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Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches
Author(s) -
Abdelmadjid Moulgada,
Djafar Ait Kaci,
Mohammed El Sallah Zagane,
Sahli Abderrahmane,
Zahi Rachid
Publication year - 2021
Publication title -
frattura ed integrità strutturale
Language(s) - English
Resource type - Journals
ISSN - 1971-8993
DOI - 10.3221/igf-esis.56.16
Subject(s) - materials science , epoxy , composite material , composite plate , ultimate tensile strength , composite number , graphite , structural engineering , aluminium , boron , alloy , engineering , chemistry , organic chemistry
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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