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
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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
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Delft University of Technology - Faculty of Aerospace Engineering
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  • Benedictus, R. (Rinze) orcid logo


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