Heat Transfer Coefficient of Film Cooling with Ellipse-Shaped Tab

被引:1
|
作者
Zheng Xianwu [1 ]
Yang Weihua [2 ]
机构
[1] China Aviation Powerplant Research Institute
[2] College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
基金
中国国家自然科学基金;
关键词
energy and power engineering; turbine machine; ellipse-shaped tab; film cooling;
D O I
10.16356/j.1005-1120.2016.02.155
中图分类号
V231.1 [热力学、传热];
学科分类号
082502 ;
摘要
The enhanced cooling performance caused by ellipse-shaped tabs located at the outlet of the film cooling holes is conducted.Three covering ratios of ellipse-shaped tabs on film holes and four blowing ratios are studied.The results show that:(1)The heat transfer coefficient ratio is higher than that without tab,indicating that the mixing of mainstream and coolant jet provides a better coverage film on the cooling wall,but increases the local turbulence production which enhances the heat transfer coefficient;(2)When the ellipse-shaped tabs are located at the film hole outlet,there is a larger pressure drop with the ellipse tab relative to the no-tab case.Thus,the discharge coefficient with ellipse tab is lower than that without tab.
引用
收藏
页码:155 / 165
页数:11
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