摘要
On the basis of the thermodynamics model of two-spool turbofan engine, the performance of two-spool turbofan engine was improved by after-burning between high and low turbines. Effects of after-burning between high and low turbines on altitude, velocity and rotational speed characters were studied. The results show that the thrust is obviously increased and SFC maintained on basic level or decreased after adopting the after-burning between high and low turbines.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 453-456 |
| 页数 | 4 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 23 |
| 期 | 6 |
| 出版状态 | 已出版 - 12月 2002 |