Abstract
The project aims at achieving the Failure Analysis mixed riveted joints of hybrid laminates Glare with plates of aeronautical monolithic alloy 2024- T3 (Glare / alloy - Al) subjected to mechanical fatigue loading after the application, and combined, hygrothermal ageing (EH) and thermal cycles of large amplitude (CT), in both their chronological sequences, namely EH+CT and CT+EH. The chara…