An irreversible cohesive zone model for interface fatigue crack growth simulation

By K. Roe, T. Siegmund. 2003

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Methods for the prediction of fatigue delamination growth in composites and adhesive bonds: A critical review (2013, methodology): “To model fatigue delamination growth an irreversible stiffness reduction must be added to the CZM formulation [171].”
Simulation of delamination in composites under high-cycle fatigue (2007, background): “Roe and Siegmund [6] describe fatigue crack growth by incorporating a damage evolution equation for cyclic loading.”
A cohesive model for fatigue failure of polymers (2005, methodology): “The fatigue model for interface cracks presented by Roe and Siegmund [17] is based on damage mechanics, where a history-dependent damage parameter gives rise to irreversibility.”
A fatigue degradation law for cohesive interface elements – Development and application to composite materials (2010, background): “Whilst formulations have been developed to account for damage under cyclic loading [20,21,22,23,24], these tend to”
Cohesive zone modeling of dynamic failure in homogeneous and functionally graded materials (2005, background): “, rate-dependent behavior, thermomechanical behavior, damage, fatigue, and viscoelasticity (Knauss and Losi, 1993; Costanzo and Walton, 1997; Lee and Prakash, 1999; Yoon and Allen, 1999; Roe and Siegmund, 2003; Hattiangadi and Siegmund, 2004).”