Modeling and Analysis of Cracks in Fuselage Lap Joints with Single-Countersunk Rivet - ABSTRACT ONLY

From National Research Council Canada

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Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceThe International Conference on Computational Methods From 12/15/2004 To 12/17/2004, Singapore
SubjectStress intensity factor; fuselage lap joint with single-countersunk rivet; global-local approach; finite elelement and symmetric Garlerkin boundary element alternating method; residual stress
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberSMPL-2004-0047
NPARC number8932952
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Record identifierb39b42fc-df20-4ee2-9b94-ec9720ef58c3
Record created2009-04-23
Record modified2020-04-16
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