elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Characterisation of textile composites under combined three dimensional load conditions

Hartung, Daniel und Aschenbrenner, Lars und Teßmer, Jan (2007) Characterisation of textile composites under combined three dimensional load conditions. Third International Conference on Computational Methods and Experiments in Material Characterisation, 2007-06-13 - 2007-06-15, Bologna, Italien.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Anisotropic textile composites show nonlinear deformation and complex failure behaviour. In particular three-dimensional reinforced textile composites are characterised by an orthotropic material behaviour. To improve the erformance of Non Crimp Fabrics (NCF) for lightweight structures the material and failure behaviour has to be analysed especially for regions dominated by three-dimensional stress distributions e. g. load introduction areas. Especially for the numerical analyses of thick laminates with significant stresses in thickness direction finite p-Volume-Elements based on hierarchical shape functions are developed and applied to selected structures. With focus on the material behaviour under combined load conditions an experimental procedure was designed. Aiming at the determination of throughthickness material properties a modified Arcan test device was developed that also enables evaluation of strength properties under combined tension and shear loads in material thickness direction of a moderately thick specimen plate. These advantageous small material thickness allows a tufting in thickness direction. By this process a three-dimensional fibre reinforced composite structure is provided that enables higher delamination strength compared to two-dimensional reinforced textile materials. Therefore the modified Arcan test device provides high potential to characterise influences of three-dimensional reinforcements within textile laminates. Furthermore combined test results are derived characterising material behaviour under combined interlaminar-shear and through-thickness tension load conditions. These tests require different specimen geometries for different combined and uncombined load conditions. Preliminary experimental and numerical studies show the optimisation of specimen geometry due to generate well defined stress states for an untufted NCF material. The experimentally determined material parameters serve as basis for a material model to describe the behaviour of three-dimensional reinforced laminates. Numerical simulations of the conducted experiments and structural analyses of a thick double holed plate demonstrate applicability of the material model and its implementation in the developed p-Volume-Element.

elib-URL des Eintrags:https://elib.dlr.de/50913/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Characterisation of textile composites under combined three dimensional load conditions
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Hartung, DanielNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Aschenbrenner, LarsNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Teßmer, JanNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:Juni 2007
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Stichwörter:textile composites, failure, lightweight structures
Veranstaltungstitel:Third International Conference on Computational Methods and Experiments in Material Characterisation
Veranstaltungsort:Bologna, Italien
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:2007-06-13 - 2007-06-15
HGF - Forschungsbereich:Verkehr und Weltraum (alt)
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:14 Aug 2007
Letzte Änderung:27 Apr 2009 14:16

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.