Völkerink, Oliver and Petersen, Enno and Koord, Josef and Hühne, Christian (2020) A pragmatic approach for a 3D material model considering elasto-plastic behaviour, damage initiation by Puck or Cuntze and progressive failure of fibre-reinforced plastics. Computers & Structures, 236 (106280). Elsevier. doi: 10.1016/j.compstruc.2020.106280. ISSN 0045-7949.
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Official URL: http://www.sciencedirect.com/science/article/pii/S0045794920300833
Abstract
Fibre reinforced plastics with tough epoxy and thermoplastic matrices are spreading increasingly in many lightweight applications. For an efficient and reliable design the mechanical behaviour, considering non-linear plasticity, various failure modes under complex loading and damage progression, has to be estimated with numerical simulations. Most state-of-the-art continuum damage mechanics models do not consider the non-linear behaviour of the matrix material or are not suited for 3D solid elements. This work proposes a combined 3D continuum damage/plasticity model. It uses a single parameter flow criterion in combination with Cuntze’s Failure Mode Concept (FMC) for intralaminar failure. The FMC requires no iterative fracture angle search as the Action Plane Strength Criterion by Puck (APSC). This work describes details of the developed model like the coupling of the FMC with a degradation model as well as the implementation into Abaqus/Standard. A validation against open-hole tension tests made out of AS4/PEEK from literature is performed. It can be shown that the prediction of experimental failure loads with the FMC as well as with the APSC provides comparable results. The maximum deviations are between -7.85% and +12.85%. However, the computation times for predictions with the FMC are significantly less than with the APSC.
| Item URL in elib: | https://elib.dlr.de/135247/ | ||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||
| Title: | A pragmatic approach for a 3D material model considering elasto-plastic behaviour, damage initiation by Puck or Cuntze and progressive failure of fibre-reinforced plastics | ||||||||||||||||||||
| Authors: |
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| Date: | 19 May 2020 | ||||||||||||||||||||
| Journal or Publication Title: | Computers & Structures | ||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||
| Volume: | 236 | ||||||||||||||||||||
| DOI: | 10.1016/j.compstruc.2020.106280 | ||||||||||||||||||||
| Publisher: | Elsevier | ||||||||||||||||||||
| ISSN: | 0045-7949 | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | Damage mechanics, Finite element analysis (FEA), Failure criterion, Non-linear behaviour, Plastic deformation, Fibre reinforced plastics | ||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||
| DLR - Research theme (Project): | L - Simulation and Validation (old), L - Structures and Materials (old) | ||||||||||||||||||||
| Location: | Braunschweig | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures | ||||||||||||||||||||
| Deposited By: | Völkerink, Dr. Oliver | ||||||||||||||||||||
| Deposited On: | 21 Jun 2020 16:53 | ||||||||||||||||||||
| Last Modified: | 23 Oct 2023 13:27 |
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