刚性弹丸低速冲击2024-T351铝合金靶板仿真研究
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中国民用航空飞行学院

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V214.3

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Simulation Research of 2024-T351 Aluminum Alloy Targets under Low-velocity Impact by Rigid Projectiles
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    摘要:

    为探究2024-T351铝合金抗低速冲击响应特性,利用ABAQUS有限元软件,建立了0.6 mm半径弹丸以60 m/s初始速度正冲击2 mm厚度的2024-T351铝合金靶板仿真模型,并借鉴已有文献验证其有效性。为方便后续研究,建立了弹丸以不同初始速度(40 m/s~120 m/s)正冲击和不同入射角度(10°、20°和30°)斜冲击靶板模型,从靶板凹坑深度和弹丸速度两个角度进行分析。结果表明:冲击过程时间较短(约1.2 μs),凹坑深度随着冲击过程先增加后有所下降;靶板凹坑深度随冲击速度增加而增加,随入射角度增加而降低;靶板能量吸收率随冲击速度增加而增加,随入射角度增加而降低。

    Abstract:

    In order to explore the response characteristics of 2024-T351 aluminum alloy under low-velocity impact, the simulation model of 2 mm thickness 2024-T351 aluminum alloy target impacted by a radius of 0.6 mm projectile with an initial velocity of 60 m/s was established by using ABAQUS finite element software, and its effectiveness was verified by the existing literature. In order to facilitate the follow-up research, the models of targets impacted positively by projectiles with different initial velocities (40 m/s~120 m/s) and impacted obliquely by projectiles with different incidence angles (10°, 20° and 30°) were established, and the analysis was carried out from two perspectives: the depth of the target crater and the velocity of the projectile. The results show that the impact process time is short (about 1.2 μs), and the crater depth increases first and then decreases with the impact process. The crater depth of the target increases with the increase of impact velocity, and decreases with the increase of incidence angle.

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  • 收稿日期:2024-12-09
  • 最后修改日期:2024-12-09
  • 录用日期:2025-04-02
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