Literature DB >> 34238991

Unsteady squeezing flow of Cu-Al2O3/water hybrid nanofluid in a horizontal channel with magnetic field.

Najiyah Safwa Khashi'ie1, Iskandar Waini2, Norihan Md Arifin3, Ioan Pop4.   

Abstract

The proficiency of hybrid nanofluid from Cu-Al2O3/water formation as the heat transfer coolant is numerically analyzed using the powerful and user-friendly interface bvp4c in the Matlab software. For that purpose, the Cu-Al2O3/water nanofluid flow between two parallel plates is examined where the lower plate can be deformed while the upper plate moves towards/away from the lower plate. Other considerable factors are the wall mass suction/injection and the magnetic field that applied on the lower plate. The reduced ordinary (similarity) differential equations are solved using the bvp4c application. The validation of this novel model is conducted by comparing a few of numerical values for the reduced case of viscous fluid. The results imply the potency of this heat transfer fluid which can enhance the heat transfer performance for both upper and lower plates approximately by 7.10% and 4.11%, respectively. An increase of squeezing parameter deteriorates the heat transfer coefficient by 4.28% (upper) and 5.35% (lower), accordingly. The rise of suction strength inflates the heat transfer at the lower plate while the presence of the magnetic field shows a reverse result.

Entities:  

Year:  2021        PMID: 34238991      PMCID: PMC8266913          DOI: 10.1038/s41598-021-93644-4

Source DB:  PubMed          Journal:  Sci Rep        ISSN: 2045-2322            Impact factor:   4.379


Introduction

The enrichment of heat transfer performance for the working fluid in cooling/heating appliances with optimum use of cost and energy has been the main concern for industrial and societal benefits. The addition of a single nanoparticle into a host working fluid is originated by Choi[1] to enhance the base fluid’s thermal conductivity. Since then, many investigations were conducted through experimental works or fundamental studies (computational boundary layer flow) with less cost and time consumption. The model by Buongiorno[2] which related to the effects of Brownian motion and thermopheresis as well as the model by Tiwari and Das[3], are widely used by many researchers in the computational analysis of the nanofluid’s flow. Using the spectral relaxation method, Oyelakin et al.[4] solved the Buongiorno’s model of Casson nanofluid flow with the inclusion of slip and convective conditions, magnetic field and thermal radiation. Further, Oyelakin et al.[5] discussed the three-dimensional flow of unsteady magnetohydrodynamics (MHD) Casson nanofluid utilizing the Buongiorno’s model. Another interesting works regarding the Buongiorno’s model of nanofluid can be read from these papers[6-11]. Meanwhile, Karmakar et al.[12] scrutinized the stagnation point flow of carbon nanotubes (CNT)-water nanofluid towards a stretching sheet with convective boundary condition. In recent times, the combination of a base fluid with suspended dissimilar nanoparticles is experimentally conducted to create a superior nanocomposite liquid known as hybrid nanofluid. The hybrid nanofluid’s correlations by Takabi and Salehi[13] and Devi and Devi[14] were extensively used in the estimation of the thermophysical properties. The advantages of hybrid nanofluid in augmenting the heat transfer performance could also be found in these references[15-21]. For the distant future of the cooling/heating applications, there are tremendous demands in the investigation of both internal and external hybrid nanofluid flows. Acharya et al.[22] observed the temperature profile of working fluid with Cu-TiO2 nanosuspension was greater than single nanofluids when it was streaming over a revolving disk. The inclined magnetic field with a suitable inclination angle was shown as one of the potential factors in augmenting the thermal rate of the hybrid nanofluid[23]. Further assessment of the nonlinear radiation and magnetic field effects have been conducted by Acharya et al.[24] for hybrid Ag-Fe3O4/kerosene nanofluid flow over a permeable stretching sheet. The Cu-Al2O3/water hybrid nanofluid flow past an exponentially stretching/shrinking surface was recently studied by Wahid et al.[25,26]. The squeezing flow which emerged from the moving boundaries is significant in polymer processing, lubrication equipment, molding’s injection, and compression including the hydrodynamical machines. The connection between the squeezing flow and the loaded bearings’ performance in engines including the phenomenon of adhesion has been highlighted by Jackson[27]. Stefan[28] used lubrication approximation to initiate his work on squeezing flow. Meanwhile, other early works considering numerical schemes on the squeezing flow were studied by Verma[29] and Singh et al.[30]. Hamza[31] inspected the squeezing flow and highlighted the impact of the suction and injection parameters. Other interesting papers reflecting the squeezing viscous flow have been debated in Ahmad et al.[32], Shah et al.[33], Khan et al.[34], Magalakwe et al.[35] and Basha[36]. Later, the analysis of squeezing flow in nanofluids was also considered by a few of researchers. The time-dependent bioconvection flow containing motile gyrotactic microorganisms was solved by Raees et al.[37] using Buongiorno’s model of nanofluid. Hayat et al.[38] analyzed the unsteady squeezed flow of nanofluid with the presence of magnetic field while Hayat et al.[39] scrutinized the effect of couple stress due to time-dependent applied magnetic field. Both Hayat et al.[38,39] implemented the Buongiorno nanofluid model which indirectly examined any specific nanoparticles. Recently, Acharya et al.[40] analyzed the simultaneous effects of chemical reaction, magnetic field, and second-order slip on the bioconvection nanofluid squeezing flow between two parallel plates. Meanwhile, interesting work of the squeezing hybrid nanofluid with Fe3O4-MoS2 and the combination of water and ethylene glycol for the base fluid was conducted by Salehi et al.[41]. The impact of radiation from the solar energy on the Cu-Al2O3/water hybrid nanofluid inside a channel was deliberated by Acharya[42]. Another interesting aspect of the internal hybrid nanofluid flow inside a channel also has been scrutinized by Ikram et al.[43] and Islam et al.[44]. Detail description of previous works[37-44] concerning the internal flow between two plates is presented in Table 1 which highlights the gap between previous works and the present study.
Table 1

Detail description of references concerning the internal flow between two plates.

ReferencesSingle/Hybrid NanofluidDescription of lower and upper platesAdditional physical parametersMethod of solution
Raees et al.[37]Unsteady flow of single nanofluid (Buongiorno model)Both lower and upper plates are impermeableBioconvectionHomotopy Analysis Method
Hayat et al.[38]Unsteady flow of single nanofluid (Buongiorno model)Lower plate is permeable and stretchableMagnetic fieldHomotopy Analysis Method
Hayat et al.[39]Unsteady flow of single nanofluid (Buongiorno model)Lower plate is permeable and stretchableMagnetic field and couple stress viscosity effectHomotopy Analysis Method
Acharya et al.[40]Single nanofluid flow (Buongiorno model)Bioconvection, magnetic field, chemical reaction and second order slipRunge–Kutta-Fehlberg method
Salehi et al.[41]Unsteady flow of hybrid Fe3O4-MoS2/mixture of ethylene glycol–water (correlations of hybrid nanofluid as in Devi and Devi[14])Lower plate is impermeable and staticMagnetic field and heat generationAkbari and Ganji's method
Acharya[42]Hybrid Cu-Al2O3/water (correlations of hybrid nanofluid as in Takabi and Salehi[13])

Lower plate is stretchable

Upper plate is permeable

Solar radiationShooting method
Ikram et al.[43]Hybrid Ag-TiO2/water (correlations of hybrid nanofluid as in Takabi and Salehi[13])Magnetic field, natural convection and heat generationLaplace transform method
Islam et al.[44]Micropolar hybrid GO-Cu/water (correlations of hybrid nanofluid as in Takabi and Salehi[13])

Lower plate is stretchable

Upper plate is permeable

Magnetic field, thermal radiation and rotating systemHomotopy Analysis Method
Detail description of references concerning the internal flow between two plates. Lower plate is stretchable Upper plate is permeable Lower plate is stretchable Upper plate is permeable Inspired from the existing literature while fulfilling the available research gaps, this work aims to analyze the time-dependent squeezing flow of hybrid Cu-Al2O3/water nanofluid in a horizontal channel (between two parallel plates) with the magnetic field effect. The physical geometry of the lower plate is presumed as permeable and stretchable. Our main focus is to analyze the features of hybrid nanofluid flow like distribution of velocity, skin friction, temperature, and thermal rate for several physical parameters such as suction/injection, stretching, unsteadiness squeezing, the magnetic and volumetric concentration of the nanoparticles. In long term, this study is can be applied in designing an optimum thermal process for example in refrigeration systems and heat pumps using relevant physical sources. To accomplish the objectives, the single-phase mathematical model of Cu-Al2O3/water is formulated based on this physical problem and then, transformed into reduced differential equations via the similarity transformation. The bvp4c application is completely used for the results’ generation and validated based on the available numerical values from the previous works. This study is novel and original which considers a time-dependent Cu-Al2O3/water hybrid nanofluid flow with different boundary conditions as compared to the existing references in Table 1.

Mathematical model

Physical assumptions and thermophysical correlations

Cu-Al2O3/water formation is considered to flow between two infinite parallel plates, as shown in Fig. 1. The upper plate is placed at from the lower plate, while the upper plate with velocity is moving towards (squeezing) the lower plate. Further assumption is the lower and upper plates are maintained at fixed temperatures and , respectively. Meanwhile, the porous lower plate is included in the physical illustration for the possible fluid suction/injection with the wall mass velocity is denoted as ; for suction, for injection and corresponds to an impermeable plate. Also, the lower plate is stretchable with linear velocity while the inclusion of time-dependent magnetic field is formulated with (see Hayat et al.[38,39]).
Figure 1

Physical illustration with coordinate system.

Physical illustration with coordinate system. Under these assumptions and using the hybrid nanofluid model proposed by Takabi and Salehi[13], the governing conservation equations are[37-39].where . The associate conditions at the lower and upper plates are (see Raees et al.[37] and Hayat et al.[38,39])Here and are the velocities along and directions and is the hybrid nanofluid temperature. For the evaluation of the thermophysical properties (see Table 2), we adopt the correlations by Takabi and Salehi[13] which are feasible and correct based on the experimental validation. These correlations are built based on the physical assumptions. Meanwhile, Table 3 display the the physical properties of the pure water and nanoparticles.
Table 2

Hybrid nanofluid’s correlations[13].

PropertiesHybrid Nanofluid
Density \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( \rho \right)$$\end{document}ρ\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\rho _{{hnf}} = \left( {1 - \phi _{{hnf}} } \right)\rho _{f} + \phi _{1} \rho _{{s1}} + \phi _{2} \rho _{{s2}}$$\end{document}ρhnf=1-ϕhnfρf+ϕ1ρs1+ϕ2ρs2
Heat Capacity \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( {\rho C_{p} } \right)$$\end{document}ρCp\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( {\rho C_{p} } \right)_{{hnf}} = \left( {1 - \phi _{{hnf}} } \right)\left( {\rho C_{p} } \right)_{f} + \phi _{1} \left( {\rho C_{p} } \right)_{{s1}} + \phi _{2} \left( {\rho C_{p} } \right)_{{s2}}$$\end{document}ρCphnf=1-ϕhnfρCpf+ϕ1ρCps1+ϕ2ρCps2
Dynamic Viscocity \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( \mu \right)$$\end{document}μ\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\frac{{\mu _{{hnf}} }}{{\mu _{f} }} = \frac{1}{{\left( {1 - \phi _{{hnf}} } \right)^{{2.5}} }}$$\end{document}μhnfμf=11-ϕhnf2.5
Thermal Conductivity \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( k \right)$$\end{document}k\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\frac{{k_{{hnf}} }}{{k_{f} }} = \left[ {\frac{\begin{gathered} \left( {\frac{{\phi _{1} k_{1} + \phi _{2} k_{2} }}{{\phi _{{hnf}} }}} \right) + 2k_{f} + 2\left( {\phi _{1} k_{1} + \phi _{2} k_{2} } \right) \hfill \\ - 2\phi _{{hnf}} k_{f} \hfill \\ \end{gathered} }{\begin{gathered} \left( {\frac{{\phi _{1} k_{1} + \phi _{2} k_{2} }}{{\phi _{{hnf}} }}} \right) + 2k_{f} - \left( {\phi _{1} k_{1} + \phi _{2} k_{2} } \right) \hfill \\ + \phi _{{hnf}} k_{f} \hfill \\ \end{gathered} }} \right]$$\end{document}khnfkf=ϕ1k1+ϕ2k2ϕhnf+2kf+2ϕ1k1+ϕ2k2-2ϕhnfkfϕ1k1+ϕ2k2ϕhnf+2kf-ϕ1k1+ϕ2k2+ϕhnfkf
Electrical Conductivity \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( \sigma \right)$$\end{document}σ\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\frac{{\sigma _{{hnf}} }}{{\sigma _{f} }} = \left[ {\frac{\begin{gathered} \left( {\frac{{\phi _{1} \sigma _{1} + \phi _{2} \sigma _{2} }}{{\phi _{{hnf}} }}} \right) + 2\sigma _{f} + 2\left( {\phi _{1} \sigma _{1} + \phi _{2} \sigma _{2} } \right) \hfill \\ - 2\phi _{{hnf}} \sigma _{f} \hfill \\ \end{gathered} }{\begin{gathered} \left( {\frac{{\phi _{1} \sigma _{1} + \phi _{2} \sigma _{2} }}{{\phi _{{hnf}} }}} \right) + 2\sigma _{f} - \left( {\phi _{1} \sigma _{1} + \phi _{2} \sigma _{2} } \right) \hfill \\ + \phi _{{hnf}} \sigma _{f} \hfill \\ \end{gathered} }} \right]$$\end{document}σhnfσf=ϕ1σ1+ϕ2σ2ϕhnf+2σf+2ϕ1σ1+ϕ2σ2-2ϕhnfσfϕ1σ1+ϕ2σ2ϕhnf+2σf-ϕ1σ1+ϕ2σ2+ϕhnfσf
Table 3

Thermophysical properties for pure water and nanoparticles[45,46].

Thermophysical PropertiesH2ONanoparticles
Al2O3Cu
\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\rho {\text{~}}\left( {{\text{kgm}}^{{ - 3}} } \right)$$\end{document}ρkgm-3997.139708933
\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$C_{p} \left( {{\text{Jkg}}^{{ - 1}} {\text{K}}^{{ - 1}} } \right)$$\end{document}CpJkg-1K-14179765385
\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$k{\text{~}}\left( {{\text{Wm}}^{{ - 1}} {\text{K}}^{{ - 1}} } \right)$$\end{document}kWm-1K-10.613040400
\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\sigma {\text{~}}\left( {sm^{{ - 1}} } \right)$$\end{document}σsm-10.053.69 \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\times 10^{7}$$\end{document}×1075.96 \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\times 10^{7}$$\end{document}×107
Hybrid nanofluid’s correlations[13]. Thermophysical properties for pure water and nanoparticles[45,46].

Reduced differential equations

According to Raees et al.[37] and Hayat et al.[38,39], the suitable dimensionless variables are Hence, substituting (5) into Eqs. (2)-(4), the ODEs and boundary conditions arewhere refers to the stretching lower plate and denotes the fixed/static lower plate. Another dimensionless parameters are the unsteadiness squeezing parameter , magnetic parameter , suction parameter , Prandtl number and constant . These parameters are defined as[37-39] In this work, we set which in accordance with Hayat et al.[38,39]. Further, we notice that Eq. (6) is compatible with the reduced momentum equation in Hayat et al.[38] and Hayat et al.[39] (if the couple stress parameter is zero) with the exclusion of the hybrid nanoparticles or (regular fluid). The reduced skin friction coefficients and local Nusselt numbers at lower and upper plates are[37-39]where

Numerical methods and validation test

In solving the boundary layer equations, there are many methods proposed by the researchers such as homotopy analysis method (HAM), shooting technique, Keller-box method, Runge–Kutta method, Laplace transform and many others. A concise review of the numerical methods which used to solve the boundary layer equations specifically for Casson fluid was discussed by Verma and Mondal[47]. Meanwhile, Rai and Mondal[48] reviewed spectral methods like spectral relaxation method, spectral homotopy analysis method, spectral quasi-linearization method and spectral local linearization method in solving fluid flow problem. Another interesting technique namely multi domain bivariate quasi-linearization method was used by Oyelakin et al.[49] in solving mixed convection flow of Casson nanofluid. Meanwhile, the bvp4c solver procurable in the Matlab software was also widely used by many researchers to solve the nonlinear ODEs. It is validated that the results of limiting cases using bvp4c is in accordance with the previously published results that used another methods (i.e., analytical, shooting, Keller-box method). The finite difference method under subclass 3-stage Lobatto IIIa scheme was programmed into the bvp4c solver through a general syntax sol = bvp4c (@OdeBVP, @OdeBC, solinit, options). For the completion of the numerical solutions in this study, Eqs. (6) to (8) are solved by transforming it first into the language of the bvp4c code as follows:where and implies the boundary conditions at lower and upper plates, respectively. The bvp4c solver will code Eqs. (13) and (15) into @OdeBVP while the condition (16) is coded into @OdeBC. Generally, the solinit function refers to the initial mesh point and guesses at the mesh points. However, modifications are necessary for the solinit and options functions in the bvp4c syntax to solve the present internal flow problem which affirms the novelty of this work. The asymptotical profile (for usual boundary layer flow) is necessary when the problem is dealing with the external flow over an infinite surface where these profiles must satisfy the free stream condition. However, in this work, the validation part is based on the comparison with previous similar works as presented in Tables 4 and 5. The validation is important to highlight the precision of the present model and code. Hence, the numerical values are compared with Hayat et al.[38,39] (main references) as displayed in Tables 4 and 5 which shows identical results when suction and magnetic parameters are considered.
Table 4

Comparative values of -lower plate and -upper plate when , , with various and .

\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$M$$\end{document}M\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$S$$\end{document}S\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$f^{\prime\prime}\left( 0 \right)$$\end{document}f0\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$f^{\prime\prime}\left( 1 \right)$$\end{document}f1
PresentHayat et al.[39]PresentHayat et al.[39]
00.5−7.4111525−7.4111534.71330284.713303
10.5−7.5916177−7.5916184.73901654.739017
40.5−8.1103342−8.1103344.82025114.820251
90.5−8.9100956−8.9100964.96486984.964870
40.0−4.5878911−4.5878911.84244691.842447
40.3−6.6656620−6.6656623.65369483.653695
40.6−8.8514442−8.8514445.39124755.391248
41.0−11.9485843−11.9485847.59342627.593426
Table 5

Comparative values of -upper plate when and with various , and .

\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$M$$\end{document}M\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$Sq$$\end{document}Sq\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$S$$\end{document}S\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$f^{\prime\prime}\left( 1 \right)$$\end{document}f1
PresentHayat et al.[38]
010.51.8146341.81463
0.2510-1.171551-1.17155
0.2510.51.8081771.80818
0.2500.54.7196564.79166
0.251.50.50.2839480.28395
0.25114.5730164.57302
110.51.7893721.78937
Comparative values of -lower plate and -upper plate when , , with various and . Comparative values of -upper plate when and with various , and .

Results and discussion

The results are generated and graphically presented for the distribution of the skin friction coefficients, velocity, heat transfer rates, and temperature of both upper and lower plates. The value of the Prandtl number is fixed to 6.2 which indicates the use of water at 25 °C while the initial temperature at the lower plate’s wall is represented by so that . Other parameters are controlled within the ranges of (unsteadiness squeezing parameter), (suction/injection parameter), (stretching parameter), and (magnetic parameter). Table 6 shows the variety of , , and . With the consideration of viscous fluid, lower static plate, and the exclusion of magnetic, suction/injection, and squeezing parameters, the internal flow has zero frictions and equal heat transfer rates at both plates. The observation in Table 6 shows that as the stretching parameter increases from to , increases, but the stretching lower plate tends to increase . Further, we analyze four types of fluids: viscous/water , Al2O3-water , Cu-water , and Cu-Al2O3/water which reveals that the Cu-Al2O3/water has the highest heat transfer coefficients at both plates followed by the Cu-water, Al2O3-water, and water. This implies the suitability of Cu-Al2O3/water hybrid nanofluid as an effective coolant in engineering and technology appliances. Since the inclusion of the squeezing parameter can reduce the heat transfer rate at both plates, it is useful to know the exact parameters which can assist the heat transfer performance for this situation. In Table 7, we analyze the difference percentage of the heat transfer rate at both upper and lower plate which can be used for future assessment by other engineers or researchers. This analysis also can help in determining the preferable strength of the parameters either in the augmentation or reduction of the heat transfer in both locations.
Table 6

Numerical values of , , and with various values of the control parameters.

\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$Sq$$\end{document}Sq\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$M$$\end{document}M\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$S$$\end{document}S\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\phi _{1}$$\end{document}ϕ1\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\phi _{2}$$\end{document}ϕ2\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\lambda$$\end{document}λ\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\text{Re} _{x} ^{{1/2}} C_{{f1}}$$\end{document}Rex1/2Cf1\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\text{Re} _{x} ^{{1/2}} C_{{f2}}$$\end{document}Rex1/2Cf2\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$- \text{Re} _{x} ^{{ - 1/2}} Nu_{{x1}}$$\end{document}-Rex-1/2Nux1\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$- \text{Re} _{x} ^{{ - 1/2}} Nu_{{x2}}$$\end{document}-Rex-1/2Nux2
0000000011
000000.5-2.0214100.9881951.1618530.898716
000001-4.0855631.9531791.3366140.802165
0000.0101-4.1898902.0026741.3637470.831425
00000.011-4.1941402.0003851.3651140.832586
0000.010.011-4.3021302.0517121.3938700.863450
1000.010.011-1.240570-1.2202731.3231250.828030
1100.010.011-1.322328-1.3013131.3189210.831390
110.20.010.011-2.688739-0.0039141.8936560.668863
11-0.20.010.011-0.003540-2.6359650.8873391.001950
Table 7

Heat transfer analysis with the addition of the control parameters.

ParametersDevelop/reduce the thermal rate at lower plateDifference percentage of \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$- \text{Re} _{x} ^{{ - 1/2}} Nu_{{x1}}$$\end{document}-Rex-1/2Nux1Develop/reduce the thermal rate at upper plateDifference percentage of \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$- \text{Re} _{x} ^{{ - 1/2}} Nu_{{x2}}$$\end{document}-Rex-1/2Nux2
Squeezing \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( {Sq} \right)$$\end{document}SqReduce-5.35%Reduce-4.28%
Magnetic \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( M \right)$$\end{document}MReduce-0.32%Develop0.40%
Suction \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( {S > 0} \right)$$\end{document}S>0Develop30.35%Reduce-24.30%
Injection \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\left( {S < 0} \right)$$\end{document}S<0Reduce-48.64%Develop17.02%
Numerical values of , , and with various values of the control parameters. Heat transfer analysis with the addition of the control parameters. The exploration of pertinent parameters’ impact such as squeezing, suction/injection, and stretching parameters is continued with the observation on and as displayed in Figs. 2–7. In Fig. 2, the velocity distribution enhances with the addition of the unsteadiness squeezing parameter. As the squeezing parameter’s magnitude increases up to , the velocity distribution is depreciated at the upper plate. This is due to the squeezing effect which originated from the upper plate. However, the temperature profile in Fig. 3 slightly reduces near to the lower plate while increases near to the upper plate .
Figure 2

Effect of squeezing parameter on when , , and .

Figure 7

Effect of stretching parameter on when , and .

Figure 3

Effect of squeezing parameter on when , , and .

Effect of squeezing parameter on when , , and . Effect of squeezing parameter on when , , and . Further, the impact of the suction/injection parameter on both profiles is visualized in Figs. 4 and 5. As the suction/injection parameter increases from injection to suction , the velocity profile decreases which reflects the higher magnitude of suction strength can reduce the velocity distribution. Since the suction is applied through the lower permeable plate, the velocity lessens while increases near to the upper plate. The temperature profile augments at both locations (lower and upper plate). Figures 6 and 7 present the plots of velocity and temperature distribution with variety values of the stretching parameter. The velocity gradually increases when while a contrary observation is obtained for . The temperature profile increases for both lower and upper plates.
Figure 4

Effect of suction/injection parameter on when , and .

Figure 5

Effect of suction/injection parameter on when , and .

Figure 6

Effect of stretching parameter on when , and .

Effect of suction/injection parameter on when , and . Effect of suction/injection parameter on when , and . Effect of stretching parameter on when , and . Effect of stretching parameter on when , and .

Conclusion

This novel work presents a numerical study of Cu-Al2O3/water inside two plates (parallel lower and upper) with the appearance of the magnetic field. The lower plate is permeable for the suction/injection processes and also can be stretched. Meanwhile, the upper plate can move towards the lower plate and creates the squeezing flow phenomenon. The mathematical model which suits this physical phenomenon follows the usual approximations of boundary layer flow while the bvp4c programme is fully utilized for the generation of the results. The distribution of , , and are examined. The heat transfer rate of the lower plate reduces with the increase of magnetic, squeezing, and injection parameters. However, about 30.35% of is developed with the inclusion of suction. Meanwhile, the enhancement of magnetic and injection parameters can lead to the development of the upper plate’s heat transfer performance. Another observation is conducted for the distribution of the velocity and temperature profiles. The addition of squeezing and stretching parameters can increase the velocity profile whereas high suction’s magnitude shows the opposite trend.
  7 in total

1.  Dissipated electroosmotic EMHD hybrid nanofluid flow through the micro-channel.

Authors:  M Bilal; I Asghar; M Ramzan; K S Nisar; A-H Abdel Aty; I S Yahia; H A S Ghazwani
Journal:  Sci Rep       Date:  2022-03-19       Impact factor: 4.379

2.  Significance of induced hybridized metallic and non-metallic nanoparticles in single-phase nano liquid flow between permeable disks by analyzing shape factor.

Authors:  S Bilal; Imtiaz Ali Shah; Muhammad Ramzan; Kottakkaran Sooppy Nisar; Ashraf Elfasakhany; Emad M Eed; Hassan Ali S Ghazwani
Journal:  Sci Rep       Date:  2022-02-28       Impact factor: 4.379

3.  Numerical Simulation of a Time-Dependent Electroviscous and Hybrid Nanofluid with Darcy-Forchheimer Effect between Squeezing Plates.

Authors:  Muhammad Sohail Khan; Sun Mei; Unai Fernandez-Gamiz; Samad Noeiaghdam; Aamir Khan
Journal:  Nanomaterials (Basel)       Date:  2022-03-06       Impact factor: 5.076

4.  Numerical Analysis of an Unsteady, Electroviscous, Ternary Hybrid Nanofluid Flow with Chemical Reaction and Activation Energy across Parallel Plates.

Authors:  Muhammad Bilal; A El-Sayed Ahmed; Rami Ahmad El-Nabulsi; N Ameer Ahammad; Khalid Abdulkhaliq M Alharbi; Mohamed Abdelghany Elkotb; Waranont Anukool; Zedan A S A
Journal:  Micromachines (Basel)       Date:  2022-05-31       Impact factor: 3.523

5.  Thermally Dissipative Flow and Entropy Analysis for Electromagnetic Trihybrid Nanofluid Flow Past a Stretching Surface.

Authors:  Kamel Guedri; Arshad Khan; Taza Gul; Safyan Mukhtar; Wajdi Alghamdi; Mansour F Yassen; Elsayed Tag Eldin
Journal:  ACS Omega       Date:  2022-09-02

6.  Hall current and morphological effects on MHD micropolar non-Newtonian tri-hybrid nanofluid flow between two parallel surfaces.

Authors:  Abdul Rauf; Nehad Ali Shah; Thongchai Botmart
Journal:  Sci Rep       Date:  2022-10-05       Impact factor: 4.996

7.  Dynamics of ethylene glycol-based graphene and molybdenum disulfide hybrid nanofluid over a stretchable surface with slip conditions.

Authors:  Syed M Hussain
Journal:  Sci Rep       Date:  2022-02-02       Impact factor: 4.379

  7 in total

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