Effects of Leading Edge Injection on the Film Cooling Characteristics of Multirow Cooling Holes on the Turbine Vane Suction Side

被引：0
|
作者：
Yao, Chun-Yi [1 ]
Zhu, Hui-Ren [1 ,2 ]
Li, Xin-Lei [1 ]
Liu, Cun-Liang [1 ,2 ]
Guo, Wen [3 ]
Liu, Song [3 ]
Li, Shi-Feng [3 ]
机构：
[1] School of Power and Energy, Northwestern Polytechnical University, Xi'an,710129, China
[2] Shaanxi Key Laboratory of Thermal Sciences in Aero-Engine System, Northwestern Polytechnical University, Xi'an,710129, China
[3] AECC Sichuan Gas Turbine Establishment, Chengdu,610500, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2021年 / 42卷 / 03期
关键词：
D O I：
10.13675/j.cnki.tjjs.190672
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学科分类号：
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页码：620 / 629
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