STUDY ON HEAT TRANSFER PERFORMANCES OF CIRCUMFERENTIAL OVERLAP TRISECTION HELICAL BAFFLE HEAT EXCHANGERS

被引:1
|
作者
Wang, Wei-Han [1 ]
Cheng, Dao-Lai [1 ]
Liu, Tao [2 ]
Chen, Ya-Ping [3 ]
机构
[1] Shanghai Inst Technol, Coll Urban Construct & Safety Engn, Shanghai 201418, Peoples R China
[2] Baoshan Iron & Steel CO LTD, Shanghai 201900, Peoples R China
[3] Southeast Univ, Sch Energy & Environm, Nanjing 210096, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
performance experiments; helical baffle heat exchangers; circumferential overlap of baffles; inclination angle of baffle; heat transfer enhancement;
D O I
10.1615/HeatTransRes.2016014354
中图分类号
O414.1 [热力学];
学科分类号
摘要
The circumferential overlap trisection helical baffle shell-and-tube heat exchangers are suitable for equilateral triangular layout of tubes and can dampen shortcut leakage in triangular zones of adjacent baffles. The performance tests were conducted on oil-water heat transfer in circumferential overlap trisection helical baffle heat exchangers with inclination angles of 12 degrees, 16 degrees, 20 degrees, 24 degrees, and 28 degrees, and compared with a segmental baffle heat exchanger. The results show that both the shell-side heat transfer coefficient h(0) and pressure drop Delta p0 increase while the comprehensive index h0/Delta p0 decreases with increase in the mass flow rate of all schemes. The shell-side heat transfer coefficient, pressure drop, and the comprehensive index h0/Delta p0 decrease with increase in the baffle inclination angle at a certain mass flow rate. The average values of the shell-side heat transfer coefficient and the comprehensive index h0/Delta p0 of the 12 degrees helical baffle scheme are above 50% higher than those of the segmental one correspondingly, while the pressure drop is approximate and the ratios of the average values are about 1.664 and 1.596, respectively. The shell-side Nusselt number Nu(0) and the comprehensive index Nu(0.)Eu(z0)(- 1) increase with the Reynolds number of the shell-side axial Reynolds numberRe(z0) in all schemes. The correlation equations for the shell-side Nusselt number and axial Euler number are presented varying with the axial Reynolds number, Prandtl number, and with the helical baffle inclination angle; the deviations are within +/- 10%.
引用
收藏
页码:347 / 359
页数:13
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