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涡轮叶片尾缘针肋的换热研究
引用本文:凌长明,刘斌,闵春华. 涡轮叶片尾缘针肋的换热研究[J]. 上海理工大学学报(社会科学版), 2002, 24(3): 295-298
作者姓名:凌长明  刘斌  闵春华
作者单位:湛江海洋大学工程学院 524025(凌长明,刘斌),湛江海洋大学工程学院 524025(闵春华)
基金项目: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)
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。

关 键 词:涡轮叶片尾缘针肋 强化传热 形状曲线

Heat transfer in the tail section of channel of cooling blade with pin-fin arrays
LING Chang-ming,LIU Bin,MIN Chun-hua. Heat transfer in the tail section of channel of cooling blade with pin-fin arrays[J]. Journal of University of Shanghai For Science and Technilogy(Social Science), 2002, 24(3): 295-298
Authors:LING Chang-ming  LIU Bin  MIN Chun-hua
Abstract: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.
Keywords:pin-fin  enhanced heat transfer  curvilinear shape  
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