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Damage and failure of triaxial braided composites under multi-axial stress states

Title: Damage and failure of triaxial braided composites under multi-axial stress states
Authors: Wehrkamp-Richter, T
Hinterholz, R
Pinho, ST
Item Type: Journal Article
Abstract: Damage and failure of triaxial braided composites under multi-axial stress states was investigated. In order to introduce different multi-axial stress states in the material, uni-axial tensile tests were performed at different off-axis orientations. Three braid architectures, comprising braiding angles of 30°, 45° and 60° were each loaded parallel to their axial, transverse and braid yarn direction. Digital image correlation measurement techniques were used to quantify the effects of the textile architecture and its heterogeneity on the strain field, to identify and locate constituent failure mechanisms and to investigate damage initiation and development. In order to identify the driving physical mechanisms behind the material non-linearity, the evolution of the damage variable and the accumulated inelastic strain was quantified using incremental loading/unloading experiments. A high-speed camera was employed in order to study the dynamic nature of catastrophic failure. The triaxial braids within this study exhibited severe non-linearities in the mechanical response before final failure as a result of extensive matrix cracking. While we found the underlying textile architecture to slightly reduce the elastic properties compared to equivalent tape laminates, it functions as a natural crack arresting grid. As a result of this mechanism, braids under certain load conditions were capable of withstanding a higher strain to failure, even if a large portion of the specimen surface was saturated with matrix cracks. The accompanying mechanical behaviour can be desirable in the design of crash absorbing or pseudo-ductile materials. An additional failure mode intrinsic to the textile architecture was encountered for loading in the heavily undulated braid yarn direction. Due to yarn straightening and out-of-plane movements, braided composites were found to fail as a result of large scale delaminations accompanied by progressive fibre bundle pull-out.
Issue Date: 6-Jul-2017
Date of Acceptance: 2-Jul-2017
URI: http://hdl.handle.net/10044/1/53456
DOI: https://dx.doi.org/10.1016/j.compscitech.2017.07.002
ISSN: 0266-3538
Publisher: ELSEVIER SCI LTD
Start Page: 32
End Page: 44
Journal / Book Title: COMPOSITES SCIENCE AND TECHNOLOGY
Volume: 150
Copyright Statement: © 2017 Elsevier Ltd. All rights reserved. This manuscript is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/
Keywords: Science & Technology
Technology
Materials Science, Composites
Materials Science
Textile composites
Non-linear behaviour
Matrix cracking
Braiding
TEXTILE COMPOSITES
BEHAVIOR
MODEL
09 Engineering
Materials
Publication Status: Published
Appears in Collections:Faculty of Engineering
Aeronautics



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