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Aircraft structures are often treated with corrosion protective compounds. However, these compounds can alter the structural fatigue life. This study continues the investigation into how Corrosion Inhibiting Compounds (CICs) change mechanical fatigue behaviour.
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This page is a summary of: Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds, Journal of Aircraft, February 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037639.
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