Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches
DOI:
https://doi.org/10.3221/IGF-ESIS.56.16Keywords:
Fatigue, Crack, Composite patch, Load ratioAbstract
This research is based on the study of the fatigue behavior of an aluminum alloy plate with a central crack. The plate is subjected to a tensile loading on its lower and upper parts. Several parameters were highlighted, such as the loading effect with a load ratio R = 0. The effects of the load ratio on both the repaired and not repaired plates, by two composite patches, which are boron/epoxy and graphite/epoxy, were investigated, as well as the effect of the plate material on plate life, comparing different materials
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Copyright (c) 2021 Abdelmadjid Moulgada, Djafar Ait kaci, Mohammed El Sallah Zagane, Sahli Abderrahmane, Rachid Zahi
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