A high-strength aluminum alloy, 7075-T6, was studied to quantitatively evaluate chemical pitting effects of its corrosion fatigue life. The study focused on pit nucleation, pit growth, and fatigue crack nucleation. Pitting corrosion fatigue experiments were conducted in 3.5 percent NaCl aqueous solution under constant amplitude sinusoidal loading at two frequencies, 5 and 20 Hz. Smooth and unnotched specimens were used in this investigation. A video recording system was developed to allow in situ observation of the surface changes of the specimens during testing. The results indicated that pitting corrosion considerably reduces the fatigue strength by accelerating fatigue crack nucleation. A metallographic examination was conducted on the s...
dissertationIt is well known that corrosion and simultaneous cyclic loading have a detrimental impac...
The present study investigates the influence of anodizing process on fatigue life of aluminium alloy...
Aluminum alloy 7050-T451 is generally used in aerospace structure due to its high strength-to-weight...
Localized corrosion and corrosion fatigue crack nucleation and growth are recognized as degradation ...
The presence of corrosion is known to dramatically reduce the fatigue failure resistance of material...
Research on fatigue crack formation from two types corrosion pits tangent to a circular hole in a 70...
Corrosion leading to fatigue crack nucleation and crack growth is considered to be among the most si...
Corrosion fatigue crack initiation in aluminum alloys can have significant effects on part life. An ...
The design and development of high performance structural materials requires a thorough understandin...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
abstract: 7XXX Aluminum alloys have high strength to weight ratio and low cost. They are used in man...
Corrosion fatigue (CF) is defined as the sequential stages of metal damage that evolve with accumula...
Fatigue corrosion phenomenon is a form of degradation that is because of the combined occurrence of ...
Corrosion has always been a concern in the manufacturing industry as it shortens the lifespan of a m...
[Abstract] This work studies the influence of the saline atmospheric corrosion on the fatigue streng...
dissertationIt is well known that corrosion and simultaneous cyclic loading have a detrimental impac...
The present study investigates the influence of anodizing process on fatigue life of aluminium alloy...
Aluminum alloy 7050-T451 is generally used in aerospace structure due to its high strength-to-weight...
Localized corrosion and corrosion fatigue crack nucleation and growth are recognized as degradation ...
The presence of corrosion is known to dramatically reduce the fatigue failure resistance of material...
Research on fatigue crack formation from two types corrosion pits tangent to a circular hole in a 70...
Corrosion leading to fatigue crack nucleation and crack growth is considered to be among the most si...
Corrosion fatigue crack initiation in aluminum alloys can have significant effects on part life. An ...
The design and development of high performance structural materials requires a thorough understandin...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
abstract: 7XXX Aluminum alloys have high strength to weight ratio and low cost. They are used in man...
Corrosion fatigue (CF) is defined as the sequential stages of metal damage that evolve with accumula...
Fatigue corrosion phenomenon is a form of degradation that is because of the combined occurrence of ...
Corrosion has always been a concern in the manufacturing industry as it shortens the lifespan of a m...
[Abstract] This work studies the influence of the saline atmospheric corrosion on the fatigue streng...
dissertationIt is well known that corrosion and simultaneous cyclic loading have a detrimental impac...
The present study investigates the influence of anodizing process on fatigue life of aluminium alloy...
Aluminum alloy 7050-T451 is generally used in aerospace structure due to its high strength-to-weight...