Heat transfer coefficients over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method

被引:73
作者
Ekkad, SV [1 ]
Zapata, D [1 ]
Han, JC [1 ]
机构
[1] TEXAS A&M UNIV,TURBINE HEAT TRANSFER LAB,DEPT ENGN MECH,COLLEGE STN,TX 77843
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1997年 / 119卷 / 03期
关键词
D O I
10.1115/1.2841161
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents the detailed heat transfer coefficients over a flat surface with one row of injection holes inclined streamwise at 35 deg for three blowing ratios (M = 0.5-2.0). Three compound angles of 0, 45, and 90 deg with air (D.R. = 0.98) and CO2 (D.R. = 1.46) as coolants were tested at an elevated free-stream turbulence condition (Tu approximate to 8.5 percent). The experimental technique involves a liquid crystal coating on the test surface. Two related transient tests obtained detailed heat transfer coefficients and film effectiveness distributions. Heat transfer coefficients increase with increasing blowing ratio for a constant density ratio, bur decrease with increasing density ratio for a constant blowing ratio. Hear transfer coefficients increase for both coolants over the test surface as the compound angle increases from 0 to 90 deg. The detailed heat transfer coefficients obtained using the transient liquid crystal technique, particularly in the near-hole region, will provide a better understanding of the film cooling process in gas turbine components.
引用
收藏
页码:580 / 586
页数:7
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