Pascoe, John-Alan; Al Amery, A. M.K. H. (Ali); Zavatta, N. (Nicola) (2016): Effect of Bondline Thickness on Fatigue Crack Growth in FM94. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/uuid:1495c951-33e2-43ab-9f41-5ed3b57ba02f

Dataset

• Aerospace Engineering

Adhesive bond, Aerospace engineering, Bonded joint, dissertation, Double cantilever beam, Double Cantilever Beam (DCB), Epoxy, Fatigue crack growth, FM94, Glass-fibre reinforced polymer, Glass-Fibre Reinforced Polymer (GFRP), Mode I

4TU General Terms of Use

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

by John-Alan Pascoe , A. M.K. H. (Ali) Al Amery, N. (Nicola) Zavatta

Fatigue crack growth experiments on aluminium-2024-T3 / FM94 epoxy / aluminium-2024-T3 bonded joint specimens in the double cantilever beam (DCB) configuration. Different adhesive thicknesses were tested. Also contains data from fatigue crack growth experiments conducted on S2-glass / FM94 epoxy composite laminates again in the DCB configuration. Different fibre orientations were tested. Included data are raw data: crack length, force, and displacement measurements, as well as processed data such as strain energy release rates and energy dissipation per cycle.

• 2016-06-08 first online, published, posted

TU Delft

media types: application/octet-stream, application/pdf, application/zip, text/csv, text/plain

• https://doi.org/10.1016/j.engfracmech.2020.106959
• http://amslaurea.unibo.it/9713/1/zavatta_nicola_tesi.pdf.pdf
• https://doi.org/10.4233/uuid:ebbf552a-ce98-4ab6-b9cc-0b939e12ba8b
• https://doi.org/10.4121/uuid:4400f37c-7168-4275-a778-09b237bd34c6

Delft University of Technology - Faculty of Aerospace Engineering

• Alderliesten, R.C. (René)
• Benedictus, R. (Rinze)