摘要 : Turbine-based combined cycle (TBCC) engines are the most promising propulsion systems for the horizontal takeoff and landing of hypersonic vehicles. However, the high air-inlet temperature, engine-wall temperature, and electrical-... 展开
作者 | Yinhai Zhu Xiaofeng Ma Peixue Jiang |
---|---|
作者单位 | |
期刊名称 | 《Applied thermal engineering: Design, processes, equipment, economics》 |
总页数 | 15 |
语种/中图分类号 | 英语 / TK12 |
关键词 | Hypersonic vehicle Turbine-based combined cycle Limited cold source Brayton cycle Supercritical CO_2 Optimization |
馆藏号 | N2007EPST0002837 |