Mixed-mode delamination growth in carbon-fibre composite laminates under cyclic loading

By Norbert Blanco, E. Gamstedt, Leif E. Asp, Josep Costa. 2004

168 citations recorded by the source corpus.

Subfields: Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/15aeda0fb379fc4513d6f5f3e9c0a460a92de2d2

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Mechanics of Materials

1. S. Hallett
2. Pedro P. Camanho
3. C. Dávila
4. Paul W. Harper
5. A. Turón
6. Josep Costa
7. J. Pascoe
8. Rinze Benedictus

Citations in the corpus

• 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, background): “In this paper, the dependence of the parameters C and m on the mode ratio is assumed to be of the form [34]:”
• Methods for the prediction of fatigue delamination growth in composites and adhesive bonds: A critical review (2013, methodology): “[97] (see equations 31 and 32) is used to predict the delamination growth rate.”