Modeling the effects of prior exfoliation corrosion on fatigue life of aircraft wing skins

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DOIResolve DOI: http://doi.org/10.1016/j.ijfatigue.2003.08.005
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TypeArticle
Proceedings titleInternational Journal of Fatigue
ConferenceInternational Conference on Fatigue Damage of Structural Materials IV, Sept. 22-27, Hyannis, MA
ISSN0142-1123
Volume25
Issue9-11
Pages10591067; # of pages: 9
SubjectAluminum alloys; Corrosion fatigue; Crack propagation; Finite element method; Wings; Exfoliation corrosion; Fatigue testing
Abstract
Publication date
LanguageEnglish
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NPARC number21275958
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Record identifieraa696f41-358e-47a4-9c98-cca698cacecf
Record created2015-08-21
Record modified2016-05-09
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