删除或更新信息,请邮件至freekaoyan#163.com(#换成@)

Numerical Simulation of MHD Peristaltic Flow with Variable Electrical Conductivity and Joule Dissipa

本站小编 Free考研考试/2022-01-02

Muhammad Qasim,1, Zafar Ali1, Abderrahim Wakif2, Zoubair Boulahia2 Department of Mathematics, COMSATS University Islamabad (CUI), Park Road, Tarlai Kalan, Islamabad-455000,Pakistan
Laboratory of Mechanics, Faculty of Sciences A¨?n Chock, Hassan II University, B.P. 5366, M?aarif, Casablanca, Moroccoa

Corresponding authors: E-mail:mq qau@yahoo.com



Abstract
In this paper, the MHD peristaltic flow inside wavy walls of an asymmetric channel is investigated, where the walls of the channel are moving with peristaltic wave velocity along the channel length. During this investigation, the electrical conductivity both in Lorentz force and Joule heating is taken to be temperature dependent. Also, the long wavelength and low Reynolds number assumptions are utilized to reduce the governing partial differential equations into a set of coupled nonlinear ordinary differential equations. The new set of obtained equations is then numerically solved using the generalized differential quadrature method (GDQM). This is the first attempt to solve the nonlinear equations arising in the peristaltic flows using this method in combination with the Newton-Raphson technique. Moreover, in order to check the accuracy of the proposed numerical method,our results are compared with the results of built-in Mathematica command NDSolve. Taking Joule heating and viscous dissipation into account, the effects of various parameters appearing in the problem are used to discuss the fluid flow characteristics and heat transfer in the electrically conducting fluids graphically. In presence of variable electrical conductivity, velocity and temperature profiles are highly decreasing in nature when the intensity of the electrical conductivity parameter is strengthened.
Keywords: peristaltic flow;MHD;variable electrical conductivity;Joule dissipation;generalized differential quadrature method (GDQM)


PDF (5978KB)MetadataMetricsRelated articlesExportEndNote|Ris|BibtexFavorite
Cite this article
Muhammad Qasim, Zafar Ali, Abderrahim Wakif, Zoubair Boulahia. Numerical Simulation of MHD Peristaltic Flow with Variable Electrical Conductivity and Joule Dissipation Using Generalized Differential Quadrature Method. [J], 2019, 71(5): 509-518 doi:10.1088/0253-6102/71/5/509




Nomenclature

New window|CSV

1 Introduction

Study of peristaltic pumping of fluids has been the point of interest and motivation for researchers through many years. Peristalsis in practice is to push the material inside the tube-like structures when the progressive waves of area contraction and expansion are made to propagate along the tube's length. A wide range of applications of peristalsis is reported in medical and engineering science such as in physiology, the mechanism is used by the body to mix and drive the content inside the tube such as urine is pushed from kidney to bladder in ureter duct,[1] digestive system,[2] blood circulation in vessels, bile movement in a bile ducts, movement of food bolus, transport of ovum and cilia are a few applications. Similarly, the working of biomedical instruments such as a heart-lung machine (HLM) and blood pumps used in dialysis are also based on this principle. The same mechanism is also exploited in many industrial processes such as corrosive and toxic fluids are transported through roller and finger pumps.

Mathematical modeling and analysis of peristaltic transport were developed by Shapiro et al.[3] in wave frame and Fung and Yih[4] in the laboratory frame for the Newtonian fluids. Two-dimensional peristaltic means of transport was investigated numerically by Takabatake et al.[5] and Brown et al.[6] without using assumptions of long wavelength and low Reynolds number. Interaction of peristaltic transport and heat transfer has also acquired much attention due to their extensive use in industrial and clinical processes. Laser therapy, cryosurgery, oxygenation and hemodialysis require thermal modeling. Also, other processes like condensation, crystallization, evaporation are amongst the core applications of heat transfer. Radhakrishnamacharya and Srinivasulu[7] studied the peristaltic flow of viscous fluid in presence of wall properties and heat transfer. Mekheimer[8] combined the effects of MHD and heat transfer on wavy motion of viscous fluid in the vertical channel. Srinivas and Kothandapani[9] studied heat effects on the peristaltic motion of fluid through the asymmetric channel. Very recently, Mosayebidorcheh and Hatami[10-11] analytically investigated the heat transfer effects on the peristaltic flow of nanofluids in an asymmetric channel. Bhatti et al.[12] studied the peristaltic transport of two-phase fluid flow with heat and mass transfer in a porous channel.

Magnetohydrodynamics (MHD) refers to study the effects of the magnetic field when applied to the electrically conducting fluids in motion. MHD peristaltic motion fluids are of great importance because of its wide range of applications in geophysics, astrophysics, sensors, engineering and magnetic drug targeting in clinical science. Misra et al.[13] combined heat and MHD effects on the peristaltic motion of a fluid with varying physical and thermal properties in an asymmetric channel. Noreen and Saleem[14] studied MHD peristaltic motion in a porous medium under the Soret and Dufour effects with chemical reaction and thermal radiation. Reddy[15] analytically investigated the velocity slip and MHD effects on the peristaltic flow through a porous medium together with heat and mass transfer. Sud et al.[16] observed the effect of magnetic field on the blood flow and concluded that it increases the velocity of the blood. Akbar[17] investigated the MHD effects with nanoparticles on Eyring-Powell fluid model in peristaltic motion. Agrawal and Anwaruddin[18] studied different aspects of MHD blood flowing peristaltically in the equally branched channel, viewing its applications in cardiac operations and arterial stenosis. Abbasi et al.[19] also analyzed mathematically the effects of variable viscosity on peristaltic motion of MHD fluids with Soret and Dufour relations. Reddy et al.[20-21] conducted the study of peristaltic flow of an incompressible non-Newtonian fluid in presence of MHD and partial slip effects in asymmetric channel.

Influence of Joule heating on peristaltic flow of fluidswith constant electrical conductivity has been carried out by many researchers, such as Refs.[22-24] but none has related temperature dependent electrical conductivity with peristalsis as per authors' knowledge. In this paper, we propose a peristaltic flow model of Newtonian fluid with variable electrical conductivity. Assumptionsof long wavelength and low Reynolds number are used to simplify governing equations from laboratory frame to wave frame. Thus, resulting equations after simplification are solved numerically by utilizing Generalized Differential Quadrature Method (GDQM).[25-27] Results obtained by the aforementioned method for velocity profile, temperature profile, pressure rise and streamlines are analyzed graphically by giving different values to the appearing parameters in the flow phenomenon.

2 Mathematical Model

In an asymmetric arrangement of the channel of width $(d_{1}+d_{2})$, viscous type of electrically conducting fluid is assumed to be in peristaltic motion. The fluid is subject to a constant transverse magnetic field $B=\left( 0,B_{0},0\right)$. The lower and upper walls of the channel are assumed to be in $T_{1}$ and $T_{0}$ temperatures, respectively, where $T_{1}>T_{0}.$ Furthermore, the geometry of the wavy fluid walls is described by following sinusoidal function

$$ \bar{H}_{1}=d_{1}+a_{1}\cos \Bigl[ \frac{2\pi }{\lambda }( \bar{X}-c\bar{t}) \Bigr], $$
$$ \bar{H}_{1}=-d_{2}-a_{2}\cos \Bigl[ \frac{2\pi }{\lambda }( \bar{X}-c\bar{t}) +\phi \Bigr]. $$
Here $a_{1},a_{2},d_{1},d_{2}$ are constrained to criterion of inequality $% \left[ a_{1}^{2}+a_{2}^{2}+2a_{1}a_{2}\cos \phi \right] \leq \left(d_{1}+d_{2}\right) ^{2},$ in which $\phi $ is the phase difference between the upper and the lower wallsand $0\leq \phi \leq \pi .$ Also, the symmetry of the channel depends on $\phi$, where $\phi =0$ corresponds to a symmetric channel with waves out of phase and $\phi =\pi $ is taken for a symmetric channel with waves are in phase. Vector form of continuity,momentum and heat equations is:

$$ △\cdot{V}=\mathbf{0}\,,$$
$$ \frac{{\rm d}\mathbf{V}}{{\rm d}\bar{t}}=-\mathbf{\nabla }\bar{P}+\mu (\mathbf{\nabla }^{2}{V}) +{J}\times {B}\,,$$
$$ C_{p}\Bigl( \frac{{\rm d}T}{{\rm d}\bar{t}}\Bigr) =k( \mathbf{\nabla }^{2}T)+\mu ({S}\cdot{L}) +\frac{{J}\cdot{J}}{\bar{\sigma}( T) }\,,$$
where ${V}$ is the velocity field, ${\rm d}/{{\rm d}t}$ is the material derivative, ${L}=\nabla{V}$ is the gradient of velocity, ${S}={L}+{L}^{\rm T}$ and ${J}$ is the current density in absence of induced magnetic field, is defined as ${J}=\bar{\sigma}\left(T\right) \left[{V}\times {B}\right] .$ In the fixed frame, the governing Eqs. (3)-(5) become

$$ \frac{\partial \bar{U}}{\partial \bar{X}}+\frac{\partial \bar{V}}{\partial \bar{Y}}=0,$$
$$ \Bigl[ \frac{\partial \bar{U}}{\partial \bar{t}}+\bar{U}\frac{\partial \bar{U}}{\partial \bar{X}}+\bar{V}\frac{\partial \bar{U}}{\partial \bar{Y}}% \Bigr] =-\frac{\partial \bar{P}}{\partial \bar{X}}+\mu \Bigl[ \frac{% \partial ^{2}\bar{U}}{\partial \bar{X}^{2}}+\frac{\partial ^{2}\bar{U}}{% \partial \bar{Y}^{2}}\Bigr] -\bar{\sigma}\left( T\right) B_{0}^{2}\bar{U}, $$
$$ \rho \Bigl[ \frac{\partial \bar{V}}{\partial \bar{t}}+\bar{U}\frac{\partial \bar{V}}{\partial \bar{X}}+\bar{V}\frac{\partial \bar{V}}{\partial \bar{Y}} \Bigr] =-\frac{\partial \bar{P}}{\partial \bar{Y}}+\mu \Bigl[ \frac{% \partial ^{2}\bar{V}}{\partial \bar{X}^{2}}+\frac{\partial ^{2}\bar{V}}{ \partial \bar{Y}^{2}}\Bigr],$$
$$ \rho C_{p}\Bigl[ \frac{\partial T}{\partial \bar{t}}+\bar{U}\frac{\partial T}{\partial \bar{X}}+\bar{V}\frac{\partial T}{\partial \bar{Y}}\Bigr] =k \Bigl[\frac{\partial ^{2}T}{\partial \bar{X}^{2}}+\frac{\partial ^{2}T}{\partial \bar{Y}^{2}}\Bigr] +\mu \Phi +\bar{\sigma}\left(T\right) B_{0}^{2} \bar{U}^{2}.$$
Here, $k$ is the thermal conductivity, $\Phi $ is the viscous dissipation and $\bar{\sigma}\left( T\right) $ is the temperature dependent electrical conductivity, where

$$ \Phi =\Bigl( \frac{\partial \bar{U}}{\partial \bar{Y}}+\frac{\partial \bar{V}}{\partial \bar{X}}\Bigr) ^{2}+2\Bigl[ \Bigl( \frac{\partial \bar{U}}{ \partial \bar{X}}\Bigr) ^{2}+\Bigl( \frac{\partial \bar{V}}{\partial \bar{Y} }\Bigr) ^{2}\Bigr], $$
and $\bar{\sigma}\left( T\right) $ is the temperature dependent electrical conductivity, given by[28]

$$ \bar{\sigma}\left( T\right) =\sigma _{0}\left[ 1+\beta _{1}\left(T-T_{0}\right) \right]. $$
In order to reduce Eqs. (6)-(9) in a set of coupled ordinary differential equations; we introduce the following transformations and dimensionless variables and parameters as:

$$ \bar{U}\left(\bar{X},\bar{Y},\bar{t}\right) =\bar{u}\left(\bar{x},\bar{y}\right) +c\,,\quad \bar{V}\left(\bar{X},\bar{Y},\bar{t}\right) =\bar{v}\left(\bar{x},\bar{y}\right)\,,\bar{P}\left(\bar{X},\bar{Y},\bar{t}\right) =\bar{p} \left(\bar{x},\bar{y}\right)\,,T\left(\bar{X},\bar{Y},\bar{t}\right) =\bar{T}\left( \bar{x},\bar{y} \right)\,,\quad \bar{X}=\bar{x}+c\bar{t},\quad \bar{Y}=\bar{y}\,,$$
$$ \bar{x} =x\lambda,\quad \bar{y}=yd_{1},\quad \bar{u}=uc,\quad \bar{v}=vc\delta\,,=\left( c\lambda \mu /d_{1}^{2}\right) p,\quad \theta =\frac{\bar{T}-\bar{T}_{0}}{\bar{T}_{1}-\bar{T}_{0}}\,,\bar{\psi} =\psi /\left( cd_{1}\right)\,,\quad u=\partial \psi \partial y,\quad v=-\delta \partial \psi /\partial x\,,\;\;\beta =\beta _{1}\left( \bar{T}_{1}-\bar{T}_{0}\right),\quad \delta =d_{1}/\lambda \,, \ \ h_{1} =\bar{H}_{1}/d_{1},\quad h_{2}=\bar{H}_{2}/d_{1},\quad d=d_{2}/d_{1},\;\;b=a_{2}/d_{1},\quad {Re}=\rho cd_{1}/\mu \,,\;\;M =B_{0}d_{1}\sqrt{\sigma _{0}/\mu },\quad Br=\mu c^{2}/\left[ k\left( \bar{T}_{1}-\bar{T}_{0}\right) \right]\,.$$
Finally, after considering the assumptions of long wave length $\delta $ (i.e. $\delta \ll 1$) and low Reynolds number ${Re}$ (i.e., ${Re}% \ll 1$) we get,

$$ \quad \frac{\partial p}{\partial x}=\frac{\partial ^{3}\psi }{\partial y^{3}}-M^{2}\Bigl( \frac{\partial \psi}{\partial y}+1\Bigr) \left( \beta \theta +1\right), $$
$$\ quad\frac{\partial p}{\partial y}=0, $$
$$ \quad\frac{\partial ^{2}\theta }{\partial y^{2}}+Br\Bigl( \frac{\partial ^{2}\psi }{\partial y^{2}}\Bigr) ^{2}+BrM^{2}\Bigl( \frac{\partial \psi }{\partial y}+1\Bigr) ^{2}\left( \beta \theta +1\right). $$
From Eq. (15) the pressure $p$ depends only on $x$ alone, hence, the pressure gradient can be eliminated from Eq. (14) for giving the reducing equation

$$ \frac{\partial ^{4}\psi }{\partial y^{4}}-M^{2}\frac{\partial }{\partial y} \Bigl[ \Bigl( \frac{\partial \psi }{\partial y}+1\Bigr) \left( \beta \theta +1\right) \Bigr] =0. $$
In dimensionless form, the associated boundary conditions are defined as

$$ \psi =-F/2,\text{ }\frac{\partial \psi }{\partial y}=-1,\text{ }\theta =1\text{ at }y=h_{2}, \nonumber \psi =+F/2,\text{ }\frac{\partial \psi }{\partial y}=-1,\text{} \theta =0\text{ at }y=h_{1}\,.$$
Here, $h_{2}\leq y\leq h_{1},$ where $h_{1}=1+a\cos \left( 2\pi x\right) $ and $h_{2}=-d-b\cos \left( 2\pi x+\phi \right) .$

In a fixed frame, the instantaneous volume flow rate is given by

$$ \bar{Q}=\int_{\bar{H}_{2}}^{\bar{H}_{1}}\bar{U}\left( \bar{X},\bar{Y},\bar{t} \right) {\rm d}\bar{Y}, $$
in which the limits of integration $H_{1}$ and $H_{2}$ are functions of $%\bar{X}$ and $\bar{t}.$

In view of Eq. (19), we define the volumetric flow rate in a wave frame as

$$ q=\int_{\bar{h}_{2}}^{\bar{h}_{1}}\bar{u}\left( \bar{x},\bar{y}\right) {\rm d}\bar{y}, $$
since $\bar{h}_{1}$ and $\bar{h}_{2}$ depend only on $\bar{x}$, then

$$ \bar{Q}=q+c\left( \bar{h}_{1}-\bar{h}_{2}\right). $$
The time averaged flow over a period $T$ at a fixed position $\bar{X}$ is defined as

$$ Q^{\ast }=\frac{1}{T}\int_{0}^{T}\bar{Q}{\rm dt}. $$
Making use of Eq. (21) in Eq. (22), we obtain

$$ Q^{\ast }=q+c\left( d_{1}+d_{2}\right). $$
For the present problem, the dimensionless time-mean flows $Q$ and $F$ in the fixed and wavy frame are defined respectively as

$$ Q=\frac{Q^{\ast }}{cd_{1}},$$
$$ F=\frac{q}{cd_{1}}.$$
Hence, we can write the following relationship%

$$ Q=F+1+d. $$
As shown in Fig. 1, the irregular physical domain $\left[ h_{2}, h_{1}\right] $ considered in this investigation can be mapped into the computational domain $\left[ 0,1\right] $ by considering the following transformations%

$$ x=f^{\ast }( \xi ),~~~y=g^{\ast }( \xi ,\eta ),~~~h_{1}( x) =h_{1}( f^{\ast }( \xi ) )=h_{1}^{\ast }( \xi ),\;\;h_{2}( x) =h_{2}( f^{\ast }( \xi ) )=h_{2}^{\ast }( \xi ),\quad \psi ( x,y)=\psi ( f^{\ast }( \xi ),\;\;g^{\ast}( \xi ,\eta ) ) =\psi ^{\ast }( \xi,\eta ),\quad \theta ( x,y) =\theta ( f^{\ast }( \xi ),\;\;g^{\ast}( \xi ,\eta ) ) =\theta ^{\ast }( \xi,\eta ). $$
Here

$$ f^{\ast }\left( \xi \right) =\xi, \quad g^{\ast }\left( \xi ,\eta \right) =\Delta \left( \xi \right) \eta+h_{2}^{\ast }, \quad \Delta \left( \xi \right) =h_{1}^{\ast }-h_{2}^{\ast },\dfrac{\partial ^{m}\psi ^{\ast }}{\partial y^{m}}=\dfrac{1}{\Delta ^{m}}\dfrac{\partial ^{m}\psi ^{\ast }}{\partial \eta ^{m}},\quad\dfrac{\partial ^{m}\theta ^{\ast }}{\partial y^{m}}=\dfrac{1}{\Delta ^{m}} \dfrac{\partial ^{m}\theta ^{\ast }}{\partial \eta ^{m}}, $$
where $m$ denotes the order of the partial derivative.

New window|Download| PPT slide
Fig.1Streamlines mapped into (a) the physical domain $(x,y)$ and (b) the computational domain $\left( \xi, \eta \right) $ when $a=0.5,$ $% b=0.5,$ $d=1,$ $Q=1.5,$ $\phi =\pi /3, $ $M=0.9, Br=0.3$, and $\beta =0.4$.



Consequently, for each cross-section of the geometry, the resulting dimensionless Eqs.(16) and (17) can be written in the form

$$ \qquad\quad L_{\psi ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) +N_{\psi ^{\ast}}\left( \psi ^{\ast },\theta ^{\ast }\right) =0,$$
$$ \qquad\quad L_{\theta ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) +N_{\theta^{\ast }}\left(\psi ^{\ast },\theta ^{\ast }\right) +BrM^{2}=0,$$
in which the linear and nonlinear parts $L_{\psi ^{\ast }}, L_{\theta ^{\ast}}, N_{\psi ^{\ast }}$, and $N_{\theta ^{\ast }}$ are given by

$$ L_{\psi ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) =\frac{1}{\Delta ^{4}}\frac{\partial ^{4}\psi ^{\ast }}{\partial \eta ^{4}}-\frac{M^{2}}{\Delta ^{2}}\frac{\partial ^{2}\psi ^{\ast }}{\partial \eta ^{2}}-\frac{\beta M^{2}}{\Delta }\frac{\partial \theta ^{\ast }}{\partial \eta }, $$
$$ L_{\theta ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) =\frac{1}{\Delta ^{2}}\frac{\partial ^{2}\theta ^{\ast }}{\partial \eta ^{2}}+Br\beta M^{2}\theta ^{\ast }+\frac{2BrM^{2}}{\Delta }\frac{\partial \psi ^{\ast }}{\partial \eta }, $$
$$ N_{\psi ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) =-\frac{\beta M^{2}}{\Delta ^{2}}\frac{\partial \psi ^{\ast }}{\partial \eta }\frac{\partial \theta ^{\ast }}{\partial \eta }-\frac{\beta M^{2}}{\Delta ^{2}} \frac{\partial ^{2}\psi ^{\ast }}{\partial \eta ^{2}}\theta ^{\ast }, $$
$$ N_{\theta ^{\ast }}\left( \psi ^{\ast },\theta ^{\ast }\right) =\frac{Br}{\Delta ^{4}}\left( \frac{\partial ^{2}\psi ^{\ast }}{\partial \eta ^{2}} \right) ^{2}+\frac{BrM^{2}}{\Delta ^{2}}\Bigl( \frac{\partial \psi ^{\ast }}{\partial \eta }\Bigr) ^{2} +\frac{2Br\beta M^{2}}{\Delta }\frac{\partial \psi ^{\ast }}{\partial \eta }\theta ^{\ast } +\frac{Br\beta M^{2}}{\Delta ^{2}}\Bigl( \frac{\partial \psi ^{\ast }}{\partial \eta }\Bigr) ^{2}\theta^{\ast }, $$
and the modified boundary conditions take the following form

$$ \psi ^{\ast }=-F/2,\text{}\frac{\partial \psi ^{\ast }}{\partial \eta }=-\Delta ,\text{}\theta ^{\ast }=1\text{ at}\eta =0\,, \\\psi ^{\ast }=+F/2,\text{ }\frac{\partial \psi ^{\ast }}{\partial \eta }=-\Delta ,\text{ }\theta ^{\ast }=0\text{ at }\eta =1\,.$$
As mentioned above, we can express the longitudinal pressure gradient as follows

$$ \frac{{\rm d}p^{\ast }}{{\rm d}\xi }= \frac{1}{\Delta^{3}}\left. \frac{\partial^{3}\psi^{\ast }} {\partial \eta ^{3}}\right\vert _{\eta =0}-\frac{M^{2}}{\Delta }\left. \frac{\partial \psi ^{\ast }}{\partial \eta }\right\vert _{\eta=0} \\ -\beta M^{2}\theta ^{\ast }\left( \xi ,0\right) -M^{2}\,.$$
Here $p^{\ast }$ is the transformed pressure, where $p^{\ast }=p\left(f^{\ast }\left( \xi \right) \right).$

3 Solution Methodology and Validation

For solving the obtained coupled system of nonlinear partial differential equations described by Eqs. (29) and (30) and the boundary conditions (35), the generalized differential quadrature method (GDQM) is used during in this investigation as a powerful method to find out the numerical results by computing the $m^{\rm th}$-order partial derivatives with respect to $\eta $ of both $\psi ^{\ast }\left( \xi ,\eta \right) $ and $\theta ^{\ast }\left( \xi ,\eta \right) .$ Following this approach, the partial derivatives of $\psi ^{\ast }\left( \xi ,\eta \right) $ and $\theta ^{\ast }\left( \xi ,\eta \right) $ with respect to space variable $\eta $ at a given discrete point $% \eta _{i}$ can be written as follows

$$ \left.\frac{\partial^{m}\psi^{\ast}}{\partial \eta^{m}} \right\vert_{\eta=\eta_{i}}=\mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(m)}\psi^{\ast}(\xi,\eta_{i})\,, $$
$$ \left.\frac{\partial ^{m}\theta^{\ast }}{\partial \eta ^{m}}\right\vert_{\eta=\eta_{i}}=\mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(m)}\theta^{\ast}(\xi, \eta_{i})\,.$$
Here, $d_{ij}^{(m)}$ are the weighting coefficients for the $m^{\rm th}$-order derivative and $N$ is the total number of sampling points of the grid distribution in the transversal direction, where $i$ and $j$ are integers varying from $1$ to $N.$ According to Shu,[25] the weighting coefficients for the first-order derivative discretization with arbitrary distribution of grid points are expressed as follows

$$ d_{ij}^{(1)}=\prod\limits^{N}_{k=1,k\neq i}\left( \eta _{i}-\eta _{k}\right)/[ \left( \eta _{i}-\eta _{j}\right) \prod\limits^{N}_{k=1,k\neq j}\left( \eta _{j}-\eta _{k}\right)], $$
for $i\neq j$ and

$$ d_{ij}^{(1)}=-\sum_{{j=1,~j\neq i}}^{N}d_{ij}^{(1)},$$
for $i=j,$ where $i=1,2,3,\ldots,N.$

Similarly, the weighting coefficients of the second and higher-order derivatives can be calculated from those of the first-order derivative by the following recurrence relations

$$ d_{ij}^{(m)}=m\Bigl( d_{ii}^{(m-1)}d_{ij}^{(1)}-\frac{d_{ij}^{(m-1)}}{\eta_{i}-\eta _{j}}\Bigr),$$
for $i\neq j$ and

$$ d_{ij}^{(m)}=-\sum\limits_{{j=1,j\neq i}}^{N}d_{ij}^{(m)},$$
for $i=j,$ where $i=1,2,\ldots,N.$

In order to obtain accurate results using a few numbers of grid points $N$, it is more useful to choose the Chebyshev-Gauss-Lobatto grid points, which are greatlydenser close to the boundaries and their co-ordinates constitute the roots of the Chebyshev polynomial. These collocation points can be written in the form

$$ \eta _{i}=\frac{1}{2}\Bigl\{ 1-\cos \Bigl[ \Bigl( \frac{i-1}{N-1}\Bigr) \pi % \Bigr] \Bigr\} ,$$
where $i=1,2,\ldots,N$ and $0\leq \eta _{i}\leq 1.$ Under the above consideration, the dimensionless functions $\psi ^{\ast}\left( \xi ,\eta \right) $ and $\theta ^{\ast }\left( \xi ,\eta \right) $ are approximated in each collocation point $\eta _{i}$ by $\psi _{i}^{\ast}\left( \xi \right) $ and $\theta _{i}^{\ast }\left( \xi \right) ,$ respectively. Hence, after discretizing the transformed problem with some rearrangements, Eqs. (29) and (30) together with the boundary conditions (35) are simplified as

$$ \left( S\right):\cases\psi _{i}^{\ast }\left( \xi \right) + {F}/{2}=0\,, \quad\mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(1)}\psi _{j}^{\ast }\left( \xi\right) +\Delta =0\,,L_{\psi _{i}^{\ast }}\left( \psi _{i}^{\ast }\left( \xi \right),\theta_{i}^{\ast }\left( \xi \right) \right) +N_{\psi _{i}^{\ast }}\left( \psi_{i}^{\ast }\left( \xi \right),\theta _{i}^{\ast }\left( \xi \right)\right)=0\,,\hfill\cr\quad 3\leq i\leq N-2\,,\hfill\cr\mathop\sum\limits^{N}_{{j=1}}d_{Nj}^{(1)}\psi _{j}^{\ast }\left( \xi\right) +\Delta =0\,, \quad\psi _{N}^{\ast }\left( \xi \right) - {F}/{2}=0\,,\hfill\cr\theta _{i}^{\ast }\left( \xi \right) -1=0\,,L_{\theta _{i}^{\ast }}\left( \psi _{i}^{\ast }\left( \xi \right),\theta_{i}^{\ast }\left( \xi \right) \right) +N_{\theta _{i}^{\ast }}\left( \psi_{i}^{\ast }\left( \xi \right),\theta _{i}^{\ast }\left( \xi \right)\right)\hfill\cr +\,BrM^{2}=0,\quad 2\leq i\leq N-1,\hfill\cr\theta _{N}^{\ast }\left( \xi \right) =0\,,}$$
where

$$ L_{\psi _{i}^{\ast }}\left( \psi _{i}^{\ast },\theta _{i}^{\ast }\right) =\frac{1}{\Delta ^{4}}\mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(4)}\psi _{j}^{\ast }-\frac{M^{2}}{\Delta ^{2}}\mathop\sum\limits^{N}_{{j=1}} d_{ij}^{(2)}\psi _{j}^{\ast } -\frac{\beta M^{2}}{\Delta } \mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(1)}\theta _{j}^{\ast },$$
$$ L_{\theta _{i}^{\ast }}\left( \psi _{i}^{\ast },\theta _{i}^{\ast }\right) = \frac{1}{\Delta ^{2}}\mathop\sum\limits^{N}_{{j=1} }d_{ij}^{(2)}\theta_{j}^{\ast }+Br\beta M^{2}\theta _{i}^{\ast }+\frac{2BrM^{2}}{\Delta } \mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(1)}\psi _{j}^{\ast },$$
$$ N_{\psi _{i}^{\ast }}\left( \psi _{i}^{\ast },\theta _{i}^{\ast }\right) =-\frac{\beta M^{2}}{\Delta ^{2}}\Bigl( \mathop\sum\limits^{N}_{{j=1}}%d_{ij}^{(1)}\psi _{j}^{\ast }\Bigr) \Bigl( \mathop\sum\limits^{N}_{{j=1}%}d_{ij}^{(1)}\theta _{j}^{\ast }\Bigr)-\frac{\beta M^{2}}{\Delta ^{2}} \Bigl( \mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(2)}\psi _{j}^{\ast}\Bigr) \theta _{i}^{\ast }\,,$$
$$ N_{\theta _{i}^{\ast }}\left( \psi _{i}^{\ast },\theta _{i}^{\ast }\right)=\frac{Br}{\Delta ^{4}}\Bigl( \mathop\sum\limits^{N}_{{j=1}} d_{ij}^{(2)}\psi _{j}^{\ast }\Bigr) ^{2} \! \!+\frac{BrM^{2}}{\Delta ^{2}}\Bigl(\mathop\sum\limits^{N}_{{j=1}}d_{ij}^{(1)}\psi _{j}^{\ast }\Bigr) ^{2}\!+\!\frac{2Br\beta M^{2}}{\Delta }\Bigl( \mathop\sum\limits^{N}_{{j=1}} d_{ij}^{(1)}\psi _{j}^{\ast }\Bigr) \theta _{i}^{\ast }+\frac{Br\beta M^{2}}{\Delta ^{2}}\Bigl( \mathop\sum\limits^{N}_{{j=1}} d_{ij}^{(1)}\psi _{j}^{\ast }\Bigr) ^{2}\theta _{i}^{\ast }.$$
$$ \frac{{\rm d}p^{\ast }}{{\rm d}\xi }=\frac{1}{\Delta ^{3}}\mathop\sum\limits^{N}_{{j=1}}d_{1j}^{(3)}\psi _{j}^{\ast }-\frac{M^{2}}{\Delta }\mathop\sum\limits^{N}_{{j=1}{ }}d_{1j}^{(1)} \psi _{j}^{\ast }-\beta M^{2}\theta_{1}^{\ast }-\frac{\beta M^{2}}{\Delta }\Bigl( \mathop\sum\limits^{N}_{{j=1}}d_{1j}^{(1)}\psi _{j}^{\ast }\Bigr) \theta _{1}^{\ast }-M^{2}\,.$$
As shown above, the numerical procedure used in this investigation leads to a nonlinear system $\left( S\right) $ constituted by $2N$ algebraic equations, which can then be solved using an algorithm based on the Newton-Raphson technique.

To validate our numerical computations and test the efficiency of the proposed method, several tabular and graphical comparisons are carried out, in order to obtain a reliable physical prediction. In Tables 1 and 2, we present a comparison of the engineering quantities $\psi _{y}^{\left( 2\right) }\left( x,h_{2}\right) ,$ $\psi _{y}^{\left( 2\right) }\left( x,h_{1}\right) ,$ $\theta _{y}^{\left( 1\right) }\left( x,h_{2}\right) $, and $\theta _{y}^{\left( 1\right) }\left( x,h_{1}\right) $ obtained by the help of the Mathematica's NDSolve function and the generalized differential quadrature method (GDQM), for various parametric values $M,$ $Br$ and $% \beta ,$ when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1$, and $\phi =\pi /3.$ As expected, it is found an excellent agreement in term of the absolute accuracy of the order of $10^{-6}$ between both methods, when we choose $N=50 $ as the number of collocation points. Hence, the tabular results confirm the validity of our numerical code and the effectiveness of the generalized differential quadrature method (GDQM). More, comparison of present results with the existing study is presented in Table 3. The obtained results are found to be in an excellent agreement.

Tab. 1


Tab. 1Comparison between our numerical results and those given by software for $\psi _{y}^{2}\left( x,h_{2}\right) $ and $\psi _{y}^{2}\left( x,h_{1}\right) $ in the case where $% a=0.5,b=0.5,d=1,Q=1.5,x=0.1$ and $\phi =\pi /3.$

New window|CSV

Tab. 2


Tab. 2Comparison between our numerical results and those given by software for $\theta _{y}^{1}\left( x,h_{2}\right) $ and $% \theta _{y}^{1}\left( x,h_{1}\right) $ in the case where $% a=0.5,b=0.5,d=1,Q=1.5,x=0.1$ and $\phi =\pi /3.$

New window|CSV

Tab. 3


Tab. 3Comparison between our numerical results and the results of Srinivas and Kothandapani[29] for the ideal heat transfer coefficient $% Z=h_{1}^{(1)}\theta _{y}^{(1)}\left( x,h_{1}\right) $ in the case where $% \beta =0,b=0.6,d=1.5$ and $\phi =\pi /4.$

New window|CSV

4 Results and Discussions

This section is devoted to analyze and discuss the behavior of velocity profile $u\left( x,y\right),$ temperature profile $\theta \left(x,y\right)$, pressure gradient ${\rm d}p/{\rm d}x$ and streamlines on varying the dominating physical parameters appearing in the flow problem like Hartmann number $M,$ electrical conductivity parameter $\beta,$ and Brinkman number $Br.$ In Fig.2 velocity profiles $u$ are plotted for various values of Hartmann number $M$. It is obvious to note that velocity profile $u$ is decreasing centrally but increasing slightly near the walls of channel when Hartmann number $M$ is steadily increased. This happens because, the magnetic field interacts with the electrically conducting fluid and generate a Lorentz force which is opposite in the direction of fluid flow and therefore, the fluid velocity decreases. Since the electrical conductivity parameter $\beta $ appears due to the Lorentz force in momentum equation, it might affect in the same way as does the Hartmann number $M$. Its effect on velocity profile $u$ is exhibited in Fig.3, wherein velocity profile $u$ is seen to be weakened on strengthening the intensity of electrical conductivity.

New window|Download| PPT slide
Fig.2Velocity profile $u\left( x,y\right) $ for different values of Hartmann number $M$, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $ \phi =\pi /3,$ $Br=0.3$, and $\beta =0.4.$



New window|Download| PPT slide
Fig.3Velocity profile $u\left( x,y\right) $ for different values of electrical conductivity parameter $\beta $, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.3$, and $M=0.8.$



New window|Download| PPT slide
Fig.4Temperature profile $\theta \left( x,y\right) $ for different values of Hartmann number $M$, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.3$, and $\beta =0.4.$



Figure 4 presents the analysis of temperature profile $\theta $ against the increasing values of Hartmann number $M$. Physically, increasing values of decelerate the fluid flow consequently the friction between the fluid layers increases and generates frictional heating, which enhances the temperature. It is noticed that down the stream temperature is decreasing because of increasing values of Hartmann number $M$. Similar effects on temperature profile $\theta $ are observed in case of increasing electrical conductivity parameter $\beta $, shown in Fig.5. Brinkman number $Br$ appears in heat equation due the dissipation term. In the flow process kinetic energy is converted into heat energy due to viscous dissipation and increasing Brinkman number $Br$ is same as to increase the heat energy. Thus Fig.6 follows the trend of increasing temperature on increasing the values of Brinkman number $Br$.

Figure 7 is drawn to study the effects of Hartmann number $M$ on pressure gradient. Here pressure gradient may be classified as the adverse pressure gradient and favorable pressure gradient on being positive and negative respectively. From this figure we note that pressure gradient is increasing in the domain $[-0.4,0]$ and $[0.4,1.0]$ while decreasing in $[-1.0,-0.4]$ and $[0,0.4].$ Overall pressure gradient is decreasing in magnitude on the increase in Hartmann number $M$.

New window|Download| PPT slide
Fig.5Temperature profile $\theta \left( x,y\right) $ for different values of electrical conductivity parameter $\beta $, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.3$, and $M=0.8.$



New window|Download| PPT slide
Fig.6Temperature profile $\theta \left( x,y\right) $ for different values of Brinkman number $Br$, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $\beta =0.3$, and $M=0.6.$



New window|Download| PPT slide
Fig.7Variation of pressure gradient ${\rm d}p/{\rm d}x$ for different values of Hartmann number $M$, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $ \phi =\pi /3,$ $Br=0.3$, and $\beta =0.4.$



New window|Download| PPT slide
Fig.8Variation of pressure gradient ${\rm d}p/{\rm d}x$ for different values of electrical conductivity parameter $\beta $, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.4$, and $\beta =0.8.$



Figure 8 shows the behavior of pressure gradient when electrical conductivity parameter $\beta $ is given boost. It is noticeable that strengthening the intensity of electrical conductivity, the same effects of decreasing pressure gradient are observed.Since the electrical conductivity parameter $\beta $ contributes in Lorentz force and Joule heating so its effects might be the same as to that of magnetic number and Joule heating parameter.The phenomenon of trapping in peristalsis is the split of streamlines and formation of a bolus when the fluid is moving in wave frame. Figures 9 and 10 are exhibited to observe the effects of Hartmann number $M$ and electrical conductivity parameter $\beta $ respectively. In both figures volume of trapped bolus is observed to be decreasing subsequently on increasing the Hartmann number $M$ and electrical conductivity parameter $\beta $. Initially bolus is seen to be formed centrally in the absence of magnetic field and electrical conductivity. Gradually strengthening both the factors,trapped bolus is seen to shift to upward boundary of the channel and eventually disappears on increasing Hartmann number $M$ and electrical conductivity parameter $\beta$.

New window|Download| PPT slide
Fig.9Streamlines for different values of Hartmann number $M$,when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.3$, and $\beta =0.4.$



New window|Download| PPT slide
Fig.10Streamlines for different values of electrical conductivity parameter $\beta $, when $a=0.5,$ $b=0.5,$ $d=1,$ $Q=1.5,$ $x=0.1,$ $\phi =\pi /3,$ $Br=0.4$, and $M=0.8.$




Reference By original order
By published year
By cited within times
By Impact factor

F.C Yin . and Y. C .Fung , Am. J. Physiol. Content. 221(1971) 1484.
[Cited within: 1]

J. G. Brasseur, S. Corrsin, N. Q. Lu, J. Fluid Mech . 174(1987) 495.
[Cited within: 1]

A. H. Shapiro, M. Y. Jaffrin, S. L. Weinberg, J. Fluid Mech . 37(1969) 799.
[Cited within: 1]

Y.C Fung .and C. S .Yih , J. Appl. Mech. 35(1968) 669.
[Cited within: 1]

S. Takabatake and K. Ayukawa, J. Fluid Mech. 122(1982) 439.
[Cited within: 1]

T.D Brown . and T. K. Hung, J. Fluid Mech. 83(1977) 249.
[Cited within: 1]

G. Radhakrishnamacharya and C. Srinivasulu , Comptes Rendus Mec. 335(2007) 369.
[Cited within: 1]

S. Mekheimer , Phys. Lett. A 372 ( 2008) 1657.
[Cited within: 1]

S. Srinivas and M. Kothandapani , Int. Commun. Heat Mass Transf. 35(2008) 514.
[Cited within: 1]

S. Mosayebidorcheh and M. Hatami , Int. J. Heat Mass Transf. 126(2018) 790.
[Cited within: 1]

S. Mosayebidorcheh and M. Hatami Int. J. Heat Mass Transf. 126(2018) 800.
[Cited within: 1]

M. M. Bhatti, A. Zeeshan, R. Ellahi, G. C. Shit , Adv.Powder Technol. 29(2018) 1189.
[Cited within: 1]

J. C. Misra, B. Mallick, A. Sinha , Alex. Eng. J. 57(2018) 391.
[Cited within: 1]

S. Noreen and M.Saleem, Heat Transf. Res. 47(2016) 1.
[Cited within: 1]

M. G. Reddy , Alex. Eng. J. 55(2016) 1225.
[Cited within: 1]

V. K. Sud, G. S. Sekhon, R. K. Mishra , Bull. Math. Biol. 39(1977) 385.
[Cited within: 1]

N. S. Akbar, J. Comput. Theor . Nanosci. 12(2015) 94.
[Cited within: 1]

H. L . Agrawal and B. Anwaruddin, Ranchi Univ.Math. J. 15(1984) 111.
[Cited within: 1]

F. M. Abbasi, T. Hayat, A. Alsaedi, B. Ahmed , Appl.Math. Inf. Sci. 8(2014) 211.
[Cited within: 1]

M. G. Reddy, K. V. Reddy, O. D. Makinde , Int. J. Appl. Comput. Math. 3(2017) 3201, DOI 10.1007/s40819-016-0293-1.
[Cited within: 1]

M. G . Reddyand O. D .Makinde , J. Mol. Liq. 223(2016) 1242.
[Cited within: 1]

N. K. Ranjit, G. C. Shit, D. Tripathi , Microvasc. Res. 117(2018) 74.
[Cited within: 1]

T. Hayat, S. Ayub, A. Tanveer, A. Alsaedi, J. Therm. Sci . Eng. Appl. 10(2018) 1.


M. G. Reddy and K. V. Reddy , Procedia Engineering 127( 2015) 1002.
[Cited within: 1]

C. Shu, Differential Quadrature and Its Application in Engineering, Springer Science Business Media , London ( 2012).
[Cited within: 2]

M. Fidanoglu, E. Baskaya, G. Komurgoz, I. Ozkol , ASME 2014 12th Bienn
Conf. Eng. Syst. Des. Anal.( 2014) 1.



E. Baskaya, G. Komurgoz, I. Ozkol , Entropy. 19(2017) 1.
[Cited within: 1]

H. A. Attia , Arch. Appl. Mech. 75(2006) 268.
[Cited within: 1]

S. Srinivas and M .Kothandapani , Int. Commun. Heat Mass Transfer. 35(2008) 514.
[Cited within: 1]

相关话题/Numerical Simulation Peristaltic