Multiaxial mechanical behavior of aramid fibers and identification of skin/core structure from single fiber transverse compression testing |
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Authors: | Judith Wollbrett‐Blitz Sébastien Joannès Rémi Bruant Christophe Le Clerc Marc Romero De La Osa Anthony Bunsell Alba Marcellan |
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Affiliation: | 1. ESPCI ParisTech, PSL—Research University, Laboratoire Sciences et Ingénierie de la Matière Molle, CNRS UMR CNRS 7615, France;2. Mines ParisTech, PSL—Research University, Centre des Matériaux, Evry Cedex, France;3. Manufacture Fran?aise des Pneumatiques Michelin, Clermont Ferrand Cedex 9, France;4. Sorbonne Universités, UPMC Univ. Paris 06, UMR 7615, Laboratoire Sciences et Ingénierie de la Matière Molle, Paris, France |
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Abstract: | The transverse and longitudinal mechanical properties of aramid fibers like Kevlar? 29 (K29) fibers are strongly linked to their highly oriented structure. Mechanical characterization at the single fiber scale is challenging especially when the diameter is as small as 15 µm. Longitudinal tensile tests on single K29 fibers and single fiber transverse compression test (SFTCT) have been developed. Our approach consists of coupling morphological observations and mechanical experiments with SFTCT analysis by comparing analytical solutions and finite element modeling. New insights on the analysis of the transverse direction response are highlighted. Systematic loading/unloading compression tests enable to experimentally determine a transverse elastic limit. Taking account of the strong anisotropy of the fiber, the transverse mechanical response sheds light on a skin/core architecture. More importantly, results suggest that the skin of the fiber, typically representing a shell of one micrometer in thickness, has a transverse apparent modulus of 0.2 GPa. That is around more than fifteen times lower than the transverse modulus of 3.0 GPa in the core. By comparison, the measured longitudinal modulus is about 84 GPa. The stress distribution in the fiber is explored and the critical areas for damage initiation are discussed. © 2015 Wiley Periodicals, Inc. J. Polym. Sci., Part B: Polym. Phys. 2016 , 54, 374–384 |
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Keywords: | aramid biaxiality compression computer modeling damage zone fibers finite element modeling interfaces Kevlar mechanical behavior modeling polyaromatics polyamides single fiber transverse compression test (SFTCT) skin/core structure stiffness surfaces structure‐property relation transverse compression uniaxial |
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