| 超音速气流中氢燃料强化混合的燃烧实验研究 |
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| 引用本文： | 刘敬华,刘兴洲,胡欲立,凌文辉,刘陵,张榛.超音速气流中氢燃料强化混合的燃烧实验研究[J].推进技术,1996,17(1):1-7. |
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| 作者姓名： | 刘敬华 刘兴洲 胡欲立 凌文辉 刘陵 张榛 |
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| 作者单位： | 航天工业总公司３１所，西北工业大学航空动力与热力工程系 |
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| 摘 要： | 扼要介绍了在超音速气流中，采用后掠斜坡、多级喷射、振荡激波技术强化混合的氢燃料喷嘴，进行自点火和燃烧的实验概况。以实验模型结合喷射方式特点，分析了强化机理。实验表明，多级喷射的燃烧效率高，扩张型后掠斜坡喷嘴的抗干扰能力强，总压损失低，液体喷射产生的振荡激波能加强混合，提高燃烧效率。
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| 关 键 词： | 超音速燃烧，氢燃料，燃料喷射，燃烧试验 |
AN EXPERIMENTAL STUDY ON COMBUSTION IN SVPERSONIC FLOW WITH ENHANCED MIXING OF HYDROGEN FUEL |
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| Liu Jinhua, Liu Xingzhou, Hu Yuli, Ling Wenhui.AN EXPERIMENTAL STUDY ON COMBUSTION IN SVPERSONIC FLOW WITH ENHANCED MIXING OF HYDROGEN FUEL[J].Journal of Propulsion Technology,1996,17(1):1-7. |
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| Authors: | Liu Jinhua Liu Xingzhou Hu Yuli Ling Wenhui |
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| Abstract: | An experimental study on autoignition and combustion of hydrogen in supersonicairstrgm, by technique of enhanced mixing injectors with swept ramp, multi--injection and oscillatingshocks, is briefly introducted in this paper. Combined the experimental model with the injection patterns the mechanism of enhanced mixing is analysed. The results indicate that higher combustion efficiency is obtained with multiple injection with expansing ramp injectors, but better anti-interaction ability and lower total pressure loss with the latter. It is also shown that the oscillating shocks generated by liquid injection will enhance mixing and increase combustion efficiency. |
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| Keywords: | Supersonic combustion Hydrogen fuel Fuel injection Combustion test |
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