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: 10.4121/72b67fbb-dd92-41b0-8d16-bf7679df01b0

Tu, Wenjie; Pascoe, John-Alan; René Alderliesten (2024): Mode II Delamination Test Results for Unidirectional and Multidirectional Carbon/Epoxy Composite Laminates Using End-Loaded Split. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/72b67fbb-dd92-41b0-8d16-bf7679df01b0.v1

Dataset

• Aerospace Engineering
• Materials Engineering
• Engineering

Acoustic Emission (AE), Delamination, Digital Image Correlation (DIC), Fracture Resistance, Mode II

CC BY 4.0

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Wenjie Tu , John-Alan Pascoe , René Alderliesten

This dataset collects the test results of Mode II delamination for unidirectional and multidirectional Carbon Fibre Reinforced Polymer (CFRP) composite laminates using the End-Loaded Split (ELS) test configuration. The experiments were performed under the guidance of the test standard ISO 15114 (2014). The composite laminates consist of 16 layers manufactured with unidirectional prepreg. In total, 6 types of specimens with different layups and initial delamination interfaces were tested. The force-displacement responses, delamination length and area measurements, and Acoustic Emission (AE) events are stored in the dataset. The calculated R-curve based on the J-integral method is also provided, as well as the energy dissipation per area increment for determining the total Energy Release Rate (ERR).

• 2024-06-20 first online, published, posted

4TU.ResearchData

7z-zipped files include: DIC image/.tif; datafile/.csv, .xlsx; AE dataset/.pridb, .tridb

• China Scholarship Council

TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures & Materials.