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INVESTIGATION OF RESIDUAL STRESS IN RIVETED LAP JOINTS --- Computational Simulation

From National Research Council Canada

AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Technical Report
SubjectFinite element method; residual stress; fuselage lap joint; squeeze force
Access condition
  • available
  • unclassified
  • unlimited
NRC numberSMPL-2003-0101
NPARC number8933499
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Record identifier4d4b1803-23d9-45b5-993b-fa68cc663b74
Record created2009-04-23
Record modified2020-03-09
Date modified: