Effect of the Riveting Process on the Residual Stress in Fuselage Lap Joints - 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 49th Annual General Meeting and Conference of the Canadian Aeronautics and Space Institute From 4/28/2003 To 4/30/2003, Montreal, Quebec, Canada
SubjectFinite element method; Force-controlled riveting method; Residual stress; Riveted lap joint
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberSMPL-2002-0250
NPARC number8933664
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Record identifier8235b21e-e423-4a20-aa12-253dfe1ca07a
Record created2009-04-23
Record modified2020-04-16
Date modified: