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Modelling of composite sandwich structures with honeycomb core subjected to high-velocity impact

机译:高速冲击下蜂窝状复合夹层结构的建模

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摘要

In this study the perforation of composite sandwich structures subjected to high-velocity impact was analysed. Sandwich panels with carbon/epoxy skins and an aluminium honeycomb core were modelled by a three-dimensional finite element model implemented in ABAQUS/Explicit. The model was validated with experimental tests by comparing numerical and experimental residual velocity, ballistic limit, and contact time. By this model the influence of the components on the behaviour of the sandwich panel under impact load was evaluated; also, the contribution of the failure mechanisms to the energy-absorption of the projectile kinetic energy was determined.
机译:在这项研究中,分析了复合材料夹层结构在高速冲击下的穿孔情况。通过在ABAQUS / Explicit中实现的三维有限元模型对具有碳/环氧表皮和铝蜂窝芯的夹芯板进行建模。通过比较数值和实验残余速度,弹道极限和接触时间,通过实验测试验证了该模型。通过该模型,评估了在冲击载荷下组件对夹芯板性能的影响。此外,确定了破坏机理对弹丸动能能量吸收的贡献。

著录项

  • 来源
    《Composite Structures》 |2010年第9期|2090-2096|共7页
  • 作者单位

    Department of Continuum Mechanics and Structural Analysis, University Carlos III of Madrid, Avda. de la Universidad 30, 28911 Leganes, Madrid, Spain Department of Industrial Technology, Simon Bolivar University, Valle de Sartenejas, Caracas, Venezuela;

    rnDepartment of Continuum Mechanics and Structural Analysis, University Carlos III of Madrid, Avda. de la Universidad 30, 28911 Leganes, Madrid, Spain;

    rnDepartment of Continuum Mechanics and Structural Analysis, University Carlos III of Madrid, Avda. de la Universidad 30, 28911 Leganes, Madrid, Spain;

    rnDepartment of Continuum Mechanics and Structural Analysis, University Carlos III of Madrid, Avda. de la Universidad 30, 28911 Leganes, Madrid, Spain;

    rnDepartment of Continuum Mechanics and Structural Analysis, University Carlos III of Madrid, Avda. de la Universidad 30, 28911 Leganes, Madrid, Spain;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    sandwich structures; numerical simulation; high-velocity impact; honeycomb core;

    机译:夹层结构数值模拟高速冲击;蜂窝芯;

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