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A Virtual Test Facility for Simulating Detonation-and Shock-Induced Deformation and Fracture of Thin Flexible Shells

机译:虚拟试验设备,用于模拟薄壳的起爆和冲击诱发的变形和断裂

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The coupling of a dynamically adaptive Eulerian Cartesian detonation solver with hierarchical time-step refinement to a Lagrangian thin-shell finite element solver with fracture and fragmentation capabilities is presented. The approach uses a level-set function to implicitly represent arbitrarily evolving solid structures on the Cartesian mesh. The auxiliary algorithm used to efficiently transform the shell solver mesh on the fly into a distance function is sketched briefly. We detail the derivation of the employed engineering combustion model that eliminates the numerical stiffness otherwise inherent to detonation waves and describe our approach to modeling fracture. The thin-shell solver utilizes a subdivision finite element discretization and achieves element separation with interface edges and a cohesive law. For method validation and benchmarking, the simulation of the deformation of a circular thin copper plate under impulsive pressure loading is presented. As a realistic computational application, we consider a three-dimensional setup in which the passage of an ethylene-oxygen detonation wave induces large plastic deformations and rupture of a thin-walled tubular specimen made of aluminum. Special attention is paid to the verification of the hydrodynamic loading conditions. The computational fluid-structure interaction results are found to be in agreement with experimental observations.
机译:提出了动态自适应欧拉笛卡尔爆轰求解器与具有分段和分段功能的拉格朗日薄壳有限元求解器的分层时间步细化的耦合。该方法使用水平集函数隐式表示笛卡尔网格上任意演化的实体结构。简要概述了用于将飞行中的壳求解器网格有效地转换为距离函数的辅助算法。我们详细介绍了所采用的工程燃烧模型的推导,该模型消除了爆震波固有的数值刚度,并描述了我们对裂缝建模的方法。薄壳求解器利用细分有限元离散化,并通过界面边缘和内聚律实现元素分离。为了进行方法验证和基准测试,对圆形薄铜板在脉冲压力载荷下的变形进行了仿真。作为一个实际的计算应用,我们考虑三维设置,其中乙烯-氧爆轰波的通过会引起大的塑性变形和铝制薄壁管状试样的破裂。特别注意流体动力载荷条件的验证。计算的流体-结构相互作用结果被发现与实验观察结果一致。

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