Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843, USA Department of Materials Science and Engineering, Texas A&M University, College Station, TX 77843, USA Department of Engineering Sciences and Mathematics, Luleå University of Technology, 971 87 Luleå, Sweden
Philos Trans A Math Phys Eng Sci. 2016 Jul 13;374(2071):20150280. doi: 10.1098/rsta.2015.0280.
Structural integrity of composite materials is governed by failure mechanisms that initiate at the scale of the microstructure. The local stress fields evolve with the progression of the failure mechanisms. Within the full span from initiation to criticality of the failure mechanisms, the governing length scales in a fibre-reinforced composite change from the fibre size to the characteristic fibre-architecture sizes, and eventually to a structural size, depending on the composite configuration and structural geometry as well as the imposed loading environment. Thus, a physical modelling of failure in composites must necessarily be of multi-scale nature, although not always with the same hierarchy for each failure mode. With this background, the paper examines the currently available main composite failure theories to assess their ability to capture the essential features of failure. A case is made for an alternative in the form of physical modelling and its skeleton is constructed based on physical observations and systematic analysis of the basic failure modes and associated stress fields and energy balances. This article is part of the themed issue 'Multiscale modelling of the structural integrity of composite materials'.
复合材料的结构完整性受微观结构尺度上开始的失效机制控制。局部应力场随失效机制的发展而演变。在失效机制从开始到临界的整个过程中,纤维增强复合材料中的控制长度尺度从纤维尺寸变化为特征纤维结构尺寸,最终根据复合材料的配置和结构几何形状以及施加的载荷环境变化为结构尺寸。因此,复合材料失效的物理建模必须具有多尺度性质,尽管对于每种失效模式并非总是具有相同的层次结构。在此背景下,本文研究了目前可用的主要复合材料失效理论,以评估它们捕获失效基本特征的能力。提出了一种替代方法,即物理建模,并基于对基本失效模式以及相关应力场和能量平衡的物理观察和系统分析,构建了其框架。本文是“复合材料结构完整性的多尺度建模”主题问题的一部分。