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Microstructural and mechanical responses of various aluminum alloys to ballistic impacts by armor piercing projectile

机译:各种铝合金对盔甲弹性弹射弹道弹道的微观结构和机械反应

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摘要

The ballistic performances and deformation behaviors of AA5052-H112, AA5083-H112, AA6061-T6, and AA7075-T651 aluminum alloy plates struck by 7.62 mm armor piercing projectiles were investigated. Ballistic impact tests were performed using 25 mm thick aluminum alloy plates with different projectile velocities to obtain the ballistic limit velocity (V-50). Microstructural and mechanical responses to the ballistic impacts were studied using optical microscopy, electron backscattered diffraction, transmission electron microscopy, and hardness measurements. Finite element analysis was performed to simulate the deformation behavior of the materials of interest. The ballistic limit velocity exhibited a linear relationship with the hardness and yield strength of the alloys, but not with the tensile strength or elongation. Ductile hole formation and strain hardening were observed in the AA5052-H112 and AA5083-H112 alloy plates, whereas AA6061-T6 exhibited both strain hardening and softening behaviors. The AA7075-T651 plate failed by a spalling mechanism accompanied by formation of adiabatic shear bands.
机译:研究了AA5052-H112,AA5083-H112,AA6061-T6和AA7075-T651铝合金板的弹道性能和变形行为被7.62mm Armor刺穿射弹撞击。使用具有不同射弹速度的25mm厚的铝合金板进行弹道冲击试验,以获得弹道极限速度(V-50)。使用光学显微镜,电子背散射衍射,透射电子显微镜和硬度测量研究了对弹道冲击的微观结构和机械响应。进行有限元分析以模拟感兴趣材料的变形行为。弹道极限速度与合金的硬度和屈服强度表现出直线关系,但不具有拉伸强度或伸长率。在AA5052-H112和AA5083-H112合金板中观察到延性孔形成和应变硬化,而AA6061-T6表现出应变硬化和软化行为。 AA7075-T651板通过伴随绝热剪切带的形成而失效。

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