High-temperature corrosion fatigue, a combination of corrosion with a fatigue cycle, is an emerging generic issue affecting power generation and aero gas turbine engines and has the potential to limit component life. Historically, surface treatments, such as shot peening have been used to improve component life and have been optimised for fatigue response. Research into optimisation of shot peening techniques for hot corrosion and high-temperature corrosion fatigue has shown 6–8A 230H 200% coverage to provide overall optimum performance for nickel-based superalloy 720Li based on the limited data within this study. Utilisation of electron backscatter diffraction techniques, in combination with detailed assessment of corrosion products have b...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The nickel based superalloy 720Li is employed in the gas turbine due to its mechanical performance a...
High-temperature corrosion fatigue, a combination of corrosion with a fatigue cycle, is an emerging ...
Surface treatments such as shot peening to inhibit fatigue crack initiation are essential processes ...
Corrosion and fatigue aspects of high temperature turbine components made from Alloy 720Li and RR100...
A corrosive environment can have a detrimental effect on the fatigue life of a material due to a cha...
The effects of type II hot corrosion on the fatigue resistance of turbine blade superalloys is of gr...
As turbine entry temperatures (TET) in modern gas turbine engines continue to increase, Type II hot ...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
Combinations of temperature, stress and hot corrosion may cause environmentally-assisted cracking in...
The development of gas turbines to increase fuel efficiency is resulting in progressively higher ope...
Due to global warming, the demand for more efficient gas turbines has increased. A way to achieve th...
When exposed to a high temperature corrosive environment nickel based superalloys may experience sur...
Due to global warming, the demand for more efficient gas turbines has increased. A way to achieve th...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The nickel based superalloy 720Li is employed in the gas turbine due to its mechanical performance a...
High-temperature corrosion fatigue, a combination of corrosion with a fatigue cycle, is an emerging ...
Surface treatments such as shot peening to inhibit fatigue crack initiation are essential processes ...
Corrosion and fatigue aspects of high temperature turbine components made from Alloy 720Li and RR100...
A corrosive environment can have a detrimental effect on the fatigue life of a material due to a cha...
The effects of type II hot corrosion on the fatigue resistance of turbine blade superalloys is of gr...
As turbine entry temperatures (TET) in modern gas turbine engines continue to increase, Type II hot ...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
Combinations of temperature, stress and hot corrosion may cause environmentally-assisted cracking in...
The development of gas turbines to increase fuel efficiency is resulting in progressively higher ope...
Due to global warming, the demand for more efficient gas turbines has increased. A way to achieve th...
When exposed to a high temperature corrosive environment nickel based superalloys may experience sur...
Due to global warming, the demand for more efficient gas turbines has increased. A way to achieve th...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The goal of this work was to determine effects of shot peening (SP) coverage on the compressive resi...
The nickel based superalloy 720Li is employed in the gas turbine due to its mechanical performance a...