The work presents a summary of previous studies on fatigue crack propagation within various Aluminum alloys. The effective characteristics on crack growth are first highlighted and the influence of surface engineering such as polishing, shot peening and skimming to enhance the failure resistance are discussed. Several different existing developed models for predicting the rate of crack propagation are compared in terms of incorporated effective parameters. Finally numerical and computational analyses as the accurate, fast and cheap methods which have attracted the Engineers’ interest are reviewed and compared with other methods
An analytical method using crack driving force parameter K was developed to account for the single o...
Shot peening is an attractive technique for fatigue enhanced performance of metallic components, bec...
A fatigue crack growth rate study has been carried out on L-72 aluminium alloy plate specimens with ...
Fatigue is a gradual process of local strength reduction. It is a phenomenon of damage accumulation ...
Fatigue crack propagation has been observed for a number of commercial aluminium alloys. Comparable ...
The approach to engineering design based on the flaws propagation assumption applying the principles...
AbstractThe approach to engineering design based on the flaws propagation assumption applying the pr...
AbstractLong and small fatigue crack growth (FCG) studies at various stress ratios have been perform...
The increased use of cast aluminum in structural components requires a deeper understanding of the m...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
This thesis presented about the fatigue life of the material, which is focus on aluminium alloy. The...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
In this paper fatigue crack growth behavior of aeronautical aluminum alloy 2024 T351 was studied. Ef...
Les alliages d'aluminium utilisés dans les structures aéronautiques (fuselage, voilure) sont soumis ...
This paper present a mechanical characteristics on fatigue crack propagation in Aluminium Plate base...
An analytical method using crack driving force parameter K was developed to account for the single o...
Shot peening is an attractive technique for fatigue enhanced performance of metallic components, bec...
A fatigue crack growth rate study has been carried out on L-72 aluminium alloy plate specimens with ...
Fatigue is a gradual process of local strength reduction. It is a phenomenon of damage accumulation ...
Fatigue crack propagation has been observed for a number of commercial aluminium alloys. Comparable ...
The approach to engineering design based on the flaws propagation assumption applying the principles...
AbstractThe approach to engineering design based on the flaws propagation assumption applying the pr...
AbstractLong and small fatigue crack growth (FCG) studies at various stress ratios have been perform...
The increased use of cast aluminum in structural components requires a deeper understanding of the m...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
This thesis presented about the fatigue life of the material, which is focus on aluminium alloy. The...
Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly...
In this paper fatigue crack growth behavior of aeronautical aluminum alloy 2024 T351 was studied. Ef...
Les alliages d'aluminium utilisés dans les structures aéronautiques (fuselage, voilure) sont soumis ...
This paper present a mechanical characteristics on fatigue crack propagation in Aluminium Plate base...
An analytical method using crack driving force parameter K was developed to account for the single o...
Shot peening is an attractive technique for fatigue enhanced performance of metallic components, bec...
A fatigue crack growth rate study has been carried out on L-72 aluminium alloy plate specimens with ...