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Preparation and properties of nanopolymer advanced composites: A review  41


                         140
                         130
                         120
                        CAI strength (MPa)  100  3% Clay
                         110


                          90
                                     5% Clay
                                     0% Clay
                          80
                          70
                          60
                          50
                               0   4   8    12  16   20  24   28  32
                                         Impact energy (J)
           Fig. 2.14 CAI strength of composite laminate containing different wt% of nanoclay [29].


              And also, they have concluded that, the presence of nanoclay in the epoxy matrix
           has induced the transition of failure mechanisms of CFRP laminates during the CAI
           test,  from  the  brittle-buckling  mode  to  more  ductile  and  multilayer
           delamination mode.
              Greenetal.[30]haveevaluatedtheflexural,ILSS,andthermomechanicalproperties
           of multiscale fiber-reinforced composites (M-FRCs) based on the carbon nanofibers
           (CNFs) dispersed in an epoxy resin. They have found that, the flexural strength and
           modulus have increased from (16%–20%) and (23%–26%), respectively, for the 0.1
           and 1 wt% M-FRCs, when they are compared with the neat FRCs. The ILSS properties
           increased (6 and 25%) for the 0.1 and 1 wt% M-FRCs, respectively when they are com-
           pared with neat FRCs. The glass transition temperatures (T g ) of both M-FRC samples
           are 25°C higher than the neat FRCs. Coefficients of thermal expansion (CTE) of the
           M-FRC samples have improved when they are compared with the neat FRCs.
              Kostopoulos et al. [31] have investigated the influence of multiwall carbon nan-
           otubes (MWCNTs) on the impact and after impact behavior of carbon fiber-reinforced
           polymer (CFRP) laminates. They have observed that, the delamination area or the
           absorbed energy per unit delamination area; low-velocity impact makes no radical dif-
           ference when directly comparing the neat and the modified specimens for low-energy
           impact levels. The reinforcing effect of the CNTs seems to be more pronounced for
           higher impact energy levels. Therefore, the impact tests have performed with higher
           energy levels or high-velocity impact to investigate the further the effect of the CNTs.
           Fig. 2.15 presents the force responses and energies for the five defined impact energy
           levels for the nonmodified (A) and modified with the addition of CNTs and (B) CFRP
           laminates.
              Hossain et al. [32] have studied the mechanical responses of Treated Jute fiber-
           reinforced Biopol Composites (TJBC) without nanoclay, Treated Jute fiber-reinforced
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