2017
DOI: 10.1016/j.compscitech.2017.10.004
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Three dimensional fatigue damage evolution in non-crimp glass fibre fabric based composites used for wind turbine blades

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Cited by 41 publications
(50 citation statements)
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“…The fatigue test was interrupted for X-ray CT examination after 47,300, 57,300, 67,300, and 77,300 load cycles followed by failure of the specimen. The last interruption point was close to final failure (see also [1] ).…”
Section: Experimental Design Materials and Methodsmentioning
confidence: 81%
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“…The fatigue test was interrupted for X-ray CT examination after 47,300, 57,300, 67,300, and 77,300 load cycles followed by failure of the specimen. The last interruption point was close to final failure (see also [1] ).…”
Section: Experimental Design Materials and Methodsmentioning
confidence: 81%
“…Ex-situ X-ray CT fatigue experiments were carried out on a 410 mm long butterfly shaped test specimen optimised for testing uni-directional (UD) fibre composites [2] with a 15 mm wide gauge section [1] . The material system considered was a glass fibre non-crimp fabric reinforced polyester composite with the layup [b/biaxial,b/0,b/0] s where “b” refers to the supporting backing layer and “0” to the UD fibre bundles, which are stitched to the backing layer.…”
Section: Experimental Design Materials and Methodsmentioning
confidence: 99%
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“…The scanned unidirectional (UD) glass fibre composite is a non-crimp fabric commonly used in the load-carrying parts of wind turbine blades, for details on this type of composite see [4] . The imaged sample of cross-sectional size 2 mm × 2 mm consists of UD fibre bundles stitched on backing bundles angled 45°, −45° and 90° with respect to the UD (0°) bundles.…”
Section: Experimental Design Materials and Methodsmentioning
confidence: 99%