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Computational Modeling, Simulation, and Tailoring of Nonpenetrating Impact on a Generic Structure

机译:非穿透性影响通用结构的计算建模,仿真和量身定制

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摘要

A computational modeling and simulation study is carried out to gain insight and formulate strategy for the design and tailoring of panel-like space structure that can withstand space debris impact without penetration. To represent a generic engineering structure, the impacted panel structure is modeled as a set of bonded plates. The analysis is based on fundamental principles, which are elaborated and numerically simulated. The objective is to identify optimum configuration in terms of loading, structural dimensions, material properties, and composite layup. The analyses are based on dynamic response with emphasis on the elastic region. The direct numerical simulation is carried out in parallel for the analysis, synthesis, parametric study, and optimization. Simulation results of impact loading by a spherical rigid body at certain velocity perpendicular to the panel show how fiber-metal laminates can be structurally tailored to achieve a nonpenetrating impact. (C) 2015 American Society of Civil Engineers.
机译:进行了计算建模和仿真研究,以获取洞见并制定设计和定制面板状空间结构的策略,该结构可以承受空间碎片的撞击而不会穿透。为了表示通用的工程结构,将受影响的面板结构建模为一组粘合板。该分析基于基本原理,这些基本原理已详细阐述并进行了数值模拟。目的是在载荷,结构尺寸,材料特性和复合材料铺层方面确定最佳配置。分析基于动态响应,重点是弹性区域。并行进行直接数值模拟,以进行分析,综合,参数研究和优化。球形刚体在垂直于面板的一定速度下的冲击载荷仿真结果表明,如何在结构上调整纤维-金属层压板以实现非穿透性冲击。 (C)2015年美国土木工程师学会。

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  • 来源
    《Journal of aerospace engineering 》 |2016年第3期| 04015061.1-04015061.10| 共10页
  • 作者单位

    Univ Putra Malaysia, Dept Aerosp Engn, Fac Engn, Upm Serdang 43400, Selangor, Malaysia|Univ Al Azhar Indonesia, Fac Engn, Jalan Sisingamangaraja, Jakarta 121010, Indonesia;

    Univ Putra Malaysia, Dept Aerosp Engn, Fac Engn, Upm Serdang 43400, Selangor, Malaysia;

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