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首页> 外文期刊>Thin-Walled Structures >Effect of eccentricity and obliquity on the ballistic performance and energy dissipation of hemispherical shell subjected to ogive nosed
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Effect of eccentricity and obliquity on the ballistic performance and energy dissipation of hemispherical shell subjected to ogive nosed

机译:偏心和倾斜对术后颈椎壳弹道性能和能量耗散的影响

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摘要

A numerical study was undertaken to investigate the effect of projectile eccentricity and obliquity impact on the ballistic performance of the Aluminium 1100-H12 1 mm thick hemispherical shell against ogive nose projectile. The projectile eccentric distance was taken with respect to the radius of the shell such as 0th, R/4th, 2R/4th and 3R/4th whereas, the incidence angle of the projectile as 0?, 15?, 30?, 45?, and 60? for each shell (68, 100, 150 and 200 mm diameter). The projectile was impacted at different velocities for each incidence angle and eccentric distance and ballistic limit obtained. Three-dimensional finite element simulations were carried out by using the Abaqus/explicit solver. Johnson cook material model was used to simulate the behaviour of a hemispherical shell. The results of the numerical study were elucidated through the experimental result conducted for normal impact. Moreover, user-defined coding written in python was used to obtain the energy dissipation in different stretching mode. The result showed that the ballistic performance of the target was influenced by both the eccentricity and obliquity. Also, the target was failed in ductile hole enlargement with petals formation however, the number of petals form was depended upon the eccentricity and obliquity.
机译:采取了数值研究,以研究射弹偏心和倾斜对铝合金1100-H12 1毫米厚的半球壳体的弹道性能的影响。射弹偏心距离相对于壳的半径,例如0th,R / 4,2R / 4th和3r / 4th,而射弹的入射角为0?,15?,30?,45?,和60?对于每个壳(68,100,150和200mm直径)。射弹对每个入射角和偏心距离和弹道限制的不同速度影响。通过使用ABAQUS /显式求解器进行三维有限元模拟。 Johnson Cook材料模型用于模拟半球形壳的行为。通过对正常撞击进行的实验结果阐明了数值研究的结果。此外,在Python中写入的用户定义编码用于获得不同拉伸模式的能量耗散。结果表明,目标的弹道性能受到偏心率和倾斜的影响。此外,靶在延性空穴扩大中失效,具有花瓣形成,然而,花瓣形式的数量依赖于偏心和倾斜。

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