Volume 22 Issue 3
Mar.  2007
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DU Hui, CHEN Bao-shi, HU Guo-rong, JIANG Da-zhi. Preliminary development of fan and compressor aerodynamic design system[J]. Journal of Aerospace Power, 2007, 22(3): 454-459.
Citation: DU Hui, CHEN Bao-shi, HU Guo-rong, JIANG Da-zhi. Preliminary development of fan and compressor aerodynamic design system[J]. Journal of Aerospace Power, 2007, 22(3): 454-459.
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Preliminary development of fan and compressor aerodynamic design system

  • Shenyang Aeroengine Research Institute(SAeRI), AVIC Ⅰ, Shenyang 110015, China

  • Received Date: 2006-03-24
  • Rev Recd Date: 2006-07-05
  • Publish Date: 2007-03-28
    Abstract
  • This paper provides a brief introduction of the development of SAeRI's Fan and compressor aerodynamic design system.The new developed system is also a platform to cumulate experience and design rules.Emphasis was place on making the system efficient,easy to use and flexible.Now the system has been used in compressor design.

     

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    • References(3)
  • [1]
    Miller M J,Durschmidt D F,Medlock A,et al.An integrated design system for fan,compressor and turbines-Part 1 overview[R].ASME GT2004-53631.
    [2]
    Sandel W A,Miller M J.An integrated design system for fan,compressor,and turbines-Part 2 interactive interface[R].ASME GT2004-53632.
    [3]
    Durschmidt D F,Medlock A,Miller M J.An integrated design system for fan,compressor,and turbines-Part 3 fan and compressor airfoil geometry generators[R].ASME GT2004-53633.
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