Small-crack growth and fatigue-life prediction of corroded open-hole specimens

11th International Conference on Fracture 2005, ICF11

Volumn 1, Issue , 2005, Pages 162-167

  Newman Jr , J C ^a   Abbott, W ^b  

^a MISSISSIPPI STATE UNIVERSITY   (United States)

^b BATTELLE MEMORIAL INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

2024-T3 ALUMINUM ALLOY; BENDING SPECIMENS; CANTILEVER BENDING; CORROSION PITS; CRACK-TIP CONSTRAINTS; DRILLED HOLES; FATIGUE BEHAVIOR; FATIGUE LIFE PREDICTION; INCLUSION PARTICLES; MICRO-STRUCTURAL; NOTCHED SPECIMENS; OPEN HOLES; OPEN-HOLE SPECIMENS; STRESS LEVELS; STRESS RATIO; WEATHER CONDITIONS;

AMPLITUDE MODULATION; CORROSION; CRACK PROPAGATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE; NANOCANTILEVERS; PLASTICITY; STRESS ANALYSIS;

CRACKS;

EID: 84869828459     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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2. Minakawa K and McEvily AJ. (1981) On near-threshold fatigue crack growth in steels and aluminum alloys. Proc Int Conf Fatigue Thresholds, 2:373-390.
3. Newman Jr JC. (1983) A nonlinear fracture mechanics approach to the growth of small cracks. AGARD CP 328:6.1-6.26.
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5. Short-crack growth behaviour in various aircraft materials. (1990) Edwards PR and Newman Jr JC (eds.), AGARD R-767.
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12. Dubensky RG. (1971) Fatigue crack propagation in 2024-T3 and 7075-T6 aluminum aAlloys at high stress. NASA CR 1732.
13. Landers CB and Hardrath HF. (1956) Results of axial-load fatigue tests on electropolished 2024-T3 and 7075-T6 aluminum alloy sheet specimens with central holes. NACA TN 3631.
14. Newman Jr JC. (1976) Fracture analysis of various cracked configurations in sheet and plate materials. ASTM STP 605:104-123.
15. Newman Jr JC. (1992) Effects of constraint on crack growth under aircraft spectrum loading. Fatigue of Aircraft Materials, Beukers et al (eds), Delft University Press, 83-109.
16. Newman Jr JC. (1994) Review of modeling small-crack behavior and fatigue-life prediction for aluminum alloys. Fat Frac Engng Mat Struct. 17:429-439.