Numerical Simulation on Shock Initiation of Double-Shell Charges by High Velocity Impact

Author:

Liu Xue1,Zhang Qing Ming2

Affiliation:

1. Beijing University of Technology

2. Beijing Institute of Technology

Abstract

A two dimensional axisymmetric finite element analysis is preformed using AUTODYN-2D hydrocode, to simulate the dynamic response of explosive, named PBX9404 which is located behind double-shell, by the impact to shell surface resulted from high velocity spherical projectile. Simulation results shows that shock to detonation transition occurs when impact velocity is between 3.6~3.9km/s; but when the velocity increases to 4~4.3km/s, projectile will break up into pieces and the surface momentum density of debris cloud to second shell will decrease dramatically so no shock to detonation could occur. When the velocity further elevates to 4.4 km/s and above, projectile kinetic energy will cover the energy of projectile break-up, and also provide sufficient energy to further increase the surface momentum density of debris cloud, with a result that shock to detonation can be observed again. In conclusion, there is a velocity blind zone in shock to detonation of high velocity projectile to double-shell charges.

Publisher

Trans Tech Publications, Ltd.

Reference10 articles.

1. Shin Hyunho, Lee Woong. A numerical study on the detonation behavior of double reactive cassettes by impacts of projectiles with different nose shapes, International Journal of Impact Engineering, vol. 28, pp.349-362, (2003).

2. D. Touati, G. Tivon, S. Peles, A. Alfo, L. Bank, A. Shvarts, et al. Numerical prediction of the initiation of confined heterogeneous explosives by fragment penetration, 23rd International Symposium on Ballistics. Tarragona, Spain, 2007, pp.145-152.

3. Wei Yuzhang, Fang Qing, Tan Hua, Zhang Shouqi. On the projectile oblique impact initiation conditions for explosives covered with a plate, 16th International Symposium on Ballistics. San Francisco, California, 1996, pp.87-91.

4. C. Doolan, Two-stage light gas gun for the study of high speed impact in propellants, p. 30p, (2001).

5. Larry D. Libersky, Albert G. Petschek, Theodore C. Carney, Jim R. Hipp, Firooz A. Allahdadi. High strain lagrangian hydrodynamics: a three-dimensional SPH code for dynamic material response, Journal of Computational Physics, vol. 109, pp.67-75, (1993).

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