推进技术 ›› 1991, Vol. 12 ›› Issue (3): 62-70.
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王裕人,刘敬华
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摘要: 本文通过计算分析,探讨了氢、煤油和甲烷三种燃料补氧加热器的性能和结构冷却方案.包括油气比、补氧量、各种成分的重量百分比等对加热空气的影响.这些结果将有助于开展补氧加热器的试验研究.
关键词: 超音速燃烧冲压发动机;燃烧试验;加热器;高空模拟
Abstract: This paper describes the performance analysis of heater and its cooling structure design for three kinds of fuel(hydrogen, kerosene and methan-e). The effect of fuel-air ratio, oxygen supplement, constituent of fuel on the heated air was obtained.These results can used for the development of heater with oxygen supplement.
Key words: Supersonic combustion ramjet engine;Combustion test;Heater;Altitude simulation
王裕人,刘敬华. 补氧加热器性能计算分析[J]. 推进技术, 1991, 12(3): 62-70.
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