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以去离子水为工质,实验研究了横截面形状为圆形、椭圆及菱形的叉排微肋片组成的流道内的流动阻力特性。结果表明,3种形状肋片流道内压降随流量增大而增大。受微/小尺度下层流边界层的影响,流量较低时微肋形状对流动影响较弱,椭圆形肋片与菱形肋片内压降几乎相同,而圆形截面肋片内由于流动距离较长导致流动阻力最大;当流量较大时,椭圆形肋片内压降最小。Re较小时,长短轴一致的菱形肋片内的流动阻力系数f比椭圆形肋片略低,但在Re较高时,椭圆形肋片内的f值仍然最低。研究还表明,在现有各种关联式中,只有菱形微肋片关联计算值与本实验值较吻合。 相似文献
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以去离子水为工质,实验研究了横截面形状为圆形、椭圆及菱形的叉排微肋片组成的流道内的流动阻力特性。结果表明,3种形状肋片流道内压降随流量增大而增大。受微/小尺度下层流边界层的影响,流量较低时微肋形状对流动影响较弱,椭圆形肋片与菱形肋片内压降几乎相同,而圆形截面肋片内由于流动距离较长导致流动阻力最大;当流量较大时,椭圆形肋片内压降最小。Re较小时,长短轴一致的菱形肋片内的流动阻力系数f比椭圆形肋片略低,但在Re较高时,椭圆形肋片内的f值仍然最低。研究还表明,在现有各种关联式中,只有菱形微肋片关联计算值与本实验值较吻合。 相似文献
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基于MATLAB的肋片传热特性分析与优化设计 总被引:3,自引:0,他引:3
利用MATLAB对肋片传热过程进行数值模拟,并对肋片的传热特性进行了分析研究。在此基础上获得肋片温度分布、散热量、肋效率等重要参数,探讨肋片厚度、肋片高度、肋片形状对散热量的影响及肋片结构优化设计方法。 相似文献
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涂层吸附床能够降低吸附剂间的热阻提高吸附床传热性能,是一种高效吸附床。文中采用COMSOL Multiphysics软件建立了局部非热平衡的二维板翅式吸附床模型,开展板翅式吸附床性能数值模拟;采用制冷性能(COP)和单位质量吸附剂制冷能力(SCP)分别对不同翅片形状吸附床(三角形翅片吸附床、梯形翅片吸附床与六边形翅片吸附床)的性能进行分析和评价。研究发现:驱动热源为333—363 K时,随着热源温度的升高,3种不同结构的板翅式涂层吸附床的COP和SCP都随之增大;在相同的条件下,3种不同翅片结构的板翅式吸附床中,六边形翅片吸附床的COP最大,其值为0.514;而梯形翅片吸附床的SCP最高,其值为848.61 W/kg。 相似文献
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由于板翅式换热器结构的复杂性,存在着内部流动速度分布的不均匀性,从而引起其换热效率下降,影响了换热器的整体效能.引起流动速度分布不均匀的因素是多方面的,针对不同导流片结构参数(h/H)对导流片导流性能的影响进行了深入研究,发现导流片结构参数对换热器内部流动速度分布不均匀性的影响主要表现在总管流动方向上,通过改变板翅式换热器导流片的结构参数可有效地改善换热器内部物流在总管流动方向上的分配情况,从而有效地改善换热器内部流动速度的分布.研究结果对板翅式换热器的优化设计具有重要意义. 相似文献
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为了对比板翅式换热器不同平直翅片的换热性能,采用CFD软件FLUENT数值模拟计算方法,研究了空气在三角形和矩形不同结构参数翅片中的表面传热与流动阻力特性。揭示了2种形状不同结构参数翅片中流体的速度对翅片表面换热因子和翅片表面摩擦因子的影响规律;并用CFD-Post分析了各参数在翅片中的分布情况。结果表明:在所有翅片中,翅片表面换热因子和翅片表面摩擦因子都随着流体速度的增大而减小;在三角形翅片中,翅片表面摩擦因子由翅顶部位对称向翅底两端均匀递减,在翅底两端最边缘附近分布最小;在矩形翅片中,翅片表面摩擦因子在翅片中部分布比较均匀,在翅片两端最边缘附近突然变小。 相似文献
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Yong-Seog Seo Sang-Pil Yu Sung-June Cho Kwang-Sup Song 《Chemical engineering science》2003,58(1):43-53
The characteristics of a catalytic heat exchanger which integrates heat generation and heat exchange into one equipment have been investigated by the experiment and numerical simulation. The surface of the fin tubes was catalyzed by the formation of the oxide layer and the subsequent washcoating of ZrO2, followed by the impregnation of Pd catalyst. The experimental results showed that the performance of catalytic combustion in the catalytic heat exchanger was more significantly affected by the inlet velocity of the mixture than by its inlet temperature and equivalence ratio. It was also found that the catalytic surface area was a critical parameter to obtain the complete conversion of the mixture. Numerical simulation has been performed with a commercial software FLUENT. The calculated results indicated that the performance of the catalytic combustion was influenced by the catalytic fin configuration as well as the flow pattern of the mixture over the catalytic fins. The results recommend that the number and thickness of catalytic fins should be designed above 6 pieces/inch and less than to achieve the best performance in the catalytic heat exchanger. 相似文献
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In present work, a stepping optimization algorithm is proposed for the geometric optimization of conical fin, and the heat transfer rate of the fin is treated as the objective function in the optimization algorithm. The conical fin is divided into finite elements which have different generatrix slopes, and the geometry of the conical fin is finally determined by ensuring that every divided element can maintain the maximum heat transfer rate. Based on the actual condition of every element of the fin, the heat conduction equation is solved step by step. The present result shows that the optimized conical fin has more heat transfer quantity and higher fin efficiency compared with those of some typical fins. Furthermore, the theoretical feasibility and the error analysis of present optimization algorithm have been performed as well. 相似文献
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具有特殊结构特点的高温热管翅的出现推动了高温热管技术的发展。高温热管翅至今还处于开发研究阶段。对高温热管翅的结构、特点进行了详细的介绍,概括高温热管翅的研究状况,并通过实例说明高温热管翅的工程应用。 相似文献
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以水为介质,对三角多孔翅片(TP)和横排锯齿翅片(TDS)两种变截面翅片通道的过冷沸腾进行了可视化试验。研究了体积流量、过冷度与热通量对过冷沸腾起始位置的影响,通过观察变截面翅片流道内单个气泡形成、生长与合并或脱离的过程,对比分析两种变截面翅片对流沸腾传热强化机理。试验结果表明:TDS翅片通道内气泡从出现到消失的平均周期约为TP翅片的一半;过冷沸腾起始位置随着体积流量的增大,逐渐向流道出口处移动;而随着热通量的增大和过冷度的减小逐渐靠近流道入口处;过冷度对过冷沸腾起始位置的影响比热通量对其的影响更大。 相似文献
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For an alcohol/water system and with fin baffle packing, continuous distillation experiments were carried out in a rotating packed bed (RPB) system at atmospheric pressure. The effects of the average high gravity factor (β), liquid reflux ratio (R) and feedstock flux (F) on the momentum transfer and mass transfer were investigated. The gas phase pressure drop of RPB increased with the average high gravity factor, liquid reflux ratio and feedstock flux, which was 13.55-64.37 Pa at β of 2.01-51.49, R of 1.0-2.5, and F of 8-24 L&;#8226;h-1 for a theoretical tray in the RPB with fin baffle packing. The investigation on the mass transfer in the RPB with different packings showed that the number of transfer units of RPB with a packing also increased with the average high gravity factor, reflux ratio and feedstock flux. It is found that the fin baffle packing (packing III) presents the best mass transfer performance and lowest pressure drop for the height equivalent to a theoretical plate (HETP), which is 6.59-9.84 mm. 相似文献
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