Introduction

Carbon-reinforced epoxy resin composites are often used in aircraft. Because of their high specific mechanical properties, they are mainly used as structural components. Epoxy resin is sometimes used as a matrix material in these composites. Graphene nanoplatelets (GnPs) and multi-walled carbon nanotubes (MWCNTs) are new carbon materials that have recently been developed. Graphene has generated much more interest due to its high specific area and novel mechanical, electrical and thermal properties. (Higginbotham et al. 2010; Stankovich et al. 2006; Jiao et al. 2009; Kosynkin et al. 2009; Li et al. 2008; Wang et al. 2009; Rafiee et al. 2010; Han et al. 2007) combined high electrical conductivity with record of thermal conductivity and mechanical properties. Used as additives, they can impart their properties to the materials and coatings they are added to. They have countless potential applications, some of which we cannot even begin to imagine today (Chen et al. 2007; Iijima 1991; Sinnott and Andrews 2001).

Carbon nanotubes are the most promising 1D material for nanotechnology, optical, electronic and composite material applications. Advances in carbon nanotube growth technique led to considerable increases in both production rates. Nanotube synthesis by CVD process was chosen because it offers a promising method to bulk production of high-purity nanotube that can be carried to commercialization. Useful composite research requires a bulk supply of nanotube of high purity and in a useable (i.e. easily dispersible) form. Existing technologies for the production of single-walled carbon nanotube (SWCNT) do not yield sufficient quantities and lack the required purity. Purification of these materials is often tedious, low in yield, and damaging to the tubes’ structure through oxidative shortening. For applications such as conductive filler or as reinforcing fibre, MWCNT is likely to be preferred over SWCNT on a cost basis. Also, technologies developed for MWCNT applications can be directly transferred to SWCNT composites should SWCNT synthesis reach industrial scale (Gojny et al. 2005).

One of the most promising applications of MWCNT and GnP materials is in polymer composite, which incorporates nano-scale filler materials. Polymer composites show substantial property enhancements at much lower loadings than polymer composites with conventional microscale fillers (such as glass or carbon fibre), which ultimately results in lower component weight and can simplify processing; moreover, the multifunctional property enhancements made possible with composites may create new applications of polymers (Dassios et al. 2012; King et al. 2013; Singh et al. 2013).

The main objective of the present work was to compare the mechanical properties of GnP/epoxy resin and MWCNT/epoxy resin composites with the variation of weight percentage ratio of nanofillers ranging from 0.5, 1.0, 2.0 and 3.0.

Experimentation

Materials and specimen preparation

Graphene nanoplatelet and multi-walled carbon nanotube were used as filler materials. Graphene nanoplatelet was obtained from J. K. Impex Company, Mumbai with 99.5 % purities. Multi-walled carbon nanotube was available from TUHH, Harburg, Hamburg, Germany. Epoxy resin was obtained from Ciba-Geigy Ltd., Mumbai. The material properties are listed in Table 1.

Table 1 Material properties

First, araldite (LY-556) 55 %, hardener (HY-917) 49 % and accelerator (DY-070) 0.28 % were used as epoxy resin matrix. MWCNT filler was used as reinforcement in epoxy resin with weight percentage variation of MWCNT filler ranging from 0.5, 1.0, 2.0 and 3.0. MWCNT particle was manually mixed with the resin (LY-556). MWCNT filled resin was dispersed using a lab-scale three-roll-mill (Exakt 120 EXAKT Advanced Technology GmbH, Germany), which enables the introduction of very high shear forces (up to 200,000/s) throughout the suspension. The curing time 20 min is allowed to cure the specimen. The pre-dispersed suspension was then given batchwise onto the roll with dwell times of 2 min. The dispersive forces on the suspension were acting in the gap (5 µm) between the rolls. After dispersion of the MWCNT in the resin LY-556, the hardener and accelerator were usually added in a vacuum dissolver, to avoid trapped air in the suspension. Then the mixture was placed in a vacuum chamber for 20 min to eliminate the bubbles introduced during the rolling process. The dispersed mixtures of MWCNT and resin were subsequently diluted by adding an appropriate amount of hardener (HY-917) in the weight ratio of 10:1. Again, MWCNT/epoxy resin mixture was dispersed by the same method and air bubble removed completely from the mixture before curing.

In this paper, we were considered to differentiate between mechanical properties of MWCNT/epoxy resin composite and GnP/epoxy resin composite with the same percentage of fillers. For this objective, GnP composite was manually mixed with the resin and then mixer was placed in the mechanical stirrer at the speed of 1 m/min for 1 h. After proper dispersion of graphene nanoplatelet in the resin, hardener was added to the weight ratio of 10:1. Again, mixture of graphene nanoplatelet (weight percentage variation of ranging from 0.5, 1.0, 2.0 and 3.0) added to the resin and hardener was gently mixed with the stirrer and allowed removing the air bubble from the mixture. Finally, GnP/epoxy resin mixture was placed in vacuum for 20 min to escape out the bubbles introduced during the mixing process. The dispersed mixtures were poured into the mould and allowed curing the mixture for 24 h. After curing, tensile, compressive, Izod and Charpy impact test specimens were prepared as per the ASTM standard for the measurement of mechanical properties.

Mechanical tests

Mechanical properties of the MWCNT/epoxy resin and GnP/epoxy resin composites were measured under tensile, compression, Izod and Charpy impact tests. The shape and size of the specimens were prepared according to the ASTM standard (Dassios et al. 2012). A dog bone-shaped tensile specimen size of 165 × 5.3 × 3 mm was used. The compression specimen size (25 × 7 × 6.5 mm) was used in short length to avoid the buckling effect. These tests were performed on the universal testing machine (UTM-5T; SC Deys & Company, Calcutta) with the cross-head speed of 0.05 mm/min. Load versus displacement results were used to measure elastic modulus under the tensile and compressive loading conditions. At least five specimens were tested for each sample with the variation of 10 %. The tensile strength, compressive strength and elastic modulus are reported on average.

The impact test was performed with instrumented Izod and Charpy equipment (Model; Resil Impactor-50, CEAST, S. p. A., Italy). The impact hammer and vice lever with specimen adapter were used different in Izod and Charpy impact tests. The impact length and impact velocity were 0.327 m and 3.46 m/s. Izod and Charpy impact tests were performed on notched and un-notched sandwich specimens. The dimensions of Izod impact test were length 66 mm, width 20 mm, thickness 18 mm. Charpy impact test dimensions are length 123 mm, width 20 mm and thickness 18 mm. A V-notch of depth 2 mm was introduced in Izod and Charpy impact test specimens.

Microstructure observation and surface analysis

The morphologies of the fractured specimens of graphene nanoplatelet/epoxy resin and MWCNT/epoxy resin composites were observed by scanning electron microscope (High resolution SEM SUPRA 40, 5 kV, Zeiss, Germany). TEM (Jeol JEM-2100, HR) was carried out to characterize the structure of nanotubes. To prepare TEM samples, some alcohol was dropped on the nanotubes film, then, these films were transferred with a pair of tweezers to a carbon-coated copper grid.

Results and discussion

The SEM and TEM images of nanofiller are presented in Figs. 1, 2, 3. Figures 1, 2 clearly indicate that the nanofillers are well dispersed within the epoxy resin. It is obvious, from the images that all the nanofillers are hollow and tubular in shape as shown in Fig. 3a. In some of the images, catalyst particles can be seen inside the nanotubes. TEM images indicate that the nanotubes are high purity, with uniform diameter distribution and contain no deformity in the structure. While Fig. 3b shows the GnP particles interact well with each other at magnification of 20 nm. This indicates that the GnP particles are dispersed uniformly within the epoxy resin.

Fig. 1
figure 1

SEM image of graphene nanoplatelet particles

Fig. 2
figure 2

SEM image of MWCNT particles

Fig. 3
figure 3

TEM micrograph shows that interact with each other a MWCNT particles, b GnP particles

To measure the influence of MWCNT and GnP nanofiller on mechanical properties of epoxy resin matrix, the samples with specific size of composite were prepared according to the requirements of tensile, compressive, Izod impact and Charpy impact tests. The tensile strength and compressive strength were obtained based on the maximum load. Figures 4, 5 show that the tensile strength and compressive strength increase with increase of weight percentage of nanofillers. The tensile strength and compressive strength of GnP/epoxy resin composite specimen give better strength compared to neat epoxy resin and MWCNT/epoxy resin composite specimens. However, the proper dispersion of nanofillers has great effect on the mechanical properties of the epoxy resin. The tensile strength and compressive strength of epoxy resin were increased about 20 and 31 % with the addition of GnP filler, whereas tensile strength and compressive strength of epoxy resin were increased about 18 and 19 % with the addition of MWCNT filler. These results clearly indicate that the nanofiller improve the tensile and compressive strength of epoxy resin. The results are parallel to other reported works (Dassios et al. 2012; King et al. 2013). It is now well known that the mechanical properties of nanofiller-filled polymer matrix, especially the strength and modulus depend to a great extent on filler dispersion and interfacial interaction. Modulus measurement by nanohardness followed the trends reported in the literature for polymers, that is, the modulus obtained was higher than the results obtained from macroscopic testing (King et al. 2013; Singh et al. 2013).

Fig. 4
figure 4

Variation of tensile strength with weight percentage of nanofillers

Fig. 5
figure 5

Variation of compressive strength with weight percentage of nanofillers

Izod impact and Charpy impact test results are shown in Figs. 6, 7. Also, dynamic fracture toughness (αk) was calculated using the following equation (Gojny et al. 2005),

Fig. 6
figure 6

Variation of Izod impact energy with weight percentage of nanofillers

Fig. 7
figure 7

Variation of Charpy impact energy with weight percentage of nanofillers

$$ \alpha_{\text{k}} = \Delta E/wh, $$
(1)

where ΔE is the absorbing energy of material during impact processing, w and h are the width and thickness of specimen, respectively.

The impact tests result shows that the MWCNT/epoxy resin composite gave higher Izod impact energy, Charpy impact energy, dynamic fracture toughness (Izod) and dynamic fracture toughness (Charpy) compared to GnP/epoxy resin composite and neat epoxy resin specimen as indicated in Figs. 6, 7, 8, 9.

Fig. 8
figure 8

Variation of dynamic fracture toughness with weight percentage of nanofillers under Izod impact energy

Fig. 9
figure 9

Variation of dynamic fracture toughness with weight percentage of nanofillers under Charpy impact energy

Figures 6, 7 indicate the variation of Izod impact energy and Charpy impact energy with the percentage of filler ratio. The higher impact resistance clearly represents that the multi-walled nanotube absorbed more energy and it is dissipated within the area of nanotubes and take more time to penetrate the more area of the specimen (Singh et al. 2013). But, in the case of graphene nanoplatelets, impact energy spread easily all over the specimen because graphene nanoplatelets dispersed in the plate form. The reduced in absorbed energy may be caused by stress concentration in the vicinity of the graphene nanoplatelet (Chen et al. 2007); this typically occurs when hard fillers are incorporated into a brittle matrix. Besides, agglomeration of MWCNT/epoxy resin or GnP/epoxy resin composites can lead to defects in the matrix that can act as seed points for crack initiation and premature fracture (Dassios et al. 2012; King et al. 2013).

Figures 8, 9 show the variation in dynamic fracture toughness under Izod and Charpy impact tests, which indicates the material toughness of neat epoxy resin, MWCNT/epoxy resin and GnP/epoxy resin composites. MWCNT/epoxy resin composite shows higher dynamic fracture toughness than the neat epoxy resin and GnP/epoxy resin composite. This result is evident that the lower weight fractions of nanofillers begin to agglomerate in epoxy resin. Figure 10 shows that MWCNT particle is well dispersed in epoxy resin, which indicates that the three mill rolling process is most suitable for dispersion of MWCNT in epoxy resin (Sinnott and Andrews 2001).

Fig. 10
figure 10

SEM micrographs showing the dispersion of MWCNTs in epoxy resin

However, GnP nanofiller is not fully dispersed because of stirrer mixing process, as shown in Fig. 11. This highlights the need for continued research to develop new methods to enhance GnP dispersion at higher weight fraction (Han et al. 2007).

Fig. 11
figure 11

SEM micrographs showing the dispersion of GnPs in epoxy resin

To understand the underlying mechanisms that are responsible for the improved performance of GnPs, we compared the thermal and microstructure chemistry of GnPs/epoxy resin and MWCNT/epoxy resin by TGA and SEM analysis. We find that the MWCNT and GnP filler can be affected with the temperature due to variation in weight loss, as shown in Fig. 12. It is observed from the Fig. 12 that the nanocomposite made with MWCNT/epoxy resin can increase the initial decomposing temperature than the GnP-filled epoxy resin composite.

Fig. 12
figure 12

Variation of weight loss with temperature

This means the percentage weight loss reduces abruptly with increase of temperature. MWCNT/epoxy resin composite could significantly enhance interfacial interaction between the MWCNT and epoxy resin matrix in composites (Singh et al. 2013). Where, GnP/epoxy resin composite reduces the stability of the composite at higher temperature, because GnP molecules can be retarded under high temperature. Therefore, dispersion of nanofillers can be improving the thermal stability of nanocomposites (Iijima 1991). But a noticeable increase in decomposition temperature was observed with incorporation of 2 % MWCNT and GnP filler in epoxy resin. This was solely attributed to the synergistic effect of the composite structure formed between MWCNT and epoxy resin, as shown in Fig. 10. The increase through the synergistic effect was more than the composite containing GnPs (0.5 %), but considerably smaller compared to the composite containing 2 % MWCNT. The likely possibility for this low increase compared to a binary system containing 2 % MWCNT may be due to the effective low concentration of GnPs (0.5 %) in the epoxy resin. Another possible reason may be due to the fact that the high thermal conductivity of the MWCNT/epoxy resin composites resulted in a greater flow of heat throughout the sample. GnP/epoxy resin and MWCNT/epoxy resin composites started to lose weight as temperature increases continuously (Dassios et al. 2012) as indicated in Fig. 12.

Figure 13 shows SEM images of the fracture surfaces of GnP/epoxy resin composites. These composite fails in catastrophic mode. Figure 13a, b shows the fracture surface of the polymer composites made with GnPs, this clearly indicate that the epoxy resin fractured as a catastrophic pattern, because epoxy resin becomes more brittle due to addition of nanofillers. This shows the fracture surface of composite made with graphene nanoplatelet. Micrographs indicate that the cracks were propagated at different planes and continued all around the specimen. Once cracks started, they spread quickly along the crack direction and then developed into macroscopic failure. Also, dispersion and agglomeration graphene nanoplatelet were clearly identified from the Fig. 13c, d. In most cases, the crack damage started from the interface, and then nanofillers suffered from the external force and were pulled out, leaving the smooth resin matrix which exposed the weak interfacial bonding. It was discovered that there were many CNT existing in the surrounding agglomerates, which might have been caused by the shear force around the nanofillers during the fabrication process, or by poor dispersion (Singh et al. 2013). However, the morphology of fractured surfaces depicts the intimate contact and high embedding with polymer matrices, indicating good interfacial bonding between nanofillers and the epoxy resin. This further confirms that the presence of hydroxyl groups on graphene nanoplatelet surfaces has a strong interaction with the epoxy resin and significantly improves adhesion at interfaces. In general, nanoplatelets can be easily attracted to each other due to their very high specific area and high surface energy, due to these properties, tensile and compressive strength of GnP/epoxy resin composite give more value compared to MWCNT/epoxy resin composite (King et al. 2013).

Fig. 13
figure 13

SEM micrograph showing a microcracks formed in the resin area and b cracks formed around the graphene platelets, c graphene nanoplatelets agglomerated in the epoxy resin and d graphene nanoplatelets sticked with resin-like mushroom

Conclusion

Based on the experimental observation, the results clearly indicate that the GnP and MWCNT nanofiller can improve the performance of epoxy resin. The tensile strength and compressive strength of GnP/epoxy resin composite are higher than those of the MWCNT/epoxy resin composite with the variation of weight percentage of nanofiller ranging from 0.5, 1, 2 and 3. Whereas, MWCNT/epoxy resin composite gives higher impact resistance compared to GnP/epoxy resin composite at the same variation of nanofiller. The results of this study suggest that MWCNT plays an important role of absorbing the impact resistance because nanotube dampens the more energy compared to graphene nanoplatelet. On the other side, tensile strength and compressive strength of GnPs/epoxy resin increase due to more surface area and significant increase in the interfacial contact area of graphene nanoplatelet compared to multi-walled carbon nanotube. The GnPs are more effective than MWCNT, which contributes to better interfacial binding. These results indicate that GnPs show significant potential as a structural reinforcement additive in polymer-based composite materials.