Volume 23 Issue 1
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CHI Run-Qiang, GUAN Gong-Shun, PANG Bao-Jun, ZHANG Wei, TANG Qi. Models for Momentum of Debris Cloud and Ejecta Produced by Hypervelocity Impacts of Aluminum Spheres with Thin Aluminum Sheets[J]. Chinese Journal of High Pressure Physics, 2009, 23(1): 59-64 . doi: 10.11858/gywlxb.2009.01.010
Citation: CHI Run-Qiang, GUAN Gong-Shun, PANG Bao-Jun, ZHANG Wei, TANG Qi. Models for Momentum of Debris Cloud and Ejecta Produced by Hypervelocity Impacts of Aluminum Spheres with Thin Aluminum Sheets[J]. Chinese Journal of High Pressure Physics, 2009, 23(1): 59-64 . doi: 10.11858/gywlxb.2009.01.010

Models for Momentum of Debris Cloud and Ejecta Produced by Hypervelocity Impacts of Aluminum Spheres with Thin Aluminum Sheets

doi: 10.11858/gywlxb.2009.01.010
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  • Corresponding author: CHI Run-Qiang
  • Received Date: 15 Apr 2008
  • Rev Recd Date: 10 Jul 2008
  • Issue Publish Date: 15 Feb 2009
  • Debris clouds produced by the normal impact of an aluminum alloy sphere with an aluminum alloy sheet can scatter flying downrange, as well as an ejecta veil is produced at the same time. The momentum of debris clouds and ejecta are necessary to create the debris clouds and ejecta theoretical models. 54 numerical simulations were performed using the SPH (smoothed particle hydrodynamics) technique in AUTODYN-2D, in which 6.35 mm diameter of 1100-O aluminum spheres impacted six thicknesses of 6061-T6 aluminum sheets at velocities ranging from 1.0 km/s to 5.0 km/s. Using the data from the numerical simulations, two respective regression models are developed for characterizing the momentum of debris clouds and ejecta produced by impacts with 1.0 km/sv5.0 km/s, 0.5 mm3.0 mm. In the two models, the independent variables are the impact velocity, v, and the thickness of the sphere, t, while the dependent variables are the momentum ratios (ratios of debris clouds momentum and ejecta momentum to sphere momentum). The effects of v and on the momentum of debris clouds and ejecta are investigated. Seven additional numerical simulations in the same way as above were carried out and values obtained are compared with the experimental data of NASA to evaluate the performance of the simulation.

     

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  • Zhang W, Pang B J, Zou J X, et al. Meteoroid and Space Debris Shielding Concepts for Spacecraft [J]. Journal of Harbin Institute of Technology, 1999, 32(2): 18-22. (in Chinese)
    张伟, 庞宝君, 邹经湘, 等. 航天器微流星体及空间碎片防护方案 [J]. 哈尔滨工业大学学报, 1999, 32(2): 18-22.
    Bernhard P P, Christiansen E L, Hyde J, et al. Hypervelocity Impact Damage into Space Shuttle Surfaces [J]. Int J Impact Eng, 1995, 17(1-3): 57-68.
    Christiansen E L. Enhanced Meteoroid and Orbital Debris Shielding [J]. Int J Impact Eng, 1995, 17(1-3): 217-228.
    Piekutowski A J. Formation and Description of Debris Cloud Produced by Hypervelocity Impact [R]. USA: NASA Marshall Space Flight Center, 1996.
    Schonberg W P, Ebrahim A R. Modeling Oblique Hypervelocity Impact Phenomena Using Elementary Shock Physics [J]. Int J Impact Eng, 1999, 23(1): 823-834.
    Schafer F K. An Engineering Fragmentation Model for the Impact of Spherical Projectiles on Thin Metallic Plates [J]. Int J Impact Eng, 2006, 33(1-12): 745-762.
    Zee R. Physics of Debris Clouds from Hypervelocity Impacts [R]. USA: NASA Marshall Space Flight Center, 1993.
    Hiermaier S, Konke D, Stilp A J, et al. Computational Simulation of the Hypervelocity Impact of Al-Sphere on Thin Plates of Different Materials [J]. Int J Impact Eng, 1997, 20(1-5): 363-374.
    Hayhurst C J, Hiermaier S J, Clegg R A, et al. Development of Material Models for Nextel and Kevlar-Epoxy for High Pressure and Strain Rates [J]. Int J Impact Eng, 1999, 23(1): 365-376.
    Hayhurst C J, Livingstone I H. Advanced Numerical Simulations for Hypervelocity Impact [R]. USA: Century Dynamics Incorporated, 1998.
    Zhang W, Pang B J, Jia B, et al. Numerical Simulation of Debris Cloud Produced by Hypervelocity Impact of Projectile on Bumper [J]. Chinese Journal of High Pressure Physics, 2004, 18(1): 47-52. (in Chinese)
    张伟, 庞宝君, 贾斌, 等. 弹丸超高速撞击防护屏碎片云数值模拟 [J]. 高压物理学报, 2004, 18(1): 47-52.
    AUTODYN Users Manual Revision 6. 0 [Z]. Concord, CA94520 USA: Century Dynamics Incorporated, 2005.
    Christiansen E L. Shielding Sizing and Response Equations [R]. USA: NASA Johnson Space Center, 1991.
    Zhou Y Z, Jiang F H. The Regression Analysis of the Experimental Data and the Remarkable Examination [J]. Physical Experiment of College, 2001, 14(4): 43-46. (in Chinese)
    周玉珠, 姜奉华. 实验数据的一元线性回归分析及其显著性检验 [J]. 大学物理实验, 2001, 14(4): 43-46.
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