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DBD等离子体激励控制外掠后台阶流场的机理研究

俞建阳 吴延龙 谢维潇 孙丰实

俞建阳, 吴延龙, 谢维潇, 等. DBD等离子体激励控制外掠后台阶流场的机理研究[J]. 航空动力学报, 2025, 40(8):20230160 doi: 10.13224/j.cnki.jasp.20230160
引用本文: 俞建阳, 吴延龙, 谢维潇, 等. DBD等离子体激励控制外掠后台阶流场的机理研究[J]. 航空动力学报, 2025, 40(8):20230160 doi: 10.13224/j.cnki.jasp.20230160
YU Jianyang, WU Yanlong, XIE Weixiao, et al. Study on the mechanism of backward-facing step flow controlled by DBD plasma excitation[J]. Journal of Aerospace Power, 2025, 40(8):20230160 doi: 10.13224/j.cnki.jasp.20230160
Citation: YU Jianyang, WU Yanlong, XIE Weixiao, et al. Study on the mechanism of backward-facing step flow controlled by DBD plasma excitation[J]. Journal of Aerospace Power, 2025, 40(8):20230160 doi: 10.13224/j.cnki.jasp.20230160

DBD等离子体激励控制外掠后台阶流场的机理研究

doi: 10.13224/j.cnki.jasp.20230160
基金项目: 国家自然科学基金青年基金(52006045); 黑龙江省科技攻关项目(2022ZXJ09C01)
详细信息
    作者简介:

    俞建阳(1987-),男,副教授、博士生导师,博士,主要从事航空宇航动力系统气动热力学研究

  • 中图分类号: V231.3

Study on the mechanism of backward-facing step flow controlled by DBD plasma excitation

  • 摘要:

    为探究介质阻挡放电(dielectric barrier discharge, DBD)等离子体控制外掠后台阶流场结构机理,通过数值模拟获得了DBD激励诱导流场结构与大尺度自由驻涡耦合流动过程,利用本征正交分解(proper orthogonal decomposition, POD)分析方法提取了耦合流场的主要含能模态分布特征,基于湍动能分布等流场特征信息探讨了流动结构特性及其相互作用,分析对比了不同激励参数下的流场结构发展演变过程。结果表明:非定常等离子体激励增强了剪切层的动量传输能力,使得回流区中的小尺度涡结构被抑制,分离区长度减小。通过POD模态分析,发现中频激励与低、高频激励实现流动控制的机理存在显著差异。低、高频激励下剪切层位置的往复摆动是等离子体激励作用下诱导流场的主要运动形式,而中频激励的作用则体现在对小尺度湍流脉动作用上。

     

  • 图 1  DBD等离子体激励器示意图

    Figure 1.  Schematic of the DBD plasma actuator

    图 2  等离子体激励模型验证方案示意图

    Figure 2.  Schematic diagram of the DBD excitation model validation

    图 3  CFD计算结果与实验结果对比

    Figure 3.  Comparison of the results between the CFD and the experiment

    图 4  非定常扰动周期

    Figure 4.  Period of unsteady perturbation

    图 5  外掠后台阶流场几何尺度与激励参数示意图

    Figure 5.  Geometric scale and unsteady excitation parameters of outer-swept step flow field

    图 6  计算域网格示意图

    Figure 6.  Schematic diagram of computational grid

    图 7  后台阶流场流动状态与再附点位置对比

    Figure 7.  Comparison of flow state and position of reattachment point in flow field of rear step

    图 8  台阶后不同位置的截面流向速度分布

    Figure 8.  Flow velocity distribution of cross section at different positions behind the step

    图 9  一个流动周期内基准流场和激励流场的流场结构演变

    Figure 9.  Evolution of flow structure in a period of baseline flow field and excitation flow field

    图 10  分离涡A核心区位置随流动周期的变化

    Figure 10.  Position of the core region of the separating vortex A varies with the flow period

    图 11  分离涡A、B核心区涡量在流动周期内的变化

    Figure 11.  Variation of the vorticity position in the core regions of the separated vortices A and B with the flow period

    图 12  不同激励频率下流场各阶POD模态含能和累计含能对比

    Figure 12.  Comparison of the energy content and cumulative energy content of each POD mode in the flow field with different excitation frequencies

    图 13  无激励流场中各阶模态脉动速度矢量分布

    Figure 13.  Pulsating velocity vector distribution of each mode in non-excitation flow field

    图 14  不同激励频率下低阶模态脉动速度对比

    Figure 14.  Comparison of pulsation velocities of low modes under different excitation conditions

    图 15  不同激励频率下高阶模态脉动速度对比

    Figure 15.  Comparison of pulsation velocities of high modes under different excitation conditions

    图 16  非定常等离子体激励控制后台阶流动示意图

    Figure 16.  Schematic of the step flow after unsteady plasma excitation control

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  • 收稿日期:  2023-03-15
  • 网络出版日期:  2025-05-22

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