Cooling efficiency study of impingement pin fin /reversed convection/ film cooling in curved section Part 1: experiments
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Cooling efficiency study of impingement pin fin /reversed convection/ film cooling in curved section Part 1: experiments
Vol. 26, Issue 4, (2011)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 长沙航空职业技术学院 航空装备维修工程系,长沙,410124
3. 中国航空工业集团公司 中国航空动力机械研究所,湖南,株洲,412002
作者简介:
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Published:2011
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SHI Rui, XIONG Chun, CAO Jun, et al. Cooling efficiency study of impingement pin fin /reversed convection/ film cooling in curved section Part 1: experiments[J]. 2011, 26(4).
DOI:
SHI Rui, XIONG Chun, CAO Jun, et al. Cooling efficiency study of impingement pin fin /reversed convection/ film cooling in curved section Part 1: experiments[J]. 2011, 26(4).DOI:
Cooling efficiency study of impingement pin fin /reversed convection/ film cooling in curved section Part 1: experiments
In order to study the influence of impingement pin fin/reversed convection/film cooling structure on cooling efficiency in curved section of combustion chamber
five different kinds of geometry dimension test pieces were designed and studied experimentally.The test results show that:(1) The efficiency of impingement pin fin/reversed convection/film cooling in curved section with pin fins is better than that without pin fins
especially when the blowing ratio is small.(2) The blowing ratio has great influence on the efficiency of compound cooling;the efficiency of compound cooling increases with the blowing ratio at the same wall position.When the blowing ratio exceeds 1.0
efficiency improvement for blowing ratio is not obvious.(3) The arrangement of pin fins has little effect on cooling efficiency.