Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches

Authors

  • Abdelmadjid Moulgada LRI, Department of mechanical Engineering, University of Ibn Khaldoun Tiaret, City Zaaroura BP 78 14000 Tiaret, Algeria
  • Djafar Ait kaci Department of Mechanical Engineering, University of Djillali Liabes Sidi Bel Abbes, Algeria
  • Mohammed El Sallah Zagane Department of Mechanical Engineering, University of Ibn Khaldoun Tiaret, City Zaaroura BP 78 14000 Tiaret, Algeria
  • Sahli Abderrahmane
  • Rachid Zahi Department of Mechanical Engineering, University of Ahmed Zabana Relizane 48000, Algeria

DOI:

https://doi.org/10.3221/IGF-ESIS.56.16

Keywords:

Fatigue, Crack, Composite patch, Load ratio

Abstract

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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Published

28-03-2021

How to Cite

Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches. (2021). Frattura Ed Integrità Strutturale, 15(56), 195-202. https://doi.org/10.3221/IGF-ESIS.56.16