1. Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates
- Author
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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, and Camanho, Pedro P.
- 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
- Published
- 2018