2010
DOI: 10.1016/j.ijfatigue.2009.07.011
|View full text |Cite
|
Sign up to set email alerts
|

Crack growth-based fatigue life prediction using an equivalent initial flaw model. Part I: Uniaxial loading

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
47
0

Year Published

2011
2011
2023
2023

Publication Types

Select...
6
2
1

Relationship

1
8

Authors

Journals

citations
Cited by 79 publications
(52 citation statements)
references
References 0 publications
0
47
0
Order By: Relevance
“…2 , the value of CAFL would decrease as the crack size increases because the value of th K remains constant. It is concluded that this condition would subsequently allow slightly lower magnitude stress-range cycles in a spectrum to contribute to the crack growth [5,[8][9].…”
Section: The Concept Of Bi-linear S-n Curvesmentioning
confidence: 99%
“…2 , the value of CAFL would decrease as the crack size increases because the value of th K remains constant. It is concluded that this condition would subsequently allow slightly lower magnitude stress-range cycles in a spectrum to contribute to the crack growth [5,[8][9].…”
Section: The Concept Of Bi-linear S-n Curvesmentioning
confidence: 99%
“…Previous researches showed that cracks initiated at the very beginning of fatigue life and the propagation of small crack were influenced by the inherent microstructure resulting in the abnormal propagation behavior as compared with the long crack behavior [29][30][31][32]. Therefore, the precise measurement of small crack growth rate and the good understanding of small crack growth mechanism are very important in the reliable prediction of the fatigue life of materials [33][34][35][36][37][38][39][40][41][42][43][44][45][46].…”
Section: Fatiguementioning
confidence: 99%
“…Two major components of the crack phase will occur during the fatigue failure process: the initiation, and the propagation of fatigue cracks under cycling load (Xiang et al, 2010;Domínguez Almaraz et al, 2010;Kamal et al, 2012;Zulkifli et al, 2011). The summation of these components in number of cycles is called the fatigue life, and the stress or strain under which the fatigue life occurs is defined as the fatigue strength.…”
Section: Prediction Of Fatigue Lifementioning
confidence: 99%
“…The second method of fatigue life prediction is used to calculate the number of cycles for failure of a component by taking into account the equivalent initial flaw size (EIFS). The basic equation for calculating the EIFS using a short crack has been proposed by several researchers (El Haddad et al, 1979;Xiang et al, 2010). The equation expresses the fatigue endurance by using the fatigue threshold stress intensity factor ΔΚ th , crack length a, and a geometry correction factor Y=0.73, which is crack configuration dependent (Nan et al, 2008):…”
Section: Prediction Of Fatigue Lifementioning
confidence: 99%