Numerical investigation on film cooling effectiveness of converging slot hole at turbine blade suction surface

被引：0
|
作者：
Yao, Yu [1 ]
Zhang, Jingzhou [1 ]
He, Fei [2 ]
Guo, Wen [3 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
[2] Hongdu Aviation Industry Group, Nanchang 330024, China
[3] China Gas Turbine Establishment, Chengdu 610500, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2010年 / 31卷 / 06期
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D O I：
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学科分类号：
摘要：
14
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页码：1115 / 1120
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