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用于叶尖射流扩稳的Coanda喷嘴参数化研究
引用本文:王前,胡骏,李亮. 用于叶尖射流扩稳的Coanda喷嘴参数化研究[J]. 航空计算技术, 2014, 0(2): 74-76,80
作者姓名:王前  胡骏  李亮
作者单位:江苏省航空动力系统重点实验室/南京航空航天大学能源与动力学院,江苏南京210016
基金项目:高等学校博士学科点专项科研基金资助(20113218120006)
摘    要:为提高压气机叶尖射流扩稳研究中喷嘴的附壁性能,采用数值方法研究了Coanda表面形式以及喷嘴宽度对Coanda喷嘴附壁性能的影响。计算结果表明:Coanda喷嘴的附壁性能与喷嘴上型线出口段的曲率密切相关,上型线出口段曲率大于1/6 mm-1时,喷嘴的附壁性能随着上型线出口段曲率的减小而提高;上型线出口段曲率减小到1/6 mm-1后,喷嘴的附壁性能不再改变。型线确定后,喷嘴的附壁性能随喷嘴宽度的增大而降低。

关 键 词:压气机  叶尖射流扩稳  Coanda效应  参数化研究

Paar metric Study of Coanda Injector Applied in Compressor Satb ility/Enhancement
WANG Qian,HU Jun,LI Liang. Paar metric Study of Coanda Injector Applied in Compressor Satb ility/Enhancement[J]. Aeronautical Computer Technique, 2014, 0(2): 74-76,80
Authors:WANG Qian  HU Jun  LI Liang
Affiliation:(Jiangsu Province Key Laboratory of Aerospace Power Systems & College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
Abstract:In order to improve the injector wall attachment performance in the research of compressor sta-bility enhancement by tip injection ,the influence of Coanda surface form and injector width on the Coanda injector wall attachment performance was studied by numerical simulation .The results show that:the in-jector wall attachment performance is closely related to the curvature of the upper molded line at the out-let section,when the curvature of the upper molded line at the outlet section exceeds 1/6mm ^-1 , the Coanda injector wall attachment performance improves with the decrease of the curvature ;when the curva-ture of the upper molded line at the outlet section is lower than 1/6 mm^-1 ,the Coanda injector wall at-tachment performance is no longer change with the curvature .When the molded line is determined ,the Coanda injector wall attachment performance decreases with the increase of injector width .
Keywords:compressor  stability enhancement by tip injection  Coanda effect  parametric study
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