[1] 张向荣, 朱玉荣, 林俊德, 等. 压缩氮气驱动的高速气炮实验技术[J]. 航天器环境工程, 2015, 32(4): 343-348. Zhang Xiangrong, Zhu Yurong, Lin Junde, et al.Experimental Techniques of High Velocity Gas Gun Driven by Compressed Nitrogen[J]. Spacecraft Environment Engineering, 2015, 32(4): 343-348. [2] Schmidt R M, Housen K R, Piekutowski A J, et al.Cadmium Simulation of Orbital-Debris Shield Performance to Scaled Velocities of 18 km/s[J]. Journal of Spacecraft and Rockets (S0022-4650), 1994, 31(5): 866-877. [3] Ma S, Zhang X, Qiu X M.Comparison Study of MPM and SPH in Modeling Hypervelocity Impact Problems[J]. International Journal of Impact Engineering (S0734-743X), 2009, 36: 272-282. [4] 张雄, 廉艳平, 刘岩, 等. 物质点法[M]. 1版. 北京:清华大学出版社, 2013: 7, 46-50. Zhang Xiong, Lian Yanping, Liu Yan, et al.The Material Point Method[M]. Beijing: Tsinghua University Press, 2013: 7, 46-50. [5] 唐蜜. 基于欧拉方法的超高速撞击程序研制及碎片云物相分布数值模拟[D]. 绵阳: 中国工程物理研究院, 2015. Tang Mi.Development of Hypervelocity Impact Codes Based on Euler Method and Numerical Study of the Phase Distribution in Debris Cloud[D]. Mianyang: China Academy of Engineering Physics, 2015. [6] 李宝宝, 汤文辉, 冉宪文. 两种物态方程在超高速碰撞数值模拟中的比较[J]. 航天器环境工程, 2010, 27(5): 576-581. Li Baobao, Tang Wenhui, Ran Xianwen.Comparison of Two Equations of State in Numerical Simulation of Hypervelocity Impacts[J]. Spacecraft Environment Engineering, 2010, 27(5): 576-581. [7] 汤文辉, 张若棋. 物态方程理论及计算概论[M]. 2版. 北京: 高等教育出版社, 2008: 159-167. Tang Wenhui, Zhang Ruoqi.Introduction to Theory and Computation of Equations of State[M]. Beijing: Higher Education Press, 2008: 159-167. [8] ROYCE E B.GRAY, a Three-Phase Equation of State for Metals: UCRL-51121[R]. USA: Lawrence Livermore Lab, 1971. [9] Wingate C A, Stellingwerf R F, Davison R F, et al.Models of High Velocity Impact Phenomena[J]. International Journal of Impact Engineering (S0734-743X), 1993, 14: 819-830. [10] 张庆明, 黄风雷. 超高速碰撞动力学引论[M]. 1版. 北京: 科学出版社, 2000: 107-109. Zhang Qingming, Huang Fenglei.Introduction to Hypervelocity Impact Dynamics[M]. Beijing: Science Press, 2000: 107-109. [11] Christiansen E L.Meteoroid/Debris Shielding: TM-2003-210788[R]. USA: NASA, 2003 [12] 张庆明, 谈庆明, 张德良, 等. 超高速冲击铝双层板的熔化效应[J]. 力学学报, 1995, 27(3): 257-266. Zhang Qingming, Tan Qingming, Zhang Deliang, et al.Melting Effects of Aluminum Dual-Sheet Structure in Hypervelocity Impact[J]. Acta Mechanica Sinica, 1995, 27(3): 257-266. [13] 徐小刚, 贾光辉, 黄海, 等. 双层板超高速撞击弹道极限方程综合建模[J]. 系统仿真学报, 2011, 23(1), 172-176. Xu Xiaogang, Jia Guanghui, Huang Hai, et al.Integrated Method for Ballistic Limit Equations of Double Plate under Hypervelocity Impact[J]. Journal of System Simulation, 2011, 23(1): 172-176. [14] Christiansen E L.Whipple Shield Sizing Equations: TM-2003-105539[R]. USA: NASA, 1991. [15] Poormon K L, Piekutowski A J.Comparison of Cadmium and Aluminum Debris Clouds[J]. International Journal of Impact Engineering (S0734-743X), 1995, 17: 639-648. |