Home CFD analysis of particle shape and Reynolds number on heat transfer characteristics of nanofluid in heated tube
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CFD analysis of particle shape and Reynolds number on heat transfer characteristics of nanofluid in heated tube

  • Savas Evran EMAIL logo and Mustafa Kurt
Published/Copyright: June 22, 2024

Abstract

Various nanoparticles have been used to increase the heat transfer characteristics (HTC) of nanofluids in the heated tube. The use of various shapes of the same nanoparticle can have major impact on the HTC. In this study, computational fluid dynamics (CFD) analysis of the impact of particle shape (Brick and Platelet) and Reynolds (Re) number (4,500, 6,000, 7,500, and 9,000) on the HTC of nanofluid in the heated tube was carried out in accordance with Taguchi method. Heat transfer coefficient, Nusselt (Nu) number, performance evaluation criteria, and average static pressure drop were chosen as HTC. CFD analyses for 1% Fe3O4 nanofluids in ANSYS Fluent software were performed in accordance with L8 orthogonal array. Particle shape and Re number were selected as the first and second factors, respectively. Signal/noise analysis was used to decide optimum levels and impact direction on HTC for each factor, whereas analysis of variance was implemented to define the importance levels and percentage impact ratios of the factors. According to the results obtained from the study, the nanofluids with platelet nanoparticles have a higher impact on the heat transfer coefficient compared to Brick nanoparticles. Although the increase in the Re number causes an increase in the heat transfer coefficient, Nu number, and average static pressure drop, it does not have any effect on the performance evaluation criteria. The results obtained from this study can be used as a guidance for experimental studies.

Nomenclature

b l

base fluid

CFD

computational fluid dynamics

D b

generation of turbulence kinetic energy due to buoyancy

D k

generation of turbulence kinetic energy due to the mean velocity gradients

F

external force

g

gravity

HTC

heat transfer characteristics

h

heat transfer coefficient

J j

diffusion flux

k eff

effective conductivity

k

turbulence kinetic energy

Nu

Nusselt number

n l

nanofluid

PEC

performance evaluation criteria

Q

heat transfer rate

Re

Reynolds number

S h

energy source

S k and S ϵ

user defined source terms

S m

source

S/N

signal/noise

T i and T o

inlet and outlet temperature

t

time

U

specific total energy

v

velocity vector

ρ

fluid density

µ

viscosity

ϵ

rate of dissipation

σ k

turbulent Prandtl numbers for k

τ ̿

stress tensor

Φ

volume fraction

σ ε

turbulent Prandtl numbers for ε

μ t

eddy viscosity

P

pressure drop

Ω İ Ɉ

mean rate-of-rotation tensor

1 Introduction

The energy needs may increase day by day in many industries and research has been carried out on carbon emissions and energy consumption [1]. Especially in heat energy, the usage of nanofluids has become extensive to increase efficiency. Many researchers [2,3] have analyzed improving the thermal conductivity by using nanofluids. Nanofluids are fluids made of nanoparticles such as metals, carbides, and ceramics using a base liquid [4,5]. Due to the several improved physical properties of nanofluids, they are subject to implementation in many sectors such as energy systems [6] and solar collectors [7], electronics cooling system [8], nuclear power plants [9], heat exchangers [10], microfluidics [11], enhanced oil recovery [12], impingement jets [13], renewable energy [14], combustions [15], porous media [16], etc. Different mathematical methods have been presented on the thermal conductivity of nanofluids and several approach and empirical relations were used for these methods [17,18]. Fe3O4 has been used as nanoparticle in many studies [19,20,21] to create nanofluids. Additionally, different nanoparticles such as Cu [22], Al2O3 [23], CuO [24], TiO2 [25], ZnO [26], Ag [27], MWCNT [28], Ni [29], SiO2 [30], ZrO2 [31], CNT [32], and Au [33] have been the subject of many studies. Several research works have been done, such as improving performance and heat transfer, using nanofluids. Maddah et al. [34] examined the HTC of nanofluids and determined that thermal conductivity is affected by the change in volume fractions of the particles. They also found that Re number has key effects on the Nusselt (Nu) number and friction factor. Barik et al. [35] reported the impact of duct Re number on the heat transfer performances and decided that increasing duct Re number can also cause an increase in Nu number. Additionally, they detected that increasing nozzle Re number can also lead to a rise in pump power. They applied turbulent flow in the calculations. Mir et al. [36] examined the impact of volume fraction of nanoparticles on overall Nu number and determined that the rise in nanoparticle volume fraction can cause a rise in Nu number of nanofluids. In analysis, they applied Re numbers as 150, 300, 500, and 700. Zhang et al. [37] obtained nanofluids using Fe3O4 nanoparticles and water and they examined the variation among mass fraction and convective heat transfer for these nanofluids. They also discussed the trend among magnetic field and convective heat transfer. As an outcome of their studies, they found that the increase in Re number leads to an important increase in the convective heat transfer coefficient. Xuan and Li [38] examined the correlation among thermal conductivity and particle volume fraction for nanofluid formed in alumina–water system and found that the increase in volume fraction caused an increase in the thermal conductivity ratio. Additionally, many studies [39,40,41,42,43,44,45] have applied the Taguchi technique for various analyses of nanofluids. As literature research exhibits, many papers are related to heat transfer performance of nanofluids. Most of these studies have experimental and numerical approaches. However, studies with numerical, theoretical and statistical methods are very limited. In the numerical and statistical paper, the heat transfer characteristics (HTC) of nanofluids depending on various particle shapes and Re numbers were discussed using computational fluid dynamics (CFD) and Taguchi methods. The purpose for selecting various particle shapes in the analyses is to examine various thermal conductivity and viscosity for nanofluids. As understood in Table 4, the thermal conductivity and viscosity of the nanofluid including platelet nanoparticles is higher compared to the nanofluid including Brick nanoparticles. Thus, it can also explain the variations in the HTC of the nanofluid. Therefore, more effective HTC may be obtained by utilizing various shaped particle reinforcement for the same nanofluids. Additionally, ANOVA was implemented to govern the contribution fractions of the particle shape on the HTC. Thus, it may be easier to determine which factor has the maximum efficiency on the systems. With all these advantageous aspects, this study can support many contributions to the literature.

2 CFD analysis

CFD analyses for HTC of the nanofluids were carried out using ANSYS Fluent commercial software. In modelling, the pipe was used under the heat flux of 4,000 W/m2. The heat flux was implemented homogeneously on the pipe wall surface. The pipe has a length of 1,000 mm and diameter of 15 mm. 3D computational domain was considered for the pipe flow. 3D domain for pipe in CFD analysis was illustrated in Figure 1.

Figure 1 
               3D domain for tube.
Figure 1

3D domain for tube.

In mesh processing, multi-zone method with free mesh type including hexa-dominant was applied. To ensure homogeneous distribution of the mesh process, face meshing process was applied to the inlet and outlet areas of the pipe. Additionally, inflation method was added. 2,544,000 elements and 2,571,569 nodes were used in the mesh process. Previous study shows that using 425,691 elements was sufficient for the Nu number and fraction factor [46]. Thus, the number of elements and nodes in this study were considered appropriate for mesh operations. Additionally, the enhanced wall treatment including pressure gradient and thermal effects was utilized. Absolute criteria for the continuity, xyz velocities, energy, k and epsilon were considered to be 10−6 and the hybrid method was employed for solution initialization. The realizable kϵ approach in ANSYS Fluent was determined to be viscos model and this model can be stated as follows [47]:

(1) t ( ρ k ) + x ɉ ( ρ k u ɉ ) = x ɉ μ + μ t σ k k x ɉ + D k + D b ρ ϵ Y M + S k ,

(2) t ( ρ ϵ ) + x ɉ ( ρ ϵ u ɉ ) = x ɉ μ + μ t σ ϵ ϵ x ɉ + ρ C 1 S ϵ ρ C 2 ϵ 2 k + υ ϵ + C 1 ϵ ϵ k C 3 ϵ G b + S ϵ ,

(3) C 1 = ma x 0.43 , η η + 5 , η = S k ϵ , S = 2 S i ɉ S i ɉ ,

(4) μ t = ρ C μ k 2 ϵ ,

(5) C μ = 1 A 0 + A s k U * ϵ ,

(6) U * S İ Ɉ S İ Ɉ + Ω İ Ɉ Ω İ Ɉ ,

(7) Ω İ Ɉ = Ω i ɉ 2 ϵ i ɉ k ω k Ω i ɉ = Ω i ̅ ɉ ̅ ϵ i ɉ k ω k ,

(8) A 0 = 4.04 , A S = 6 cos ϕ ,

(9) ϕ = 1 3 cos 1 ( 6 W ) W = S i ɉ S ɉ k S ki S 3 S = S i ɉ S İ Ɉ S i ɉ = 1 2 u ɉ x i + u i x ɉ ,

(10) C 1 ϵ = 1.44 , C 2 = 1.9 , σ k = 1.0 , σ ϵ = 1.2 .

Equations containing continuity, momentum, stress tensor, and energy for pipe flow in ANSYS commercial software can be calculated as follows, respectively [47]:

(11) ρ t + ( ρ v ) = S m ,

(12) t ( ρ v ) + ( ρ v v ) = p + τ ̿ + ρ g + F ,

(13) τ ̿ = μ ( v + v T ) 2 3 v I ,

(14) ( ρ U ) t + . [ v ( ρ U + p ) ] = . k eff T ɉ h ɉ Ɉ ɉ + ( τ ̿ eff . v ) + S h .

3 Statistical analysis

In the statistical analyses, Taguchi method and ANOVA were statistically employed. L8 orthogonal array in Taguchi methodology was used for the grouping of various particle shape and Re number in CFD analyses. Two factors were determined in numerical modeling. The first factor has four levels, whereas the second factor has two levels. Re number was decided to be the first factor, whereas the particle shape was chosen as the second factor. Factors and their levels are established in Table 1.

Table 1

Factors and levels in L8 orthogonal array

Factors Icon Levels
Level 1 Level 2 Level 3 Level 4
Re number Re 4,500 6,000 7,500 9,000
Particle shape PS Brick Platelet

One of the main purposes of this study is to determine the maximum data of the heat transfer characteristic such as heat transfer coefficient, Nu number, performance evaluation criteria (PEC), and average static pressure drop ( P ) . In this context, “Larger is Better” quality characteristic can be considered to achieve maximum responses. The equation for this quality characteristic can be explained as follows [48]:

(15) ( S / N ) LB for HTC = 10 log n 1 i = 1 n ( y i 2 ) 1 .

To detect the factors at the optimum levels and their influence directions on the heat transfer characteristic, analysis of signal-to-noise S/N ratio was statistically applied. Minitab R12 statistical program was implemented in all statistical determinations.

4 Nanofluid analysis

In nanofluid characteristic, 1% Fe3O4 nanofluids were used. Nanoparticles have brick and platelet shapes in this study. In literature, nanoparticles with brick and platelet shapes have been limited, whereas shapes such as spherical, quasi-spherical, polyhedral, irregular, etc., are generally common. Nanoparticles with different shapes can display various properties and these properties can play a key role on heat transfer characteristic. In the study, the nanofluids with 1% Fe3O4 nanoparticle was utilized and water was chosen to be the base fluid. Properties for water [49] and Fe3O4 nanoparticles [50] are exhibited in Table 2.

Table 2

Properties for base fluid and nanoparticle

Properties Symbol Unit Base fluid [49] Nanoparticle [50]
Water Fe3O4
Density ρ kg/m3 998.2 5,200
Specific heat C p J/kg K 4,180 670
Thermal conductivity ҟ W/m K 0.6 6
Viscosity μ kg/ms 0.001003

Volume fraction of nanoparticles in nanofluid can be expressed as follows [51]:

(16) φ = V np V bl + V np .

Density of the nanofluid may be determined as follows [52]:

(17) ρ nl = ρ bl ( 1 φ ) + φ ρ np .

Specific heat in the nanofluid may be calculated as follows [53]:

(18) C p , nl = ( 1 φ ) ρ bl C p , bl + φ ρ np C p , np ρ nl .

Thermal conductivity in the nanofluid may be evaluated as follows [54]:

(19) ҟ nl ҟ l = ҟ p + ( n 1 ) ҟ l + ( n 1 ) ( ҟ p ҟ l ) φ ( n 1 ) ҟ l ( ҟ p ҟ l ) φ + ҟ p .

Viscosity of the nanofluid can be solved as follows [55]:

(20) μ nl = μ bl ( 1 + A 1 φ + A 2 φ 2 ) .

Constants in accordance with thermal conductivity and viscosity based on the nanoparticle shapes are described in Table 3 [54].

Table 3

Constants for nanoparticles [54]

Nanoparticle shape N A 1 A 2
Brick 3.7 1.9 471.4
Platelet 5.7 37.1 612.6

The properties of the nanofluid were found using Eqs (16)–(20) and the results considered are established in Table 4.

Table 4

Properties for nanofluids

Nanofluid Nanoparticle shape Density (kg/m3) Specific heat (J/kg K) Thermal conductivity (W/m K) Viscosity (kg/m s)
1 vol% Fe3O4/water Brick 1040.218 4004.537 0.615844 0.001069
Platelet 1040.218 4004.537 0.621068 0.001437

As can be understood from Table 3, although the nanoparticle shape does not have any impact in the density and specific heat of the nanofluids, it plays a dominant role on thermal conductivity and viscosity. Therefore, variations that may occur in the HTC can be detected in accordance with the thermal conductivity and viscosity of the nanofluids.

5 HTC analysis

In the presented work, the influence of particle shape and Re number on the heat transfer coefficient (h), Nu number, PEC, and ΔP of nanofluid in heated pipe was analyzed as numerically and statistically. Four different Re numbers were considered in the analyses. Re number may be evaluated as follows [56]:

(21) Re = ρ VR µ .

Heat transfer coefficient in nanofluid may be solved as follows [56]:

(22) h = Q A ( T s T l , ave ) .

Heat transfer rate for nanofluid in pipe may be described as follows [56]:

(23) Q = m l c P ( T o T i ) .

Nu number of nanofluid may be evaluated as follows [56]:

(24) Nu = hR k .

PEC can be solved as follows [46,57]:

(25) PEC = ( Nu nl / Nu bl ) ( f nl / f bl ) 1 3 .

Pressure drop in accordance with inner pressure and outer pressure can be found as follows [56]:

(26) P = P i P o .

6 Results and discussion

This CFD and statistical study is concerned about the evaluation of influence of particle shape and Re number on the h, Nu number, PEC, and ΔP of nanofluid in heated pipe. CFD analyses for 1% Fe3O4 nanofluids were carried out in accordance with the L8 orthogonal array and mathematical results achieved are presented in Table 5.

Table 5

CFD results for L8 orthogonal array

Test Designation Factors CFD results
Re PS h (W/m2 K) Nu (−) PEC (−) ΔP (Pa)
1 Re1PS1 4,500 Brick 1671.9 40.722 0.998 159.44
2 Re1PS2 4,500 Platelet 1902.2 45.942 1.128 287.69
3 Re2PS1 6,000 Brick 2116.8 51.558 0.998 253.88
4 Re2PS2 6,000 Platelet 2409.3 58.189 1.128 458.13
5 Re3PS1 7,500 Brick 2547.3 62.044 0.998 366.31
6 Re3PS2 7,500 Platelet 2900.6 70.055 1.128 661.06
7 Re4PS1 9,000 Brick 2966.5 72.254 0.998 495.77
8 Re4PS2 9,000 Platelet 3379.0 81.609 1.128 894.73
Overall mean value 2486.7 60.297 1.063 447.13

As described in Table 5, overall mean values of h, Nu number, PEC, and ΔP were calculated to be 2486.7 W/m2 K, 60.297, 1.063, and 447.13 Pa, respectively. S/N ratios corresponding to CFD results based on “the Larger is better” quality characteristic are described in Table 6.

Table 6

S/N ratios of CFD results for L8 orthogonal array

Test Designation Factors S/N ratios (dB)
Re PS Ƞ for h Ƞ for Nu Ƞ for PEC Ƞ for ΔP
1 Re1PS1 4,500 Brick 64.4642 32.1966 −0.0169 44.0519
2 Re1PS2 4,500 Platelet 65.5851 33.2442 1.0464 49.1785
3 Re2PS1 6,000 Brick 66.5136 34.2460 −0.0198 48.0926
4 Re2PS2 6,000 Platelet 67.6378 35.2969 1.0468 53.2198
5 Re3PS1 7,500 Brick 68.1216 35.8540 −0.0194 51.2770
6 Re3PS2 7,500 Platelet 69.2498 36.9088 1.0434 56.4048
7 Re4PS1 9,000 Brick 69.4449 37.1773 −0.0200 53.9056
8 Re4PS2 9,000 Platelet 70.5758 38.2348 1.0428 59.0338

Velocity and temperature contours of CFD results using L8 orthogonal approach in Taguchi methodology are presented in Figures 2 and 3, respectively.

Figure 2 
               CFD velocity contour plots for (a) Re1PS1, (b) Re1PS2, (c) Re2PS1. (d) Re2PS2, (e) Re3PS1, (f) Re3PS2, (g) Re4PS1, (h) Re4PS2.
Figure 2

CFD velocity contour plots for (a) Re1PS1, (b) Re1PS2, (c) Re2PS1. (d) Re2PS2, (e) Re3PS1, (f) Re3PS2, (g) Re4PS1, (h) Re4PS2.

Figure 3 
               CFD temperature contour plots for (a) Re1PS1, (b) Re1PS2, (c) Re2PS1, (d) Re2PS2, (e) Re3PS1, (f) Re3PS2, (g) Re4PS1, (h) Re4PS2.
Figure 3

CFD temperature contour plots for (a) Re1PS1, (b) Re1PS2, (c) Re2PS1, (d) Re2PS2, (e) Re3PS1, (f) Re3PS2, (g) Re4PS1, (h) Re4PS2.

As understood from Figure 2, the velocity of the nanofluid rises from the pipe walls to the center of the pipe. This finding can be described by the resistance of the fluid against the pipe walls. As defined in Figure 3, the nanofluid temperature reduces from the pipe walls to the pipe center. This finding can be clarified by the temperature occurring on the pipe walls by the heat flux data. Temperature of pipe walls is high, whereas the temperature decreases towards the center of the pipe. Thus, difference was detected in temperature distribution due to the nanofluid.

6.1 Effect on HTC

To understand the influence of particle shape and Re number on the HTC of nanofluids, CFD analyses were carried out using various levels of different factors. The numerical results achieved by ANSYS Fluent software were evaluated as S/N ratio values to obtain the maximum HTC of nanofluids. Average CFD data corresponding to average S/N ratios were used to define the impact of each particle shape and Re number on the HTC at various levels. Graphs were drawn based on the S/N ratios. Impact of particle shape and Re number on the HTC of nanofluids are displayed in Figure 4.

Figure 4 
                  Main impact plots for (a) h, (b) Nu number, (c) PEC, (d) ΔP.
Figure 4

Main impact plots for (a) h, (b) Nu number, (c) PEC, (d) ΔP.

Figure 4a–d displays that nanofluids containing 1% Fe3O4 nanoparticles with platelet shape have a higher influence on the h, Nu number, PEC, and ΔP compared to brick nanoparticles. This finding may be defined by thermal conductivity and viscosity. This situation is clearly determined in Eqs (19) and (20). The thermal conductivity and viscosity for nanofluid including platelet nanoparticle are greater than nanofluid with brick nanoparticle. The increase in thermal conductivity of nanofluids causes an increase in the h, Nu number, and PEC. Although the increase in the Re number from 4,500 to 9,000 leads to an increase in the h, Nu number, and ΔP, it does not have any effect on the PEC. These findings were supported by the study by Garud and Lee [46]. Additionally, another study [58] showed that increasing Re number causes an increase in h, Nu number, and ΔP.

6.2 Optimal levels of particle shape and Re number

ANOVA is one of the statistical methods and it was employed to define the HTC. ANOVA was implemented to achieve the significance level and percent contribution ratio of particle shape and Re number on the HTC of nanofluids. Analyses were implemented in accordance with 95% confidence level. ANOVA results for h and Nu number are shown in Table 7.

Table 7

ANOVA for h and Nu

Source DF h Nu
Seq SS Adj MS F P % Effect Seq SS Adj MS F P % Effect
Re 3 2,132,963 710,988 231.23 0 90.77 1254.05 418.02 263.94 0 91.84
PS 1 207,561 207,561 67.50 0.004 8.83 106.70 106.70 67.37 0.004 7.81
Error 3 9,224 3,075 0.39 4.75 1.58 0.35
Total 7 2,349,749 100 1365.5 100
R 2 = 99.61% and R 2 (adj) = 99.08 R 2 = 99.65% and R 2 (adj) = 99.19%

According to the F-test results in Table 5, particle shape and Re number were determined as the most important factors on the heat transfer coefficient. Additionally, Re number has a 90.77% impact on h, whereas particle shape has 8.83% effect. This finding shows that Re number is dominant on h and Nu number compared to the particle shape. For the Nu number, particle shape and Re number were considered as important factors based on F-test results. Re number has a 91.84% influence on the Nu number, whereas particle shape has 7.81% effect. This finding indicates that the influence of turbulent flow on Nu number is more dominant compared to the particle shape. ANOVA outcomes for the PEC and average static pressure drop are displayed in Table 8.

Table 8

ANOVA for PEC and ΔP

Source DF PEC ΔP
Seq SS Adj MS F P % Effect Seq SS Adj MS F P % Effect
Re 3 0 0 ** 0 248,556 82,852 12.14 0.035 62.04
PS 1 0.0338 0.0338 ** 100 131,638 131,638 19.29 0.022 32.86
Error 3 0 0 0 20,468 6,823 5.11
Total 7 0.0338 100 400,663 100
R 2 = 100.00% and R 2 (adj) = 100.00% R 2 = 94.89% and R 2 (adj) = 88.08%

ANOVA results in Table 6 show that Re number has no impact on the PEC. But, the impact of particle shape is great. Thus, the denominator of F-test was calculated as zero for the PEC. According to this outcome, the one major factor was determined to be the particle shape. Therefore, the particle shape of nanoparticle has a 100% influence on PEC, whereas RE number has a 0% influence. According to the F-test results on the average static pressure drop, both particle shape and Re number were found to be important factors. According to the influence ratios, the Re number had a 62.04% influence on the average static pressure drop, whereas the particle shape had a 32.86% influence. This finding displays that the flow velocity in turbulent flow is greater than the effect of particle shape. The key purpose of the presented work is to determine the optimum levels of factors to obtain the highest HTC of nanofluids. In this context, the numerically calculated h, Nu number, PEC, and ΔP of nanofluid results were converted into S/N ratios. Average CFD results and S/N ratios were calculated for each level of particle shape and Re number. Overall CFD data and S/N ratios at all levels of particle shape and Re number according to h and Nu are exhibited in Table 9.

Table 9

Mean results for h and Nu

Level h Nu
S/N ratio (dB) Mean value (W/m2 K) S/N ratio (dB) Mean value
Re PS Re PS Re PS Re PS
1 65.02 67.14 1,787 2326 32.72 34.87 43.33 56.64
2 67.08 68.26 2,263 2648 34.77 35.92 54.87 63.95
3 68.69 2,724 36.38 66.05
4 70.01 3,173 37.71 76.93
Delta 4.99 1.13 1,386 322 4.99 1.05 33.60 7.30
Rank 1 2 1 2 1 2 1 2

The overall results obtained from Table 9 display that the increase in Re number causes an increase in the h and Nu number. Thus, the particle with platelet shape had the optimum impact levels on the h and Nu number, whereas the optimum Re number was determined as 9,000. Therefore, to obtain the maximum h and Nu number, nanofluids including platelet nanoparticles and Re number of 9,000 should be determined. Average data of CFD and S/N ratios at all levels of particle shape and Re number in accordance with the PEC, and average static pressure drop of nanofluid are presented in Table 10.

Table 10

Main results for PEC and ΔP

Level PEC ΔP
S/N ratio (dB) Mean value S/N ratio (dB) Mean value (Pa)
Re PS Re PS Re PS Re PS
1 0.51472 −0.01902 1.0630 0.9978 46.62 49.33 223.60 318.90
2 0.51349 1.04484 1.0629 1.1278 50.66 54.46 356.00 575.40
3 0.51200 1.0627 53.84 513.70
4 0.51143 1.0626 56.47 695.30
Delta 0.0033 1.06387 0.0004 0.1300 9.85 5.13 471.70 256.60
Rank 2 1 2 1 1 2 1 2

The results shown in Table 10 exhibits that the nanofluids with platelet-shaped nanoparticles were determined as the optimum since the maximum PEC and static pressure drop were reached while using platelet-shaped nanoparticles. Additionally, because no impact of Re number on the PEC was detected, the ideal level for Re number cannot be analyzed. It indicates that the increase in the Re number in the average static pressure drop leads to an increase in the pressure drop. Therefore, the ideal level for Re number on pressure drop was observed as 9,000. The maximum static pressure drop can be achieved by applying nanofluid including platelet nanoparticles and Re number of 9,000.

6.3 Estimation of optimal heat transfer responses

Particle shape and Re numbers at the optimal levels were selected to achieve the maximum HTC of nanofluids. S/N ratio analysis was applied to decide optimum levels and average results were evaluated. ANOVA was implemented and significant particle shape and Re number based on F-test results were discussed. Determination of predicted HTC regarding S/N ratio and ANOVA results at 95% confidence level can be solved as follows [48]:

(27) μ est = PS opt ̅ + Re opt ̅ T ave ̅ ,

where PS opt ̅ and Re opt ̅ for the heat transfer coefficient were calculated as 3,173 and 2,648 W/m2 K, whereas PS opt ̅ and Re opt ̅ for the Nusellt number were solved as 76.93 and 63.95, respectively. Additionally, PS opt ̅ and Re opt ̅ for the PEC were determined as 1.063 and 1.1278, whereas PS opt ̅ and Re opt ̅ for the average static pressure drop were found as 695.30 and 575.40 Pa, respectively. T ave ̅ for the h, Nu number, PEC, and ΔP were calculated as 2486.7 W/m2 K, 60.297, 1.063, and 447.13 Pa, respectively. These data are substituted in Eq. (27) and the predicted Taguchi results are exhibited in Table 11.

Table 11

CFD and estimated optimal heat transfer responses

HTC h (Re4PS2) Nu (Re4PS2) PEC (ReallPS2) ΔP (Re4PS2)
CFD results 3379.0 W/m2 K 81.609 1.128 894.73
Taguchi results 3334.3 W/m2 K 80.583 1.128 823.57
% differences 1.32 1.16 0 7.95

7 Validation

Numerical and statistical results of Nu number and PEC of nanofluids were compared with theoretical approach. In this context, Nu number and Darcy friction factor were solved theoretically. Calculations for validation were carried out for particle shape and Re numbers under the optimal levels. Theoretical Nu number and Darcy friction factors were considered using Eqs (28) [59] and (29) [60], respectively.

(28) Nu ̅ R = 0.023 Re 0.8 Pr 0.4 ,

(29) 1 f = 2 log e / R 3.7 + 2.52 R e f .

CFD, estimated Taguchi results, and theoretical results obtained for Nu number and PEC utilizing particle shape and Re number under the ideal levels are exhibited in Table 12.

Table 12

Theoretical validation of CFD results

Nu (Re4PS2) % Difference PEC (ReallPS2) % Difference
CFD Formula CFD Formula
81.609 81.624 0.02 1.128 1.132 0.35

Table 12 shows that while the difference among CFD and theoretical data of the Nu number was found to be 0.02%, the difference for the PEC was determined to be 0.35%. These findings prove the precision of the numerical and statistical data.

8 Conclusion

In the presented study, the impact of particle shape and Reynolds (Re) number on the h, Nu number, PEC, and ΔP of nanofluid in heated tube was analyzed in accordance with Taguchi method. Fe3O4 was selected as nanoparticle and so 1% Fe3O4 nanofluids for CFD analyses was used. Particle shape and Re number were assumed as the first and second factors. Brick and platelet were considered as particle shapes. CFD calculations for HTC of nanofluids were carried out by ANSYS Fluent commercial software regarding L8 orthogonal range utilizing Taguchi methodology. A pipe of 1,000 mm length and 15 mm diameter was implemented in numerical modeling. The heat flux was chosen as 4,000 W/m2. S/N ratio analysis was implemented to find optimum levels and impact trend on HTC for each factor, whereas ANOVA was conducted to release the dominant levels and percentage impact rates of the factors. The key results obtained from this study are summarized below:

  • Increasing Re number from 4,500 to 9,000 causes an increase in HTC of the nanofluid.

  • The influence of platelet nanoparticles on the HTC of the nanofluid is greater than brick nanoparticles.

  • The maximum heat transfer characteristic of the nanofluid is achieved by using platelet nanoparticles and Re number of 9,000.

  • According to the F-test data in the ANOVA results, particle shape is detected as a significant factor. However, Re number was determined to be a significant factor on heat transfer coefficient, Nu number, and average static pressure drop, whereas no impact was found on the PEC.

  • The contribution ratio of particle shape on the heat transfer coefficient, Nu number, PEC, and average static pressure drop is found to be 8.83, 7.81, 100, and 32.86%, respectively.

  • The contribution ratio of Re number on heat transfer coefficient, Nu number, PEC, and average static pressure drop is decided to be 90.77, 91.84, 0, and 62.04%, respectively.

  • The difference between numerical and Taguchi prediction results obtained for heat transfer coefficient, Nu number, performance evaluation criteria, and average static pressure drop was determined to be 1.32, 1.16, 0, and 7.95%, respectively.

  • In the validation calculations, the difference between the CFD and theoretical results for the Nu number was found to be 0.02%, whereas the difference between the CFD and theoretical data obtained for the performance evaluation criteria was solved to be 0.35%.

  • The temperature of the nanofluid reduces from the pipe walls to the center of the pipe, whereas the nanofluid velocity increases from the pipe walls to the center.

  1. Funding information: The authors state no funding involved.

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors state no conflict of interest.

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Received: 2024-03-14
Revised: 2024-04-04
Accepted: 2024-05-22
Published Online: 2024-06-22

© 2024 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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