TY - JOUR
T1 - Study on the anti-penetration performance and perforation failure of Ti/Al3Ti/Al-laminated target
AU - Miao, Yuzhong
AU - Ding, Xuefeng
AU - Shi, Yan
AU - Yuan, Du
AU - Zhang, Rui
AU - Zhan, Yewang
AU - Wang, Wenbo
AU - Zhang, Shoubin
N1 - Publisher Copyright:
© 2025 World Scientific Publishing Europe Ltd.
PY - 2025
Y1 - 2025
N2 - The numerical simulation of bullet penetrating Ti/Al3Ti/Al-laminated targets with different individual thicknesses at initial velocity of 800 m/s and anti-penetration properties of the same-sized bullet under different initial velocities was carried out by Ansys/LS-DYNA. The implementation of the finite element model was validated against theoretical and penetration experimental results. The residual velocity of the bullet and specific energy absorption of area density (SEA) were employed to evaluate the anti-penetration performance of Ti/Al3Ti/Al-laminated target, and the resultant deformation process and failure modes of individual layers were, respectively, specified. Results show that the failure process consists of the fragmentation of local Al3Ti layers induced by compression wave, individual delamination failure induced by tensile longitudinal wave, compression shear fracture induced by the reflected transverse wave and shear wave, and shear bending of backboard induced by the tensile transverse wave and shear wave. Among the individual layers of the Ti/Al3Ti/Al-laminated target, the role of Al layers possessed the characteristics of energy absorption and wave-absorbing properties, TC4 layers presented the external toughening and main energy absorption, and the residual velocity of the bullet and supporting impact on the adjacent ductile layers were regulated by Al3Ti layers. This work aims to provide a theoretical basis and guidance for the military application and research on high-performance, lightweight laminated targets.
AB - The numerical simulation of bullet penetrating Ti/Al3Ti/Al-laminated targets with different individual thicknesses at initial velocity of 800 m/s and anti-penetration properties of the same-sized bullet under different initial velocities was carried out by Ansys/LS-DYNA. The implementation of the finite element model was validated against theoretical and penetration experimental results. The residual velocity of the bullet and specific energy absorption of area density (SEA) were employed to evaluate the anti-penetration performance of Ti/Al3Ti/Al-laminated target, and the resultant deformation process and failure modes of individual layers were, respectively, specified. Results show that the failure process consists of the fragmentation of local Al3Ti layers induced by compression wave, individual delamination failure induced by tensile longitudinal wave, compression shear fracture induced by the reflected transverse wave and shear wave, and shear bending of backboard induced by the tensile transverse wave and shear wave. Among the individual layers of the Ti/Al3Ti/Al-laminated target, the role of Al layers possessed the characteristics of energy absorption and wave-absorbing properties, TC4 layers presented the external toughening and main energy absorption, and the residual velocity of the bullet and supporting impact on the adjacent ductile layers were regulated by Al3Ti layers. This work aims to provide a theoretical basis and guidance for the military application and research on high-performance, lightweight laminated targets.
KW - Laminated target
KW - anti-penetration performance
KW - failure mechanisms
KW - stress evolution
KW - stress wave propagation
UR - https://www.scopus.com/pages/publications/105008525022
U2 - 10.1142/S2047684125500137
DO - 10.1142/S2047684125500137
M3 - 文章
AN - SCOPUS:105008525022
SN - 2047-6841
JO - International Journal of Computational Materials Science and Engineering
JF - International Journal of Computational Materials Science and Engineering
M1 - 2550013
ER -