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Structural Analyses of Solid Propellant Grains under Ignition Pressurization using Explicit Dynamics Method

机译:点火压力下固体推进剂颗粒的显式动力学分析

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A 3-dimensional structural analysis of propellant grains in a gas generator during its ignition event using explicit dynamic method was conducted in this study. This innovative approach enabled the author to reproduce the failure modes and understand the system failure in detail. Explicit Dynamics method integrates the time of all meshes at every time step (explicit) and the time step is controlled by the speed of sound traveling through the structural materials ensuring solutions representative to the real time behavior (dynamics). Largangian/ Eulerian coupled meshes are utilized to solve the behaviors and interactions of solid (propellant grains assembly by Lagrange) and fluid (gaseous combustion products from igniter by Euler) parts. This method computes the transient pressure loading representative to device geometry directly and not in need of making major assumption of stress loading conditions while performing the analysis. Results of pressure measurements at various locations inside gas generators for the model validations are also reported in this paper.
机译:在这项研究中,采用显式动力学方法对气体发生器中的推进剂颗粒进行点火过程进行了三维结构分析。这种创新的方法使作者能够重现故障模式并详细了解系统故障。显式动力学方法将每个时间步(显式)中所有网格的时间进行积分,并且该时步由通过结构材料传播的声音速度控制,从而确保代表实时行为(动力学)的解决方案。 Largangian / Eulerian耦合网格用于解决固体(Lagrange的推进剂颗粒组装)和流体(Euler的点火器产生的气态燃烧产物)零件的行为和相互作用。该方法直接计算代表设备几何形状的瞬态压力载荷,并且在执行分析时不需要对应力载荷条件做出主要假设。本文还报告了气体发生器内部各个位置的压力测量结果,以进行模型验证。

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