Fatigue behavior and damage analysis by the acoustic emission technique of cross-ply laminates under tensile loading

Purpose The purpose of this paper is to study the mechanical behavior in fatigue tensile mode of different cross-ply laminates constituted of unidirectional carbon fibers, hybrid fibers and glass fibers in an epoxy matrix; and to identify and characterize the local damage in the laminated materials...

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Bibliographic Details
Published in:Multidiscipline modeling in materials and structures Vol. 13; no. 2; pp. 150 - 164
Main Authors: Ben Ammar, Imen, El Mahi, Abderrahim, Karra, Chafik, El Guerjouma, Rachid, Haddar, Mohamed
Format: Journal Article
Language:English
Published: Bingley Emerald Publishing Limited 14-08-2017
Emerald Group Publishing Limited
Emerald
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Summary:Purpose The purpose of this paper is to study the mechanical behavior in fatigue tensile mode of different cross-ply laminates constituted of unidirectional carbon fibers, hybrid fibers and glass fibers in an epoxy matrix; and to identify and characterize the local damage in the laminated materials with the use of the acoustic emission (AE) technique. Design/methodology/approach The tests in the fatigue mode permitted the determination of the effect of the stacking sequences, thickness of 90° oriented layers and reinforcement types on the fatigue mechanical behavior of the laminated materials. The damage investigation in those materials is reached with the analysis of AE signals collected from fatigue tensile tests. Findings The results show the effects of reinforcement type, stacking sequences and thicknesses ratio of 90° and 0° layers on the mechanical behavior. A cluster analysis of AE data is achieved and the resulting clusters are correlated with the damage mechanism of specimens under loading tests. Originality/value The analysis of AE signals collected from tensile tests of the fatigue failure load allows the damage investigation in different types of cross-ply laminates which are differentiated by the reinforcement type, stacking sequences and thicknesses ratio of 90° and 0° layers.
ISSN:1573-6105
1573-6113
DOI:10.1108/MMMS-08-2016-0036