| 反应装甲结构参数对飞板运动影响 |
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| 引用本文： | 刘宏伟,夏松林,赵靖,朱生盛. 反应装甲结构参数对飞板运动影响[J]. 兵器材料科学与工程, 2011, 34(5): 41-43 |
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| 作者姓名： | 刘宏伟 夏松林 赵靖 朱生盛 |
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| 作者单位： | 徐州空军学院,江苏徐州,221000;南空后勤部机场工兵勤务队,江苏南京,210022 |
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| 摘 要： | 根据反应装甲结构飞板变形的物理现象,利用瞬时爆轰理论,并考虑散心爆轰作用,建立了射夹层装药平板运动规律工程计算模型,分析不同结构参数反应装甲飞板运动影响。结果表明,实验和数值模拟结果一致。
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| 关 键 词： | 飞板运动 反应装甲 瞬时爆轰 |
Influence of the structure parameter of ERA on the moving of flying-panel |
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| LIU Hongwei,XIA Songlin,ZHAO Jing,ZHU Shengsheng. Influence of the structure parameter of ERA on the moving of flying-panel[J]. Ordnance Material Science and Engineering, 2011, 34(5): 41-43 |
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| Authors: | LIU Hongwei XIA Songlin ZHAO Jing ZHU Shengsheng |
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| Affiliation: | LIU Hongwei1,XIA Songlin1,ZHAO Jing2,ZHU Shengsheng1(1.Xuzhou Air Force College,Xuzhou 221000,China,2.Airfield Service Team of Air Force Logistic Department in Nanjing Army District,Nanjing 210022,China) |
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| Abstract: | According to the physical phenomen on of flying-panel deformation in confined-explosive structure,based on the theory of instantaneous detonation and the action of scatter denotation,calculation model of the moving rule of flying-panel was founded.The influence of the structure parameter of ERA on the moving of flying-panel was analysed.The results show that the simulation results agree with experimental data. |
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| Keywords: | moving of flying-panel ERA instantaneous detonation |
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