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

From National Research Council Canada

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  1. National Research Council Canada. Aerospace
Proceedings titleSAMPE 2014 Seattle
ConferenceSAMPE Technical Conference, June 2-5, 2014, Seattle, Washington
Pages112; # of pages: 12
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
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Peer reviewedYes
NPARC number21275918
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Record identifierb8c0c947-7081-46c2-a28d-e326c123e266
Record created2015-08-05
Record modified2016-05-09
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