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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 207
NUMERICAL SIMULATION ON LAMINAR CONVECTION FLOW
AND HEAT TRANSFER OVER AN ISOTHERMAL VERTICAL PLATE
EMBEDDED IN A SATURATED POROUS MEDIUM
Asish Mitra
Associate Prof. and HOD, Basic Science and Humanities Department, College of Engineering & Management,
Kolaghat. East Midnapur, India
mitra_asish@yahoo.com
Abstract
A numerical algorithm is presented for studying laminar convection flow and heat transfer over an isothermal vertical horizontal
plate embedded in a saturated porous medium. By means of similarity transformation, the original nonlinear partial differential
equations of flow are transformed to a pair of nonlinear ordinary differential equations. Subsequently they are reduced to a first
order system and integrated using Newton Raphson and adaptive Runge-Kutta methods. The computer codes are developed for
this numerical analysis in Matlab environment. Velocity and temperature profiles are illustrated graphically. Heat transfer
parameters are derived.
Keywords: Free Convection, Heat Transfer, Isothermal Vertical Plate, Matlab, Numerical Simulation, Porous
Medium.
---------------------------------------------------------------***---------------------------------------------------------------
List of Symbolsa1, a2 initial values eq (21)
f function defined in eq (13)
g gravitational acceleration, 9.81 m/s2
K permeability of the fluid, dimensionless
Nux Nusselt number at x, dimensionless
qw heat flux of the plate, W/m2
Ra Rayleigh number, dimensionless
T temperature, K
Tw surface temperature, K
T∞ free streams temperature, K
u velocity component in x, m/s
v velocity component in y, m/s
x coordinate from the leading edge, m
y coordinate normal to plate, m
z1, z2, z3, z4 variables, eq (18)
Greek Symbols
θ function defined in eq (12), dimensionless
β coefficient of thermal expansion, 1/K
δ boundary layer thickness, m
αa apparent thermal diffusivity, m2
/s
μf dynamic viscosity, N.s/m2
νf kinematic viscosity, m2
/s
η similarity variables, eq (14)
ψ stream function, m2
/s
ρf density, kg/m3
1. INTRODUCTION
There have been a number of studies on natural convection
over an isothermal vertical plate in a porous medium due to
its relevance to a variety of industrial applications and
naturally occurring processes, such as heat insulation by
fibrous materials, spreading of pollutants and convection
in the earth’s mantle, storage of agricultural products such
as fruits, vegetables and grains, ground water hydrology,
disposal of wastes, petroleum reservoir engineering,
mineral extraction and oil recovery system, recovery of
water for drinking and irrigation, salt water
encroachment into fresh water reservoirs, in biophysics-
life processes such as flow in the lungs and kidneys etc.
The earliest analytical investigation in this regard was a
similarity analysis of the boundary layer equations by P.
Cheng and W. J. Minkowycz, J. [1]. The problem is also
discussed by several authors [2-5]. The problem was
discussed in several text books [6-10].
In the present numerical investigation, a simple accurate
numerical simulation of laminar free-convection flow and
heat transfer over an isothermal horizontal plate is
developed.
The paper is organized as follows: Mathematical model of
the problem, its solution procedure, development of code in
Matlab, interpretation of the results, comparison with
Previous work.
2. MATHEMATICAL MODEL
We consider the natural convection about an isothermal
vertical impermeable flat plate immersed in a saturated
porous medium with constant permeability K. We
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 208
assume the natural convection flow to be steady, laminar,
two-dimensional, having no dissipation, and the flow
through the porous medium is governed by Darcy’s law,
with constant properties, including density, with one
exception: the density difference
   is to be
considered since it is this density difference between the
inside and the outside of the boundary layer that gives rise to
buoyancy force and sustains flow, known in the literature as
Boussinesq approximation. We take the direction along the
plate to be x, and the direction normal to surface to be y, as
shown in Fig 1.
Fig. 1 Physical Model and its coordinate system
The equations governing the flow are




u
x
v
y
  0
1
u
gK T Tf
f

  

( )
2
u
T
x
v
T
y
T
y
a







 
2
2
3
The boundary conditions on the solution are:
At y=0: v=0, T=Tw
For large y: u→0, T→T∞ 4
The continuity equation (1) is automatically satisfied
through introduction of the stream function:
u
y
v
x
  



 5
Eqs (2) and (3) can be written in terms of stream function:


 
y
gK T Tf
f

 ( )
6










y
T
x x
T
y
T
y
a 
2
2
7
From (6), we can write


 



2
2
T
y
gK T
y
f
f

8
From scale analysis, it can be shown that

x
o Ra 
( ).0 5
9
And
  o Raa( ).0 5
10
Where
Ra
gK T T gK T T xf w
a f
w
a f



 
 
 

 
( ) ( )
11
is Darcy-modified Rayleigh number.
We expect that in the boundary layer, the stream function
and temperature profiles are similar:
T T
T T
y y
x
Ra
w


  



  ( ) ( ) ( ).0 5
12
and



a Ra
f0 5.
( )
13
where η is the similarity solution given by
 
y
x
Ra0 5.
14
With the help of eqs (12) and (13), eqs (8) and (7) can be
written as (with a prime denoting differentiation with
respect to η)
  f  15
and
  


f
2 16
Hence the velocity boundary layer problem is reduced to an
ordinary differential equation (15) and energy eq (3) is also
reduced to an ordinary differential equation (16). This
confirms the assumption that velocity and temperature
profiles are similar. The appropriate boundary conditions (4)
are now:
y = 0: v = 0, T=Tw i.e., at η = 0: f = 0, θ = 1
large y: u→0, T→T∞ i.e., η large:  f 0,  0
17
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 209
3. SOLUTION PROCEDURE
Eqs (15) and (16) are simultaneous nonlinear ordinary
differential equations for the velocity and temperature
functions, f and θ. No analytical solution is known, so
numerical integration is necessary. Values of f and θ at the
surface of the plate (y = 0), and that of f and  far away
from the surface (y → ∞) are known.
3.1 Reduction of Equations to First-order System
This is done easily by defining new variables:
z f1 
z z f2 1   
z3  
z z4 3    18
Therefore from eqs (15) and (16), we get the following set
of differential equations
  z f1
      z z f z2 1 4
 z z3 4
     

 z z
f z z
4 3
1 4
2 2


19
with the following boundary conditions:
z f1 0 0 0( ) ( ) 
z z f2 1 0( ) ( ) ( )       
z3 0 0 1( ) ( ) 
z3 0( ) ( )    20
Eqs (15) and (16) are second-order each and are replaced by
two first-order equations (21).
3.2 Solution to Initial Value Problems
To solve eqs (21), we denote the two unknown initial values
by a1 and a2, the set of initial conditions is then:
z f1 0 0 0( ) ( ) 
z z f a2 1 10 0 0( ) ( ) ( )    
z3 0 0 1( ) ( ) 
z z a4 3 20 0 0( ) ( ) ( )     21
If eqs (19) are solved with adaptive Runge-Kutta method
using the initial conditions in eq (21), the computed
boundary values at    depend on the choice of a1 and
a2 respectively. We express this dependence as
z z f f a2 1 1 1( ) ( ) ( ) ( )       
z f a3 2 2( ) ( ) ( )    22
The correct choice of a1 and a2 yields the given boundary
conditions at    ; that is, it satisfies the equations
f a1 1 0( ) 
f a2 2 0( )  23
These nonlinear equations can be solved by the Newton-
Raphson method. A value of 10 is fine for infinity, even if
we integrate further nothing will change.
3.3 Program Details
This section describes a set of Matlab routines for the
solution of eqs (19) along with the initial conditions (21).
They are listed in Table 1.
Table 1. A set of Matlab routines used sequentially to solve
Equations (24).
Matlab
code
Brief Description
deqs.m Defines the differential
equations (19).
incond.m Describes initial values for
integration, a1 and a2 are guessed
values, eq (21)
runKut5.m Integrates as initial value
problem using adaptive Runge-
Kutta method.
residual.m Provides boundary residuals and
approximate solutions.
newtonraph
son.m
Provides correct values a1 and a2
using approximate solutions
from residual.m
runKut5.m Again integrates eqs (19) using
correct values of a1 and a2.
The final output of the code runKut5.m gives the tabulated
values of f , f for velocity profile, and  and  for
temperature profiles as function of η.
4. INTERPRETATION OF THE RESULTS
Physical quantities are related to the dimensionless functions
f and  through eqs (12), (13) and (14). f and  are now
known.
4.1 Computed Values of the Parameters
Some accurate initial values from this computation are listed
in Table 2. These theoretical computations are in good
agreement with results published in literatures [10].
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 210
Table 2. Computed values from eqs (15) & (1)
η f f  
0.00000 0.00000 1.00000 1.00000 -0.44390
0.10000 0.09778 0.95565 0.95565 -0.44281
0.56453 0.49467 0.75551 0.75551 -0.41263
1.06139 0.82149 0.56527 0.56527 -0.34971
1.58921 1.07474 0.40121 0.40121 -0.27178
2.17789 1.26863 0.26537 0.26537 -0.19212
2.81160 1.40304 0.16583 0.16583 -0.12561
3.44239 1.48601 0.10208 0.10208 -0.07956
4.03844 1.53462 0.06386 0.06386 -0.05070
4.65045 1.56554 0.03914 0.03914 -0.03154
5.29663 1.58523 0.02316 0.02316 -0.01895
5.99060 1.59747 0.01305 0.01305 -0.01091
6.74612 1.60476 0.00687 0.00687 -0.00596
7.57896 1.60881 0.00325 0.00325 -0.00305
8.50860 1.61079 0.00125 0.00125 -0.00144
9.56051 1.61149 0.00023 0.00023 -0.00062
10.00000 1.61154 0.00000 0.00000 -0.00043
4.2 Dimensionless Stream Function and
Temperature Profiles
Variations of f and  obtained from the present computation
are shown in Fig 2.
0 1 2 3 4 5 6 7 8 9 10
0
0.2
0.4
0.6
0.8
1
1.2
1.4
1.6
1.8

f

Fig. 2 Solutions of f and 
4.3 Comparison With Experiments
Fig 3 compares the dimensionless temperature profile θ,
with the experiments of Evans and Plumb [11]. The
agreement is excellent.
Fig 3. Comparison of the computed dimensionless
temperature profile with experimental data.
4.4 Heat Transfer Parameters
Besides the velocity and temperature distributions, it is often
desirable to compute other physically important quantities
associated with the convection flow.
The heat transfer rate at the wall is given by
q k
T
y
w
y
 


 0
24
Hence, using eq (12)
q x
k T T
Raw
a w( )
.

  

0 5
0

25
From Table 2, we see that
   0
0 4439.
Hence,
Nu Rax  0 444 0 5
. .
26
where, Nux is the local Nusselt number based on x. Fig 4
illustrates the comparison of the correlation (26) with the
experimental data of Evans and Plumb [11].
The mean heat transfer rate is then given by using
27
Fig 4. Comparison of the computed correlation with
experimental data.
Eqs (26) and (27) gives
Nu RaL L 0888
0 5
.
.
28
where NuL is the mean Nusselt number based on the length
of the plate, L and RaL is Darcy-modified Rayleigh number
based on L. These empirical correlations are found in the
text books [6-10].
5. CONCLUSION
In the present numerical simulation, laminar convection
flow and heat transfer over an isothermal vertical horizontal
plate embedded in a saturated porous medium is presented.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 211
Details of the solution procedure of the nonlinear partial
differential equations of flow are discussed. The computer
codes are developed for this numerical analysis in Matlab
environment. Velocity profile and temperature profiles are
computed using these codes. The computed and
experimental velocity and temperature distributions are in
very good agreement with results published in literatures.
Heat transfer parameters are derived. A good agreement
between the present results and the past indicates that the
developed numerical simulation as an efficient and stable
numerical scheme in natural convection.
REFERENCES
[1] P. Cheng and W. J. Minkowycz, J. Geophys. Res.
82,2040 (1977).
[2] P. Cheng, Int. J. Heat Mass Transfer 20, 201
(1977).
[3] J. H. Merkin, Int. .I. Heat Mass Transfer 21, 1499
(1978).
[4] J. H. Merkin, .I. Engng. Math. 14, 301 (1980).
[5] Mitra A., “Numerical Simulation on Laminar Free-
Convection Flow and Heat Transfer Over an Isothermal
Vertical Plate,” International Journal of Research in
Engineering & Technology, 04, 2015, pp 488-494.
[6] Hansen, A. G., “Similarity Analysis of Boundary Value
Problems in Engineering”, Prentice-Hall, Englewood
Cliffs, N. J., 1964.
[7] An Introduction to Convective Heat Transfer Analysis
by P O Oosthuizen and D Nalyor, McGraw-Hill, 1999.
[8] Sachdev, P. L., “Self-Similarity and Beyond: Exact
Solutions of Nonlinear Problems”, CRC Press, Boca
Ratton, Fla, 2000
[9] Incropera F.P. and DeWitt D.P., Introduction to Heat
Transfer, Fourth edition, John Wiley, New York, 2002.
[10]Bejan A., Convection Heat Transfer, Fourth Edition,
John Wiley & Sons, Inc. 2013.
[11]Evans, G. H. and Plumb, O. A., Natural convection
from a vertical isothermal surface imbedded in a
saturated porous medium, AIAA-ASME
Thermophysics and Heat Transfer Conf., Paper 78-HT
-55, Palo Alto, California. 1978.

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Numerical simulation on laminar convection flow and heat transfer over an isothermal vertical plate embedded in a saturated porous medium

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 207 NUMERICAL SIMULATION ON LAMINAR CONVECTION FLOW AND HEAT TRANSFER OVER AN ISOTHERMAL VERTICAL PLATE EMBEDDED IN A SATURATED POROUS MEDIUM Asish Mitra Associate Prof. and HOD, Basic Science and Humanities Department, College of Engineering & Management, Kolaghat. East Midnapur, India mitra_asish@yahoo.com Abstract A numerical algorithm is presented for studying laminar convection flow and heat transfer over an isothermal vertical horizontal plate embedded in a saturated porous medium. By means of similarity transformation, the original nonlinear partial differential equations of flow are transformed to a pair of nonlinear ordinary differential equations. Subsequently they are reduced to a first order system and integrated using Newton Raphson and adaptive Runge-Kutta methods. The computer codes are developed for this numerical analysis in Matlab environment. Velocity and temperature profiles are illustrated graphically. Heat transfer parameters are derived. Keywords: Free Convection, Heat Transfer, Isothermal Vertical Plate, Matlab, Numerical Simulation, Porous Medium. ---------------------------------------------------------------***--------------------------------------------------------------- List of Symbolsa1, a2 initial values eq (21) f function defined in eq (13) g gravitational acceleration, 9.81 m/s2 K permeability of the fluid, dimensionless Nux Nusselt number at x, dimensionless qw heat flux of the plate, W/m2 Ra Rayleigh number, dimensionless T temperature, K Tw surface temperature, K T∞ free streams temperature, K u velocity component in x, m/s v velocity component in y, m/s x coordinate from the leading edge, m y coordinate normal to plate, m z1, z2, z3, z4 variables, eq (18) Greek Symbols θ function defined in eq (12), dimensionless β coefficient of thermal expansion, 1/K δ boundary layer thickness, m αa apparent thermal diffusivity, m2 /s μf dynamic viscosity, N.s/m2 νf kinematic viscosity, m2 /s η similarity variables, eq (14) ψ stream function, m2 /s ρf density, kg/m3 1. INTRODUCTION There have been a number of studies on natural convection over an isothermal vertical plate in a porous medium due to its relevance to a variety of industrial applications and naturally occurring processes, such as heat insulation by fibrous materials, spreading of pollutants and convection in the earth’s mantle, storage of agricultural products such as fruits, vegetables and grains, ground water hydrology, disposal of wastes, petroleum reservoir engineering, mineral extraction and oil recovery system, recovery of water for drinking and irrigation, salt water encroachment into fresh water reservoirs, in biophysics- life processes such as flow in the lungs and kidneys etc. The earliest analytical investigation in this regard was a similarity analysis of the boundary layer equations by P. Cheng and W. J. Minkowycz, J. [1]. The problem is also discussed by several authors [2-5]. The problem was discussed in several text books [6-10]. In the present numerical investigation, a simple accurate numerical simulation of laminar free-convection flow and heat transfer over an isothermal horizontal plate is developed. The paper is organized as follows: Mathematical model of the problem, its solution procedure, development of code in Matlab, interpretation of the results, comparison with Previous work. 2. MATHEMATICAL MODEL We consider the natural convection about an isothermal vertical impermeable flat plate immersed in a saturated porous medium with constant permeability K. We
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 208 assume the natural convection flow to be steady, laminar, two-dimensional, having no dissipation, and the flow through the porous medium is governed by Darcy’s law, with constant properties, including density, with one exception: the density difference    is to be considered since it is this density difference between the inside and the outside of the boundary layer that gives rise to buoyancy force and sustains flow, known in the literature as Boussinesq approximation. We take the direction along the plate to be x, and the direction normal to surface to be y, as shown in Fig 1. Fig. 1 Physical Model and its coordinate system The equations governing the flow are     u x v y   0 1 u gK T Tf f      ( ) 2 u T x v T y T y a          2 2 3 The boundary conditions on the solution are: At y=0: v=0, T=Tw For large y: u→0, T→T∞ 4 The continuity equation (1) is automatically satisfied through introduction of the stream function: u y v x        5 Eqs (2) and (3) can be written in terms of stream function:     y gK T Tf f   ( ) 6           y T x x T y T y a  2 2 7 From (6), we can write        2 2 T y gK T y f f  8 From scale analysis, it can be shown that  x o Ra  ( ).0 5 9 And   o Raa( ).0 5 10 Where Ra gK T T gK T T xf w a f w a f             ( ) ( ) 11 is Darcy-modified Rayleigh number. We expect that in the boundary layer, the stream function and temperature profiles are similar: T T T T y y x Ra w           ( ) ( ) ( ).0 5 12 and    a Ra f0 5. ( ) 13 where η is the similarity solution given by   y x Ra0 5. 14 With the help of eqs (12) and (13), eqs (8) and (7) can be written as (with a prime denoting differentiation with respect to η)   f  15 and      f 2 16 Hence the velocity boundary layer problem is reduced to an ordinary differential equation (15) and energy eq (3) is also reduced to an ordinary differential equation (16). This confirms the assumption that velocity and temperature profiles are similar. The appropriate boundary conditions (4) are now: y = 0: v = 0, T=Tw i.e., at η = 0: f = 0, θ = 1 large y: u→0, T→T∞ i.e., η large:  f 0,  0 17
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 209 3. SOLUTION PROCEDURE Eqs (15) and (16) are simultaneous nonlinear ordinary differential equations for the velocity and temperature functions, f and θ. No analytical solution is known, so numerical integration is necessary. Values of f and θ at the surface of the plate (y = 0), and that of f and  far away from the surface (y → ∞) are known. 3.1 Reduction of Equations to First-order System This is done easily by defining new variables: z f1  z z f2 1    z3   z z4 3    18 Therefore from eqs (15) and (16), we get the following set of differential equations   z f1       z z f z2 1 4  z z3 4         z z f z z 4 3 1 4 2 2   19 with the following boundary conditions: z f1 0 0 0( ) ( )  z z f2 1 0( ) ( ) ( )        z3 0 0 1( ) ( )  z3 0( ) ( )    20 Eqs (15) and (16) are second-order each and are replaced by two first-order equations (21). 3.2 Solution to Initial Value Problems To solve eqs (21), we denote the two unknown initial values by a1 and a2, the set of initial conditions is then: z f1 0 0 0( ) ( )  z z f a2 1 10 0 0( ) ( ) ( )     z3 0 0 1( ) ( )  z z a4 3 20 0 0( ) ( ) ( )     21 If eqs (19) are solved with adaptive Runge-Kutta method using the initial conditions in eq (21), the computed boundary values at    depend on the choice of a1 and a2 respectively. We express this dependence as z z f f a2 1 1 1( ) ( ) ( ) ( )        z f a3 2 2( ) ( ) ( )    22 The correct choice of a1 and a2 yields the given boundary conditions at    ; that is, it satisfies the equations f a1 1 0( )  f a2 2 0( )  23 These nonlinear equations can be solved by the Newton- Raphson method. A value of 10 is fine for infinity, even if we integrate further nothing will change. 3.3 Program Details This section describes a set of Matlab routines for the solution of eqs (19) along with the initial conditions (21). They are listed in Table 1. Table 1. A set of Matlab routines used sequentially to solve Equations (24). Matlab code Brief Description deqs.m Defines the differential equations (19). incond.m Describes initial values for integration, a1 and a2 are guessed values, eq (21) runKut5.m Integrates as initial value problem using adaptive Runge- Kutta method. residual.m Provides boundary residuals and approximate solutions. newtonraph son.m Provides correct values a1 and a2 using approximate solutions from residual.m runKut5.m Again integrates eqs (19) using correct values of a1 and a2. The final output of the code runKut5.m gives the tabulated values of f , f for velocity profile, and  and  for temperature profiles as function of η. 4. INTERPRETATION OF THE RESULTS Physical quantities are related to the dimensionless functions f and  through eqs (12), (13) and (14). f and  are now known. 4.1 Computed Values of the Parameters Some accurate initial values from this computation are listed in Table 2. These theoretical computations are in good agreement with results published in literatures [10].
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 210 Table 2. Computed values from eqs (15) & (1) η f f   0.00000 0.00000 1.00000 1.00000 -0.44390 0.10000 0.09778 0.95565 0.95565 -0.44281 0.56453 0.49467 0.75551 0.75551 -0.41263 1.06139 0.82149 0.56527 0.56527 -0.34971 1.58921 1.07474 0.40121 0.40121 -0.27178 2.17789 1.26863 0.26537 0.26537 -0.19212 2.81160 1.40304 0.16583 0.16583 -0.12561 3.44239 1.48601 0.10208 0.10208 -0.07956 4.03844 1.53462 0.06386 0.06386 -0.05070 4.65045 1.56554 0.03914 0.03914 -0.03154 5.29663 1.58523 0.02316 0.02316 -0.01895 5.99060 1.59747 0.01305 0.01305 -0.01091 6.74612 1.60476 0.00687 0.00687 -0.00596 7.57896 1.60881 0.00325 0.00325 -0.00305 8.50860 1.61079 0.00125 0.00125 -0.00144 9.56051 1.61149 0.00023 0.00023 -0.00062 10.00000 1.61154 0.00000 0.00000 -0.00043 4.2 Dimensionless Stream Function and Temperature Profiles Variations of f and  obtained from the present computation are shown in Fig 2. 0 1 2 3 4 5 6 7 8 9 10 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8  f  Fig. 2 Solutions of f and  4.3 Comparison With Experiments Fig 3 compares the dimensionless temperature profile θ, with the experiments of Evans and Plumb [11]. The agreement is excellent. Fig 3. Comparison of the computed dimensionless temperature profile with experimental data. 4.4 Heat Transfer Parameters Besides the velocity and temperature distributions, it is often desirable to compute other physically important quantities associated with the convection flow. The heat transfer rate at the wall is given by q k T y w y      0 24 Hence, using eq (12) q x k T T Raw a w( ) .      0 5 0  25 From Table 2, we see that    0 0 4439. Hence, Nu Rax  0 444 0 5 . . 26 where, Nux is the local Nusselt number based on x. Fig 4 illustrates the comparison of the correlation (26) with the experimental data of Evans and Plumb [11]. The mean heat transfer rate is then given by using 27 Fig 4. Comparison of the computed correlation with experimental data. Eqs (26) and (27) gives Nu RaL L 0888 0 5 . . 28 where NuL is the mean Nusselt number based on the length of the plate, L and RaL is Darcy-modified Rayleigh number based on L. These empirical correlations are found in the text books [6-10]. 5. CONCLUSION In the present numerical simulation, laminar convection flow and heat transfer over an isothermal vertical horizontal plate embedded in a saturated porous medium is presented.
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 10 | OCT-2015, Available @ http://www.ijret.org 211 Details of the solution procedure of the nonlinear partial differential equations of flow are discussed. The computer codes are developed for this numerical analysis in Matlab environment. Velocity profile and temperature profiles are computed using these codes. The computed and experimental velocity and temperature distributions are in very good agreement with results published in literatures. Heat transfer parameters are derived. A good agreement between the present results and the past indicates that the developed numerical simulation as an efficient and stable numerical scheme in natural convection. REFERENCES [1] P. Cheng and W. J. Minkowycz, J. Geophys. Res. 82,2040 (1977). [2] P. Cheng, Int. J. Heat Mass Transfer 20, 201 (1977). [3] J. H. Merkin, Int. .I. Heat Mass Transfer 21, 1499 (1978). [4] J. H. Merkin, .I. Engng. Math. 14, 301 (1980). [5] Mitra A., “Numerical Simulation on Laminar Free- Convection Flow and Heat Transfer Over an Isothermal Vertical Plate,” International Journal of Research in Engineering & Technology, 04, 2015, pp 488-494. [6] Hansen, A. G., “Similarity Analysis of Boundary Value Problems in Engineering”, Prentice-Hall, Englewood Cliffs, N. J., 1964. [7] An Introduction to Convective Heat Transfer Analysis by P O Oosthuizen and D Nalyor, McGraw-Hill, 1999. [8] Sachdev, P. L., “Self-Similarity and Beyond: Exact Solutions of Nonlinear Problems”, CRC Press, Boca Ratton, Fla, 2000 [9] Incropera F.P. and DeWitt D.P., Introduction to Heat Transfer, Fourth edition, John Wiley, New York, 2002. [10]Bejan A., Convection Heat Transfer, Fourth Edition, John Wiley & Sons, Inc. 2013. [11]Evans, G. H. and Plumb, O. A., Natural convection from a vertical isothermal surface imbedded in a saturated porous medium, AIAA-ASME Thermophysics and Heat Transfer Conf., Paper 78-HT -55, Palo Alto, California. 1978.