Silva, N.M. und Degenhardt, Richard und Camotim, D. und Silvestre, N. (2008) Application of generalised beam theory to the study of the stability behaviour of laminated CFRP cylindrical stiffened panels. In: Proceedings of the 2nd International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures. 2nd International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, 2008-09-03 - 2008-09-05, Braunschweig, Deutschland.
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Kurzfassung
The paper presents the application of a novel fast numerical tool, based on Generalised Beam Theory (GBT), to perform buckling and post-buckling analyses of laminated CFRP panels. GBT is a beam theory developed for prismatic thinwalled members (e.g., columns, beams or panels), which takes into account both global and local deformations. One of its main features is the fact that the cross-section is discretised into deformation modes with clear mechanical meanings (e.g., global bending, distortional, local-plate, shear and transverse extension deformation modes) − this (i) allows for a better understanding of the member structural behaviour and (ii) makes it possible to perform analyses with very few d.o.f. (by preselecting a set of deformation modes). No stiffness degradation is taken into consideration and the material is deemed linear elastic and orthotropic. One presents numerical results concerning the local buckling and post-buckling behaviour of stiffened CFRP cylindrical panels, including one that was experimental and numerically investigated in the context of the COCOMAT project. The panel deformed configurations and buckling loads obtained with GBT are validated through the comparison with either experimental data or values yielded by shell finite element analyses carried out in the code ABAQUS.
elib-URL des Eintrags: | https://elib.dlr.de/55198/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
Titel: | Application of generalised beam theory to the study of the stability behaviour of laminated CFRP cylindrical stiffened panels | ||||||||||||||||||||
Autoren: |
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Datum: | September 2008 | ||||||||||||||||||||
Erschienen in: | Proceedings of the 2nd International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Herausgeber: |
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Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | generalised beam theory, local buckling and post-buckling, laminated CFRP panels | ||||||||||||||||||||
Veranstaltungstitel: | 2nd International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures | ||||||||||||||||||||
Veranstaltungsort: | Braunschweig, Deutschland | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 3 September 2008 | ||||||||||||||||||||
Veranstaltungsende: | 5 September 2008 | ||||||||||||||||||||
Veranstalter : | DLR Braunschweig, Institut für Faserverbundleichtbau und Adaptronik | ||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||
HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Strukturen & Werkstoffe (alt) | ||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Strukturmechanik | ||||||||||||||||||||
Hinterlegt von: | Ries, Doris | ||||||||||||||||||||
Hinterlegt am: | 09 Sep 2008 | ||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:19 |
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