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An integral treatment for heat and mass transfer along a vertical wall by natural convection in a porous media

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Selçuk J. Appl. Math. Selçuk Journal of Vol. 7. No.2. pp. 125-133, 2006 Applied Mathematics

An Integral Treatment For Heat And Mass Transfer Along A Vertical Wall By Natural Convectıon In A Porous Media

B. B. Singh

Department of Mathematics, Dr. Babasaheb Ambedkar Technological University, Lonere-402103, Dist. Raigad (M.S.), India

e-mail:brijbhansingh@ yaho o.com

Summary.This paper deals with the free convective heat and mass transfer along a vertical wall embedded in a fluid saturated porous medium by using integral method . The governing parameters for the problem are the buoyancy ratio N and Lewis Number Le. The results for the local Nusselt and Sherwood numbers are presented for wide range of parameters. The thermal and concen-tration boundary layer thicknesses have also been calculated for the flow field. It has been observed that the results obtained by integral method are in good agreement with those obtained by Bejan and Khair

Key words: Natural convection; Porous media; Heat transfer; Mass transfer.

1. Introduction

The natural convection flows arising out of the combined buoyancies due to ther-mal and mass diffusion in a porous medium are of importance because of the fundamental nature of the problem and broad range of their applications per-taining to manufacturing and process industries such as geothermal systems, fi-bre and grannular insulation, storage of nuclear waste materials, usage of porous conical bearings in lubrication technology, chemical catalytic reactors, disper-sion of chemical contaminant through water saturated soil , natural gas storage tanks , etc.

On account of the afore-mentioned applications , Bejan and Khair [1] used the Darcy’s law to study the features of the free convection boundary layer flow driven by temperature and concentration gradients. Recently, Lai and Kulacki [2] have re-examined the free convection boundary layer along a vertical wall with constant heat and mass flux including the effect of wall injection. The heat and mass transfer by natural convection near a vertical wall in a porous

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medium under boundary layer approximations has been studied by Nakayama and Hossain [3] and Singh and Queeny [4]. A further review of coupled heat and mass transfer by natural convection in porous medium is given by Nield and Bejan [5]

The objective of the present paper is to apply integral method to analyze free convection problem along a vertical wall in the presence of temperature and con-centration gradients . A comparison of the numerical values of the local Nusselt and local Sherwood numbers obtained by the integral method has been done with those obtained by Bejan and Khair [1]for different values of the buoyancy ratio

It has been found that the results obtained by the present method are in good agreement with those obtained by Bejan and Khair.

2. Mathematical Analysis

We consider a two-dimentional laminar flow over a vertical flat plate in a porous medium embedded in a Darcian fluid. The co-ordinate system and the physical model are shown in figure 1. In the mathematical formulation of the problem, we note the following conventional assumptions:

The physical properties are considered to be constant, except for the density term that is associated with the body force.

Flow is sufficiently slow so that the convecting fluid and the porous matrix are in local thermodynamic equilibrium.

Darcy’s law, the Boussinesq and boundary layer approximations have been em-ployed.

With these assumptions, the governing equations are given by

(1)  +   = 0 (2)  =   (( − ∞+ ( − ∞) (3)   +    =  2 2 (4)  +  =  2

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The symbols have got their meanings as mentioned in the Nomenclature . The boundary conditions at the wall are

(5)  = 0 :  = 0  =   = 

and at infinity are

(6)  → ∞;  = 0  →   → 

3. Integral Method

The boundary layer equations (2)-(4) along with boundary conditions (5) and (6) have been solved by using integral method. The partial differential equa-tions get converted into the ordinary differential equaequa-tions by making use of the following transformations: (7)  =  () 12 (8)  = ()12 () (9)  =  −   − ∞ (10)  =  −  − ∞

where  = (−∞ ) is the modified local Rayleigh number ,  is the

stream function .

After transformation the resulting equations become

(11) ¨() − 0() − 0() = 0

(12) 00() +1

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(13) ¨() + (2) () 0() = 0 with boundary conditions

(14)  (0) = 0 (0) = (0) = 1

(15)  0(∞) = (∞) = (∞) = 0

where primes denote the differentiation with respect to ‘’,  ∈ [ 0, ∞ ). Here, f’() is non-dimensional velocity related to the stream function (x,y). In the above equations (11) — (13) , N is the buoyancy ratio defined by

(16)  = (− ∞)

(− ∞)

and Le is Lewis number defined by

(17)  = 

From (12) and (13) , we get

(18) −0(0) = 1 2 ∞ Z 0 0 (19) −0(0) =  2 ∞ Z 0 0

The infinity is boundary layer thickness for temperature and concentration. We now assume the exponential temperature and concentration profiles as follows:

(20) () = (−)

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Here  is arbitrary scale for the thermal boundary layer thickness whereas 

is its ratio to the concentration boundary thickness . With the help of above

profiles, and using equation (11), the equations (10) and (11) can be obtained in two distinct expressions as

(22) 1 2 = + 1 + 2 4( + 1) (23) 1 2 = ½ 2 +  ( + 1) 42( + 1)  ¾

The above two equations (12) and (13) can be combined together to give the following cubic equation for determining the boundary layer thickness ratio  as

(24) 3 + (1 + 2 )2− [(2 + )] −  = 0

As  is determined by using the computer programming like MATLAB from the equation (24), the local Nusselt and Sherwood numbers which are of our main interest in terms of heat and mass transfer respectively, are given as

(25)   ()12 = 05 µ  + 1 + 2  + 1 ¶12 and (26)  ()12 = 05 µ  + 1 + 2  + 1 ¶12

The accuracy acquired in the above approximations may be examined by com-paring the heat and mass transfer results against those obtained by Bejan and Khair [1] . It is not unusual to have an error of 5 % or more , depending on the assumed profile . However, the situation can be remedied by adjusting the multiplicative constant, namely, replacing 0.5 by 0.444. Thus, the following approximate formulae are proposed :

(27)   ()12 = 0444 µ  + 1 + 2  + 1 ¶12 (28)  ()12 = 05 µ  + 1 + 2  + 1 ¶12

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The formulae (16) and (17) give the values of the local Nusselt number (Nu) and Sherwood number (Sh) as 0.444 for N = 0 and Le = 1 .These values are the same as obtained by Bejan and Khair [1]. The above assertion is clear from table 1. We have done calculations for a wide range of the parameters N (buoyancy ratio) and Le (Lewis number) in order to understand their influence on the combined heat and mass transfer along a vertical wall due to free convection . These values have been given in table 1. From the table, it is evident that the values of local Nu and Sh obtained by the integral method for different values of Le are in excellent agreement with those obtained by Bejan and Khair who obtained the corresponding values by the similarity solution technique.

From the table, it is clear that the thermal boundary layer thickness  shows

an increasing trend for N = 1 , 4 for the increasing values of the Lewis number Le. On the contrary, the concentration boundary layer thickness  shows a

decreasing trend for N = 0 , 1 , 4 for the increasing values of Le. From the table, it is obvious that the Lewis number has more pronounced effect on the concentration field than it has on temperature field. From the table, it is further evident that the magnitudes of the thermal boundary layer and concentration boundary layer thicknesses are equal for N = 0 ,

Le = 1 ; N = 1 , Le = 1 and N = 4, Le =1.

The local Nusselt number has been plotted in fig. 2 as a function of buoyancy ratio for various values of Lewis number ( Le = 0.1 , 1 , 10 , 100 ). It is found that the rate of heat transfer decreases with increasing Lewis number for N  0 . Similarly the local Sherwood number has been plotted in fig. 3 against the buoyancy ratio N for various values of the Lewis number ( Le = 1 , 10 , 50 , 100 ). It is found that the rate of mass transfer increases with increasing Lewis number for all N.

The local Nusselt number has been plotted in fig. 4 as a function of Lewis number for various values of buoyancy ratio N = 0, 2 and 4. It is found that the local Nusselt number decreases with increasing Lewis number for N  0 . Similarly the local Sherwood number is plotted in fig. 5 as a function of Lewis number for various values of buoyancy ratio N = 0, 1 and 4 . It is found that the local Sherwood number increases with increasing Lewis number for all N . From figures 4and 5, also it is evident that the values of local Nusselt and local Sherwood numbers in the present case are in excellent agreement with those obtained by Bejan and Khair.

5. Concluding Remarks

This paper deals with the free convective heat and mass transfer along a vertical wall embedded in a fluid saturated porous medium. The heat and mass transfer coefficients obtained in the present study by the integral method agree very well with those obtained by Bejan and Khair. In the present analysis , the

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results have been presented in such a way that any practicing engineer can easily obtain the physical characteristic of the problem for arbitrary values of the buoyancy ratio and Lewis number. The advantage of this method is that it also provides with great freedom the approximate solutions to non-linear problems. The further advantage of this method is that the results are obtained with more ease as compared to Bejan and Khair.

Nomenclature N buoyancy ratio T temperature C concentration

D mass diffusivity of porous medium f dimensionless stream function g gravitational acceleration h local heat transfer coefficient k thermal conductivity

K permeability Le Lewis number Nu local Nusselt number Sh local Sherwood number Ra modified Rayleigh number

u Darcy’s velocity in x- direction v Darcy’s velocity in y- direction x, y cartesian co-ordinate Greek Symbols

 thermal diffusivity of porous medium  similarity variable

 coefficient of thermal expansion

 coefficient of concentration expansion

 arbitrary length scale for thermal boundary

layer

 arbitrary length scale for concentration

boundary layer  stream function

 dimensionless concentration  boundary layer thickness ratio  kinematic viscosity

Subscripts

∞ condition at the infinity w condition at the wall

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1.A. Bejan and K.R.Khair, Heat and mass transfer by natural convection in a porous medium Int. J. Heat Mass Transfer 28, 909-918 (1985).

2. F.C. Lai and Kulacki, Coupled Heat and Mass Transfer by Natural Convection from Vertical Surface in Porous Media, Int. J. Heat Mass Transfer, 34, 1189-1194 (1991). 3. A. Nakayama and M.A.Hossain, An Integral Treatment for Combined Heat and Mass Transfer by Natural Convection in a Porous Media, Int. J. Heat Mass Transfer 38, 761-765 (1995)

4. P. Singh and Queeny, Free convection Heat and Mass Transfer along a Vertical Surface in a Porous Media; Acta Mechanica 123, 69-73 (1997).

5.D. A. Nield and A. Bejan, Convection in Porous Media, second edition, Springer-Verlag, New York (1999).

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Fig. 2 Heat transfer coefficient as a function of buoyancy ratio 0 0,2 0,4 0,6 0,8 1 1,2 0 1 2 3 4 5 N Nu /R ax 1/ 2 Le 0.1 1 10 100

Fig. 3 Mass transfer coefficient as a function of buoyancy ratio 0 2 4 6 8 10 12 0 2 4 6 N Sh/ R ax 1/ 2 Le 100 50 10 1

Fig.4 Heat transfer results 0 0,2 0,4 0,6 0,8 1 1,2 0 20 40 60 80 100 120 Le Nu/R ax 1/ 2 N=0 (Present) N=0 (Numerical) N=2 (Present) N=2 (Numerical) N=4 (Present) N=4(Numerical) N=4 N=2 N=0

Fig. 5 Mass transfer results 0 0,5 1 1,5 2 2,5 3 3,5 4 0 3 6 9 12 Le Sh /Ra x 1/2 N=0 (Present) N=0 (Numerical) N=1(Present) N=1 (Numerical) N=4 (Present) N=4 (Numerical) N=4 N=1 N=0

Şekil

Table 1: Comparison of Local Nusselt and Sherwood numbers
Fig. 3  Mass transfer coefficient as a  function of buoyancy ratio 024681012024 6NSh/Rax1/2Le10050101

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