Shell-Side Flow Condensation Heat Transfer on Three-Dimensional Enhanced Surface

被引:1
作者
Li, Wei [1 ]
Yang, Desong [1 ]
Chen, Jingxiang [1 ]
Sun, Zhichuan [2 ]
Wang, Jiacheng [3 ]
Ayub, Zahid [4 ]
机构
[1] Zhejiang Univ, Dept Energy Engn, 38 Zheda Rd, Hangzhou 310027, Peoples R China
[2] AVIC Nanjing Engn Inst Aircraft Syst, Nanjing 211106, Peoples R China
[3] Qingdao Univ Sci & Technol, Dept Mech & Elect Engn, 99 Songling Rd, Qingdao 266061, Peoples R China
[4] Isotherm Inc, 7401 Commercial Blvd East, Arlington, TX 76001 USA
基金
美国国家科学基金会;
关键词
shell-side condensation; enhanced tube; heat transfer coefficient; heat exchangers; HORIZONTAL SMOOTH; REFRIGERANTS; COEFFICIENT; HERRINGBONE; PREDICTION; TUBES;
D O I
10.1115/1.4051617
中图分类号
O414.1 [热力学];
学科分类号
摘要
An experimental investigation of shell-side flow condensation was performed on three-dimensional surface enhanced tubes, including a herringbone micro-fin tube and a newly developed 1-EHT tube. An equivalent plain tube was also tested for performance comparison. All the test tubes had similar geometry parameters, i.e., inner diameter 11.43 mm and outer diameter 12.7 mm. The outer shell diameter was 24.5 mm with a wall thickness of 0.6 mm. Tests were conducted using R410A as the working fluid at a dew point of 45 degrees C. The mass flux range of 10-55 kg/(m(2) center dot s) with an inlet quality of 0.8 and an outlet quality of 0.1. Experimental results showed that the plain tube exhibited a better condensation heat transfer performance. Moreover, the mass flux had a significant influence on the heat transfer coefficient for shell-side condensation. A new prediction model based on the Cavallini's equation was developed to predict the condensing coefficient where the mean absolute error is less than 4%.
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页数:7
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