2017
DOI: 10.2514/1.c033875
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Analysis and Design for the Moderately Deep Postbuckling Behavior of Composite Plates

Abstract: General rightsThis document is made available in accordance with publisher policies. Please cite only the published version using the reference above. Full terms of use are available: http://www.bristol.ac.uk/pure/about/ebr-terms

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Cited by 9 publications
(2 citation statements)
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References 33 publications
(34 reference statements)
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“…The evaluation of such the geometrically nonlinear response of thin‐walled structures under thermal–mechanical effects requires general, efficient, and robust numerical methods. The closed‐form and/or analytical methods are cumbersome to such problems, 18‐22 while the discretization technique, generally the nonlinear finite element (FE) method, is the most common tool for geometrically nonlinear problems 23 . The nonlinear systems of equations are solved in an incremental‐iterative manner using the Newton–Raphson method and its variants 24‐26 .…”
Section: Introductionmentioning
confidence: 99%
“…The evaluation of such the geometrically nonlinear response of thin‐walled structures under thermal–mechanical effects requires general, efficient, and robust numerical methods. The closed‐form and/or analytical methods are cumbersome to such problems, 18‐22 while the discretization technique, generally the nonlinear finite element (FE) method, is the most common tool for geometrically nonlinear problems 23 . The nonlinear systems of equations are solved in an incremental‐iterative manner using the Newton–Raphson method and its variants 24‐26 .…”
Section: Introductionmentioning
confidence: 99%
“…Pandey and Sherbourne 36 deduced an analytical formula to calculate the nonlinear performance of compressed composite plate and found that only optimizing the postbuckling performance would lead to the decrease of buckling load. The approximate solution of the initial postbuckling response was achieved by Wu et al, 37 followed by a two‐stage optimization strategy using the lamination parameters as the design variables. An asymptotic numerical method (ANM) based on the perturbation theory was applied by Raju et al 38 to achieve the nonlinear buckling optimization for variable stiffness composite laminates under axial compression.…”
Section: Introductionmentioning
confidence: 99%