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头部锥角对弹体高速入水流场变化特性的影响

李腾,  高贵山,  姚伟光,  仇洋,  胡顺治,  桂毓林,  何雨,  郑晓波

李腾, 高贵山, 姚伟光, 仇洋, 胡顺治, 桂毓林, 何雨, 郑晓波. 头部锥角对弹体高速入水流场变化特性的影响[J]. 爆炸与冲击, 2026, 46(11): 113401. doi: 10.11883/bzycj-2025-0312
引用本文: 李腾, 高贵山, 姚伟光, 仇洋, 胡顺治, 桂毓林, 何雨, 郑晓波. 头部锥角对弹体高速入水流场变化特性的影响[J]. 爆炸与冲击, 2026, 46(11): 113401. doi: 10.11883/bzycj-2025-0312
LI Teng, GAO Guishan, YAO Weiguang, QIU Yang, HU Shunzhi, GUI Yulin, HE Yu, ZHENG Xiaobo. Effect of head cone angle on flow field variation during high-speed projectile water entry[J]. Explosion And Shock Waves, 2026, 46(11): 113401. doi: 10.11883/bzycj-2025-0312
Citation: LI Teng, GAO Guishan, YAO Weiguang, QIU Yang, HU Shunzhi, GUI Yulin, HE Yu, ZHENG Xiaobo. Effect of head cone angle on flow field variation during high-speed projectile water entry[J]. Explosion And Shock Waves, 2026, 46(11): 113401. doi: 10.11883/bzycj-2025-0312

头部锥角对弹体高速入水流场变化特性的影响

doi: 10.11883/bzycj-2025-0312
基金项目: 中物院院长基金(YZJJZL2024019)
详细信息
    作者简介:

    李 腾(1999- ),男,硕士,工程师,liteng201606@163.com

    通讯作者:

    郑晓波(1986- ),男,博士,高级工程师,zxb3710@163.com

  • 中图分类号: O352

Effect of head cone angle on flow field variation during high-speed projectile water entry

  • 摘要: 弹体高速入水过程中会发生空化现象形成空泡,引起流场变化,进一步影响弹体运动稳定性。针对不同头部锥角双锥段弹体穿越自由液面后的流场变化影响特性展开研究,基于电磁发射装置进行弹体高速入水试验,采用重叠网格技术和流体域体积(volume of fluid,VOF)多相流模型建立弹体高速入水数值模型并展开计算,通过试验验证了数值模型的有效性,获取了不同头型弹体垂直入水后的流场变化特性。研究发现:双锥段弹体垂直入水后,空泡对称发展,空泡面闭合后,总长度增大,最大宽度逐渐减小;随着弹体空化器头部锥角的增大,弹体入水初期空泡闭合、表面沾湿的位置向尾部靠近,空泡轮廓越宽,入水瞬间和水中运动时的阻力也越大,速度衰减越快,空泡发生面闭合的时间越迟,水中运动同一时刻,弹体尾空泡的长度越长,水域内涡结构的长度越短。
  • 图  1  弹体模型

    Figure  1.  Projectile model

    图  2  计算模型及网格划分

    Figure  2.  Computational model and mesh generation

    图  3  不同网格量下速度变化对比

    Figure  3.  Comparison of velocity variations under different mesh quantities

    图  4  不同区域宽度下速度变化对比

    Figure  4.  Comparison of velocity variations under different area widths

    图  5  不同区域宽度下入水5 m处水蒸气流场对比

    Figure  5.  Comparison of water vapor flow fields at a depth of 5 m under different area widths

    图  6  试验布局

    Figure  6.  Test layout

    图  7  水深1.25 m时试验和数值模拟空泡对比

    Figure  7.  Comparison of cavitations between test and simulation at a water depth of 1.25 m

    图  8  弹体入水运动过程

    Figure  8.  Motion process of the projectile’s water entry

    图  9  弹体高速入水试验中的位移和速度随时程曲线

    Figure  9.  Displacement and velocity histories of the projectile during water entry

    图  10  空泡尺度变化特性

    Figure  10.  Characteristic of cavitation size variation

    图  11  不同时刻空泡轮廓

    Figure  11.  The contours of the cavitation at different times

    图  12  弹体入水运动流场变化

    Figure  12.  Flow field changes during the water entry motion of the projectile

    图  13  弹体入水位移变化

    Figure  13.  Displacement variation of the projectile during water entry

    图  14  弹体入水速度变化

    Figure  14.  Velocity variation of the projectile during water entry

    图  15  水面处空泡宽度对比

    Figure  15.  Comparison of cavitation width at the water surface

    图  16  不同时刻空泡轮廓对比

    Figure  16.  Comparison of cavitation contours at different times

    图  17  不同头型弹体入水初期空泡演化过程

    Figure  17.  The initial cavitation change process of projectiles with different head types during water entry

    图  18  弹体入水初期空泡最大宽度变化曲线

    Figure  18.  Variation of maximum cavitation width at the initial stage of the projectile entering the water

    图  19  不同头型弹体入水6 ms后压力场

    Figure  19.  Pressure field of the projectile with different head types after entering water for 6 ms

    图  20  不同头型弹体入水24 ms后水蒸气体积分数场

    Figure  20.  Vapor volume fraction field of projectiles with different head types after entering water for 24 ms

    图  21  不同头型弹体入水24 ms后压力场

    Figure  21.  Pressure field of projectiles with different head types after entering water for 24 ms

    图  22  不同头型弹体入水48 ms后流场相云图

    Figure  22.  Flow field phase nephograms of projectiles with different head types after entering water for 48 ms

    图  23  不同头型弹体入水48 ms后涡结构场

    Figure  23.  Vortex structure fields of projectiles with different head types after entering water for 48 ms

    图  24  入水速度随位移的变化

    Figure  24.  Variation of velocity with displacement during water entry process

    图  25  弹体绕x轴和z轴偏转角度随入水位移的变化

    Figure  25.  Variation of the deflection angle of the projectile around the x-axis and the z-axis with displacement

    图  26  头部顶点压力随位移的变化

    Figure  26.  Variation of pressure at the head vertex with displacement

    表  1  不同时刻各弹体入水初期空泡最大宽度

    Table  1.   The maximum width of the cavitation at the initial stage of each projectile entering the water at different times

    弹体模型 空泡最大宽度/mm
    1 ms 2 ms 3 ms 4 ms 5 ms 6 ms
    60°锥头 64.10 75.71 106.06 110.89 116.66 123.25
    90°锥头 74.37 89.45 103.19 114.11 120.42 124.90
    120°锥头 82.98 103.82 114.55 126.38 134.49 136.10
    150°锥头 86.88 106.97 120.82 133.87 138.11 147.02
    平头 90.16 110.06 125.19 137.44 144.93 153.83
    下载: 导出CSV

    表  2  弹体入水后速度、压力变化

    Table  2.   Variation of velocity and pressure of projectiles after entering the water

    弹体模型 入水5 m后速度/(m·s−1) 速度衰减/(m·s−1) 入水瞬间头部顶点峰值压力/MPa 入水5 m后头部顶点压力/MPa
    60°锥头 99.3 10.7 5.1 3.47
    90°锥头 103.5 6.5 7.7 4.58
    120°锥头 101.9 8.1 12.6 5.08
    150°锥头 100.6 9.4 17.9 5.17
    平头 99.5 10.5 22.7 5.09
    下载: 导出CSV
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出版历程
  • 收稿日期:  2025-09-28
  • 修回日期:  2025-11-13
  • 网络出版日期:  2025-11-13
  • 刊出日期:  2026-11-05

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