Effect of Bondline Thickness on Fatigue Crack Growth in FM94
Datacite citation style:
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-9f41-5ed3b57ba02fOther citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
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
formatmedia types: application/octet-stream, application/pdf, application/zip, text/csv, text/plain
organizationsDelft University of Technology - Faculty of Aerospace Engineering