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飞机排液射流雾化全历程仿真计算与机理分析

吕萌 杨扬 吕乐 徐绯

吕萌, 杨扬, 吕乐, 等. 飞机排液射流雾化全历程仿真计算与机理分析[J]. 航空动力学报, 2026, 41(4):20240203 doi: 10.13224/j.cnki.jasp.20240203
引用本文: 吕萌, 杨扬, 吕乐, 等. 飞机排液射流雾化全历程仿真计算与机理分析[J]. 航空动力学报, 2026, 41(4):20240203 doi: 10.13224/j.cnki.jasp.20240203
LYU Meng, YANG Yang, LYU Le, et al. Numerical simulation and mechanism analysis of jet atomization in the whole process of aircraft drainage[J]. Journal of Aerospace Power, 2026, 41(4):20240203 doi: 10.13224/j.cnki.jasp.20240203
Citation: LYU Meng, YANG Yang, LYU Le, et al. Numerical simulation and mechanism analysis of jet atomization in the whole process of aircraft drainage[J]. Journal of Aerospace Power, 2026, 41(4):20240203 doi: 10.13224/j.cnki.jasp.20240203

飞机排液射流雾化全历程仿真计算与机理分析

doi: 10.13224/j.cnki.jasp.20240203
基金项目: 国家自然科学基金面上项目(12272309)
详细信息
    作者简介:

    吕萌(1999-),男,助理工程师,硕士生,主要从事流固耦合仿真研究工作。E-mail:lvmeng0929@163.com

    通讯作者:

    杨扬(1986-),男,副教授、博士生导师,博士,主要从事计算力学研究工作。E-mail:npuyang@nwpu.edu.cn

  • 中图分类号: V211.3

Numerical simulation and mechanism analysis of jet atomization in the whole process of aircraft drainage

  • 摘要:

    为实现飞机外部排液运动轨迹的有效预测,基于VOF to DPM方法建立了射流破碎计算模型,获取了飞机排液射流的初始形态;基于液滴破碎和质点弹道学理论开发计算程序,对雾化液滴沉降路径开展仿真预测;分析了在空气来流耦合作用下,排液初期射流破碎和后期液滴雾化的形成机理。研究结果表明:本文建立的全历程液滴运动计算模型可同时考虑外排液体的一次破碎和二次雾化,射流形态和雾化液滴沉降路径计算误差均小于5%,实现了滑行、爬升、高速巡航全工况下飞机排液运动路径和空间粒径分布特性的有效预测,为飞机适航符合性验证提供技术支持。

     

  • 图 1  飞机排液示意图

    Figure 1.  Diagram of aircraft drainage

    图 2  液滴雾化程序计算流程

    Figure 2.  Calculation process of droplet atomization program

    图 3  计算域示意图(单位:mm)

    Figure 3.  Schematic diagram of computational domain (unit:mm)

    图 4  仿真结果及与文献[12]射流轨迹对比图

    Figure 4.  Simulation results of jet trajectory with the literature [12]

    图 5  不同自适应网格层数x/d=1.3位置速度幅值曲线

    Figure 5.  Velocity amplitude curve at position x/d=1.3 for different adaptive mesh layers

    图 6  本文计算结果和文献[22]射流轨迹对比图

    Figure 6.  Comparison between the calculation results in this article and the jet trajectory in literature [22]

    图 7  工况1射流形态发展过程

    Figure 7.  Development process of jet form in Case 1

    图 8  3.2 ms时射流初期形态

    Figure 8.  Initial form of jet at 3.2 ms

    图 9  3.2 ms时射流各高度压力场以及截面流线图

    Figure 9.  Pressure field and cross-section streamline diagram at different heights of the jet at 3.2 ms

    图 10  8.5 ms时速度场和流线图

    Figure 10.  Velocity field and streamline diagram at 8.5 ms

    图 11  射流端部液体逐渐脱离射流主体

    Figure 11.  Liquid at the end of the jet separates from the main body

    图 12  工况2和工况3液柱主体破碎对比

    Figure 12.  Comparison of main-body breakup of the liquid column for Case 2 and Case 3

    图 13  工况2和工况3排液出口处质量流率随时间变化曲线

    Figure 13.  Temporal variation of mass flow rate at the discharge outlet for Case 2 and Case 3

    图 14  工况2液滴运动2 s后路径

    Figure 14.  Path of droplet movement for two seconds in Case 2

    图 15  工况2 Z = −15 m处液滴分布高斯处理示意图

    Figure 15.  Schematic diagram of droplet distribution processed by Gaussian filtering at Z = −15 m in Case2

    图 16  工况2不同位置处粒子分布

    Figure 16.  Droplet distribution at different positions of Case 2

    表  1  模型的求解器设置

    Table  1.   Solver settings for the model

    设置参数 设置方式
    时间 瞬态求解;一阶隐式
    VOF模型 显式求解
    二次破碎 WAVE
    湍流模型 SST k-ω
    压力速度耦合 coupled
    动量离散化方法 二阶迎风格式
    压力离散化方法 PRESTO!
    体积分数离散化方法 Geo-Reconstruct
    壁面边界 无滑移壁面;
    DPM粒子逃逸
    表面张力模型 连续表面张力模型(CSF)
    下载: 导出CSV
  • [1] 何思元, 于水. 民用飞机高置泄漏源排液设计与验证方法研究[J]. 民用飞机设计与研究, 2022(3): 94-98. HE Siyuan, YU Shui. Research on design and verification method of high-set leak source drainage of civil aircraft[J]. Civil Aircraft Design & Research, 2022(3): 94-98. (in Chinese doi: 10.19416/j.cnki.1674-9804.2022.03.015

    HE Siyuan, YU Shui. Research on design and verification method of high-set leak source drainage of civil aircraft[J]. Civil Aircraft Design & Research, 2022(3): 94-98. (in Chinese) doi: 10.19416/j.cnki.1674-9804.2022.03.015
    [2] 王东辉, 黄勇, 汪磊, 等. 离心喷嘴初始雾化性能PDPA及DOH对比试验[J]. 航空动力学报, 2022, 37(11): 2513-2523. WANG Donghui, HUANG Yong, WANG Lei, et al. Comparative experiment on initial atomization performance of centrifugal nozzle with PDPA and DOH[J]. Journal of Aerospace Power, 2022, 37(11): 2513-2523. (in Chinese doi: 10.13224/j.cnki.jasp.20220247

    WANG Donghui, HUANG Yong, WANG Lei, et al. Comparative experiment on initial atomization performance of centrifugal nozzle with PDPA and DOH[J]. Journal of Aerospace Power, 2022, 37(11): 2513-2523. (in Chinese) doi: 10.13224/j.cnki.jasp.20220247
    [3] 徐胜利, 岳朋涛, 韩肇元, 等. 雾化燃料在超声速气流中横向喷射混合的数值模拟[J]. 空气动力学学报, 2000, 18(1): 39-45. XU Shengli, YUE Pengtao, HAN Zhaoyuan, et al. Numerical simulation of atomized fuels transversely injected into a supersonic flow[J]. Acta Aerodynamica Sinica, 2000, 18(1): 39-45. (in Chinese doi: 10.3969/j.issn.0258-1825.2000.01.006

    XU Shengli, YUE Pengtao, HAN Zhaoyuan, et al. Numerical simulation of atomized fuels transversely injected into a supersonic flow[J]. Acta Aerodynamica Sinica, 2000, 18(1): 39-45. (in Chinese) doi: 10.3969/j.issn.0258-1825.2000.01.006
    [4] NAMBU T, MIZOBUCHI Y. Detailed numerical simulation of primary atomization by crossflow under gas turbine engine combustor conditions[J]. Proceedings of the Combustion Institute, 2021, 38(2): 3213-3221. doi: 10.1016/j.proci.2020.06.067
    [5] MASHAYEK A, BEHZAD M, ASHGRIZ N. Multiple injector model for primary breakup of a liquid jet in crossflow[J]. AIAA Journal, 2011, 49(11): 2407-2420. doi: 10.2514/1.J050623
    [6] 林宇震, 李林, 张弛, 等. 液体射流喷入横向气流混合特性研究进展[J]. 航空学报, 2014, 35(1): 46-57. LIN Yuzhen, LI Lin, ZHANG Chi, et al. Progress on the mixing of liquid jet injected into a crossflow[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1): 46-57. (in Chinese doi: 10.7527/S1000-6893.2013.0346

    LIN Yuzhen, LI Lin, ZHANG Chi, et al. Progress on the mixing of liquid jet injected into a crossflow[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1): 46-57. (in Chinese) doi: 10.7527/S1000-6893.2013.0346
    [7] SALLAM K, NG C, SANKARAKRISHNAN R, et al. Breakup of turbulent and non-turbulent liquid jets in gaseous crossflows: AIAA 2006-1517 [R]. Reno, US: 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
    [8] JADIDI M, SREEKUMAR V, DOLATABADI A. Breakup of elliptical liquid jets in gaseous crossflows at low Weber numbers[J]. Journal of Visualization, 2019, 22(2): 259-271. doi: 10.1007/s12650-018-0537-8
    [9] BROUMAND M, BIROUK M. Liquid jet in a subsonic gaseous crossflow: Recent progress and remaining challenges[J]. Progress in Energy and Combustion Science, 2016, 57: 1-29. doi: 10.1016/j.pecs.2016.08.003
    [10] 何园源, 于小兵, 王智华, 等. 横向射流中煤油雾化特性的数值研究[J]. 推进技术, 2023, 44(3): 210756. HE Yuanyuan, YU Xiaobing, WANG Zhihua, et al. Numerical study on spray characteristics of kerosene jet in a crossflow[J]. Journal of Propulsion Technology, 2023, 44(3): 210756. (in Chinese doi: 10.13675/j.cnki.tjjs.210756

    HE Yuanyuan, YU Xiaobing, WANG Zhihua, et al. Numerical study on spray characteristics of kerosene jet in a crossflow[J]. Journal of Propulsion Technology, 2023, 44(3): 210756. (in Chinese) doi: 10.13675/j.cnki.tjjs.210756
    [11] WANG Yansheng, LIN Yuzhen, LI Lin, et al. Research on penetration of aviation kerosene injected into crossflows based on PLIF technique[J]. Journal of Propulsion Technology, 2015, 36(9): 1395-1402.
    [12] CHU Guidong, QIAN Lijuan, ZHONG Xiaokai, et al. A numerical investigation on droplet bag breakup behavior of polymer solution[J]. Polymers, 2020, 12(10): 2172. doi: 10.3390/polym12102172
    [13] GAO Xinxin, CHEN Jianye, QIU Yinan, et al. Effect of phase change on jet atomization: a direct numerical simulation study[J]. Journal of Fluid Mechanics, 2022, 935: A16. doi: 10.1017/jfm.2021.1158
    [14] 邓甜, 李佳周, 陈伟. 剪切气流中无黏液体横向射流破碎机理[J]. 航空学报, 2021, 42(7): 124464. DENG Tian, LI Jiazhou, CHEN Wei. Breakup mechanism of inviscid liquid transverse jet in shear airflow[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(7): 124464. (in Chinese

    DENG Tian, LI Jiazhou, CHEN Wei. Breakup mechanism of inviscid liquid transverse jet in shear airflow[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(7): 124464. (in Chinese)
    [15] REITZ R. Modeling atomization processes in high-pressure vaporizing sprays[J]. Atomisation and Spray technology, 1987, 3(4): 309-337.
    [16] MADABHUSHI R K. A model for numerical simulation of breakup of a liquid jet in crossflow[J]. Atomization and Sprays, 2003, 13(4): 413-424. doi: 10.1615/AtomizSpr.v13.i4.50
    [17] PILCH M, ERDMAN C. Discrete Element Method (DEM) simulation and processing of Mo/AL2O3 Granules in fluidizing bed[J]. Proc Nat Sci Counc RAOC (A), 2000, 24(5): 394-404.
    [18] SCHMEHL R, KLOSE G, MAIER G, et al. Efficient numerical calculation of evaporating sprays in combustion chamber flows[C]// RTO AVT Symposium on Gas Turbine Engine Combustion, Emissions and Alternative Fuels. Lisbon, Portugal: RTO MP-14, 1998: 51.1-51.14.
    [19] HSIANG L P, FAETH G M. Near-limit drop deformation and secondary breakup[J]. International Journal of Multiphase Flow, 1992, 18(5): 635-652. doi: 10.1016/0301-9322(92)90036-G
    [20] LAMBERT M, ESCH T, BRAUN M, et al. Enhancement of the Madabhushi Liquid Jet in Cross-flow Breakup Model by a Ligament Breakup Mechanism [R]. Paris: 29th ILASS-Europe Conference on Liquid Atomization and Spray Systems, 2019.
    [21] ITO T, KATO H, GODA Y, et al. Water-dropping aerodynamics for fire-fighting amphibian[C]//Proceedings of the 27th International Congress of the International Council of the Aeronautical Sciences. Nice, France: ICAS, 2010: 628-637.
    [22] 闫超星, 张翼, 刘成洋, 等. 喷淋液滴在空气环境下的运动特性[J]. 原子能科学技术, 2020, 54(1): 66-71. YAN Chaoxing, ZHANG Yi, LIU Chengyang, et al. Motion characteristic of spray droplet in air environment[J]. Atomic Energy Science and Technology, 2020, 54(1): 66-71. (in Chinese doi: 10.7538/yzk.2019.youxian.0060

    YAN Chaoxing, ZHANG Yi, LIU Chengyang, et al. Motion characteristic of spray droplet in air environment[J]. Atomic Energy Science and Technology, 2020, 54(1): 66-71. (in Chinese) doi: 10.7538/yzk.2019.youxian.0060
    [23] WU Peikuan, KIRKENDALL K A, FULLER R P, et al. Breakup processes of liquid jets in subsonic crossflows[J]. Journal of Propulsion and Power, 1997, 13(1): 64-73. doi: 10.2514/2.5151
    [24] SALLAM K A, NG C L, SANKARAKRISHNAN R, et al. Breakup of turbulent and non-turbulent liquid jets in gaseous crossflows[R]. Reno, USA: 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
    [25] TAMBE S, JENG S M, MONGIA H, et al. Liquid jets in subsonic crossflow: AIAA 2005-731 [R]. Reston, US: 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005.
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  • 收稿日期:  2024-02-03
  • 网络出版日期:  2026-01-09

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