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International Journal of Applied Engineering Research ISSN 0973-4562 Volume 13, Number 22 (2018) pp. 15611-
© Research India Publications. http://www.ripublication.com
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Effect of Variable Properties on Heat and Mass Transfer Flow of Nanofluid
over a Vertical Cone Saturated by Porous Medium under Enhanced
Boundary Conditions
B. Kalavathamma 1* and C. Venkata Lakshmi 2
1, 2Department of Mathematics, Sri Padmavati Mahila Visvavidyalayam (Women’s University) Tirupati,
Andhra Pradesh-517502, India
*Corresponding Author
ABSTRACT
We have investigated the impact of variable viscosity and
thermal conductivity on MHD boundary layer flow, heat and
mass transfer of nanofluid over a vertical cone saturated by
porous medium with thermal radiation and chemical reaction.
Further, the viscosity and thermal conductivity are considered
as the function of nanoparticle volume fraction (𝜙). By using
suitable similarity variables the governing equations
represents the velocity, temperature and volume fraction of
nanoparticles are transformed into the set of ordinary
differential equations. These equations together with
associated boundary conditions are solved numerically by
using an optimized, extensively validated, variational Finite
element method. Effects of different parameters such as
variable viscosity, Buoyancy, magnetic, radiation, variable
thermal conductivity, thermophoresis, Brownian motion,
Lewis number and chemical reaction parameters on velocity,
temperature and concentration profiles are examined and the
results are presented in graphical from. Furthermore, the skin-
friction coefficient, Nusselt number and Sherwood number are
also investigated and are shown in tabular form.
Keywords: Nanofluid, Vertical cone, Variable viscosity,
Variable thermal conductivity, Chemical reaction, Thermal
radiation.
NOMENCLATURE
km Thermal conductivity Nux Nusselt number
𝜙 Nanoparticle volume fraction 𝜙w Nanoparticle volume fraction on the plate
𝜙∞ Ambient nanoparticle volume fraction (x, y) Cartesian coordinates
Tw Temperature at the plate T∞ Ambient temperature attained
T Temperature on the plate 𝑅𝑎𝑥 Rayleigh number
𝑞𝑤 Wall heat flux 𝐽𝑤 Wall mass flux
DB Brownian diffusion DT Thermophoretic diffusion coefficient
𝛽0 Strength of magnetic field g Gravitational acceleration vector
Nt Thermophoresis parameter Le Lewis number
P Pressure Nb Brownian motion parameter
𝑞𝑟 Thermal radiation M Magnetic parameter
𝑆ℎ𝑥 Local Sherwood number Nv Variable viscosity parameter
𝐾𝑟 Rate of chemical Reaction
Nc Variable thermal conductivity parameter Cr Chemical reaction parameter
Nr Buoyancy ratio K Permeability of the porous medium
Greek symbols:
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μ viscosity ε porosity
γ proportionality constant 𝛼𝑚 Thermal diffusivity .
𝜌𝑓 Fluid density 𝜌𝑝 Nanoparticle mass density
ψ Stream function V Kinematic viscosity of the fluid
τ Parameter defined by ε (𝜌𝑐)𝑝
(𝜌𝑐)𝑓 (ρc)f Heat capacity of the fluid
∅ (η) Dimensionless nanoparticle volume fraction η Similarity variable
θ (η) Dimensionless temperature (ρc)p Effective heat capacity of the nanoparticle
α Acute angle of the plate to the vertical β Volumetric expansion coefficient
Subscripts:
w Condition on the plate ∞ Condition far away from the plate
ɳ Similarity variable f Base fluid
1. INTRODUCTION
In recent years the field of science and technology,
nanotechnology has become more popular because of its
specific application to the arenas of electronics, fuel cells,
space, fuels, better air quality, batteries, solar cells, medicine,
cleaner water, chemical sensors and sporting goods.
Nanoparticles are the particles which are of 1-100 nm in size.
The convectional heat transfer fluids like water, oil, kerosene
and ethylene glycol have poor heat transfer capabilities due to
their low thermal conductivity. To improve the thermal
conductivity of these fluids nano/micro-sized materials are
suspended in liquids. Due to the nanofluid thermal
enhancement, performance, applications and benefits in
several important arenas, the nanofluid has contributed
significantly well in the field of microfluidics, manufacturing,
microelectronics, advanced nuclear systems, polymer
technology, transportation, medical, saving in energy.
Keeping above applications, Choi et al. [1] have reported in
his experimental study that there is 150% enhancement in
thermal conductivity when carbon nanotubes are added to the
ethylene glycol or oil. Copper nanoparticles dispersed in
ethylene glycol have higher intrinsic thermal conductivity
than the nanofluids consisting oxide particles and found that
40% increase in the thermal conductivity of nanofluids
consisting ethylene glycol with 0.3 vol % copper
nanoparticles of 10 nm diameter [2]. Buongiorno [3]
explained the thermal properties of nanofluid and noticed
Brownian diffusion and thermophoresis are main slip effects
in heat transfer process. Kuznetsov et al. [4] studied
analytically the convective flow of a nanofluid through
vertical plate using Buongiorno’s mathematical model.
Sudarsana Reddy et al.[5] have studied heat transfer process
over stretching sheet and reported that the rate of heat transfer
is rises with increasing values of nano particle volume fraction
parameter. Some captivating investigations on nanofluid flow
in permeable media can be found in [6, 7]. Chamkha et al. [8]
observed the impact of heat generation/absorption on entropy
generation of Cu-water based nanofluid flow through porous
medium with magnetic field effect and noticed that increase in
the volume fraction detracts the nusselt number and entropy
generation. Sulochana et al. [9] discussed the MHD nanofluid
flow over vertical revolving surface with Soret and radiation
effects. Sabour et al.[10] have analyzed the augmentation in
heat transfer of nanofluids in a square cavity. Thirupathi
Thumma et al. [11] investigated the heat transfer phenomena
of two types of nanofluids Cu – water and Al2O3 – water over
inclined porous plate. The results indicated that the thickness
of thermal and concentration boundary layer of Cu-water is
more as compared with Al2O3-water nanofluid. In addition to
this, the heat flow along the inclined porous plate using hybrid
approach has discussed in [12]. Javed et al. [13] used FEM to
investigate the MHD laminar flow of Cu-water nanofluid
inside a triangular cavity while left wall is heated
uniformly/non-uniformly. Recently, Dulal Pal et al. [15]
studied the Hall current effect on the magneto hydrodynamic
thermal characteristics of nanofluids over stretching as well as
shrinking surface. They found that Hall parameter reduces
temperature profiles over stretching sheet, whereas, revers
trend found in shrinking sheet. Mansour et al. [16] discussed
the effect of viscous dissipation on entropy generation due to
MHD convection flow of nanofluid in porous square
enclosure with active parts and observed that the increase in
length of the heated and cold parts leads to the reduction in
the local total entropy generation. Sudasana Reddy et al. [17]
have explored numerically the heat and mass transfer
boundary layer flow of Cu-water and Ag-water based
nanofluids (with volume fraction 10% and 30%) over vertical
surface utilizing FEM method. The heat and mass flow
phenomena of Non Newtonian fluid through vertical surface
with convective conditions using Buongiornio’s model
studied by Subba Rao [18]. Recently, The bio convection heat
transfer in porous truncated cone was carried out by Mahdy
[19]. Sudhagar et al. [20] investigated the effects of different
parameters on laminar, mixed convection boundary flow over
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vertical cone filled with a nanofluid for the application of loud
speaker cooling ,in which Nur decreases with increase of M
ultimately it leads to the decrease of the voice coil
temperature in the loud speaker. Based on previous works,
Prabhavathi et al. [21] explained the flow of two different
nanofluids Al2O3-water and Cu-water in the presence of heat
generation/absorption. Siddiqa et al. [22] investigated the
presence of dust particles in nanofluid along the vertical wavy
frustum of a cone. Some interesting works on convection flow
can be found in [23, 24]. Since the bio convection has its
applications in bio-microsystems, the numerical solution to
the bio convection flow of nanofluid containing gyrotactic
microorganisms through vertical wavy cone was found by
Siddiqa et al. [25] and conclude that the amplitude of the
wavy surface of the cone and half cone angle has dominated
effect on heat and mass transfer coefficients as well as density
number of the microorganisms. Chandra Shekar Balla et al.
[26] explained the Finite element analysis of unsteady
convection flow along a vertical cone by considering both
magnetic field and thermal radiation and conclude that
velocity, temperature profiles decreases with magnetic
parameter. On the other hand, the temperature profile
depreciates with increase in radiation parameter. Hady et al.
[27] presented Non-Darcy convective flow along a vertical
cone filled with porous medium. Ramana et al. [28] studied
the behavior of MHD dirty nanofluids flow. They
recognized the enhancement in heat transfer in Cu-water dusty
nanofluid than Al2O3-water dusty nanofluid. The effects of
nano particle volume fraction and the nano particles diameter
on thermal conductivity of Al2O3-water nanofluid utilizing
the drift-flux model by Ghalambaz [29] and reported that
decrease in the size of nano particles or increase in the volume
fraction of nanoparticles reduces the rate of heat transfer from
the cone when the cone surface is hot. Khan et al. [30]
investigated for the solution of natural-convective flow along
both vertical cone and plate embedded in porous media filled
with power law nanofluids by considering convective
boundary conditions. In addition to this, different aspects
related to flow and heat transfer have been discussed in
[31,32&34-36]. Carbon nanotubes are the best heat
conducting materials and are the best choice in
nanotechnology. Because of this, Sreedevi et al. [33] have
analyzed the MHD flow of single and multi-walled carbon
nanotubes about vertical cone with convective boundary
conditions.
2. MATHEMATICAL ANALYSIS OF THE PROBLEM:
We assume a steady two-dimensional viscous incompressible
natural convection nanofluid flow over a vertical cone
embedded by saturated porous medium in the presence of
variable viscosity and thermal conductivity with the
coordinate system given in Fig.1. The fluid is assumed an
electrically conducted through a non-uniform magnetic field
of strength 𝐵0 is applied in the direction normal to the surface
of the cone. It is assumed that 𝑇𝑤, and 𝜙𝑤 are the temperature
and nanoparticle volume fraction at the surface of the cone
(𝑦 = 0) and 𝑇∞ and 𝜙∞ are the temperature and nanoparticle
volume fraction of the ambient fluid, respectively. By
employing the Oberbeck - Boussinesq approximation the
governing equations describing the steady-state conservation
of mass, momentum, energy as well as conservation of
nanoparticles for nanofluids take the following form:
Fig.1. Physical model and coordinate system
𝜕(𝑟𝑢)
𝜕𝑥+
𝜕(𝑟𝑣)
𝜕𝑦 = 0 (1)
𝜕𝑝
𝜕𝑦= 0 (2)
𝜕𝑝
𝜕𝑥 = −
𝜇(𝜙)
𝐾𝑢 + 𝑔 [(1 − 𝜙∞)𝜌𝑓∞𝛽(𝑇 − 𝑇∞) − (𝜌𝑝 −
𝜌𝑓∞)(𝜙 − 𝜙∞)] 𝑐𝑜𝑠 𝛾 −𝜎𝛽𝑜
2
𝜌𝑓𝑢 (3)
(𝑢𝜕𝑇
𝜕𝑥+ 𝑣
𝜕𝑇
𝜕𝑦) =
1
(𝜌𝑐𝑝)𝑛𝑓
𝜕
𝜕𝑦(𝑘𝑚(𝜙)
𝜕𝑇
𝜕𝑦) +
(𝜌𝑐)𝑝
(𝜌𝑐𝑝)𝑛𝑓
[𝐷𝐵𝜕𝜙
𝜕𝑦 .
𝜕𝑇
𝜕𝑦+
(𝐷𝑇
𝑇∞) (
𝜕𝑇
𝜕𝑦)
2
] − 1
(𝜌𝑐𝑝)𝑛𝑓
𝜕
𝜕𝑦(𝑞𝑟) (4)
1
𝜀(𝑢
𝜕𝜙
𝜕𝑥+ 𝑣
𝜕𝜙
𝜕𝑦) = 𝐷𝐵
𝜕2𝜙
𝜕𝑦2 + (𝐷𝑇
𝑇∞)
𝜕2𝑇
𝜕𝑦2 − 𝐾𝑟(𝜙 − 𝜙∞) (5)
The boundary conditions based on the problem description are
as follows:
𝑢 = 0, 𝑇 = 𝑇𝑤 , 𝐷𝐵𝜕𝜙
𝜕𝑦+ (
𝐷𝑇
𝑇∞)
𝜕𝑇
𝜕𝑦= 0 𝑎𝑡 𝑦 = 0 (6)
𝑢 → 0, 𝑇 ⟶ 𝑇∞, 𝜙 ⟶ 𝜙∞ 𝑎𝑡 𝑦 → ∞ (7)
In the present study, the viscosity and thermal conductivity
are taken as the reciprocal and a linear function of
nanoparticle volume fraction, respectively. Therefore, the
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viscosity in terms of nanoparticle volume fraction can be
written as follows:
1
𝜇=
1
𝜇∞[1 + 𝛾(𝜙 − 𝜙∞)] (8)
The above equation can be simplified as
1
𝜇= 𝑚𝜇(𝜙 − 𝜙𝑟) (9)
Where, 𝑚𝜇 and 𝜙𝑟 are can be defined as
𝑚𝜇 =𝛾
𝜇∞ and 𝜙𝑟 = 𝜙∞ −
1
𝛾 .
In the above equations (8) and (9), 𝜇∞, 𝑚𝜇, 𝜙∞, 𝜙𝑟, and γ are
constant values. The thermal conductivity as a function of
volume fraction of nanoparticle is defined as
𝑘𝑚(𝜙) = 𝑘𝑚,∞(1 + 𝑚𝑘(𝜙 − 𝜙∞)) (10)
Where, 𝑚𝑘 =𝑁𝑐
(𝜙𝑤−𝜙∞) and Nc is the variable thermal
conductivity parameter, 𝑘𝑚,∞ is the effective thermal
conductivity. By using Rosseland approximation for radiation
[34], the radiative heat flux 𝑞𝑟 is defined as
𝑞𝑟 = −4𝜎∗
3𝐾∗
𝜕𝑇4
𝜕𝑦 (11)
where 𝜎∗ is the Stephan-Boltzman constant, 𝐾∗ is the mean
absorption coefficient. We assume that the temperature
differences within the flow are such that the term 𝑇4 may be
expressed as a linear function of temperature. This is
accomplished by expanding 𝑇4 in a Taylor series about the
free stream temperature 𝑇∞ as follows:
𝑇4 = 𝑇∞4 + 4𝑇∞
3(𝑇 − 𝑇∞) + 6𝑇∞2(𝑇 − 𝑇∞)2 + ⋯ (12)
Neglecting higher-order terms in the above equation (12)
beyond the first degree in (𝑇 − 𝑇∞), we get
𝑇4 ≅ 4𝑇∞3𝑇 − 3𝑇∞
4 . (13)
Thus, substituting Eq. (13) into Eq. (11), we get
𝑞𝑟 = −16𝑇∞
3𝜎∗
3𝐾∗
𝜕𝑇
𝜕𝑦. (14)
The continuity equation (1) is satisfied by introducing a
stream function (𝜓) as
𝑢 =1
𝑟
𝜕ψ
𝜕𝑦, 𝑣 = −
1
𝑟
𝜕ψ
𝜕𝑥 (15)
The following similarity transformations are introduced to
simplify the mathematical analysis of the problem
η = 𝑦
𝑥𝑅𝑎𝑥
12⁄
, 𝑓(𝜂) =𝜓
𝛼𝑚.𝑟.𝑅𝑎𝑥
12⁄
, 𝜃(𝜂) = 𝑇−𝑇∞
𝑇𝑤−𝑇∞ , ∅(𝜂) =
𝜙−𝜙∞
𝜙𝑤−𝜙∞ , 𝑁𝑣 =
𝜙𝑟−𝜙∞
𝜙𝑤−𝜙∞ (16)
Where 𝑅𝑎𝑥 is the local Rayleigh number and is defined as
𝑅𝑎𝑥 =𝑔𝛽𝐾𝜌𝑓∞(1 − 𝜙∞)(𝑇𝑤−𝑇∞) 𝑥 𝐶𝑜𝑠𝛾
𝜇∞𝛼𝑚 (17)
and ‘ r ’ can be approximated by the local radius of the cone,
if the thermal boundary layer is thin, and is related to the x
coordinate by 𝑟 = 𝑥 𝑠𝑖𝑛𝛾.
Using the similarity variables (16) and making use of Eqn.
(14), the governing equations (3) - (5) together with boundary
conditions (6) and (7) reduce to
𝑁𝑣(𝑁𝑣 − ∅)𝑓 ′′ + 𝑁𝑣 𝑓 ′∅′ − (𝑁𝑣 − ∅)2(𝜃 ′ − 𝑁𝑟 ∅′) −
(𝑁𝑣 − ∅)2𝑀𝑓 ′ = 0 (18)
(1 + 𝑅)𝜃 ′′ + 𝑁𝑐 ∅ 𝜃 ′′ +3
2 𝑓 𝜃 ′ + 𝑁𝑐 𝜃 ′∅′ + 𝑁𝑡(𝜃 ′)2 +
𝑁𝑏 𝑓′𝜃′ = 0 (19)
∅′′ +3
2 𝐿𝑒 𝑓 ∅′ +
𝑁𝑡
𝑁𝑏 𝜃 ′′ − 𝐶𝑟 ∅ = 0 (20)
The transformed boundary conditions are
η = 0, 𝑓 = 0 , 𝜃 = 1 , Nb 𝑓 ′ + Nt 𝜃′ = 0.
η ⟶ ∞, 𝑓′ = 0 , 𝜃 = 0 , ∅ = 0. (21)
where prime denotes differentiation with respect to η, and the
key thermophysical parameters dictating the flow dynamics
are defined by
𝑁𝑟 =(𝜌𝑝 − 𝜌𝑓∞)(𝜙𝑤 − 𝜙∞)
𝜌𝑓∞𝛽(𝑇𝑤 − 𝑇∞)(1 − 𝜙∞), 𝑁𝑏 =
𝜀𝛽(𝜌𝑐)𝑝𝐷𝐵(𝜙𝑤 − 𝜙∞)
(𝜌𝑐)𝑓 𝛼𝑚,
𝑁𝑡 =𝜀(𝜌𝑐)𝑝𝐷𝑇(𝑇𝑤−𝑇∞)
(𝜌𝑐)𝑓 𝛼𝑚𝑇∞
, 𝐿𝑒 = 𝛼𝑚
𝜀𝐷𝐵 ,
𝑁𝑣 = −1
𝛾(𝜙𝑤−𝜙∞) , 𝑀 =
𝜎𝛽02𝑥
𝜌𝑅𝑎𝑥1/2 , 𝑅 =
16𝑇∞3𝜎∗
3𝐾∗𝑘 , 𝐶𝑟 =
𝐾𝑟𝑥2
𝐷𝐵𝑅𝑎𝑥.
Quantities of practical interest in this problem are local
Nusselt number Nux, and the local Sherwood number Shx, ,
which are defined as
𝑁𝑢𝑥 = 𝑥𝑞𝑤
𝑘𝑚 ,∞(𝑇𝑤−𝑇∞) , 𝑆ℎ𝑥 =
𝑥𝐽𝑤
𝐷𝑩(𝜙𝑤−𝜙∞) (22)
Here, 𝑞𝑤 is the wall heat flux and 𝐽𝑤 is the wall mass flux.
3. NUMERICAL METHOD OF SOLUTION:
The Finite-element method (FEM) is such a powerful method
for solving ordinary differential equations and partial
differential equations. The basic idea of this method is
dividing the whole domain into smaller elements of finite
dimensions called finite elements. This method is such a good
numerical method in modern engineering analysis, and it can
be applied for solving integral equations including heat
transfer, fluid mechanics, chemical processing, electrical
systems, and many other fields. Steps involved in finite-
element method [34, 35,36] are as follows.
(i) Finite-element discretization
(ii) Generation of the element equations
(iii) Assembly of element equations
(iv) Imposition of boundary conditions
(v) Solution of assembled equations
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4. RESULTS AND DISCUSSION
Numerical examination of the boundary value problem (18) –
(20) together with boundary conditions (21) has been
conducted at the eight influenced parameters to deliver the
physical incite of the flow problem and the results are shown
graphically from Figs. 2 – 21. The results obtained in the
present study are compared with the results of Noghrehabadi
et al. [31] and are shown in table 1. Thus it is very clear from
table 1 that the results of the present study are in close
agreement with the results published previously.
Table 1: Comparison of −𝜃′(0) with previously published
work with fixed values of 𝑁𝑡 = 10−6, 𝑁𝑏 = 10−5, 𝑁𝑟 =10−3, 𝑁𝑐 = 0.
Parameter Noghrehabadi
et al. [31]
Present
Study
Nv Le −𝜃 ′(0) −𝜃 ′(0)
2.0
10.0
20.0
200.0
1000
1000
1000
1000
0.7584
0.7670
0.7680
0.7688
0.7591
0.7675
0.7686
0.7694
It is clearly noticed from Fig.2 that velocity profiles elevated
by the variable viscosity parameter (Nv) in the vicinity of the
cone surface. But, in the areas far away from the cone surface,
inside the boundary layer, the velocity profiles are poorly
affected by (Nv). The temperature distributions are
decelerated in the boundary layer region (Fig. 3) with the
rising values of (Nv). It is noted from Fig. 4 that nanoparticle
concentration distributions are elevated significantly from the
surface of the cone into the boundary layer as the values of
(Nv) increased.
It is observed from fig. 5 that the thickness of hydrodynamic
boundary layer is reduced with the enhancing values of
buoyancy ratio parameter (Nr). The temperature profiles of
the fluid rises with increasing values of (Nr) as shown in fig.
6. The concentration profiles enhances throughout the fluid
region with improving values of (Nr). This is because of the
fact that solutal boundary layer thickness elevates with
increasing values of Nr (Fig.7).
The impact of magnetic parameter (M) on velocity (𝑓′),
temperature (θ) and concentration of nanoparticle (∅) profiles
are depicted in Figs. 8 – 10. The thickness of hydrodynamic
boundary layer decelerates, whereas, the thickness of thermal
boundary layer heightens as the values of M rises. The
concentration of the fluid has changed its behavior at 𝜂 = 1.3,
fluids concentration diminishes when 𝜂 < 1.3, elevates when
𝜂 > 1.3 with enhance in the values of M (Fig 10).
With the higher values of radiation parameter (R) fluids
velocity and temperature rises in the boundary layer regime.
This is because of the fact that imposing thermal radiation into
the flow warmer the fluid, which causes an increment in the
thickness of hydrodynamic and thermal boundary layer in the
entire flow region (Fig.11 & 12). An increase in the values of
variable thermal conductivity parameter (Nc) the velocity,
temperature and concentration distributions deteriorates in the
fluid region as shown in figs. 13 – 15. This is because of the
fact that the thermal conductivity of the nanofluid decelerates
near the cone surface as the values of variable thermal
conductivity parameter (Nc) rises.
Figures 16 and 17 depict the temperature (θ) and
concentration (∅) distributions for various values of
thermophoretic parameter (Nt). Both the temperature and
concentration profiles elevate in the boundary layer region for
the higher values of thermophoretic parameter (Nt). Figures
18 – 19 shows the influence of Brownian motion parameter
(Nb) on thermal and solutal boundary layer thickness. It is
noticed that, with the increasing values of Brownian motion
parameter (Nb) the temperature of the fluid decelerates in the
boundary layer regime (Fig.18). Furthermore, the
concentration profiles are decelerated in the fluid regime as
the values of Nb rises (Fig. 19).
Fig.2: Effect of Nv on Velocity profiles.
Fig.3: Effect of Nv on Temperature profiles.
Nv 1.0, 3.0, 5.0, 7.0
R 0.1, Nt 0.5, Nr 0.5,
Le 5.0, Nb 0.5, M 0.5,
Cr 0.1, Nc 0.1.
1 2 3 4 5
0.2
0.4
0.6
0.8
1.0
f
Nv 1.0, 3.0, 5.0, 7.0
R 0.1, Nt 0.5, Nr 0.5,
Le 5.0, Nb 0.5, M 0.5,
Cr 0.1, Nc 0.1.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
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Fig.4: Effect of Nv on Concentration profiles.
Fig.5: Effect of Nr on Velocity profiles.
Fig.6: Effect of Nr on Temperature profiles.
Fig.7: Effect of Nr on Concentration profiles.
Fig.8: Effect of M on Velocity profiles.
Fig.9: Effect of M on Temperature profiles.
Nv 1.0, 3.0, 5.0, 7.0
R 0.1, Nt 0.5, Nr 0.5,
Le 5.0, Nb 0.5, M 0.5,
Cr 0.1, Nc 0.1.
1 2 3 4
0.10
0.05
0.05
0.10
Nr 0.1, 0.4, 0.7, 1.0
R 0.1, Nt 0.5, Nc 0.1,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5
0.2
0.4
0.6
0.8
1.0
1.2
f
Nr 0.1, 0.4, 0.7, 1.0
R 0.1, Nt 0.5, Nc 0.1,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
Nr 0.1, 0.4, 0.7, 1.0
R 0.1, Nt 0.5, Nc 0.1,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4
0.10
0.05
0.05
M 0.5, 1.2, 1.9, 2.5
Nt 0.5, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, R 0.1
Nv 3.0, Le 5.0.
1 2 3 4 5
0.2
0.4
0.6
0.8
1.0
f
M 0.5, 1.2, 1.9, 2.5
Nt 0.5, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, R 0.1
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
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International Journal of Applied Engineering Research ISSN 0973-4562 Volume 13, Number 22 (2018) pp. 15611-
© Research India Publications. http://www.ripublication.com
15617
Fig.10: Effect of M on Concentration profiles.
Fig.11: Effect of R on Velocity profiles.
Fig.12: Effect of R on Temperature profiles.
Fig.13: Effect of Nc on Velocity profiles.
Fig.14: Effect of Nc on Temperature profiles.
Fig.15: Effect of Nc on Concentration profiles.
M 0.5, 1.2, 1.9, 2.5
Nt 0.5, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, R 0.1
Nv 3.0, Le 5.0.
1 2 3 4
0.10
0.05
0.05
R 0.1, 0.3, 0.5, 0.7
Nt 0.5, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5
0.2
0.4
0.6
0.8
1.0
f
R 0.1, 0.3, 0.5, 0.7
Nt 0.5, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
Nc 0.5, 1.2, 1.9, 2.5
R 0.1, Nt 0.5, Nr 0.5,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5
0.2
0.4
0.6
0.8
1.0
1.2
f
Nc 0.5, 1.2, 1.9, 2.5
R 0.1, Nt 0.5, Nr 0.5,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
Nc 0.5, 1.2, 1.9, 2.5
R 0.1, Nt 0.5, Nr 0.5,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4
0.10
0.05
0.05
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International Journal of Applied Engineering Research ISSN 0973-4562 Volume 13, Number 22 (2018) pp. 15611-
© Research India Publications. http://www.ripublication.com
15618
Fig.16: Effect of Nt on Temperature profiles.
Fig.17: Effect of Nt on Concentration profiles.
Fig.18: Effect of Nb on Temperature profiles.
Fig.19: Effect of Nb on Concentration profiles.
Fig.20: Effect of Le on Concentration profiles.
Fig.21: Effect of Cr on Concentration profiles.
It is observed from fig. 20 that concentration distributions
decelerate with the increasing values of the Lewis number
(Le) in the entire boundary layer region. By definition, the
Lewis number represents the ratio of thermal diffusivity to the
mass diffusivity. Increasing the Lewis number means a
higher thermal diffusivity and a lower mass diffusivity, and
this produces thinner thermal and concentration boundary
layers. It is noticed from Fig.21 that concentration profiles are
Nt 0.1, 0.2, 0.3, 0.4
R 0.1, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0
Nt 0.1, 0.2, 0.3, 0.4
R 0.1, Nb 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4
0.04
0.02
0.02
0.04
0.06
Nb 0.3, 0.5, 0.7, 0.9
R 0.1, Nt 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4 5 6
0.2
0.4
0.6
0.8
1.0 Nb 0.3, 0.5, 0.7, 0.9
R 0.1, Nt 0.5, Nc 0.1,
Cr 0.1, Nr 0.5, M 0.5,
Nv 3.0, Le 5.0.
1 2 3 4
0.05
0.05
0.10
0.15
Le 5.0, 7.0, 9.0, 11.0
R 0.1, Nt 0.5, Nr 0.5,
Cr 0.1, Nb 0.5, M 0.5,
Nv 3.0, Nc 0.1.
1 2 3 4
0.04
0.02
0.02
0.04
0.06
Cr 0.1, 0.3, 0.5, 0.7
R 0.1, Nt 0.5, Nr 0.5,
Le 5.0, Nb 0.5, M 0.5,
Nv 3.0, Nc 0.1.
1 2 3 4
0.05
0.05
Page 9
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 13, Number 22 (2018) pp. 15611-
© Research India Publications. http://www.ripublication.com
15619
highly influenced by the chemical reaction parameter and
declines in the fluid region.
It is noticed from table 2 that the magnitude of skin-friction
coefficient, Nusselt and Sherwood numbers are amplified in
the fluid regime as the values of variable viscosity parameter
(Nv) increases. The non-dimensional velocity and heat
transfer rates upsurges, whereas, mass transfer rate diminishes
with the higher values of (Nc). It is obvious from table 2 that
the dimensionless rates of velocity escalates, whereas, rates of
heat and mass transfer are both deteriorates with the higher
values of (Nt). It is also seen from this table that the values of
skin-friction coefficient and Nusselt number decelerates,
whereas, Sherwood number values enhances in the fluid
region as the values of (Nb) rises. Higher the values of
chemical reaction parameter (Cr) lower the values of non-
dimensional velocity, heat and mass transfer rates.
Table 2: Effect of various parameters on local skin-friction
co-efficient (𝐶𝑓), local Nusselt number ( 𝑁𝑢𝑥) and local
Sherwood number (𝑆ℎ𝑥).
Parameters −𝑓 ′′(0) −𝜃′(0) −𝜑′(0)
Nv Nc Nt Nb Cr
1.0
3.0
5.0
7.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
0.1
0.1
0.1
0.1
0.5
1.2
1.9
2.5
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.1
0.2
0.3
0.4
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.3
0.5
0.7
0.9
0.5
0.5
0.5
0.5
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.3
0.5
0.7
0.891364
1.117950
1.133760
1.120990
1.152860
1.163740
1.178620
1.198130
0.988353
1.029980
1.070410
1.109660
1.279170
1.147720
1.090000
1.057610
0.896364
0.893576
0.886547
0.876047
0.569568
0.662561
0.691567
0.691253
0.742135
0.897660
1.186630
1.815350
0.708372
0.701997
0.695130
0.687843
0.691365
0.680198
0.674447
0.670993
0.574568
0.572239
0.570990
0.568162
-0.502992
-0.815183
-0.937933
-0.992331
-0.484589
-0.603443
-1.891771
-1.998438
-0.141674
-0.280799
-0.417078
-0.550274
-1.152280
-0.680198
-0.481748
-0.372774
-0.299253
-0.311181
-0.466227
-0.562668
5. CONCLUSIONS
MHD natural convection boundary layer flow, heat and mass
transfer characteristics over a vertical cone embedded in a
porous medium saturated by a nanofluid under the impact of
variable viscosity, variable thermal conductivity, thermal
radiation and chemical reaction is investigated in this
research. The hydrodynamic, thermal and solutal boundary
layers thickness were analyzed for various values of the
pertinent parameters and the results are shown in figures.
Furthermore, the impact of these parameters on Nusselt
number and Sherwood number are also calculated. The
important findings of the present study are summarized as
follows.
(i) The hydrodynamic boundary layer thickness
heightens, whereas, the thickness of thermal
boundary layer decelerates as the values of (Nv)
rises.
(ii) With the increasing values of (Nc) the values of skin-
friction coefficient and Nusselt number elevates in
the fluid region.
(iii) Both the temperature and concentration profiles
elevates in the boundary layer regime as the values of
(Nt) increases.
(iv) With increase in the values (Nb) the temperature and
concentration distributions of the fluid, deteriorates.
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