Residual life predictions of corroded fuselage lap joints

From National Research Council Canada

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  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
SubjectCrack propagation; Finite element method; Fuselages; Joints (structural components); Stress concentration; Equivalent corrosion damage (ECD); Corrosion fatigue
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Peer reviewedYes
NPARC number21275966
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Record identifiera8e0806a-e643-4042-b8d4-61ea383a6e9c
Record created2015-08-21
Record modified2020-03-27
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