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A-FEM FOR COMPLEX MULTI-SCALE DAMAGE EVOLUTION IN LAMINATED COMPOSITES

机译:层状复合材料中复杂多尺度损伤演化的有限元分析

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摘要

In this paper, a new finite element method, named augmented finite element method (A-FEM) that can deal with arbitrary cracking in a continua without a priori knowledge of crack location and direction, is introduced. The very promising capability of A-FEM based numerical platform in addressing the critical issue of complex, multi-scale damage evolution in composite laminates have been demonstrated through simulations at structural level scale, sub-ply scale, and microscopic single-fiber scale. The potential of this high-fidelity numerical modeling method in serving as a key element in establishing virtual testing methodology for laminated composites has been highlighted. Further, the conceptual, experimental, and computational challenges associated with virtual testing are summarized and recent advances on systematic attempts to address these challenges have been discussed. The remaining major challenges related to virtual testing have been identified and strategies to answer these challenges outlined.
机译:本文介绍了一种新的有限元方法,称为增强有限元方法(A-FEM),该方法可以连续处理任意裂纹而无需先验裂纹位置和方向。通过在结构级别,亚层级别和微观单纤维级别进行仿真,已证明了基于A-FEM的数值平台在解决复合材料层压板复杂,多尺度损伤演变这一关键问题方面非常有前途的功能。强调了这种高保真数值建模方法作为建立层压复合材料虚拟测试方法的关键要素的潜力。此外,总结了与虚拟测试相关的概念,实验和计算挑战,并讨论了解决这些挑战的系统性尝试的最新进展。已经确定了与虚拟测试有关的其余主要挑战,并概述了应对这些挑战的策略。

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  • 来源
  • 会议地点 Seattle WA(US)
  • 作者单位

    Dept of Mechanical and Aerospace Engineering, University of Miami Coral Gables, FL 33124, U. S. A. Tel 305-284-3221;

    Fax: 305-284-2580;

    Email: qdyang@miami.edu;

    rnDept of Mechanical and Aerospace Engineering, University of Miami Coral Gables, FL 33124, U. S. A.rnDept of Mechanical and Aerospace Engineering, University of Miami Coral Gables, FL 33124, U. S. A. Teledyne Scientific Company, 1049 Camino Dos Rios Thousand Oaks CA 91360, U.S.A;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;
  • 关键词

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