1) Rocket-based combined cycle (RBCC)
支板火箭引射冲压组合发动机
2) ejector rocket motor
引射火箭发动机
1.
Based on comprehensive analysis for combustion mode of ejector rocket,the numerical analysis of SMC+DAB hybrid combustion mode and direct connected experiments for the ejector rocket motor with fixed structure were carryied out by means of the essential principle of dual-combustor ramjet.
在综合分析引射火箭燃烧组织模式的基础上,针对固定结构的引射火箭发动机,借助双燃烧室冲压发动机的原理,开展了SMC+DAB混合燃烧组织模式的数值分析和发动机直连实验研究,详细分析了富燃一次燃气对二次燃烧火焰稳定的作用及其对发动机性能的影响。
3) Ducted rocket engine
冲压火箭发动机
5) solid rocket ramjet
固体火箭冲压发动机
1.
Quick-forecasting algorithm for performance of solid rocket ramjet;
固体火箭冲压发动机性能快速预估算法
2.
Some technological problems of solid rocket ramjet;
固体火箭冲压发动机的若干技术问题
3.
Experimental study on solid rocket ramjet with central air-inlet mode;
中心进气式固体火箭冲压发动机试验研究
6) ducted rocket motor
固体火箭冲压发动机
1.
There are a variety of influential factors to the combustion efficiency of secondary chamber of boron-based propellant ducted rocket motor,which are difficult to be expressed accurately by analytical functions.
影响含硼推进剂固体火箭冲压发动机补燃室燃烧效率的因素很多,且各因素对燃烧效率的影响很难用精确的解析函数式来表示。
补充资料：所引支
【所引支】
（术语）为十二支中无明行二能引支引起之识，名色，六处，触，受之五支也。
（术语）为十二支中无明行二能引支引起之识，名色，六处，触，受之五支也。
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