Fatigue Crack Origins in 7075-T6 and 7079-T6 Aluminum Alloys

AuthorSearch for: ; Search for: ; Search for:
Conference16th Aerospace Structures and Materials Symposium, Canadian Aeronautics and Space Institute (CASI), From 4/28/2003 To 4/30/2003., Montreal, Canada
SubjectFatigue; Aluminum alloys; Nucleation; Anodizing; Crack origin
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
Peer reviewedYes
NRC numberSMPL-2003-0015
NPARC number8926697
Export citationExport as RIS
Report a correctionReport a correction
Record identifierd8796e75-07d9-43b5-924e-ebdd354448d5
Record created2009-04-23
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)
  • Share this page with Delicious (Opens in a new window)