Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches
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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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2014 ◽
Vol 63
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pp. 162-170
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2018 ◽
Vol 18
(5)
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pp. 1159-1167
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1968 ◽
Vol 1
(2)
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pp. 259-262
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2021 ◽
Vol 09
(04)
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pp. 11-18
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