Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 1-4+51 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 30 |
| Issue number | 1 |
| State | Published - Feb 2009 |
Keywords
- Numerical simulation
- Performance
- Turbine based combined cycle propulsion system