Assessment of debond simulation and cohesive zone length in a bonded composite joint

From National Research Council Canada

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  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectBonded composite joints; Cohesive zones; Traction law; Cohesive tractions; Double cantilever beam; Experimental analysis; Progressive failure; Theoretical solutions; Cantilever beams; Finite element method; Joints (structural components); Stiffness
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Peer reviewedYes
NPARC number21275819
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Record identifierea6c3986-bb00-4eea-92d8-d558475c2458
Record created2015-07-14
Record modified2020-04-22
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