Damage tolerance implications of corrosion pillowing on fuselage lap joints

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DOIResolve DOI: http://doi.org/10.2514/2.2322
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TypeArticle
Journal titleJournal of Aircraft
ISSN0021-8669
Volume35
Issue3
Pages487491; # of pages: 5
SubjectCorrosion; Crack propagation; Finite element method; Stress analysis; Stress intensity factors; Corrosion pillowing; Fuselage lap joints; Fuselages
Abstract
Publication date
LanguageEnglish
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NRC numberSMPL-1997-0058
NPARC number21275965
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Record identifier914b5c37-1ef8-44bc-9c0a-31cccf825586
Record created2015-08-21
Record modified2016-05-09
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