| 亚／超双模态超音速燃烧的实验研究 |
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| 引用本文： | 刘敬华,凌文辉,胡欲立,刘兴洲,于守志.亚／超双模态超音速燃烧的实验研究[J].推进技术,1996,17(2):48-52. |
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| 作者姓名： | 刘敬华 凌文辉 胡欲立 刘兴洲 于守志 |
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| 作者单位： | 航天工业总公司３１所 |
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| 摘 要： | 描述了在超音速燃烧室中如何从亚音速燃烧模态转变为超音速燃烧模态的概念和目前的研究状态，并用实验表明改变氢燃料喷射位置和当量比对燃烧状态的影响，以及燃烧室各截面参数的变化规律。
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| 关 键 词： | 超音速冲压喷气发动机，超音速燃烧，亚超音速燃烧，氢燃料 |
AN EXPERIMENTAL STUDY ON SUB/SUPER DUAL MODE SUPERSONIC COMBUSTION |
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| Liu Jinghu,Ling Wenhui,FuYuli,Liu Xingzhou and Yu Shouzhi.AN EXPERIMENTAL STUDY ON SUB/SUPER DUAL MODE SUPERSONIC COMBUSTION[J].Journal of Propulsion Technology,1996,17(2):48-52. |
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| Authors: | Liu Jinghu Ling Wenhui FuYuli Liu Xingzhou and Yu Shouzhi |
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| Institution: | The 31sr Research Inst., Beijing, 100074;The 31sr Research Inst., Beijing, 100074;The 31sr Research Inst., Beijing, 100074;The 31sr Research Inst., Beijing, 100074;The 31sr Research Inst., Beijing, 100074 |
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| Abstract: | In this paper the principle and current condition of study are described that how totransfer subsonic combustion into supersonic combustion in chamber. The experiment shows thevariations of parameters at sections along combustor and the effects of injector location and fuel/airratio on combustion state |
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| Keywords: | Supersonic combustion ramjet engine Supersonic combustion Subsonic combustion Hydogen fuel |
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