TY - JOUR
T1 - Numerical investigation of buoyancy influence on flow and heat transfer characteristics in rotating square U-duct
AU - Yang, Ke
AU - Wen, Jie
N1 - Publisher Copyright:
© 2016, Editorial Department of Journal of Propulsion Technology. All right reserved.
PY - 2016/9/1
Y1 - 2016/9/1
N2 - To investigate buoyancy influence on flow and heat transfer characteristics of U-duct in high rotation number range from 0 to 2.013, k-ω SST two-equation turbulence model was adopted. The same rotation number, different temperature ratios (0.12, 0.17 and 0.22) and the same temperature ratio(0.22), different rotation numbers U-duct were studied. The results show that in radial outward passage buoyancy induces the flow seperation in the vicinity of leading surface. Heat transfer intensity of leading surface firstly increased and then decreased with the increasing of rotation numbers. In radial inward passage, due to buoyancy effect the velocity profile presents in double peaks pattern. With the increasing of rotation number, the Nu/Nus difference between leading surface and trailing surface is reduced. When the rotation number increases approximately to 1.0, the Nu/Nus value of trailing surface is beyond that of leading surface. In stationary U-duct, heat transfer is enhanced at lower temperature ratio, while it is just reversed in rotating U-duct. The calculation results prove that buoyancy number is appropriate to evaluate the combined effect of rotation number and temperature ratio on heat transfer.
AB - To investigate buoyancy influence on flow and heat transfer characteristics of U-duct in high rotation number range from 0 to 2.013, k-ω SST two-equation turbulence model was adopted. The same rotation number, different temperature ratios (0.12, 0.17 and 0.22) and the same temperature ratio(0.22), different rotation numbers U-duct were studied. The results show that in radial outward passage buoyancy induces the flow seperation in the vicinity of leading surface. Heat transfer intensity of leading surface firstly increased and then decreased with the increasing of rotation numbers. In radial inward passage, due to buoyancy effect the velocity profile presents in double peaks pattern. With the increasing of rotation number, the Nu/Nus difference between leading surface and trailing surface is reduced. When the rotation number increases approximately to 1.0, the Nu/Nus value of trailing surface is beyond that of leading surface. In stationary U-duct, heat transfer is enhanced at lower temperature ratio, while it is just reversed in rotating U-duct. The calculation results prove that buoyancy number is appropriate to evaluate the combined effect of rotation number and temperature ratio on heat transfer.
KW - Buoyancy
KW - Numerical investigation
KW - Rotation
KW - Square U-duct
UR - https://www.scopus.com/pages/publications/84988422453
U2 - 10.13675/j.cnki.tjjs.2016.09.013
DO - 10.13675/j.cnki.tjjs.2016.09.013
M3 - 文章
AN - SCOPUS:84988422453
SN - 1001-4055
VL - 37
SP - 1696
EP - 1702
JO - Tuijin Jishu/Journal of Propulsion Technology
JF - Tuijin Jishu/Journal of Propulsion Technology
IS - 9
ER -