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Structural and Multidisciplinary Optimization

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16.05.2016 | RESEARCH PAPER

Finite element model updating of honeycomb sandwich plates using a response surface model and global optimization technique

verfasst von: Wei-Qing Sun, Wei Cheng

Erschienen in: Structural and Multidisciplinary Optimization | Ausgabe 1/2017

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Abstract

Honeycomb sandwich plates are used widely in the aerospace industry. Building accurate finite element models of honeycomb sandwich plates is necessary for analyzing and optimizing the microvibration that occurs in spacecraft. This study investigated two types of finite element dynamic models of honeycomb plates: a sandwich shell model and a shell-volume-shell model. Two response surface model-based optimization methods and a particle swarm optimization method were compared for updating the finite element models. Finally, we validated the accuracy of the two optimized honeycomb sandwich plate finite element dynamic models by comparing the results obtained by the frequency response functions with experimental data.

Vorheriger Artikel Composite stacking sequence optimization for aeroelastically tailored forward-swept wings

Nächster Artikel Optimum design of laminated composite plates containing a quasi-square cutout

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Titel: Finite element model updating of honeycomb sandwich plates using a response surface model and global optimization technique
verfasst von: Wei-Qing Sun
Wei Cheng
Publikationsdatum: 16.05.2016
Verlag: Springer Berlin Heidelberg
Erschienen in: Structural and Multidisciplinary Optimization / Ausgabe 1/2017
Print ISSN: 1615-147X
Elektronische ISSN: 1615-1488
DOI: https://doi.org/10.1007/s00158-016-1479-1

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