Home Numerical results for influence the flow of MHD nanofluids on heat and mass transfer past a stretched surface
Article Open Access

Numerical results for influence the flow of MHD nanofluids on heat and mass transfer past a stretched surface

  • Nader Y. Abd Elazem EMAIL logo
Published/Copyright: April 23, 2021
Become an author with De Gruyter Brill

Abstract

Due to its significant applications in physics, chemistry, and engineering, some interest has been given in recent years to research the boundary layer flow of magnetohydrodynamic nanofluids. The numerical results were analyzed for temperature profile, concentration profile, reduced number of Nusselt and reduced number of Sherwood. It has also been shown that the magnetic field, the Eckert number, and the thermophoresis parameter boost the temperature field and raise the thermal boundary layer thickness while the Prandtl number reduces the temperature field at high values and lowers the thermal boundary layer thickness. However, if Lewis number is higher than the unit and the Eckert number increases, the concentration profiles decrease as well. Ultimately, the concentration profiles are reduced for the variance of the Brownian motion parameter and the Eckert number, where the thickness of the boundary layer for the mass friction feature is reduced.

1 Introduction

One of the most important emerging developments of the 21st century is nanotechnology. It has been commonly used in manufacturing and nanometersized materials have special physical and chemical properties. With its increasingly significant and complex effect on a wide range of industries, including biotechnology, oil, electronics and consumer goods, it promises to change our lives in this decade. In many engineering processes with applications in industries such as extrusion, melt-spinning, heat rolling, wire drawing, glass-fiber processing, plastic and rubber sheet manufacturing, cooling of a large metal plate in a bath that may be an electrolyte, etc., flow over a stretching surface is an important issue. The authors in [1] investigate the elastic deformation effects on the boundary layer flow of an incompressible second grade two phase nanofluid model over a stretching surface in the presence of suction and partial slip boundary condition.

In industry, polymer sheets and filaments are manufactured by continuous extrusion of the polymer from a die to a windup roller, which is located at a finite distance away [2]. There are many applications in engineering and industry for boundary layer flow behavior over a stretching surface [3]. Having a low heat transfer in a fluid would cause limited heat transfer and can lead to limited heat transfer efficiency. Due to the high thermal conductivity of metal particles, adding them to a fluid would increase the thermal conductivity and also heat transfer of the resultant mixture fluid. Choi's [4] initial analysis of the term "nanofluid" identified a liquid suspension containing ultra-fine particles. Nanoparticles (e.g., Copper (Cu), Silver (Ag), Alumina (Al2O3), Titanium (TiO2)) range from 1 to 100 nm in diameter [5]. The base liquid's thermal conductivity is improved by (10% – 50%) if it is suspended by a low volumetric fraction (less than 5%) of nanoparticles [6, 7, 8]. In Ref. [9], the authors examined improvements in the thermal conductivity of fluids (such as oil, water, and ethylene glycol mixture) which are poor heat transfer by suspending nano/micro or large particle materials in these fluids. Kuznetsov and Nield [10] investigated the effect of nanoparticles on the natural convection boundary-layer flow through a vertical plate, using a model in which Brownian motion and thermophoresis are represented.

During the recent decades, convective heat transfer of nanofluids is a hot topic of academic and industrial research due to its various applications in industrial processes such as thermal heating, power generation and chemical processing [11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22].

In many applications in the polymer and metallurgy industries, hydro-magnetic techniques are used [23]. Hence, the influence of the magnetic field has attracted significant interest in recent years due to its high applications in physics, chemistry, and engineering [24]. MHD free convection flow of Sodium Alginate nanofluid on a solid sphere with prescribed wall temperature is investigated by [25]. The authors examine the free convection flow of Casson nanofluid in the prsence of magnetic field. The relevant partial differential equations are first converted into non-dimensional equations by using appropriate transformation and then computed by utilizing the Keller box method. MHD peristaltic transport of copper-water nanofluid in an artery with mild stenosis for different shapes of nanoparticles is studied in [26]. The characteristics of MHD, heat sink/source, and convective boundary conditions in chemically reactive radiative Powell-Eyring nanofluid flow via Darcy channel using a nonlinearly settled stretching sheet/surface are used in Rasool and Shafiq [27]. In ref. [28], the authors concern with the examination of heat transfer rate, mass and motile micro-organisms for convective second grade nanofluid flow.

Considering these facts, and motivated by above discussed papers in the field of nanofluids. There is a physical justification to study the prsent article, there is enhance in the dimensionless of the stream function f, temperature θ, and volume of nanoparticles ϕ, respectively, (see Fig. 1 in ref. [19]). Due to the existing of Prandtl number in the momentum equation in ref. [19]. All the above previous research did not address this point. So, we studied the MHD flow of nanofluid over a stretched surface on heat and mass transfer to extend to the work of Abd Elazem [19]. Because of the importance this study for engineers and researchers in nearly every branch in engineering and science. Nuclear power plants, gas turbines and the various propulsion devices for aircraft, missiles, satellites and space vehicles are examples of such engineering areas. The governing equations of the present study are solved numerically solved by using the Chebyshev pseudospectral technique [29, 30, 31]. The effect of different parameters on temperature, concentration, local skin friction f″(0), reduced Nusselt number, and reduced Sherwood number is investigated through tables and graphs.

Figure 1 Physical diagram of the flow geometry
Figure 1

Physical diagram of the flow geometry

2 Analysis

A uniform magnetic field of force Bo is imposed in the y–direction according to Ref. [8] (see Fig. 1). For the current study, the basic steady conservation of mass, momentum, thermal energy and nanoparticles equations becomes:

(1) ux+vy=0,

(2) uux+vuy=-1ρfpx+ν(2ux2+2uy2)-σ*Bo2ρfu,

(3) uvx+vvy=-1ρfpy+ν(2vx2+2vy2),

(4) uTx+vTy=α(2Tx2+2Ty2)+τ{DB(CxTx+CyTy)+(DTT)[(Tx)2+(Ty)2]}+μf(ρcp)f(uy)2+σ*Bo2(ρcp)fu2,

(5) uCx+vCy=DB(2Cx2+2Cy2)+(DTT)(2Tx2+2Ty2),

subject to the boundary conditions:

(6) u=uw(x)=ax, v=s, T=Tw, C=Cw at y=0,u=v=0, T=T, C=C  asy.

Where, u and v are the velocity components along the axes x and y, respectively, ρf is the density of the base fluid, ν is the kinematic viscosity, σ* is the electrical conductivity, p is the fluid pressure, α=kf(ρc)f is the thermal diffusivity, DB is the Brownian diffusion coefficient, DT is the thermophoretic diffusion coefficient, τ=(ρc)p(ρc)f  is the ratio between the effective heat capacity of the nanoparticle material and heat capacity of the fluid with ρ being the density, c is the volumetric volume expansion coefficient and ρp is the density of the particles, cp is the fluid specific heat at constant pressure, μf is the viscosity of the base fluid and s is suction (or injection) parameter, respectively. T is the temperature of the fluid, C is the fraction of the volume of nanoparticles, Tw is the temperature of the stretching surface, Cw is the fraction of the volume of nanoparticles on the stretching surface, T is the ambient temperature and C is the fraction of the volume of ambient nanoparticles. Under the related work [10].

(7) f(η)=ψα Rax1/4, θ(η)=T-TTw-T, ϕ(η)=C-CCw-C,

Where ψ is a stream function provided by

(8) u=ψy, v=-ψx.

Well then, Eq. (1) identically satisfied. For converting Eqs. (1)(5) with the boundary conditions (6) into the following nonlinear ordinary differential equations a similarity solution in Ref. [10] was implemented.

(9) f'''+(14Pr)[3f f''-(f')2]-M f'=0,

(10) θ''+34f θ'+Nb ϕ'θ'+Nt  (θ')2+Ec (f'')2+M Ec (f')2=0,

(11) ϕ''+34Le f ϕ'+NtNbθ''=0,

with the boundary conditions:

(12) f(0)=s, f'(0)=1, θ(0)=1, ϕ(0)=1,f'()=0, θ()=0, ϕ()=0.

Where primes indicate differentiation for η and Pr, Nb, Nt, Ec, M, and Le are Prandtl number, Brownian motion parameter, thermophoresis parameter, Eckert number, magnetic parameter, and Lewis number, respectively. The physical parameters below are described by:

(13) η=yxRax14, Pr=να, Le=αDB,Nb=(ρc)p (ϕw-ϕ)(ρc)f α, Nt=(ρc)p DT(Tw-T)(ρc)f α T, M=σ*B02  μf L2, L=να Rax14(1-ϕ)βg(Tw-T)3,Ec=[g β (1-ϕ)]2[να RaxTw-T]3(Cp)f, Rax=(1-ϕ)βg(Tw-T)x3να.

Here, gravitational acceleration, volumetric expansion coefficient of the fluid, nanoparticle volume fraction at the surface, ambient nanoparticle volume fraction attained as y tends to be infinite, and local Rayleigh number, respectively, are also the symbols g, β, ϕw, ϕ, and Rax. In addition, f, θ, and ϕ are the dimensionless of the stream function, temperature, and volume of nanoparticles respectively. It distinguishes the local skin friction Cf, the reduced Nusselt number Nur and the reduced Sherwood number Shr[10]

(14) 12(PrRex2Rax34)Cf=f''(0),Nur=-θ'(0), Shr=-ϕ'(0).

where, Rex is the local Reynolds number based on the stretching velocity uw(x).

2.1 Chebyshev pseudospectral differentiation matrix technique

A numerical solution based on Chebyshev collocation approximations can be considered as a suitable choice for many practical problems (as described in the literature review and for example Canuto et al. [29] and Peyret [30]). Accordingly, Chebyshev collocation method will be applied for the presented model. The derivatives of the function f (x) at the Gauss-Lobatto points, xk=cos(kπL*) , which are the linear combination of the values of the function f (x) [31],

f(n)=D(n)f,

where

f=[f(x0),f(x1),...,f(xL*)]T,

and

f(n)=[f(n)(x0),f(n)(x1),...,f(n)(xL*)]T,

where

D(n)=[dk,j(n)],

or

f(n)(xk)=j=0L*dk,j(n)f(xj),

where

dk,j(n)=2γj*L*l=nL*m=0(m+l-n)evenl-nγl*am,ln (-1)[ljL*]+[mkL*]xlj-L*[ljL*]xmk-L*[mkL*],

where,

am,ln =2nl(n-1)!cm(s-m+n-1)! (s+n-1)!(s)! (s-m)!,

such that 2s = l + mn and c0 = 2, ci = 1, i ≤ 1, where k, j = 0, 1, 2, ..., L* and γ0*=γl*=12 , γj*=1  for j = 1, 2, 3, ..., L − 1. The round off errors (see Appendix A) incurred during computing differentiation matrices D(n) are investigated in [31].

2.2 Description of the numerical method

The grid points (xi, xj) in this situation are given as xi=cos(iπL1*) , xj=cos(jπL2*) for i=1,...,L1*-1 and j=1,...,L2*-1 . The domain in the x–direction is [0, xmax] where xmax is the length of the dimensionless axial coordinate and the domain in the η–direction is [0, ηmax] where ηmax corresponds to η. The domain [0, xmax] × [0, ηmax] is mapped into the computational domain [0, xmax] × [−1, 1]. The application of this method to differential equation leads to system of algebric equations. The first rows and last rows of the coefficients matrix of the algebric system are replaced by a suitable formulation of the boundary conditions. The Chebyshev collocation method is more accurate in comparison with other techniques for solving this kind of problems, espcially the finite difference and the finite elements methods. The finite difference methods replace the derivatives of a function at any point with finite difference approximation formulas in terms of its values on a grid of mesh points that span the domain of interest. The numbers of these mesh points are two and three for the central finite difference of second order of the first and second derivatives, respectively. While in Chebyshev collocation method, the derivatives of a non-singular function at any point from the Chebyshev points are expanded as a linear combination from the values of the function at all of these points. i.e. (the approximations of the derivatives are defined over the whole domain).

Therefore, Eqs. (9)(11) with the boundary conditions (12) have been solved numerically [18, 19]. Thus by applying the Chebyshev collocation approximation to equations (9)(11). The following Chebyshev collocation equations can be obtained:

(15) (2ηmax)3(l=0L*dj,l(3)fl)+(34Pr) fj (2ηmax)2(l=0L*dj,l(2)fl)-(24Pr)(2ηmax)2(l=0L*dj,l(1)fl)2-M(2ηmax)(l=0L*dj,l(1)fl)=0,

(16) (2ηmax)2 (l=0L*dj,l(2)θl)+(34) fj (2ηmax)(l=0L*dj,l(1)θl)+Nb(2ηmax)2(l=0L*dj,l(1)ϕl)(l=0L*dj,l(1)θl)+Nt(2ηmax)2(l=0L*dj,l(1)θl)2+Ec (2ηmax)4(l=0L*dj,l(2)fl)2+M Ec (2ηmax)2(l=0L*dj,l(1)fl)2=0,

(17) (2ηmax)2 (l=0L*dj,l(2)ϕl)+(34)Le fj (2ηmax)(l=0L*dj,l(1)ϕl)+NtNb(2ηmax)2 (l=0L*dj,l(2)θl)=0.

The computer program of the numerical method and the numerical computations have been done by the symbolic computation software Mathematica 6TM. Also, the solution of the above equations (15)(17) for the unknowns fi, θj and ϕj with boundary conditions (12) where j = 1(1)L* (take L* = 32) and ηmax corresponds to η are obtained using the Newton-Raphson iteration technique.

3 Results and Discussion

3.1 Validation of the numerical solution

The results for the local skin friction f″(0) are compared with those obtained by Abd Elazem [19] for different values of Pr, s, and ηmax in Table 1. It is noticed that the comparison shows excellent agreement for each values of Pr, s, and ηmax. Also, dimensionless similarity functions f (η), θ(η) and ϕ(η) are matching with the previously published [19] as shown in Fig. 2. Therefore, it is confident that the present results are very accurate.

Figure 2 Comparison of the proposed study with previous work published by Abd Elazem [19] in the case of Pr = Le = 1, Nb = Nt = 0.1, s = 0.1, and M = Ec = 0
Figure 2

Comparison of the proposed study with previous work published by Abd Elazem [19] in the case of Pr = Le = 1, Nb = Nt = 0.1, s = 0.1, and M = Ec = 0

Table 1

Comparison test results for local skin friction f″(0) when (a) Nb = Nt = 0.1, Le = 10, M = Ec = 0.0, and s = 1 at different values of Pr

(b) Nb = Nt = 0.1, Pr = Le = 10, and M = Ec = 0.0 at different values of s

(c)Nb = Nt = 0.1, Pr = 10, Le = 100, M = Ec = 0.0, and s = 5 at different values of ηmax

(a) Pr 1 3 10 103 105
Abd Elazem [19] −1.24162 −0.591478 −0.291396 −0.10255 −0.100026
Present results −1.24162 −0.591478 −0.291396 −0.10255 −0.100026
(b) s −10.0 −5.0 −0.5 −5.0 −10.0
Abd Elazem [19] −0.0645743 −0.116767 −0.270266 −0.500422 −0.825446
Present results −0.0645743 −0.116767 −0.270266 −0.500422 −0.825446
(c) ηmax 1 3 5 10 20
Abd Elazem [19] −1.22092 −0.615552 −0.53052 −0.500422 −0.49848
Present results −1.22092 −0.615552 −0.53052 −0.500422 −0.49848

3.2 Results for temperature and solid volume fraction profiles

Equations (9)(11) have been numerically solved with the boundary conditions (12) using the Chebyshev pseudospectral technique. It is found that as the distance increases from the solid boundaries, both the temperature and the concentration profiles start at unity near the wall and reach to vanish. In the case of Nt = Nb = 0.1, Pr = Le = 1, s = 0.01 and M = 1, Figure 3 serves to highlight the present numerical results for Ec = −0.05, −0.01, 0.0, 0.01 on temperature profiles. It is demonstrated that with an increase in Ec, the temperature profiles and thermal boundary layer thickness are enhanced. Physically, the ohmic heating effect due to the effects on electromagnetic work is found to be produced an increase in the fluid temperature, and thus a decrease in the surface temperature gradient. Further, it is found that the effect of viscous heating leads to an increase in the temperature; this effect is more pronounced in the presence of the magnetic filed. It is acknowledged that an increase in Nt, the temperature profile accelerates also, the temperature profile raises the elevation of the Eckert number as shown in Fig. 4 (positive Ec values correspond to wall heating, while the opposite is true for Ec negative values).

Figure 3 Effect of Ec on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1
Figure 3

Effect of Ec on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1

Figure 4 Effects of Ec and Nt on temperature profiles for Nb = 0.1, Pr = Le = 1, s = 0.01, and M = 1
Figure 4

Effects of Ec and Nt on temperature profiles for Nb = 0.1, Pr = Le = 1, s = 0.01, and M = 1

The temperature decreases as Pr increases. This is in agreement with the physical fact that the thermal boundary layer thickness decreases with increasing Pr. Further, according to Fig. 5, the numerical results for the profiles of θ(η) for (a) Ec = −0.01 and (b) Ec = 0.01 when Pr = 0.7, 1, 10, 105 at Nt = Nb = 0.1, Le = 1, s = 0.01, and M = 1. Physically the thermal boundary-layer thickness, as predicted, is less than the boundary-layer thickness of the momentum when Pr ≫ −1. Also, the temperature function decreases (see Fig. 5). At high values of the Prandtl number Pr (values of Pr ≫ −1, decrease conductivity, and increase pure convection). Besides the typical matching of temperature profiles [19] at values (10 < Pr ≤ 105). Notwithstanding this, it should also be noticed that with the rise in Ec from −0.01 to 0.01, there is a slightly greater difference in Ec = 0.01 if Pr = 0.7, 1 (see Fig. 5).

Figure 5 Effects of Ec and Pr on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1
Figure 5

Effects of Ec and Pr on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1

By contrast, it is clearly shown that an increase in M and Ec increases the thermal boundary layer thickness and the temperature profiles. Physically, application of a transverse magnetic field to an electrically conducting fluid creates a resistive-type force called the Lorentz force. This conclusion meets the logic that the magnetic field exerts a retarding force on the free-convection flow in the boundary layer and increase its temperature (see Figure 6).

Figure 6 Effects of Ec and M on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1
Figure 6

Effects of Ec and M on temperature profiles for Nb = Nt = 0.1, Pr = Le = 1, s = 0.01, and M = 1

In the case of Le > 1, the thickness of the boundary-layer for mass friction function is smaller than the thermal boundary-layer thickness (see Fig. 7). Variations in the concentration function increased with Ec growing far from the boundary. Concentration function profiles generally decrease with the rise in Lewis number as in Fig. 7. It can be seen that an increment in Lewis number decreases the solid volume fraction of nanofluid profiles. Physically, This is due to the fact that mass transfer rate of nanofluid increases as Lewis number increases. It also reveals that the concentration gradient at surface of the stretching sheet increases. Moreover, the concentration at the surface of stretching sheet decreases as Lewis number increases. Finally, Figure 8 shows the variation of Concentration profiles with Nb and Ec when Nt = 0.1, Pr = 10, Le = 1.5, s = 0.01, and M = 3. It's clear that the thickness of the boundary layer for mass friction function decreased as Nb increased. Besides, the concentration profiles decrease with the increase of the Eckert number. Physically, the Brownian motion parameter helps to measure the strength of the Brownian diffusion of the nanoparticles in the flow field. Due to the Brownian diffusion, the nanoparticles tend to move away from the surface of the sheet and as result a decrease in nanoparticle volume fraction is encountered within the boundary layer region.

Figure 7 Effects of Ec and Le on concentration profiles for Nt = Nb = 0.1, Pr = 1, s = 0.01, and M = 1
Figure 7

Effects of Ec and Le on concentration profiles for Nt = Nb = 0.1, Pr = 1, s = 0.01, and M = 1

Figure 8 Effects of Ec and Nb on concentration profiles for Nt = 0.1, Pr = 10, Le = 1, s = 0.01, and M = 1
Figure 8

Effects of Ec and Nb on concentration profiles for Nt = 0.1, Pr = 10, Le = 1, s = 0.01, and M = 1

3.3 Results for reduced Nusselt number and reduced Sherwood number

Table 2 calculates the numerical results for the reduced Nusselt number and the reduced Sherwood number when Nt = 0.1, 0.3, 0.5 for different Nb values, where Pr = Le = 10, M = 1, Ec = 0.01, and s = 0.01. It is reported that the reduced Nusselt number is a decreasing function while an increasing function is the reduced Sherwood number. Physically, It is also found that the impact of Joule heating on electromagnetic operation has resulted in a rise in the fluid temperature and therefore a decrease in the gradient of the surface temperature. Furthermore, the actual impact of viscous heating results in a temperature increase; this effect is more pronounced in the presence of the magnetic field. As shown in Table 3, it is clear that the reduced Nusselt number is a monotonous function (i.e. it is an increasing function at Ec = −0.01, whereas a decreasing function at Ec = 0.0, 0.01).

Table 2

(a) Variation of the reduced Nusselt number Nur = −θ′ (0) with Nt and Nb (b) Variation of the reduced Sherwood number Shr = − ϕ′ (0) with Nt and Nb when Pr = Le = 1, M = 1, Ec = 0.01, and s = 0.01

(a) Nt = 0.1 Nt = 0.3 Nt = 0.5



Nb Nur Nb Nur Nb Nur

0.1 0.18658 0.1 0.166257 0.1 0.147136
0.3 0.150689 0.3 0.132122 0.3 0.11468
0.5 0.11767 0.5 0.100782 0.5 0.0849405

(b) Nt = 0.1 Nt = 0.3 Nt = 0.5



Nb Shr Nb Shr Nb Shr

0.1 0.322289 0.1 0.159911 0.1 0.0592868
0.3 0.403315 0.3 0.367966 0.3 0.351229
0.5 0.418986 0.5 0.408024 0.5 0.407115
Table 3

(a) Variation of the reduced Nusselt number Nur = −θ′(0) with Ec and M (b) Variation of the reduced Sherwood number Shr = − ϕ′(0) with Ec and M when Pr = Le = 1, Nt = Nb = 0.1, and s = 0.01

(a) Ec = −0.01 Ec = 0.0 Ec = 0.01



M Nur M Nur M Nur

0 0.598195 0 0.480109 0 0.361897
1 0.605839 1 0.396299 1 0.18658
10 0.80447 10 0.216987 10 −0.370631

(b) Ec = −0.01 Ec = 0.0 Ec = 0.01



M Shr M Shr M Shr

0 0.0991581 0 0.202953 0 0.306863
1 −0.0647157 1 0.128701 1 0.322289
10 −0.50287 10 0.0754746 10 0.653956

4 Conclusion

The effects of various physical parameters on nanofluids that flow past a stretching surface were explored. This study is very important for engineers and researchers in nearly every branch in engineering and science. Nuclear power plants, gas turbines and the various propulsion devices for aircraft, missiles, satellites and space vehicles are examples of such engineering areas. Numerically a system of nonlinear ordinary differential equations was solved using Chebyshev's pseudospectral technique at specified physical parameters. From previous results, it can be concluded that:

  1. It has been found that the present results show that the reduced number of Nusselt is a decreasing function at a fixed value of Ec = 0.01, while the reduced number of Sherwood is an increasing function for variation of Nt with Nb, at Pr = Le = 10, M = 1, and s = 0.01.

  2. It has been noted that the current results indicate that the reduced number of Nusselt and the reduced number of Sherwood are monotonous functions for variation of M with Ec when Nb = Nt = 0.1, Pr = Le = 1, and s = 0.01.

  3. The magnetic field, Joule heating, Eckert number and thermophoresis parameter improves the temperature field and increases the thermal boundary layer thickness while the Prandtl number Pr reduces the temperature field and decreases the thermal boundary layer thickness where the Prandtl number Pr does not affect the temperature profile (10 ≺ Pr ≤ 105).

  4. Changing the parameter Nb as known at values (0.1, 0.3, 0.5) decreases the profile of the concentration. Furthermore, the Eckart number (from −0.01 ≤ Ec ≤ 0.01) has a direct impact on the concentration profile, where the Eckart number reduces the profile of concentration.

  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.

A Chebyshev collocation approximation

A.1 Rounding off error analysis

The round off errors incurred during computing differentiation matrices D(n) investigated by [31]. Elbarbary and Elsayed [31] show that, the elements of the first order differentiation matrix, there would be round off error as in:

dk,j1*-dk,j14γj*(δ-O(1N2δ)(N23+16))

The element d011 is the major elements concerning its values. Accordingly, it bears the major error responsibility comparing the other elements. Meanwhile, Baltensperger and Trummer [32] show that, the error in the evaluation of the element DO1 from the classical matrix D is of order O(N4δ) where δ is the machine precision and D01*-D01=8N4π4δ , whereas in Elbarbary and El-sayed [31] find the error of order O(N2 δ) where,

d011*-d011(13-N+23N2)δ

This can be taken into consideration, as itself, as modifing the classical matrix D. Due to,

d011=2Nk=1N-1k2xk-N=-13+(-4π2)N2+O(1N2),

with error upper bound

d011*-d011=2Nk=1N-1k2δk(13-N+23N2)δ

Also, Elbarbary and El-sayed [31] show that the error bound for the second order derivatives can be given by

dk,j2*-dk,j243γj*(δ-O(1N2δ))(N45-15)

and the error bound for the third order derivatives is given by Elbarbary and El-sayed [31]

dk,j3*-dk,j3γj*(δ-O(1N2δ))(2N6105-N415-N215+435)

Finally, the error bound for the fourth order derivatives is given by Elbarbary and El-sayed [31]

dk,j4*-dk,j4γj*(δ-O(1N2δ))(2N8945-8N6315+2N245+124N2945-16105)

Table 4 lists the computed errors in the elements d011 and D01.

Table 4

Computed errors in d011 and D01

N d011*-d011 Error upper bound (13-N+23N2)δ D01*-D01
16 7.80 × 10−15 3.44 × 10−14 9.78 × 10−14
32 4.06 × 10−14 1.45 × 10−13 3.64 × 10−12
64 9.07 × 10−14 5.92 × 10−13 1.70 × 10−11
128 3.05 × 10−13 2.40 × 10−12 6.58 × 10−10
256 5.29 × 10−12 9.64 × 10−12 1.34 × 10−08
512 2.15 × 10−12 3.87 × 10−11 1.89 × 10−07
1024 9.35 × 10−12 1.55 × 10−10 1.78 × 10−06
2048 3.88 × 10−10 6.20 × 10−10 4.43 × 10−05
4096 2.39 × 10−09 2.48 × 10−09 1.73 × 10−04

A.2 Example 1

Consider the following boundary value problem [33]

f''(η)+f(η)f''(η)+(f(η))2=0,

f(0)=1,f(0)=0,f()=0.

The exact solution is given by

f(η)=2tanh(η2)

Table 5 represents the values of f (η) for the exact solution, the shooting method and the present method.

Table 5

Values of f(η) for the exact solution, the shooting method and the present method.

ηi The exact solution Chebyshev collocation method Shootting method
0.0 0.0 0.0 3.1102 × 10−21
0.0192611 0.019259909142530 0.0192598893877356 0.0192598920332745
0.30448182 0.299862737492030 0.2998596464550248 0.2998595813143047
0.674122 0.627313706235097 0.6272992113043429 0.6272995450854674
1.17157 0.961141183786619 0.9611070045979400 0.9611054342686112
1.77772 1.202428601606520 1.2023643183102284 1.2023645509982483
2.46927 1.330665896574968 1.3305704365379722 1.330570838696424
3.60793 1.397114413277153 1.3969685880488372 1.396968522682298
4.39207 1.4085494708083601 1.4083673080884052 1.408367284942106
5.16114 1.4123021434700513 1.4120834942495526 1.4120834612222437
5.88559 1.4135271302075076 1.4132736020214456 1.4132735693434024
6.53757 1.4139405233760458 1.4136553770920586 1.4136553408479557
7.09204 1.4140889100927603 1.4137767754240098 1.4137767398762842
7.52769 1.4141462431225706 1.4138128682103317 1.4138128330749593
7.92314 1.4141750797928212 1.4138224084323320 1.4138223729952500
ηmax = 8 1.4141790433479533 1.4138226201158337 1.4138225847075525

The error of Shootting method (Ee,Shooting) and (the error Ee,ChC) of the present method is given in Table 6.

Table 6

The maximum absolute error

Ee,ChC Ee,Shooting
0 3.1102 × 10−21
1.97548 × 10−8 1.71093 × 10−8
3.09104 × 10−6 3.15618 × 10−6
1.44949 × 10−5 1.4161 × 10−5
3.41792 × 10−5 3.57495 × 10−5
6.42833 × 10−5 6.40506 × 10−5
9.546 × 10−5 9.50579 × 10−5
1.45825 × 10−4 1.45891 × 10−4
1.82163 × 10−4 1.82186 × 10−4
2.18649 × 10−4 2.18682 × 10−4
2.53528 × 10−4 2.53561 × 10−4
2.85146 × 10−4 2.85183 × 10−4
3.12135 × 10−4 3.1217 × 10−4
3.33375 × 10−4 3.3341 × 10−4
3.52671 × 10−4 3.52707 × 10−4
3.56423 × 10−4 3.56459 × 10−4

Nomenclature

x, y

Cartesian coordinates/m

u, v

Horizontal and vertical velocity components/m · s−1

uw(x)

Stretching velocity/m · s−1

μf

Dynamic viscosity of base fluid/Pa · s

ν

Kinematic viscosity/m2 · s−1

kf

Thermal conductivity/W · m−1 · K−1

a

Stretching rate/s−1

ρf

Density/kg · m−3

P

Fluid pressure

σ*

Fluid Electric conductivity/(Ωm)−1

B0

Applied magnetic field intensity/A · m−1

α

Thermal diffusivity

τ

Heat capacity ratio for fluid and nanoparticles

DB

Brownian diffusion

T

Local temperature of the fluid/K

C

Concentration distributions/kg · m−3

(ρc)f

Fluid's productive heat capacity/J · m−3

s

Suction or injection parameter

Tw

Temperature of the sheet/K

T

Temperature of the fluid fat away from the sheet/K

DT

Thermophoresis diffusion coefficient/m2 /s

Cw

Solid volume friction of the sheet

Shr

Reduced Sherwood number

g

Gravitational acceleration

β

Volumetric expansion coefficient of the fluid

ϕw

Nanoparticle volume fraction at the surface

ϕ

Ambient nanoparticle volume fraction attained as y tends to be infinite

Rax

Local Rayleigh number

C

Solid volume friction far away from the sheet

Ec

Eckert number

ϕ

Dimensionless of the concentration

f

Dimensionless of the stream function

θ

Dimensionless of the temperature

ψ

Stream function

Pr

Prandtl number

Cf

Local skin friction coefficient/Pascal

η

Dimensionless space variable

(ρc)p

Nanoparticles’ productive heat capacity/J · m−3

MHD

Magnetohydrodynamics

Le

Lewis number

Nb

Brownian motion parameter

Nt

Thermophoresis parameter

M

Magnetic parameter

Rex

Reynolds number

Nur

Reduced Nusselt number

References

[1] Kalaivanan R, Ganga B, Vishnu Ganesh N, Abdul Hakeem AK. Effect of elastic deformation on nanosecond grade fluid flow over a stretching surface. Front Heat Mass Transf. 2018;10(20).10.5098/hmt.10.20Search in Google Scholar

[2] Vleggaar J. Laminar boundary layer behaviour on continuous accelerating surface. Chem Eng Sci. 1977;32(12):1517–25.10.1016/0009-2509(77)80249-2Search in Google Scholar

[3] Fisher EG. Extrusion of Plastics, Journal Polymer Science: Polymer Letters Edition. New York: Halsted Press, Wiley; 1976.Search in Google Scholar

[4] Choi SUS. Enhancing thermal conductivity of fluids with nanoparticles, Developments and Applications of Non-Newtonian Flows. FED-vol. 231/MDvol. 66, 1995, 99–105.Search in Google Scholar

[5] Oztop HF, Abu-Nada E. Numerical study of natural convection in partially heated rectangular enclosures filled with nanofluids. Int J Heat Fluid Flow. 2008;29(5):1326–36.10.1016/j.ijheatfluidflow.2008.04.009Search in Google Scholar

[6] Eastman JA, Choi SU, Li S, Yu W, Thompson LJ. Anomalously increased effective thermal conductivity of ethylene glycol-based nanofluids containing copper nanoparticles. Appl Phys Lett. 2001;78(6):718–20.10.1063/1.1341218Search in Google Scholar

[7] Minsta HA, Roy G, Nguyen CT, Doucet D. New temperature dependent thermal conductivity data for water-based nanofluids. Int J Therm Sci. 2009;48(2):363–71.10.1016/j.ijthermalsci.2008.03.009Search in Google Scholar

[8] Khan WA, Pop I. Boundary-layer flow of a nanofluid past a stretching sheet. Int J Heat Mass Transf. 2010;53(11–12):2477–83.10.1016/j.ijheatmasstransfer.2010.01.032Search in Google Scholar

[9] Kakac S, Pramuanjaroenkij A. Review of convective heat transfer enhancement with nanofluids. Int J Heat Mass Transf. 2009;52(13–14):3187–319.10.1016/j.ijheatmasstransfer.2009.02.006Search in Google Scholar

[10] Kuznetsov AV, Nield DA. Natural convective boundary layer flow of a nanofluid past a vertical plate. Int J Therm Sci. 2010;49(2):243–7.10.1016/j.ijthermalsci.2009.07.015Search in Google Scholar

[11] Noghrehabad A, Salamat P, Ghalambaz M. Integral treatment for forced convection heat and mass transfer of nanofluids over linear stretching sheet. Appl Math Mech (Eng Ed). 2015;36(3):337–352.10.1007/s10483-015-1919-6Search in Google Scholar

[12] Mansur S, Ishak A, Pop I. Flow and heat transfer of nanofluid past stretching/shrinking sheet with partial slip boundary conditions. Appl Math Mech (Eng Ed). 2014;35(11):1401–1410.10.1007/s10483-014-1878-7Search in Google Scholar

[13] Das S, Choi SU, Yu W, Pradeep T. Nanofluids: Science and Technology. New York: Wiley; 2007. https://doi.org/10.1002/9780470180693.10.1002/9780470180693Search in Google Scholar

[14] Turkyilmazoglu M. Exact analytical solutions for heat and mass transfer of MHD slip flow in nanofluids. Chem Eng Sci. 2012;84:182–7.10.1016/j.ces.2012.08.029Search in Google Scholar

[15] Hamad MAA. Analytical solution of natural convection flow of a nanofluid over a linearly stretching sheet in the presence of magnetic field. Int Commun Heat Mass Transf. 2011;38(4):487–92.10.1016/j.icheatmasstransfer.2010.12.042Search in Google Scholar

[16] Niazi MD, Hang XU. Modelling two-layer nanofluid flow in a microchannel with electro-osmotic effects by means of Buongiorno's model. Appl Math Mech (Eng Ed). 2020;41(1):83–104.10.1007/s10483-020-2558-7Search in Google Scholar

[17] Elgazery NS, Abd Elazem NY. Effects of viscous dissipation and Joule heating for natural convection in a hydromagnetic fluid from heated vertical wavy surface. Z. N. A. 2011;66a:427–40.10.1515/zna-2011-6-708Search in Google Scholar

[18] Abd Elazem NY. Numerical solution for nanofluid flow past a permeable stretching or shrinking sheet with slip condition and radiation effect. J Comput Theor Nanosci. 2015;12(10):3827–34.10.1166/jctn.2015.4288Search in Google Scholar

[19] Abd Elazem NY. Numerical solution for the effect of suction or injection on flow of nanofluids past a stretching sheet. Z. N. A. 2016;71a(6):511–5.10.1515/zna-2016-0035Search in Google Scholar

[20] Kameswaran PK, Narayana M, Sibanda P, Murthy PV. Hydromagnetic nanofluid flow due to a stretching or shrinking sheet with viscous dissipation and chemical reaction effects. Int J Heat Mass Transf. 2012;55(25–26):7587–95.10.1016/j.ijheatmasstransfer.2012.07.065Search in Google Scholar

[21] Makinde OD. Analysis of Sakiadis flow of nanofluids with viscous dissipation and Newtonian heating. Appl Math Mech (Eng Ed). 33(12) (2012) 1545–1554. https://doi.org/10.1007/s10483-012-1642-8.10.1007/s10483-012-1642-8Search in Google Scholar

[22] Mousavi SM, Dinarvand S, Yazdi ME. Generalized second-order slip for unsteady convective flow of a nanofluid: a utilization of Buongiorno's two-component nonhomogeneous equilibrium model. Nonl Eng. 2020;9(1):156–68.10.1515/nleng-2020-0005Search in Google Scholar

[23] Pavlov KB. Magnetohydrodynamic flow of an incompressible viscous fluid caused by deformation of a plane surface. Magnitnaya Gidrodinamika. 1974;4:146–7.Search in Google Scholar

[24] Takhar HS, Chamkha AJ, Nath G. Unsteady three dimensional MHD boundary-layer flow due to the impulsive motion of a stretching surface. Acta Mech. 2001;146(1–2):59–71.10.1007/BF01178795Search in Google Scholar

[25] Alwawi FA, Alkasasbeh HT, Rashad AM, Idris R. MHD natural convection of Sodium Alginate Casson nanofluid over a solid sphere. Results Phys. 2020;16:102818.10.1016/j.rinp.2019.102818Search in Google Scholar

[26] Devaki P, Venkateswarlu B, Srinivas S, Sreenadh S. MHD Peristaltic flow of a nanofluid in a constricted artery for different shapes of nanosized particles. Nonlinear Eng. 2020;9(1):51–9.10.1515/nleng-2017-0064Search in Google Scholar

[27] Rasool G, Shafiq A. Numerical exploration of the features of thermally enhanced chemically reactive radiative Powell-Eyring nanofluid flow via Darcy medium over nonlinearly stretching surface afected by a transverse magnetic field and convective boundary conditions. Appl Nanosci. 2020. https://doi.org/10.1007/s13204-020-01625-2.10.1007/s13204-020-01625-2Search in Google Scholar

[28] Shafiq A, Rasool G, Khalique CM, Aslam S. Second grade bio-convective nanofluid flow with buoyancy effect and chemical reaction. Symmetry (Basel). 2020;12(4):621.10.3390/sym12040621Search in Google Scholar

[29] Canuto C, Hussaini MY, Zang TA. Spectral methods in fluid dynamics. New York: Springer-Verlag. 1988. https://doi.org/10.1007/978-3-642-84108-8.10.1007/978-3-642-84108-8Search in Google Scholar

[30] Peyret R. Spectral methods for incompressible viscous flow. New York: Springer-Verlag. 2002. https://doi.org/10.1007/978-1-4757-6557-1.10.1007/978-1-4757-6557-1Search in Google Scholar

[31] Elbarbary EM, El-Sayed SM. Higher order pseudospectral differentiation matrices. Appl Numer Math. 2005;55(4):425–38.10.1016/j.apnum.2004.12.001Search in Google Scholar

[32] Baltensperger R, Trummer MR. Spectral differencing with a twist. SIAM J Sci Comput. 2003;24(5):1465–87.10.1137/S1064827501388182Search in Google Scholar

[33] Seddeek MA, Abdelmeguid MS. Effects of radiation andthermal diffusivity on heat transfer over a stretching surface with variable heat flux. Phys Lett A. 2006;348(3–6):172–9.10.1016/j.physleta.2005.01.101Search in Google Scholar

Received: 2020-07-28
Accepted: 2021-01-28
Published Online: 2021-04-23

© 2021 Nader Y. Abd Elazem, published by De Gruyter

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

Articles in the same Issue

  1. Nonlinear absolute sea-level patterns in the long-term-trend tide gauges of the East Coast of North America
  2. Insight into the significance of Joule dissipation, thermal jump and partial slip: Dynamics of unsteady ethelene glycol conveying graphene nanoparticles through porous medium
  3. Numerical results for influence the flow of MHD nanofluids on heat and mass transfer past a stretched surface
  4. A novel approach on micropolar fluid flow in a porous channel with high mass transfer via wavelet frames
  5. On the exact and numerical solutions to a new (2 + 1)-dimensional Korteweg-de Vries equation with conformable derivative
  6. On free vibration of laminated skew sandwich plates: A finite element analysis
  7. Numerical simulations of stochastic conformable space–time fractional Korteweg-de Vries and Benjamin–Bona–Mahony equations
  8. Dynamical aspects of smoking model with cravings to smoke
  9. Analysis of the ROA of an anaerobic digestion process via data-driven Koopman operator
  10. Lie symmetry analysis, optimal system, and new exact solutions of a (3 + 1) dimensional nonlinear evolution equation
  11. Extraction of optical solitons in birefringent fibers for Biswas-Arshed equation via extended trial equation method
  12. Numerical study of radiative non-Darcy nanofluid flow over a stretching sheet with a convective Nield conditions and energy activation
  13. A fractional study of generalized Oldroyd-B fluid with ramped conditions via local & non-local kernels
  14. Analytical and numerical treatment to the (2+1)-dimensional Date-Jimbo-Kashiwara-Miwa equation
  15. Gyrotactic microorganism and bio-convection during flow of Prandtl-Eyring nanomaterial
  16. Insight into the significance of ramped wall temperature and ramped surface concentration: The case of Casson fluid flow on an inclined Riga plate with heat absorption and chemical reaction
  17. Dynamical behavior of fractionalized simply supported beam: An application of fractional operators to Bernoulli-Euler theory
  18. Mechanical performance of aerated concrete and its bonding performance with glass fiber grille
  19. Impact of temperature dependent viscosity and thermal conductivity on MHD blood flow through a stretching surface with ohmic effect and chemical reaction
  20. Computational and traveling wave analysis of Tzitzéica and Dodd-Bullough-Mikhailov equations: An exact and analytical study
  21. Combination of Laplace transform and residual power series techniques to solve autonomous n-dimensional fractional nonlinear systems
  22. Investigating the effects of sudden column removal in steel structures
  23. Investigation of thermo-elastic characteristics in functionally graded rotating disk using finite element method
  24. New Aspects of Bloch Model Associated with Fractal Fractional Derivatives
  25. Magnetized couple stress fluid flow past a vertical cylinder under thermal radiation and viscous dissipation effects
  26. New Soliton Solutions for the Higher-Dimensional Non-Local Ito Equation
  27. Role of shallow water waves generated by modified Camassa-Holm equation: A comparative analysis for traveling wave solutions
  28. Study on vibration monitoring and anti-vibration of overhead transmission line
  29. Vibration signal diagnosis and analysis of rotating machine by utilizing cloud computing
  30. Hybrid of differential quadrature and sub-gradients methods for solving the system of Eikonal equations
  31. Developing a model to determine the number of vehicles lane changing on freeways by Brownian motion method
  32. Finite element method for stress and strain analysis of FGM hollow cylinder under effect of temperature profiles and inhomogeneity parameter
  33. Novel solitons solutions of two different nonlinear PDEs appear in engineering and physics
  34. Optimum research on the temperature of the ship stern-shaft mechanical seal end faces based on finite element coupled analysis
  35. Numerical and experimental analysis of the cavitation and study of flow characteristics in ball valve
  36. Role of distinct buffers for maintaining urban-fringes and controlling urbanization: A case study through ANOVA and SPSS
  37. Significance of magnetic field and chemical reaction on the natural convective flow of hybrid nanofluid by a sphere with viscous dissipation: A statistical approach
  38. Special Issue: Recent trends and emergence of technology in nonlinear engineering and its applications
  39. Research on vibration monitoring and fault diagnosis of rotating machinery based on internet of things technology
  40. An improved image processing algorithm for automatic defect inspection in TFT-LCD TCON
  41. Research on speed sensor fusion of urban rail transit train speed ranging based on deep learning
  42. A Generalized ML-Hyers-Ulam Stability of Quadratic Fractional Integral Equation
  43. Study on vibration and noise influence for optimization of garden mower
  44. Relay vibration protection simulation experimental platform based on signal reconstruction of MATLAB software
  45. Research on online calibration of lidar and camera for intelligent connected vehicles based on depth-edge matching
  46. Study on fault identification of mechanical dynamic nonlinear transmission system
  47. Research on logistics management layout optimization and real-time application based on nonlinear programming
  48. Complex circuit simulation and nonlinear characteristics analysis of GaN power switching device
  49. Seismic nonlinear vibration control algorithm for high-rise buildings
  50. Parameter simulation of multidimensional urban landscape design based on nonlinear theory
  51. Research on frequency parameter detection of frequency shifted track circuit based on nonlinear algorithm
Downloaded on 4.11.2025 from https://www.degruyterbrill.com/document/doi/10.1515/nleng-2021-0003/html
Scroll to top button