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

A.J. de Wit; D. Akçay Perdahcıoglu; W.M. van den Brink; A. de Boer

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

A.J. de Wit
, D. Akçay Perdahcıoglu
, W.M. van den Brink
, A. de Boer

Faculty of Engineering Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › 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
Title of host publication	Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011
Editors	R. Rolfes, E.L. Jansen
Place of Publication	Hannover
Publisher	Leibniz Universität Hannover
Pages	295-302
Number of pages	8
ISBN (Print)	978-3-00-035855-5
Publication status	Published - 21 Sept 2011
Event	3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011 - Hannover, Germany Duration: 21 Sept 2011 → 23 Sept 2011 Conference number: 3

Conference

Conference	3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011
Abbreviated title	ECCOMAS 2011
Country/Territory	Germany
City	Hannover
Period	21/09/11 → 23/09/11

Keywords

EC Grant Agreement nr.: FP7/234147

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Generic Linking of Finite Element Models for non-linear static and global dynamic analyses of aircraft structures
de Wit, A. J., Akcay-Perdahcioglu, D., van den Brink, W. M. & de Boer, A., 2012, In: Computers, materials & continua (CMC). 32, 3, p. 201-218 18 p.
Research output: Contribution to journal › Article › Academic › peer-review

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de Wit, A. J., Akçay Perdahcıoglu, D., van den Brink, W. M., & de Boer, A. (2011). Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures. In R. Rolfes, & E. L. Jansen (Eds.), Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011 (pp. 295-302). Leibniz Universität Hannover.

de Wit, A.J. ; Akçay Perdahcıoglu, D. ; van den Brink, W.M. et al. / Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures. Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011. editor / R. Rolfes ; E.L. Jansen. Hannover : Leibniz Universität Hannover, 2011. pp. 295-302

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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.",

keywords = "EC Grant Agreement nr.: FP7/234147",

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year = "2011",

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de Wit, AJ, Akçay Perdahcıoglu, D, van den Brink, WM & de Boer, A 2011, Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures. in R Rolfes & EL Jansen (eds), Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011. Leibniz Universität Hannover, Hannover, pp. 295-302, 3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011, Hannover, Germany, 21/09/11.

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. et al.
Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011. ed. / R. Rolfes; E.L. Jansen. Hannover: Leibniz Universität Hannover, 2011. p. 295-302.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

TY - GEN

T1 - Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures

AU - de Wit, A.J.

AU - Akçay Perdahcıoglu, D.

AU - van den Brink, W.M.

AU - de Boer, A.

N1 - Conference code: 3

PY - 2011/9/21

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N2 - 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.

AB - 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.

KW - EC Grant Agreement nr.: FP7/234147

M3 - Conference contribution

SN - 978-3-00-035855-5

SP - 295

EP - 302

BT - Proceedings 3rd ECCOMAS Thematic Conference on the Mechanical Response of Composites 2011

A2 - Rolfes, R.

A2 - Jansen, E.L.

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CY - Hannover

T2 - 3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011

Y2 - 21 September 2011 through 23 September 2011

ER -

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

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

Cite this