It has been shown that decrease of the fatigue life of aluminium alloys treated with anodization can be explained by the degradation of surface condition due to pickling. In order to predict fatigue life of anodized aluminium alloys, a multi-site crack growth model is developed by considering the pickling pits sites as initial flaws from which fatigue cracks develop. A map of the pickled surface is built from topography measurement with a contact profilometer. Then the pits are detected and their sizes are defined (depth, length and width). At the beginning of the calculation, a short crack growth law is used for crack having depths less than grain size. Then Paris long crack growth law is used. The coalescence of cracks is considered when ...
International audienceFatigue crack growth period in cylinder heads of A356-T7 casting alloy has bee...
While it is well known that fatigue crack growth in metals that display confined slip, such as high ...
Anodized aluminum alloys are widely used in aircraft construction because of their mechanical proper...
AbstractIt has been shown that decrease of the fatigue life of aluminium alloys treated with anodiza...
10th International Fatigue Conference, Prague, CZECH REPUBLIC, JUN 06‐11, 2010International audience...
AbstractFatigue investigation on 7050-T7651 chromic acid anodized aluminium alloy has been realized ...
International audienceThe objective of this study is to predict fatigue life of anodized 7050 alumin...
The present study investigates the influence of anodizing process on fatigue life of aluminium alloy...
The fatigue of materials and structures is a phenomenon in which surface condition plays an importan...
In order to investigate the coupled effects of machining and anodizing processes on fatigue life of ...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
AbstractIn order to investigate the coupled effects of machining and anodizing processes on fatigue ...
The fatigue crack growth behaviour of long and short cracks in two aluminium alloys used in the airc...
It has been recognised that the interaction, coalescence and crack shape development of multiple sm...
The work presents a summary of previous studies on fatigue crack propagation within various Aluminum...
International audienceFatigue crack growth period in cylinder heads of A356-T7 casting alloy has bee...
While it is well known that fatigue crack growth in metals that display confined slip, such as high ...
Anodized aluminum alloys are widely used in aircraft construction because of their mechanical proper...
AbstractIt has been shown that decrease of the fatigue life of aluminium alloys treated with anodiza...
10th International Fatigue Conference, Prague, CZECH REPUBLIC, JUN 06‐11, 2010International audience...
AbstractFatigue investigation on 7050-T7651 chromic acid anodized aluminium alloy has been realized ...
International audienceThe objective of this study is to predict fatigue life of anodized 7050 alumin...
The present study investigates the influence of anodizing process on fatigue life of aluminium alloy...
The fatigue of materials and structures is a phenomenon in which surface condition plays an importan...
In order to investigate the coupled effects of machining and anodizing processes on fatigue life of ...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
AbstractIn order to investigate the coupled effects of machining and anodizing processes on fatigue ...
The fatigue crack growth behaviour of long and short cracks in two aluminium alloys used in the airc...
It has been recognised that the interaction, coalescence and crack shape development of multiple sm...
The work presents a summary of previous studies on fatigue crack propagation within various Aluminum...
International audienceFatigue crack growth period in cylinder heads of A356-T7 casting alloy has bee...
While it is well known that fatigue crack growth in metals that display confined slip, such as high ...
Anodized aluminum alloys are widely used in aircraft construction because of their mechanical proper...