Residual life predictions of corroded fuselage lap joints

International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 349-356

  Bellinger, N C ^a   Komorowski, J P ^a   Benak, T J ^a  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

Corrosion; Fatigue; Finite element analysis; Life prediction

Indexed keywords

CRACK PROPAGATION; FINITE ELEMENT METHOD; FUSELAGES; JOINTS (STRUCTURAL COMPONENTS); STRESS CONCENTRATION;

EQUIVALENT CORROSION DAMAGE (ECD);

CORROSION FATIGUE;

EID: 0035207006     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00148-7     Document Type: Article

References (7)

1. Case studies for life assessments with age degradation
2. Determining the initial quality state for materials
3. The effects of corrosion on the durability and damage tolerance characteristics of longitudinal fuselage skin splices
4. An experimental study of corrosion/fatigue interaction in the development of multiple site damage in longitudinal fuselage skin splices
5. Experimental study of the effects of corrosion on the fatigue durability and crack growth characteristics of longitudinal fuselage skin splices
6. Modelling of pillowing due to corrosion in fuselage lap joints
7. Corrosion pillowing stresses in fuselage lap joints