Data underlying the article: Unfolding the early fatigue damage process for CFRP cross-ply laminates

doi: 10.4121/12927974.v1
The doi above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
doi: 10.4121/12927974
Datacite citation style:
Xi Li; Kupski, Julian; Teixeira De Freitas, Sofia; Benedictus, Rinze; Zarouchas, Dimitrios (2020): Data underlying the article: Unfolding the early fatigue damage process for CFRP cross-ply laminates. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/12927974.v1
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Dataset
This study investigates the early fatigue damage of cross-ply carbon/epoxy laminates. The aim is to unfold the damage accumulation process, understand the interaction between different damage mechanisms, and quantify their contribution to stiffness degradation. Tension-tension fatigue tests were performed, while edge observation and DIC technique monitored the damage evolution. It was found that different accumulation process and interactive levels between transverse matrix cracks and delamination exist for specimens with similar stiffness degradation. A linear increase of stiffness degradation was observed with the increase of matrix crack density, while the growing trend of stiffness degradation converged with the increase of delamination.
history
  • 2020-09-09 first online, published, posted
publisher
4TU.ResearchData
format
media types: text/xlsx, text/plain
organizations
TU Delft, Faculty of Aerospace Engineering, Structural Integrity & Composites Group

DATA

files (14)