TY - JOUR
T1 - Experimental and numerical analyses of thermal-hydraulic characteristics of aluminium flying-wing fins
AU - Miao, Long
AU - Wang, Yichun
AU - Kavtaradze, Revaz
AU - Liu, Shiqun
AU - Zhang, Songmao
N1 - Publisher Copyright:
© 2021 Elsevier Ltd
PY - 2022/2/25
Y1 - 2022/2/25
N2 - The secondary heat transfer surface of the shovel-cut finned tube, called the flying-wing fin, eliminates the thermal contact resistance. In the present study, the thermal-hydraulic characteristics of the flying-wing fin at Reynolds number range of 1500–3000 were studied, including overall quantitative analysis and three-dimensional thermophysical field analysis. It was found that the ratio of Nu·η0/f1/3 of the flying-wing fin (Case A1) is about 8.6% larger than that of the wavy fin (Case B3). The fundamental reason is that the flying-wing fin has a smaller average field synergy angle than the wavy fin. There is a butterfly-shaped low-velocity zone at the root of the wave trough of the monitoring section on the acute-angled side of the flow channel. In addition, along the fin height direction, the influence range of this low-velocity zone on the flow field is less than around 1.34 mm. Similarly, there are butterfly-shaped zones for the temperature and field synergy angle distributions. The average value of the convective heat transfer coefficient on the left side of the flying-wing fin is greater than that on the right side. In general, the promising flying-wing fins show better thermal-hydraulic performances than the wavy fins with similar geometric parameters, which deserve further promotion and engineering application.
AB - The secondary heat transfer surface of the shovel-cut finned tube, called the flying-wing fin, eliminates the thermal contact resistance. In the present study, the thermal-hydraulic characteristics of the flying-wing fin at Reynolds number range of 1500–3000 were studied, including overall quantitative analysis and three-dimensional thermophysical field analysis. It was found that the ratio of Nu·η0/f1/3 of the flying-wing fin (Case A1) is about 8.6% larger than that of the wavy fin (Case B3). The fundamental reason is that the flying-wing fin has a smaller average field synergy angle than the wavy fin. There is a butterfly-shaped low-velocity zone at the root of the wave trough of the monitoring section on the acute-angled side of the flow channel. In addition, along the fin height direction, the influence range of this low-velocity zone on the flow field is less than around 1.34 mm. Similarly, there are butterfly-shaped zones for the temperature and field synergy angle distributions. The average value of the convective heat transfer coefficient on the left side of the flying-wing fin is greater than that on the right side. In general, the promising flying-wing fins show better thermal-hydraulic performances than the wavy fins with similar geometric parameters, which deserve further promotion and engineering application.
KW - Field synergy
KW - Flying-wing fin
KW - Shoveling molding
KW - Spatial distribution
KW - Thermal contact resistance
UR - http://www.scopus.com/inward/record.url?scp=85121301864&partnerID=8YFLogxK
U2 - 10.1016/j.applthermaleng.2021.117928
DO - 10.1016/j.applthermaleng.2021.117928
M3 - Article
AN - SCOPUS:85121301864
SN - 1359-4311
VL - 203
JO - Applied Thermal Engineering
JF - Applied Thermal Engineering
M1 - 117928
ER -