Delamination Growth and Thresholds in a Carbon/Epoxy Composite under Fatigue Loading

By E. Armanios, R. Bucinell, Dw Wilson, L. Asp, A. Sjögren, E. Greenhalgh. 2001

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Misinterpreting the Results: How Similitude can Improve our Understanding of Fatigue Delamination Growth (2011, background): “If we consider this simple DCB example and determine what applied load cycles would produce the same ΔG for different R-ratios (considering crack and specimen geometry is kept constant), we can easily see the loss in similitude when using ΔG = Gmax – Gmin.”
A fatigue degradation law for cohesive interface elements – Development and application to composite materials (2010, methodology): “Pinho et al [6] found a value of α =1.21 to give a best fit to experimental data for T300/913 carbonepoxy prepreg and for data from Juntti et al. [34] for HTA/6376C carbon epoxy pre-preg a value of α =1.23 is appropriate.”
Simulation of delamination in composites under high-cycle fatigue (2007, methodology): “060 kJ/m [38].”