Journal of the Korean Society of Industry Convergence (한국산업융합학회 논문집)
- Volume 11 Issue 2
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- Pages.65-70
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- 2008
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- 1226-833X(pISSN)
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- 2765-5415(eISSN)
A Review of the Study on a Blade Cooling for the Gas Turbine
가스터빈 날개의 냉각에 대한 연구동향
- Chang, Tae-Hyun (Korea Institute of Science and Technology Information) ;
- Kil, Sang-Cheol (Korea Institute of Science and Technology Information) ;
- Cho, Hung-Gon (Korea Institute of Science and Technology Information)
- Received : 2008.02.05
- Accepted : 2008.05.23
- Published : 2008.05.31
Abstract
This study presents gas turbine cooling blade by using experimental and numerical works. The review cover researches related to cooling channels using finite element method in rotating blade. Also, the film cooling device and the heat transfer of the external surface of the blade are included. In addition, several methods to be used for the design of the blade, numerical method and experimental techniques are introduced. This work will contribute to improving the manufacturing of engine and the efficiency of gas turbine engines.