Effect of showerhead injection of leading edge on cooling characteristics for turbine vane pressure side

被引：0
|
作者：
Yao, Chunyi [1 ]
Zhu, Huiren [1 ,2 ]
Li, Xinlei [1 ]
Liu, Cunliang [1 ,2 ]
Guo, Wen [3 ]
Liu, Song [3 ]
Li, Shifeng [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] Sichuan Gas Turbine Establishment, Aero Engine Corporation of China, Chengdu,610500, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2020年 / 35卷 / 04期
关键词：
25;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：693 / 703
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