2011
DOI: 10.1016/j.compscitech.2010.11.012
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Structurally stitched NCF CFRP laminates. Part 1: Experimental characterization of in-plane and out-of-plane properties

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Cited by 48 publications
(36 citation statements)
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“…Therefore, unstitched laminates composed from 90°UD NCFs ( Fig. 1 and Table 1 in [1]) and RTM 6 aerospace grade epoxy resin (Hexcel Composites GmbH) using a vacuum assisted resin infusion process were subjected to uni-axial tension, compression and shear in servohydraulic testing machines until ultimate failure as given in Table 1. Upon loading the force and the elongation parallel to the loading direction were recorded from which the strength and modulus were evaluated according to the given standards.…”
Section: Stiffness and Strength Properties Of Individual Ncf Layermentioning
confidence: 99%
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“…Therefore, unstitched laminates composed from 90°UD NCFs ( Fig. 1 and Table 1 in [1]) and RTM 6 aerospace grade epoxy resin (Hexcel Composites GmbH) using a vacuum assisted resin infusion process were subjected to uni-axial tension, compression and shear in servohydraulic testing machines until ultimate failure as given in Table 1. Upon loading the force and the elongation parallel to the loading direction were recorded from which the strength and modulus were evaluated according to the given standards.…”
Section: Stiffness and Strength Properties Of Individual Ncf Layermentioning
confidence: 99%
“…Experimental investigations on structurally stitched NCF carbon fiber reinforced plastic laminates (CFRP) subjected to in-plane loading (Figs. 14, 16 and 17 in [1]) showed that depending on the stitching parameters applied, at best similar, but in the majority of cases reduced tension, compression and shear strengths up to 36%, 31% and 22% compared to the unstitched laminate must be expected [1,20,21]. A comprehensive analysis of published data of 3-D reinforced composites including stitching was published in a review article by Mouritz and Cox [22] which includes quantifications and a thorough discussion of candidate mechanisms on fiber architecture, in-plane stiffness, in-plane and out-of-plane strength as well as on fatigue strength.…”
Section: Introductionmentioning
confidence: 97%
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