水下舷侧多层防护隔舱接触爆炸毁伤载荷特性分析

陈鹏宇 侯海量 吴林杰 朱锡

陈鹏宇, 侯海量, 吴林杰, 朱锡. 水下舷侧多层防护隔舱接触爆炸毁伤载荷特性分析[J]. 爆炸与冲击, 2017, 37(2): 283-290. doi: 10.11883/1001-1455(2017)02-0283-08
引用本文: 陈鹏宇, 侯海量, 吴林杰, 朱锡. 水下舷侧多层防护隔舱接触爆炸毁伤载荷特性分析[J]. 爆炸与冲击, 2017, 37(2): 283-290. doi: 10.11883/1001-1455(2017)02-0283-08
Chen Pengyu, Hou Hailiang, Wu Linjie, Zhu Xi. Analysis of the damage load of the underwater contact explosion on multi-layered defend cabins[J]. Explosion And Shock Waves, 2017, 37(2): 283-290. doi: 10.11883/1001-1455(2017)02-0283-08
Citation: Chen Pengyu, Hou Hailiang, Wu Linjie, Zhu Xi. Analysis of the damage load of the underwater contact explosion on multi-layered defend cabins[J]. Explosion And Shock Waves, 2017, 37(2): 283-290. doi: 10.11883/1001-1455(2017)02-0283-08

水下舷侧多层防护隔舱接触爆炸毁伤载荷特性分析

doi: 10.11883/1001-1455(2017)02-0283-08
基金项目: 

国家自然科学基金项目 51209211

国家自然科学基金项目 51479204

国家自然科学基金项目 51679246

详细信息
    作者简介:

    陈鹏宇(1990-),男,博士研究生

    通讯作者:

    侯海量,hou9611104@163.com

  • 中图分类号: O383.1

Analysis of the damage load of the underwater contact explosion on multi-layered defend cabins

  • 摘要: 为探讨水下多层防护隔舱结构设计,以典型三舱式结构为对象,利用Dytran软件分析了水下接触爆炸下舷侧多层防护隔舱中膨胀空舱内的毁伤载荷特性,得到了载荷的简化模型,并拟合出膨胀舱压力载荷脉动平稳阶段准静态气压值的计算公式。结果表明,膨胀空舱内的毁伤载荷特性在时间尺度上可分为气团膨胀扩散阶段和脉动平稳两个阶段;在空间分布上,主要分为正反射区和马赫反射区,正反射区作用载荷由初始瞬态脉冲载荷和后续逐渐衰减的准静态气压载荷叠加而成,马赫反射区作用载荷则以准静态气压为主。
  • 图  1  结构横剖面图与有限元模型(单位:mm)

    Figure  1.  Transverse section of the structure and the FEM model (unit: mm)

    图  2  欧拉域设置示意图(单位:mm)

    Figure  2.  Sketch of Euler region (units: mm)

    图  3  作用于膨胀舱壁的压力载荷(装药量300 g TNT)

    Figure  3.  Pressure on isolate bulkhead (300 g TNT)

    图  4  膨胀空舱中横剖面的压力变化历程(装药量300 g TNT)

    Figure  4.  Variation history of pressures on the mid transverse section of the void cabin (300 g TNT)

    图  5  膨胀舱壁承受压力典型测点布置图(单位:mm)

    Figure  5.  Pressure-measuring point arrangement on isolate bulkhead (unit: mm)

    图  6  膨胀舱壁典型测点压力历程图

    Figure  6.  Variation of measuring points on isolate bulkhead

    图  7  载荷简化模型

    Figure  7.  Simplified model of the load

    图  8  准静态气压公式计算与计算结果

    Figure  8.  Formula calculation and simulation results of quasi-static pressure

    表  1  结构材料参数

    Table  1.   Material parameters for the structure

    材料 σ0/MPa 泊松比 E/GPa Eh/MPa) ρ/(kg·m-3) 失效应变 D/s-1 n
    普通船用钢 235 0.3 210 250 7 800 0.28 40.4 5
    低合金船用钢 490 0.3 210 1 305 7 800 0.28 0.000 6 50.8
    下载: 导出CSV

    表  2  初始冲击波强度i1理论值与计算值

    Table  2.   Theoretical value and simulation value of the initial shock wave intensity

    TNT药量/g i1/(Pa·s)
    P2点理论值 P2点计算值 P3点理论值 P3点计算值 P4点理论值 P4点计算值
    100 1 455.96 1 625.48 1 959.00 2 082.93 1 588.32 1 762.26
    150 1 907.85 1 875.32 2 567.02 2 603.77 2 081.29 1 889.21
    200 2 311.20 2 288.91 3 109.72 3 059.32 2 521.30 2 487.93
    250 2 681.91 2 748.75 3 608.51 3 498.17 2 925.72 3 074.00
    300 3 028.52 3 153.06 4 074.89 3 556.57 3 303.84 3 503.23
    350 3 356.31 3 183.65 4 515.93 4 381.88 3 661.43 3 696.69
    400 3 668.80 3 453.72 4 936.37 4 759.65 4 002.32 4 008.74
    下载: 导出CSV

    表  3  5 ms时膨胀舱各测点的平均准静态压力

    Table  3.   Average quasi-static pressure on measuring points at 5 ms

    TNT药量/g p/MPa
    P1 P2 P3 P4 P5 P6 P7 P8 pe
    100 0.459 0.242 0.227 0.271 0.316 0.329 0.422 0.322 0.323
    150 0.478 0.265 0.305 0.402 0.502 0.575 0.461 0.598 0.448
    200 0.574 0.428 0.414 0.473 0.287 0.677 0.827 0.661 0.543
    250 0.625 0.505 0.406 0.401 0.598 0.686 0.677 0.667 0.571
    300 0.799 0.434 0.439 0.490 0.689 0.776 0.658 0.728 0.627
    350 0.768 0.493 0.603 0.705 0.885 0.851 0.706 0.840 0.731
    400 0.867 0.605 0.560 0.612 0.834 0.891 0.930 0.911 0.776
    下载: 导出CSV
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出版历程
  • 收稿日期:  2015-07-20
  • 修回日期:  2015-11-11
  • 刊出日期:  2017-03-25

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