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Analytical Investigation of the Toughening Potential of a Failure Tailoring Concept

机译:裁缝概念的增韧潜力的分析研究

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摘要

A parametric study has been performed to determine the upper bounds of toughening benefit achievable using an approximate model for the response of one-dimensional, tailored, flexible composite-material tethers with progressive failure. The tailoring concept is achieved through judicious arrangement of redundant load paths with unequal length and strength and has been proposed, modeled, and experimentally verified in previous research. The model is recast in this work using nondimensional material-independent parameters that are varied over ranges of interest in advanced composites. The effects of each parameter on the response of the tailored member are discussed. An increase of nearly two orders of magnitude in toughness over an untailored member is found to be attainable by taking complete advantage of the energy dissipated by the failure of each load path within the bounds of the study. Challenges to implementation of the tailored member as approximated by the model are also discussed.
机译:已经进行了参数研究,以确定使用近似模型对一维,量身定制的柔性复合材料系绳具有渐进性破坏的响应所能达到的增韧效果的上限。剪裁概念是通过合理安排长度和强度不相等的冗余载荷路径来实现的,并且在先前的研究中已提出,建模和实验验证了剪裁概念。在这项工作中,该模型使用与材料无关的无量纲参数进行重铸,这些参数在高级复合材料的关注范围内变化。讨论了每个参数对定制成员响应的影响。通过充分利用研究范围内每个载荷路径失效所耗散的能量,可以发现,与未定制的构件相比,韧性可提高近两个数量级。还讨论了由模型近似对实施定制成员的挑战。

著录项

  • 来源
    《AIAA Journal》 |2010年第12期|p.2945-2953|共9页
  • 作者单位

    Georgia Institute of Technology, Atlanta, Georgia 30332;

    rnUniversity of Texas at Arlington, Arlington, Texas 76019 Mechanical and Aerospace Engineering Department, School of Mechanical and Aerospace Engineering, Box 19018, 500 West First Street, Woolf Hall 211;

    rnUniversity of Texas at Arlington, Arlington, Texas 76019 Mechanical and Aerospace Engineering Department, School of Mechanical and Aerospace Engineering, Box 19018, 500 West First Street, Woolf Hall 211;

  • 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

    b: width of the member; E_(11): modulus of elasticity; F: nondimensional load; K: stiffness of a link; k: stiffness of a segment; et al;

    机译:b:成员的宽度;E_(11):弹性模量;F:无量纲载荷;K:连杆的刚度;k:段的刚度;等;

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