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Table · dataset · 2016

Effect of Bondline Thickness on Fatigue Crack Growth in FM94

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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.

Description

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.

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Catalogue records · 2

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Mechanical engineering

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