高压下打孔翅片通道内的流动换热性能
Behavior of Fluid Flow and Heat Transfer of Perforated Fin Channels at High Pressure
近年来,随着内压缩流程的广泛使用,对内压缩流程中采用较多的打孔板翅式换高压下打孔翅片通道内的流动换热性能热器流动换热性能的研究越发显得重要。但是针对已有文献的调研,发现打孔板翅式换热器的研究主要集中于两方面。一方面研究如何利用打孔板翅式换热器使流体均匀的进入换热器所有通道和流体有相变的地方,另一方面研究中低压下打孔板翅式换热器的流动换热性能。但是在仅公开的文献里,对于低温、高压及超临界等极端工况下打孔板翅式换热器流动换热性能的研究相对较少。鉴于此,本文将使用数值模拟的方法研究高压下打孔板翅式换热器翅片通道内的流动换热性能。首先分析了高压下打孔翅片通道内的流动换热性能的变化规律;其次拟合了高压下打孔翅片通道内的j、f因子的预测关系式,并将所提预测关系式计算所得j、f因子与文献中的实验值对比,对比结果显示,本文所提预测关系式可以较好的预测较广范围下不同结构打孔翅片通道内的流动换热性能。最后评价了打孔翅片通道内的强化换热性能,并讨论了翅片结构对高压下打孔翅片通道内强化换热性能的影响。
with the development of an internal compression process, study of fluid flow and heat transfer of perforated fin channels at high pressure is increasingly crucial. But most of researchs mainly focused on two aspects. On the one hand, studying that how to weak uniform flow distribution by using perforated plate fin heat exchanger, on the other hand, The airside thermal hydraulic performances of different finchannels are investigated numerically when fin thinkness is less than 0.3mm, the research of fluid flow and heat transfer of perforated fin channels is precious few for low temperature and high pressure. in order to design and optimize the plate-fin heat exchanger,The airside thermal hydraulic performances of different finchannels are investigated numerically.Firstly, the general behavior of flow and heat transfer in perforated finchannelsare analyzed.Secondly,Based on the analysis of a large amount of numerical data, general correlations of jand f factors are developed, and then comparing the value of j and f factors with experimental andnumerical simulation results, the results show that experimental and simulated values have good consistency. Finally, to evaluatethe performance of heat transfer enhancement for perforated fins.)
杨宇杰、康蕊、杨永斌、厉彦忠
热力工程、热机
打孔翅片流动换热性能性能评估数值模拟。
perforated finsThermal hydraulic performancePerformance evaluationNumercial simulation
杨宇杰,康蕊,杨永斌,厉彦忠.高压下打孔翅片通道内的流动换热性能[EB/OL].(2017-01-24)[2025-08-03].http://www.paper.edu.cn/releasepaper/content/201701-278.点此复制
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