Experimental investigation of turbulent flow in a rotating straight channel with continuous ribs

被引:17
作者
Li, Haiwang [1 ]
You, Haoliang [1 ]
You, Ruquan [1 ]
Tao, Zhi [1 ]
机构
[1] Beihang Univ, Natl Key Lab Sci & Technol Aeroengines Aerothermo, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
LOCAL HEAT-TRANSFER; U-BEND; SMOOTH; PIV; POD;
D O I
10.1063/1.5131223
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We experimentally study the combined effects of continuous ribs and rotations constructed in a square duct on the turbulent flows and flow separation. The ribs obstruct the channel by 10% of its height and are arranged in three different pitch-to-height ratios (P/e) of 10, 12, and 15. The Reynolds number (Re = rho U0D/mu) is fixed at 10 000, and the rotation number (R0 = Omega D/U-0) varies from 0 to 0.52. A time-resolved particle image velocimetry system is applied to provide insights into the main flow and turbulence mechanism. Results show that rotation significantly changes main flow and turbulent characteristics. In particular, a main flow phenomenon has been found: on account of the secondary flow near the ribs, velocity profile deflects to the leading side under a low rotation number, and when R0 rises to 0.48 (critical value), velocity profile deflects to the trailing side. It gives an insight into main flow in a ribbed channel. Reattachment law has been investigated, which can optimize heat transfer by optimize rib arrangement. A proper orthogonal decomposition analysis is also considered to identify the spatial characteristics of the superimposed flow fields. Based on the experimental data, the existence of ribs with different P/e ratios and Coriolis forces play significant roles in rib-generated vortices as well as their turbulent activities. Published under license by AIP Publishing.
引用
收藏
页数:14
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