International Journal for Research in Applied Science & Engineering Technology (IJRASET)

ISSN: 2321-9653; IC Value: 45.98; SJ Impact Factor: 7.538

Volume 11 Issue III Mar 2023- Available at www.ijraset.com

3) For Electrical Transformer.

4) For Bullet Proof Jacket And MilitaryAppliences

5) For Marine Vehicles.

6) In Defence Industries.

V. CONCLUSION

In this study, the ballistic performance of aluminium hemispherical sandwich thin shell structure was studied experimentally and numerically against ogive nosed projectile impact within sub ordnance velocity regime. Moreover, the effect of face sheet thickness, cell wall thickness and cell size on the sandwich shell performance also examined through numerical simulation. Bullet Impact with Aluminium PlateWith Different Angle Orientation using # ABAQUS

The work in this thesis was mainly on the study of experimental and numerical approach for the prediction of ballistic impact behavior on various surfaces against differentprojectile nose shape. Little emphasis was put on empirical and analytical modeling. Experiments were designed to serveas a basis of comparison to numerical simulations while still providing useful data to advance the field. The numerical contribution was to use and evaluate rather novel methods to Solve the penetration problem.

References

[1] Z. Wang, H. Tian, Z. Lu, W. Zhou, High-speed axial impact of aluminumhoneycomb–Experimentsand simulations, Compos. B Eng. 56 (2014) 1–8.

[2] B.L. Buitrago, C. Santiuste, S. Sanchez-Saez,

[3] E. Barbero, C. Navarro, Modelling of composite sandwich structures withhoneycomb core subjected to high-velocity

[4] impact, Compos. Struct. 92 (9) (2010) 2090–2096.

[5] J. Kepler, Impact penetration of sandwich panels at different velocities-Anexperimental parameter study: part I-Parameters and results, J. Sandw. Struct. Mater. 6 (4) (2004) 357–374.

[6] I. Iva~nez, S. Sanchez-Saez, Numerical modelling of the low-velocity impact response of composite sandwich beams with honeycomb core, Compos. Struct. 106 (2013) 716–723.

[7] K. Arslan, R. Gunes, M.K. Apalak, J. Reddy, Experimental tests and numerical

[8] modeling of ballisticimpact on honeycomb sandwich structures reinforced byfunctionally graded plates, J. Compos. Mater. 51 (29) (2017) 4009–4028.

[9] C. Menna, A. Zinno, D. Asprone, A. Prota, Numerical assessment of the impact

[10] behavior of honeycomb sandwich structures, Compos. Struct. 106 (2013)326–339.

[11] A. Kolopp, S. Rivallant, C. Bouvet, Experimental study of sandwich structures as armour against medium-velocity impacts, Int. J. Impact Eng. 61 (2013) 24–35.

[12] D. Zhang, Q. Fei, P. Zhang, Drop-weight impact behavior of honeycomb sandwich panels under a spherical impactor, Compos. Struct. 168 (2017) 633–645.

[13] Y. Chen, S. Hou, K. Fu, X. Han, L. Ye, Low-velocity impact response of composite sandwich structures: modelling and experiment, Compos. Struct. 168 (2017)

[14] 322–334.

[15] I. Elnasri, H. Zhao, Impact perforation of sandwich panels with aluminum foam core: a numerical and analytical study, Int. J. Impact Eng. 96 (2016) 50–60.

[16] C. Liu, Y. Zhang, J. Li, Impact responses of sandwich panels with fibre metal laminate skins and aluminium foam core, Compos. Struct. 182 (2017) 183–190.

[17] W. Hou, F. Zhu, G. Lu, D.-N. Fang, Ballistic impact experiments of metallic sandwich panels with aluminium foam core, Int. J. Impact Eng. 37 (10) (2010) 1045–1055.

[18] I. Iva~nez, C. Santiuste, E. Barbero, S. Sanchez-Saez, Numerical modelling of foam cored sandwich plates under high-velocity impact, Compos. Struct. 93 (9) (2011) 2392–2399.

[19] C. Liu, Y. Zhang, L. Ye, High velocity impact responses of sandwich panels with metal fibre laminate skins and aluminium foam core, Int. J. Impact Eng. 100 (2017) 139–153.

[20] L. Jing, C. Xi, Z. Wang, L. Zhao, Energy absorption and failure mechanism of metallic cylindrical sandwich shells under impact loading, Mater. Des. 52 (2013) 470–480 (1980-2015).

[21] L. Jing, Z. Wang, L. Zhao, Response of metallic cylindrical sandwich shells subjected to projectile impact experimental investigations, Compos. Struct. 107 (2014) 36–47.

[22] R. Mohmmed, F. Zhang, B. Sun, B. Gu, Finite element analyses of low- velocity impact damage of foam sandwiched composites with different ply angles face sheets, Mater. Des. 47 (2013) 189–199.

[23] S. Long, X. Yao, H. Wang, X. Zhang, Failure analysis and modeling offoam sandwich laminatesunder impact loading, Compos. Struct. 197 (2018)

[24] Eason, B. Noble, and I.N. Sneddon, “On certain integrals of Lipschitz- Hankel type involving products of Bessel functions,” Phil. Trans. Roy. Soc. London, vol. A247, pp. 529-551, April 1955. (references)