超声速燃烧冲压发动机 Supersonic combustion ramjet
对采用高温富油燃气作引导火焰的煤油超声速燃烧进行了研究。
Experimental investigation on supersonic combustion of kerosene was conducted using fuel-rich hot gas as pilot flame on direct-connect supersonic combustion facility.
结果表明激波风洞用于超声速燃烧研究的一些必要的技术问题已基本解决。
The results show that some of technological problems for experimental investigation on supersonic combustion with shock tunnels have been solved basically.
研究了超声速预混可燃气流的温度以及当量比对超声速燃烧流场结构、点火与火焰传播特性的影响。
The effects of temperature and equivalence ratio of supersonic premixed combustible flow on the structure of supersonic combustion flow field, ignition and flame propagation were studied.
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