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非均匀横流下射流破碎特征和动力学分析

张通宇 何浩吉 郭志辉

张通宇, 何浩吉, 郭志辉. 非均匀横流下射流破碎特征和动力学分析[J]. 航空动力学报, 2026, 41(7):20240780 doi: 10.13224/j.cnki.jasp.20240780
引用本文: 张通宇, 何浩吉, 郭志辉. 非均匀横流下射流破碎特征和动力学分析[J]. 航空动力学报, 2026, 41(7):20240780 doi: 10.13224/j.cnki.jasp.20240780
Zhang Tongyu, He Haoji, Guo Zhihui. Characteristics and dynamics analysis of jet breakup under non-uniform crossflow[J]. Journal of Aerospace Power, 2026, 41(7):20240780 doi: 10.13224/j.cnki.jasp.20240780
Citation: Zhang Tongyu, He Haoji, Guo Zhihui. Characteristics and dynamics analysis of jet breakup under non-uniform crossflow[J]. Journal of Aerospace Power, 2026, 41(7):20240780 doi: 10.13224/j.cnki.jasp.20240780

非均匀横流下射流破碎特征和动力学分析

doi: 10.13224/j.cnki.jasp.20240780
详细信息
    作者简介:

    张通宇(2001-),男,硕士,主要从事横向射流、燃烧室数值模拟。E-mail:46798607@qq.com

    通讯作者:

    郭志辉(1969-),男,副教授、硕士生导师,硕士,主要从事航空发动机燃烧不稳定性及燃油雾化研究。E-mail:guozhihui@buaa.edu.cn

  • 中图分类号: V231.2

Characteristics and dynamics analysis of jet breakup under non-uniform crossflow

  • 摘要:

    通过实验研究了具有正负速度梯度的横流对水射流破碎模式及动力学特性的影响。实验涵盖平均韦伯数(5.6、8、16、40)与平均射流动量比(20、30、40、50、60)的工况。结果表明:正梯度来流可增强射流穿透深度,而负梯度来流则降低穿透深度并加速射流破碎与偏转;负梯度条件下射流变形加剧,液柱迎风面积增大导致展向宽度显著增加;正梯度引发液柱剧烈振荡且表面波长大,负梯度则抑制振荡并减小波长;负梯度加速射流破碎模式转变,正梯度则延缓该过程。通过本征正交分解(POD)与快速傅里叶变换(FFT)分析发现:不同平均韦伯数下的喷雾特性差异集中于共振峰位置与幅值,非共振区特性一致;负梯度来流中振幅衰减更快,表明流体动力耗散加剧且表面张力作用减弱;随频率升高与模态阶数增加,负梯度条件下的振幅及能量占比显著降低,证实气动力抑制作用使振幅变化呈现先增加后衰减的规律,而正梯度则维持较大振幅波动。

     

  • 图 1  横向射流模型

    Figure 1.  Lateral jet model

    图 2  实验系统图

    Figure 2.  Diagram of experimental system

    图 3  坐标设置图

    Figure 3.  Coordinate setting diagram

    图 4  喷嘴处来流速度分布图

    Figure 4.  Inlet velocity profile at the nozzle

    图 5  多槽板速度分布云图

    Figure 5.  Velocity distribution contour map of the multi-slot plate

    图 6  不同韦伯数喷雾瞬时图像

    Figure 6.  Spray instantaneous image with different Weber number

    图 7  破碎点图像

    Figure 7.  Broken up point image

    图 8  流向时均图

    Figure 8.  Time-averaged flow direction map

    图 9  射流边界

    Figure 9.  Jet boundary

    图 10  展向时均图

    Figure 10.  Spanwise time-averaged plot

    图 11  平均模态能量分布图

    Figure 11.  Average modal energy distribution diagram

    图 12  1阶模态图

    Figure 12.  First order mode diagram

    图 13  模态图

    Figure 13.  Mode diagram

    图 14  正梯度1阶FFT图像

    Figure 14.  Positive gradient first-order FFT image

    图 15  无梯度1阶FFT图像

    Figure 15.  None gradient first-order FFT image

    图 16  负梯度1阶FFT图像

    Figure 16.  Negative gradient first-order FFT image

    图 17  1~6阶FFT图像

    Figure 17.  First to sixth order FFT images

    图 18  不同梯度及平均韦伯数流向图

    Figure 18.  Flowcharts of different gradients and average Weber number

    图 19  波长取法

    Figure 19.  Wavelength determination

    图 20  局部图

    Figure 20.  Local figure

    图 21  不同梯度下波长随平均韦伯数的变化

    Figure 21.  Variation of wavelength with average Weber number at different gradients

    表  1  实验工况表

    Table  1.   Experimental working conditions

    工况 $ \overline{{u}_{\mathrm{g}}} $/(m/s) $ {v}_{\mathrm{j}} $/(m/s) $ \overline{q} $ $ \overline{{We}_{\mathrm{g}}} $
    Case 1 21.24 3.06 20 5.6
    Case 2 21.24 4.16 40 5.6
    Case 3 21.24 5.20 60 5.6
    Case 4 25.06 3.74 20 8
    Case 5 25.06 5.35 40 8
    Case 6 25.06 6.47 60 8
    Case 7 34.98 5.25 20 16
    Case 8 34.98 7.52 40 16
    Case 9 55.45 8.40 20 40
    Case 10 55.45 12.16 40 40
    下载: 导出CSV
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出版历程
  • 收稿日期:  2024-11-18
  • 网络出版日期:  2026-04-27

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