Damage tolerance implications of corrosion pillowing on fuselage lap joints

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/2.2322
AuthorSearch for: 1; Search for: 1; Search for: 1
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
SubjectCorrosion; Crack propagation; Finite element method; Stress analysis; Stress intensity factors; Corrosion pillowing; Fuselage lap joints; Fuselages
Publication date
Peer reviewedYes
NRC numberSMPL-1997-0058
NPARC number21275965
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Record identifier914b5c37-1ef8-44bc-9c0a-31cccf825586
Record created2015-08-21
Record modified2020-03-20
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