摘要
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.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 62-68 |
| 页数 | 7 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 18 |
| 期 | 5 |
| 出版状态 | 已出版 - 1997 |
指纹
探究 'The effect of transient heat transfer on compressor surge margin' 的科研主题。它们共同构成独一无二的指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver