Heat transfer enhancement of water-based highly crumpled few-layer graphene nanofluids

Ahmad Amiri*a, Goodarz Ahmadib, Mehdi Shanbedi*c, Mohammadmahdi Etemadic, Mohd Nashrul Mohd Zubira, B. T. Chewa and S. N. Kazi*a
aDepartment of Mechanical Engineering, University of Malaya, Kuala Lumpur, Malaysia. E-mail: ahm.amiri@gmail.com; salimnewaz@um.edu.my
bDepartment of Mechanical and Aeronautical Engineering, Clarkson University, Potsdam, NY 13699, USA
cDepartment of Chemical Engineering, Faculty of Engineering, Ferdowsi University of Mashhad, Mashhad, Iran. E-mail: mehdi.shanbedi@stu-mail.um.ac.ir

Received 7th September 2016 , Accepted 18th October 2016

First published on 25th October 2016


Abstract

Backward-facing step heat transfer of transitional and turbulent flows occurs in many industrial applications. The heat transfer performances of different multiphase working fluids over a backward-facing step in the transitional and turbulent flow regimes, however, have not been fully investigated experimentally. Recently, highly crumpled few-layer graphene (HCFLG) with a high surface area has been introduced as a promising additive for preparing nanofluids for high performance heat transfer applications. In this work, the heat transfer properties of the HCFLG nanofluids were studied experimentally. The HCFLG was prepared by exfoliation of graphite in the presence of liquid-phase using microwave-assisted methods, which was shown to be industrially-scalable, cost-effective, and simple. Then the HCFLG was used for fabricating a new class of water-based graphene nanofluid for use in large-scale heat transfer equipment. The prepared water-based HCFLG nanofluids were shown to be stable with less than 2% sedimentation after 30 days. In addition, the measured thermophysical properties indicated that the water-based HCFLG nanofluids have huge potential for high performance heat transfer applications. Finally, the water-based HCFLG nanofluids were shown to be significantly more effective in the duct with a backward-facing step in terms of overall thermal performance including the local Nusselt number (Nu), convective heat transfer coefficient, performance index, pumping power, and rheological properties such as effective viscosity in comparison to distilled water.


1 Introduction

Using different base fluids including water and ethylene glycol, many studies have been performed on dispersing various types of carbon based-nanostructures, such as single-walled carbon nanotubes,1,2 multi-walled carbon nanotubes,3 graphene4 and nitrogen-doped graphene5 for synthesizing highly-conductive nanofluids. The unique properties of few-layer graphene have attracted the attention of a large number of scientists in different fields.6 In particular, its large specific surface area and outstanding thermal conductivity at room temperature make few-layer graphene an ideal material for heat transfer applications and for the fabrication of superconductive capacitors. Developing an efficient and quick method for mass-production of few-layer graphene, however, is critical for its large-scale industrial applications such as for developing high performance nanofluids. It is also well known that thermal conductivity and subsequently heat transfer rate improve as the specific surface area of graphene increases.7 Therefore, in order to manufacture highly-conductive nanofluids for improving the heat transfer rate in different thermal equipment, materials with high specific surface areas, such as crumpled graphene, and in particular, few-layered graphene are used. Crumpling the 2D graphene by chemical treatment can be used as an approach to achieve materials with high specific surface area and pore structures. Thus, highly-crumpled few-layer graphene (HCFLG) with a large specific surface area seems to have the ideal properties.

There are, however, a number of challenges. To fully exploit the properties of graphene with a large specific surface area as an additive in base fluids requires a method for the mass production of this remarkable material. The second problem is the lack of stability of carbon-based nanostructures in aqueous media. To solve the first problem, numerous studies have been performed. As a large-scale exfoliation technique, the production of chemically converted graphene from the reduction of graphene oxide is a convenient method to obtain large amounts of graphene;8 however, even with efficient reducing agents such as hydrazine or H2, and annealing at high temperature, the original crystalline structure of graphene is not restored, reducing all its unique properties. Also, graphene oxide is heavily functionalized with many permanent chemical defects, such as holes, introduced into the basal plane. These holes are not readily healed even upon annealing.8–11 As a new method to overcome the above-mentioned defects, the liquid phase exfoliation of graphite in the presence of high surface-tension organic solvents, along with continuous sonication,12,13 opened a new gateway to achieving few-layered graphene.

There are, however, other issues. The π–π interactions lead to a high level of aggregation and the liquid-phase exfoliated graphene cannot reach stable dispersion in base fluids.11 However, due to the lack of graphene-solubility, the exfoliation performances of most of the solvents used in previous studies14 were quite low. To increase the efficiency of exfoliation with this method and to solve the problem of low stability, in situ chemical functionalization and exfoliation of graphite with different functional groups, such as 4-bromophenyl, was used, providing a new approach for improving its solubility in polar, aprotic, organic solvents.15 For example, Sun et al.11 concluded that graphite can be changed to graphene by covalent functionalization of the graphite and the synthesis of a stable suspension in the presence of DMF without any added surfactant or stabilizer. Also, they achieved both exfoliation and functionalization by a fast procedure and obtained suitable edge-functionalization and an intact pristine graphene structure in the interior basal planes. Thus, finding a method for mass-production of HCFLG with hydrophilic functional groups to prepare highly-stable nanofluids is one major goal of this study.

The availability of highly-stable superconductive nanofluids opens a new gateway for an economical increase in the performance of thermal loops in industrial applications. Ducts and channels with abrupt expansion are broadly applied in different industrial applications and heat transfer equipment. These include passages of turbine blades, combustors, diffusers, and heat exchangers. Due to the mixing of high and low energy fluids in the flow reattachment zone, the rate of heat transfer along with other thermal parameters are affected in the back-step flows. In particular, in the reattaching flow region, momentum, mass and heat transfer vary significantly due to the presence of reverse flows.16 There have been many, mostly numerical, studies performed in the literature to determine the effects of different parameters on the heat transfer performance as well as to identify the actual mechanism of flow separation and reattachment.16–20

It is now known that one efficient way to increase the heat transfer rate in the separated flow regions is to use highly-conductive working fluids.21–25 To take advantage of this potential, numerous researchers have been employing different suspensions of metal and metal oxide nanoparticles.25,26

Abu-Nada27 was one of the pioneers in studying the heat transfer of nanofluids in a backward-facing step flow. He synthesized CuO-, Al2O3-, Ag-, Cu- and TiO2-based water nanofluids and investigated the rate of convective heat transfer enhancement for various nanofluids with different thermal conductivities. He concluded that the thermo-physical properties of the nanofluids – in particular the thermal conductivity – play the key roles in increasing the Nusselt number, particularly inside the recirculation zone.

In similar work, Mohammed et al.28,29 studied the effects of different nanofluids on the mixed convective heat transfer coefficient in vertical and horizontal backward-facing steps. According to their results, the nanofluids with secondary recirculation regions have lower Nusselt numbers and the diamond-based water nanofluids showed a significant enhancement in Nusselt number. More recently, Kherbeet et al.30 studied the heat transfer rate of Al2O3-, CuO-, SiO2- and ZnO-based water nanofluids in the laminar flow regime over a microscale backward-facing step. They reported that there was no recirculation region behind the step for all four nanofluids at various concentrations. They concluded that a SiO2-based water nanofluid showed the best performance among their prepared nanofluids.

Literature reviews of applications reveal that the majority of previous studies on the heat transfer over a backward-facing step used a water-based suspension of metal or metal oxide nanofluids, and the lack of highly-conductive nanofluids, including few-layered graphene, with high stability and specific surface area is obvious. Also, they were also mostly focused on heat transfer of the laminar regime and there is no study on transition, or turbulent flow regimes over a backward-facing step. Thus, discovering the heat transfer behavior of water and highly-conductive nanofluids in transition and turbulent flow regimes is the second target of this study.

To this end and covering the aforementioned targets, three phases of study have been performed to investigate the heat transfer behavior of water-based highly crumpled few-layer graphene nanofluids as well as water over a backward-facing step. First of all, a quick and efficient functionalization procedure was developed to fabricate highly-crumpled, few-layer graphene (HCFLG) flakes with large specific surface area. Also, the method of synthesizing HCFLG seems to be new, simple, cost-effective, and with the capability of mass-production. The HCFLG materials with a nanoscopic porous morphology have a high specific surface area, based on BET analyses of the nitrogen cryo-adsorption method. The morphology and structure of HCFLG were analyzed thoroughly. Secondly, water-based HCFLG nanofluids for different low weight concentrations were prepared, and thermophysical properties and colloidal stability in the presence of a non-covalent functional group were investigated. Lastly, heat transfer parameters such as the Nusselt number (Nu) and the convective heat transfer coefficient (h) over a backward-facing step in both of the transitional and turbulent flow regimes were investigated for water-based HCFLG nanofluids and compared with water as the base fluid. The results suggest that the water-based HCFLG nanofluid is a highly conductive nanofluid at very low weight concentration.

2 Material and methods

2.1. Exfoliation and functionalization

In order to prepare HCFLG, 10 mg of bulk graphite and 30 mL of deionized water were mixed in a 100 mL vessel. After adding cyanamide (4 equiv. per graphite C) and isoamyl nitrite (2 equiv. per graphite C), the reaction vessel was sonicated for 1 h. Then, the contents were transferred into a Teflon vessel and put under microwave irradiation at 600 W for 1 h. Then the mixture was mixed vigorously with a Pyrex-coated stir-bar at 80 °C overnight for 12 h. After cooling to room temperature, the mixture was filtered and washed with deionized water and acetone, to produce semi-stable diazonium ions, resulting in a radical reaction with the graphite flakes and the production of amino-functionalized graphite. Having high-dispersibility due to the functional group, the filtrated cake was sonicated for 1 h in dimethylformamide (DMF). The resulting black ink-like dispersion was allowed to sit for 24 h to separate the large, unstable graphite aggregates. The dispersed cyanamide-treated graphene was collected using low-speed centrifugation (2000 rpm). The centrifuged supernatant was dried. The resulting HCFLG, comprised of graphene flakes, was stored for further treatment. The mechanism for the exfoliation of the bulk graphite to HCFLG comprises the generation of semi-stable diazonium ions, which then initiate a radical reaction with the flakes. The treated graphite with higher dispersibility in DMF has more chance to expand in severe sonication conditions. It is obvious that the edges of the bulk graphite are more accessible for diazonium reaction than the interior basal plane surfaces that are stacked with strong π–π interactions.11 To synthesize water-based HCFLG nanofluids, the HCFLG was mixed with Gum Arabic by a ratio of 0.5[thin space (1/6-em)]:[thin space (1/6-em)]1 and then poured into a vessel filled with a given amount of water and finally sonicated with a probe-sonicator for 10 min.

2.2. Experimental test-rig

Fig. 1 illustrates the experimental set-up of the present study, which includes a flow loop, heating and cooling sections, measuring instruments, and data acquisition and control units. The flow loop consists of a magnetic flow meter, tank, pump, differential pressure transmitter, electromagnetic flow meter and the test section. To obtain raw data, a Cole-Parmer™ magnetic drive pump was used to pump different working fluids from a stainless steel jacketed tank with capacity of 20 L. Meanwhile, the flow rate was controlled by a Hoffman Muller™ inverter. In order to measure the flow rate and pressure loss, a N-FLO-25 Electromagnetic flow meter and a Foxboro™ differential pressure transmitter were used. Also, a PLC control system was employed in the present test-rig and WINCC software was used for recording and analyzing the input and output temperatures.
image file: c6ra22365f-f1.tif
Fig. 1 Schematic of the experimental setup.

The geometrical dimensions of the tube were 12.7 mm inlet diameter, 800 mm upstream length, 25.4 mm outlet diameter and 800 mm downstream length for an expansion ratio of 2. At the test section, the downstream part was a heated straight stainless steel tube, while all the other walls were insulated. The test section was also heated by using two programmable DC power supplies with outputs of 8 V and an output current of 600 A with maximum power of 1200 W. Sixty K-type thermocouples (Omega) were installed on the test section by using high temperature epoxy glue on the outer surface of the test section, as shown schematically in Fig. S1 (ESI). The positioning of the thermocouples on the outer surface of the cylindrical tube is shown schematically in Fig. S1. The thermocouples were flush mounted to avoid interaction with the flow boundary layer originating from the thermocouple probe protruding into the conduit inner surface. Furthermore, two RTD (PT-100) sensors (Omega) were used to measure and record the working fluid inlet and outlet temperatures. All of the thermocouples as well as RTDs were calibrated with the use of an Ametek temperature calibrator (AMETEK Test & Calibration Instruments, Denmark). The RTDs and thermocouples were connected to the PLC and SCADA system for the continuous monitoring and recording of the temperature data by WINCC software in a computer. To eliminate or minimize the amount of heat loss, two thick layers of white glass wool wrapping were used, and rubber insulation dressing was also applied. Two K-type thermocouples were installed on the outermost surface of the insulation to measure the amount of heat loss. Moreover, all the pipes were wrapped with rubber insulation to reach a steady state condition in terms of temperature at a given flow rate. Note that conduction and convection heat transfer occur simultaneously in the present system. Therefore, a further calibration test was needed to determine the exact temperature at the inner surface of the test section. Therefore, a Wilson plot was used for this purpose. The inlet temperature of the bulk fluid and the heat flux at different locations “x” of the duct were formulated, as mentioned in the Data processing section.

3 Data processing

Experimental measurements of the thermophysical properties of HCFLG nanofluids, including thermal conductivity, specific heat capacities, density and viscosity for different concentrations, were performed. Heat transfer behavior and energy management of the synthesized coolant in the test-rig were studied and the convective heat transfer coefficient (h), Nusselt number (Nu), and pressure drop (ΔP) were evaluated. By measuring the temperatures at the inlet and outlet, and on the wall for different flow rates, the local convective heat transfer coefficient was obtained. The flow Reynolds number was calculated using,
 
image file: c6ra22365f-t1.tif(1)
where D, Uave, μ and ρ are the inner diameter of test section, the average flow velocity, viscosity, and density of working fluid, respectively. Also, Uave is given as,
 
image file: c6ra22365f-t2.tif(2)
where m° and Ac are the mass flow rate and surface area of the cross section. The local heat transfer coefficient “hx” and local Nusselt number “Nux” can be obtained from the following equations:
 
Q = m°Cp(ToutTin) (3)
 
image file: c6ra22365f-t3.tif(4)
 
image file: c6ra22365f-t4.tif(5)

Also, the bulk temperature of the fluid (Tbx) at the axial distance x is given as:31

 
image file: c6ra22365f-t5.tif(6)
 
image file: c6ra22365f-t6.tif(7)

In order to calculate the friction factor, “f”, the pressure drop across the test section was measured by a Foxboro™ differential pressure transmitter and eqn (8) was used. That is,

 
image file: c6ra22365f-t7.tif(8)

Employing new working fluids as a coolant requires investigation of their thermal performance, as well as their suitability as an appropriate alternative candidate for a range of Reynolds numbers and temperatures. According to ref. 32, using nanofluids as working fluids in heat exchangers provides an increase in both the heat transfer coefficient (positive effects) and a pressure drop (negative effects). To assess the effectiveness of HCFLG nanofluids, a performance index defined as,

 
image file: c6ra22365f-t8.tif(9)
was selected. Here Rh is the ratio of the heat transfer enhancement of the new coolant to the base-fluid, RΔP is the ratio of the pressure drop of the synthesized coolant to the base-fluid, and subscripts nf and bf refer to nanofluid and base fluid, respectively. As mentioned above, the use of nanofluids along with the sudden expansion in the duct not only increases the Nusselt number, but also increases the friction factor. In order to assess the overall performance of the system, including the thermal performance, as well as the hydraulic performance of the system, the performance evaluation criterion (PEC) is evaluated. The PEC shows the ratio of thermal performance of nanofluids in comparison to the Di-water to the hydraulic performance of nanofluids in comparison to Di-water. Mathematically, the PEC is given by,33
 
image file: c6ra22365f-t9.tif(10)

Eqn (11) provides an appropriate parameter for clarifying the range of temperatures and velocities over which the synthesized coolant can be used.32 To study the energy saving in the turbulent flow region, the pumping power can be measured.34 That is,

 
image file: c6ra22365f-t10.tif(11)
where Wnf and Wbf are the pumping power for nanofluid and base fluid, respectively.

The uncertainty analysis of the experimental data for the heat transfer and flow characteristics in the test-rig are of critical importance to ensure the range of validity and the applicability of the of the test results. Here uncertainty analysis according to the method described by Kline and McClintock35 was performed and the resulting uncertainties in the Nusselt number, heat transfer coefficient and friction factor are listed in Table 1. The measurement uncertainties in the friction factor, heat transfer coefficient, and performance index (PI) were calculated as follows:

 
image file: c6ra22365f-t11.tif(12)
where φ is the derived parameter, x represents the measured variables, and Δx represents the error of the measured variables.

Table 1 Measurement uncertainties
Parameters Maximum uncertainty (%)
Friction factor 5.3%
Nusselt number 4.1%
Performance index (PI) 5.7%


4 Results and discussion

4.1. Characterization

Fig. 2a presents the Fourier transform infrared spectroscopy (FTIR) spectra of pristine graphite and HCFLG. It can be seen that the FTIR spectrum of pristine graphite provided no evidence of functional groups. The peaks at 1471, 1535 and 1577 cm−1 were consistent with the bending vibration of the CH2 group, and stretching vibrations of the C[double bond, length as m-dash]C and C[double bond, length as m-dash]O, respectively. In contrast, the HCFLG shows some peaks in its spectrum. In particular, the FT-IR spectrum of HCFLG exhibits two main peaks at 1151 and 2268 cm−1, which are related to the C–N and C[triple bond, length as m-dash]N stretching vibrations, which were created by the attachment of the –C[triple bond, length as m-dash]N chains of cyanamide during the diazonium reaction. Also, the broad peak at 3436 cm−1 can be assigned to an N–H stretching vibration. The major difference between the spectra of pristine graphite and HCFLG is the appearance of the N–H, C–N and C[triple bond, length as m-dash]N stretching vibrations after functionalization. The sharp peaks of C–N and N–H show the presence of a primary amine in the main structure.
image file: c6ra22365f-f2.tif
Fig. 2 (a) FTIR spectra (b) Raman spectra (c) high-resolution C 1s spectra (d) N 1s spectra of HCFLG; (e and f) N2 adsorption–desorption isotherms of the (e) bulk graphite and (f) HCFLG.

Raman is a powerful characterization instrument for analyzing carbon-based nanostructures, including sp2 and sp3 hybridized carbon atoms, functionalization, and exfoliation by investigating changes in hole and electron doping.36,37 The Raman spectra of the pristine graphite and HCFLG are presented in Fig. 2b. Considering the weak D band in terms of intensity in the pristine graphite, the significantly sharp D, G and 2D bands in the HCFLG sample are seen at 1351, 1578, and 2699 cm−1, respectively. The ratio of the intensities of the D-band to those of the G-band (ID/IG) was considered to be the amount of disordered carbon (sp3-hybridized carbon) relative to graphitic carbon (sp2-hybridized carbon). In edge-functionalization studies of graphene, the higher intensity ratio of ID/IG means the higher disruption of aromatic π–π electrons, implying partial damage of the graphitic carbon produced by exfoliation and functionalization.38 It can clearly be seen that the ID/IG ratio of HCFLG is significantly higher than that of bulk graphite, which verifies the successful functionalization of GNP via the diazonium reaction under microwave irradiation. Note that the G and 2D bands in the spectrum of HCFLG retained their intensities after the diazoniation reaction, which is strong evidence for the preservation of the quality of the graphene layers. In addition, Raman spectroscopy can be employed to identify the number of layers by checking the shape, size, and intensity of the 2D bands.13,39 According to the results of Ferrari et al.,39 as the layer of graphene increases, the 2D band becomes broader and up-shifted. It can be seen that the 2D bond of the bulk graphite includes a coupled peak; that is, D1 and D2 peaks, which produced a broad peak.13,39 However, a single sharp 2D peak is seen in the Raman spectrum of HCFLG. This change in the 2D bands observed in the HCFLG sample suggests the presence of the low number of sheets.

The nature and amount of different functional groups in the bulk graphite and HCFLG were studied by the X-ray photoelectron spectroscopy (XPS), which is shown in Fig. S2. The spectrum of HCFLG has C 1s at around 286 eV, N 1s at 399 eV, and O 1s at 530 eV. It can be seen that HCFLG exhibits a very small amount of oxygen, and pristine graphite shows no nitrogen molecule in its structure. Upon exfoliation and functionalization, the intensity of the N 1s peak increased considerably. The cyanamide functionalities (the –C[triple bond, length as m-dash]N chains) may be the main reason for having higher content of nitrogen in the HCFLG sample. Fig. 2c shows the XPS C 1s spectrum of HCFLG. The HCFLG mostly had a peak at 284.6 eV, which was attributed to the C–C/C[thin space (1/6-em)][double bond, length as m-dash][thin space (1/6-em)]C network. Although the intensity of the oxygen element is insignificant, the minor O component in HCFLG presents two peaks in the form of the C[thin space (1/6-em)][double bond, length as m-dash][thin space (1/6-em)]O and O–C[thin space (1/6-em)][double bond, length as m-dash][thin space (1/6-em)]O groups at around 286.8 and 288.5 eV, respectively. Also, the C–N peak was observed at 285.6 eV. The N 1s spectrum of HCFLG in Fig. 2d shows two peaks at about 399.2 and 401.8 eV, which may be associated with the bonding configurations of amine functional groups and C[triple bond, length as m-dash]N, which were detected in the FTIR section.

To investigate the effects of exfoliation and functionalization on the specific surface area of HCFLG and bulk graphite, N2 adsorption–desorption isotherms were measured by a surface area analyzer (Quantachrome Autosorb-1 analyzer at 77[thin space (1/6-em)]K). The N2 adsorption–desorption isotherms of the bulk graphite and HCFLG are illustrated in Fig. 2e and f, respectively. The comparison between the BET results of pristine graphite and HCFLG materials shows a considerable increase in the specific surface area (Table 2). It was obvious that by exfoliation of pristine graphite into HCFLG, the specific surface area was significantly enhanced from 85 m2 g−1 to 1568 m2 g−1. Also, the total pore volume increased from 0.3 nm in pristine graphite to 1.33 nm in HCFLG. Fig. S3 shows the pore size distribution curves of pristine graphite and HCFLG. From Fig. S3, it can be seen that the HCFLG has higher pore volume than pristine graphene due to the in situ exfoliation and functionalization, which can be one of the main reasons for providing a pore size less than 2 nm. It is obvious that the pore size of the HCFLG is mostly less than 2 nm. The higher specific surface area of HCFLG compared to the pristine graphite is one of the main pieces of evidence for the exfoliation. The strong dependence of heat transfer on the specific surface area suggests that the HCFLG with an increased specific surface area can be a suitable candidate for developing a highly stable and conductive nanofluid. It should be pointed out that the highly-crumpled nature of the samples can be advantageous for the highly-stable colloidal suspension.

Table 2 Specific surface area and pore structure of the HCFLG and pristine graphite
Sample SBET (m2 g−1) Total pore volume (cm3 g−1)
HCFLG 1568 1.33
Pristine graphite 85 0.3


Fig. 3 shows XRD patterns of the pristine graphite and HCFLG. The graphite exhibits a sharp diffraction peak centered at 2θ = 26.5° corresponding to the (002) graphite plane composed of well-ordered graphenes with an interlayer spacing of 3.35 Å. It is obvious that the functionalization by small moieties such as NH2 should increase the layer spacing. Therefore, the peak at 2θ = 26.5° disappears for HCFLG and a relatively low peak at 2θ = 14.8° appears, corresponding to the diffraction of the (002) HCFLG plane. The interlayer spacing of HCFLG is calculated according to Bragg's law to be 5.98 Å. This implies that as graphite transforms to HCFLG, most nitrogen atoms and/or primary amine groups are bonded to the graphite surface and that graphite expands when functionalized.40,41 We also note that there is a much broader (002) reflection peak in HCFLG than in pristine graphite. The enhanced (002) broadening of HCFLG can be correlated with the functionalization of NH2, which produces graphene with few layers. Moreover, the NH2 functionalization can prevent small graphene sheets from stacking or aggregating to form large carbon particles during the drying process for the XRD test.


image file: c6ra22365f-f3.tif
Fig. 3 XRD patterns of the pristine graphite and HCFLG.

Fig. 4a–c show the field emission scanning electron microscope (FESEM) images of HCFLG. The in situ exfoliation and functionalization procedure is able to expand the bulk graphite layers swiftly by initiating a semi-stable diazonium ion and radical reaction with layers. The FESEM images of HCFLG shown in Fig. 4a–c illustrate homogenous highly crumpled structures with a 2D geometry. Such a worm-like surface, with fully crumpled and curved sheets is due to the strong functionalization. More evidence of the crumpled structure is presented by the transmission electron microscopy (TEM) images shown in Fig. 4d–g. These TEM images of HCFLG can clearly be large few-layered graphene crumpled flakes with wrinkled morphology and folded edges. As discussed above, a sharp 2D peak in Raman spectrum of HCFLG suggested that the few-layer graphene phase is apparently a dominant phase. The TEM images show no observable graphite crystalline structure, which is in agreement with the sharp 2D bands in the Raman spectrum of HCFLG. As further evidence, the crystalline structure of HCFLG was confirmed via selected area electron diffraction (SAED), as shown in Fig. 4h and i. Fig. 4h shows the normal-incidence electron diffraction pattern of the flake in Fig. 4f, taken with the beam position close to the white dot in this figure. Fig. 4i shows the normal-incidence selected-area diffraction patterns for the flake in Fig. 4g, taken with the beam position close to the red dot. In one of the cases, the patterns show the typical six-fold symmetry expected for graphite/graphene,42 allowing the peaks to be labeled with the Miller–Bravais (hkl) indices.42 Also, the hexagonal patterns are similar to those reported by other researchers12,43 for single-layer and few-layer graphene.


image file: c6ra22365f-f4.tif
Fig. 4 (a–c) FESEM images and (d–g) TEM images of HCFLG; (h and i) selected area electron diffraction (SAED) patterns of white point in panel (f) and red point in panel (g).

Selected area electron diffraction (SAED) of the HCFLG sample also shows a ring-like diffraction pattern with dispersed bright spots. Such an amorphous structure was attributed partially to the presence of functional groups with abundant defective edges for HCFLG, which is in agreement with the high-intensity D band in the Raman spectrum of the HCFLG sample.44,45 A ring-like diffraction pattern suggests the loss of long-range ordering in the sheets.44

AFM was used for the further morphological characterization of the HCFLG and for the investigation of the thicknesses of the flakes in the final product. Fig. S4 shows typical AFM images in which the flakes were few-layered, which is in agreement with the sharp 2D bands of the Raman results. From cross-section contour results, the thickness of HCFLG is very low, even as low as about 1 nm for some of the flakes.

4.2. Dispersibility

UV-Vis spectroscopy is a common method, which is utilized for the investigation of the stability of nanofluids including solid particles. According to the Beer–Lambert law, there is a direct connection between the absorbance of a solution and the concentration of the absorbing species, such as particles in the solution. Consistent with this law, the absorption spectrum of our prepared nanofluids exhibits a maximum peak at around 265 nm corresponding to a π–π transition of the conjugation system in the polyaromatic structures. The band gap energy, Eg, can be measured from UV-Vis absorption by Tauc's equation46 given as,
 
(αhν)n = B(hνEg) (13)
where α, hν, n, Eg and B are absorption coefficient, photon energy, the nature of optical transition, band gap energy and a material constant, respectively. Therefore, the UV-Vis spectrum for the distilled water-based HCFLG nanofluids with different weight concentrations was investigated and photometric analysis of the UV-Vis spectrometer was employed to trace the weight concentration of samples versus time. To this end, a standard curve was drawn for each concentration. Fig. 5 shows the colloidal stability for distilled water-based HCFLG nanofluids versus time. It can be seen that the concentration of the samples decreases slightly with time because of agglomeration and sedimentation. Fig. 5, however, shows that the relative reduction in weight concentration for all of the samples after 30 days was less than 2%. The high colloidal stability of distilled water-based HCFLG nanofluids is attributed to the small particle size associated with very high specific surface area (1568 m2 g−1). The sedimentation of particles in the nanofluids was believed to be a major factor, because the sedimentation of particles decreased the effective weight concentration. The rate of sedimentation among the different carbon allotrope dispersions was different. Furthermore, the type of functionalization, functional groups, weight concentration, and specific surface area play key roles in the rate of sedimentation. Table 3 compares the rate of sedimentation for different nanofluids including functionalized graphene, nitrogen-doped graphene and graphene oxide materials as additives. According to the results, HCFLG with a highly specific surface area showed a very good stability compared with other water-based graphene nanofluids.

image file: c6ra22365f-f5.tif
Fig. 5 The colloidal stability of HCFLG in distilled water as a function of time and weight concentration.
Table 3 The rate of sedimentation for different nanofluids including functionalized graphene, nitrogen-doped graphene and graphene oxide flakes
Material and references Base fluid Concentration Period of time (days) Rate of sedimentation (%)
GA–GNPs47 Distilled water 0.1 wt% 60 40%
CTAB–GNPs47 Distilled water 0.1 wt% 60 46%
SDS–GNPs47 Distilled water 0.1 wt% 60 47%
SDBS–GNPs47 Distilled water 0.1 wt% 60 18%
Triethanolamine-treated graphene nanoplatelets (SSA = 300)7 Distilled water 0.1 wt% 100 23.1%
Triethanolamine-treated graphene nanoplatelets (SSA = 500)7 Distilled water 0.1 wt% 100 12.5%
Triethanolamine-treated graphene nanoplatelets (SSA = 750)7 Distilled water 0.1 wt% 100 17%
Propylene glycol-treated graphene nanoplatelets22 Distilled water 0.1 wt% 34 12%
Tetrahydrofurfuryl polyethylene glycol-treated graphene nanoplatelet48 Distilled water 0.1 wt% 30 15%
Trimethylolpropane tris[poly(propylene glycol), amine terminated] ether-treated graphene nanoplatelet49 Distilled water 0.1 wt% 30 12%
N-Doped rGO50 Distilled water 1 mg mL−1 49 Less than 5%
Graphene–SiO2[thin space (1/6-em)]51 Distilled water 0.1 wt% 7 More than 50%
Carboxylated graphene nanoplatelets52 Distilled water 0.1 wt% 10 7%
PEG-treated GNP53 Water 0.05 wt% 30 17%
Present study HCFLG 0.01 wt% 30 2%


4.3. Thermophysical properties

Thermal conductivity is an important thermophysical property and was measured using a KD2 Pro analyzer based on the transient hot wire technique. The measured values of thermal conductivity for distilled water and distilled water-based HCFLG nanofluids are shown in Fig. 6a. As expected, this figure shows that the measured thermal conductivity increases with temperature. In our recent study,7 it was found that the higher specific surface area leads to the higher thermal conductivity of water-based graphene nanofluids. Since HCFLG has a high specific surface area, the increase in thermal conductivity of the nanofluids is consistent with the earlier findings.
image file: c6ra22365f-f6.tif
Fig. 6 (a) Thermal conductivity and (b) specific heat capacity plots of water-based HCFLG nanofluids at different weight concentrations as well as distilled water.

From Fig. 6a it can be seen that all samples were prepared with very low weight concentration. Nevertheless, the amount of enhancement in the thermal conductivity of different samples is significant. As the concentration was increased from 0.0 wt% to 0.01 wt%, the figure shows that the thermal conductivity of water-based HCFLG nanofluids increases from 0.642 to 0.915 W m−1 K−1 at 50 °C, which represents a 42.5% enhancement. This amount of enhancement is quite impressive for the low weight concentration of 0.01 wt%. Also, for distilled water, Fig. 6a showed that the increase in temperature from 20 to 50 °C resulted in an 8.6% increase in the thermal conductivity, while for water-based HCFLG nanofluids at 0.001 wt%, 0.005 wt%, and 0.01 wt%, the increases in thermal conductivity were 20.8%, 23.8%, and 21.9%, respectively. Keblinski et al.54 and Eastman et al.55 suggested some potential mechanisms for the increase in the thermal conductivity in the presence of nanoparticles: Brownian motion, molecular-level layering of the liquid at the liquid/particle interface, fluctuation of fluid velocity due to the drag of Brownian nanoparticles, thermophoresis, reduction in the thermal boundary layer thickness, the nature of heat transport in nanoparticles, and the effects of nanoparticle clustering. According to recent studies,7,56–60 the thermal conductivity of nanofluids is affected by the thermal conductivities of the base fluid and nanoparticles, temperature, concentration, specific surface area, shape/geometry of nanostructures. The present results show that the specific surface area of nanoparticles also affects the thermal conductivity as well as the colloidal stability.

Furthermore, we know that different carbon allotropes as additives behave differently in terms of increasing the thermal conductivity of base fluids. According to the results, HCFLG with a highly specific surface area showed a very high thermal conductivity. Table 4 summarizes the results of thermal conductivity measurements from different researchers on graphene-based nanofluids.

Table 4 Summary of experimental results on thermal conductivity of graphene-based nanofluids
Investigator Particle type Base fluid Particle concentration Maximum enhancement Temperatures
Yu et al.61 Graphene oxide nanosheets Ethylene glycol 1–5 vol% 10.5–61% 10–60 °C
Baby and Ramaprabhu62 Exfoliated graphene Water 0.005–0.056 vol% 14–64% 25–50 °C
Ethylene glycol 4–7%
Martin-Gallego63 Functionalized graphene sheets [FGS] Water 0.2–1 wt% 10–70% 30–60 °C
Baby and Sundara64 Copper oxide-decorated graphene (CuO/HEG) Water 0.005–0.05 wt% 23–90% 25–50 °C
Ethylene glycol 0.01–0.07 wt% 17–23%
Baby and Ramaprabhu65 Hydrogen-exfoliated graphene Water 0.005–0.05 wt% 10–75% 25–50 °C
Ethylene glycol 0.05–0.08 wt% 1–5%
Yu et al.66 Graphene oxide nanosheets Ethylene glycol 2–5 wt% Up to 86% 10–60 °C
Baby and Ramaprabhu67 Silver-decorated graphene Water 0.005–0.05 wt% 7–86% 25–70 °C
Ethylene glycol 0.01–0.07 wt% 3–14%
Aravind et al.68 Graphene nanosheets Water 0.008–0.138 vol% 2.4–17% 25 °C
Ethylene glycol 2.4–6.5%
Sun et al.69 Few-layer graphene Polymer 0.55–1 vol% 18–25% 10–60 °C
Dhar et al.70 Poly-dispersed graphene Water 0.05–0.2 vol% 3–30% 25–50 °C
Ghozatloo et al.71 Functionalized graphene Water 0.01–0.05 wt% 3.8–17% 10–50 °C
Kole and Dey72 Functionalized graphene nano-sheets (GnS) Water + ethylene glycol 0.041–0.395 vol% Up to 15% 10–70 °C
Gupta et al.73 Graphene nano-sheets Water 0.05–0.2 vol% Up to 27% 30–50 °C
Yang et al.74 Diamond-treated graphene Silicon oil 0.35–5.2 vol% Up to 10% Room temperature
Baby and Sundara75 MWCNT–graphene hybrid Water 0.005–0.04 vol% 1–20% 25–50 °C
Li et al.51 SiO2-coated graphene Water 0.1 wt% Up to 20% 15–65 °C
Hajjar et al.76 Graphite oxide (GO) Water 0.05–0.25 wt% 14.75–47.57% 10–40 °C
Park and Kim77 Graphene Water 0.001–0.01 vol% 6.24–14% 25 °C
Liu et al.78 Graphene Water 0.01–0.03 wt% 3–22.9% 25–200 °C
Akhavan-Zanjani et al.79 Graphene Water 0.005–0.02 wt% 6.04–10.3% 25–45 °C
Haque et al.80 MWCNT and graphene Water Mass ratios were 1/3, 3/1, 1/1, 1/2 and 2/1 Up to 5.546% 20–40 °C
Lee and Rhee81 Graphene nanoplatelets Ethylene glycol 0.5–4 vol% Up to 32% 10–90 °C
Ma et al.82 Functionalized graphene nanosheets Silicon oil 0.01–0.07 wt% Up to 18.9% 20–60 °C
Shende and Sundara83 Nitrogen doped graphene Ethylene glycol 0.005–0.03 vol% Up to 15.1% 25–50 °C
Water 0.005–0.02 vol% Up to 17.7%
Present results HCFLG Water 0.001–0.01 wt% 10–43% 25–50 °C


In Fig. 6b, the effects of temperature and weight concentration of HCFLG on the specific heat capacity of distilled water-based HCFLG nanofluids are studied. It can be seen that an increase in the weight concentrations of HCFLG leads to a drop in the specific heat capacity. In particular, an average drop of 0.1–0.5% is observed for a weight concentration of 0.001–0.01 wt%. The specific heat capacity of distilled water-based HCFLG is lower than that of water due to the lower specific heat capacity of HCFLG loaded in the base fluid.

The measured values of viscosity are plotted in Fig. 7 as a function of shear rate for water-based HCFLG nanofluids and weight concentrations, as well as distilled water at various temperatures. This figure shows that the effective viscosity of water-based HCFLG nanofluids is higher than that of water and increases as the weight concentration increases. Furthermore, the effective viscosity decreases with an increase in the temperature. Fig. 7 also shows that the behavior of water-based HCFLG nanofluids is Newtonian, with almost constant viscosity for different values of shear rate.


image file: c6ra22365f-f7.tif
Fig. 7 Plots of the measured values of viscosity versus shear rate for water-based HCFLG nanofluids at different temperatures and weight concentrations.

The densities of water-based HCFLG nanofluids and water are measured as functions of temperature and weight concentration, and the results are shown in Table 5. It can be observed that the density of water-based HCFLG nanofluids as well as water decreases with an increase in the temperature, which may be related to the thermal expansion of the liquid. Also, there is an upward trend between the density of the samples and the weight concentration of HCFLG. Therefore as the weight concentration increases, the density grows. Since the density of solid particles is commonly more than that of liquids, the density of the prepared samples increases with concentration, which can be a reasonable issue. Also, as the temperature increases, the density is insignificantly enhanced. For example, the density of the Di-water and water-based HCFLG nanofluids at weight concentration of 0.01% decreases by 1.01% and 0.99%, when the temperature increases from 20 to 50 °C, respectively.

Table 5 Densities of the Di-water and water-based HCFLG nanofluids for different concentrations
T (°C) Density (kg m−3)
Di-water HCFLG-0.001 HCFLG-0.005 HCFLG-0.01
20 997.78 998.18 999.79 1001.80
30 995.18 995.58 997.20 999.23
40 991.80 992.20 993.84 995.88
50 987.68 988.092 989.74 991.80


4.4. Heat transfer in a backward-facing step flow

In this section, experimental investigations of heat transfer over a backward-facing step flow of the HCFLG nanofluids in transitional and turbulent flow regimes are presented. Water-based highly crumpled few-layer graphene nanofluids with different weight concentrations were synthesized and used in these experiments. The experimental data for the rate of heat transfer for different Reynolds numbers in the range of 2000 ≤ Re ≤ 16[thin space (1/6-em)]000 and HCFLG concentrations of 0.001, 0.005 and 0.01 wt% of HCFLG are obtained. The position of the thermocouples and the boundary conditions are shown schematically in Fig. S1. Accordingly, a constant heat flux of 600 W was provided after the expansion via two DC power supplies. The inlet fluid rate was in the range of 1 to 16 L min−1. Also, the inlet flow temperature was always maintained at a constant temperature of 30 ± 1 °C.

Fig. 8 shows the temperature of the heated wall (TS), the temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) versus X/D for distilled water at different Reynolds numbers (Re). In both plots of TS versus X/D and TSTb versus X/D, a U-shaped variation of the TS or TSTb with X/D can be seen. Heat transfer in the backward-facing step has been studied by a number of researchers16,20,27 in recent years. Accordingly, the boundary layer flow separates at the sharp step edge and forms a recirculation region, as shown schematically in Fig. S1. The shear layer, downstream, impinges on the surface and reattaches to the lower wall at the so-called reattachment point.84 Downstream of the reattachment point, the boundary layer begins to redevelop and far downstream the flow approached the fully developed flow in the larger diameter pipe. The separation and reattachment in this area cause major changes in the flow in this region. Close to the step, the velocity is insignificant, leading to the maximum wall temperature and consequently minimum Nusselt number. On the other hand, the velocity can reach its maximum amount in the recirculation zone, where the wall temperature is a minimum and the Nusselt number is a maximum. So, a U-shaped variation in the TS or TSTb with X/D is reasonable and was reported by a majority of recent studies in this field, such as.16,20,27


image file: c6ra22365f-f8.tif
Fig. 8 Measured temperature of the heated wall (TS), the temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) versus X/D for distilled water at different Reynolds numbers (Re).

That is, there is a sharp downward trend of temperature with X/D up to ∼2.66, after which both the temperature of the heated wall (TS) and the temperature difference between the wall and the fluid bulk for the deionized water increase moderately with further increase in X/D.

The heat transfer coefficient was computed from the temperature given by the thermocouples in different positions. Eqn (6) and (8) indicates that the local convective heat transfer coefficient (hx) and local Nusselt number (Nux) have an inverse relation with the temperature difference between the wall and the bulk fluid. Therefore, for X/D less than 2.66 for distilled water, the values of the local convective heat transfer coefficient (h) and local Nusselt number (Nu) increase. By contrast, the h and Nu show a downward trend for X/D higher than 2.66.

Fig. 9–11 present the measured temperature of the heated wall (TS), the measured temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) for different Re numbers and X/D location for water-based HCFLG nanofluids with concentrations of 0.001, 0.005 and 0.01 wt%, respectively. Like distilled water, these figures show a similar U-shaped variation in the TS or TSTb with X/D, representing a sudden decrease and a gradual increase. Also, the local convective heat transfer coefficient (hx) and local Nusselt number (Nux) show the same trends as the variations of distilled water. From a comparison between Fig. 8–11, it can be observed that the measured temperature of the heated wall (TS) and the measured temperature difference between the wall and the fluid bulk temperature (TSTb) become closer for higher weight concentrations of HCFLG, representing the key role of HCFLG in transferring heat in the recirculation zone. All of the Nusselt profiles present the same characteristic behavior: their values are low in the recirculation zone, increase through a maximum at the reattachment point and decrease in the recovery region to a stable value, as found in by Nie and Armaly85 for a confined configuration.


image file: c6ra22365f-f9.tif
Fig. 9 Measured temperature of the heated wall (TS), the temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) versus X/D for water-based HCFLG nanofluid at 0.001 wt%.

image file: c6ra22365f-f10.tif
Fig. 10 Measured temperature of the heated wall (TS), the temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) versus X/D for water-based HCFLG nanofluid at 0.005 wt%.

image file: c6ra22365f-f11.tif
Fig. 11 Measured temperature of the heated wall (TS), the temperature difference between the wall and the fluid bulk (TSTb), local convective heat transfer coefficient (h) and Nusselt number (Nu) versus X/D for water-based HCFLG nanofluids at 0.01 wt%.

Also, as the concentration of HCFLG in the nanofluids increases, the U-shaped variation in TS or TSTb with X/D becomes wider. As mentioned above, the local convective heat transfer coefficient and local Nusselt number have an inverse relationship with the measured temperature difference between the wall temperature and the fluid bulk temperature. In order to perform an appropriate comparison, the variations in average heat transfer coefficient with the Reynolds number for water-based HCFLG nanofluids at different weight concentrations as well as water were calculated, as shown in Fig. S5. For all samples, the average heat transfer coefficient increases with the Reynolds number and weight concentrations. The highest average heat transfer coefficient was achieved for a water-based HCFLG nanofluid with a weight concentration of 0.01% and Re number of 16[thin space (1/6-em)]000, representing an average heat transfer coefficient of 5520.26 W m−2 K−1. For instance, the maximum ratio of enhancement in the average heat transfer coefficient was almost 60% for a water-based HCFLG nanofluid at 0.01 wt% and Re number of 16[thin space (1/6-em)]000 as compared with pure water, which is a brilliant improvement.

In order to clarify the key role of weight concentration of HCFLG, the measured results for Nusselt number are shown for Reynolds numbers of 2000, 3500, 7000, 13[thin space (1/6-em)]000 in Fig. 12. We selected these four Reynolds numbers as candidates for all conditions. It can be seen that as the concentration of HCFLG in the nanofluids increases, the Nu number increases for a constant Re number. However, Fig. 12 shows that the effects of HCFLG concentration on the Nusselt number term are more pronounced than for other parameters. The reason for the larger enhancement of the Nusselt number for nanofluids compared to that of distilled water was suggested by the present authors86 using a simple analogy. Accordingly, the connective heat transfer is proportional to k/δt, where δt is the thickness of the thermal boundary layer. Thus, to increase the convective heat transfer coefficient, k should be increased and/or δt should be decreased. According to ref. 86 and 87, carbon nanomaterials such as carbon nanotubes and graphene have a tendency to decrease the thermal boundary layer thickness. On the other hand, as the concentration of HCFLG increases, the measured thermal conductivity of the nanofluids increases, implying a higher convective heat transfer coefficient. Therefore, both the thermal boundary layer thickness term and the thermal conductivity term have positive effects on increasing the heat transfer rate. Therefore, nanofluids with a higher weight concentration (higher thermal conductivity) enhance the value of the Nusselt number more. This conclusion is consistent with recent studies.27 Obviously, the maximum value of the Nusselt number coincides with the point of reattachment. As in other studies,27,88 after the point of reattachment, an increase in Nusselt number is observed by increasing the weight concentration of the HCFLG. Therefore, the high Nusselt number inside the recirculation depends mainly on the thermophysical properties of the nanoparticles. Also, outside the recirculation zone both the Reynolds number and the thermophysical properties of the nanofluids affect the value of the Nusselt number.


image file: c6ra22365f-f12.tif
Fig. 12 The effects of Reynolds number and weight concentration of HCFLG on the Nusselt number at different axial ratios.

Fig. 9–12 show that the position of the maximum Nusselt number (Xmax/D) changes as the Re number changes. Fig. 13 shows the variations in Xmax/D for water-based HCFLG nanofluids and distilled water for different Re numbers and weight% concentrations. It can be seen that the position of the maximum value of the Nusselt number increases (shifts up) with the Re number and the weight concentration of HCFLG. It can be observed that as the concentration increased, the temperature difference between the tube wall and the working fluid decreased due to higher thermal conductivity, implying higher heat transfer rate. For the same expansion ratio of 2, it is observed that the higher Re number leads to a higher Nux. For the same expansion ratio of 2 and Re number of 16[thin space (1/6-em)]000, the experimentally measured values of Xmax/D are, 4.66, 3.99, 3.33 and 3.33 for water-based HCFLG nanofluids at 0.01, 0.005, 0.001 and 0 wt%, respectively. The position as well as the amount of Xmax/D increased as the Re number increased, showing that Xmax is dependent on Re and the concentration of additives (thermal conductivity).


image file: c6ra22365f-f13.tif
Fig. 13 The effects of Reynolds number and weight concentration of HCFLG on the position of maximum Nusselt number.

Fig. 14 plots the pressure drop of the flow over the backward-facing step for different Re numbers and weight concentrations of HCFLG, including distilled water. It can be seen that as the Re number and concentration of HCFLG in base fluid increase, the pressure drop increases. It is noteworthy that the pressure drops for the prepared samples are quite close to that for the distilled water, which is attributable to the low concentrations of 0.001 wt%, 0.005 wt% and 0.01 wt%. Fig. 14 shows that the pressure drop for the water-based HCFLG nanofluids at a concentration of 0.01 wt% and Re number of 16[thin space (1/6-em)]000 has the highest pressure drop for the current range of measurement. Note that the pressure drop is proportional to the viscosity of the working fluids, exhibiting the highest and lowest amounts in similar conditions.


image file: c6ra22365f-f14.tif
Fig. 14 The measured value of pressure drop of the set-up at different Re numbers for distilled water and water-based HCFLG nanofluids with different weight concentrations.

Table 6 shows the average percentage increase in the friction factor of the nanofluids compared with the deionized water for the flow over the backward-facing step. From Table 6, we can see that the measured friction factor decreases with an increase in the Re number for different weight concentrations of HCFLG. In addition, the friction factor increases as the concentration of HCFLG increases, although the percentage enhancement is more obvious for low values of Re numbers. It can also be seen that as the Re number increases, the dependence of the friction factor on the weight concentration of HCFLG decreases. At low Reynolds numbers, the Brownian motion is the main mechanism that influences the momentum transfer between the HCFLG and base-fluid molecules. Thus, as Brownian motion increases the concentration of HCFLG in the nanofluids increases, leading to an increase in the friction factor with a higher slope as compared with the base fluid.26 In contrast, this mechanism loses its dominance for high Reynolds number flows, where turbulent agitations in the flow play the key role. In summary, the turbulence of the working fluid can be considered to be the most important parameter in increasing the friction factor at high Reynolds numbers. Also, the small differences between friction factors of the distilled water and water-based HCFLG suspensions at different weight concentrations are attributable to the small differences between the viscosities of the base fluid and the prepared nanofluid samples.

Table 6 The average increase in the friction factor of nanofluids compared with deionized water
Percentage increase in the friction factor
Weight concentration Re number
16[thin space (1/6-em)]000 13[thin space (1/6-em)]000 10[thin space (1/6-em)]000 7000 4000 3500 3000 2500 2400 2300 2200 2100 2000
0.001 0.018234 0.043588 0.09094 0.084823 0.209077 0.214451 0.247023 0.093786 0.163302 0.174387 0.224146 0.19396 0.206224
0.005 0.074384 0.129912 0.108376 0.171763 0.245811 0.330957 0.308987 0.334116 0.38078 0.341263 0.356486 0.349793 0.326606
0.01 0.101268 0.216088 0.23571 0.375622 0.738048 0.695673 0.848073 0.788283 0.81984 0.708389 0.704982 0.643127 0.673305


The economic performance of working fluids for different heat transfer equipment is measured via the performance index (ε), which is identified as the ratio of the heat transfer rate to the pressure drop ratios. Recent studies (e.g., ref. 89) suggested that while the addition of solid nanoparticles improves the heat transfer rate, the pressure drop in the flow loops also increases, which is undesirable. Therefore, the performance index is presented to consider both parameters. The variations in the average performance index and PEC for water-based HCFLG nanofluids are illustrated for different Re numbers and weight concentrations in Fig. 15a. It can be seen that the average performance index as well as PEC of all samples including HCFLG is higher than 1, representing the effectiveness of the prepared coolant samples for use over the backward-facing step flows. It can also be seen that, as the weight concentration of HCFLG in the nanofluids increases, the average performance index as well as the PEC increase, which shows that the enhancement in heat transfer is more effective than the increase in pressure drop. This figure also shows that the average performance index curves for different Re numbers. Also, the performance index results showed a gradual decrease with Re numbers.


image file: c6ra22365f-f15.tif
Fig. 15 (a) Performance evaluation criterion (PEC) and performance index (PI) of water-based HCFLG nanofluid; (b) pumping power for the backward-facing step in the presence of distilled water and water-based HCFLG nanofluids with different weight concentrations.

Pumping power can be considered to be an economic performance indicator in a loop system for evaluating the operability of fluids and the performance of power plants. Fig. 15b compares the pumping power of the water-based HCFLG nanofluids for different weight concentrations with that of the base-fluid. This figure shows that there is a slight increase in the pumping power with the HCFLG loading but the percentage increase in pumping power increase is negligible. The small growth in the pumping power could be due to the low weight fraction of HCFLG in the base fluid.

5 Conclusion

A simple and cost-effective approach was utilized for mass production of HCFLG with a large specific surface area. Highly-crumpled few-layer graphene was then used as an additive for preparing highly stable and highly conductive nanofluids with superior thermophysical properties. The results suggested that the thermophysical properties of water-based HCFLG were enhanced, making the nanofluid well-suited for heat transfer applications. The experimental study of the heat transfer of the prepared nanofluids over a backward-facing step in transitional and turbulent flow regimes for a range of Re and concentration was performed. The results showed that the water-based HCFLG nanofluids at very low concentrations exhibited a noticeably higher heat transfer rate compared to the distilled water. Overall, the heat transfer rate showed a 90% enhancement by loading just 0.01 wt% of HCFLG into the distilled water. Also, experimental data for the Nu number and local heat transfer coefficient of water-based nanofluids for transitional and turbulent flow regimes were presented. The data showed that as the wt% of HCFLG in the nanofluids and/or Re number increase over the backward-facing step, the position of the maximum heat transfer point (Xmax/D) shifts to higher distances, leading to a larger recirculation zone. The presented results showed that the water-based HCFLG nanofluids are great candidates for a new generation of heat transfer fluids.

Nomenclature

CpSpecific heat, J g−1 K−1
DDiameter, m
hHeat transfer coefficient, W m−2 K−1
kThermal conductivity (W m−1 K−1)
Nu (h = Dh/k)Nusselt number
qHeat flux (W m−2)
QHeat transfer rate, W
ReReynolds number
PECPerformance evaluation criterion
UaveAverage velocity (m s−1)
fFriction factor
m°Mass flow rate (kg s−1)
AcSurface area of the cross section (m2)
LChannel length (m)
Lx/LRatio of the length of x to the channel length
TSxThe wall temperature of fluid at the axial distance x
TbxThe bulk temperature of fluid at the axial distance x
AwArea of downstream wall (m2)
RhRatio of the heat transfer coefficient enhancement of new coolant to the base-fluid
RΔPRatio of pressure drop of new coolant to the base-fluid
PIPerformance index
PLCProgrammable logic controller
RTDResistance temperature detector

Greek symbols

μViscosity (Pa s)
ρDensity (kg m−3)
ΔPPressure drop (Pa)

Subscripts

nfNanofluid
bfBase fluid
aveAverage
sTube wall
ininlet
outoutlet

Acknowledgements

The authors gratefully acknowledge Bright Sparks Unit of University Malaya, UMRG Grant RP035B-15AET, High Impact Research Grant UM.C/625/1/HIR/MOHE/ENG/45, BK009-2016 and IPPP grant PV113/2011A Faculty of Engineering, University of Malaya, Malaysia for support to conduct this research work.

References

  1. J. Nanda, C. Maranville, S. C. Bollin, D. Sawall, H. Ohtani, J. T. Remillard and J. Ginder, J. Phys. Chem. C, 2008, 112, 654–658 CAS.
  2. Z. Sun, V. Nicolosi, D. Rickard, S. D. Bergin, D. Aherne and J. N. Coleman, J. Phys. Chem. C, 2008, 112, 10692–10699 CAS.
  3. M. Shanbedi, S. Z. Heris, A. Amiri, S. Adyani, M. Alizadeh and M. Baniadam, Numer. Heat Transfer, Part A, 2014, 66, 947–962 CrossRef.
  4. P. Sudeep, J. Taha-Tijerina, P. Ajayan, T. Narayanan and M. Anantharaman, RSC Adv., 2014, 4, 24887–24892 RSC.
  5. A. Amiri, M. Shanbedi, B. Chew, S. Kazi and K. Solangi, Chem. Eng. J., 2016, 289, 583–595 CrossRef CAS.
  6. M. Myekhlai, B. Munkhbayar, T. Lee, M. R. Tanshen, H. Chung and H. Jeong, RSC Adv., 2014, 4, 2495–2500 RSC.
  7. W. S. Sarsam, A. Amiri, M. N. M. Zubir, H. Yarmand, S. Kazi and A. Badarudin, Colloids Surf., A, 2016, 500, 17–31 CrossRef CAS.
  8. A. Amiri, M. Shanbedi, G. Ahmadi, H. Eshghi, S. N. Kazi, B. T. Chew, M. Savari and M. N. M. Zubir, Sci. Rep., 2016, 6, 32686 CrossRef PubMed.
  9. R. Ruoff, Nat. Nanotechnol., 2008, 3, 10–11 CrossRef CAS PubMed.
  10. H. Wang, J. T. Robinson, X. Li and H. Dai, J. Am. Chem. Soc., 2009, 131, 9910–9911 CrossRef CAS PubMed.
  11. Z. Sun, S.-i. Kohama, Z. Zhang, J. R. Lomeda and J. M. Tour, Nano Res., 2010, 3, 117–125 CrossRef CAS.
  12. C. E. Hamilton, J. R. Lomeda, Z. Sun, J. M. Tour and A. R. Barron, Nano Lett., 2009, 9, 3460–3462 CrossRef CAS PubMed.
  13. Y. Hernandez, V. Nicolosi, M. Lotya, F. M. Blighe, Z. Sun, S. De, I. McGovern, B. Holland, M. Byrne and Y. K. Gun'Ko, Nat. Nanotechnol., 2008, 3, 563–568 CrossRef CAS PubMed.
  14. L. Niu, J. N. Coleman, H. Zhang, H. Shin, M. Chhowalla and Z. Zheng, Small, 2016, 12, 272–293 CrossRef CAS PubMed.
  15. J. R. Lomeda, C. D. Doyle, D. V. Kosynkin, W.-F. Hwang and J. M. Tour, J. Am. Chem. Soc., 2008, 130, 16201–16206 CrossRef CAS PubMed.
  16. H. Mohammed, O. A. Alawi and M. Wahid, Powder Technol., 2015, 275, 329–343 CrossRef CAS.
  17. M. Sheikholeslami, D. D. Ganji, M. Y. Javed and R. Ellahi, J. Magn. Magn. Mater., 2015, 374, 36–43 CrossRef CAS.
  18. A. Amiri, H. Khajeh Arzani, S. N. Kazi, B. T. Chew and A. Badarudin, Int. J. Heat Mass Transfer, 2016, 97, 538–546 CrossRef CAS.
  19. A. S. Kherbeet, H. Mohammed, B. Salman, H. E. Ahmed and O. A. Alawi, Int. J. Heat Mass Transfer, 2014, 79, 858–867 CrossRef CAS.
  20. N. Lancial, F. Beaubert, S. Harmand and G. Rolland, Int. J. Heat Fluid Flow, 2013, 44, 336–347 CrossRef.
  21. H. K. Arzani, A. Amiri, S. Kazi, B. Chew and A. Badarudin, Int. Commun. Heat Mass Transfer, 2016, 75, 67–77 CrossRef CAS.
  22. K. Solangi, A. Amiri, M. Luhur, S. A. A. Ghavimi, M. N. M. Zubir, S. Kazi and A. Badarudin, Int. Commun. Heat Mass Transfer, 2016, 73, 43–53 CrossRef CAS.
  23. H. Yarmand, S. Gharehkhani, S. F. S. Shirazi, A. Amiri, E. Montazer, H. K. Arzani, R. Sadri, M. Dahari and S. Kazi, Int. Commun. Heat Mass Transfer, 2016, 72, 10–15 CrossRef CAS.
  24. E. Abu-Nada, Z. Masoud and A. Hijazi, Int. Commun. Heat Mass Transfer, 2008, 35, 657–665 CrossRef CAS.
  25. S. Zeinali Heris, S. G. Etemad and M. Nasr Esfahany, Int. Commun. Heat Mass Transfer, 2006, 33, 529–535 CrossRef CAS.
  26. H. Mohammed, A. Al-Aswadi, N. Shuaib and R. Saidur, Renewable Sustainable Energy Rev., 2011, 15, 2921–2939 CrossRef CAS.
  27. E. Abu-Nada, Int. J. Heat Fluid Flow, 2008, 29, 242–249 CrossRef CAS.
  28. H. Mohammed, A. Al-aswadi, H. Abu-Mulaweh and N. Shuaib, Heat Tran. Asian Res., 2011, 40, 287–307 CrossRef.
  29. H. Mohammed, A. Al-Aswadi, M. Yusoff and R. Saidur, Thermophysics and Aeromechanics, 2012, 42, 1–30 Search PubMed.
  30. A. S. Kherbeet, H. A. Mohammed and B. Salman, Int. J. Heat Mass Transfer, 2012, 55, 5870–5881 CrossRef CAS.
  31. S. S. J. Aravind, P. Baskar, T. T. Baby, R. K. Sabareesh, S. Das and S. Ramaprabhu, J. Phys. Chem. C, 2011, 115, 16737–16744 CAS.
  32. M. Shanbedi, S. Zeinali Heris, A. Amiri, E. Hosseinipour, H. Eshghi and S. N. Kazi, Energy Convers. Manage., 2015, 105, 1366–1376 CrossRef CAS.
  33. O. Manca, S. Nardini and D. Ricci, Appl. Therm. Eng., 2012, 37, 280–292 CrossRef CAS.
  34. R. B. Mansour, N. Galanis and C. T. Nguyen, Appl. Therm. Eng., 2007, 27, 240–249 CrossRef.
  35. S. J. Kline and F. A. McClintock, Mech. Eng., 1953, 75, 3–8 Search PubMed.
  36. H. Zare-Zardini, A. Amiri, M. Shanbedi, A. Taheri-Kafrani, S. N. Kazi, B. T. Chew and A. Razmjou, J. Biomed. Mater. Res., Part A, 2015, 103A, 2959–2965 CrossRef PubMed.
  37. B. Das, R. Voggu, C. S. Rout and C. Rao, Chem. Commun., 2008, 5155–5157 RSC.
  38. W. Lv, D.-M. Tang, Y.-B. He, C.-H. You, Z.-Q. Shi, X.-C. Chen, C.-M. Chen, P.-X. Hou, C. Liu and Q.-H. Yang, ACS Nano, 2009, 3, 3730–3736 CrossRef CAS PubMed.
  39. A. Ferrari, J. Meyer, V. Scardaci, C. Casiraghi, M. Lazzeri, F. Mauri, S. Piscanec, D. Jiang, K. Novoselov and S. Roth, Phys. Rev. Lett., 2006, 97, 187401 CrossRef CAS PubMed.
  40. M. Naebe, J. Wang, A. Amini, H. Khayyam, N. Hameed, L. H. Li, Y. Chen and B. Fox, Sci. Rep., 2014, 4, 4375 Search PubMed.
  41. D. Mhamane, W. Ramadan, M. Fawzy, A. Rana, M. Dubey, C. Rode, B. Lefez, B. Hannoyer and S. Ogale, Green Chem., 2011, 13, 1990–1996 RSC.
  42. J. C. Meyer, A. K. Geim, M. I. Katsnelson, K. S. Novoselov, T. J. Booth and S. Roth, Nature, 2007, 446, 60–63 CrossRef CAS PubMed.
  43. U. Khan, A. O'Neill, M. Lotya, S. De and J. N. Coleman, Small, 2010, 6, 864–871 CrossRef CAS PubMed.
  44. G. Wang, J. Yang, J. Park, X. Gou, B. Wang, H. Liu and J. Yao, J. Phys. Chem. C, 2008, 112, 8192–8195 CAS.
  45. A. Amiri, G. Ahmadi, M. Shanbedi, M. Savari, S. N. Kazi and B. T. Chew, Sci. Rep., 2015, 5, 17503 CrossRef CAS PubMed.
  46. M. Hadadian, E. K. Goharshadi and A. Youssefi, J. Nanopart. Res., 2014, 16, 1–17 CrossRef CAS.
  47. W. S. Sarsam, A. Amiri, S. Kazi and A. Badarudin, Energy Convers. Manage., 2016, 116, 101–111 CrossRef CAS.
  48. H. K. Arzani, A. Amiri, S. Kazi, A. Badarudin and B. Chew, RSC Adv., 2016, 6, 65654–65669 RSC.
  49. K. Solangi, A. Amiri, M. Luhur, S. A. A. Ghavimi, S. Kazi, A. Badarudin and M. N. M. Zubir, RSC Adv., 2016, 6, 4552–4563 RSC.
  50. K. Z. Kamali and A. M. Golsheikh, Colloids Surf., A, 2016, 509, 574–582 CrossRef.
  51. X. Li, Y. Chen, S. Mo, L. Jia and X. Shao, Thermochim. Acta, 2014, 595, 6–10 CrossRef CAS.
  52. H. Yarmand, S. Gharehkhani, S. F. S. Shirazi, A. Amiri, M. S. Alehashem, M. Dahari and S. Kazi, Energy Convers. Manage., 2016, 114, 38–49 CrossRef CAS.
  53. A. Amiri, M. Shanbedi, G. Ahmadi, H. Eshghi, B. T. Chew and S. N. Kazi, Colloids Surf., A, 2015, 487, 131–141 CrossRef CAS.
  54. P. Keblinski, S. Phillpot, S. Choi and J. Eastman, Int. J. Heat Mass Transfer, 2002, 45, 855–863 CrossRef CAS.
  55. J. A. Eastman, S. Phillpot, S. Choi and P. Keblinski, Annu. Rev. Mater. Res., 2004, 34, 219–246 CrossRef CAS.
  56. L. Godson, B. Raja, D. M. Lal and S. Wongwises, Exp. Heat Transfer, 2010, 23, 317–332 CrossRef CAS.
  57. H. U. Kang, S. H. Kim and J. M. Oh, Exp. Heat Transfer, 2006, 19, 181–191 CrossRef CAS.
  58. S. Choi, Z. Zhang, W. Yu, F. Lockwood and E. Grulke, Appl. Phys. Lett., 2001, 79, 2252–2254 CrossRef CAS.
  59. C.-W. Nan, R. Birringer, D. R. Clarke and H. Gleiter, J. Appl. Phys., 1997, 81, 6692–6699 CrossRef CAS.
  60. S. T. Huxtable, D. G. Cahill, S. Shenogin, L. Xue, R. Ozisik, P. Barone, M. Usrey, M. S. Strano, G. Siddons and M. Shim, Nat. Mater., 2003, 2, 731–734 CrossRef CAS PubMed.
  61. W. Yu, H. Xie, L. Chen, Y. Li and D. Li, 14th International Heat Transfer Conference, 2010, vol. 6, pp. 569–573 Search PubMed.
  62. T. T. Baby and S. Ramaprabhu, J. Appl. Phys., 2010, 108, 124308 CrossRef.
  63. M. Martin-Gallego, R. Verdejo, M. Khayet, J. M. O. de Zarate, M. Essalhi and M. A. Lopez-Manchado, Nanoscale Res. Lett., 2011, 6, 1–7 CrossRef PubMed.
  64. T. T. Baby and R. Sundara, J. Phys. Chem. C, 2011, 115, 8527–8533 CAS.
  65. T. T. Baby and S. Ramaprabhu, Nanoscale Res. Lett., 2011, 6, 1 CrossRef PubMed.
  66. W. Yu, H. Xie, X. Wang and X. Wang, Phys. Lett. A, 2011, 375, 1323–1328 CrossRef CAS.
  67. T. T. Baby and S. Ramaprabhu, J. Mater. Chem., 2011, 21, 9702–9709 RSC.
  68. S. J. Aravind and S. Ramaprabhu, J. Appl. Phys., 2011, 110, 124326 CrossRef.
  69. Z. Sun, S. Pöller, X. Huang, D. Guschin, C. Taetz, P. Ebbinghaus, J. Masa, A. Erbe, A. Kilzer and W. Schuhmann, Carbon, 2013, 64, 288–294 CrossRef CAS.
  70. P. Dhar, S. S. Gupta, S. Chakraborty, A. Pattamatta and S. K. Das, Appl. Phys. Lett., 2013, 102, 163114 CrossRef.
  71. A. Ghozatloo, M. Shariaty-Niasar and A. M. Rashidi, Int. Commun. Heat Mass Transfer, 2013, 42, 89–94 CrossRef CAS.
  72. M. Kole and T. Dey, J. Appl. Phys., 2013, 113, 084307 CrossRef.
  73. S. S. Gupta, V. M. Siva, S. Krishnan, T. Sreeprasad, P. K. Singh, T. Pradeep and S. K. Das, J. Appl. Phys., 2011, 110, 084302 CrossRef.
  74. Y. Yang, A. Oztekin, S. Neti and S. Mohapatra, ASME/JSME 2011 8th Thermal Engineering Joint Conference, American Society of Mechanical Engineers, 2011, vol. 44448, pp. 30087–30087. Search PubMed.
  75. T. T. Baby and R. Sundara, AIP Adv., 2013, 3, 012111 CrossRef.
  76. Z. Hajjar, A. Morad Rashidi and A. Ghozatloo, Int. Commun. Heat Mass Transfer, 2014, 57, 128–131 CrossRef CAS.
  77. S. S. Park and N. J. Kim, J. Ind. Eng. Chem., 2014, 20, 1911–1915 CrossRef CAS.
  78. J. Liu, F. Wang, L. Zhang, X. Fang and Z. Zhang, Renewable Energy, 2014, 63, 519–523 CrossRef CAS.
  79. H. Akhavan-Zanjani, M. Saffar-Avval, M. Mansourkiaei, M. Ahadi and F. Sharif, J. Dispersion Sci. Technol., 2014, 35, 1230–1240 CrossRef CAS.
  80. A. M. Haque, S. Kwon, J. Kim, J. Noh, S. Huh, H. Chung and H. Jeong, J. Cent. South Univ., 2015, 22, 3202–3210 CrossRef.
  81. G.-J. Lee and C. K. Rhee, J. Mater. Sci., 2014, 49, 1506–1511 CrossRef CAS.
  82. W. Ma, F. Yang, J. Shi, F. Wang, Z. Zhang and S. Wang, Colloids Surf., A, 2013, 431, 120–126 CrossRef CAS.
  83. R. Shende and R. Sundara, Sol. Energy Mater. Sol. Cells, 2015, 140, 9–16 CrossRef CAS.
  84. J. Eaton and J. Johnston, AIAA J., 1981, 19, 1093–1100 CrossRef.
  85. J. Nie and B. F. Armaly, Int. J. Heat Mass Transfer, 2002, 45, 2431–2438 CrossRef.
  86. M. Savari, S. Rashidi, A. Amiri, M. Shanbedi, S. Zeinali Heris and S. N. Kazi, Numer. Heat Transfer, Part A, 2016, 70, 103–116 CrossRef CAS.
  87. S. J. Aravind and S. Ramaprabhu, RSC Adv., 2013, 3, 4199–4206 RSC.
  88. A. Heshmati, H. Mohammed and A. Darus, Appl. Math. Comput., 2014, 240, 368–386 CrossRef.
  89. M. Shanbedi, S. Z. Heris, A. Amiri and H. Eshghi, J. Taiwan Inst. Chem. Eng., 2016, 60, 547–554 CrossRef CAS.

Footnote

Electronic supplementary information (ESI) available. See DOI: 10.1039/c6ra22365f

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