Effect of attack angle and jet height on impingement and film composite cooling of turbine blade leading edge

Author
Liu, Zhao
International Society for Air Breathing Engines
Ye, Lv
Yang, Xing
Feng, Zhenping
Date
2015-10-22
Item Type
Degree Name
Academic Department
Identifiers
20109
Keywords
Subject
Thermal management: Cooling technology
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Abstract
Description
This paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.
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