Effects of gaps and overlaps on the buckling behavior of an optimally designed variable-stiffness composite laminates - A numerical and experimental study

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1016/j.compstruct.2016.01.012
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  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectABAQUS; Buckling; Computer software; Finite element method; Laminates; MATLAB; Nonlinear analysis; Paper laminates; Stiffness; Composite laminate; Critical buckling loads; Fiber placement; Finite element simulations; Gaps/overlaps; Linear buckling analysis; Numerical and experimental study; Numerical investigations; Laminated composites; Composites; Fibers
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Peer reviewedYes
NPARC number21277434
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Record identifiera1dad797-c921-46b5-92d7-b527f11cd9be
Record created2016-03-09
Record modified2020-03-16
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