High cycle fatigue (HCF) has been of great concern of late in light of the many HCF gas turbine engine failures experienced by the U.S. Air Force. Due to the high frequency, failures occur rapidly when components sustain damage from other sources. Low cycle fatigue (LCF) can initiate cracks that produce such damage. This study investigates the HCF threshold of Ti-6A1-4V when naturally initiated small surface cracks (2a = 25 μm–600 μm) are present. Small surface cracks are initiated in notched specimens using two different LCF loading histories at room temperature and 10 Hz. Direct current potential difference (DCPD) is used to detect crack initiation. Surface crack measurements are made using a scanning electron microscope prior to HCF test...
To assess residual life for those component parts where low cycle fatigue (LCF) design is adopted, e...
Nowadays, several components for aerospace and energy applications (i.e., turbine disks, offshore pi...
During low-cycle fatigue test with smooth bars the number of cycles to initiation is commonly define...
The characterization of critical levels of microstructural damage that can lead to fatigue-crack pro...
All manufacturers of gas turbines, and indeed, of engineering systems, suffer from both managed and ...
The effect of low cycle fatigue (LCF) predamage on the subsequent very high cycle fatigue (VHCF) beh...
The definition of the critical levels of microstructural damage that can lead to the propagation of ...
International audienceFatigue crack growth rates have been experimentally determined for the superal...
The objective of this study was to quantify the effect of fretting fatigue stress histories on fatig...
Nowadays, several components for aerospace and energy applications (i.e., turbine disks, offshore pi...
Within the gas turbine engine, the high transient thermal stresses developed due to variations in po...
Materials in rotating machinery are typically subjected to loading conditions that combine both low ...
Ti-Al alloys such as Ti-6Al-4V belong to a group of materials that show tremendous potential in airc...
Aircraft turbine engines, especially military engines, experience variable amplitude loading (missio...
To assess residual life for those component parts where low cycle fatigue (LCF) design is adopted, e...
Nowadays, several components for aerospace and energy applications (i.e., turbine disks, offshore pi...
During low-cycle fatigue test with smooth bars the number of cycles to initiation is commonly define...
The characterization of critical levels of microstructural damage that can lead to fatigue-crack pro...
All manufacturers of gas turbines, and indeed, of engineering systems, suffer from both managed and ...
The effect of low cycle fatigue (LCF) predamage on the subsequent very high cycle fatigue (VHCF) beh...
The definition of the critical levels of microstructural damage that can lead to the propagation of ...
International audienceFatigue crack growth rates have been experimentally determined for the superal...
The objective of this study was to quantify the effect of fretting fatigue stress histories on fatig...
Nowadays, several components for aerospace and energy applications (i.e., turbine disks, offshore pi...
Within the gas turbine engine, the high transient thermal stresses developed due to variations in po...
Materials in rotating machinery are typically subjected to loading conditions that combine both low ...
Ti-Al alloys such as Ti-6Al-4V belong to a group of materials that show tremendous potential in airc...
Aircraft turbine engines, especially military engines, experience variable amplitude loading (missio...
To assess residual life for those component parts where low cycle fatigue (LCF) design is adopted, e...
Nowadays, several components for aerospace and energy applications (i.e., turbine disks, offshore pi...
During low-cycle fatigue test with smooth bars the number of cycles to initiation is commonly define...