Numerical investigation on the effect of different anti-vortex hole configurations on film cooling effectiveness

被引:0
作者
Wu, Hong [1 ]
Meng, Heng-Hui [2 ]
Tao, Zhi [1 ]
Xu, Guo-Qiang [1 ]
Ding, Shui-Ting [1 ]
机构
[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
[2] Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology, China Aerospace Science and Technology Corporation, Beijing 100063, China
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2010年 / 25卷 / 10期
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12
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页码:2238 / 2243
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