Abstract
This investigation reports the numerical analysis of multilayered plates subjected to high velocity projectile impact. The numerical model is used to explain the residual velocity with respect to the time and study its effect on multilayered plates made with different materials. It is observed that impact velocity reduces significantly while using a layered combination of materials. The projectile is an ogive nose shape and it is modeled as 3D rigid body wherein the target plates are modeled as 3D deformable solids. Based on this study, effect of projectile velocity on deformation of layered plates is explained using sophisticated material model which is found to be the key to the success of such simulations. Mechanism of deformation and relation between striking and residual velocities is presented.
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References
Deb A, Raguraman M, Gupta NK, Madhu V (2008) Numerical simulation of projectile impact on mild steel armour plates using LS-DYNA: part I: validation. Def Sci J 58:422–432
Raguraman M, Deb A, Gupta NK (2008) A simulation-driven study of oblique impact of ogival-nosed projectiles on mild steel armour. Latin Am J Solids Struct 5:225–235
Shah QH (2009) Impact resistance of a rectangular polycarbonates armour plate subjected to single and multiple impacts. Int J Impact Eng 36(9):1128–1135
Klimpel A, Luksa K, Burda M (2010) Structure and properties of GMA surfaced armour plates. Arch Mater Sci Eng 43:109–116
Krishnan K, Sockalingam S, Bansal S, Rajan SD (2010) Numerical simulation of ceramic composite armour subjected to ballistic impact. Compos: Part B 41(8):583–593
Durmuşa A, Güden M, Gülçimen B, Ülkü S, Musa E (2011) Experimental investigations on the ballistic impact performances of cold rolled sheet metals. Mater Des 32(3):1356–1366
Nia AA, Hoseini GR (2011) Experimental study of perforation of multi-layered targets by hemispherical-nose projectile. Mater Des 32:1057–1065
Feli S, Asgari MR (2011) Finite element simulation of ceramic/composite armour under ballistic impact. Compos: Part B 42:771–780
Reis PNB, Ferreira JAM, Santos P, Richardson MOW, Santos JB (2012) Impact response of Kevlar composites with filled epoxy matrix. Compos Struct 94:3520–3528
Wang Q, Chen Z, Chen Z (2013) Design and characteristics of hybrid composite armour subjected to projectile impact. Mater Des 46:634–639
Deng Y, Zhang W, Cao Z (2013) Experimental investigation on the ballistic resistance of monolithic and multi-layered plates against ogival-nosed rigid projectiles impact. Mater Des 44:228–239
ABAQUS/Explicit (2011) User’s manual, version 6.11. Dassault Systèmes Simulia Corporation, Providence, Rhode Island, USA
Johnson GR, Cook WH (1983) A constitutive model and data for metals subjected to large strains, high strain rates and high temperatures. In: Proceedings of 7th international symposium on Ballistics, pp 541–547
Cowper GR, Symonds PS (1958) Strain hardening and strain rate effect in the impact loading of cantilever beams. Applied mathematics report, Brown University, p 28
Zukas JA (2008) Introduction to hydrocodes. Elsevier, USA
Steinberg DJ (1996) Equation of state and strength properties of selected materials. Lawrence Livermore National Laboratories, USA
Piekutowski AJ, Forrestal MJ, Poormon KL, Warren TL (1996) Perforation of aluminum plates with ogive-nose steel rods at normal and oblique impacts. Int J Impact Eng 18(7–8):877–887
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Goel, M.D. (2015). A Numerical Study of Ogive Shape Projectile Impact on Multilayered Plates. In: Matsagar, V. (eds) Advances in Structural Engineering. Springer, New Delhi. https://doi.org/10.1007/978-81-322-2190-6_23
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DOI: https://doi.org/10.1007/978-81-322-2190-6_23
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Publisher Name: Springer, New Delhi
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Online ISBN: 978-81-322-2190-6
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