René Alderliesten; Yao, L. (Liaojun) (2017): Mode I fatigue delamination growth in composite laminates with fibre bridging. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/uuid:6da548f6-f801-41b4-8d88-db9ae81f6913

Dataset

• Aerospace Engineering
• Materials Engineering

Bridging effect, Composite laminates, Damage state different, Delamination, dissertation, Fatigue, Fibre bridging, Mode I

4TU General Terms of Use

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by René Alderliesten , L. (Liaojun) Yao

This dataset contains data collected during crack growth experiments at Delft University of Technology, as part of Liaojun Yao's PhD Thesis project (December 2015): Mode I fatigue delamination growth in composite laminates with fibre bridging. It is being made public both to act as supplementary data for publications and the PhD thesis of Liaojun Yao and in order for other researchers to use this data in their own work. The data in this data set was collected in the Structures and Materials Laboratory of the Delft University of Technology - Faculty of Aerospace Engineering, between October 2012 and December 2015.

• 2017-12-08 first online, published, posted

TU Delft

media types: application/pdf, application/vnd.openxmlformats-officedocument.wordprocessingml.document, application/zip, text/plain

• https://doi.org/10.1016/j.compositesa.2014.04.007
• https://doi.org/10.1016/j.compositesa.2014.06.018
• https://doi.org/10.1016/j.compositesa.2015.08.005
• https://doi.org/10.1016/j.compositesb.2017.09.007
• https://doi.org/10.1016/j.compstruct.2015.12.027
• https://doi.org/10.1016/j.compstruct.2017.05.070
• https://doi.org/10.1016/j.ijfatigue.2017.06.004
• https://doi.org/10.4233/uuid:66e210e1-c884-45d6-b9d4-711907680452

TU Delft, Faculty of Aerospace Engineering, Structural Integrity & Composites Group