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Published in 2017 at "International Journal of Fatigue"
DOI: 10.1016/j.ijfatigue.2016.09.014
Abstract: Abstract This paper presents a method of developing Total Fatigue Life Model (TFLM) for a unidirectional composite laminate with a delamination subjected to mode-II stress state. The model includes three domains of delamination growth rates:…
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Keywords:
im7 8552;
carbon epoxy;
iic;
composite laminate ... See more keywords