Wolff, Caroline und Wilckens, Dirk (2015) Testing and simulation of impact damaged stiffened CFRP-panels. 3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, 2015-03-25 - 2015-03-27, Braunschweig.
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Kurzfassung
In the present contribution, the residual strength behaviour of stiffened CFRP shells under axial compression loading is discussed. In this context, two stiffened CFRP panels are pre-damaged by impact and tested under axial compression until collapse. The panels without damage were tested before in order to obtain a reference result. Two different impact scenarios are investigated on a T- and a J-stringer stiffened panel, respectively. The damaged area is assessed by ultra-sonic (US) inspection. Load shortening data, strains as well as full field displacements are recorded during the test. Additionally to the experiments, the structural behaviour is simulated for the undamaged and damaged structures using the commercial FE-code Abaqus. The US inspection results of the impacted areas are transferred into the FE-models, and the stiffness and strength of affected elements are degraded accordingly. The numerical results are compared to the experimental findings. Through this approach, the influence of both impact scenarios on the structural behaviour of stiffened CFRP shells is assessed by test and simulation.
elib-URL des Eintrags: | https://elib.dlr.de/99009/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag, Poster) | ||||||||||||
Titel: | Testing and simulation of impact damaged stiffened CFRP-panels | ||||||||||||
Autoren: |
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Datum: | März 2015 | ||||||||||||
Referierte Publikation: | Nein | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | stiffened panel, buckling, postbuckling, impact, residual strength, NDI-FEM-transfer, test and simulation | ||||||||||||
Veranstaltungstitel: | 3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures | ||||||||||||
Veranstaltungsort: | Braunschweig | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsbeginn: | 25 März 2015 | ||||||||||||
Veranstaltungsende: | 27 März 2015 | ||||||||||||
Veranstalter : | DLR-Institut für Faserverbundleichtbau und Adaptronik | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Strukturen und Werkstoffe (alt) | ||||||||||||
Standort: | Braunschweig | ||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Strukturmechanik | ||||||||||||
Hinterlegt von: | Lüders, Dr.-Ing. Caroline | ||||||||||||
Hinterlegt am: | 14 Dez 2015 07:58 | ||||||||||||
Letzte Änderung: | 24 Apr 2024 20:04 |
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