期刊文献+

Aerodynamic design of transonic fan/compressor by 3D viscous RNS combined with genetic algorithms

Aerodynamic design of transonic fan/compressor by 3D viscous RNS combined with genetic algorithms
下载PDF
导出
摘要 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. This paper presents an aerodynamic design of a small transonic fan by 3D viscous RNS solver com- bined 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.
出处 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2011年第2期143-148,共6页 哈尔滨工业大学学报(英文版)
基金 Sponsored by the Major State Basic Research Development Progrma of China(Grant No. 2007CB210104)
关键词 transonic fan aerodynamic design shock structure genetic algorithm transonic fan aerodynamic design shock structure genetic algorithm
  • 相关文献

参考文献7

  • 1Weingold H D.Reduction of compressor stator endwall losses through the use of bowed stators.ASME 95-GT380,1995.
  • 2Fischer A,Riess W,Seurae J R.Performance of strongly bowed stators in a 4-stage high speed compressor.ASME GT2003-38392,2003.
  • 3Glimmer V,Wenger U,Kau H P.Using sweep and dihedral to control three-dimensional flow in transonic stators of axial compressor.Journal of Turbomachinery,2001,123 (1):40-48.
  • 4Gallimore S J,Bolger J J,Cumpsty N A,et al.The use of sweep and dihedral in multistage axial flow compressor bla-ding,Part 1:university research and methods development.ASME GT-2002-30328,2002.
  • 5Yang Ke.Turbomachinary Optimization and Design Based on CFD Technology:Theory and Practice.Beijing:Institute of Engineering Thermophysics,Chinese Academy of Sciences,2007.7.
  • 6Li Shaobin.Design of Highly Loaded Dihedral Stator and Investigation on the Aerodynamic Stage Performance in an Axial Transonic Compressor.Harbin:Harbin Institute of Technology,2007.
  • 7Reid L,Moore R D.Performance of single-stage axial-flow transonic compressor with rotor and atator aspect ratios of 1.19 and 1.26,respectively,and with design pressure.NASA-TP-1338,1978.

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部