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

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

Faculty of Engineering Technology

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

59 Downloads (Pure)

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 of 3rd Eccomas conference
Editors	R. Rolfes, E.L. Jansen
Place of Publication	Hannover
Publisher	Leibniz Universität
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
IR-77613
METIS-273829

Access to Document

Wit11generic

Cite this

@inproceedings{345f6791783d4736908fe9ddad51ca8f,

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

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, IR-77613, METIS-273829",

author = "{de Wit}, A.J. and Didem Akcay-Perdahcioglu and {van den Brink}, W.M. and {de Boer}, Andries",

year = "2011",

month = sep,

day = "21",

language = "English",

isbn = "978-3-00-035855-5",

pages = "295--302",

editor = "R. Rolfes and E.L. Jansen",

booktitle = "Proceedings of 3rd Eccomas conference",

publisher = "Leibniz Universit{\"a}t",

note = "3rd ECCOMAS Thermatic Conference on Mechanical Response of Composites 2011, ECCOMAS 2011 ; Conference date: 21-09-2011 Through 23-09-2011",

}

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. et al.
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 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 - Akcay-Perdahcioglu, Didem

AU - van den Brink, W.M.

AU - de Boer, Andries

N1 - Conference code: 3

PY - 2011/9/21

Y1 - 2011/9/21

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

KW - IR-77613

KW - METIS-273829

M3 - Conference contribution

SN - 978-3-00-035855-5

SP - 295

EP - 302

BT - Proceedings of 3rd Eccomas conference

A2 - Rolfes, R.

A2 - Jansen, E.L.

PB - Leibniz Universität

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

Abstract

Conference

Keywords

Access to Document

Fingerprint

Cite this