Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 82-86 |
| Number of pages | 5 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 18 |
| Issue number | 5 |
| State | Published - 1997 |
Keywords
- Axial flow compressor
- Flow distortion
- Numerical calculation