Wrinkling patterns of electrospun nanofabrics in uniaxial tension
Date Issued
2021
Author(s)
Abstract
Electrospun nanofabrics are gaining popularity in a variety of applications [1,2]. One such application is the use of nanofabrics, as enhancers of the mechanical performance of fiber-reinforced polymers (FRPs). The enhancement is realized through a multi-scale structure comprising the polymer matrix, the fibers which form the layered macro scale reinforcement and the nano-scale reinforcement introduced as interlayers [3]. Candidate nanofabric systems, were investigated in uniaxial tension in order to evaluate their potential as interlayer reinforcements.
This contribution, aims to bring forth wrinkling pattens that were observed in the transverse direction, during the performed tensile strength tests. The tests were performed with a custom-made tensile apparatus which provided force and displacement resolutions of 0.25N of 200 microns. The specimens used for tensile testing were two strips of nanofabric placed back to back, with gauge length between 122-125 mm, width 32 mm and thickness ranging between 9-16 microns per strip, depending on the nanofabric system. The testing was captured on video and the evolution of wrinkling patterns were inferred by video analysis.
We find that out of plane wrinkling initiates at small linear strains at the direction normal to the loading axis. In the post-wrinkling stage, mode-jumping is observed with higher frequency wrinkles at lower amplitudes, which manifest beyond the nanofabrics’ yielding stress. Furthermore, wrinkling appears to be heterogeneous, in the sense that there are regions within the specimen that exhibit higher frequency wrinkles than others for the same loading increment, while there exist bands in between them that show none to minimal wrinkling. These phenomena will be juxtaposed to the measured stress-strain curves for a selection of the nanofabrics tested and will be discussed in relationship to existing analytical models [4] and the potential development of further analytical models to describe this response.
[1] Z.-M. Huang, Y.-Z. Zhang, M. Kotaki, and S. Ramakrishna, “A review on polymer nanofibers by electrospinning and their applications in nanocomposites,” Compos. Sci. Technol., vol. 63, no. 15, pp. 2223–2253, 2003, doi: https://doi.org/10.1016/S0266-3538(03)00178-7.
[2] N. E. Zander, “Hierarchically Structured Electrospun Fibers,” Polymers (Basel)., vol. 5, no. 1, pp. 19–44, 2013, doi: 10.3390/polym5010019.
[3] V. Kostopoulos, A. Masouras, A. Baltopoulos, A. Vavouliotis, G. Sotiriadis, and L. Pambaguian, “A critical review of nanotechnologies for composite aerospace structures,” CEAS Sp. J., vol. 9, no. 1, pp. 35–57, 2017, doi: 10.1007/s12567-016-0123-7.
[4] E. Cerda and L. Mahadevan, “Geometry and Physics of Wrinkling,” Phys. Rev. Lett., vol. 90, no. 7, p. 74302, Feb. 2003, doi: 10.1103/PhysRevLett.90.074302
This contribution, aims to bring forth wrinkling pattens that were observed in the transverse direction, during the performed tensile strength tests. The tests were performed with a custom-made tensile apparatus which provided force and displacement resolutions of 0.25N of 200 microns. The specimens used for tensile testing were two strips of nanofabric placed back to back, with gauge length between 122-125 mm, width 32 mm and thickness ranging between 9-16 microns per strip, depending on the nanofabric system. The testing was captured on video and the evolution of wrinkling patterns were inferred by video analysis.
We find that out of plane wrinkling initiates at small linear strains at the direction normal to the loading axis. In the post-wrinkling stage, mode-jumping is observed with higher frequency wrinkles at lower amplitudes, which manifest beyond the nanofabrics’ yielding stress. Furthermore, wrinkling appears to be heterogeneous, in the sense that there are regions within the specimen that exhibit higher frequency wrinkles than others for the same loading increment, while there exist bands in between them that show none to minimal wrinkling. These phenomena will be juxtaposed to the measured stress-strain curves for a selection of the nanofabrics tested and will be discussed in relationship to existing analytical models [4] and the potential development of further analytical models to describe this response.
[1] Z.-M. Huang, Y.-Z. Zhang, M. Kotaki, and S. Ramakrishna, “A review on polymer nanofibers by electrospinning and their applications in nanocomposites,” Compos. Sci. Technol., vol. 63, no. 15, pp. 2223–2253, 2003, doi: https://doi.org/10.1016/S0266-3538(03)00178-7.
[2] N. E. Zander, “Hierarchically Structured Electrospun Fibers,” Polymers (Basel)., vol. 5, no. 1, pp. 19–44, 2013, doi: 10.3390/polym5010019.
[3] V. Kostopoulos, A. Masouras, A. Baltopoulos, A. Vavouliotis, G. Sotiriadis, and L. Pambaguian, “A critical review of nanotechnologies for composite aerospace structures,” CEAS Sp. J., vol. 9, no. 1, pp. 35–57, 2017, doi: 10.1007/s12567-016-0123-7.
[4] E. Cerda and L. Mahadevan, “Geometry and Physics of Wrinkling,” Phys. Rev. Lett., vol. 90, no. 7, p. 74302, Feb. 2003, doi: 10.1103/PhysRevLett.90.074302
File(s)![Thumbnail Image]()
Name
EMI_2021_abstract_Orestes_Marangos_Stylianos_Yiatros.pdf
Size
45.41 KB
Format
Adobe PDF
Checksum (MD5)
608d990a891b4beb5ee0f6d822654e69