Computational Design of Graded Density Impactors for Convergent Hypervelocity Launchers
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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。Abstract: When the convergent hypervelocity launcher is applied to measure the equation of states, the second stage flyer are required to have well impact planarity and high impact velocity. Taking this into consideration, our paralleled Eulerian code HVL-MFPPM is employed to investigate the hypervelocity launcher.According to the simulation results, the structure and dimensions of the first stage flyer are optimized.Finally, the best scheme (the diameter of the first stage flyer is 20 mm, and its thickness is 1.8 mm) is obtained, which leads to the successful launch of an intact gram magnitude tantalum flyer to a velocity over 14 km/s in numerical simulation, and significant improvements in the impact velocity and planarity of the second stage flyer.
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Key words:
- multi-fluid /
- hypervelocity launch /
- high resolution algorithm
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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
gainδ/(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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