论文部分内容阅读
为了提高我导弹对抗生存能力和我拦截弹药摧毁来袭导弹的毁伤概率,以巡航导弹发动机舱为研究对象进行了巡航导弹的易损性和毁伤效应研究。在建立巡航导弹发动机舱模拟等效靶的基础上,利用模拟战斗部对巡航导弹发动机舱模拟等效靶进行了冲击毁伤作用实验,研究了发动机舱在破片与冲击波耦合作用下的毁伤模式,分析了其毁伤机理,得到了其在破片与冲击波耦合作用下的毁伤判据。
In order to enhance the missile’s ability to survive against missiles and the missile’s ability to intercept ammunition to destroy incoming missiles, the cruise missile engine compartment was studied for the vulnerability and damage effects of cruise missiles. Based on the simulation equivalent target of the cruise missile engine compartment, a simulation warhead was used to simulate the impact of the cruise missile on the simulated equivalent target. The damage modes of the engine compartment under the coupling of the fragment and shock wave were studied. The damage mechanism is obtained and its damage criterion is obtained under the coupling action of fragments and shock wave.