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

Author(s):




Medium: journal article
Language(s): English
Published in: Frattura ed Integrità Strutturale, , n. 56, v. 15
Page(s): 195-202
DOI: 10.3221/igf-esis.56.16
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

Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.3221/igf-esis.56.16.
  • About this
    data sheet
  • Reference-ID
    10603707
  • Published on:
    17/04/2021
  • Last updated on:
    17/04/2021
 
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