AbstractIn the present work, the effect of artificial ageing of AA2024-T3 on the tensile mechanical properties and fracture toughness degradation due to corrosion exposure will be investigated. Tensile and fracture toughness specimens were artificially aged to tempers that correspond to Under-Ageing (UA), Peak-Ageing (PA) and Over-Ageing (OA) conditions and then were subsequently exposed to exfoliation corrosion environment. The corrosion exposure time was selected to be the least possible according to the experimental work of Alexopoulos et al. (2016) so as to avoid the formation of large surface pits, trying to simulate the hydrogen embrittlement degradation only. The mechanical test results show that minimum corrosion-induced decrease in...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...
AbstractIn the present work, the effect of artificial ageing of AA2024-T3 on the tensile mechanical ...
The effect of corrosion environment aggressiveness on the tensile mechanical properties degradation ...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
AbstractAl-Cu-Li-Mg based alloys exhibit an excellent combination of low density, high elastic modul...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
The 2024-T351 aluminium alloy is widely used in aircraft industry especially for skin and wings due ...
The 2024-T351 aluminium alloy is widely used in aircraft industry especially for skin and wings due ...
Aluminum alloy 2024-T3 was examined using a range of microscopy techniques at the early stages of co...
In the framework of a collaborative program research with EADS Innovation Works and AIRBUS, this wor...
The age hardening, stress corrosion cracking (SCC) and hydrogen embrittlement (HE) of an Al-Zn-Mg-Cu...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...
AbstractIn the present work, the effect of artificial ageing of AA2024-T3 on the tensile mechanical ...
The effect of corrosion environment aggressiveness on the tensile mechanical properties degradation ...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
AbstractAl-Cu-Li-Mg based alloys exhibit an excellent combination of low density, high elastic modul...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
The 2024-T351 aluminium alloy is widely used in aircraft industry especially for skin and wings due ...
The 2024-T351 aluminium alloy is widely used in aircraft industry especially for skin and wings due ...
Aluminum alloy 2024-T3 was examined using a range of microscopy techniques at the early stages of co...
In the framework of a collaborative program research with EADS Innovation Works and AIRBUS, this wor...
The age hardening, stress corrosion cracking (SCC) and hydrogen embrittlement (HE) of an Al-Zn-Mg-Cu...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...
A multi-scale modeling approach for simulating the tensile behavior of the corroded aluminum alloy 2...