학술대회자료
가스터빈 날개의 냉각에 대한 연구동향
A Review of the Study on a blade cooling for the Gas Turbine
- 한국항해항만학회
- 한국항해항만학회 학술대회논문집
- 2008년도 공동학술대회 지구환경변화와 해양산업의 전망 논문집
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2008.06287 - 289 (3 pages)
- 38
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.
Abstract
1. 서론
2. 수치해석적 연구
4. 결론
후기
References
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