Due to the increasing number of aging aircraft, the inspection and assessment of corrosion and fatigue damage on airframe structures is of major concern [1]. Among the different types of corrosion damage, pitting corrosion is an important factor in triggering widespread fatigue crack initiation and reduced fatigue life. Therefore, the ability to predict surface crack origination from pitting corrosion is necessary for timely maintenance of aging aircraft
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
Localised corrosion plays a dominant role in the failure of components and structures exposed to the...
Pitting corrosion is considered to be one of the principal degradation mechanisms for high-strength ...
Material degradation due to pitting corrosion and fatigue crack initiation from pits may trigger wid...
The presence of corrosion is known to dramatically reduce the fatigue failure resistance of material...
The objective of this PhD Thesis is to further the understanding of the effect of environmentally as...
In this paper we hypothesize that pitting corrosion can alter the location of fatigue failures in ai...
Localized corrosion and corrosion fatigue crack nucleation and growth are recognized as degradation ...
Heterogeneous microstructures of aluminium alloys such as 7075, which are extensively used in aircra...
Corrosion leading to fatigue crack nucleation and crack growth is considered to be among the most si...
Cycles of pressurization and depressurization of the fuselage and gust disturbances are a few of the...
The present thesis describes a programme of research into corrosion pitting in the airframe aluminiu...
A high-strength aluminum alloy, 7075-T6, was studied to quantitatively evaluate chemical pitting eff...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
The objective of this research project is to identify the effects of service exposure on aircraft ma...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
Localised corrosion plays a dominant role in the failure of components and structures exposed to the...
Pitting corrosion is considered to be one of the principal degradation mechanisms for high-strength ...
Material degradation due to pitting corrosion and fatigue crack initiation from pits may trigger wid...
The presence of corrosion is known to dramatically reduce the fatigue failure resistance of material...
The objective of this PhD Thesis is to further the understanding of the effect of environmentally as...
In this paper we hypothesize that pitting corrosion can alter the location of fatigue failures in ai...
Localized corrosion and corrosion fatigue crack nucleation and growth are recognized as degradation ...
Heterogeneous microstructures of aluminium alloys such as 7075, which are extensively used in aircra...
Corrosion leading to fatigue crack nucleation and crack growth is considered to be among the most si...
Cycles of pressurization and depressurization of the fuselage and gust disturbances are a few of the...
The present thesis describes a programme of research into corrosion pitting in the airframe aluminiu...
A high-strength aluminum alloy, 7075-T6, was studied to quantitatively evaluate chemical pitting eff...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
The objective of this research project is to identify the effects of service exposure on aircraft ma...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
Localised corrosion plays a dominant role in the failure of components and structures exposed to the...
Pitting corrosion is considered to be one of the principal degradation mechanisms for high-strength ...