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

A 3D Continuum Damage Model for Tough Fibre Reinforced Polymer Composites Using Cuntze's Failure Mode Concept

Völkerink, Oliver und Petersen, Enno und Hühne, Christian (2019) A 3D Continuum Damage Model for Tough Fibre Reinforced Polymer Composites Using Cuntze's Failure Mode Concept. VI International Conference on Computational Modeling of Fracture and Failure of Materials and Structures, 2019-06-12 - 2019-06-14, Braunschweig, Deutschland.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Offizielle URL: https://congress.cimne.com/cfrac2019/admin/files/fileabstract/a65.pdf

Kurzfassung

Fibre Reinforced Plastics with tough epoxy and thermoplastic matrices showing inherent non-linear behaviour are spreading increasingly. Conventional design approaches, which assume linear elastic mate- rial behaviour and laminate failure at First Ply Failure, are very conservative. For an efficient and reliable design of structures the mechanical behaviour considering various failure modes under complex loading and damage progression has to be estimated in the design phase with numerical simulations. For this purpose continuum damage models are available. However, most state-of-the-art continuum damage models do not consider the inherent non-linear behaviour of the matrix material or are not suited for 3D solid finite elements. This work proposes a 3D continuum damage model. It uses a single-parameter flow criterion from Sun and Chen in combination with Cuntze's Failure Mode Concept for intra laminar failure. As the Failure Mode Concept by Cuntze is based on invariants, no computational expensive iterative fracture angle search for inter-fibre failure is needed. In addition, the model features a strain-based gradual degradation model adopted from Donadon et al. This work describes details of the developed model like the coupling of the Failure Mode Concept with the degradation model as well as the implementation of the model into Abaqus / Standard as a user-defined material model (UMAT). The model is verified with single element models using periodic boundary conditions. Furthermore, the model is validated against tests on coupon level from literature. Both tough epoxy and thermoplastic carbon fibre composite specimens are considered. It can be shown that the model is able to capture the failure behaviour of the specimens and accurately predict failure loads.

elib-URL des Eintrags:https://elib.dlr.de/127889/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:A 3D Continuum Damage Model for Tough Fibre Reinforced Polymer Composites Using Cuntze's Failure Mode Concept
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Völkerink, Oliveroliver.voelkerink (at) dlr.dehttps://orcid.org/0000-0002-9589-1963NICHT SPEZIFIZIERT
Petersen, EnnoEnno.Petersen (at) dlr.dehttps://orcid.org/0000-0002-1488-5618NICHT SPEZIFIZIERT
Hühne, ChristianChristian.Huehne (at) dlr.dehttps://orcid.org/0000-0002-2218-1223NICHT SPEZIFIZIERT
Datum:14 Juni 2019
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:UMAT, CDM, material model, Failure Mode Concept, fibre reinforced plastic, frp, damage, continuum damage mechanics, composite, Cuntze, finite element method, FEM, FEA, progressive damage analysis
Veranstaltungstitel:VI International Conference on Computational Modeling of Fracture and Failure of Materials and Structures
Veranstaltungsort:Braunschweig, Deutschland
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:12 Juni 2019
Veranstaltungsende:14 Juni 2019
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 - Simulation und Validierung (alt), L - Strukturen und Werkstoffe (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau
Hinterlegt von: Völkerink, Dr. Oliver
Hinterlegt am:21 Jun 2019 09:52
Letzte Änderung:29 Jul 2024 08:56

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.