In this study, fatigue crack growth rates (FCGR) of 7% nickel steel at room and cryogenic temperatures were evaluated using damage-coupled finite element analysis (FEA). In order to perform the computational fatigue analysis effectively, methods for coupling damage to FEA are introduced and adopted. A hybrid method including the damage-coupled constitutive model and jump-in-cycles procedure was implemented into the ABAQUS user-defined material subroutine. Finally, the represented method was validated by comparing its results with the FCGR test results for 7% nickel steel under room and cryogenic temperatures. In particular, da/dN versus ∆K and the crack length versus the number of cycles were compared
AbstractBackgroundMitigation of primary water stress corrosion cracking (PWSCC) is a significant iss...
Recently, incidents of SCC in Ni-base alloy weld metal of BWR components have been reported. When th...
Crack propagation in full plastic zones is one of the main factors for life assessment of a componen...
The criteria used to prevent failure of wind-tunnel models and support hardware were revised as par...
When defects are detected by in-service inspections of the nuclear power plants in Japan, allowable ...
AbstractCold expansion process is widely used to enhance fatigue life of fastener holes in aircraft ...
In this study, the fatigue crack growth behavior in an aero-engine material under a standard spectru...
In terms of steel alloying elements, generally, nickel is used as an austenite stabilizing element t...
Aircraft engine structures often contain small cracks, which have developed from defects induced dur...
In aerospace industry and other major mechanical industry systems, engineering components that are s...
Damage tolerance concept is widely used in aerospace industry for designing structural components ag...
In the present work, low-cycle fatigue (LCF) test and crack tip opening displacement (CTOD) test wer...
Background: Mitigation of primary water stress corrosion cracking (PWSCC) is a significant issue in ...
The influence of hold time on the crack growth behaviour of a single crystal nickel base superalloy ...
This thesis deals with different aspects of fatigue crack propagation in IN718. The ultimate objecti...
AbstractBackgroundMitigation of primary water stress corrosion cracking (PWSCC) is a significant iss...
Recently, incidents of SCC in Ni-base alloy weld metal of BWR components have been reported. When th...
Crack propagation in full plastic zones is one of the main factors for life assessment of a componen...
The criteria used to prevent failure of wind-tunnel models and support hardware were revised as par...
When defects are detected by in-service inspections of the nuclear power plants in Japan, allowable ...
AbstractCold expansion process is widely used to enhance fatigue life of fastener holes in aircraft ...
In this study, the fatigue crack growth behavior in an aero-engine material under a standard spectru...
In terms of steel alloying elements, generally, nickel is used as an austenite stabilizing element t...
Aircraft engine structures often contain small cracks, which have developed from defects induced dur...
In aerospace industry and other major mechanical industry systems, engineering components that are s...
Damage tolerance concept is widely used in aerospace industry for designing structural components ag...
In the present work, low-cycle fatigue (LCF) test and crack tip opening displacement (CTOD) test wer...
Background: Mitigation of primary water stress corrosion cracking (PWSCC) is a significant issue in ...
The influence of hold time on the crack growth behaviour of a single crystal nickel base superalloy ...
This thesis deals with different aspects of fatigue crack propagation in IN718. The ultimate objecti...
AbstractBackgroundMitigation of primary water stress corrosion cracking (PWSCC) is a significant iss...
Recently, incidents of SCC in Ni-base alloy weld metal of BWR components have been reported. When th...
Crack propagation in full plastic zones is one of the main factors for life assessment of a componen...