Corner Separations around a NACA65 Blade in a Decelerating Flow (Experimental Investigations by Five-Hole Probe and PIV)

查看全文 作　　者：Yoichi [1]Kinoue;Ryutaro [1]Ohhira;Norimasa [1]Shiomi;Toshiaki [2]Setoguchi

机构地区：[1]Department of Mechanical Engineering,Saga University;[2]Institute of Ocean Energy,Saga University

出　　处：《Journal of Thermal Science》索引2013年第22卷第1期,共6页

摘　　要：In order to examine the fundamental characteristics of corner separation in a decelerating cascade flow,the experimental apparatus was made and separations around a NACA65 blade in a decelerating channel flow were examined.Two-dimensional calculations show that the NACA65 cascade flow that has 45 deg.of turning,1.24 of solidity and 17 deg.of stagger angle is equivalent to the channel flow that has 14 deg.of stagger angle in terms of pitchwise blade force.Experimental investigation by five-hole probe shows that the accumulations of low energy fluid can be seen around the corner part and the overturning flow due to the secondary flow exists.And,as the periodicity of the blade wake in a pitchwise direction is comparably good,the wake of this channel flow is similar to the wake of the cascade flow for two pitch portion.PIV measurement results shows that a vortex pattern can be seen in the momentary streamline on the suction surface of the blade and in the averaged streamline on the perpendicular to both the suction surface and the endwall. 关键词：五孔探针流分离 PIV实验减速流量刀片 PIV测量叶片力

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Corner Separations around a NACA65 Blade in a Decelerating Flow (Experimental Investigations by Five-Hole Probe and PIV)

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