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Numerical simulations of semi-armor-piercing projectile penetrating aircraft carrier target with different attack angle

机译:不同攻击角度半铠装射伤射击飞机载体靶的数值模拟

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Finite element method (FEM) models of semi-armor-piercing warhead penetrating aircraft carrier deck are established by numerical simulation method, which are validated by related experimental data. Base on the models, the process of semi-ARMOR-piercing warhead penetrating aircraft carrier deck with different attack angles are carried out. The results show that Attack angles have notable influence on penetration capability of the projectile. When the attack angel are 5°, 10°, 15°, 20°, and 25°, the values of residual velocity of the projectile decrease 1.7%, 6.9%, 17.8%, 34.6%, and 54.5%, respectively, and durative high accelerations come forth in the penetration process with varying degrees of structure distortion of the projectile. Ductility reaming damage mode and adiabatic plugging damage mode are exhibited in the penetration process. The FEM models and the results could provide reference for penetration effect research of semi-armor-piercing warhead penetrating aircraft carrier target.
机译:通过数值模拟方法建立了半铠装弹头穿透飞行器甲板的有限元方法(FEM)模型,由相关实验数据验证。基于模型,进行了具有不同攻击角的半铠装弹头穿透飞行器甲板的过程。结果表明,攻击角对射弹的渗透能力有显着影响。当攻击天使为5°,10°,15°,20°和25°时,射弹的剩余速度值分别降低1.7%,6.9%,17.8%,34.6%和54.5%,以及持续性渗透过程中的高速加速度出现,具有射弹的不同程度的结构变形。延展性铰孔损坏模式和绝热堵塞损坏模式在渗透过程中展出。有限元模型和结果可以为半铠装弹头穿透飞机载体目标提供渗透效果研究。

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