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氧化剂环缝宽度对旋转爆震波传播特性影响的实验

赵明皓 王可 朱亦圆 张玉坤 黄忻昱 范玮

赵明皓, 王可, 朱亦圆, 等. 氧化剂环缝宽度对旋转爆震波传播特性影响的实验[J]. 航空动力学报, 2023, 38(8):1984-1994 doi: 10.13224/j.cnki.jasp.20210637
引用本文: 赵明皓, 王可, 朱亦圆, 等. 氧化剂环缝宽度对旋转爆震波传播特性影响的实验[J]. 航空动力学报, 2023, 38(8):1984-1994 doi: 10.13224/j.cnki.jasp.20210637
ZHAO Minghao, WANG Ke, ZHU Yiyuan, et al. Experiment on propagation characteristics of rotating detonation waves in different oxidizer inlet slots[J]. Journal of Aerospace Power, 2023, 38(8):1984-1994 doi: 10.13224/j.cnki.jasp.20210637
Citation: ZHAO Minghao, WANG Ke, ZHU Yiyuan, et al. Experiment on propagation characteristics of rotating detonation waves in different oxidizer inlet slots[J]. Journal of Aerospace Power, 2023, 38(8):1984-1994 doi: 10.13224/j.cnki.jasp.20210637

氧化剂环缝宽度对旋转爆震波传播特性影响的实验

doi: 10.13224/j.cnki.jasp.20210637
基金项目: 国家自然科学基金(52076181,52176133); 陕西省创新能力支撑计划项目(2021KJXX-93);中央高校基本科研业务费项目(3102019ZX024); 西北工业大学博士论文创新基金(CX2021072)
详细信息
    作者简介:

    赵明皓(1995-),男,博士生,主要从事爆震燃烧与爆震推进研究

    通讯作者:

    王可(1986-),男,教授,博士,主要从事爆震燃烧与爆震推进研究。E-mail:wangk@nwpu.edu.cn

  • 中图分类号: V231.2

Experiment on propagation characteristics of rotating detonation waves in different oxidizer inlet slots

  • 摘要:

    为了揭示氧化剂环缝宽度对旋转爆震波传播特性的影响,在凹腔形旋转爆震燃烧室中,采用环缝-喷孔式喷注器,燃料和氧化剂分别为乙烯和氧气体积分数为50%的富氧空气,实验研究了氧化剂环缝宽度对旋转爆震波传播模态及传播特性的影响。结果表明:在不同氧化剂环缝宽度下,均成功实现了旋转爆震波的稳定传播,并观察到稳定爆震、周期性振荡和非周期性振荡3种模态;周期性振荡模态的当量比范围随着氧化剂环缝宽度的增加而扩大,且每个振荡周期包括爆震波解耦、缓燃波加速和爆震波形成3个过程;与稳定爆震模态相比,在两种振荡模态中,燃烧波的平均传播速度大幅降低且存在较大的速度波动。

     

  • 图 1  实验系统示意图

    Figure 1.  Schematic diagram of the experimental system

    图 2  旋转爆震燃烧室示意图

    Figure 2.  Schematic diagram of the rotating detonation chamber

    图 3  压力传感器分布

    Figure 3.  Distribution of the pressure transducers

    图 4  稳定爆震模态的压力波形

    Figure 4.  Pressure profiles measured at the stable detonation mode

    图 5  稳定爆震模态的传播速度分布

    Figure 5.  Propagation velocities distribution of the stable detonation mode

    图 6  稳定爆震模态的STFT和FFT结果

    Figure 6.  STFT and FFT results of the stable detonation mode

    图 7  稳定爆震模态的起始过程压力波形

    Figure 7.  Pressure profiles of the initiation process measured at the stable detonation mode

    图 8  周期性振荡模态的压力波形

    Figure 8.  Pressure profiles measured at the periodic oscillation mode

    图 9  周期性振荡模态的传播速度分布

    Figure 9.  Propagation velocities distribution of the periodic oscillation mode

    图 10  周期性振荡模态的STFT和FFT结果

    Figure 10.  STFT and FFT results of the periodic oscillation mode

    图 11  周期性振荡模态的起始过程压力波形

    Figure 11.  Pressure profiles of the initiation process measured at the periodic oscillation mode

    图 12  非周期性振荡模态的压力波形

    Figure 12.  Pressure profiles measured at the aperiodic oscillation mode

    图 13  非周期性振荡模态的传播速度分布

    Figure 13.  Propagation velocities distribution of the aperiodic oscillation mode

    图 14  非周期性振荡模态的STFT和FFT结果

    Figure 14.  STFT and FFT results of the aperiodic oscillation mode

    图 15  非周期性振荡模态的起始过程压力波形

    Figure 15.  Pressure profiles of the initiation process measured at the aperiodic oscillation mode

    图 16  不同传播模态的工作范围

    Figure 16.  Operating ranges of different propagation modes

    图 17  喷注压比随当量比的变化

    Figure 17.  Injection pressure ratio with equivalent ratio

    图 18  3种模态的平均传播速度

    Figure 18.  Average propagation velocities of three modes

    图 19  传播速度标准差分布

    Figure 19.  Standard deviations distribution of the propagation velocity

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  • 收稿日期:  2021-11-08
  • 网络出版日期:  2023-04-03

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