Post oblique ballistic impact behaviour of hybrid composite plates reinforced with carbon nanotubes
The present experimental investigation endeavoured to examine the tensile, compression, and 3-point bending strength of the laminates made of carbon/Kevlar hybrid reinforced textiles with carbon nanotubes (CNTs) fillers subjected to oblique ballistic impact loads. The advanced nano-fillers were c...
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Main Author: | |
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Format: | Thesis |
Language: | English |
Published: |
2022
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Subjects: | |
Online Access: | http://psasir.upm.edu.my/id/eprint/104056/1/FK%202022%2099%20IR.pdf http://psasir.upm.edu.my/id/eprint/104056/ |
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Institution: | Universiti Putra Malaysia |
Language: | English |
Summary: | The present experimental investigation endeavoured to examine the tensile,
compression, and 3-point bending strength of the laminates made of carbon/Kevlar
hybrid reinforced textiles with carbon nanotubes (CNTs) fillers subjected to oblique
ballistic impact loads. The advanced nano-fillers were chosen as reinforcement for the
carbon/Kevlar hybrid textile composite because of their high Young's modulus.
Although there are a number of experimental investigations on tensile properties of
CNTs, the coupling effects of CNTs and oblique impacts on tensile, compression, and 3-
point bending strengths have not been examined yet. Consequently, individual oblique
impacts ranging from 0 to 40 degrees were conducted on the composite plates made-up
of fabrics with diverse volumes of CNTs, which ranged from 0.1% to 1.5%. The plates
were fabricated with eight layers of equal thickness arranged in different percentages of
CNTs and neat epoxy resin. A conical steel projectile at dimensions of 15 mm length and
10 mm diametre was considered for a high velocity impact. While the projectile was
placed very close to the plates, i.e. at their centres, they were impacted at sundry speeds.
The modulus of elasticity and toughness were calculated for the stress-strain curves
obtained from the mechanical tests. In the progress of the experiments, the variation of
the kinetic energy, the increase in the internal energy of the laminates, and the decrease
in the velocity of the projectile with disparate angles were examined. Results from the
experimental tests indicated that the kinetic energy absorption of the projectile increased
by 38% with the increase of the oblique angle of 40 degrees at 0.3% CNTs' desperation.
The optimum dispersion of the CNTs fillers was 0.3% and by adding the CNTs, the
kinetic energy absorption increased by about 35%. Additionally, the inclusion of the
CNTs' fillers by 1.5% resulted in improving the compressive toughness of the specimens
more than triple times. The increase of CNTs fillers by 1.5% caused the decrease of the
tensile strength and toughness by 86%. Moreover, the incorporation of 1.5% of CNTs
caused the increase of the flexural bending toughness of the specimens more than four
times. Simultaneously, the flexural modulus of elasticity decreased by up to 38%. The
incorporation of CNTs by 1.5% increased the flexural bending toughness more than four
times; however, the flexural modulus of elasticity decreased by up to 38%. |
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