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Ballistic Performance of Thin Aluminium Cylindrical and Hemispherical Shells

机译:薄铝圆柱和半球壳的弹道性能

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The objective of study was to carry out the numerical simulation to compare the ballistic resistance failure mode and energy-dispersed characteristic of Al-H1100 thin hemispherical shell and cylindrical shell. Span diameter (200 mm), thickness (0.7 and 1 mm) and mass of hemispherical and cylindrical shells kept constant for direct comparison. Ogive-nosed projectiles of 19 mm diameter, 50.8 mm length and 52 mass were impacted at tip of the both shells target. Finite element modelling was carried out by using Abaqus explicit solver. Numerical result of cylindrical shell was elucidated against experimental result of hemispherical shell. The response of both the targets was compared in terms of global deformation, residual velocity, ballistic limit, failure mode and energy dispersed in plastic deformation. Result shows that the cylindrical shell outperformed than the hemispherical shell due to the large global deformation. Also both the cylindrical and hemispherical target failed by hole enlargement with petal formation.
机译:研究的目的是进行数值模拟,以比较Al-H1100薄半球壳和圆柱壳的抗弹性故障模式和能量分散特性。跨度直径(200mm),厚度(0.7和1mm)和半球形和圆柱形壳体的质量保持恒定,直接比较。在两个壳靶的尖端撞击了直径为19毫米,50.8mm长度和52质量的滴注液。使用ABAQUS明确求解器进行有限元建模。柱面壳的数值结果阐明了半球壳的实验结果。在全局变形,残余速度,弹道极限,故障模式和分散在塑性变形方面的响应,对目标的响应进行了比较。结果表明,由于全球变形大,圆柱形外壳比半球壳优于半球壳。圆柱形和半球形目标也通过孔扩大而失效,具有花瓣形成。

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