摘要
The flow field and aerodynamic design characteristics of core driven fan stage(CDFS) were simulated and analyzed with modified Denton code. The results show that: 1)adjustable inlet guide vane (IGV) is needed to achieve the switch of different working modes; 2) the conflict between high tip speed and low aerodynamic loading restrains the efficiency of CDFS; 3) IGV outlet swirl distribution and switch mode have remarkable effects on CDFS performance; 4) the challenge in the aerodynamic design of CDFS rotor is the shock loss in single bypass mode; 5) the change in distribution and magnitude of CDFS stator inlet flow angle is the main challenge in CDFS stator design.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 434-442 |
| 页数 | 9 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 25 |
| 期 | 2 |
| 出版状态 | 已出版 - 2月 2010 |
学术指纹
探究 'Analysis of aerodynamic design characteristics of core driven fan stage' 的科研主题。它们共同构成独一无二的学术指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver