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
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Name affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Subjectfatigue life; global/local FE model coupling; crack growth; riveted lap joint; the Smith-Watson-Topper (SWT) equation
Publication date
Peer reviewedYes
NPARC number23002574
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Record identifier8d1cc6ba-e17f-4984-9416-624438e3fed4
Record created2017-11-30
Record modified2020-03-16
Date modified: