Investigation of thermal–hydraulic characteristics of cut-out type flying-wing fins

IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL
Xin Qi , Pengcheng Zheng , Zipei Zhang , Wenqiang Suo , Shiqun Liu , Xiangshu Lei , Aiyan Li , Peng Yang , Yingwen Liu
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引用次数: 0

Abstract

The study investigates the potential of a cut-out structure to enhance the heat transfer and flow characteristics of fins in the flying-wing condenser for refrigerator. The proposed cut-out structure is designed to address the limitations of conventional methods for strengthening heat transfer accompanied by an increase in flow resistance. The introduction of a cut-out structure facilitates the flow of cooling air from the front part to the rear area of the fins, thereby enhancing the heat transfer efficiency for rear fins. Additionally, it minimizes the collision between the airflow and the fins, enabling the flying-wing fins to achieve augmented heat transfer and reduced flow resistance simultaneously. The findings of the study demonstrate that the heat exchange rate of the flying-wing fins is enhanced by 7% and the flow resistance is reduced by 20.8% following the integration of the cut-out. Concurrently, an augmentation in the cut-out height and length of the fins resulted in a concurrent decrease in both heat exchange rate and flow resistance. Furthermore, an analysis of the field synergy angle and local convective heat transfer coefficient (LCHTC) of the different cut-out type flying-wing fins reveals that the introduction of the cut-out leads to a significant enhancement in the synergy between the velocity field and the temperature field. Concurrently, the LCHTC exhibits a “high and low” distribution pattern within the fin channel, with the LCHTC on the right side being notably higher than that on the left side.
切开式飞翼翅片热液特性研究
研究了在冷冻机飞翼式冷凝器中采用切割结构提高翅片传热和流动特性的潜力。所提出的切割结构旨在解决传统方法的局限性,以加强传热伴随着流动阻力的增加。引入了开孔结构,便于冷却空气从前部流向尾翼后部,从而提高了尾翼的换热效率。此外,它最大限度地减少了气流与翅片之间的碰撞,使飞翼翼片能够同时实现增强传热和降低流动阻力。研究结果表明:加配切孔后,飞翼翅片的换热率提高了7%,流动阻力降低了20.8%。同时,翅片切割高度和长度的增加导致热交换率和流动阻力的同时降低。此外,通过对不同切割型飞翼翅片的场协同角和局部对流换热系数(LCHTC)的分析表明,切割的引入显著增强了速度场和温度场的协同作用。同时,LCHTC在翅片通道内呈“高低”分布,右侧LCHTC明显高于左侧LCHTC。
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来源期刊
International Journal of Heat and Fluid Flow
International Journal of Heat and Fluid Flow 工程技术-工程:机械
CiteScore
5.00
自引率
7.70%
发文量
131
审稿时长
33 days
期刊介绍: The International Journal of Heat and Fluid Flow welcomes high-quality original contributions on experimental, computational, and physical aspects of convective heat transfer and fluid dynamics relevant to engineering or the environment, including multiphase and microscale flows. Papers reporting the application of these disciplines to design and development, with emphasis on new technological fields, are also welcomed. Some of these new fields include microscale electronic and mechanical systems; medical and biological systems; and thermal and flow control in both the internal and external environment.
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