Effect of connecting holes on flow and heat transfer in a two-pass channel with and without rib turbulators

被引:18
作者
Luan, Yigang [1 ]
Yang, Lianfeng [1 ]
Bu, Shi [1 ]
Sun, Tao [1 ]
Sun, Haiou [1 ]
Zunino, Pietro [2 ]
机构
[1] Harbin Engn Univ, Coll Power & Energy Engn, Harbin 150001, Heilongjiang, Peoples R China
[2] Univ Genoa, DIME Dept Mech Energy Management & Transportat En, Via allOpera Pia 15, I-16145 Genoa, Italy
基金
中国国家自然科学基金;
关键词
Rib; Connecting hole; Two-pass channel; Heat transfer; Gas turbine; PRESSURE-DROP; SQUARE CHANNEL; FLUID-FLOW; FRICTION; SMOOTH; DUCT;
D O I
10.1016/j.ijheatmasstransfer.2018.12.043
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this work, connecting holes are used between the two legs of a two-pass channel with and without ribs. The flow and heat transfer are obtained by numerical simulation at the Reynolds number of 10,000, 30,000 and 50,000. Different rib configurations and positions of the connecting holes are considered. The result shows positive effect of the holes on the performance especially in ribbed channels. Connecting holes can largely reduce the pressure drop across the channel but the decrease in heat transfer is very small, thus the overall thermal performance can be improved significantly. For the smooth channel, pressure loss can be reduced by 14.66% at the heat transfer loss of 1.68%, for the ribbed channel pressure loss can be reduced by 47.99% with merely 8.24% decrease in heat transfer if the ribs and connecting holes are carefully arranged. Connecting holes can affect the boundary layer separation and reattachment between ribs. Separation bubble behind the rib can be suppressed or moved by connecting holes and acceleration occurs within the low velocity region. Therefore the weak heat transfer related to the separation can be improved. Based on this interaction between ribs and holes, further improvement in the performance of two-pass channel can be expected after better design of ribs and connecting holes. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:80 / 95
页数:16
相关论文
共 30 条
[1]  
[Anonymous], 2013, GAS TURBINE HEAT TRA
[2]   Effect of sidewall slots and pin fins on the performance of latticework cooling channel for turbine blades [J].
Bu, Shi ;
Yang, Lianfeng ;
Qiu, Hanghai ;
Luan, Yigang ;
Sun, Haiou .
APPLIED THERMAL ENGINEERING, 2017, 117 :275-288
[3]   Numerical prediction of heat transfer and pressure drop in three-dimensional channels with alternated opposed ribs [J].
Desrues, T. ;
Marty, P. ;
Fourmigue, J. F. .
APPLIED THERMAL ENGINEERING, 2012, 45-46 :52-63
[4]   Local heat transfer distribution in a square channel with 90° continuous, 90° saw tooth profiled and 60° broken ribs [J].
Gupta, Abhishek ;
SriHarsha, V. ;
Prabhu, S. V. ;
Vedula, R. P. .
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2008, 32 (04) :997-1010
[5]  
Han JC, 2010, HEAT TRANSF RES, V41, P803, DOI 10.1615/HeatTransRes.v41.i8.30
[6]   Computation of flow and heat transfer in two-pass channels with 60 deg ribs [J].
Jang, YJ ;
Chen, HC ;
Han, JC .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2001, 123 (03) :563-575
[7]   The Effects of Ribs and Tip Wall Distance on Heat Transfer for a Varying Aspect Ratio Two-Pass Ribbed Internal Cooling Channel [J].
Jenkins, Sean C. ;
Zehnder, Frank ;
Shevchuk, Igor V. ;
von Wolfersdorf, Jens ;
Weigand, Bernhard ;
Schnieder, Martin .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (02)
[8]   Numerical investigation of heat transfer and fluid flow in a solar air heater duct with multi V-shaped ribs on the absorber plate [J].
Jin, Dongxu ;
Zhang, Manman ;
Wang, Ping ;
Xu, Shasha .
ENERGY, 2015, 89 :178-190
[9]   The importance of rib shape effects on the local heat transfer and flow friction characteristics of square ducts with ribbed internal surfaces [J].
Kamali, R. ;
Binesh, A. R. .
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2008, 35 (08) :1032-1040
[10]   Analysis of Turbulent Flow in 180 deg Turning Ducts With and Without Guide Vanes [J].
Luo, Jiang ;
Razinsky, Eli H. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 131 (02)