内爆爆距对舱壁变形影响的数值研究

Numerical Simulation of Influence of Detonation Distance on Deflection of Bulkhead Deformation in In-Cabin Explosion

  • 摘要: 为研究舱内爆炸时爆距的改变对舱壁的毁伤效应,运用有限元分析软件建立了舱室内爆的仿真模型,分析了爆距变化对舱壁的变形影响及舱内冲击波压力的作用情况.结果表明:在爆距比L1/L2>1时,远端舱壁的变形挠度总大于近端舱壁.当爆距L1增大时,远端舱壁的挠度值呈线性增加,挠度增量约为爆距增量的11%,而近端舱壁的挠度变化不明显;舱内爆炸后作用于远端舱壁的冲击波为初始冲击波与来自近端舱壁及四周刚性舱壁的反射冲击波相互作用而形成的叠加波.

     

    Abstract: In order to study the damage effect of the change of explosion distance on in-cabin explosion, the simulation model of cabin explosion was established by using the finite element analysis software. The deformation of the bulkhead and the pressure of shock wave were analyzed. The results show that when the blasting distance ratio is L1/L2>1, the deflection of the far bulkhead is always greater than that of the near bulkhead. When the detonation distance L1 increases, the deflection of the far bulkhead increases linearly, and the deflection increment is about 11% of the explosion distance increment, but the deflection of the near bulkhead does not change significantly. The shock wave that reaches the far bulkhead for the first time after the explosion in the cabin is the superimposed wave formed by the interaction of the initial shock wave and the reflection shock wave from the near bulkhead and the rigid bulkhead.

     

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