Abstract
This paper presents a novel approach for
introducing aligned carbon nanotubes (CNTs)
at the crack interface of pre-impregnated (prepreg)
carbon fibre composite plies, creating a
hierarchical (three-phase) composite structure.
The aim of this approach is to improve the
interlaminar fracture toughness. The developed
method for transplanting the aligned CNTs
from the silicon wafer onto the pre-preg
material is described. Scanning electron
microscopy (SEM) was used to analyse the
effects of the transplantation method. Double
Cantilever Beam (DCB) specimens were
prepared, according to ASTM standard D5528-
01R07E03 [1] and aligned multi-walled carbon
nanotubes (MWCNTs) were introduced at the
crack-tip. Mode I fracture tests for pristine
(control) specimens and CNT-enhanced
specimens were conducted and an average
increase in the critical strain energy release
rate (GIc) of approximately 50 % was achieved.
Original language | English |
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Number of pages | 9 |
Publication status | Published - 28 Sept 2012 |
Event | 28th International Congress of the Aeronautical Sciences - Brisbane, Australia Duration: 23 Sept 2012 → 28 Sept 2012 |
Conference
Conference | 28th International Congress of the Aeronautical Sciences |
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Country/Territory | Australia |
City | Brisbane |
Period | 23/09/2012 → 28/09/2012 |