摘要
In order to provide a professional blade design software with easily operation and perfect function for those turbomachinery blade designers, one set of blade optimization design system with some intelligent capability was developed by applying advanced artificial neural network method. The second stators optimization reshape of a three stages axial compressor and the second rotor's optimization reshape of a two stages fan compressor were used to validate this software system. The comparison analysis result of aero-dynamical performance between the two original blades and the two optimized blades shows that this software has friendly interface and strong function and some intelligence, which can meet all of basic requirements for blade design and blade optimization design.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 1859-1862 |
| 页数 | 4 |
| 期刊 | Zhongguo Jixie Gongcheng/China Mechanical Engineering |
| 卷 | 18 |
| 期 | 15 |
| 出版状态 | 已出版 - 10 8月 2007 |