摘要
The radial-equilibrium equation and multi-sector parallel compressor model are used to settle complex distorted flow field in this paper. The effects of inlet flow field combined distortion on compressor characteristics and performance are calculated. The details of compressor flow field with inlet distortion are described.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 82-86 |
| 页数 | 5 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 18 |
| 期 | 5 |
| 出版状态 | 已出版 - 1997 |