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Fatigue and post-fatigue tensile behaviour of non-crimp stitched and unstitched carbon/epoxy composites

机译:非卷曲缝合和未缝合的碳/环氧树脂复合材料的疲劳和疲劳后拉伸行为

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摘要

An experimental study is described in this paper dealing with the tensile–tensile fatigue and the quasistatic\udpost-fatigue tensile behaviour of a structurally stitched multi-ply carbon composite and the\udunstitched counterpart. The influence of the stitching on the fatigue life and on the residual post-fatigue\udquasi-static properties in two principal direction is investigated. The fatigue behaviour of both composites\udis represented by Wöhler-like diagrams. The damage imparted during fatigue is studied by X-ray\udanalyses. The residual mechanical properties of the fatigued composites after different number of cycles\udare compared in term of stiffness and strength. The post-fatigue quasi-static tensile tests include acoustic\udemission (AE) registration and full-field surface strain mapping (SM) to investigate the damage onset and\uddevelopment. The main conclusions of the experimental work are: the fatigue life is improved in the\uddirection of the structural stitching and is reduced in the orthogonal direction; for the considered cyclic\udstress level the post-fatigue reduction of the mechanical properties is limited by the structural stitching.
机译:本文描述了一项实验研究,涉及结构缝合的多层碳复合材料和未缝合的复合材料的拉伸-拉伸疲劳和准静态/后期疲劳拉伸性能。研究了缝合对两个主要方向上的疲劳寿命和残余疲劳后准静态性能的影响。用Wöhler图表示的两种复合材料\ dis的疲劳行为。通过X射线\ udanalysis研究疲劳过程中产生的损坏。在刚度和强度方面比较了不同循环次数后的疲劳复合材料的残余机械性能。疲劳后准静态拉伸测试包括声学\发射(AE)配准和全场表面应变图(SM),以研究损伤的发生和发展。实验工作的主要结论是:疲劳寿命在结构缝的\方向上得到改善,在正交方向上减小;对于考虑的循环\应力水平,疲劳后机械性能的降低受结构缝合的限制。

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