Home Technology Non-Similar Comutational Solutions for Double-Diffusive MHD Transport Phenomena for Non-Newtnian Nanofluid From a Horizontal Circular Cylinder
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Non-Similar Comutational Solutions for Double-Diffusive MHD Transport Phenomena for Non-Newtnian Nanofluid From a Horizontal Circular Cylinder

  • V. Ramachandra Prasad EMAIL logo , S. Abdul gaffar and B. Rushi Kumar
Published/Copyright: December 2, 2018
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Abstract

This article aims to study theoretically the combined magneto hydrodynamic flows of casson viscoplastic nanofluid from a horizontal isothermal circular cylinder in non-Darcy porous medium. The impacts of Brownian motion and thermophoresis are consolidated and studied. The governing partial differential equations are converted into nonlinear ordinary differential equations using suitable non-similarity transformation and are solved numerically using Keller-Box finite difference technique. The numerical method is validated with previous published work and the results are found to be in excellent agreement. Numerical results for velocity, temperature, concentration along with skin friction coefficient, heat and mass transfer rate are discussed for various values of physical parameters. It is observed that velocity, heat and mass transfer rate are increased with increasing casson fluid parameter whereas temperature, concentration and skin friction are decreased. Velocity is reduced with increasing Forchheimer parameter whereas temperature and nano-particle concentration are both enhanced. An increase in magnetic parameter is seen to increase temperature and concentration whereas velocity, skin friction heat and mass transfer rate are decreased. The present model finds applications in electric-conductive nano-materials of potential use in aviation and different enterprises, energy systems and thermal enhancement of industrial flow processes.

1 Introduction

The convection transport study of nanofluid has gained interest in the recent years due to its wide spread application in industry, transportation, electronics, fuel cells, incorporate and medical applications. Usually, base fluids like ethylene glycol, kerosene, water, etc. have low thermal conductivity [1, 2]. The suspension of nano-sized metallic or non-metallic particles into the base fluids, enhances the thermal conductivity of the base fluids. Choi [3] was the first researcher to use the term Nanofluid, in order to represent the engineered colloids. He observed that on addition of 1% of nanoparticles to the normal fluid, the fluid thermal conductivity increases twice. Flow, heat and mass transfer of Nanofluids has attracted many researchers due to its prominent role in industry and technology such as electronics, transportation, biomedical (cancer therapy, drug delivery, etc.), micro-electronics, fuel cells, hybrid-powered engines, etc. [1, 2]. The heat transfer enhancement technology has been widely used in refrigerators, automobiles, process and chemical industry, etc. The continuous collision of nanoparticles and molecules of the base fluid is called Brownian motion. The nanoparticle concentration and size of the particle are the most important parameter for enhancing the heat transfer of nanofluid as discussed by Buongiorno [4]. In Buongiorno model [4] the nanoparticle concentration is considered to vary and incorporates the effects of Brownian motion and thermophoresis. Sheikholeslami et al. [5] presented an experimental analysis of hydrothermal behavior of nano-refrigerant duty condensation. Sheikholeslami and Rokni [6] used control volume based finite element method to simulate the effects of Lorentz forces on nanofluid flow in porous media. Shrivan et al. [7] utilized the finite element method to study the influence of wavy surface characteristics on natural convection flows in a cosine corrugated square cavity filled with Cu-water nanofluid. Rashidi et al. [8] used the volume of fluid model to investigate the nanofluid flow and entropy generation in a single slope solar still using finite volume method. Sheikholeslami and Shehzad [9] considered convective flow of nanofluid inside a porous enclosure by means of two-temperature model taking into account the effects of Lorentz forces. Sheikholeslami [10] numerically investigated the electrohydrodynamic radiative free convection flow of nanofluid in a porous media. Shirvan et al. [11] explored the response surface methodology and two phase mixture model to examine the heat exchanger effectiveness in a double pipe heat exchanger filled with nanofluid. Esfahani et al. [12] used finite volume technique to analyze the entropy generation of nanofluid flow through a wavy channel over heat exchanger plat.

In many fluids the flow properties are difficult to explain by a single constitutive equation like Newtonian model. Geological materials and polymer solutions used in different industries and engineering processes are such fluids which cannot be explained by Newtonian model. The materials that cannot be explained using Newtonian model are called Non-Newtonian fluid models. In past few decades, due to the applications in industries, engineering and technology, non-Newtonian fluid flows has gained interest in researchers [13, 14]. In such fluids the shear stress and strain rate relation is non-linear. Examples of such fluids include china clay, coal in water, sewage sludge, oil-water emulsions, gas-liquid dispersions, coal-oil slurries, detergent and paint production, smart coating and suspension fabrication, pharmacology, cosmetic creams, physiological transport processes (blood, bile and synovial fluid), slurry conveyance, polymer synthesis and food processing. The mathematical models in non-Newtonian fluids are more complicated and relate the shear stresses to the velocity field [15]. Few non-Newtonian transport modeling include oblique micropolar stagnation flows [16], Walter’s-B viscoelastic flows [17], Jeffrey’s viscoelastic boundary layers [18], magnetized Williamson fluids [19], nanofluid transport from a sphere [20], Maxwell fluids [21], Eyring-Powell fluid [22], Tangent Hyperbolic fluid [23], Oldroyd-B fluid [24] and Power-law model [25]. Of the different non-Newtonian fluids discussed in the literature, the Casson’s viscoplastic fluid model [26] is simple and a realistic fluid model that exhibits shear thinning characteristics, yield stress and high shear viscosity [27]. This particular fluid model has infinite viscosity at zero shear rate. The Casson fluid behaves like solid elastic when the shear stress is less than the yield stress and deforms when the shear stress is greater than yield stress. The study of Casson fluid by different researchers include Kumaran and Sandeep [28], Khan et al. [29], Nawaz et al. [30], Kahsif et al. [31], Ahmed et al. [32], Mahanthesh and Gireesh [33] and Rehman et al. [34].

The presence of magnetic field in natural convection flows plays an important role and has many applications like nuclear reactor cooling, magnetohydrodynamic (MHD) generators, geophysics, astrophysics, aerodynamics, plasma engineering, exploration of oil, etc. [35]. Ahmad and Ishak [36] considered an implicit finite difference scheme to study the MHD convection flow of Jeffrey fluid over a stretched sheet immersed in porous medium. Sheikholeslami and Houman [37] investigated the convective heat transfer flow of nanofluid in a porous cavity in the existence of Lorentz forces. Sheikholeslami [38] investigated the MHD forced convection flow of nanofluid inside a porous cavity. He employed CVFEM to simulate the vorticity stream function. Hassan et al. [39] employed homotopy analysis method to examine the nanoparticle shapes behavior on heat and mass transfer flow of ferrofluid over a rotating disk in the presence of low oscillating magnetic field. Ellahi et al. [40] discussed the influence of nano-ferroliquid under the low oscillating magnetic field over a stretchable rotating disk. Xie and Jian [41] studied the entropy analysis of magnetohydrodynamic electroosmotic flow. Zeeshan et al. [42] used homotopy analysis method to explore the MHD radiative Couette-Ooiseuille flow of nanofluid in horizontal channel with convective boundary conditions. Recent studies include Abdul Gaffar et al. [43, 44, 45] and Beg et al. [46].

Flows in fluid saturated porous media has a wide range of applications in different areas of engineering and industry like food processing, fuel cell technologies, geothermics, trickle bed chromatography, etc. Most of studies utilize the Darcy model which is valid for low Reynolds number flows [47]. Srinivasacharya et al. [48] explored the mixed convection flow of viscous fluid past a vertical porous plate with the flow in porous medium is characterized by Darcy-Forchheimer model. Gireesh et al. [49] attempted to analyze the unsteady MHD flow of dusty fluid over stretching surface in non-Darcy porous medium. Natalia et al. [50] presented the mixed convection flow of nanofluid over a vertical flat plate embedded in fluid saturated non-porous medium. Recent studies include Hady et al. [51], V.R. Prasad et al. [52], Som et al. [53], Nazir et al. [54], Abdul gaffar et al. [55, 56].

To the authors’ knowledge no studies have been communicated with regard to viscoplastic nanofluid MHD convection flow of isothermal horizontal circular cylinder in non-Darcy porous media. The heat transfer with nanoparticles is analyzed by employing Buongiorno model [4]. In the present study a non-similarity mathematical analysis is developed for steady double-diffusive magnetohydrodynamic flows in Casson nanofluid saturated in non-Darcy porous media from a permeable horizontal circular cylinder. The Keller-box difference scheme is used to solve the normalized boundary layer equations and the effects of Forchheimer parameter (𝛬), Brownian motion (Nb), thermophoresis (Nt), buoyancy ratio (Nr) and Darcy number (Da) on the relevant flow variables are described in detail. The present study finds application in solar film collectors, heat exchanger technology, geothermal energy storage systems, etc.

2 Viscoplastic Casson Nanofluid Mathematical Model

The steady-state, laminar, double-diffusive, incompressible, electrically-conducting,MHD convection flows of viscoplastic Nanofluid past a horizontal circular permeable cylinder embedded in fully-saturated porous medium is considered, as shown in Figure 1. An induced magnetic field, B0 is assumed to be uniform and acts normal to the surface of the cylinder. A non-Darcy drag force model is employed to simulate porous media and also inertial effects. The x - & y – coordinates are measured along the circumference and normal to the surface of the cylinder respectively, with a denoting the radius of the cylinder. Φ = x/a represent the angle of the y – axis with respect to the vertical 0 ≤ Φπ.The gravitational acceleration g, acts downwards. We assume that the Oberbeck-Boussineq approximation holds. Let Tw and Cwbe the constant temperature of the cylinder and viscoplastic nanofluid and Tand Cbe the ambient temperature and concentration of the fluid. The governing boundary layer equations in line with Casson [26] & Buongiorno [4] are:

Fig. 1 Physical Model and Coordinate
Fig. 1

Physical Model and Coordinate

(1)ux+vy=0.
(2)uux+vuy=v(1+1β)2uy2+g[(1C)ρfβ1(TT)(ρpρf)(CC)]sin(x/a)vKu=Γu2σB02ρu.
(3)uTx+vTy=αm2Ty2+τ[DBCyTy+(DTT)2].
(4)uCx+vCy=DB2Cy2+(DTT)2Ty2.

Where αm=km(ρc)fand τ=(ρc)p(ρc)f.Where ρp is the density of the particle, and is the effective heat capacity. The boundary conditions are defined as:

(5)Aty=0,u=v=0,T=Tw,C=CwAsy,u=0,TT,CC.

Defining the stream function, as u=(ψ)y,v=(ψ)x,Eq. (1) is satisfied. We now introduce the following dimensionless variables:

(6)ξ=xa,η=yaGr4,ψ(ξ,η)=vGr4ξf,θ(ξ,η)=TTTwT,ϕ(ξ,η)=CCCwCGr=(1C)ρfgβ(TwT)a3v2,Pr=vα,Le=vDm,Da=KGra2,Λ=Γa,M=σB02a2vρGr,Nb=τDB(CwC)v,Nt=τDT(TwT)vT,

Using Eq. (6) into Eqs. (24), reduce as follows:

(7)(1+1β)f+ff"(1+Λξ)f2+sinξξ(θNrϕ)(1Da+M)f=ξ(ffξf"fξ).
(8)θ"Pr+fθ+Nbθϕ+Ntθ2=ξ(fθξθfξ).
(9)ϕ"Le+fϕ+1LeNtNbθ"=ξ(fϕξϕfξ).

And the transformed non-dimensional boundary conditions are:

(10)Atη=0,f=0,f=0,θ=1,ϕ=1Asη,f0,θ0,ϕ0

Here primes denote the differentiation with respect to η. The skin-friction coefficient, Nusselt number and Sherwood number, which are given by:

(11)12CfGr3/4=(1+1β)ξf"(ξ,0).
(12)NuGr4=θ(ξ,0).
(13)LeGr4=ϕ(ξ,0).

3 Computational Solution With Keller Box Method (KBM)

The Keller-Box method (KBM), an implicit difference method is implemented to solve the non-linear boundary layer eqns. (7)(9) subject to the boundary conditions (10). This technique has remained extremely popular and maintained comparable efficiency to other numerical methods such as finite element, boundary elements, spectral methods etc. the disadvantage of the methodhowever is that the computational effort per time step is expensive due to its step which has to replace the higher derivative by first derivatives, so that the second-order equations can be written as a system of two first-order equations. Also laborious algebraic expressions must be generated for the discretized equations. However KBM has a second order accuracy with arbitrary spacing and attractive extrapolation features. It is unconditionally stable and achieves exceptional accuracy. It converges quickly and provides stable numerical meshing features. KBM provides an improvement in accuracy on explicit or semi-implicit schemes and utilizes customizable stepping in a fully implicit approach. Relevant details are provided in Keller [57]. KBM has been employed extensively in computational non-Newtonian transport modelling. The Keller-Box discretization is fully coupled at each step which reflects the physics of parabolic systems – which are also fully coupled. Discrete calculus associated with the Keller-Box scheme has also been shown to be fundamentally different from all other mimetic (physics capturing) numerical methods. The Keller Box Scheme comprises four stages.

  1. Decomposition of the Nth order partial differential equation system to N first order equations.

  2. Finite Difference Discretization

  3. Quasilinearization of Non-Linear Keller Algebraic Equations and finally.

  4. Block-tridiagonal Elimination solution of the Linearized Keller Algebraic Equations.

Step1: Reduction of the Nthorder partial differential equation system to N first order equations

New variables are introduced to Eqns. (7)(9) and (10), to render the boundary value problem as a multiple system of first order equations. A set of eight simultaneous first order differential equations are therefore generated by introducing the new variables:

(14)u(x,y)=f,v(x,y)=f",g(x,y)=ϕ,g(x,y)=p,s(x,y)=θ,t(x,y)=θ.
(15)f=u.
(16)u=v.
(17)g=p.
(18)s=t.
(19)(1+1β)v+fv(1+Λξ)u2(1Da+M)u+B(sNrg)=ξ[uuξvfξ].
(20)tPr+ft+Nbtp+Ntt2=ξ(usξtfξ).
(21)pLe+fp+1LeNtNbt=ξ(ugξpfξ).

where primes denote differentiation with respect to η. In terms of the dependent variables, the boundary conditions become:

(22)Atη=0,f=0,u=0,s=1,g=1Asη,u0,s0,g0.

Step 2: Finite Difference Discretization

A two-dimensional computational grid is imposed on the ξ-η plane as sketched in Fig. 2 The stepping process is defined by:

Fig. 2 Keller box computational cell
Fig. 2

Keller box computational cell

(23)η0=0,ηj=ηj1+hj,j=1,2,,J,ηJη
(24)ξ0=0,ξn=ξn1+kn,n=1,2,,N

where kn is the Δξ - spacing and hjis the Δη - spacing. If gnj denotes the value of any variable at(ηj , ξ n), then the variables and derivatives of Equations (15)(21) at (ηj1/2,ξn1/2)are replaced by:

(25)gj1/2n1/2=14(gjn+gj1n+gjn1+gj1n1).
(26)(gη)j1/2n1/2=12hj(gjngj1n+gjn1gj1n1).
(27)(gξ)j1/2n1/2=12kn(gjngj1n+gjn1gj1n1).

The resulting finite - difference approximation of equations (15)(21) for the mid - point (ηj−1/2, ξ n), are:

(28)hj1(fjnfj1n)=uj1/2n.
(29)hj1(ujnuj1n)=vj1/2n.
(30)hj1(vjnvj1n)=qj1/2n.
(31)hj1(gjngj1n)=pj1/2n.
(32)hj1(sjnsj1n)=tj1/2n.
(33)(1+1β)(vjvj1)+hj(1+α)4(fj+fj1)(vj+vj1)(1+α+Λξ)hj16(uj+uj1)2(1Da+M)hj2(uj+uj1)+Bhj2(sj+sj1Nr(gj+gj1))αhj2fj1/2n1(vj+vj1)+αhj2vj1/2n1(fj+fj1)=[R1]j/12n1.
(34)1Pr(tjtj1)+(1+α)hj4(fi+fj1)(tj+tj1)+Nbhj4(tj+tj1)(pj+pj1)+Nthj4(tj+tj1)2αhj4(uj+uj1)(sj+sj1)+αhj2sj1/2n1(uj+uj1)αhj2uj1/2n1(sj+sj1)αhj2fj1/2n1(tj+tj1)+αhj2tj1/2n1(fj+fj1)=[R2]j1/2n1.
(35)1Le(pjpj1)+(1+α)hj4(fj+fj1)(pj+pj1)+1LeNtNb(tjtj1)αhj4(uj+uj1)(gj+gj1)+αhj2gj1/2n1(uj+uj1)αhj2uj1/2n1(gj+gj1)αhj2fj1/2n1(pj+pj1)+αhj2pj1/2n1(fj+fj1)=[R3]j1/2n1.

where we have used the abbreviations

(36)α=ξn1/2kn,B=sin(ξn1/2)ξn1/2
(37)[R1]j1/2n1=hj[(1+1β)(v)j1/2n1+(1α)(fv)j1/2n1(1αΛξ)(uj1/2n1)2(1Da+M)uj1/2n1+B(sj1/2n1Nrgj1/2n1)].
(38)[R2]j1/2n1=hj[1Pr(t)j1/2n1+(1α)(ft)j1/2n1+Nb(tp)j1/2n1+Nt(t2)j1/2n1+α(us)j1/2n1].
(39)[R3]j1/2n1=hj[1Le(p)j1/2n1+(1α)(fp)j1/2n1+1LeNtNb(t)j1/2n1+α(ug)j1/2n1].

The boundary conditions are:

(40)f0n=u0n=0,s0n=1,g0n=1,uJn=0,sJn=0,gJ0=0.

Stage 3: Quasilinearization of Non-Linear Keller Algebraic Equations

If we assume fjn1,ujn1,vjn1,gjn1,pjn1,sjn1,tjn1to be known for 0 ≤ jJ, this leads to a system of 8J+8 equations for the solution of 8J+8 unknowns fjn,ujn,vjn,gjn,pjn,sjn,tjn,j=0,1,2,,J.This non-linear system of algebraic equations is linearized by means of Newton’s method.

Stage 4: Block-tridiagonal Elimination Solution of Linear Keller Algebraic Equations

The linearized system is solved by the block-elimination method, since it possess a block-tridiagonal structure. The bock-tridiagonal structure generated consists of block matrices. The complete linearized system is formulated as a block matrix system, where each element in the coefficient matrix is a matrix itself, and this system is solved using the efficient Keller-box method. The numerical results are strongly influenced by the number of mesh points in both directions. After some trials in the η-direction (radial coordinate) a larger number of mesh points are selected whereas in the ξ-direction (tangential coordinate) significantly less mesh points are utilized. ηmax has been set at 16.0 and this defines an adequately large value at which the prescribed boundary conditions are satisfied. ξmax is set at 3.0 for this flow domain. Mesh independence is achieved in the present computations. The numerical algorithm is executed in MATLAB on a PC. The method demonstrates excellent stability, convergence and consistency, as elaborated by Keller [57].

4 Interpretation of Results

The system of Eqs. (79) subject to Eq. (10) are numerically solved using an implicit finite difference Keller-Box technique and is programmed using MATLAB. The accuracy present code is validated and presented in Table 1 by comparing the present results of heat transfer rate with those of Merkin [58] and Yih [59] for different values of ξ. It has been found that the present results are in good correlation. In Tables 2 and 3 we present the effects of β, 𝛬 and Pr on Cf , Nu and Sh along with a variation in ξ. With increasing β, the Cf is reduced whereas Nu is enhanced. A small increment in Sh is observed with increasing β. An increasing Pr is found to increase Cf slightly whereas Nu is reduced. However, Sh is strongly increased with Pr. With increasing 𝛬, a significant decrease in Cf , Nu and Sh is observed. This trend is sustained for ξ > 0. Tables 4 and 5 present the impact of Da and Le on Cf , Nu and Sh along with a variation in ξ. An increasing Da is seen to increase Cf significantly. Also an increase in Da is observed to increase both Nu and Sh. An increasing Da is seen to increase C f significantly. In these Tables we also present the results of C f , Nu and Sh for different values of Le. Also an increasing Le is observed to increase C f significantly. Whereas, Nu is reduced with increasing Le values. The Sh is strongly increased with increasing Le. This trend is sustained for ξ > 0.

Table 1

The values of the Local heat transfer coefficient (Nu) for different values of ξ with Pr = 0.71, β → ∞, 𝛬 = 0, Da ! ∞and Nb = Nr = Nt = 0, Le = 0.6, M = 0.5

ξNu Gr− 1/4 = −θ' (ξ , 0)
Merkin [58]Yih [59]Present
0.00.42120.42140.4211
0.20.42040.42070.4206
0.40.41820.41840.4185
0.60.41450.41470.4146
0.80.40930.40960.4095
1.00.40250.40300.4027
1.20.39420.39500.3947
1.40.38430.38540.3852
1.60.37270.37400.3735
1.80.35940.36080.3598
2.00.34430.34570.3448
2.20.32700.32830.3280
2.40.30730.30860.3076
2.60.28470.28600.2852
2.80.25810.25950.2592
3.00.22520.22670.2255
π0.19630.19620.1961
Table 2

Values of Cf , Nu and Sh for various values of β, Pr, Sc and ξ (Nb = Nt = 0.2, Nr = 0.1, Da = 1.0, M = 0.5, Le = 0.6)

β𝛬Prξ = 00ξ = 300ξ = 600
CfNuShCfNuShCfNuSh
0.100.17910.10120.69010.17450.09811.21710.16380.0912
0.1500.19020.10420.60670.18500.10081.06780.17320.0934
0.351.000.21110.10860.46990.20460.10480.82360.19070.0961
0.6500.22350.11030.39950.21610.10580.63830.20070.0970
1.000.23030.11100.36340.22230.10630.63410.20610.0973
2.00.7100.23830.11140.32340.22950.10660.56320.21230.0974
0.0100.23030.11090.36820.22530.10810.64970.21130.1004
500.23030.11090.34730.21220.10020.58800.19050.0886
1000.23030.11090.33220.20240.09470.55060.17750.0820
1500.23030.11090.32070.19480.09070.52420.16830.0778
2000.23030.11090.31160.18870.08760.50410.16120.0748
1.03000.23030.11090.29800.17950.08340.47490.15090.0708
0.500.32460.37220.31560.32140.37110.54580.31410.3683
100.31570.38080.31590.31050.38160.54910.29860.3834
1.0200.29760.39810.31630.29040.40090.55340.27350.4075
300.27950.41530.31670.27150.41930.55610.25260.4282
500.24480.44880.31760.23640.45320.56000.21680.4631
700.21280.47960.31870.20480.48380.56320.18620.4930
Table 3

Values of Cf , Nu and Sh for various values of β, Pr, Sc and ξ (Nb = Nt = 0.2, Nr = 0.1, Da = 1.0, M = 0.5, Le = 0.6)

β𝛬Prξ = 900ξ = 1200ξ = 1800
CfNuShCfNuShCfNuSh
0.11.46240.14640.08041.35110.12130.06520.10590.02460.0074
0.151.27930.15440.08191.17710.12730.06530.08980.02490.0078
0.351.00.98130.16890.08350.89570.13780.06570.06450.02500.0083
0.650.82920.17700.08380.75340.14350.06580.05330.02520.0090
1.00.75160.18130.08390.68120.14650.06590.04740.02540.0102
2.00.710.66610.18920.08400.60200.14980.06610.04130.02550.0108
0.010.77710.18780.08750.70870.15310.06890.04820.02580.0093
50.68310.16350.07480.61280.12990.05820.04520.02180.0085
100.63250.15030.06890.56510.11840.05420.04330.02010.0081
150.59850.14140.06560.53360.11100.05210.04180.01890.0077
200.57310.13480.06330.51030.10560.05090.04050.01810.0075
1.0300.53670.12540.06060.47720.09800.04970.03810.01690.0071
0.50.63370.30360.36460.55240.29110.36080.02910.27310.3570
10.64290.28050.38700.56760.25730.39320.03100.21340.4121
1.020.65510.24700.41950.58880.21030.43750.03510.11010.5021
30.66270.22250.44320.60200.18010.46560.03820.04990.5471
50.67210.18570.47900.61740.14190.50140.04070.01270.5618
70.67840.15780.50730.62660.11610.52590.04120.00610.5569
Table 4

Values of Cf , Nu and Sh for different Da, Le and ξ (β = 1.0, Nb = Nt = 0.2, Nt = 0.1, 𝛬 = 1.0, M = 0.5, Pr = 0.71)

DaLeξ = 00ξ = 300ξ = 600
CfNuShCfNuShCfNuSh
0.2500.2313-0.01920.35840.2234-0.01710.62630.2074-0.0129
0.7500.22990.15430.36500.22180.14810.63680.20570.1362
1.01.000.22920.21330.36720.22110.20530.64030.20500.1895
2.000.22740.36830.37210.21930.35580.64850.20330.3308
3.000.22640.46920.37490.21830.45400.65310.20230.4230
5.000.22520.61010.37800.21710.59120.65850.20120.5522
0.100.12870.07130.18320.12440.06990.31640.11300.0662
0.1500.14810.07380.21590.14310.07190.37330.13040.0671
0.20.600.16250.07710.24020.15710.07490.41610.14350.0692
0.2500.17360.08070.25940.16790.07810.44990.15380.0718
0.300.18260.08410.27500.17650.08130.47740.16200.0745
0.3500.18990.08730.28800.18360.08420.50030.16880.0771
Table 5

Values of Cf , Nu and Sh for different Da, Le and ξ (β = 1.0, Nb = Nt = 0.2, Nt = 0.1, 𝛬 = 1.0, M = 0.5, Pr = 0.71)

DaLeξ = 900ξ = 1200ξ = 1800
CfNuShCfNuShCfNuSh
0.250.74350.1826-0.00720.67530.1477-0.00090.04740.02480.0000
0.750.75440.18090.11810.68350.14610.09320.04750.02450.0129
1.01.00.75830.18020.16560.68650.14560.13240.04750.02440.0206
2.00.74750.17870.29220.69420.14440.23790.04770.02420.0429
3.00.77270.17790.37510.69860.14370.30730.04780.02410.0581
5.00.77890.17700.49130.70400.14300.40480.04800.02400.0801
0.10.36450.09480.05930.31370.07910.04790.01620.00590.0035
0.150.43180.10990.06020.37390.08190.04840.01970.00600.0035
0.20.60.48290.12170.06030.42030.09160.04850.02250.00720.0039
0.250.52350.13110.06200.45790.09960.04940.02500.00950.0049
0.30.55690.13880.06400.48920.10640.05070.02720.00980.0078
0.350.58500.14520.06600.51580.11210.05170.02910.01120.0181

Figs. 3 – 12 illustrate the profiles of velocity and temperature for different values of the thermophysical parameters, viz., β, Nb, Nt, Nr, Le, Da, 𝛬, Pr and M. The default values of for these parameters are: β = Da = 𝛬 = 1.0, Pr = 0.71, Nb = Nt = 0.2, Nr = 0.1, Le = 0.6, M = 0.5 and ξ = 1.0.

Fig. 3 (a) Influence of β on Velocity Profiles; (b) Influence of β on Temperature Profiles; (c) Influence of β on Concentration Profiles
Fig. 3

(a) Influence of β on Velocity Profiles; (b) Influence of β on Temperature Profiles; (c) Influence of β on Concentration Profiles

Figs. 3(a)3(c) present the impact of β on velocity (f' ), temperature (θ) and concentration (φ). It is observed that increasing β values increases velocity near the cylinder surface but decreases it further away i.e., the viscoplastic fluid behaves as Newtonian fluid as β increases. It is observed that an increase in β decreases the yield stress and hence decreases the momentum boundary layer thickness. This contraction in boundary layer thickness is caused due to the tensile stress. Whereas, the temperature and spices concentration are decreased slightly throughout the boundary layer regime. The viscoplastic fluid parameter β appears only in the momentum boundary layer Eq. (7) via the shear term (1+1/β) f 000 . The momentum equation couples strongly with the energy and species concentration equations via the thermal and species buoyancy force

terms and hence the effect of casson parameter is indirectly transmitted to both temperature and concentration filed. The similar trends are observed by Subba Rao et al. [60].

Figs. 4(a)4(c) presents the profiles of velocity (f/), temperature (θ) and concentration (φ) for different values of Nb.An increase in velocity is observed for various values of Nb throughout the boundary layer regime. Also, a slight increase in temperature is observed which is due to the collision between the random motions of the nanoparticles. Whereas, the species concentration is found to decrease with an increase in Nb. Keblinski et al. [61] has elaborated various mechanisms which may contribute to enhancement in temperatures via augmentation of the thermal conductivity with nano-particles. These include Brownian motion of nanoparticles, ballistic transport of energy carriers within individual nanoparticles and between nanoparticles that are in contact, nanoparticle distribution and also the interfacial ordering of liquid molecules on the surface of nanoparticles. Brownian motion elevates thermal conduction via nanoparticles carrying thermal energy. However it has been seen that the direct contribution of Brownian motion is less significant as the time scale of the Brownian motion is about two orders of magnitude larger than that for the thermal diffusion of the base liquid. Nanoparticles frequently are in the form of agglomerates and/or aggregates. For small particles, Brownian motion is strong and the parameter Nb will have high values; the opposite will apply for large particles.

Fig. 4 (a) Influence of Nb on Velocity Profiles; (b) Influence of Nb on Temperature Profiles; (c) Influence of Nb on Concentration Profiles
Fig. 4

(a) Influence of Nb on Velocity Profiles; (b) Influence of Nb on Temperature Profiles; (c) Influence of Nb on Concentration Profiles

Figs. 5(a)5(c) illustrates the impact of Nt on velocity (f/), temperature (θ) and concentration (φ). A decrease in velocity is seen for various values of Nt throughout the boundary layer regime. A significant increase in both temperature and nano-particle concentration is generated as Nt increases. Thermophoresis heats the boundary layer and assists in particle deposition away from the fluid regime, thereby accounting for the elevated concentration (nano-particle) as shown in Fig. 5(c). For Nt = 0.1, a monotonic decay in nano-particle concentration from the wall of the cylinder into the free stream. However, for Nt > 0.1, a concentration peak is observed further from the surface of the cylinder.

Fig. 5 (a) Influence of Nt on Velocity Profiles; (b) Influence of Nt on Temperature Profiles; (c) Influence of Nt on Concentration Profiles
Fig. 5

(a) Influence of Nt on Velocity Profiles; (b) Influence of Nt on Temperature Profiles; (c) Influence of Nt on Concentration Profiles

Fig. 6 (a) Influence of Nr on Velocity Profiles; (b) Influence of Nr on Temperature Profiles; (c) Influence of Nr on Concentration Profiles
Fig. 6

(a) Influence of Nr on Velocity Profiles; (b) Influence of Nr on Temperature Profiles; (c) Influence of Nr on Concentration Profiles

Figs. 5(a) - 5(c) depicts the profiles for velocity (f/), temperature (θ) and concentration (φ) for different values of Nr. By definition, Nr represents the ratio of nanoparticle concentration to the thermal buoyancy force. The parameter Nr, arises only in the momentum boundary layer equation in the term (sinξ /ξ) (θ - Nrφ) and couples the momentum equation to the thermal and concentration boundary layer equations respectively. With increasing Nr values, the velocity is decreased throughout the boundary layer. A slight increase in both temperature and concentration is observed. Hence, the buoyancy forces aid in the diffusion of heat and species (nano-particles) in the regime, whereas they induce a deceleration in the flow regime. Similar trends have been recently observed for other free convection nanofluid boundary layer flows by Gorla and Kumari [62].

Figs. 7(a)7(c) presents the impact of Forchheimer parameter, 𝛬 on velocity (f/), temperature (θ) and concentration (φ). The parameter 𝛬 is associated with the second or- der Forchheimer resistance term,-ξ𝛬(f')2 in the momentum equation. The Forchheimer drag is directly proportional to 𝛬. As shown in Fig. 7(a), the flow is markedlydecelerated with increasing values of 𝛬. As indicated by Kaviany [63], the Forchheimer effects are associated with higher velocities in porous media transport. A significant elevation in both temperature and nano-particel species diffusion concentration is seen with an increase in 𝛬.

Fig. 7 (a) Influence of 𝛬 on Velocity Profiles; (b) Influence of 𝛬 on Temperature Profiles; (c) Influence of 𝛬 on Concentration Profiles
Fig. 7

(a) Influence of 𝛬 on Velocity Profiles; (b) Influence of 𝛬 on Temperature Profiles; (c) Influence of 𝛬 on Concentration Profiles

Figs. 8(a)8(c) depict the profiles for velocity (f/), temperature (θ) and concentration (φ) for increasing values of magnetic parameter, M. The parameter M represents the ratio of magnetic Lorentzian drag force to viscous hydrodynamic force in the flow. For M < 1, the viscous force dominates the magnetic force and the magnetohydrodynamic effect is weak. However, Fig. 8a shows that even a small increase in M induces a marked deceleration in velocity. This reveals that the magnetic field resists the fluid transport due to rise in M lends an enhancement in the Lorentz force, which resist the fluid flow. This concurs with many other studies of magnetized nanofluid convection since the radial magnetic field acts to generate a perpendicular drag force which acts to decelerate the flow. Figs. 8b and 8c indicate that the dominant effect of greater magnetic parameter is to elevate both temperatures and nano-particle concentrations. The supplementary work expended in dragging the viscoplastic nanofluid against the action of the magnetic field manifests in kinetic energy dissipation. This energizes the boundary layer since the kinetic energy is dissipated as thermal energy and this further serves to agitate improved species diffusion. As a result both thermal and nano-particle (species) concentration boundary layer thicknesses are increased.

Fig. 8 (a) Influence of M on Velocity Profiles; (b) Influence of M on Temperature Profiles; (c) Influence of M on Concentration Profiles
Fig. 8

(a) Influence of M on Velocity Profiles; (b) Influence of M on Temperature Profiles; (c) Influence of M on Concentration Profiles

Figs. 9(a)9(c) presents the effects of Nb on skin friction (Cf), heat transfer rate (Nu) and mass transfer rate (Sh) at the cylinder surface. Cf is observed to increase slightly for different values of Nb. Conversely, Nu is decreased significantly with increasing Nb. There is also a progressive depletion in heat transfer rate with increasing transverse coordinate i.e. x–value. This agrees with the corresponding enhancement in temperature in the boundary layer owing to the nanofluid properties as represented by the Brownian diffusion effect. A decrease in heat transfer rate at the wall implies that less heat is convected from the fluid regime to the cylinder, thereby heating the boundary layer. Dimensionless mass transfer rate (local Sherwood number) is boosted up with increasing Nb.

Fig. 9 (a) Influence of Nb on Skin Friction; (b) Influence of Nb on Nusselt Number; (c) Influence of Nb on Sherwood Number
Fig. 9

(a) Influence of Nb on Skin Friction; (b) Influence of Nb on Nusselt Number; (c) Influence of Nb on Sherwood Number

Figs. 10(a)10(c) depicts the profiles for on skin friction (Cf), heat transfer rate (Nu) and mass transfer rate (Sh) at the cylinder surface for increasing Nt values. Clearly from Fig. 11(a) a very slight increase in Cf is observed with an increase in Nt whereas, an increase in Nt decreases both heat transfer rate and mass transfer rate. Hence, thermophoresis exerts a significant effect on both heat and mass transfer characteristics at the cylinder surface.

Fig. 10 (a) Influence of Nt on Skin Friction; (b) Influence of Nt on Nusselt Number; (c) Influence of Nt on Sherwood Number
Fig. 10

(a) Influence of Nt on Skin Friction; (b) Influence of Nt on Nusselt Number; (c) Influence of Nt on Sherwood Number

Fig. 11 (a) Influence of Nr on Skin Friction; (b) Influence of Nr on Nusselt; (c) Influence of Nb on Sherwood Number
Fig. 11

(a) Influence of Nr on Skin Friction; (b) Influence of Nr on Nusselt; (c) Influence of Nb on Sherwood Number

Figs. 11(a)11(c) illustrate the responses of buoyancy ratio Nr, on skin friction (Cf ), heat transfer rate (Nu) and mass transfer rate (Sh) at the cylinder surface. For Nr > 0, the C f at the cylinder surface is observed to decrease for increasing values of Nr. Also, the heat transfer rate and mass transfer rates are found to reduce with increasing Nr values.

Figs. 12(a)12(c) presents the responses of magnetic parameter M, on skin friction (Cf), heat transfer rate (Nu) and mass transfer rate (Sh) at the cylinder surface. A significant decrease in Cf is observed at the cylinder surface for increasing values of M. Similar trends are observed in the case of heat and mass transfer rates i.e., both Nu and Sh are found to be strongly reduced with increasing M values.

Fig. 12 (a) Influence of M on Skin Friction; (b) Influence of M on Nusselt Number; (c) Influence of M on Sherwood Number
Fig. 12

(a) Influence of M on Skin Friction; (b) Influence of M on Nusselt Number; (c) Influence of M on Sherwood Number

5 Conclusions

A numerical analysis is developed to study the laminar MHD convection flows of Casson nanofluid from an isothermal horizontal circular cylinder in fluid-saturated non-Darcy porous medium. An implicit finite difference Keller-Box technique is used to solve the non-dimensional boundary layer equations with prescribed boundary conditions. A comprehensive assessment of the impact of Casson fluid parameter (β), Brownian motion parameter (Nb), Thermophoresis parameter (Nt), Buoyancy ratio parameter (Nr), Darcy number (Da), Magnetic parameter (M), Forchheimer parameter (𝛬), Prandtl number (Pr) and Schmidt number (Sc). Very stable and accurate solutions are obtained with the present code. The present has been validated with the earlier Newtonian study. The present numerical code is able to solve the nonlinear rheological boundary layer flow problems very efficiently and hence presents excellent promise in simulating transport phenomena in other non-Newtonian fluids.

Nomenclature

aRadius of the cylinderu, vDimensionless velocity components in X and Y direction respectively
B0Constant imposed magnetic fieldxStream wise coordinate
CFluid concentrationyTransverse coordinate
CfSkin Friction CoefficientGreek Symbols
DaDarcy ParameterαThermal diffusivity
D BBrownian diffusion coefficientβCasson fluid parameter
DmMass diffusionβ1Coefficient of thermal expansion
DTThermophoretic diffusion coefficientΦAzimuthal coordinate
fDimensionless stream functionσElectric conductivity of the fluid
gGravitational accelerationηNon-dimensional radial coordinate
KThermal diffusivityΓInertial drag coefficient
kThermal conductivity of the fluidμDynamic viscosity
GrGrashof numberξNon-dimensional tangential coordinate
MMagnetic ParameterNon-dimensional stream function
NbBrownian motion parameterνKinematic viscosity
NtThermophoresis parameterφDimensionless concentration
NrBuoyancy ratio parameterθDimensionless temperature
NuHeat transfer coefficientρFluid density
PrPrandtl number𝛬Forchheimer parameter (local inertial drag coefficient)
TFluid temperature
SCauchy stress tensorSubscripts
LeLewis numberwConditions on the wall
ShSherwood numberFree stream condition

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Received: 2018-02-15
Revised: 2018-05-16
Accepted: 2018-08-03
Published Online: 2018-12-02
Published in Print: 2019-01-28

© 2019 V. Ramachandra Prasad et al., published by De Gruyter

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

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