Fatigue analysis for CF-18 component:wing fold shear-tie lug

From National Research Council Canada

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DOIResolve DOI: https://doi.org/10.1016/j.proeng.2010.03.180
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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
SubjectLife prediction; HOLSIP; Short crack; FEM; Fractography; 7050
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LanguageEnglish
Peer reviewedYes
NPARC number21276092
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Record created2015-09-23
Record modified2020-06-04
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