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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-9f41-5ed3b57ba02f
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Dataset

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.

History

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

Publisher

TU Delft

Format

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

Organizations

Delft University of Technology - Faculty of Aerospace Engineering

Contributors

  • Alderliesten, R.C. (RenĂ©) orcid logo
  • Benedictus, R. (Rinze) orcid logo

DATA

Files (1)

  • 3,695,993 bytesMD5:4dfe7d6400222be9dcaa74aa0aa0416cdata.zip