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Peristaltic Transport of a Couple-stress Fluid with nanoparticles having permeable
walls
K. Maruthi Prasad1, N. Subadra*2 and S. Karunakar Reddy3
1Department of Mathematics, School of Technology, GITAM University, Hyderabad Campus, Hyderabad, Telangana, India-502329.
Email: [email protected] of Mathematics, Geethanjali College of Engg.& Tech., Cheeryal (V),
Keesara (M), R.R. Dist., Telangana, India-501301.Email: [email protected]
3Department of Mathematics, JNTUH, Kukatpally, Hyderabad, Telangana, India-500085.Email: [email protected]
* Corresponding author: [email protected]
Abstract: The paper deals with a theoretical investigation of the peristaltic transport of a
couple-stress fluid with heat and mass transfer effects. The velocity, pressure drop, time
averaged flux, frictional force, mechanical efficiency, temperature profile, nano particle
phenomena, heat transfer coefficient and mass transfer coefficient of the fluid are
investigated, when the Reynolds number is small and wave length is large by using
appropriate analytical methods. Effects of different physical parameters like couple-stress
fluid parameters, Brownian motion parameter, thermophoresis parameter, local temperature
Grashof number as well as local nano particle Grashof number on pressure drop
characteristics, frictional force, heat transfer coefficient, mass transfer coefficient and steam
line patterns of the fluid are studied. The expressions for pressure drop, temperature profile,
nano particle phenomenon, heat transfer coefficient and mass transfer coefficients are
sketched through graphs. The streamlines are drawn to discuss trapping phenomena for some
physical quantities.
Keywords: Peristalsis, Couple-stress fluid, Brownian motion parameter, Thermophoresis
parameter, Heat transfer coefficient, Mass transfer coefficient.
1. Introduction
Peristalsis is an important mechanism for fluid transport which can be generated by the
propagation of waves along the walls of a flexible tube containing liquid. Physiologically, it
is known as an automatic and vital process that drives the urine from kidney to bladder
through the ureters, food through the digestive tract, bile from the gall bladder into the
duodenum, vasomotion in small blood vessels and so on. The peristaltic transport is also
exploited in industrial pumping as it provides efficient means for sanitary fluid transport in
nuclear industries and in roller pumps. Several investigations have analyzed the peristaltic
motion of both Newtonian and non-Newtonian fluids in physiological as well as mechanical
systems (Fung & Yih, [1], Shapiro, Jaffrin, & Weinberg, [2], Shehawey & Sebaei, [3],
Radhakrishnamacharya & Srinivasulu, [4], Alemayehu & Radhakrishnamacharya, [5],
Prasad et al. [6]).
Couple-stress fluid is a special case of non-Newtonian fluid which was developed by
Stokes, [7]. The important feature of these fluids is that the stress tensor is not symmetric and
their accurate flow behaviour cannot be predicted by the classical Newtonian theory. The
main effect of couple stresses will to be introducing a size dependent effect that is not present
in the classical viscous theories. Shehawey & Mekheimer, [8] studied Couple-stresses in
peristaltic transport of fluids. Effect of peripheral layer on peristaltic transport of a couple-
stress fluid was investigated by Prasad & Radhakrishnamacharya, [9]. Alemayehu &
Radhakrishnamacharya, [5] discussed dispersion of a solute in peristaltic motion of a couple-
stress fluid through a porous medium with slip condition. Hydromagnetic effect on inclined
peristaltic flow of a couple stress fluid was investigated by Shit & Roy, [10].
Nanofluid is a fluid containing nano-sized particles called nanoparticles. These fluids are
engineered colloidal suspensions of nanoparticles in a base fluid. The nanoparticles used in
nanofluids are typically made of metals, oxides, or carbon nanotubes. Nanofluids have new
properties that make them potentially useful in many applications in heat transfer, including
microelectronics, fuel cells, pharmaceutical processes and hybrid powered engines (Das,
Putra, & Roetzel, [11]). They exhibit enhanced thermal conductivity and the convective heat
transfer coefficient compared to the base fluid. Many researchers done their research in
nanofluid technology (Noreen Sher Akbar, [12]), Akbar & Nadeem, [13], Prasad et al. [14].
Most of the researchers have done their study using no slip boundary condition at the
walls of the vessels. But the blood vessel walls may be movable, flexible and permeable in
nature. Chu & Fang, [15] investigated peristaltic transport in a slip flow. Slip effects on
peristaltic transport of power-law fluid through an inclined tube was studied by Naby &
Shamy, [16]. Hayat et al. [17] studied slip effects on peristaltic transport in an inclined
channel with mass transfer and chemical reaction.
Motivated by the above studies, peristaltic transport of a couple-stress fluid with
nanoparticles having permeable walls under the assumption of long wavelength and low
Reynolds number have been investigated. Homotopy perturbation method is used to solve
coupled equations of temperature profile and nanoparticle phenomena. The analytical
solutions of velocity, pressure drop and frictional force are obtained. The effects of various
parameters on these flow variables are investigated.
2. Mathematical Formulation
Consider the peristaltic transport of an incompressible couple stress fluid with
nanoparticles in a tube of uniform cross section of radius ‘a’ with sinusoidal wave travelling
along the boundary of the tube with speed c , amplitude band wave lengthλ. Choosing the
cylindrical polar coordinate system (R ,θ ,Z ) , the wall deformation due to the propagation of
an infinite train of peristaltic waves is given by
R=H ( z , t )=a+b sin 2πλ
(Z−ct) (1)
The governing equations in the fixed frame for an incompressible couple-stress fluid
flow with nano particles in the absence of body moment and body couple are given as (Maiti
et al. [18])
T ji . j=ρd w i
dt(2)
e ijkT jkA +M ji. j=0 (3)
lij=−pδij+2μ ijd ij (4)
μij=4ηω j .i+4 η'ωij (5)
(ρc )fdT '
dt=k∇2T '+( ρc )p[DB∇C
' .∇T '+DT
T0' ∇T
' .∇T ' ] (6)
dC '
dt=DB∇
2C '+[DT '
T0' ]∇2T ' (7)
where w i is the velocity vector, T ij and T ijA are the symmetric and antisymmetric parts of
the tensor T ij respectively, M ij is the couple-stress tensor, μij is the deviatoric part ofM ij, ωij is
the vorticity vector, d ij is the symmetric part of the velocity gradient, η and η' are constants
associated with the couple-stress, p is the pressure and other terms have their usual meaning
from tensor analysis.ρ f is the density of the fluid, ρpis the density of the particle, Cis the
volumetric volume expansion coefficient, f represents the body forces, ddt represents the
material time derivative, Cis the nano particle concentration, DBis the Brownian diffusion
coefficient and DT is the thermophoretic diffusion coefficient. The ambient values of T∧C as
r tend to h are denoted by T oand Co .
Using the transformation
r=R , z=Z−ct , u=U ,w=W−c ,θ=θ
From a stationary to a moving frame of reference, the equations (2) – (7) are converted to
μ∇2[1− 1α2 ∇
2]w'=d p'd z '+ρgβ (T '−T 0
' )+ρgβ (C'−C 0' ) (8)
[u' ∂T '∂r '+w' ∂T
'
∂ z ' ]=β [ ∂2T '
∂r '2+ 1r '∂T '
∂ r '+ ∂
2T '
∂z '2 ]+τ ¿(9)
[u' ∂C'∂ r '+w' ∂C
'
∂ z ' ]¿DB[ ∂2C '
∂ r '2+ 1r '∂C '
∂r '+ ∂
2C'
∂ z'2 ]+DT '
T0' [ ∂2T '
∂ r '2+ 1r '∂T '
∂ r '+ ∂
2T '
∂ z '2 ] (10)
with∇2=1r∂∂r (r ∂∂ r )
whereτ=(ρC)P(ρC )f
is the ratio between the effective heat capacity of the nanoparticle material
and heat capacity of the fluid.
Introducing the following non-dimensional quantities:
r=r'
a, z= z '
λ,w=w
'
c, p=a
2 p '
λcμ, t= c t
'
λ,u= λu '
ac,θ t=
T '−T 0'
T 0' ,
δ=aλ,R e=
2 ρcaμ
,σ=C'−C0
'
C0' , β= k
( ρc )f, Nb=
(ρc )pDBC 0'
(ρc )f,
N t=( ρc )pDT 'T 0
'
(ρc )f β,Gr=
gβa3T 0'
γ 2 , B r=gβa3C 0
'
γ2 ,
α=aα=√ μη a ,h'=haUsing the non-dimensional quantities in equations (8)-(10) and applying the long
wavelength and low Reynolds number approximations and neglecting the inertial terms, the
equations (8)-(10) are converted to
1r∂∂r (r ∂∂ r (1− 1
α 2 ∇2)w)=dpdz +Grθt+B rσ (11)
0=1r∂∂ r (r ∂θ t∂ r )+N b
∂σ∂r∂θt∂ r
+N t ( ∂θ t∂ r )2
(12)
0=1r∂∂ r (r ∂σ∂ r )+ N t
Nb(1r∂∂ r (r ∂θ t∂ r )) (13)
whereθt , σ ,Nb , N t ,Gr ,B r are the temperature profile, nanoparticle phenomena, Brownian
motion parameter, Thermophoresis parameter, local temperature Grashof number and local
nano particle Grashof number, and w is the axial velocity, r is the radial coordinate,α is the
couple-stress fluid parameter.
The non-dimensional boundary conditions are:
∂w∂r
=0 ,∂ θt∂r
=0 , ∂ σ∂ r
=0at r=0, (14)
w=−k ∂w∂r,θt=0 , σ=0at r=h ( z )=1+ε sin 2π z , (15)
∂2w∂r2 −η
r∂w∂r
=0at r=h (z )=1+ε sin 2πz, (16)
∂2w∂r2 −η
r∂w∂ris finite at r=0. (17)
whereε (¿ba) is the amplitude ratio and η'=
ηη is a couple-stress fluid parameter.
Boundary conditions (16) and (17) indicate that the couple-stresses vanish at the tube
wall and is finite at the tube axis respectively.
3. Solution of the Problem
Homotopy perturbation method is used to solve the coupled equations of temperature
profile and nanoparticle phenomena i. e. Eqs. (12) and (13).
The homotopy for the equations (12) and (13) are as follows Akbar & Nadeem, [13]:
H (ζ , θt )=(1−ζ ) [L (θ t )−L (θ t10 ) ]+ζ [L (θt )+N b∂σ∂r∂θ t∂r
+N t( ∂θt∂r )2] (18)
H (ζ , σ )= (1−ζ ) [L (σ )−L (σ10 ) ]+ζ [L (σ )+N t
Nb(1r∂∂ r (r ∂θ t∂r ))] (19)
where,L=1r∂∂ r (r ∂∂ r ) is taken as linear operator for convenience.
θ1 0 (r , z )=( r2−h2
4 ) ,σ 1 0 (r , z )=−(r 2−h2
4 ) (20)
are chosen as initial guess which satisfy the boundary conditions.
Define
θt (r , z )=θ t0+ζ θt1+ζ2θ t2+−−−−¿ (21)
σ (r , z )=σ 0+ζ σ1+ζ2σ2+−−−−¿ (22)
The series (21) and (22) are convergent for most of the cases. The convergent rate
depends on the nonlinear part of the equation.
Adopting the same procedure as done by Akbar & Nadeem, [13], the solution for
temperature profile and nano particle phenomena can be written for ζ=1 as
θ (r , z )=( r 4−h4
64 ) (Nb−N t ) (23)
σ (r , z )=−( r2−h2
4 ) N t
N b (24)
Substituting Eqs. (23) and (24) in Eq. (11), and solving Eq. (11) using the boundary
conditions (14)-(17), the expression for velocity is
w=B ( I 0 (α r )−I 0 (α h )−k α I 1 (α h ) )−C+ dpdz ( r
2
4−h
2
4− kh
2 )+Gr (N b−N t ) ( 1
α6 −h4
64α 2 +r2
4 α 4 −r2h2
256+ r4
64 α 4 +r6
2304 )+Br( N t
N b)(−1α 4 + h2
4 α2 −r 2
4 α2 +r2h2
16− r4
64 ) (25)
where
A=α [α I 0 (α h )−(1+ηh )I 1(α h)]
B=−Gr
A (Nb−N t )(( 12α 4 (1−η ))+( h
4
192(1+η ))+( h2
16 α2 (1−3η )))
−B rA ( N t
N b)(( 1
2α 2 (η−1 ))−( h2
16(1+η )))
C=Gr (Nb−N t )( 1α6 +
h2
4α 4 −h4
256+ h6
2304+ hk
2α 4 −k h3
128+ k h3
16α2 + k h5
384 )+Br( N t
N b)(−1α 4 + 3h4
64− kh
2α2 + k h3
16 )The dimension less flux in the moving frame is given as
q=∫0
h
2 rwdr (26)
Substituting Eq. (25) in Eq. (26) and solving, the flux is
q= dpdzS+2B(h I 1 (α h )− k h
2α2
I 1 (α h )− h2
2I 0 (α h ))−C h2
+Gr (N b−N t ) ( h2
α6 + h4
8α4 − h6
192α 2 +h8
9216 )+Br( N t
Nb)(−h2
α 4 + 5h6
192 ) (27)where, S=−h4
8− k h
3
2
From Eq. (27), the expression for dpdz is
dpdz
=1Sq−2B (h I1 (α h )− k h
2α2
I 1 (α h )− h2
2I0 (α h ))+C h2
−Gr (Nb−N t )( h2
α6 +h4
8 α4 −h6
192α2 + h8
9216 )−B r( N t
N b)(−h2
α 4 + 5h6
192 ) (28)
The pressure drop over the wavelength ∆ Pλ is defined as
∆ Pλ=−∫0
1 dPdzdz . (29)
Substituting the expression dpdz in Eq. (29), the pressure drop is
∆ Pλ=q L1+L2 (30)
where, L1=∫0
1 1Sdz
and
L2=∫0
1 2BS (h I 1 (α h )− k h
2α2
I1 (α h )−h2
2I 0 (α h ))dz−∫
0
1 C h2
Sdz
+Gr (Nb−N t )∫0
1
( h2
α6 + h4
8α4 − h6
192α 2 +h8
9216 ) 1Sdz
+Br( N t
N b)∫
0
1
(−h2
α 4 + 5h6
192 ) 1Sdz
Following the analysis of Shapiro et al. (1969), the time averaged flux over a period in the
laboratory frame Q is given as
Q=1+∈2
2+q (31)
Substituting Eq. (31) in equation Eq. (34), the time averaged flux is
Q=1+∈2
2+∆ P λL1
−L2
L1 (32)
The dimensionless frictional force F at the wall is
F=∫0
1
h2(−dPdz )dz (33)
Heat Transfer Coefficient
The heat transfer coefficient at the wall is given as
Zθ (r , z )=( ∂h∂z )(∂θ t∂ r ) (34)
Mass Transfer Coefficient
The mass transfer coefficient at the wall is as follows
Zσ (r , z )=( ∂h∂ z )( ∂σ∂r ) (35)
4. Results and Discussion
Analytical expressions for the pressure drop, time averaged flux, frictional force, heat
transfer coefficient and mass transfer coefficient have been calculated. Various graphs are
depicted by using Mathematica software.
4.1 Pressure rise characteristics
Figs. 1.1-1.7 illustrate the variation of pressure rise(−∆ pλ)with time averaged flux (Q) of
peristaltic waves for different values of couple-stress fluid parametersα ,η, Brownian motion
parameter(N b), thermophoresis parameter(N t), local temperature Grashof number (Gr ) , local
nano particle Grashof number(Br )and slip parameter (k ) .
From Figs. 1.1 – 1.3 it is clear that, pressure rise(−∆ pλ ) decreases with the couple-stress
fluid parameterα , ηand Brownian motion parameter(N b ) . From Figs. 1.4-1.7 it is noticed that
pressure rise(−∆ pλ ) increases with the increase of thermophoresis parameter(N t), local
temperature Grashof number(Gr ) ,local nano particle Grashof number(Br )and with slip
parameter (k ).
It is also observed that pressure rise (−∆ pλ ) increases with the increase of time averaged
flux (Q ) for fixed values of α ,η ,Nb , N t ,Gr ,Br ,k .
Fig.1.1: Effect of Q∧α on(∆ pλ )(ϵ=0.9 , η=0.2 ,Gr=0.5 ,Br=0.3 ,N b=1.3 , N t=1.8 , k=0.6 )
Fig.1.2: Effect of Q∧ηon(∆ pλ)(ϵ=0.4 , α=1 ,G r=0.5 , Br=0.3 ,N b=1.3 ,N t=1.8 , k=0.6 )
4.2 Frictional Force
The variation of frictional force (F)with various parameters is shown graphically from
Figs. 2.1-2.6. The frictional force (F) increases with couple-stress fluid parameterη,
thermophoresis parameter (N ¿¿ t) ,¿local temperature Grashof number (Gr ) , local Nano
Fig.1.3: Effect of Q∧N bon(∆ pλ)(ϵ=0.1 , α=3.2, η=1.2,Gr=0.5 ,B r=0.3 , k=0.6 , N t=1.8 )
Fig1.4: Effect of Q∧N t on(∆ pλ)(ϵ=0.1 , α=1.2 , η=0.8 ,G r=0.5 , Br=0.3 , k=0.6 , Nb=1.3 )
Fig.1.5: Effect of Q∧Gr on(∆ pλ)(ϵ=0.3 , α=2.2 ,η=1.8 ,N b=1.3 ,B r=0.3 , k=0.6 , N t=1.8 )
Fig.1.6: Effect of Q∧Br on(∆ pλ)(ϵ=0.9 , α=2.2 ,η=0.8 , k=0.6 ,G r=0.5 , Nb=1.3 ,N t=1.8 )
Fig.1.7: Effect of Q∧k on(∆ pλ)(ϵ=0.9 , α=2.2 ,η=0.8 ,Gr=0.5 ,Nb=1.3 , ,N t=1.8 ,B r=0.3 )
particle Grashof number (Br )and with slip parameter (k )but decreases with Brownian motion
parameter¿¿) (Figs. 2.1-2.6).
4.3Temperature Profile
Effects of temperature profile (θt) with respect to the Brownian motion parameter (Nb)
and thermophoresis parameter (N t) has been shown from Figs. 3.1-3.2. It can be seen that,
temperature profile(θt) increaseswith the increase of Brownian motion parameter (Nb) and
Fig.2.4: Effect of Q∧N t onF(ϵ=0.5 , α=3.2 ,η=1.2 ,Gr=0.5 ,B r=0.3 ,Nb=1.3 , k=0.6 )
Fig.2.1: Effect of Q∧ηonF(ϵ=0.9 , α=1.8 ,Gr=0.5 ,B r=0.3 ,N b=1.3 ,N t=1.8 , k=0.6 )
Fig.2.3: Effect of Q∧N bonF(ϵ=0.5 , η=0.2 ,Gr=0.5 ,Br=0.3 , α=1.2 ,N t=1.8 , k=0.6 )
Fig.2.5: Effect of Q∧Gr onF(ϵ=0.1 , α=1.8 ,η=1.5 ,N b=1.3 ,B r=0.3 , , N t=1.8 , k=0.6 )
Fig.2.6: Effect of Q∧Br onF(ϵ=0.1 , α=0.8 , η=0.5 ,Gr=0.5 ,N b=1.3 , ,N t=1.8 , k=0.6 )
Fig.2.2: Effect of Q∧k onF(ϵ=0.1 , α=0.8 , η=0.5 ,Gr=0.5 ,N b=1.3 ,N t=1.8 , Br=0.3)
decreases with the increase of thermophoresis parameter(N t ) .It is interesting to observe that
value of temperature profile(θ) is maximum in the range[−0.5 ,0.5 ].
4.4Nano particle phenomenon
Figs. 4.1-4.2 explain the nature of nano particle phenomena (σ ) for different values of
Brownian motion parameter (Nb )and thermophoresis parameter(N t ). It can be seen that, the
nano particle phenomena(σ ) increases with the increase of Brownian motion parameter (N b )
and decreases with thermophoresis parameter (N t ) .It is also observed that nano particle
phenomena (σ ) attains maximum value atr=0.
4.5 Heat Transfer Coefficient
Figs.5.1-5.3 indicate the variation of heat transfer coefficient (Zθ) for various values of
Brownian motion parameter(Nb), thermophoresis parameter (N t) and amplitude ratio(ϵ ).
From Figs. 5.1-5.3, it can be observed that, the value of the heat transfer coefficient (Zθ)
Fig. 3.1: Variation in Temperature profile with N b
Fig. 3.2: Variation in Temperature profile with N t
Fig. 4.1: Variation in Nano particle with N b
Fig. 4.2: Variation in Nano particle with N t
increases with Brownian motion parameter (Nb )and thermophoresis parameter(N t ) , amplitude
ratio(ϵ ) and then decreases after attaining a constant value.
4.6 Mass Transfer Coefficient
Figs. 6.1-6.3 illustrate the effect of various parameters on mass transfer coefficient(Zσ). It
is interesting to observe that, mass transfer coefficient(Zσ) decreases with the increase of
Brownian motion parameter(N b), thermophoresis parameter(N t )and then increases after
attaining a constant value. However, mass transfer coefficient(Zσ)shows an opposite
behaviour with respect to amplitude ratio(ϵ ).
Fig. 5.1: Variation in heat transfer coefficient with Nb
Fig. 5.2: Variation in heat transfer coefficient with N t
Fig. 5.3: Variation in heat transfer coefficient with ϵ(z¿3 , N t=2.8 ,Nb=0.2¿
4.7 Streamline patterns
Trapping is a phenomenon where the streamlines on the center line in the moving frame
are divided in order to encircle a bolus of fluid particles circulating along closed streamlines
under certain given conditions. Trapping is a characteristic of peristaltic motion. As the bolus
emanate to be trapped by the wave, the bolus moves at equal speed with that of the wave.
Figs. 7.1-7.4 illustrates the streamline patterns and trapping for different values of couple-
stress fluid parameters, Brownian motion parameter, thermophoresis parameter, local
temperature Grashof number, local nano particle Grashof number and amplitude ratio.
From Fig. 7.1 it is clear that, the volume of the trapped bolus increases with the increase
of couple-stress fluid parameterα . From figs. 7.2-7.4 it is observed that the volume of the
trapped bolus decreases with the decrease of couple-stress fluid parameter η, slip parameter
(k ) and with Brownian motion parameter N b .
Fig. 6.1: Variation in Mass transfer coefficient with N b
Fig. 6.2: Variation in Mass transfer coefficient with N t
Fig. 6.3: Variation in Mass transfer coefficient with ϵ
5 Conclusion
Fig.7.1: Stream line patterns for different values ofα(ϵ=0.9 ,Q=−1.5 , η=0.2 ,Gr=0.5 ,Br=0.3 , Nb=5 , N t=4 , k=0.4 )
Fig.7.2: Stream line patterns for different values of η(ϵ=0.9 ,Q=−1.5 , α=0.2 ,Gr=0.5 , Br=0.3 ,Nb=5 ,N t=4 , k=0.4 )
Fig.7.3: Stream line patterns for different values of Nb
(ϵ=0.9 ,Q=−1.5 , α=0.2 ,Gr=0.5 , Br=0.3 , η=0.2 ,N t=4 , k=0.4 )
Fig.7.4: Stream line patterns for different values of k
(ϵ=0.7 ,Q=−1.5 , α=0.2 ,Gr=0.5 ,Br=0.3 , η=0.2 , Nb=5 , N t=4 )
The major premise of the paper is peristaltic transport of a couple-stress fluid with
nanoparticles having permeable walls. The study particularly pertains to a situation when the
Reynolds number is low and wavelength is large. Emphasis was laid to investigate the
pressure drop characteristics, frictional force, temperature profile, nanoparticle phenomena,
heat transfer coefficient, mass transfer coefficient and stream line patterns of the couple-
stress fluid parameters, Brownian motion parameter, thermophoresis parameter. Homotopy
perturbation method is used to solve the coupled equations of temperature profile and
nanoparticle phenomena and analytical methods have been applied to the present study to
find the other variables.
The main points of the analysis are as follows:
a. Pressure rise decreases with the couple-stress fluid parameterα , ηand Brownian
motion parameter. Pressure rise increases with the increase of thermophoresis
parameter, local temperature Grashof number, local nano particle Grashof number and
with slip parameter.
b. Frictional force (F) increases with couple-stress fluid parameterη, thermophoresis
parameter, local temperature Grashof number, local Nano particle Grashof number
and with slip parameter but decreases with Brownian motion parameter.
c. Temperature profile increases with the increase of Brownian motion parameter and
decreases with thermophoresis parameter and the value of temperature profile is
maximum/minimum forr∈ [−0.5,0 .5 ] .
d. Nano particle phenomenon increases with the increase of Brownian motion parameter
and decreases with thermophoresis parameter and it reaches maximum atr=0.
e. Heat transfer coefficient increases with Brownian motion parameter and
thermophoresis parameter, amplitude ratio and after attaining a constant value, the
heat transfer coefficient starts decreasing.
f. Mass transfer coefficient decreases with the increase of Brownian motion parameter,
thermophoresis parameter and after attaining a constant value atr=0, the mass
transfer coefficient starts increasing. However, mass transfer coefficientshows an
opposite behaviour with respect to amplitude ratio.
g. The volume of the trapped bolus increases with the increase of couple-stress fluid
parameterα and decreases with the increase of couple-stress fluid parameter η ,
Brownian motion parameter and with slip parameter.
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