Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates

Thin-ply carbon fiber laminates have exhibited superior mechanical properties, including higher initiation and ultimate strength, when compared to standard thickness plies and enable greater flexibility in laminate design. However, the increased ply count in thin-ply laminates also increases the num...

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Main Authors: Arteiro, Albertino, Borstnar, Gregor, Mavrogordato, Mark N., Sinclair, Ian, Spearing, S. Mark, Camanho, Pedro P., Cohen, Estelle, Kopp, Reed Alan, Furtado Pereira da Silva, Carolina, Ni, Xinchen, Wardle, Brian L
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:en_US
Published: Elsevier 2018
Online Access:http://hdl.handle.net/1721.1/115302
https://orcid.org/0000-0001-6430-428X
https://orcid.org/0000-0002-2260-2374
https://orcid.org/0000-0002-3327-3764
https://orcid.org/0000-0003-3530-5819
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author Arteiro, Albertino
Borstnar, Gregor
Mavrogordato, Mark N.
Sinclair, Ian
Spearing, S. Mark
Camanho, Pedro P.
Cohen, Estelle
Kopp, Reed Alan
Furtado Pereira da Silva, Carolina
Ni, Xinchen
Wardle, Brian L
author2 Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
author_facet Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Arteiro, Albertino
Borstnar, Gregor
Mavrogordato, Mark N.
Sinclair, Ian
Spearing, S. Mark
Camanho, Pedro P.
Cohen, Estelle
Kopp, Reed Alan
Furtado Pereira da Silva, Carolina
Ni, Xinchen
Wardle, Brian L
author_sort Arteiro, Albertino
collection MIT
description Thin-ply carbon fiber laminates have exhibited superior mechanical properties, including higher initiation and ultimate strength, when compared to standard thickness plies and enable greater flexibility in laminate design. However, the increased ply count in thin-ply laminates also increases the number of ply-ply interfaces, thereby increasing the number of relatively weak and delamination-prone interlaminar regions. In this study, we report the first experimental realization of aligned carbon nanotube interlaminar reinforcement of thin-ply unidirectional prepreg-based carbon fiber laminates, in a hierarchical architecture termed ‘nanostitching’. We synthesize a baseline effective standard thickness laminate using multiple thin-plies of the same orientation to create a ply block, and we find an ∼15% improvement in the interlaminar shear strength via short beam shear (SBS) testing for thin-ply nanostitched samples when compared to the baseline. This demonstrates a synergetic strength effect of nanostitching (∼5% increase) and thin-ply lamination (∼10% increase). Synchrotron-based computed tomography of post mortem SBS specimens suggests a different damage trajectory and mode of damage accumulation in nanostitched thin-ply laminates, notably the complete suppression of delaminations in the nanostitched region. Finite element predictions of damage progression highlight the complementary nature of positive thin-ply and nanostitching effects that are consistent with an ∼15% improvement in Modes I and II interlaminar fracture toughness due to the aligned carbon nanotubes at the thin-ply interfaces. Keywords: Thin-ply laminate; Carbon nanotube; Mechanical properties; Finite element analysis
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spelling mit-1721.1/1153022022-09-30T23:45:03Z Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates Arteiro, Albertino Borstnar, Gregor Mavrogordato, Mark N. Sinclair, Ian Spearing, S. Mark Camanho, Pedro P. Cohen, Estelle Kopp, Reed Alan Furtado Pereira da Silva, Carolina Ni, Xinchen Wardle, Brian L Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Massachusetts Institute of Technology. Department of Mechanical Engineering Estelle Kalfon-Cohen Cohen, Estelle Kopp, Reed Alan Furtado Pereira da Silva, Carolina Ni, Xinchen Wardle, Brian L Thin-ply carbon fiber laminates have exhibited superior mechanical properties, including higher initiation and ultimate strength, when compared to standard thickness plies and enable greater flexibility in laminate design. However, the increased ply count in thin-ply laminates also increases the number of ply-ply interfaces, thereby increasing the number of relatively weak and delamination-prone interlaminar regions. In this study, we report the first experimental realization of aligned carbon nanotube interlaminar reinforcement of thin-ply unidirectional prepreg-based carbon fiber laminates, in a hierarchical architecture termed ‘nanostitching’. We synthesize a baseline effective standard thickness laminate using multiple thin-plies of the same orientation to create a ply block, and we find an ∼15% improvement in the interlaminar shear strength via short beam shear (SBS) testing for thin-ply nanostitched samples when compared to the baseline. This demonstrates a synergetic strength effect of nanostitching (∼5% increase) and thin-ply lamination (∼10% increase). Synchrotron-based computed tomography of post mortem SBS specimens suggests a different damage trajectory and mode of damage accumulation in nanostitched thin-ply laminates, notably the complete suppression of delaminations in the nanostitched region. Finite element predictions of damage progression highlight the complementary nature of positive thin-ply and nanostitching effects that are consistent with an ∼15% improvement in Modes I and II interlaminar fracture toughness due to the aligned carbon nanotubes at the thin-ply interfaces. Keywords: Thin-ply laminate; Carbon nanotube; Mechanical properties; Finite element analysis 2018-05-10T19:30:06Z 2018-05-10T19:30:06Z 2018-01 2017-12 Article http://purl.org/eprint/type/JournalArticle 0266-3538 http://hdl.handle.net/1721.1/115302 Kalfon-Cohen, Estelle et al. “Synergetic Effects of Thin Plies and Aligned Carbon Nanotube Interlaminar Reinforcement in Composite Laminates.” Composites Science and Technology (January 2018) © 2018 Elsevier Ltd https://orcid.org/0000-0001-6430-428X https://orcid.org/0000-0002-2260-2374 https://orcid.org/0000-0002-3327-3764 https://orcid.org/0000-0003-3530-5819 en_US https://doi.org/10.1016/j.compscitech.2018.01.007 Composites Science and Technology Creative Commons Attribution-NonCommercial-NoDerivs License http://creativecommons.org/licenses/by-nc-nd/4.0/ application/pdf Elsevier Prof. Kalfon-Cohen
spellingShingle Arteiro, Albertino
Borstnar, Gregor
Mavrogordato, Mark N.
Sinclair, Ian
Spearing, S. Mark
Camanho, Pedro P.
Cohen, Estelle
Kopp, Reed Alan
Furtado Pereira da Silva, Carolina
Ni, Xinchen
Wardle, Brian L
Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title_full Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title_fullStr Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title_full_unstemmed Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title_short Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
title_sort synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
url http://hdl.handle.net/1721.1/115302
https://orcid.org/0000-0001-6430-428X
https://orcid.org/0000-0002-2260-2374
https://orcid.org/0000-0002-3327-3764
https://orcid.org/0000-0003-3530-5819
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