Article ID Journal Published Year Pages File Type
5028308 Procedia Engineering 2017 7 Pages PDF
Abstract
Hollow Al-6061 T6 cylinders weighing 11 g, after being accelerated through a four-stage electromagnetic launcher at upto 434 m/s, impact on 3 mm thick Al-6061 T6 plates. Plate perforation occurs at 367 m/s and residual velocity of the projectiles is obtained. Post-impact, the projectiles fail by ejection of tip as a thin ring. Simulations are carried out using Smooth Particle Hydrodynamics technique using either Bao-Wierzbicki or a recent parameterization of the Johnson-Cook failure model for Al-6061 T6. Trend in the residual velocities is insensitive to the failure model employed. Tip failure is reproduced in both failure models. Thus, the tip failure in the hollow AL-6061 T6 projectiles is adequately explained as an instance of ductile failure. The target plates fail by petalling which is reproduced in the simulations as well.
Related Topics
Physical Sciences and Engineering Engineering Engineering (General)
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