Numerical research on influence of different slot configurations on film cooling characteristics

被引:5
|
作者
Zhang, Dahai [1 ]
Wang, Qiuwang [1 ]
Zeng, Min [1 ]
Sun, Lu [1 ]
机构
[1] Xian Jiaotong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
来源
关键词
film cooling performance; aerodynamic performance; numerical research; both end trenched hole;
D O I
10.1504/PCFD.2008.021330
中图分类号
O414.1 [热力学];
学科分类号
摘要
Numerical approach has been conducted to compare the film cooling characteristics of one end or both ends trenched holes. The influence of different slot configurations on the adiabatic cooling effectiveness and discharge coefficients from the point view of flowing mechanism was revealed. It is found that the trenched holes can improve the film cooling effectiveness especially for the short double end trenched hole. At low blowing ratio, the inclined trench is superior, at high blowing ratio, narrow trench wins. The rectangular trench increases the aerodynamic loss, while the inclined trench avail the decrease of the aerodynamic loss.
引用
收藏
页码:518 / 525
页数:8
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