Dieses Dokument steht unter einer CreativeCommons Lizenz by/4.0
Verlagslink DOI: 10.3390/ma10091039
Titel: Compression fracture of CFRP laminates containing stress intensifications
Sprache: en
Autor/Autorin: Leopold, Christian 
Schütt, Martin 
Liebig, Wilfried V. 
Philipkowski, Timo 
Kürten, Jonas 
Schulte, Karl 
Fiedler, Bodo 
Schlagwörter: compression after impact (CAI);fractography;free-edge;kink-band;open-hole;scaling;scanning electron microscopy (SEM);stacking sequence
Erscheinungsdatum: 5-Sep-2017
Verlag: MDPI
Quellenangabe: Materials 10(2017),9: 1039
Zeitschrift: Materials 
Zusammenfassung (englisch): For brittle fracture behaviour of carbon fibre reinforced plastics (CFRP) under compression, several approaches exist, which describe different mechanisms during failure, especially at stress intensifications. The failure process is not only initiated by the buckling fibres, but a shear driven fibre compressive failure beneficiaries or initiates the formation of fibres into a kink-band. Starting from this kink-band further damage can be detected, which leads to the final failure. The subject of this work is an experimental investigation on the influence of ply thickness and stacking sequence in quasi-isotropic CFRP laminates containing stress intensifications under compression loading. Different effects that influence the compression failure and the role the stacking sequence has on damage development and the resulting compressive strength are identified and discussed. The influence of stress intensifications is investigated in detail at a hole in open hole compression (OHC) tests. A proposed interrupted test approach allows identifying the mechanisms of damage initiation and propagation from the free edge of the hole by causing a distinct damage state and examine it at a precise instant of time during fracture process. Compression after impact (CAI) tests are executed in order to compare the OHC results to a different type of stress intensifications. Unnotched compression tests are carried out for comparison as a reference. With this approach, a more detailed description of the failure mechanisms during the sudden compression failure of CFRP is achieved. By microscopic examination of single plies from various specimens, the different effects that influence the compression failure are identified. First damage of fibres occurs always in 0°-ply. Fibre shear failure leads to local microbuckling and the formation and growth of a kink-band as final failure mechanisms. The formation of a kink-band and finally steady state kinking is shifted to higher compressive strains with decreasing ply thickness. Final failure mode in laminates with stress intensification depends on ply thickness. In thick or inner plies, damage initiates as shear failure and fibre buckling into the drilled hole. The kink-band orientation angle is changing with increasing strain. In outer or thin plies shear failure of single fibres is observed as first damage and the kink-band orientation angle is constant until final failure. Decreasing ply thickness increases the unnotched compressive strength. When stress intensifications are present, the position of the 0°-layer is critical for stability under compression and is thus more important than the ply thickness. Central 0°-layers show best results for OHC and CAI strength due to higher bending stiffness and better supporting effect of the adjacent layers.
URI: http://tubdok.tub.tuhh.de/handle/11420/1505
URN: nbn:de:gbv:830-88218032
DOI: 10.15480/882.1502
ISSN: 1996-1944
Institut: Kunststoffe und Verbundwerkstoffe M-11 
Dokumenttyp: (wissenschaftlicher) Artikel
Enthalten in den Sammlungen:tub.dok

Dateien zu dieser Ressource:
Datei Beschreibung GrößeFormat 
materials-10-01039-v2.pdfPublisher's version4,92 MBAdobe PDFMiniaturbild
Zur Langanzeige


Letzte Woche
Letzten Monat
checked on 22.01.2018


checked on 22.01.2018

Google ScholarTM



Alle Ressourcen in diesem Repository sind urheberrechtlich geschützt.