A Stress Analysis Method for Bi-axially loaded fastener hole in a laminate of finite geometry

AuthorSearch for:
TypeOther
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionunclassified/unlimited
Peer reviewedNo
NRC numberSMPL-1997-0079
NPARC number8933296
Export citationExport as RIS
Report a correctionReport a correction
Record identifiera26cc8f7-b6b1-43e5-ab5c-7e83d48b1fc2
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)