Mode-II total fatigue life model for unidirectional IM7/8552 carbon/epoxy composite laminate
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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:… read more here.
Keywords: im7 8552; carbon epoxy; iic; composite laminate ... See more keywords