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涡轮叶片尾缘针肋的换热研究     被引量:2

Heat transfer in the tail section of channel of cooling blade with pin-fin arrays

文献类型:期刊文献

中文题名:涡轮叶片尾缘针肋的换热研究

英文题名:Heat transfer in the tail section of channel of cooling blade with pin-fin arrays

作者:凌长明[1];刘斌[1];闵春华[1]

机构:[1]湛江海洋大学工程学院,524025

年份:2002

卷号:24

期号:3

起止页码:295

中文期刊名:上海理工大学学报

外文期刊名:Journal of University of Shanghai For Science and Technology

收录:CSTPCD、、北大核心2000、Scopus、北大核心

基金:湛江海洋大学工程热物理重点学科资助项目(200137) ;航空部608所资助项目(200127)

语种:中文

中文关键词:涡轮叶片尾缘针肋;强化传热;形状曲线

外文关键词:pin-fin; enhanced heat transfer; curvilinear shape

中文摘要:以涡轮叶片尾缘中针肋通道的换热为研究对象,讨论并计算出了一定条件下获得最大针肋通道换热量时针肋的形状曲线和换热优势,系统分析了这种拥有最佳形状曲线针肋的通道散热量随针肋物性参数及几何特征变化的规律.

外文摘要:Heat transfer in the tail section of channel of cooling blade with pin-fin arrays is studied. According to the theoretical calculation, a curvilinear pin-fin shape is acquired which make the maximum heat transferred under certain conditions. The quantity of heat transferred is compared with that of corresponding cylindrical pin-fin arrays to show the advantage. Finally, the relations of the heat transfer to the rib's physical parameters or geometrical characters are analyzed systematically.

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