Abstract
This is a study of a uni-directional non-crimp fabric reinforced epoxy composite material typically used as the load carrying laminate in wind turbine blades. Based on a 3D xray
tomography scan, the bundle and fibre/matrix structure of the composite is segmented. This segmentation is used in a multi-scale finite element model bridging the gap from the
individual fibers organized in bundles to the stitched non-crimp fabric used for building up the load carrying laminates.
tomography scan, the bundle and fibre/matrix structure of the composite is segmented. This segmentation is used in a multi-scale finite element model bridging the gap from the
individual fibers organized in bundles to the stitched non-crimp fabric used for building up the load carrying laminates.
| Original language | English |
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| Title of host publication | Proceedings of 29th Nordic Seminar on Computational Mechanics |
| Number of pages | 4 |
| Publication date | 2016 |
| Publication status | Published - 2016 |
| Event | 29th Nordic Seminar on Computational Mechanics - Gothenburg, Sweden Duration: 26 Oct 2016 → 28 Oct 2016 |
Conference
| Conference | 29th Nordic Seminar on Computational Mechanics |
|---|---|
| Country/Territory | Sweden |
| City | Gothenburg |
| Period | 26/10/2016 → 28/10/2016 |