Numerical study on impinging cooling for a high-pressure turbine blade

被引：0
|
作者：
Zhu, Wei-Bing [1 ]
Sun, Run-Peng [1 ]
Xu, Ling-Zhi [2 ]
Guo, Hao-Yan [2 ]
机构：
[1] College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China
[2] The 31st Research Institute of CASIC, Beijing 100074, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2012年 / 33卷 / 05期
关键词：
Cooling - Flow of gases - Turbine components - Gas temperature - Fighter aircraft - Numerical methods - Turbomachine blades;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：710 / 718
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