Issue |
EPJ Web Conf.
Volume 183, 2018
DYMAT 2018 - 12th International Conference on the Mechanical and Physical Behaviour of Materials under Dynamic Loading
|
|
---|---|---|
Article Number | 02018 | |
Number of page(s) | 6 | |
Section | Experimental Techniques | |
DOI | https://doi.org/10.1051/epjconf/201818302018 | |
Published online | 07 September 2018 |
https://doi.org/10.1051/epjconf/201818302018
Intralaminar fracture toughness of UD glass fiber composite under high rate fiber tension and fiber compression loading
1
Technical University of Munich, Department of Mechanical Engineering, Chair of Carbon Composites,
Boltzmannstrasse 15,
85748
Garching,
Germany
2
School of Mechanical and Aerospace Engineering, Queen’s University Belfast,
United Kingdom
3
INEGI, Institute of Science and Innovation in Mechanical and Industrial Engineering,
Rua Dr. Roberto Frias 400,
4200-465,
Porto,
Portugal
4
CITAB, University of Tras-os-Montes e Alto Douro, UTAD,
Quinta de Prados,
5000-801
Vila Real,
Portugal
* e-mail: kuhn@lcc.mw.tum.de
Published online: 7 September 2018
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g. crash, bird strike). In both industrial areas, energy-based damage models for composite materials, able to predict initiation and evolution of damage of a composite ply under various loading conditions, are increasingly used. These models require the specification of fracture toughness parameters for the main failure modes. In previous works [1],[2], the authors have successfully enhanced a methodology suggested by Catalanotti et al. [3],[4] to measure the fiber failure crack resistance curves of a UD carbon fiber composite under dynamic loading. This methodology uses the relation between the energy release rate, the crack resistance curve and the size-effect law. For the determination of the size-effect law, double-edge-notched specimens of different sizes are tested. In this work, the developed approach is used for the measurement of the fracture toughness for fiber tension and compression failure of a UD glass-epoxy composite under high rate loading. Static tests are performed on an electromechanical test machine. For the high rate tests, split-Hopkinson bars for tensile (SHTB) and compressive (SHPB) loading are used. The results show, that the fracture toughness of the UD glass-epoxy composite, associated with the fiber failure modes, increases with increasing loading rate for tension as well as for compression. The observed strain rate effect on the fracture toughness of the glass-epoxy composite is more pronounced than for the carbon-epoxy composite investigated in [1],[2], in particular for fiber tensile failure.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.