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电弧射流激励器工作特性仿真研究

袁野 张岩 赵青 黄小平 郭成

袁野, 张岩, 赵青, 等. 电弧射流激励器工作特性仿真研究[J]. 强激光与粒子束, 2022, 34: 065003. doi: 10.11884/HPLPB202234.210527
引用本文: 袁野, 张岩, 赵青, 等. 电弧射流激励器工作特性仿真研究[J]. 强激光与粒子束, 2022, 34: 065003. doi: 10.11884/HPLPB202234.210527
Yuan Ye, Zhang Yan, Zhao Qing, et al. Numerical study on the characteristics of an arc jet plasma actuator[J]. High Power Laser and Particle Beams, 2022, 34: 065003. doi: 10.11884/HPLPB202234.210527
Citation: Yuan Ye, Zhang Yan, Zhao Qing, et al. Numerical study on the characteristics of an arc jet plasma actuator[J]. High Power Laser and Particle Beams, 2022, 34: 065003. doi: 10.11884/HPLPB202234.210527

电弧射流激励器工作特性仿真研究

doi: 10.11884/HPLPB202234.210527
基金项目: 上海市科学技术委员会资助项目(17DZ2280800)
详细信息
    作者简介:

    袁 野,494050711@qq.com

    通讯作者:

    赵 青,zhaoq@uestc.edu.cn

  • 中图分类号: V224+.4

Numerical study on the characteristics of an arc jet plasma actuator

  • 摘要: 为了在高超声速飞行器减阻中达到更好的减阻效果,设计了一种电弧射流等离子体激励器。采用有限元法求解非线性多物理方程,对此电弧射流等离子体激励器的工作特性进行了数值模拟,得到了激励器内部的电势、压力、温度和速度分布,综合分析了进气口气体速度、放电电流、激励器管道半径对电势、压力、温度和速度分布的影响。获得了全面的影响规律,通过仿真结果还得到:电弧射流等离子体激励器可产生最高温度为8638 K、最高速度为655 m/s的等离子体射流。当电流20 A,进气速度0.5 m/s,管道半径2.5 mm时,所需功率最小;当电流20 A,入口气体流速5 m/s,管道半径2.5 mm时,出口处平均温度最高;当电流20 A,进口气体速度10 m/s,管道半径2.5 mm时,出口处平均速度最大。并对仿真得到的放电电压进行了实验验证,在等离子体参数相似的情况下,实验结果与仿真结果吻合较好。
  • 图  1  电弧射流等离子体激励器结构图

    Figure  1.  Structure diagram of arc jet plasma actuator

    图  2  电流20 A、气体入口速度10 m/s、管道半径2.5 mm时的等离子体特性分布图

    Figure  2.  Plasma characteristic distribution at current 20 A, gas inlet velocity 10 m / s and pipe radius 2.5 mm

    图  3  电流、气体入口速度和管道半径对径向和轴向电位分布的影响

    Figure  3.  Influences of current, gas inlet velocity and pipe radius on radial and axial potential distribution

    图  4  电流、进气速度和管道半径对径向和轴向压力分布的影响

    Figure  4.  Influences of current, inlet velocity and pipe radius on radial and axial pressure distribution

    图  5  电流、进气速度和管道半径对径向和轴向温度分布的影响

    Figure  5.  Influences of current, inlet velocity and pipe radius on radial and axial temperature distribution

    图  6  电流、进气速度和管道半径对径向和轴向速度分布的影响

    Figure  6.  Influences of current, inlet velocity and pipe radius on radial and axial velocity distribution

    图  7  电弧射流等离子体激励器实验拍摄图

    Figure  7.  Experimental photos of arc jet plasma actuator

    图  8  电流20 A、气体入口速度0.5 m/s、管道半径2.5 mm 时的电势分布图

    Figure  8.  Potential distribution at current 20 A, gas inlet velocity 0.5 m / s and pipe radius 2.5 mm

    表  1  电弧射流等离子体激励器的关键性能参数

    Table  1.   Key performance parameters of arc jet plasma actuator

    current/
    A
    inlet gas
    velocity/(m/s)
    pipe radius/
    mm
    internal minimum
    voltage/V
    average temperature
    at the exit/K
    average speed
    at exit/(m/s)
    20 0.5 2.5 −83.7 3035.9 26.8
    20 5.0 2.5 −145.2 3994.3 308.5
    20 10.0 2.5 −176.8 3185.9 424.6
    10 10.0 2.5 −171.7 1963.3 275.4
    15 10.0 2.5 −177.2 2565.7 340.1
    20 10.0 3.0 −168.0 3035.7 281.9
    20 10.0 3.5 −157.8 2982.5 199.9
    下载: 导出CSV

    表  2  实测电流电压特性表

    Table  2.   Measured current and voltage characteristics

    inlet flow/
    (L·min−1)
    preset current
    before discharge/A
    stable discharge
    current/A
    preset voltage
    before discharge/V
    stable discharge
    voltage/V
    572049384
    7721493130
    5820.249386
    58.521.449388
    5921.549386.7
    592049488
    51021.549484
    5112249480
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-11-26
  • 修回日期:  2022-02-26
  • 录用日期:  2022-03-15
  • 网络出版日期:  2022-03-21
  • 刊出日期:  2022-06-15

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