Abstract
The effect of transient heat transfer on the stability of axial flow compressor is analyzed. Based on the analysis, the mathematical model is established to study the effect of transient heat transfer on compressor surge margin. According to the established model, a turbofan engine with compression ratio 26 is investigated. The results show the validation of the model.
| Original language | English |
|---|---|
| Pages (from-to) | 62-68 |
| Number of pages | 7 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 18 |
| Issue number | 5 |
| State | Published - 1997 |
Keywords
- Air compressor
- Heat transfer
- Stability
- Transient response
- Turbofan engine