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基于PLIF技术的气氧/气甲烷同轴剪切喷嘴试验

俞南嘉 鲍启林 李峰 张洋

俞南嘉, 鲍启林, 李峰, 张洋. 基于PLIF技术的气氧/气甲烷同轴剪切喷嘴试验[J]. 航空动力学报, 2018, 33(10): 2483-2491. doi: 10.13224/j.cnki.jasp.2018.10.021
引用本文: 俞南嘉, 鲍启林, 李峰, 张洋. 基于PLIF技术的气氧/气甲烷同轴剪切喷嘴试验[J]. 航空动力学报, 2018, 33(10): 2483-2491. doi: 10.13224/j.cnki.jasp.2018.10.021
Experiment on coaxial shear injector of GO2/GCH4 based on PLIF[J]. Journal of Aerospace Power, 2018, 33(10): 2483-2491. doi: 10.13224/j.cnki.jasp.2018.10.021
Citation: Experiment on coaxial shear injector of GO2/GCH4 based on PLIF[J]. Journal of Aerospace Power, 2018, 33(10): 2483-2491. doi: 10.13224/j.cnki.jasp.2018.10.021

基于PLIF技术的气氧/气甲烷同轴剪切喷嘴试验

doi: 10.13224/j.cnki.jasp.2018.10.021

Experiment on coaxial shear injector of GO2/GCH4 based on PLIF

  • 摘要: 以数值仿真的结果作为参考,开展了基于PLIF(平面激光诱导荧光)技术、高速摄影技术等非接触光学燃烧诊断技术的气氧/气甲烷同轴剪切喷嘴试验研究。通过联合光学诊断对不同设计工况的燃烧流场进行诊断测量,获得燃烧室内OH分布,燃烧流场发展演化过程、火焰的结构等信息,对燃烧流场进行详细的分析。研究结果表明:气氧/气甲烷剪切燃烧火焰存在明显的剪切燃烧层,且随着轴向距离的增加,火焰逐渐失稳;随燃氧速度比的增加,流场涡旋作用明显加强,火焰根部稳定段变短,瞬时火焰结构卷曲和褶皱增多;仿真计算的OH分布与试验测得的OH分布相似,仿真模型能够合理预测气氧/气甲烷同轴剪切喷嘴的燃烧流场。

     

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出版历程
  • 收稿日期:  2017-06-05
  • 刊出日期:  2018-10-28

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