风扇/压气机气动设计系统建设初探

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Preliminary development of fan and compressor aerodynamic design system

摘要: 简述了中国一航沈阳发动机设计研究所风扇/压气机气动设计系统建设的基本思路.为了积累设计经验、规范设计方法、减轻设计人员劳动强度、提高设计效率和可靠性, 在多年风扇/压气机设计及型号研制的基础上, 初步完成了可视化、网络化的风扇/压气机现代气动设计系统的建设.该系统已经过初步测试, 现已应用于工程设计中.
- 航空、航天推进系统 /
- 风扇 /
- 压气机 /
- 气动设计系统
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.
- aerospace propulsion system /
- fan /
- compressor /
- aerodynamic design system

[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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