Computation of flow and heat transfer in two-pass channels with 60 deg ribs

被引:43
作者
Jang, YJ [1 ]
Chen, HC
Han, JC
机构
[1] Texas A&M Univ, Dept Mech Engn, Turbine Heat Transfer Lab, College Stn, TX 77843 USA
[2] Texas A&M Univ, Dept Civil Engn, Ocean Engn Program, College Stn, TX 77843 USA
来源
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME | 2001年 / 123卷 / 03期
关键词
computational; cooling; heat transfer enhancement; turbines; turbulence;
D O I
10.1115/1.1371931
中图分类号
O414.1 [热力学];
学科分类号
摘要
Numerical predictions of three-dimensional flow and heat transfer are presented for a two-pass square channel with and without 60 deg angled parallel ribs. Square sectioned ribs were employed along one side surface. The rib height-to-hydraulic diameter ratio (e/D-h) is 0.125 and the rib pitch-to-height ratio (P/e) is 10. the computation results were compared with the experimental data of Ekkad and Han [1] at a Reynolds number (Re) of 30,000. A multi-block numerical method was used with a chimera domain decomposition technique. The finite analytic method solved the Reynolds-Averaged Navier Stokes equation in conjunction with a near-wall second-order Reynolds stress (second-moments) closure model, and a two-layer k-epsilon isotropic eddy viscosity model. Comparing the second-moment and two-layer calculation with the experimental data clearly demonstrated that the angled rib turbulators and the 180 sharp turn of the channel produced strong non-isotropic turbulence and heat fluxes, which significantly affected the flow fields and heat transfer coefficients. The near-wall second-moment closure model provides an improved heat transfer prediction in comparsion with the k-epsilon model.
引用
收藏
页码:563 / 575
页数:13
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