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Effect of Bondline Thickness on Fatigue Crack Growth in FM94

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posted on 08.06.2016 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.

History

Contributors

Alderliesten, R.C. (René) [orcid:0000-0003-1882-5396]; Benedictus, R. (Rinze) [orcid:0000-0003-3219-3161]; Delft University of Technology - Faculty of Aerospace Engineering

Publisher

TU Delft

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

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