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

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

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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 languageEnglish
Title of host publicationProceedings of 3rd Eccomas conference
EditorsR. Rolfes, E.L. Jansen
Place of PublicationHannover
PublisherLeibniz Universität
Pages295-302
Number of pages8
ISBN (Print)978-3-00-035855-5
Publication statusPublished - 21 Sep 2011
Event3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011 - Hannover, Germany
Duration: 21 Sep 201123 Sep 2011
Conference number: 3

Conference

Conference3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011
Abbreviated titleECCOMAS 2011
CountryGermany
CityHannover
Period21/09/1123/09/11

Fingerprint

Aircraft
Static analysis
Modal analysis
Carbon fibers
Personnel
Finite element method

Keywords

  • EC Grant Agreement nr.: FP7/234147
  • IR-77613
  • METIS-273829

Cite this

de Wit, A. J., Akcay-Perdahcioglu, 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 of 3rd Eccomas conference (pp. 295-302). Hannover: Leibniz Universität.
de Wit, A.J. ; Akcay-Perdahcioglu, Didem ; van den Brink, W.M. ; de Boer, Andries. / Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures. Proceedings of 3rd Eccomas conference. editor / R. Rolfes ; E.L. Jansen. Hannover : Leibniz Universität, 2011. pp. 295-302
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de Wit, AJ, Akcay-Perdahcioglu, 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 of 3rd Eccomas conference. Leibniz Universität, 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.; Akcay-Perdahcioglu, Didem; van den Brink, W.M.; de Boer, Andries.

Proceedings of 3rd Eccomas conference. ed. / R. Rolfes; E.L. Jansen. Hannover : Leibniz Universität, 2011. p. 295-302.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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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.

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de Wit AJ, Akcay-Perdahcioglu D, van den Brink WM, de Boer A. Generic linking of finite element models for non-linear static and global dynamic analyses for aircraft structures. In Rolfes R, Jansen EL, editors, Proceedings of 3rd Eccomas conference. Hannover: Leibniz Universität. 2011. p. 295-302