Experimental study on film cooling performance of imperfect holes

被引:0
|
作者
Ke'nan HUANG [1 ]
Jingzhou ZHANG [1 ,2 ]
Xiaoming TAN [1 ]
Yong SHAN [1 ]
机构
[1] College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics
[2] Collaborative Innovation Center for Advanced Aero-Engine
基金
中国国家自然科学基金;
关键词
Discharge coefficient; Experimental test; Film cooling effectiveness; Heat transfer; In-hole blockage;
D O I
暂无
中图分类号
TK124 [传热学];
学科分类号
080701 ;
摘要
An experimental study is made to investigate the film cooling performance of imperfect holes due to in-hole blockage over a flat plate. A specifically pyramid-shaped element is used to simulate the in-hole blockage. Six in-hole blockage orientations(such as leading-inlet, leading-middle,leading-exit, trailing-inlet, trailing-middle and trailing-exit) and four blocking ratios(ranging from 0.1 to 0.4) are taken into considerations. Based on the experimental results, the influences of in-hole blockage on the film cooling effectiveness and discharge coefficient under typical blowing ratios are analyzed. It is confirmed that the in-hole blockage results in a reduction of discharge coefficient related to the perfect film cooling holes, especially for the leading-exit and trailing-inlet orientations with a big blocking ratio. However, in the view of film cooling effectiveness, the in-hole blockage shows complicated affecting roles. In general, except for the leading-exit orientation, the in-hole blockages produce detrimental influence on the film cooling effectiveness.
引用
收藏
页码:1215 / 1221
页数:7
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