摘要
The paper focuses on the turbo ramjet engine, which is a kind of airbreathing engine.It is expected to apply for hypersonic transport propulsion system. In the process fromturbo mode to ramjet mode, the turbo ramjet composed engine operates through the way ofcombined cycle. In this paper the combined cycle performance was simulated for two layouts.The results show that the laws are feasible.
The paper focuses on the turbo ramjet engine, which is a kind of airbreathing engine.It is expected to apply for hypersonic transport propulsion system. In the process fromturbo mode to ramjet mode, the turbo ramjet composed engine operates through the way ofcombined cycle. In this paper the combined cycle performance was simulated for two layouts.The results show that the laws are feasible.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
1999年第1期9-12,共4页
Journal of Engineering Thermophysics
基金
国家攀登B计划
国家自然科学基金
