Fatigue analysis for CF-18 component:wing fold shear-tie lug

Download
  1. (PDF, 2 MB)
  2. Get@NRC: Fatigue analysis for CF-18 component:wing fold shear-tie lug (Opens in a new window)
DOIResolve DOI: http://doi.org/10.1016/j.proeng.2010.03.180
AuthorSearch for: ; Search for:
TypeArticle
Journal titleProcedia Engineering
ISSN1877-7058
Volume2
Issue1
Pages16731682; # of pages: 10
SubjectLife prediction; HOLSIP; Short crack; FEM; Fractography; 7050
Abstract
Publication date
LanguageEnglish
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NPARC number21276092
Export citationExport as RIS
Report a correctionReport a correction
Record identifierd60e9b05-10f7-47d8-97ad-2c564418afb0
Record created2015-09-23
Record modified2016-05-09
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
Date modified: