Generic Linking of Finite Element Models for non-linear static and global dynamic analyses of aircraft structures

A.J. de Wit; D. Akcay-Perdahcioglu; W.M. van den Brink; A. de Boer

doi:10.3970/cmc.2012.032.201

Generic Linking of Finite Element Models for non-linear static and global dynamic analyses of aircraft structures

A.J. de Wit, D. Akcay-Perdahcioglu, W.M. van den Brink, A. de Boer

Faculty of Engineering Technology

Research output: Contribution to journal › Article › Academic › peer-review

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Abstract

Depending on the type of analysis, Finite Element(FE) models of different fidelity are necessary. Creating these models manually is a labor intensive task. This paper discusses a generic approach for generating FE models of different fidelity from a single reference FE model. These different fidelity models are created by sub-structuring and a multi-scale superposition technique. Efficiency of the developed approach is demonstrated via non-linear static and modal analysis of a carbon-fiber stiffened panel.

Original language	English
Pages (from-to)	201-218
Number of pages	18
Journal	Computers, materials & continua (CMC)
Volume	32
Issue number	3
DOIs	https://doi.org/10.3970/cmc.2012.032.201
Publication status	Published - 2012

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1 Conference contribution

Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures
de Wit, A. J., Akçay Perdahcıoglu, D., van den Brink, W. M. & de Boer, A., 21 Sept 2011, Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011. Rolfes, R. & Jansen, E. L. (eds.). Hannover: Leibniz Universität Hannover, p. 295-302 8 p.
Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

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AU - de Boer, A.

PY - 2012

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Generic Linking of Finite Element Models for non-linear static and global dynamic analyses of aircraft structures

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Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures

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