此前对微通道传热性能研究所用的实验工质绝大多数属于低粘性流体,针对高粘性流体的研究很少.本研究以航空煤油和水为实验工质,在层流状态范围Re数为10-100,对两种流体在微通道中的传热性能进行了实验研究.铝基微通道阵列包括163条横截面尺寸为1mm×1mm、长度400 mm的微通道.微通道长径比l/Dh=400.实验发现...  相似文献   

2.
陆向迅  徐斌  吴建  王洋  薛宏 《节能技术》2008,26(2):103-106
本文针对矩形微通道内单相流动和传热特性,利用CFD模拟分析软件对其进行三维数值模拟研究.微矩形通道宽为50μm,高为200μm,工质采用去离子水.模型以有限体积法离散,SIMPLEC方法求解速度、压力和温度耦舍方程组.讨论了流体热物性随温度变化和雷诺数对速度场和温度场的影响.并与理论预测值、参考文献值比较.分析结果显示,流体粘度随温度对触的影响和粘性耗散对热起始段的作用不能忽略.fRe数随Re数的增加而减小,Nu数不受Re数的变化影响.  相似文献   

3.
基于欧拉-拉格朗日方法,对冷却管道内超临界航空煤油焦炭颗粒沉积过程进行了数值模拟研究。物理模型为内径1.8mm、长度2 000.0mm的细圆管,数值计算模型中考虑了流体对颗粒的曳力、重力、Saffman力和附加质量力等。假设物理模型入口处已产生航空煤油焦炭颗粒,重点研究了航空煤油压力对焦炭颗粒沉积过程的影响。研究结果表明,压力对颗粒沉积过程的影响与颗粒大小、温度有着密切的关系。对于10、50、70μm的焦炭颗粒,煤油处于低温区时,压力对颗粒沉积过程影响并不显著,较高的压力对焦炭颗粒沉积略有抑制作用;然而随着温度的升高,压力升高对颗粒沉积过程具有明显的抑制作用。对于30μm的焦炭颗粒,高压反而有利于颗粒沉积。此外,对不同流动方式下颗粒沉积率进行了研究,结果发现竖直向上管中颗粒沉积率最低。  相似文献   

4.
粗糙圆管内超临界航空煤油湍流换热特性分析   总被引:1,自引:0,他引:1  
给出了国产航空煤油RP-3的三组分热物性替代燃料模型。采用k-ε湍流模型结合增强壁面处理的方法对超临界压力下航空煤油RP-3在圆形粗糙冷却通道中的流动与换热过程进行数值研究。分析了粗糙元形状、高度以及间高比等因素对其超临界流动和传热特性的影响规律,探究了人为粗糙度强化超临界航空煤油换热的机理。结果表明,人为设置粗糙元能使壁面附近产生局部回流区和旋涡结构,强化煤油与受热壁面间的对流换热。通过合理布置粗糙元结构,能大幅降低圆形冷却通道的壁面温度,有效抑制航空煤油的超临界传热恶化现象的发生。  相似文献   

5.
有扰流片的矩形通道内空气流动和传热过程的数值模拟   总被引:1,自引:0,他引:1  
以高温透叶片尾部区内部冷却为应用背景,对带顺排、错排扰流片肋的通道内空气流动和传热过程进行了数值模拟。计算结果表明,在相同雷诺数下,错排扰流片的阻力系数比针肋和顺排绕流片的阻力因子均增大约2%,而冷却能力分别增大约50%和9%。  相似文献   

6.
对矩形微通道实体模型进行简化处理,并建立微通道内流体流动的数学模型.设定矩形微通道水力直径Dh=120~480 μm,入口雷诺数Re=ll.9~3 817.1,以20℃蒸馏水为流动工质,借助FLUENT分别对不同水力直径的三组矩形微通道内流体流动特性展开数值模拟研究,并将数值模拟结果与理论预测值及其他学者的研究结论进行对比.结果表明:随着微通道水力直径的减小,摩擦阻力系数、速度梯度和压强梯度都呈现增大趋势;在微尺度下,矩形微通道内临界Re提前,而且水力直径越小,临界Re值越小.  相似文献   

7.
以高温透平叶片冷却为应用背景,对带有顺排、错排扰流片的矩形通道进行了实验研究。实验结果表明:在相同的雷诺数下,错排扰流片比顺排扰流片具有更好的强化换热效果,即便保持相同的流动阻力,错排扰流片的冷却效果仍强于顺排扰流片。  相似文献   

8.
对竖直上升管内超临界压力下航空煤油的传热特性进行了实验研究。分析了不同质量流量、热流密度、压力和进口温度对超临界压力下航空煤油传热特性的影响。实验结果表明,提高质量流量或进口温度均使煤油传热效果变好。而热流密度对流体传热的影响主要在于改变了流体和壁面温度,热流密度越大,传热系数越高。压力对煤油传热影响不大,一般情况下,提高压力会恶化传热。超临界状态下,煤油物性变化很大,因此对煤油的传输和热力学性质的准确计算是研究超临界压力下传热现象的关键。利用拓展的对比态法来计算煤油的密度和传输特性,如黏度、热导率等。给出了煤油在超临界压力下的传热关联式,其计算值和实验值吻合良好。  相似文献   

9.
以干燥器内对流传热问题为研究对象,建立了褐煤干燥过程气-固对流传热模型。通过流-固界面传热耦合,利用CFD仿真技术进行模拟,对褐煤在不同粒径、风速及温度下的干燥过程进行了数值模拟,得到不同工况下的温度场分布及对流传热系数。根据模拟结果拟合得到气-固传热关联式,结果表明该关联式与褐煤干燥过程较吻合,可为工程实践提供理论指导。  相似文献   

10.
11.
INTRODUCTIONHeattransferenllancen1enttechniquesplayaveryimportantroleintllermalcontroltechnologies1lsedwithnlicroelectronicchips,powerfullasermirrors,aerospacecraft,thermalnuclearfusion,etc.Itiswidelyrecognizedthattl1eheattransfercanbein-creasedbyil1creasingthesurfaceareaincontactwiththecoolant.TuckermanandPease[1,2]pointedoutthatforlaminarflowinconfinedchannels,theheattransfercoefficientisinverselyproportionaltothewidthofthechannelsincethelimitingNusseltnum-berisconsta11t.Theybuiltawate…  相似文献   

12.
An experimental study of heat transfer characteristics in superheated steam cooled rectangular channels with parallel ribs was conducted.The distribution of the heat transfer coefficient on the rib-roughed channel was measured by IR camera.The blockage ratio(e/Dh) of the tested channel is 0.078 and the aspect ratio(W/H) is fixed at3.0.Influences of the rib pitch-to-height ratio(P/e) and the rib angle on heat transfer for steam cooling were investigated.In this paper,the Reynolds number(Re) for steam ranges from 3070 to 14800,the rib pitch-to-height ratios were 8,10 and 12,and rib angles were 90°,75°,60°,and 45°.Based on results above,we have concluded that:In case of channels with 90° tranverse ribs,for larger rib pitch models(the rib pitch-to-height ratio=10 and12),areas with low heat transfer coefficient in front of rib is larger and its minimum is lower,while the position of the region with high heat transfer coefficient nearly remains the same,but its maximun of heat transfer coefficient becomes higher.In case of channels with inclined ribs,heat transfer coefficients on the surface decrease along the direction of each rib and show an apparent nonuniformity,consequently the regions with low Nusselt number values closely following each rib expand along the aforementioned direction and that of relative high Nusselt number values vary inversely.For a square channel with 90° ribs at Re= 14800,wider spacing rib configurations(the rib pitch-to-height ratio=10 and 12) give an area-averaged heat transfer on the rib-roughened surface about8.4%and 11.4%more than P/e=8 model,respectively;for inclined parallel ribs with different rib angles at Re=14800,the area-averaged heat transfer coefficients of 75°,60° and 45° ribbed surfaces increase by 20.1%,42.0%and 44.4%in comparison with 90° rib angle model.45° angle rib-roughened channel leads to a maximal augmentation of the area-averaged heat transfer coefficient in all research objects in this paper.  相似文献   

13.
During the past six years comprehensive research programs have been conducted at the Beijing PolytechnicUniversity to provide a better understanding of heat transfer characteristics of existing and condidate cool-ing techniques for electronic and microelectronic devices.This paper provides a review and summary of theprograms with emphasis on direct liquid cooling.Included in this review are the heat transfer investigationsrelated to the following cooling modes:liquid free,mixed and forced convection,liquid jet impingement,flowingliquid film cooling,pool boiling,spray cooling,foreign gas jet impingement in liquid pool,and forced convectionair-cooling.  相似文献   

14.
Numerical investigation has been performed to analyze forced convective heat transfer to supercritical water in horizontal rectangular ducts. Convective heat transfer near the critical region in the rectangular ducts is strongly influenced by large variations of thermodynamic and transport properties of supercritical fluid with gravity force, especially close to pseudocritical temperature. Fluid flow and heat transfer characteristics such as velocity, temperature, and local heat transfer coefficient with water properties distribution in the ducts are presented. Flow accelerates along the horizontal ducts because of decreased water density from heat transfer at the duct walls. Center of large flow recirculation in the duct section locates near the middle of vertical surface and additional secondary recirculation in clockwise direction appears with the increase of duct height. Local wall temperature severely varies along the inner surface of the duct section and its variation depends on aspect ratio of the duct. The heat transfer coefficient distributions along the ducts for various aspect ratios are compared with the proximity effect to the critical pressure.  相似文献   

15.
空气横掠矩形翅片椭圆管束换热规律的数值研究   总被引:1,自引:0,他引:1  
采用Fluent软件对矩形翅片椭圆管束空气侧的对流换热情况进行了三维数值模拟,获得了不同流速下翅片表面温度分布,分析了迎面风速与换热系数之间的关系,随着速度的增大,空气侧的换热系数增加,并拟合了换热计算公式。同时分析了不同翅片间距对换热的影响因素,随着翅片间距的增大,空气侧换热系数增加,而且随着Rg数的增加,换热的强化更加明显。  相似文献   

16.
垂直矩形窄缝内的过冷流动沸腾换热性能   总被引:1,自引:0,他引:1  
用高速摄像等方法研究了有压模化介质在单一垂直矩形窄缝流道内的气泡形态和传热情况 ,发现窄缝流动沸腾换热强化的原因在于流道尺寸较小 ,气泡的形状发生变化 ,增加了界面体积浓度 ,并强化了对加热面附近的扰动 ,使换热有所强化。通过与实际测量的壁温数据进行比较 ,发现用于计算大流道和池过冷沸腾换热的 Rohsenow关系式预测窄流道内高热流密度下的过冷流动沸腾换热的误差不大 ,但对于较低热流密度下的过冷流动沸腾时误差较大 ;通过最小二乘法对 Rohsenow关系式进行修正后 ,误差低于± 2 5 %。  相似文献   

17.
基于Brinkman-Darcy模型和两方程模型,本文对流体在金属泡沫平板通道内的强制对流换热进行了自编程数值模拟,采用体积平均法对流体在金属泡沫内的流动和换热进行宏观处理。模拟结果表明:流体主流速度随孔密度增大而减小,随孔隙率增大而增大;流体相和固体相之间的局部对流换热系数随孔隙率和孔密度增加而增加,金属泡沫对流换热性能随孔隙率增大而减小,随孔密度增大而增大。金属泡沫强化换热的效果十分明显,可以应用于需要强化换热的紧凑式换热器和散热器。  相似文献   

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