This paper has compared the electrochemical and tribological behavior of Aluminum-Lithium (Al-Cu-Li) alloys with conventional aluminum alloy. Potentiodynamic polarization test and Scanning Electron Microscopy (SEM) surface analysis were conducted. Results depicted that the 2060 alloy showed a 20% better polarization resistance and corrosion rate than the remaining alloys. Energy Dispersive Spectroscopy (EDS) analysis showed that the corroded surfaces were mostly composed of oxides and chlorides indicating mainly fretting corrosion and environmental-assisted corrosion in all tested alloys. Tribological behavior was evaluated using a ball-on-disk tribometer with load variation (3 N and 5 N). Conventional alloys showed better wear results with low values Coefficient of friction (COF) and almost 50% lesser wear rate than 2060 and 2195. Numerical Modelling based on corrosion results was conducted using Finite Element Analysis (FEA). The simulation of the plate (containing pitting, line cracks, and abrasive grooves) revealed that the abrasive grooves stand out to be the most intense stress risers than the rest within the corroded alloy. These stress risers are detrimental to the integrity of the aircraft. Furthermore, the comparative stress-strain analysis during simulation, showed that conventional alloy produced the highest strain under the same applied environment. There was more than 90% agreement in the experimental and simulated results.
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