Fatigue disbond growth for an adhesively bonded composite joint under mixed mode I/II loading

From National Research Council Canada

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Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Proceedings titleSAMPE 2014 Seattle
ConferenceSAMPE Technical Conference, June 2-5, 2014, Seattle, Washington
ISBN978-193455116-5
Pages112
Subjectaircraft manufacture; airframes; failure modes; fracture toughness; joints (structural components); repair; adhesively bonded composite joints; bonded composite joints; composite aircraft structure; critical fracture toughness; fatigue performance; growth characteristic; loading condition; part manufacturing
Abstract
Publication date
LanguageEnglish
Peer reviewedYes
NPARC number21275918
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Record identifierb8c0c947-7081-46c2-a28d-e326c123e266
Record created2015-08-05
Record modified2019-06-18
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