The results show that the software is applicable to RBCC motor performance analysis.
结果表明，该软件适用于RBCC发动机性能分析。
As for the research of the performance of the motor, the directed RBCC is adopted mostly.
对于发动机性能的研究，国内外大多采用直连式RBCC实验系统进行研究。
By applying the obtained thrust augmentation mechanism, an improved RBCC configuration was proposed.
应用研究获得的推力增强机理提出了实验样机构型的改进方案。
This paper aims designs the ground test system of direct-connect RBCC, and disposes of the experimental data.
本文就是针对这一有效的方法，进行了直连式RBCC发动机地面实验，对实验数据进行了处理。
The investigation lays a fine foundation for realizing stable high efficient combustion based on the thermal throat RBCC ramjet mode.
研究工作为实现基于热力喉道的RBCC亚燃模态稳定高效燃烧提供了良好的基础。
The progress in subsonic and supersonic combustions has been attained, but the ejecting mode and mode match of RBCC has just been begun.
国内已制定了研究计划并正在开展，其中亚燃和超燃模态的研究取得了相当的进展，但引射模态以及模态匹配的研究还刚刚起步。
It is in the first time in domestic RBCC researches that the RBCC configuration with relatively higher thrust augmentation in ejecting mode is obtained.
在国内RBCC研究中首次从理论上获得了具有较高推力增强的RBCC引射模态方案，对开展RBCC引射模态研究有重要意义。
In ejector and ramjet modes, working over a wide Mach number range is very important for the RBCC inlet, so the 2d RBCC inlet should be variable-geometry.
对工作于引射和亚燃模态的RBCC发动机进气道来说，宽马赫数工作的要求显得尤为突出，使得二元进气道应采用变几何结构。
Secondary combustion was experimentally investigated to improve thrust of rocket ejector mode of RBCC, and to find the influence of thermal choke on thrust.
为了提高RBCC引射火箭模态的推力性能，探索热力壅塞对引射模态推力的影响，开展了二次燃烧实验研究。
The present situation and progress of investigation on rocket based combined cycle (RBCC) propulsion system was introduced both at home and abroad in details.
对火箭基组合循环(RBCC)推进系统的国内外研究现状和进展进行了详细综述。
Strutjet is a new kind of Rocket Based Combined Cycle (RBCC), and is an integrated propulsion system that can satisfy low cost and high performance requirements.
支板簇引射发动机是火箭基组合循环(RBCC)方案的一种基础动力，是为满足低费用高性能要求而提出的组合推进系统。
RBCC engine performance analysis model plays an important part in scheme selection and model design for Hypersonic Flight Vehicle, RBCC engine design and performance analysis.
RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。
RBCC engine performance analysis model plays an important part in scheme selection and model design for Hypersonic Flight Vehicle, RBCC engine design and performance analysis.
RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。
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