This work investigates experimentally and theoretically the local crack tip stress and strain fields, and plasticity-induced crack closure acting on the crack flanks behind the crack tip, in fine-grained aluminium alloy 5091 (Al-Mg-Li-C-O) compact tension fatigued specimens. Compressive residual stresses ahead of the crack tip and plasticity-induced crack closure are often attributed to be the two main mechanisms responsible for crack growth retardation. Specimens investigated were prepared: with constant amplitude fatigue; with constant amplitude fatigue followed by a single overload; and finally with constant amplitude fatigue followed by a single overload followed by further constant amplitude fatigue. Experimental crack tip strain (and ...
In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plast...
In quantifying the fatigue crack growth behaviour of a material, it is possible to identify intrinsi...
Abrupt increase in the maximum load during fatigue cycling modifies the deformation conditions at th...
There have been many theoretical studies to predict the stress fields around the tip of a growing fa...
The mechanisms responsible for the transient retardation or acceleration of fatigue crack growth sub...
The mechanisms responsible for the transient retardation or acceleration of fatigue crack growth sub...
A modified elastic-plastic finite element program was used to simulate fatigue crack growth and clos...
This paper describes a new methodology for characterising the plastic zoneahead of a fatigue crack. ...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
Crack closure effects during fatigue crack growth have been studied by many researchers with the fin...
In this study effect of strain hardening on crack closure has been examined with the help of experim...
In this study effect of strain hardening on crack closure has been examined with the help of finite ...
Crack closure influences fatigue crack growth rate and must be included in the design of components....
The evolution of crack-tip strain fields in a thin (plane stress) compact tension sample following a...
The paper analyses previously reported work, which uses digital image correlation to measure fatigue...
In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plast...
In quantifying the fatigue crack growth behaviour of a material, it is possible to identify intrinsi...
Abrupt increase in the maximum load during fatigue cycling modifies the deformation conditions at th...
There have been many theoretical studies to predict the stress fields around the tip of a growing fa...
The mechanisms responsible for the transient retardation or acceleration of fatigue crack growth sub...
The mechanisms responsible for the transient retardation or acceleration of fatigue crack growth sub...
A modified elastic-plastic finite element program was used to simulate fatigue crack growth and clos...
This paper describes a new methodology for characterising the plastic zoneahead of a fatigue crack. ...
The mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were ...
Crack closure effects during fatigue crack growth have been studied by many researchers with the fin...
In this study effect of strain hardening on crack closure has been examined with the help of experim...
In this study effect of strain hardening on crack closure has been examined with the help of finite ...
Crack closure influences fatigue crack growth rate and must be included in the design of components....
The evolution of crack-tip strain fields in a thin (plane stress) compact tension sample following a...
The paper analyses previously reported work, which uses digital image correlation to measure fatigue...
In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plast...
In quantifying the fatigue crack growth behaviour of a material, it is possible to identify intrinsi...
Abrupt increase in the maximum load during fatigue cycling modifies the deformation conditions at th...