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Damage analysis for structural integrity and durability of composite materials

机译:复合材料结构完整性和耐久性的损伤分析

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摘要

Composite structures for mechanical and aerospace applications are designed to retain structural integrity and remain durable for the intended service life. Since the early 1970s important advances have been made in characterizing and modelling the underlying mechanical behaviour and developing tools and methodologies for predicting fracture and fatigue of composite materials. This paper presents a review of the concepts and analyses related to this area, and illustrates these by a few examples. The topics discussed are composite material strength in tension, compression and shear, damage and its progression in monotonic and cyclic loading, fatigue life prediction and damage induced changes in visco-elastic response.
机译:机械和航空航天应用的复合结构旨在保持结构完整性,并在预期使用寿命内保持耐用。自1970年代初以来,在表征和建模基本机械行为以及开发用于预测复合材料的断裂和疲劳的工具和方法方面取得了重要进展。本文介绍了与此领域相关的概念和分析,并通过一些示例进行了说明。讨论的主题是复合材料的拉伸,压缩和剪切强度,损伤及其在单调和循环载荷下的进展,疲劳寿命预测以及损伤引起的粘弹性响应变化。

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