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Static and fatigue interlaminar shear reinforcement in aligned carbon nanotube-reinforced hierarchical advanced composites

Title
Static and fatigue interlaminar shear reinforcement in aligned carbon nanotube-reinforced hierarchical advanced composites
Type
Article in International Scientific Journal
Year
2019
Authors
Ni, XC
(Author)
Other
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Furtado, C
(Author)
FEUP
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Kalfon Cohen, E
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Zhou, Y
(Author)
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Valdes, GA
(Author)
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Hank, TJ
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Camanho, PP
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Wardle, BL
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Journal
Vol. 120
Pages: 106-115
ISSN: 1359-835X
Publisher: Elsevier
Other information
Authenticus ID: P-00Q-9G5
Abstract (EN): High densities (>10 billion fibers per cm(2)) of aligned carbon nanotubes (A-CNTs) are used to reinforce the interlaminar resin-rich region of aerospace-grade unidirectional carbon microfiber plies in a hierarchical carbon fiber reinforced plastic (CFRP) laminate architecture. Such nano-engineered interfaces have been shown to increase interlaminar fracture toughness and substructural in-plane strengths, and here we show a 115% average increase in fatigue life across all load levels (60-90% of static strength), with a larger increase of 249% in high-cycle (at 60% of static strength) fatigue, despite no statistically significant increase in static strength. These findings are in agreement with a numerical damage progression model developed to simulate both interlaminar and intralaminar damage in the laminates, which shows the relative insensitivity of short-beam shear (SBS) strength to the enhancement of interlaminar fracture toughness, e.g., a 50% increase in interlaminar toughness yields an SBS strength increase of less than 20%. Consistent with observations of other CNT-reinforced epoxy architectures, larger improvements in fatigue life are noted in low-stress regimes (e.g., high-cycle fatigue) vs. in high-stress regimes (e.g., static and low-cycle fatigue), indicating a transition in dominant mechanisms from high-energy dissipation caused by CNT pullout to low-energy dissipation caused by CNT fracture as stress increases.
Language: English
Type (Professor's evaluation): Scientific
No. of pages: 10
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