Add to ORKGAluminum-lithium alloys are candidate materials for many aerospace applications because of their high specific strength and elastic modulus. These alloys have several unique characteristics such as excellent fatigue crack growth resistance when compared with that of the conventional 2000 and 7000 series alloys. In this study, fatigue crack propagation behavior has been examined in a commercial thin plate of Al-Li-Cu-Mg alloy (8090), with specific emphasis at the fatigue threshold. The results are compared with those of the traditional Al-Cu-Mg alloy (2024). Fatigue crack closure is used to explain the different behavior of the compared alloys
Micromechanisms influencing the propagation of long (>10 mm) fatigue cracks in aluminum-lithium allo...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
The fatigue crack propagation behaviour of the Al-Li alloy 8090 was evaluated on 25mm plate material...
Characteristics of fatigue-crack propagation behavior are reviewed for recently developed commercial...
This document describes fatigue crack growth properties of Lital-A aluminium -lithium alloy in tests...
This document describes fatigue crack growth properties of Lital-A aluminium -lithium alloy in tests...
The fatigue crack propagation behaviour of the AI-Li alloy 8090 was evaluated on 25mm plate material...
This work was undertaken as a comparative study on fatigue properties of a typical third generation ...
This report presents the experimental result on fatigue13; crack progation(FCP) of 2mm thick Al-Li a...
This report presents the experimental result on fatigue13; crack progation(FCP) of 2mm thick Al-Li a...
Aluminum-lithium alloys exhibit similar environmental fatigue crack growth characteristics compared ...
Micromechanisms influencing the propagation of long (>10 mm) fatigue cracks in aluminum-lithium allo...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
Aluminum-lithium alloys are candidate materials for many aerospace applications because of their hig...
The fatigue crack propagation behaviour of the Al-Li alloy 8090 was evaluated on 25mm plate material...
Characteristics of fatigue-crack propagation behavior are reviewed for recently developed commercial...
This document describes fatigue crack growth properties of Lital-A aluminium -lithium alloy in tests...
This document describes fatigue crack growth properties of Lital-A aluminium -lithium alloy in tests...
The fatigue crack propagation behaviour of the AI-Li alloy 8090 was evaluated on 25mm plate material...
This work was undertaken as a comparative study on fatigue properties of a typical third generation ...
This report presents the experimental result on fatigue13; crack progation(FCP) of 2mm thick Al-Li a...
This report presents the experimental result on fatigue13; crack progation(FCP) of 2mm thick Al-Li a...
Aluminum-lithium alloys exhibit similar environmental fatigue crack growth characteristics compared ...
Micromechanisms influencing the propagation of long (>10 mm) fatigue cracks in aluminum-lithium allo...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...
This report presents the results of a fatigue and fracture data generation program to evaluate an al...