Numerical Simulation of Internal Flow Field in Transonic Axial Compressor

被引:0
|
作者
Ye, Tao [1 ]
Chen, Fei [1 ]
机构
[1] WHUT, Sch Mech & Elect Engn, Wuhan 430070, Peoples R China
关键词
axial compressor; internal flow field; profile loss; numerical simulation; fitting;
D O I
暂无
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
The transonic axial compressor Stage35 was selected as a research object, using software NUMECA taking numerical simulation of it. And then, the distribution rules of pressure and temperature of meridional channel and blade surface are derived. On this basis, the formation process of shock wave and the influence of it on boundary layer were analyzed in detail. Using the least square cubic fit method, the characteristic curve of the compressor was fitted. The analysis results indicate that the profile loss makes the energy loss of compressor remarkable add, and the characteristic curve can be fitted precisely by using the least square cubic fit method.
引用
收藏
页码:371 / 377
页数:7
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