Add to ORKGA fatigue data consolidation model that incorporates recent advances in life prediction methodology was developed. A combined analytic and experimental study of fatigue of notched 2024-T3 aluminum alloy under constant amplitude loading was carried out. Because few systematic and complete data sets for 2024-T3 were available in the program generated data for fatigue crack initiation and separation failure for both zero and nonzero mean stresses. Consolidations of these data are presented
The three main stages of fatigue life (accommodation, crack initiation and crack growth) are briefly...
Despite its importance in many engineering applications, fatigue life assessment is still not well u...
This paper evaluates the methodology for, and effectiveness of, common equivalent stress- and strain...
Analytical methods have been developed for consolidation of fatigue, fatigue-crack propagation, and ...
Fatigue crack growth tests were performed on center crack panels and radial crack hole samples. The ...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
Constitutive and life prediction models are developed and verified for materials typically used in h...
Stress-number of cycles characteristics determined for notched aluminum alloy, 7075-T6, specimens, b...
In this investigation, fatigue criterion was established to predict crack-initiation at the tip of a...
A brief overview of the status of the fatigue and fracture programs is given. The programs involve t...
Fully reversed uniaxial strain controlled fatigue tests were performed on smooth cylindrical specime...
AbstractThis paper investigates fatigue behavior under variable amplitude multiaxial service loading...
Fatigue crack growth tests were conducted on 0.09 inch thick, 3.0 inch wide middle-crack tension spe...
This paper presents a study of crack growth behaviour in aluminium alloys 2324- T39 and 7050-T7451 s...
A large number of axially loaded specimens of 2024-T3 aluminum sheet alloy were fatigued to failure ...
The three main stages of fatigue life (accommodation, crack initiation and crack growth) are briefly...
Despite its importance in many engineering applications, fatigue life assessment is still not well u...
This paper evaluates the methodology for, and effectiveness of, common equivalent stress- and strain...
Analytical methods have been developed for consolidation of fatigue, fatigue-crack propagation, and ...
Fatigue crack growth tests were performed on center crack panels and radial crack hole samples. The ...
The fracture toughness and fatigue flaw growth characteristics of 2024-T861 and 2124-T851 aluminum w...
Constitutive and life prediction models are developed and verified for materials typically used in h...
Stress-number of cycles characteristics determined for notched aluminum alloy, 7075-T6, specimens, b...
In this investigation, fatigue criterion was established to predict crack-initiation at the tip of a...
A brief overview of the status of the fatigue and fracture programs is given. The programs involve t...
Fully reversed uniaxial strain controlled fatigue tests were performed on smooth cylindrical specime...
AbstractThis paper investigates fatigue behavior under variable amplitude multiaxial service loading...
Fatigue crack growth tests were conducted on 0.09 inch thick, 3.0 inch wide middle-crack tension spe...
This paper presents a study of crack growth behaviour in aluminium alloys 2324- T39 and 7050-T7451 s...
A large number of axially loaded specimens of 2024-T3 aluminum sheet alloy were fatigued to failure ...
The three main stages of fatigue life (accommodation, crack initiation and crack growth) are briefly...
Despite its importance in many engineering applications, fatigue life assessment is still not well u...
This paper evaluates the methodology for, and effectiveness of, common equivalent stress- and strain...