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离心喷嘴气涡固有声学频率预测

乔兴伟 孙纪国 刘倩

乔兴伟, 孙纪国, 刘倩. 离心喷嘴气涡固有声学频率预测[J]. 航空动力学报, 2023, 38(12):2895-2904 doi: 10.13224/j.cnki.jasp.20220054
引用本文: 乔兴伟, 孙纪国, 刘倩. 离心喷嘴气涡固有声学频率预测[J]. 航空动力学报, 2023, 38(12):2895-2904 doi: 10.13224/j.cnki.jasp.20220054
QIAO Xingwei, SUN Jiguo, LIU Qian. Prediction of natural acoustic frequency of gas core in centrifugal injector[J]. Journal of Aerospace Power, 2023, 38(12):2895-2904 doi: 10.13224/j.cnki.jasp.20220054
Citation: QIAO Xingwei, SUN Jiguo, LIU Qian. Prediction of natural acoustic frequency of gas core in centrifugal injector[J]. Journal of Aerospace Power, 2023, 38(12):2895-2904 doi: 10.13224/j.cnki.jasp.20220054

离心喷嘴气涡固有声学频率预测

doi: 10.13224/j.cnki.jasp.20220054
详细信息
    作者简介:

    乔兴伟(1996-),男,硕士生,研究领域为液体火箭发动机设计

    通讯作者:

    刘倩(1987-),女,高级工程师,博士,研究领域为液体火箭发动机设计。E-mail:liuqian_mingbai@163.com

  • 中图分类号: V434.13

Prediction of natural acoustic frequency of gas core in centrifugal injector

  • 摘要:

    为得到准确的离心喷嘴气涡固有声学频率,通过renormalization group(RNG)$k{\text{-}}\varepsilon$湍流模型和volume of fluid(VOF)气液两相流模型进行数值仿真研究。仿真结果表明将离心喷嘴与喷嘴出口锥形液膜视为一个声学系统可准确预测固有声学频率,修正后离心喷嘴固有声学频率计算公式可准确计算气涡中不同气体介质的1、2阶声学频率,误差在3%以内。室压扰动频率等于离心喷嘴固有声学频率时两者发生耦合共振,气涡压力脉动振幅增加量约为室压扰动幅值的16倍,气涡声学压力脉动可能传入上游供应系统,引起喷注不稳定。

     

  • 图 1  喷嘴结构图

    Figure 1.  Schematic diagram of injector

    图 2  物理模型与监测点位置示意图

    Figure 2.  Physical model and probe position diagram

    图 3  不同密度网格压力振荡频谱图

    Figure 3.  Spectrum diagram of pressure oscillation with different density grids

    图 4  离心喷嘴充填过程氧体积分数云图

    Figure 4.  Oxygen volume fraction nephogram of centrifugal injector filling process

    图 5  液氧体积分数、温度、压力云图

    Figure 5.  Liquid oxygen volume fraction, temperature and pressure nephogram

    图 6  离心喷嘴压力振荡时间序列及幅频特性

    Figure 6.  Time series of pressure oscillation and amplitude-frequency characteristics of oscillation of centrifugal injector

    图 7  离心喷嘴工作原理示意图

    Figure 7.  Schematic diagram of working principle of open centrifugal injector

    图 8  离心喷嘴固有声学频率模态

    Figure 8.  Natural acoustic frequency mode of centrifugal injector

    图 9  液膜表面波振幅示意图

    Figure 9.  Schematic of the amplitude of the disturbance on the liquid sheet

    图 10  同轴离心喷嘴压力振荡时间序列及振荡幅频特性图

    Figure 10.  Time series of pressure oscillation and amplitude-frequency characteristics of oscillation of swirl coaxial injector

    图 11  氧体积分数和流场温度云图

    Figure 11.  Oxygen volume fraction and temperature nephogram

    图 12  不同频率反压扰动下缩进室内部压力振荡时间序列和振荡频谱图

    Figure 12.  Time series of pressure oscillation and amplitude-frequency characteristics of oscillation in different frequency disturbance of back pressures

    图 13  水体积分数和流场温度云图

    Figure 13.  Water volume fraction and temperature nephogram

    图 14  监测点1处压力振荡时间序列及振荡幅频特性图

    Figure 14.  Time series of pressure oscillation and amplitude-frequency characteristics of oscillation at probe 1

    表  1  喷嘴结构参数表

    Table  1.   Injector structure size

    参数数值
    Lc/Dc13.15
    Do/Dc1.74
    Dit/Dc0.32
    Dot/Dc0.32
    Rsw/Dc0.34
    Lh/Dc0.43
    Lr/Dc0.43
    Wa/Dc0.23
    下载: 导出CSV

    表  2  不同计算方法气涡固有声学频率结果及误差

    Table  2.   Acoustic frequency calculation and error with different methods

    方法L/mmc/(m/s)ft/Hz误差/%
    1/4波长管60965.934024.715.1
    黄玉辉等人[5]60958.293992.914.2
    王小龙等人[11]62965.933894.911.4
    方法171965.933401.22.7
    方法270965.933449.81.3
    下载: 导出CSV
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出版历程
  • 收稿日期:  2022-02-07
  • 网络出版日期:  2023-08-28

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