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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:JiangBin,WANG Song-tao,FENG Guo-tai,WANG Zhong-qi.Aerodynamic design of transonic fan/compressor by 3D viscous RNS combined with genetic algorithms[J].Journal of Harbin Institute Of Technology(New Series),2011,18(2):143-148.DOI:10.11916/j.issn.1005-9113.2011.02.028.
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Aerodynamic design of transonic fan/compressor by 3D viscous RNS combined with genetic algorithms
Author NameAffiliation
JiangBin School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
WANG Song-tao School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
FENG Guo-tai School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
WANG Zhong-qi School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
This paper presents an aerodynamic design of a small transonic fan by 3D viscous RNS solver combined with genetic algorithms.The aerodynamic design system based on the 3D viscous RNS solver reduces the dependency on the design experience for designers.Furthermore the optimum with genetic algorithms is an effective method for improving the transonic fan performance as a part of the design system.The design result showed that the transonic fan designed by this method reaches the design requirement even with more efficiency value.
Key words:  transonic fan  aerodynamic design  shock structure  genetic algorithm
DOI：10.11916/j.issn.1005-9113.2011.02.028
Clc Number:V233
Fund:

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