在激波风洞一激波管组合设备上开展了碳氢燃料超声速预混可燃气流的点火与燃烧实验研究。

Experimental investigation on ignition and combustion of supersonic premixed hydrocarbon fuel-air mixture has been conducted in the combination facility consisting of a shock tunnel and a shock tube.

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对目前广泛采用的各种燃烧系统，分析揭示了其能量效益与燃气终温以及系统中各设备的分效率之间的内在规律。

For combustion systems in wide-ranging applications the analysis has proved: the energy cost for combustion systems vary as gas temperature and component efficiencies.

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对目前广泛采用的各种燃烧系统，分析揭示了其能量效益与燃气终温以及系统中各设备的分效率之间的内在规律。

For combustion systems in wide-ranging applications the analysis has proved: the energy cost for combustion systems vary as gas temperature and component efficiencies.

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