Stress corrosion and corrosion fatigue represent major threats to the structural integrity of aircraft structures and have been extensively investigated [1–3]. Among others, Pantelakis et al. [4] observed dramatic degradation of toughness and ductility of Al-Li alloys 2091 and 8090, as well as conventional 2024 alloy in several types of accelerated corrosion tests. Based on a comparison of mechanica
Heterogeneous microstructures of aluminium alloys such as 7075, which are extensively used in aircra...
AbstractThe present work investigates the corrosion resistance of the innovative Al-Cu-Li (2198) alu...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
In the framework of a collaborative program research with EADS Innovation Works and AIRBUS, this wor...
A brief overview of aircraft aluminum alloys, along with a discussion of their susceptibility to cor...
The objective of the present work were to study the influence of exfoliation corrosion (EFC) of 2024...
The embrittlement of high strength landing gear steels is occurred due to hydrogen absorption during...
The effect of corrosion environment aggressiveness on the tensile mechanical properties degradation ...
The 2024 and 7050 aluminium alloys used as aircraft components were subjected to laboratory corrosio...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
The study investigates the effect of prior corrosive exposure on crack growth resistance behaviour o...
The concept of the Fatigue Damage Map (FDM) is implemented to quantify the effects of exfoliation co...
The present paper focuses on the observed corrosion-induced embrittlement of alloy 2024 and tries to...
Heterogeneous microstructures of aluminium alloys such as 7075, which are extensively used in aircra...
AbstractThe present work investigates the corrosion resistance of the innovative Al-Cu-Li (2198) alu...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
Corrosion is a major concern to the structural integrity of aging aircraft structures. The effect of...
In the framework of a collaborative program research with EADS Innovation Works and AIRBUS, this wor...
A brief overview of aircraft aluminum alloys, along with a discussion of their susceptibility to cor...
The objective of the present work were to study the influence of exfoliation corrosion (EFC) of 2024...
The embrittlement of high strength landing gear steels is occurred due to hydrogen absorption during...
The effect of corrosion environment aggressiveness on the tensile mechanical properties degradation ...
The 2024 and 7050 aluminium alloys used as aircraft components were subjected to laboratory corrosio...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
The study investigates the effect of prior corrosive exposure on crack growth resistance behaviour o...
The concept of the Fatigue Damage Map (FDM) is implemented to quantify the effects of exfoliation co...
The present paper focuses on the observed corrosion-induced embrittlement of alloy 2024 and tries to...
Heterogeneous microstructures of aluminium alloys such as 7075, which are extensively used in aircra...
AbstractThe present work investigates the corrosion resistance of the innovative Al-Cu-Li (2198) alu...
Corrosion damage accumulation represents a major threat for the structuralintegrity of metallic airc...