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利用液晶测量吹风比对尾缘半劈缝换热特性的影响(英文)
引用本文:Yuan Hepeng,Zhu Huiren*,Kong Manzhao School of Power and Energy,Northwestern Polytechnical University,Xi’an ,China.利用液晶测量吹风比对尾缘半劈缝换热特性的影响(英文)[J].中国航空学报,2008,21(6):488-495.
作者姓名:Yuan Hepeng  Zhu Huiren*  Kong Manzhao School of Power and Energy  Northwestern Polytechnical University  Xi’an  China
作者单位:西北工业大学动力与能源学院
基金项目:国家重点基础研究发展规划(973计划) 
摘    要:This article deals with the effects of a blowing ratio measured with narrowband liquid crystal in transonic experiments on the heat transfer characteristics of trailing edge cutback. The experimental results are compared and contrasted in terms of available data for traditional experiments with thermocouples. It is concluded that the blowing ratio exerts rather significant effects on film cooling effectiveness distribution of the rib center line. As the blowing ratio decreases, similar to the cooling effectiveness distribution curve of the slot center line, that of the rib center line makes a clockwise rotation about the end. When the blowing ratio increases, the regular film cooling effectiveness curve of the surface becomes rather smooth. On the whole measuring surface, the most intensive heat transfer occurs at the extended borderline of the slot and the rib, neither at the rib center line nor at the slot center line. The experimental results of cooling effectiveness measured with thermocouples are lower than those with liquid crystal. In addition, the transient experiments using narrowband liquid crystal can eliminate the higher errors of Nusselt numbers in measurements with thermocouples at the slot outlet.

关 键 词:涡轮叶片  拖尾边缘  热量传输系数  薄膜冷却有效性  液体晶体
收稿时间:21 April 2008

Effects of Blowing Ratio Measured by Liquid Crystal on Heat Transfer Characteristics of Trailing Edge Cutback
Yuan Hepeng,Zhu Huiren,Kong Manzhao.Effects of Blowing Ratio Measured by Liquid Crystal on Heat Transfer Characteristics of Trailing Edge Cutback[J].Chinese Journal of Aeronautics,2008,21(6):488-495.
Authors:Yuan Hepeng  Zhu Huiren  Kong Manzhao
Institution:aSchool of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:This article deals with the effects of a blowing ratio measured with narrowband liquid crystal in transonic experiments on the heat transfer characteristics of trailing edge cutback.The experimental results are compared and contrasted in terms of available data for tra-ditional experiments with thermocouples.It is concluded that the blowing ratio exerts rather significant effects on film cooling effec-tiveness distribution of the rib center line.As the blowing ratio decreases,similar to the cooling effectiveness distribution curve of the slot center line,that of the rib center line makes a clockwise rotation about the end.When the blowing ratio increases,the regular film cooling effectiveness curve of the surface becomes rather smooth.On the whole measuring surface,the most intensive heat transfer oc-curs at the extended borderline of the slot and the rib,neither at the rib center line nor at the slot center line.The experimental results of cooling effectiveness measured with thermocouples are lower than those with liquid crystal.In addition,the transient experiments using narrowband liquid crystal can eliminate the higher errors of Nusselt numbers in measurements with thermocouples at the slot outlet.
Keywords:turbine blade  trailing edge  heat transfer coefficient  film cooling effectiveness  thermo-chromic liquid crystal
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