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A NEW METHOD TO JUDGE THE ENHANCEMENT OF HEAT TRANSFER IN THE TRAILING EDGE OF TURBINE BLADES

A NEW METHOD TO JUDGE THE ENHANCEMENT OF HEAT TRANSFER IN THE TRAILING EDGE OF TURBINE BLADES
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摘要 An experimental investigation of heat transfer and friction loss with taper pin fin configurations were dealed with. Three kinds of configurations-full cross pin fins (FCF), shorter round pin fins (SRF) and taper pin fins (TPF), with different height md spacing of the fins and friction loss are compared with each other. Besides, a new dimensionless number, the ratio of f to Nu, cslled here the specific friction loss, is put forward to judge the validity of configurations. The comparison obviously shows that:
出处 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 1994年第2期170-176,共7页 南京航空航天大学学报(英文版)
关键词 HEAT flux cooling BLADES pressure drag BEAT TRANSFER with pin fin EXPERIMENTATION heat flux cooling blades pressure drag beat transfer with pin fin experimentation
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