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Numerical simulation of shock wave processes at rocket explosion at launch position or in flight

机译:火箭爆炸在发射位置或飞行中的冲击波过程的数值模拟

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摘要

The two-dimensional gas dynamic problem concerning the rocket explosion in the launch position and during the active flight leg is solved. The shock wave stage of the process, accompanying the explosion, has been studied using the numerical simulation. Space and time distribution of the gas dynamic functions after the explosion is determined, and also the center-of-mass trajectory of the exploded rocket is estimated and initial data are formulated for solving the problem of the creation and dynamics of the fire ball, which is necessary to develop the emergency system of cosmonauts rescue.
机译:解决了发射位置和活动飞行腿部火箭爆炸的二维气体动态问题。 已经使用数值模拟研究了伴随爆炸的过程的冲击波阶段。 在确定爆炸后,气体动态功能的空间和时间分布,并且估计爆炸火箭的质量轨迹估计,并配制了初始数据以解决消防球的创作和动态的问题 有必要开发宇航员救援的急救体系。

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