A methodology for assessing fatigue life of a countersunk riveted lap joint

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DOIResolve DOI: http://doi.org/10.12989/aas.2017.4.1.001
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TypeArticle
Journal titleAdvances in Aircraft and Spacecraft Science
ISSN2287-5271
Volume4
Issue1
Pages# of pages: 19
Subjectfatigue life; global/local FE model coupling; crack growth; riveted lap joint; the Smith-Watson-Topper (SWT) equation
Abstract
Publication date
PublisherTechno-Press
LanguageEnglish
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number23002574
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Record identifier8d1cc6ba-e17f-4984-9416-624438e3fed4
Record created2017-11-30
Record modified2017-11-30
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