爆轰波对碰驱动平面组合飞片的数值模拟

袁帅 胡海波 张崇玉 李平

袁帅, 胡海波, 张崇玉, 李平. 爆轰波对碰驱动平面组合飞片的数值模拟[J]. 高压物理学报, 2016, 30(1): 49-54. doi: 10.11858/gywlxb.2016.01.008
引用本文: 袁帅, 胡海波, 张崇玉, 李平. 爆轰波对碰驱动平面组合飞片的数值模拟[J]. 高压物理学报, 2016, 30(1): 49-54. doi: 10.11858/gywlxb.2016.01.008
YUAN Shuai, HU Hai-Bo, ZHANG Chong-Yu, LI Ping. A Numerical Simulation of the Assembled Flyers Driven by Two Head-on Colliding Detonation Waves[J]. Chinese Journal of High Pressure Physics, 2016, 30(1): 49-54. doi: 10.11858/gywlxb.2016.01.008
Citation: YUAN Shuai, HU Hai-Bo, ZHANG Chong-Yu, LI Ping. A Numerical Simulation of the Assembled Flyers Driven by Two Head-on Colliding Detonation Waves[J]. Chinese Journal of High Pressure Physics, 2016, 30(1): 49-54. doi: 10.11858/gywlxb.2016.01.008

爆轰波对碰驱动平面组合飞片的数值模拟

doi: 10.11858/gywlxb.2016.01.008
基金项目: 

中国工程物理研究院科学技术发展基金 2013B0201022

详细信息
    作者简介:

    袁帅(1972-), 男, 硕士, 主要从事计算流体力学研究.E-mail:yscaep_01@sina.com

  • 中图分类号: O347

A Numerical Simulation of the Assembled Flyers Driven by Two Head-on Colliding Detonation Waves

  • 摘要: 采用SG (Steinberg-Guinan)强度模型描述组合飞片(铅和铝)的动力学响应行为, 对两侧对称点起爆圆柱炸药、爆轰波对碰驱动组合飞片实验模型进行了数值模拟计算。得到了爆轰波对碰驱动组合飞片的计算图像, 并与实验结果进行了对比分析, 明确了SG强度模型对描述爆轰波对碰驱动下组合飞片的适用性, 为高应变率条件下材料强度模型的适应性研究奠定基础, 同时也为更好地理解材料在高应变率条件下的本构关系以及材料在对碰区的动力学行为提供参考。

     

  • 图  计算模型示意图

    Figure  1.  Schematic layout of simulation setup

    图  起爆后不同时刻的压力云图

    Figure  2.  Pressure nephograms at different time points after ignition

    图  不同时刻组合飞片(铅和铝)中的压力云图

    Figure  3.  Pressures undergone by the combined flyers (Pb and Al) at different time points

    图  不同时刻铅飞片自由面的外形

    Figure  4.  4 Outline of free surface of Pb flyer at different time points

    图  实验和计算结果的比较

    Figure  5.  Comparison of experiment with simulation

    图  自由面粒子速度历史比较

    Figure  6.  Measured and calculated velocities of the free surface particle

    图  铅飞片对称轴上不同测点的速度历史

    Figure  7.  Profile of velocities at different gauge points on the symmetry axis of Pb flyer

    表  1  铅飞片中不同时刻的马赫杆长度

    Table  1.   The length of Mach stem in Pb flyer at different time points

    t/(μs) Length of Mach stem/(mm)
    2.6 0
    2.7 0.80
    2.8 1.20
    2.9 1.60
    3.0 2.04
    3.1
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出版历程
  • 收稿日期:  2014-07-02
  • 修回日期:  2014-09-11

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