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Journal of Projectiles, Rockets, Missiles and Guidance >
The Analysis and Simulation of the Effect of Explosion Shock Overload on Follow-on Projectile
Received date: 2010-08-26
Online published: 2025-05-30
A simulation calculation for the flight and explosion of the following-on warhead by the nonlinear dynamic software "Autodyn" was conducted, the initial process in which the warhead detonates and submunition follow-on process target was simulated, and the simulation calculation of the effect of overload caused by warhead detonation on flight velocity, flight attitude and structure strength was performed. The data of the follow-on submunition before and after overload were obtained, and the compare and analysis between the simulation result and test result for a certain version were completed.
LI Guodeng , WANG Ping , XUE Xinying . The Analysis and Simulation of the Effect of Explosion Shock Overload on Follow-on Projectile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(2) : 102 -104 . DOI: 10.15892/j.cnki.djzdxb.2011.02.064
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