TY - GEN
T1 - Characteristics of shock initiation of single-shell and double-shell casing charges
AU - Liu, Xue
AU - Zhang, Qingming
AU - He, Yuanhang
AU - Zhai, Zhe
PY - 2012
Y1 - 2012
N2 - According to different type tactical missile warhead, structure of which was equivalent to charges covered by single-shell or double-shell. The shock initiation response of cast TNT charges, covered by single-shell and double-shell casing impacted by hypervelocity fragment was investigated using non-linear dynamics software AUTODYN. Results shows that in hypervelocity impact conditions, the first layer of double-shell charge imposed severe breaking effect to fragment and generated debris clouds, then the surface impulse density of fragment to rear shell reduces significantly. When impacted by same mass, shape, velocity projectile, deflagration will occur for single shell charges, however, no deflagration can be observed for double shell charges with the same thickness.
AB - According to different type tactical missile warhead, structure of which was equivalent to charges covered by single-shell or double-shell. The shock initiation response of cast TNT charges, covered by single-shell and double-shell casing impacted by hypervelocity fragment was investigated using non-linear dynamics software AUTODYN. Results shows that in hypervelocity impact conditions, the first layer of double-shell charge imposed severe breaking effect to fragment and generated debris clouds, then the surface impulse density of fragment to rear shell reduces significantly. When impacted by same mass, shape, velocity projectile, deflagration will occur for single shell charges, however, no deflagration can be observed for double shell charges with the same thickness.
KW - Characteristic of shock initiation
KW - Double-shell casing
KW - Hypervelocity impact
KW - Shock initiation
UR - http://www.scopus.com/inward/record.url?scp=81255189370&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMM.110-116.485
DO - 10.4028/www.scientific.net/AMM.110-116.485
M3 - Conference contribution
AN - SCOPUS:81255189370
SN - 9783037852620
T3 - Applied Mechanics and Materials
SP - 485
EP - 491
BT - Mechanical and Aerospace Engineering
T2 - 2nd International Conference on Mechanical and Aerospace Engineering, ICMAE 2011
Y2 - 29 July 2011 through 31 July 2011
ER -