摘要
The arrangement of turbine based combined cycle engines were investigated. Co-axial and tandem configuration was selected as a turbofan-ram combined engine. The design parameters of both turbofan engine and ramjet were laid out, and the rules were expounded to explain how to ascertain the transition point of operation mode. Based on a modular structure code, the performance characteristic of turbo-ramjet was simulated by numerical method.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 1-4+51 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 30 |
| 期 | 1 |
| 出版状态 | 已出版 - 2月 2009 |