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

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.12989/aas.2017.4.1.001
AuthorSearch for: 1 ; Search for: 1 ; Search for: 1 ; Search for: ; Search for:
Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
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
Terms of use
LanguageEnglish
Peer reviewedYes
NPARC number23002574
Export citationExport as RIS
Report a correctionReport a correction
Record identifier8d1cc6ba-e17f-4984-9416-624438e3fed4
Record created2017-11-30
Record modified2017-11-30
Date modified: