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경계조건에 따른 가스터빈 블레이드 냉각공기 유량변화Effect of Boundary Conditions on the Flow Rate of the Internal Coolant in Gas Turbine Blades
- Other Titles
- Effect of Boundary Conditions on the Flow Rate of the Internal Coolant in Gas Turbine Blades
- Issue Date
- Sep-2001
- Publisher
- 대한설비공학회
- Citation
- 공기조화냉동공학논문집 (설비공학논문집), v.13, no.9, pp 888 - 894
- Pages
- 7
- Journal Title
- 공기조화냉동공학논문집 (설비공학논문집)
- Volume
- 13
- Number
- 9
- Start Page
- 888
- End Page
- 894
- ISSN
- 1229-6422
2465-7611
- Abstract
- Advanced gas turbine engines employ turbine entry temperatures so high that cooling of the turbine blades is essential. The coolant flow introduces losses which need to be minimized, and therefore it is important that the minimum amount of coolant should be used. This work presents the result of the one-dimensional analysis and the effect of the boundary conditions on coolant flow rate in gas turbine blades.
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Collections - 공과대학 > 기계시스템학부 > 1. Journal Articles
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