가스터빈 날개의 냉각에 대한 연구동향

• 영문명: A Review of the Study on a blade cooling for the Gas Turbine
• 발행기관: 한국항해항만학회
• 저자명: 장태현(Tae-Hyun Chang) 길상철(Sang-Cheol Kil) 조홍곤(Hung-Gon Cho)
• 간행물 정보: 『한국항해항만학회 학술대회논문집』2008년도 공동학술대회 지구환경변화와 해양산업의 전망 논문집, 287~289쪽, 전체 3쪽
• 주제분류: 공학 > 해양공학
• 파일형태: PDF
• 발행일자: 2008.06.30

영문 초록

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.

목차

Abstract

1. 서론

2. 수치해석적 연구

4. 결론

후기

References

키워드

Gas turbine blade cooling Cooling channel Leading edge