汇聚型超高速发射装置一级飞片的计算设计

王宇 柏劲松 王翔 谭华 李平

王宇, 柏劲松, 王翔, 谭华, 李平. 汇聚型超高速发射装置一级飞片的计算设计[J]. 高压物理学报, 2015, 29(2): 155-160. doi: 10.11858/gywlxb.2015.02.011
引用本文: 王宇, 柏劲松, 王翔, 谭华, 李平. 汇聚型超高速发射装置一级飞片的计算设计[J]. 高压物理学报, 2015, 29(2): 155-160. doi: 10.11858/gywlxb.2015.02.011
WANG Yu, BAI Jin-Song, WANG Xiang, TAN Hua, LI Ping. Computational Design of Graded Density Impactors for Convergent Hypervelocity Launchers[J]. Chinese Journal of High Pressure Physics, 2015, 29(2): 155-160. doi: 10.11858/gywlxb.2015.02.011
Citation: WANG Yu, BAI Jin-Song, WANG Xiang, TAN Hua, LI Ping. Computational Design of Graded Density Impactors for Convergent Hypervelocity Launchers[J]. Chinese Journal of High Pressure Physics, 2015, 29(2): 155-160. doi: 10.11858/gywlxb.2015.02.011

汇聚型超高速发射装置一级飞片的计算设计

doi: 10.11858/gywlxb.2015.02.011
基金项目: 国家自然科学基金(11372294);中国工程物理研究院科学技术发展基金(2011B0202005,2011A0201002)
详细信息
    作者简介:

    王宇(1988-), 男, 硕士, 主要从事计算流体力学理论和数值模拟研究.E-mail:mishiwufeng@126.com

    通讯作者:

    柏劲松(1968—),男,博士,研究员,主要从事计算流体力学、计算爆炸力学等理论和数值模拟研究.E-mail:bjsong@foxmail.com

  • 中图分类号: O35; O347.1

Computational Design of Graded Density Impactors for Convergent Hypervelocity Launchers

  • 摘要: 在利用汇聚型超高速发射装置进行超高压条件下物质状态方程测量时,二级飞片需要具有平面性好、击靶速度高的特点。为此采用具有自主知识产权的多介质流体高精度欧拉并行计算程序HVL-MFPPM,对汇聚型超高速发射装置进行了数值模拟,优化设计了一级飞片93W层的结构。计算结果表明:当采用最优设计方案时(93W层的直径为20 mm,厚度为1.8 mm),一级飞片能够将克级的二级飞片加速到14 km/s以上;同时,这种设计可以提高速度增益和汇聚效果,并大幅度地改善二级飞片在发射管出口处的平面性。

     

  • 图  1.4 μs时二级飞片的ABC点和平面性参数

    Figure  1.  The ABC positions and planarity parameter of the second stage flyer at 1.4 μs

    图  二级飞片上ABC 3点的速度变化曲线

    Figure  2.  The velocity history of ABC positions on the second stage flyer

    图  Model 25-1.2和Model 22-1.6二级飞片在不同时刻的密度分布图

    Figure  3.  Density distributions of the second flyer at certain times for Model 25-1.2 and Model 22-1.6

    图  Model 25-1.2和Model 22-1.6二级飞片的变形过程

    Figure  4.  Deformation processes of the second stage flyer for Model 25-1.2 and Model 22-1.6

    图  计算模型一级飞片相对于初始模型的质量变化量

    Figure  5.  Mass of the first stage flyer for computation models in comparison with Model 25-1.2

    图  二级飞片自由面中心速度和速度增益随93W层直径的变化

    Figure  6.  Free surface velocity and velocity gain of the second stage flyer versus the diameter of 93W layer

    图  二级飞片平面性参数随93W层直径的变化

    Figure  7.  Planarity parameter varies with the diameter of 93W layer

    图  Model 20-1.8二级飞片在不同时刻的密度图

    Figure  8.  Density distributions of the second stage flyer at certain times for Model 20-1.8

    表  1  各模型参数和计算结果比较

    Table  1.   Parameters and calculated results of different computation models

    Diameter of
    93W/(mm)
    Thickness of combined
    layers/(mm)
    Mass variation of the
    1st stage flyer/(g)
    Velocity of the 2nd
    stage flyer/(g)
    Velocity
    gain
    δ/(mm)
    15 1.7 -0.325 14.07 2.07 -0.200
    15 2.0 1.451 14.52 2.14 -0.141
    18 1.6 0.167 14.17 2.08 -0.204
    18 1.8 1.486 14.68 2.16 -0.136
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出版历程
  • 收稿日期:  2013-05-06
  • 修回日期:  2014-09-12

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