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

Authors :
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
Arteiro, Albertino
Borstnar, Gregor
Mavrogordato, Mark N.
Sinclair, Ian
Spearing, S. Mark
Camanho, Pedro P.
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
Arteiro, Albertino
Borstnar, Gregor
Mavrogordato, Mark N.
Sinclair, Ian
Spearing, S. Mark
Camanho, Pedro P.
Source :
Prof. Kalfon-Cohen
Publication Year :
2018

Abstract

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

Details

Database :
OAIster
Journal :
Prof. Kalfon-Cohen
Notes :
application/pdf, en_US
Publication Type :
Electronic Resource
Accession number :
edsoai.on1037801278
Document Type :
Electronic Resource