The Analysis and Simulation of the Effect of Explosion Shock Overload on Follow-on Projectile
Xinying Xue · Journal of Projectiles.Rockets.Missiles and Guidance · 2011
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.