Conjugate heat transfer analysis of convection-cooled turbine vanes using ã-reè transition model

被引：0
|
作者：
Lin, Gang [1 ]
Kusterer, Karsten [1 ]
Ayed, Anis Haj [1 ]
Bohn, Dieter [2 ]
Sugimoto, Takao [3 ]
机构：
[1] 1 BB-AGEMA GmbH, Jülicher Strasse 338, Aachen,52070, Germany
[2] RWTH Aachen University, Germany
[3] University of Hyogo, Japan
来源：
International Journal of Gas Turbine, Propulsion and Power Systems | 2014年 / 6卷 / 03期
关键词：
Aircraft engines - Flow of fluids - Gas turbines - Heat convection - Numerical methods - Turbine components - Turbomachine blades;
D O I：
10.38036/jgpp.6.3_9
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：9 / 15
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