Numerical study of film cooling characteristics on a rotating turbine blade model

被引：0
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作者：
Yang, Bin [1 ]
Xu, Guoqiang [1 ]
Ding, Shuiting [1 ]
Luo, Xiang [1 ]
机构：
[1] National Key Laboratory on Aeroengines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2008年 / 29卷 / 02期
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页码：274 / 279
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