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18 IJSTR©2018

www.ijstr.org

Solving MHD Pipe Flow Of A Third Grade Fluid

With Vogel Model Viscosity And Joule Heating

Using The Adomian Decomposition Method

M. 0. Iyoko, G. T. Okedayo, L. N. Ikpakyegh, J. O. Ode

Abstract: In this paper we investigated the effect of a magnetic force on the flow of a third grade fluid through a pipe. The existing model equations were extended to incorporate a magnetic effect term in the momentum equation and a joule heating term in the energy equation. The dimensional analysis of the momentum and energy equations was carried out and the Adomian decomposition method was used to find a three point series solution to the velocity and temperature of the fluid, for the Vogel’s model viscosity. Graphs for the velocity and temperature profiles for various values of the thermo-physical parameters were presented. When the magnetic effect parameter and the joule heating parameter are set to be zero, the result was compared with the regular perturbation method result of a previous work in order to validate the use of the Adomian decomposition method.

Index Terms: Adomian decomposition method, Joule heating, Magnetohydrodynamics (MHD), Pipe flow, Third grade fluid, Vogel model viscosity, Regular perturbation method.

————————————————————

1

INTRODUCTION

A substance that continually deforms (flows) under an applied shear stress and that has the tendency to assume the shape of its container is regarded as a fluid. Fluids may be divided into liquids and gases. Some fluids obey Newton’s constitutive laws and are called Newtonian fluids, while those that do not obey these laws are known as non-Newtonian fluids. Examples of non-Newtonian fluids include mud, paints, ice cream, blood, lubricants, polymers, oils, personal care products, pasta, cheese, slurries, asphalt and many others. Most biological fluids with higher molecular weight components are also non-Newtonian in nature. They exhibit effects such as climbing of a rotating rod in an otherwise still container of fluid, self-siphoning, drag reduction, and transformation into a semisolid when an electric or magnetic field is applied. The non-Newtonian fluids in particular have key importance in geophysics, chemical and nuclear industries, material processing, oil reservoir engineering, bioengineering and many others. Rheological properties of all non-Newtonian fluids cannot be predicted using simple constitutive equations (unlike the case of viscous fluids). Therefore many models of non-Newtonian fluids are based either on ―natural‖ modifications of established macroscopic theories or molecular considerations. The additional rheological parameters in the constitutive equations of non-Newtonian fluids are the main culprit for the lack of analytical solutions.

The resulting equations are more complex and of higher order than the Navier-Stokes equations. Hence these equations have been considered from a modelling as well as solutions point of view [10]. Because of the various applications Non-Newtonian fluids, such as preheating of coal-water mixture, polymer melts and many emulsions several aspects of its steady laminar flow have been studied extensively during the past few decades. Due to the complexities of such fluids, there are many mathematical models governing them. The differential type of fluid is a type of non-Newtonian fluid. Dunn and Rajagopal [] had critically reviewed and presented its thermodynamic analysis. When faced with the problem of heat transfer in fluids of differential type; the third-grade fluid has being of most interest. The rheological and heat transfer characteristics of coal-water mixtures, which is an example of a third grade fluid was presented by [24]. The Reynolds’ and the Vogel’s model viscosities are temperature dependent viscosities. Therefore when studying the flow of a third grade fluid in the presence of heat transfer researchers have used of these model viscosities. Massoudi and Christe [16] presented a model which was used to study the effect of variable viscosities and viscous dissipation on the flow of third grade fluid in a pipe. Approximate analytic solutions to the model were then found by [23]. Olajuwon [18] extended this model to incorporate a heat generation and absorption term in the energy equation, which he solved using a finite difference method. Jayeoba and Okoya [14] worked with the model of Olajuwon [18]. This study considered both Reynolds’ and Vogel’s model viscosities, and the analysis was based on the regular perturbation technique. The heat transfer model was also solved numerically and the numerical solutions for special cases were found to agree excellently with previous ones obtained by the finite difference method. Iyoko et. al. [13] further extended the model equations of Olajuwon [18] to incorporate a magnetic effect term in the momentum equation and a joule heating term in the energy equation. By this extension therefore, the problem became a magnetohydrodynamic flow problem. They used the Adomian decomposition method to find a series solution to the velocity and temperature of the fluid for the Reynolds’ model viscosity. Researchers have applied various methods to obtain approximate analytical solutions of various differential equations of magnetohydrodynamic flow problems, such

___________________________________

M. O. Iyoko holds a master of science degree in industrial mathematics from the University of Agriculture Makurdi,Benue State, Nigeria.

E-mail: [email protected]

G. T. Okedayo is currently a doctor of mathematics at Ondo State University of Science and Technology Okitipupa,Nigeria.

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19 IJSTR©2018

www.ijstr.org research include those of [30], [25], [26], [27], [28], [29] and many others in the references. In this paper therefore we shall present results for the Vogel’s model case of the model equations of Iyoko et. al. [13]. The difference between the Adomian solution and the regular perturbation solution of Jayeoba and Okoya [14] will be computed, and the effect of the various thermo-physical parameters will be discussed with the help of graphical illustrations.

2 DESCRIPTION OF THE MODEL

An infinitely long cylinder is considered with the steady incompressible flow of a third grade fluid as can be seen in Figure 1.

The equations for the velocity and the temperature, given by Massoudi and Christe [16] as well as Yurusoy and Pakdemirli [23], may be extended to incorporate a source term (Olajuwon, [18]) and further extended to incorporate a magnetic effect term and a joule heating term, and given by

r

p

r

d

d

r

r

d

d

r





2 2 1

)

2

(

1

(1)

p

0

(2)

z p r d d r r d d r r d d r r d d r                      



2

0 3 3 2 ( 1

1 (3)

0

2

1 2 2

0 0 4 3 2                                T T C Q r d d r d d r d T d r r d d r K (4)

The required boundary conditions to solve equations (3) and (4) are

0

)

(

)

(

R

T

R

,

(

0

)

(

0

)

0

r

d

T

d

r

d

d

(5)

where all symbols are defined in the Nomenclature. The

source term Q represents the heat generation when Q0 and

the heat absorption term when Q 0. The term 02is the magnetic effect term while the term 022 is the joule heating term. Here equation (3) is to be integrated for a given z

p  

and once the flow field is determined, the actual pressure field can be obtained from equation (1) and (3). Equation (3) is called the momentum equation while equation (4) is called the energy equation. The corresponding dimensionless equations for equations (3)-(5) are given as the following:

C H dr d r dr d dr d r dr d r dr d r dr d dr

d

                           2 2 2 2 2

3 (6)

0 1 2 2 2 2 2                            



J dr d dr d dr d r dr

d (7)

with boundary conditions

0

)

1

(

)

1

(

, (0)(0)0 dr d dr

d

, (8)

The form of equations (6) and (7) depends on the viscosity model, and the viscosity is assumed to be a function of temperature. We now present the Vogel’s model case as can be found in Massoudi and Christe [31], Pakdemirli and Yilmas [19] and Okoya [17].

Here,





)

(

exp

)

(

0 0

T

b

a

T

(9)

The corresponding non-dimensional form of equation (9) is





0

)

(

exp

T

B

A

(10)

The coupled nonlinear ordinary differential equations (6) and (7), with the boundary conditions (8), can be solved in principle by several methods, the Adomian decomposition method being a convenient and effective tool. Here, we shall use the Adomian decomposition method to determine the flow field and thermal distribution.

3 A

NALYTICAL

S

OLUTIONS

In this section, the Adomian decomposition method series solution will be obtained for the dimensionless velocity and temperature by using the Vogel’s model viscosity. Taking the Maclaurin’s series expansion of the exponential term, we can express equation (10) as





1

(

)

)

(

exp

0

2

2

O

B

A

T

B

A

(11)

Which can be written as

 

*

1

2

B

A

C

C

(12)

Where





0 *

)

(

exp

T

B

A

C

C

This implies that

 

2 * 1

1

B

A

C

C

(13)

We can write equation (6) as

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20 IJSTR©2018 www.ijstr.org 3 1 1 2 2

1





 

dr

d

r

dr

d

dr

d

dr

d

r

dr

d

1 1 2 2 2 1

3





H

C

dr

d

dr

d

(14)

With the operator 2 2

dr d L

and dr d R

, applying the inverse operator



 

drdr L1 ()

to both sides of equation (14) and (7) we have equation (15) and (16) respectively

)

(

1

)

(

1

1 1

1

1

R

L

R

R

r

L

CL

Br

A

r

 

 

 

3

 

(

)

1

1 3 1 1 2 1 1

1

R

L

R

L

HL

r

L

(15)

R

r

L

JL

L

Er

C

r

)

1

(

1

1 2

1

 

2

 

2

R

R

(16)

Assuming solutions of the form

 

0

)

(

n n

r

(17)

 

0

)

(

n m

r

(18)

Substituting the series solutions (17) - (18) into equations (11) - (16) and making a one-to-one correspondence between the contributions on the LHS and the terms on the RHS, we obtain the following three point approximations for the velocity and temperature profile as

3 6 7 * 2 2 8 3 * 2 8 5 * 2 6 2 * 2 4 2 * 2 6 2 * 2 4 * 2 4 2 * 2 2 * 4 * 2 4 4 * 4 4 * 2 2 * ) 0 ( 5 8 6720 1 5040 277 360 1 )) 0 ( ( 24 1 ) 0 ( 360 1 ) 0 ( 24 1 ) 0 ( 24 1 ) 0 ( ) 0 ( 2 1 24 1 ) 0 ( 3 1 3 1 ) 0 ( 2 1 ) 1 ( ) 0 ( C r Hw C B AJr C B r A C B Cr A C B r w AJ C B r AJw C B r A C CB r A HC CB r w A HC C r HC CB r A C C r C B r A C w w w                          (19) 2 2 8 3 * 2 4 2 8 2 5 * 2 4 8 2 3 * 2 2 8 5 * 2 8 3 * 6 4 * 2 4 * 4 * 2 2 4 * 6 2 * 2 ) 0 ( ) 0 ( 672 1 ) 0 ( )) 0 ( ( 168 1 )) 0 ( ( 1344 1 ) 0 ( 168 1 ) 0 ( 1344 1 25 14 ) 0 ( 12 1 18 1 2 1 ) 0 ( 12 1 120 1 ) 0 ( 2 1 ) 1 ( ) 0 ( B C r w C JAH B C r w C H JA CB r C H JA CB r C JA B r AJH C r C B Cr A C r CC r JA r C Jw r JC r                               (20)

4 C

OMPUTATIONAL

R

ESULT

S

HOWING THE

DIFFERENCE BETWEEN

ADOMIAN

DECOMPOSITION

AND PERTURBATION SOLUTIONS

For the purpose of comparison, the mid plane temperature distribution of the pipe (0)max for the obtained Adomian decomposition method solution (ADM) when HJ0, and the perturbation solution (P) of Jayeoba and Okoya (2012) are tabulated. The difference between the solutions obtained by the two methods is also computed.

TABLE 1:DIFFERENCE BETWEEN THE VALUE OF max(ADM) AND

) ( max P

WHEN T0C1

TABLE 2:DIFFERENCE BETWEEN THE VALUE OF max(ADM) AND )

( max P

WHEN 1

0 

 

  T C

TABLE 3:DIFFERENCE BETWEEN THE VALUE OF max(ADM) AND )

( max P

WHEN 

AB1

TABLE 4:DIFFERENCE BETWEEN THE VALUE OF max(ADM) AND )

( max P

WHEN

A

B

1

A B1

)

(

max

ADM

max

(

P

)

Difference

B A1

)

(

max

ADM

max

(

P

)

Difference

C T01

)

(

max

ADM

max(P) Difference

0

T C1

) ( max ADM

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21 IJSTR©2018

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TABLE 5:DIFFERENCE BETWEEN THE VALUE OF ( )

max ADM

AND

) ( max P

WHEN AT0CB1

TABLE 6:DIFFERENCE BETWEEN THE VALUE OF ( )

max ADM

AND

) ( max P

WHEN AT0CB1

TABLE 7:DIFFERENCE BETWEEN THE VALUE OF max(ADM) AND )

( max P

WHEN AT0CB1

The physical quantities of principle interest according to the Vogel’s model viscosity are

A

,

B

and

T

0. The difference between the Adomian solution and the perturbation solution as

the values of

A

is varied could be analyzed through Table 1. It is seen from the table that there is a good agreement between the two results as the difference decreases when the

value of

A

increases. For the variation of

B

in Table 2 the difference is at most

1

%

. In Table 3 the variation of the

pressure gradient parameter

C

is considered and it is noticed that as the difference increases for

C

0

.

25

. For

T

0

0

.

5

the difference is less than

1

%

in Table 4. In Table 5 the

difference as the parameter

is varied is investigated and it is observed that for

1

the difference is at most

10

2. Table 6 shows that as

increases the difference increases to at most

10

1, which indicates a good agreement between the two results. Finally, the variation of the heat generation/absorption parameter

is shown in Table 7. For

1

4

.

0

the results are in good agreement with a the

difference reducing to

0

.

7

%

. From the above data it is clear that the Adomian decomposition method is appropriate for solving the problem presented in this paper. Now that we have established the validity of the Adomian decomposition method, we proceed to capture the effect of the various thermo-physical parameters on the solutions of the momentum and energy equations.

5 OUTPUTS AND ANALYSIS

The analytical solutions (19) – (20) for the dimensionless velocity and temperature distributions, for various values of the thermo-physical parameters are plotted against the radius of the pipe. The velocity graphs for the different thermo-physical parameters are represented by Figs. 2 – 10 while the temperature graphs are represented by Figs. 11 – 19. In these figures, the variations of the thermo-physical parameters are taken into account.

1

) ( max ADM

 max(P) Difference

1

) ( max ADM

 max(P) Difference

max(ADM) max(P) Difference

Fig. 2.Velocity Graphs for Different Values of the Dimensionless Constant from Vogel’s Viscosity Model

A

with

1

0    

   

H J

T C

Fig. 3.Velocity Graphs for Different Values of the DimensionlessConstant from Vogel’s Viscosity Model B with

1 0  

   

H JT C

Fig. 4.Velocity Graphs for Different Values of the Pressure Gradient Parameter

C

with

1 0  

   

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22 IJSTR©2018

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Fig. 5.Velocity Graphs for Different Values of the Initial

TemperatureT0with

H

J

A

B

C

1

Fig. 6. Velocity Graphs for Different Values of the Non-Newtonian Parameter

with

H

J

A

B

T

0

C

1

Fig. 7. Velocity Graphs for Different Values of the Viscous Dissipation Parameter

withHJ ABT0 C1

Fig. 8. Velocity Graphs for Different Values of the Heat Generation Parameterwith HJABT0C1

Fig. 9. Velocity Graphs for Different Values of the Magnetic Effect Parameter H with 

J ABT0C1

Fig. 10. Velocity Graphs for Different Values of the Joule Heating Parameter J with H

ABT0C 1

Fig. 11. Temperature Graphs for Different Values of the Dimensionless Constant from Vogel’s Viscosity Model

A

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23 IJSTR©2018

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Fig. 12.Temperature Graphs for Different Values of the Dimensionless Constant from Vogel’s Viscosity Model B with

1 0 

   

H J

T C

Fig. 13. Temperature Graphs for Different Values of the Pressure Gradient Parameter Cwith HJ T0AB1

Fig. 14. Temperature Graphs for Different Values of the Initial Temperature

T

0 with HJ ABC1

Fig. 15. Temperature Graphs for Different Values of the

Non-Newtonian Parameter with 1

0 

     

H JA B T C

Fig. 16. Temperature Graphs for Different Values of the Viscous Dissipation Parameter with 1

0  

    

H JA B T C

Fig. 17. Temperature Graphs for Different Values of the Heat Generation Parameter

with HJABT0C1

Fig. 18. Temperature Graphs for Different Values of the Magnetic

Effect Parameter H with 1

0 

      

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24 IJSTR©2018

www.ijstr.org Figures 2 and 11 are the velocity and temperature profiles for various values of the dimensionless constant from Vogel’s viscosity model A, when the values of the other thermo-physical parameters are equal to one (1), respectively. In Figures 2 and 11 the maximum velocity occurs at the point

0

r

which is the middle of the pipe. As the values of A increases the velocity and temperature of the fluid reduces. Figures 3 and 12 reveal the effect of the dimensionless constant from Vogel’s viscosity model B on the velocity and temperature profiles respectively. As the values of B increases there is a corresponding increase in both the velocity and temperature of the fluid. The behaviour of the velocity and temperature of the fluid as the pressure gradient parameter Cis varied is captured in Figures 4 and 13 respectively. As the

value of C drops from 0.5 to 1 there is a steady increase in both the velocity and temperature. Figure 5 and 14 presents the effect of the Initial Temperature

T

0 on the velocity and temperature profiles respectively. Increase in the Initial Temperature T0 leads to a reduction in both the velocity and temperature of the fluid as can be seen. Influence of the non-Newtonian material parameter of the fluid  on the velocity and temperature profiles is shown in Figures 6 and 15 respectively. In Figure 6, it is observed that as the value of  increases the maximum velocity at the middle of the pipe decreases. Increase in the value of  results in an increase in the maximum temperature of the fluid at the middle of the pipe, as can be seen in Figure 15. The case when 0 corresponds to a Newtonian fluid. The velocity and temperature distribution for various values of the viscous dissipation parameter  is presented in Figures 7 and 16 respectively. Increase in values of  tends to increase the velocity as seen in Figure 7. Also, in Figure 16 increase in the value of  appears to increase the temperature of the fluid due to the irreversible conversion of mechanical energy to thermal energy. This holds true for this study as well as for the study by Jayeoba and Okoya (2012) and previous ones. The effect of the heat generation parameter

on the velocity and temperature is shown in Figures 8 and 17 respectively. These figures indicate that as the value of

increases the velocity and temperature of the fluid also increases. The influence of various values of the magnetic effect parameter H on the dimensionless velocity and temperature is depicted by Figures 9 and 18 respectively. In Figure 9 increment in the value of

H

brings about a steady increase in the velocity of the fluid. While in Figure 12 it is evident that increase in the value of the magnetic effect parameter only brings about a gradual increase the temperature of the fluid. Figures 10 and 19 portray the effect of the joule heating parameter

J

on the velocity and temperature of the fluid respectively. As the value of

J

increases the velocity increases as well as the temperature of the fluid. When

J

is relatively large the fluid finally exceeds the least temperature distribution.

6 CONCLUSION

In this paper we extended the model equations of Olajuwon (2009) by incorporating a magnetic effect term in the momentum equation and a joule heating term in the energy equation. This extension of ours gave rise to a magnetohydrodynamic flow problem of a third grade fluid through a cylindrical pipe. We converted the dimensional momentum and energy equations to dimensionless equations and used the Adomian decomposition method for the Vogel’s viscosity model to develop a recurrence algorithm. A three point approximate analytical solution to the velocity and temperature was obtained using the computer software Mapple (13). The results for various values of the thermo-physical parameters were presented in graphs, from which we make the following conclusions: Increase in dimensionless constant from Vogel’s viscosity model A brings about a decrease in both the velocity and the temperature, while increase in the dimensionless constant from Vogel’s viscosity model

B

results in an increase in both the velocity and temperature of the fluid. The more negative the value of the pressure gradient parameter becomes, the higher the velocity and temperature of the fluid. Increase in the initial temperature reduces the velocity and temperature of the fluid, this is as a result of the presence of joule heating. Increase in the non-Newtonian material parameter of the fluid decreases the velocity and increases the temperature of the fluid. Increase in the viscous dissipation parameter increases both the velocity and temperature of the fluid. The heat generation parameter increases the velocity and temperature of the fluid. The magnetic effect parameter increases the velocity of the fluid as well as its temperature. Increases in the joule heating parameter results in the increase in both the velocity and temperature of the fluid.

7 DEFINITION OF PARAMETERS

r

Dimensional perpendicular dist.

from pipe axis

R r

r Dimensionless perpendicular

distance from pipe axis

R

Radius of the pipe

0

T

The initial temperature

 0

T a

A Dimensionless Vogel’s model viscosity constant from

0 0

T

T

b

B

Dimensionless constant from Vogel’s model viscosity

)

(

R

0

Dimensionless velocity component in the axis 0

Dimensional reference velocity

z

Axis of the cylinder

z

p

R

C

0 0

2

Pressure gradient parameter

K

Constant thermal conductivity

r

p

Pressure gradient along the normal

to the pipe axis

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25 IJSTR©2018

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z

p

Pressure gradient in the axial

direction

p

Pressure gradient in rotational direction

Q

Heat generation constant

0

C

Initial concentration of the reactant species

Greek symbols

3 2 1

,

,

Constant material

coefficients

E T R 0

 Activation energy

0

T M

 Reynold’s Viscosity

Variational Parameter

Dynamic shear viscosity

e

0

 

,

)

exp(

0 0

0

0

T

e

Dimensionless viscosity

Rotational direction

2 0

0

T

R

E

T

T

Dimensionless

temperature excess

0 2 0 0

4

T

e



Viscous heating

parameter

2 0 0

2 0 3

r

Non-Newtonian material

parameter of the fluid

2 0

0 2 0

T

KR

C

R

EA

Q

Heat generation

parameter

0 2 0 2

R

H  Magnetic Parameter Effect

2 0

2 0 2 0 2

T

KR

R

E

J



Joule Heating Parameter

REFERENCES

[1] G. A. Adomian, ―A Review of the Decomposition Method and some Results for Non-linear Equation,‖ Mathematics and Computer Modelling, vol. 13, no. 7, pp. 17-43, 1992.

[2] G. A. Adomian, Solving Frontier Problems of Physics: The Decomposition Method, Volume 60. Dordrecht, Kluwer Academic Publishers. 370pp.

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Figure

Fig.1  Representation of fluid flow in a cylindrical pipe.
TABLE 6: DIFFERENCE BETWEEN THE VALUE OF ()max ADM AND
Fig. 10. Velocity Graphs for Different Values of the Joule Heating Parameter J  with HABT10C
Fig. 13. Temperature Graphs for Different Values of the Pressure Gradient Parameter C with HJT10AB
+2

References

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