The motivation for this work was 1) to generate and observe extremely slow average crack growth rates, 2) to determine the coresponding values of stress intensity factors, and 3) to correlate these results with previous experimental findings on crack growth rates
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
This report summarizes the results of an exploratory experimental investigation into the possibility...
Aerospace structures are optimally designed and analyzed to specifically-defined engineering paramet...
A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
The stress intensity factors have been shown to control the rate of propagation of a crack when mate...
Fatigue and fracture testing and analyses were performed on four engineering materials: a low-streng...
The effects of stress ratio (R) and crack opening behavior on fatigue crack growth rates (da/dN) for...
Fatigue crack propagation and fracture toughness characteristics of 7079 aluminum alloys in underage...
The problem of fatigue crack growth acceleration was investigated in crack propagation studies and e...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
This report summarizes the results of an exploratory experimental investigation into the possibility...
Aerospace structures are optimally designed and analyzed to specifically-defined engineering paramet...
A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...
Present investigation involves the study of fatigue crack growth behavior of thermo-mechanically tre...
The main objective of this study is to experimentally determine the fatigue life of the aluminum all...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
The stress intensity factors have been shown to control the rate of propagation of a crack when mate...
Fatigue and fracture testing and analyses were performed on four engineering materials: a low-streng...
The effects of stress ratio (R) and crack opening behavior on fatigue crack growth rates (da/dN) for...
Fatigue crack propagation and fracture toughness characteristics of 7079 aluminum alloys in underage...
The problem of fatigue crack growth acceleration was investigated in crack propagation studies and e...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...
The present study relates to fracture mechanics and its aim is to validate the experimental analysis...