Dynamical Penetration Simulation of Solid Target under Shaped Charge Liner

Article Preview

Abstract:

A finite element model of rock mass under linear conical shaped charge liner including explosive, metal liner, air and rock mass is built. The ALE algorithm is applied to simulate the penetration characteristic of rock mass and analyze the influencing factors such as the cone angle, the wall thickness of metal liner, and the standoff distance. Fluid-structure coupling condition is used between metal liner and air as well as between air and rock mass. The present results show that LS-DYNA can be well used to simulate the progress of jet formation and rock penetration with the transmission and focusing of shock stress wave. The different cone angles, wall thicknesses of the metal liner, and the standoff distances will influence the penetration effect.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

410-416

Citation:

Online since:

April 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Y. Xun, L.H. Yan, S.Y. Zeng, Process of the shaped charge technique. Science Technology and Engineering. 8(2008) 4251-4257.

Google Scholar

[2] D. Novotney, M. Mallery, Historical development of linear shaped charge. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH, USA, 2007, pp.8-11.

DOI: 10.2514/6.2007-5141

Google Scholar

[3] J.F. Molinari, Finite element simulation of shaped charge. Finite Elem Anal Des. 38(2002) 921-936.

Google Scholar

[4] D.Q. Cao, S.R. Yun, G.Y. Ding , Q.K. Jin , 3-D numerical simulation of jet penetrate target using ALE method. Journal of Beijing Institute of Technology. 20(2000) 171-173.

Google Scholar

[5] L.W. Chen, J.G. Ning, Three-dimensional numerical simulation of shaped charge jet. Chinese Journal of Computational Mechanics. 22(2005) 55-58.

Google Scholar

[6] V.V. Bashurov, G.V. Bebenin, A.G. Ioilev, Numerical simulation of rod particles hypervelocity impact effectiveness at various attack angles. Int J Impact Eng. 20 (1997) 255-262.

DOI: 10.1016/s0734-743x(97)87481-7

Google Scholar

[7] T. Rabczuk, S.P. Xiao, M. Sauer, Coupling of mesh free methods with finite elements: Basic concepts and test results. Comm Numer Meth Eng. 22(2006) 1031-1065.

DOI: 10.1002/cnm.871

Google Scholar

[8] T. Rabczuk, T. Belytschko, A three dimensional large deformation mesh free method for arbitrary evolving cracks. Comput Method Appl M. 196(2007) 2777-2799.

DOI: 10.1016/j.cma.2006.06.020

Google Scholar

[9] T. Rabczuk, G. Zi, S. Bordas, H. Nguyen-Xuan, A simple and robust three dimensional cracking-particle method without enrichment. Comput Method Appl M. 199(2010) 2437-2455.

DOI: 10.1016/j.cma.2010.03.031

Google Scholar

[10] Z.C. Mi, R.H. Yang, Shaped charge penetrating rocks. Journal of China University of Science and Technology. 28(1998) 200-204.

Google Scholar

[11] Z. Z Xiong, C. Wang, D.W. Zhong, Numerical simulation of linear shaped charge on rock cutting. Chinese Journal of Explosives and Propellants. 27(4) (2004) 29-32.

Google Scholar

[12] D.H. Liu, Study on the penetration of frozen soil and stone by shaped charge. Master thesis of Dalian University of Technology, Dalian, Liaoning, CHN, (2006).

Google Scholar

[13] S. Heimbs, Computational methods for bird strike simulations: A review. Comput Struct. 89 (2011) 2093-2112.

DOI: 10.1016/j.compstruc.2011.08.007

Google Scholar

[14] LSTC (Livemore Software Technology Corporation), LS-DYNA theoretical manual. Livermore Software Technology Corporation, Livermore, CA, USA, (1998).

Google Scholar

[15] LSTC (Livemore Software Technology Corporation), LS-DYNA keyword user's manual, Livermore Software Technology Corporation, Livermore, CA, USA, (2003).

Google Scholar

[16] D.Y. Shi, Y.C. Li, S.M. Zhang, Explicit dynamical analysis based on ANSYS/ LS-DYNA 8. 1, Tsinghua University Press, Beijing, CHN, (2005).

Google Scholar