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Characterization, Modeling, and Failure Analysis of Composite Structure Materials under Static and Dynamic Loading.

机译:静态和动态载荷下复合结构材料的表征,建模和破坏分析。

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摘要

Composite structures have long been used in many industries where it is advantageous to reduce weight while maintaining high stiffness and strength. Composites can now be found in an ever broadening range of applications: sporting equipment, automobiles, marine and aerospace structures, and energy production. These structures are typically sandwich panels composed of fiber reinforced polymer composite (FRPC) facesheets which provide the stiffness and the strength and a low density polymeric foam core that adds bending rigidity with little additional weight. The expanding use of composite structures exposes them to high energy, high velocity dynamic loadings which produce multi-axial dynamic states of stress. This circumstance can present quite a challenge to designers, as composite structures are highly anisotropic and display properties that are sensitive to loading rates. Computer codes are continually in development to assist designers in the creation of safe, efficient structures. While the design of an optimal composite structure is more complex, engineers can take advantage of the effect of enhanced energy dissipation displayed by a composite when loaded at high strain rates. In order to build and verify effective computer codes, the underlying assumptions must be verified by laboratory experiments. Many of these codes look to use a micromechanical approach to determine the response of the structure. For this, the material properties of the constituent materials must be verified, three-dimensional constitutive laws must be developed, and failure of these materials must be investigated under static and dynamic loading conditions. In this study, simple models are sought not only to ease their implementation into such codes, but to allow for efficient characterization of new materials that may be developed. Characterization of composite materials and sandwich structures is a costly, time intensive process. A constituent based design approach evaluates potential combinations of materials in a much faster and more efficient manner.
机译:复合结构长期用于许多行业,在这些行业中,减轻重量同时保持高刚度和强度是有利的。现在,复合材料的应用范围越来越广:运动器材,汽车,船舶和航空航天结构以及能源生产。这些结构通常是由纤维增强聚合物复合材料(FRPC)面板组成的夹心板,可提供刚度和强度,以及低密度聚合物泡沫芯,可增加弯曲刚度而几乎没有额外的重量。复合材料结构的广泛使用使它们承受高能量,高速动态载荷,从而产生应力的多轴动态状态。这种情况对设计人员可能构成很大的挑战,因为复合材料结构具有高度的各向异性,并且显示出对加载速率敏感的特性。正在不断开发计算机代码,以帮助设计人员创建安全,高效的结构。虽然最佳复合材料结构的设计更加复杂,但工程师可以利用以高应变速率加载时复合材料显示出的增强的能量耗散效果。为了构建和验证有效的计算机代码,必须通过实验室实验来验证基本假设。这些代码中的许多代码看起来都使用微机械方法来确定结构的响应。为此,必须验证组成材料的材料特性,必须建立三维本构定律,并且必须在静态和动态载荷条件下研究这些材料的失效。在这项研究中,寻求简单的模型不仅可以简化将其实施为此类代码的方法,还可以有效地表征可能开发的新材料。复合材料和三明治结构的表征是一个昂贵,费时的过程。基于成分的设计方法以更快,更有效的方式评估材料的潜在组合。

著录项

  • 作者

    Werner, Brian Thomas.;

  • 作者单位

    Northwestern University.;

  • 授予单位 Northwestern University.;
  • 学科 Engineering General.;Engineering Materials Science.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 231 p.
  • 总页数 231
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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