Residual life predictions of corroded fuselage lap joints

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DOIResolve DOI: http://doi.org/10.1016/S0142-1123(01)00148-7
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TypeArticle
Journal titleInternational Journal of Fatigue
ISSN0142-1123
Volume23
IssueSUPPL. 1
PagesS349S356
SubjectCrack propagation; Finite element method; Fuselages; Joints (structural components); Stress concentration; Equivalent corrosion damage (ECD); Corrosion fatigue
Abstract
Publication date
LanguageEnglish
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NPARC number21275966
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Record identifiera8e0806a-e643-4042-b8d4-61ea383a6e9c
Record created2015-08-21
Record modified2016-05-09
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