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Multiaxial mechanical behavior of aramid fibers and identification of skin/core structure from single fiber transverse compression testing
Authors:Judith Wollbrett‐Blitz  Sébastien Joannès  Rémi Bruant  Christophe Le Clerc  Marc Romero De La Osa  Anthony Bunsell  Alba Marcellan
Institution: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
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
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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