A model of initial flaw sizes in aluminum alloys

International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 79-86

  DeBartolo, E A ^a   Hillberry, B M ^b  

^a Kate Gleason College of Engineering   (United States)

^b PURDUE UNIVERSITY   (United States)

Author keywords

Aluminum; Fatigue crack formation; Nucleation sites

Indexed keywords

AIRCRAFT; ALUMINUM ALLOYS; CRACK INITIATION; FATIGUE OF MATERIALS; NUCLEATION; PARTICLE SIZE ANALYSIS;

CHOLESKI DECOMPOSITION;

CRACKS;

EID: 0035214473     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00122-0     Document Type: Article

References (18)

1. Fatigue life prediction from inclusion initiated cracks
2. Probabilistic method for predicting the variability in fatigue behavior of 7075-T6 aluminum
3. Metallography of fatigue crack initiation in and overaged high-strength aluminum alloy
4. Microstructural effects on the small fatigue crack behaviour of an aluminum alloy plate
5. Effects of constituent particle clusters on fatigue behavior of 2024-T3 aluminum alloy
6. Characterization of fatigue crack nucleation sites in 2024-T3 aluminum
7. The effect of grain size on the fatigue of commercially pure aluminum
8. Elastic-plastic analysis of small defects - Voids and inclusions
9. A finite-element study of the notch effect at surface inclusions
10. A FEM study of driving forces of short cracks at inclusions in hard steels
11. A finite element study of short cracks with different inclusion types under rolling contact fatigue load
12. Effect of prior corrosion on fatigue performance of toughness improved fuselage skin sheet alloy 2524-T3