1) MHD-Arc-Ramjet combined cycle engine
MHD-Arc-Ramjet联合循环发动机
1.
Effects of multi-stage arc on the performance of MHD-Arc-Ramjet combined cycle engine;
多级电弧对MHD-Arc-Ramjet联合循环发动机性能的影响
2) MHD-Arc-Ramjet combined cycle
MHD-Arc-Ramjet联合循环
1.
The disadvantage of energy-reintroduction in AJAX,proposed by Russian as a special case of ranjet engine with energy-bypass system,is explored in this paper,and a new hypersonic propulsive system named as MHD-Arc-Ramjet combined cycle is proposed,which uses arc for energy injection.
热力分析表明:MHD-Arc-Ramjet联合循环的单位推力与AJAX是相当的;由于前者可以在更高的温度下进行能量注入,其在单位推力方面是具有优势的。
2.
And the study results show that under the ideal conditions the specific thrust of AJAX is more than that of MHD-Arc-Ramjet combined cycle,and the latter is superior with the co.
采用热力学方法针对两种带有能量旁路的冲压发动机分别在理想和实际情况下进行了性能分析和比较,结果表明:理想条件下AJAX的单位推力要高于MHD-Arc-Ramjet联合循环;考虑到后者可以在更高的温度下进行能量注入,其在单位推力方面是具有优势的。
3) combined cycle generating unit
联合循环发电机组，联合循环发动机组
4) composite engine,mix cycle engine
混合循环发动机
5) combined cycle engines
组合循环发动机
1.
A brief introduction of the hypersonic airbreathing propulsion system is first given, followed by a de- scriptions of working principles and composition of typical hypersonic airbreathing engines, including scramjet, detonation engine and combined cycle engines.
第2部分介绍了超燃冲压发动机、爆震发动机和组合循环发动机等典型高超声速吸气式发动机的基本工作原理与系统组成,描述了各自的特点。
6) combined cycle power plant(CCPP)
联合循环发电机组(CCPP)
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条