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Fig. 1 The SEM images of the carbonized composites at various temperatures in argon atmosphere.
Fractographic analysis figured out various failure modes in all composites at various temperatures.
Fig. 7 XRD patterns of a GNS, neat PVA, 200 % drawn PVA, b GNS-PVA composites at various filler fractions.
The impact and post-impact (CAI) behavior of hybrid composites at various impact energies were investigated.
Open image in new window Fig. 3 Volumetric shrinkage of carbon and basalt fibre reinforced fly ash geopolymer composites at various elevated temperatures.
Open image in new window Fig. 4 Mass loss of carbon and basalt fibre reinforced fly ash geopolymer composites at various elevated temperatures.
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Later, the experimentally determined mechanical properties of the composite at various percentage compositions of the date palm wood fibre and at various particle sizes were used to train an ANN; the trained ANN was later used to predict the mechanical properties of the composite at various percentage compositions of the date palm wood fibre and at various particle sizes.
Figure 8c shows the charge/discharge profiles of the V/GO-I composite at various rates.
Open image in new window Fig. 3 TEM (a) and galvanostatic cycling (b) of FeF3·0.33H2O/RGO composite at various C rates.
Figure 5d displays the charge discharge curves of the Co3O4-0.5/MWCNT Co3O4-0.5/MWCNTrious compositeensities in the ratge of 0.5 to 1.5 Ag−1.
Open image in new window Figure 17 Compressive stress-strain responses of the SiCp/Al-5Cu composite at various strain rates (Lu et al. 1999 ).
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