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超声速气流中的斜激波诱导自点火

席文雄 孙明波 李庆

席文雄, 孙明波, 李庆. 超声速气流中的斜激波诱导自点火[J]. 航空动力学报, 2016, 31(2): 377-382. doi: 10.13224/j.cnki.jasp.2016.02.016
引用本文: 席文雄, 孙明波, 李庆. 超声速气流中的斜激波诱导自点火[J]. 航空动力学报, 2016, 31(2): 377-382. doi: 10.13224/j.cnki.jasp.2016.02.016
XI Wen-xiong, SUN Ming-bo, LI Qing. Self-ignition in supersonic flow induced by oblique shock wave[J]. Journal of Aerospace Power, 2016, 31(2): 377-382. doi: 10.13224/j.cnki.jasp.2016.02.016
Citation: XI Wen-xiong, SUN Ming-bo, LI Qing. Self-ignition in supersonic flow induced by oblique shock wave[J]. Journal of Aerospace Power, 2016, 31(2): 377-382. doi: 10.13224/j.cnki.jasp.2016.02.016

超声速气流中的斜激波诱导自点火

doi: 10.13224/j.cnki.jasp.2016.02.016
基金项目: 

激光推进及其应用国家重点实验室开放课题基金

国家自然科学基金(11102230)

详细信息
    作者简介:

    席文雄(1984-),男,江西高安人,助理研究员,博士,研究领域为超燃冲压发动机燃烧过程、火箭发动机系统设计.

  • 中图分类号: V233.3

Self-ignition in supersonic flow induced by oblique shock wave

  • 摘要: 在来流马赫数为2.5的条件下对氢气和乙烯燃料的斜激波诱导自点火过程进行了试验研究.采用纹影和高速摄影获得了自点火初始火核的形成和发展过程.试验考察了不同的来流总温、喷注条件、凹腔长度、斜激波强度等因素对自点火过程和点火边界的影响.研究结果表明:入射斜激波能够提高气流的局部参数起到强化自点火的作用.凹腔内形成的低速回流区有助于初始火核形成后的火核逆流传播,并起到防止初始火核因气流振荡而吹脱的稳定源作用.增加喷注压力、增加凹腔长度、提高来流总温有助于自点火的发生.

     

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出版历程
  • 收稿日期:  2015-07-21
  • 刊出日期:  2016-02-28

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