Probability modelling and statistical analysis of damage in the lower wing skins of two retired B-707 aircraft

Fatigue and Fracture of Engineering Materials and Structures

Volumn 24, Issue 8, 2001, Pages 523-535

  Harlow, D G ^a   Wei, R P ^a  

^a Lehigh University   (United States)

Author keywords

Ageing aircraft; Aluminium alloy; Corrosion fatigue crack growth; Multiple site damage; Pitting corrosion; Probability of occurrence; Tear down data

Indexed keywords

AGING OF MATERIALS; CRACK PROPAGATION; FATIGUE OF MATERIALS; MATHEMATICAL MODELS; METALLOGRAPHY; PITTING; PROBABILITY; STATISTICAL METHODS;

BENDING CYCLES; FATIGUE CRACK NUCLEATION; FLEET LIFE MANAGEMENT; PROBABILITY MODELLING; WING SKIN;

WINGS;

EID: 0035420470     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2001.00402.x     Document Type: Article

References (13)

1. Probability approach for prediction of corrosion and corrosion fatigue life
2. A probability model for the growth of corrosion pits in aluminum alloys induced by constituent particles
3. Probabilities of occurrence and detection of damage in airframe materials
4. Probability modeling of corrosion fatigue crack growth and pitting corrosion
5. A technique for studying the 3-dimensional shape of corrosion pits
6. Particle induced pitting corrosion of aluminum alloys
7. Transition from pitting to fatigue crack growth-modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy
8. The effect of pitting on fatigue life
9. Environmental fatigue crack propagation of aluminum alloys at low stress intensity levels