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The flow has been made by considering variable temperature and radiation effects for the magnetohydrodynamic viscoelastic fluid past a moving vertical plate in a porous medium. Chemical reaction and concentration have been taken into account. The governed mathematical statement is handled analytically by perturbation technique. The main view of this research is to investigate the effects of parameters and numbers in the problem on fluid flow, thermal boundary and concentration profiles. The velocity profile has been reduced by increasing the magnetic parameter due to the Lorentz force in the opposite direction of flow. Temperature profile is increased by rising thermal radiation and concentration distribution is decreased by enhancing the chemical reaction and Schmidt number. The Schmidt number represents the relative ease of the molecular momentum and mass transfer and it is very important in multiphase flows. The effect of increasing values of the Schmidt number is to reduce the momentum boundary layer and this leads to the thinning of the diffusion layer. Furthermore, at the end of this paper the effects of different parameters on skin friction coefficient and local Nusselt number are investigated.
Viscoelastic, MHD, porous media, heat sink, radiation, chemical reaction
Convection is of fundamental interest in numerous engineering, industrial, and environmental applications such as cooling of electronic devices, airconditioning systems, atmospheric flows, and security of energy systems and in designs related to thermal insulation. Flow, of combined thermal and mass transfer in a porous media has several industrial applications such as filtration process and powerengineering equipment such as cooling of electronic devices, microelectronic chips, printed circuit boards and photovoltaic sheets. It is also important in various engineering and geophysical problems. In numerous engineering and technological applications, importance of nonNewtonian fluids cannot be negated. Examples of these materials may include shampoos, mayonnaise, blood, paints, alcoholic beverages, yogurt, cosmetics, and syrups etc. Mathematical modelling of these fluids is very tedious as typical NavierStokes equations are not enough to express characteristics of nonNewtonian fluids. These fluids are categories as differential, rate and integral types. Viscoelastic fluids are subclasses of nonNewtonian fluids which possess memory effect. These fluids exhibit certain amount of energy which is responsible for the partial elastic recovery upon the removal of stress. Beard and Walters [1] first perceived the boundary layer analysis of idealized viscoelastic fluid. Natural convection flow between two vertical parallel plates was proposed by Singh et al. [2]. Sajid et al. [3] developed a fully mixed convection flow between two permeable vertical walls in viscoelastic. The importance of viscoelastic fluid flow in presence of different parameters have studied by many authors [414]. Radiative dissipative MHD natural convection flow under the influence of heat source and sink was derived by Suneetha et al. [15].
The effect of thermal radiation becomes significant for several industrial processes such as glass production, furnace design, electrical power generation and solar power technology. A good working knowledge of thermal radiation helps in designing of important equipments such as design of fins, ceramic and glass producing units and various propulsion devices for aircraft, missiles, satellites, space vehicles etc. Keeping in mind such importance, Chemical reaction is notable in several procedures like chemical processing, hydrometallurgical industry, fibrous insulation, atmospheric flows, damage of crops because of freezing, water and air pollutions, production of ceramics and polymer, fog formation and dispersion etc. Reddy et al. [16] studied the proposed the magnetohydrodynamic free convection flow behaviour in a porous medium with constant heat and mass flux under thermal radiation and chemical reaction. Ahmed [17] and Sandeep et al. [18] observed the nature of chemically reactive flow over a vertical plate under different background.
In certain fluid applications, working fluid heat source or sink effects are important. Sample studies dealing with these effects have been reported by many authors. In recent past, great care has been taken to audit the repercussion of chemical reaction and heat source (or sink) on different flow types [1923]. The grasp on this subject assist to reconcile abundant biological problems. Considering the model of viscoelastic fluid, many scientists have solved problems of engineering interests viz. In the last few years, many investigations [2438], have been carried out regarding the present work.
In the light of the above studies, the objective of the current investigation is to prove the influence of heat generation or absorption and first order chemical reaction effects on laminar boundary layer flow through porous medium with thermal radiation, variable temperature and concentration. The dimensionless equations are then solved analytically using perturbation technique. The behaviors of different parameters on the physical quantities have been examined.
A twodimensional unsteady MHD flow of an incompressible electrically conducting fluid over a semiinfinite vertical permeable moving plate permeable stretching surface in presence of thermal radiation is considered. The system of coordinate is taken in way that xaxis is measured along the sheet and yaxis is orthogonal to it as presented in Figure 1. Induced magnetic field is negligible as compared to the applied magnetic field. We assume that the equations are subjected to viscoelastic fluid flow proposed by Babu et al. [39]. In the absence of the gradient of pressure, the governing equations expressing conservation of mass, momentum, energy and species are given as follows:
Figure 1. Physical model of the problem
$\frac{\partial v^{*}}{\partial y^{*}}=0$ (1)
$\frac{\partial u^{*}}{\partial y^{*}}+v^{*} \frac{\partial u^{*}}{\partial y^{*}}=v \frac{\partial^{2} u^{*}}{\partial y^{* 2}}\left(\frac{\sigma B_{0}^{2}}{\rho}+\frac{v}{K^{*}}\right) u^{*}+g \beta_{T}\left(T^{*}T_{\infty}\right)$$+g \beta_{C}\left(C^{*}C_{\infty}\right)k_{0}\left(\frac{\partial^{3} u^{*}}{\partial t^{*} \partial y^{* 2}}+v^{*} \frac{\partial^{3} u^{*}}{\partial y^{* 3}}\right)$ (2)
$\frac{\partial T^{*}}{\partial t^{*}}+v^{*} \frac{\partial T^{*}}{\partial y^{*}}=\frac{k}{\rho C_{p}} \frac{\partial^{2} T^{*}}{\partial y^{*^{2}}}\frac{1}{\rho C_{p}} \frac{\partial q_{r}^{*}}{\partial y^{*}}\frac{Q_{0}}{\rho C_{p}}\left(T^{*}T_{\infty}\right)$ (3)
$\frac{\partial C^{*}}{\partial t^{*}}+v^{*} \frac{\partial C^{*}}{\partial y^{*}}=D \frac{\partial^{2} C^{*}}{\partial y^{*^{2}}}k_{1}\left(C^{*}C_{\infty}\right)$ (4)
The boundary conditions for the above described model
$u^{*}=u_{p^{*}}, T^{*}=T_{w}+\varepsilon\left(T_{w}T_{\infty}\right) e^{n t^{*}}$,
$C^{*}=C_{w}+\varepsilon\left(C_{w}C_{\infty}\right) e^{n^{*} t^{*}},$ at $y^{*}=0$
$u^{*}=0, T^{*} \rightarrow T_{\infty}, C^{*} \rightarrow C_{\infty}$ at $y^{*} \rightarrow \infty$ (5)
It is unambiguous that Eq. (1) that the velocity of suction at the surface plate is time function. Presuming it yields into the form:
$v^{*}=V_{0}\left(1+\varepsilon A e^{n^{*} t^{*}}\right)$ (6)
$\varepsilon$ and $A$ are small such that $\varepsilon<<1, A<<1$.
Acknowledging a selfsimilar solution of the form
$u=\frac{u^{*}}{V_{0}}, u=\frac{v^{*}}{V_{0}}, y=\frac{V_{0} y^{*}}{v}, t=\frac{V_{0}^{2} y^{*}}{v}, u_{p}=\frac{u_{p}^{*}}{V_{0}}$
$n=\frac{n^{*} v}{V_{0}^{2}}, \theta=\frac{T^{*}T_{\infty}}{T_{w}T_{\infty}}, C=\frac{C^{*}C_{\infty}}{C_{w}C_{\infty}}$ (7)
the basic field Eqns. (2) to (4) can be expressed in non dimensional form as
$\begin{aligned} \frac{\partial u}{\partial t}\left(1+\varepsilon A e^{n t}\right) \frac{\partial u}{\partial y} &=\frac{\partial^{2} u}{\partial y^{2}}\left(M+\frac{1}{K}\right) u+G r \theta+G m C \\ &E\left[\frac{\partial^{3} u}{\partial t \partial y^{2}}\left(1+\varepsilon A e^{n t}\right) \frac{\partial^{3} u}{\partial y^{3}}\right] \end{aligned}$ (8)
$\frac{\partial \theta}{\partial t}\left(1+\varepsilon A e^{n t}\right) \frac{\partial \theta}{\partial y}=\frac{1}{\operatorname{Pr}} \frac{\partial^{2} \theta}{\partial y^{2}}(Q+R) \theta$ (9)
$\frac{\partial C}{\partial t}\left(1+\varepsilon A e^{n t}\right) \frac{\partial C}{\partial y}=\frac{1}{S c} \frac{\partial^{2} C}{\partial y^{2}}K r C$ (10)
$u=u_{p}, \theta=1+\varepsilon e^{n t}, C=1+\varepsilon e^{n t}$ at $y=0$
$u \rightarrow 0, \theta \rightarrow 0, C \rightarrow 0$ as $y \rightarrow \infty$ (11)
$G r=\frac{\left(T_{w}T_{\infty}\right) \beta_{T} g v}{V_{0}^{3}}, G m=\frac{\left(C_{w}C_{\infty}\right) \beta_{C} g v}{V_{0}^{3}}$
$R=\frac{4 v}{\rho C_{p} V_{0}^{2}}, \operatorname{Pr}=\frac{\rho C_{p} v}{k}, K=\frac{K^{*} V_{0}^{2}}{v^{2}}, K r=\frac{K_{1} v}{V_{0}^{2}}$
$S c=\frac{v}{D}, Q=\frac{v Q_{0}}{\rho C_{p} V_{0}^{2}}, E=\frac{k_{0} V_{0}^{2}}{v^{2}}$ (12)
Solutions of Eqns. (8) to (10) are reaped by regular and multiparameter perturbation technique. E, ε and A are presumed small, such that E <<1 and ε<<1.
For getting solutions we introduce
$\left.\begin{array}{l}u(y, t)=u_{0}(y)+\varepsilon e^{n t} u_{1}(y)+0\left(\varepsilon^{2}\right) \\ \theta(y, t)=\theta_{0}(y)+\varepsilon e^{n t} \theta_{1}(y)+0\left(\varepsilon^{2}\right) \\ C(y, t)=C_{0}(y)+\varepsilon e^{n t} C_{1}(y)+0\left(\varepsilon^{2}\right)\end{array}\right\}$ (13)
where, $u_{0},$ is the mean velocity, $\theta_{0}$ is the mean temperature and $C_{0}$ is the mean concentration. Applying Eq. (13) into Eqns. (8) to (10). Tallying nonharmonic and harmonic statement to above location, after neglecting coefficient of $\varepsilon^{2}$ we secure zero order
$E u_{0}^{\prime \prime \prime}+u_{0}^{\prime \prime}+u_{0}^{\prime}n_{1} u_{0}=G r \theta_{0}G m C_{0}$ (14)
$\theta_{0}^{\prime \prime}+\operatorname{Pr} \theta_{0}^{\prime}n_{3} \operatorname{Pr} \theta_{0}=0$ (15)
$C_{o}^{\prime \prime}+S c C_{0}^{\prime}S c K r C_{0}=0$ (16)
where, $n_{1}=M+\frac{1}{K}, n_{3}=Q+R$
With
$u_{0}=u_{p}, \theta_{0}=1, C_{0}=1$
at $y=0$
$u_{0} \rightarrow 0, \theta_{0} \rightarrow, C_{0} \rightarrow 0$
as $y \rightarrow \infty$ (17)
And first order
$E u_{1}^{\prime \prime \prime}+(1n E) u_{1}^{\prime \prime}+u_{1}^{\prime}n_{2} u_{1}=G r \theta_{1}G m C_{1}$$A E u_{0}^{\prime \prime \prime}A u_{0}^{\prime}$ (18)
$\theta_{1}^{\prime \prime}+\operatorname{Pr} \theta_{1}^{\prime}n_{4} \operatorname{Pr} \theta_{1}=\operatorname{Pr} A \theta_{0}^{\prime}$ (19)
$C_{1}^{\prime \prime}+S c C_{1}^{\prime}S c n_{5} C_{1}=A S c C_{0}^{\prime}$ (20)
where, $n_{2}=\left(M+\frac{1}{K}+n\right), n_{4}=Q+R+n, n_{5}=K r+n$.
With corresponding boundary conditions
$u_{1}=0, \theta_{1}=1, C_{1}=1$
at $y=0$ $u_{1} \rightarrow 0, \theta_{1} \rightarrow, C_{1} \rightarrow 0$
as $y \rightarrow \infty$ (21)
Eqns. (14) and (18) are differential equations of 3^{rd} order by virtue of viscoelastic parameter. Since there are exclusively two accessible boundary conditions, it necessitates an additional boundary condition to novel solution.
$u_{0}(y)=u_{00}(y)+E u_{01}(y)+0\left(E^{2}\right)$
$u_{1}(y)=u_{10}(y)+E u_{11}(y)+0\left(E^{2}\right)$ (22)
Put Eq. (22) in Eq. (14). Now compare the coefficient of first and zero order of E, Ne can procure
$u_{00}^{\prime \prime}+u_{00}^{\prime}n_{1} u_{00}=G r \theta_{0}G_{m} C_{0}$ (23)
$u_{01}^{\prime \prime}+u_{01}^{\prime}n_{1} u_{01}=u_{00}^{\prime \prime \prime}$ (24)
The boundary conditions are
$u_{00}=u_{p}, u_{01}=0,$ on $\quad y=0$
$u_{00} \rightarrow 0, u_{01} \rightarrow 0,$ as $\quad y \rightarrow \infty$ (25)
Put Eq. (22) in Eq. (18) and compare the coefficients of zero and first order of E,
We get
$u_{10}^{\prime \prime}+u_{10}^{\prime}n_{2} u_{10}=G r \theta_{01}G_{m} C_{1}A u_{00}^{\prime}$ (26)
$u_{11}^{\prime \prime}+u_{11}^{\prime}n_{2} u_{11}=A u_{00}^{\prime \prime}A u_{01}^{\prime}u_{10}^{\prime \prime \prime}+n u_{10}^{\prime \prime}$ (27)
with
$u_{10}=0, u_{11}=0$
$u_{10} \rightarrow 0, u_{11} \rightarrow 0$
on $y=0$
as $y \rightarrow \infty$ (28)
Using the Eqns. (25) and (28) one can solve the Eqns. (23), (24), (26), and (27) in order to obtain
$u_{00}=A_{7} e^{m_{5} y}A_{5} e^{m_{3} y}A_{6} e^{m_{1} y}$
$u_{01}=A_{11} e^{m_{6} y}+A_{8} e^{m_{5} y}A_{9} e^{m_{3} y}A_{10} e^{m_{1} y}$
$u_{10}=A_{17} e^{m_{7} y}+A_{12} e^{m_{5} y}A_{13} e^{m_{4} y}A_{14} e^{m_{3} y}$
$A_{15} e^{m_{2} y}A_{16} e^{m_{1} y}$
$u_{11}=A_{25} e^{m_{8} y}+A_{18} e^{m_{7} y}+A_{19} e^{m_{6} y}+A_{20} e^{m_{5} y}A_{21} e^{m_{4} y}$
$A_{22} e^{m_{3} y}A_{23} e^{m_{2} y}A_{24} e^{m_{1} y}$
$u_{0}(y)=u_{00}(y)+E u_{01}(y)$
$u_{0}(y)=\left(A_{7} e^{m_{5} y}A_{5} e^{m_{3} y}A_{6} e^{m_{1} y}\right)$
$+E\left(A_{11} e^{m_{6} y}+A_{8} e^{m_{5} y}A_{9} e^{m_{3} y}A_{10} e^{m_{1} y}\right)$
$u_{1}(y)=u_{10}(y)+E u_{11}(y)$
$u_{1}(y)=\left(\begin{array}{l}A_{17} e^{m_{7} y}+A_{12} e^{m_{6} y}A_{13} e^{m_{4} y} \\ A_{14} e^{m_{3} y}A_{15} e^{m_{2} y}A_{16} e^{m_{1} y}\end{array}\right)$
$+E\left(\begin{array}{c}A_{25} e^{m_{8} y}+A_{18} e^{m_{7} y}+A_{19} e^{m_{6} y}+A_{20} e^{m_{5} y} \\ A_{21} e^{m_{4} y}A_{22} e^{m_{3} y}A_{23} e^{m_{2} y}A_{24} e^{m_{1} y}\end{array}\right)$
$u(y, t)=u_{0}(y)+\varepsilon e^{n t} u_{1}(y)$ (29)
$C(y, t)=e^{m_{1} y}+\varepsilon e^{n t}\left(A_{2} e^{m_{2} y}+A_{1} e^{m_{1} y}\right)$ (30)
$\theta(y, t)=e^{m_{3} y}+\varepsilon e^{n t}\left(A_{4} e^{m_{4} y}+A_{3} e^{m_{3} y}\right)$ (31)
Nondimensional skin friction coefficient Cf, heat transfer rate and mass transfer rates are
$\tau=\left(\frac{\partial u}{\partial y}\right)_{y=0}=\left[\begin{array}{l}\left(m_{5} A_{7}+m_{3} A_{5}+m_{1} A_{6}\right) \\ +E\left(m_{6} A_{11}m_{5} A_{8}+m_{3} A_{9}+m_{1} A_{10}\right)\end{array}\right]$$\varepsilon e^{n t}\left[\begin{array}{l}m_{7} A_{17}m_{5} A_{12}+m_{4} A_{13}+m_{3} A_{14} \\ +m_{2} A_{15}+m_{1} A_{16} \\ +E\left(m_{8} A_{25}m_{7} A_{18}m_{6} A_{19}m_{5} A_{20}+m_{4} A_{21}\right)\end{array}\right]$ (32)
$N u=\left(\frac{\partial \theta}{\partial y}\right)$ at $(\mathrm{y}=0)=\left(m_{3}\right)+\varepsilon e^{n t}\left(m_{4} A_{4}+m_{3} A_{3}\right)$ (33)
$S h=\left(\frac{\partial C}{\partial y}\right)$ at $(\mathrm{y}=0)=\left(m_{1}\right)+\varepsilon e^{n t}\left(m_{2} A_{2}+m_{1} A_{1}\right)$ (34)
Selected computations have been depicted graphically in all the figures by assigning the values to the pertinent parameters characterizing the fluid flow mechanism. Extensive analytical computations are done for velocities, thermal and concentration distributions together with friction factor feature, Nusselt as well as Sherwood number for distinct standards of physical constraints which illustrate the structures of flow. Numerical conclusions are well established in Figures 2 to 10 additionally Tables 1 to 3.
Figure 2. Distribution of u for Gr & Gm
Figure 2, illustrates the impact of the flow for heterogeneous values of Grashof number Gr and modified Grashof number Gm. The figure conveys that, Grashof number Gr, modified Grashof number Gm are enlarged, it is perceived that the velocity elevated in general. Also, it is observed that as we shift away from the plate it is perceived that the effect of Grashof number Gr, modified Grashof number Gm are spotted to be not that notable. Figure 3, illustrates the end result of magnitic field parameter M and permeability parameter K on velocity profile. It is fascinating to note from figure that the repercussion of magnetic field is to slow down the value of the velocity profile. The spire value radically declines with raise in the value of the magnetic field, because, the existence of magnetic field incites a force called the Lorentz force. It is also noticed from Figure 3 that the velocity of the flow accelerates with the increase of permeability parameter K.
Figure 3. Distribution of u for M & K
Figure 4. Distribution of u for Pr
Figures 4 and 8 display the dimensionless flow of the fluid and thermal boundary profiles for different values of Pr. These figures explore that the fluid flow and thermal boundary deescalate with uplift in Pr. This is due to the fact that with the raising values of Pr, thermal conductivity decreases, thus the velocity and temperature decreases with an increase in Pr.
Figures 5 and 9, show the antecedent profiles for assorted values of heat sink parameter Q and radiation R. The fluid flow and temperature profiles decrease with the increase of Q and the fluid flow and temperature profiles are increased with the increase of radiation parameter R. Figure 6 displays the dimensionless velocity for different values of Schmidt number Sc. We observe in this figure that the velocity profiles are reduced with increasing values of the Schmidt number Sc. The influence of viscoeleastic parameter E and suction parameter A on velocity profiles has been illustrated in Figure 7. It can identify that when E and A increase the velocity profile increases. From Figure 10, it can be seen that concentration distribution is detraining function of Sc. Further, it is seen that Sc does not contribute much to the concentration field as we move far away from the boundary surface. Analogous effect is noted with chemical reaction parameter Kr on concentration profile.
Figure 5. Distribution of u for Q & R
Figure 6. Distribution of u for Sc
Figure 7. Distribution of u for E & A
Figure 8. Distribution of T for Pr
Figure 9. Distribution of T for Q & R
Figure 10. Distribution of C for Sc & Kr
The effects of varous parameter such as Grashaf value Gr, modified Grashaf value Gm, magnitic parameter M, porosity parameter K, Prandtl value Pr, radiation parameter R, viscoelastic parameter E, suction parameter A, heat sink parameter Q, Schmidt value Sc and chemical reaction parameter Kr on the friction factor (Cf), Nusselt value (Nu) and Sherwood value (Sh) are represented in Tables 1 to 3. From the Table 1, It is perceptible that as Grashaf value Gr or modified Grashaf value Gm or porosity parameter K or suction parameter A enhances, the friction factor uplifts, where as the friction factor downtrends as magnetic parameter M or viscoelastic parameter E increases from Table 1. It is concluded that as radiation parameter R or heat sink parameter Q or Prandtl number Pr escalates, it is observed from Table 2 that the friction factor and Nusselt number escalates. From Table 3, it is found that the Sherwood value escalate when both the Schmidth value Sc and chemical reaction parameter Kr accelerate.
Table 1. Impact of different physical parameter on friction factor, Nusselt value and Sherwod value for $P r=0.7, Q=0.0, R=0.2, S c=0.1, K r=2.0$
Gr 
Gm 
M 
K 
E 
A 
Cf 
Nu 
Sh 
8.0 
1.0 
0.2 
1.0 
0.01 
0.1 
2.0115 
5.7375 
0.6432 
9.0 





2.2585 
5.7375 
0.6432 
10.0 




2.5055 
5.7375 
0.6432 


2.0 




2.1408 
5.7375 
0.6432 

3.0 



2.2702 
5.7375 
0.6432 



0.4 



3.6009 
5.7375 
0.6432 


0.6 


3.3221 
5.7375 
0.6432 




1.5 


5.5941 
5.7375 
0.6432 



2.0 

7.8830 
5.7375 
0.6432 





0.02 

6.0344 
5.7375 
0.6432 




0.03 
4.0230 
5.7375 
0.6432 






0.15 
3.0172 
5.7375 
0.6432 





0.17 
3.4195 
9.7538 
0.6432 
Table 2. Impact of different physical parameter on friction factor, Nusselt value and Sherwod value for $G r=8.0, G m=K=1.0, M=0.2, E c=0.01, K r=2.0, S c=A=0.1$
Pr 
R 
Q 
Cf 
Nu 
Sh 
0.7 
0.2 
0.5 
2.0115 
5.7375 
0.6432 
0.8 


2.8576 
1.3118 
0.6432 
1.0 


8.7732 
3.3588 
0.6432 

0.8 

3.8078 
1.8848 
0.6432 

0.9 

4.4935 
1.9581 
0.6432 


1.0 
3.3065 
1.8110 
0.6432 


1.5 
9.9184 
2.1758 
0.6432 
Table 3. Impact of different physical parameter on friction factor, Nusselt value and Sherwod value for $G r=8.0, G m=1.0, K=1.0, M=0.2, R=0.2, P r=0.7, E c=0.01, K r=2.0$
Sc 
Kr 
Cf 
Nu 
Sh 
0.1 
2.0 
2.0115 
5.7375 
0.6432 
0.3 

2.0313 
5.7375 
1.2076 
0.5 

2.1053 
5.7375 
1.6467 

3.0 
2.0124 
5.7375 
0.7667 

4.0 
2.0146 
5.7375 
0.8714 
In the present study a mathematical model has been developed to simulate 2D unsteady magneto hydrodynamic flow of an incompressible electrically conducting fluid over a permeable moving plate through porous medium under the importance of thermal radiation and chemical reaction. The governed mathematical statement is handled analytically by perturbation technique. The obtained results have led to the following conclusions:
$A$ 
suction parameter 
$B_{0}$ 
agnetic field intensity, N. m^{1}.A^{1} 
$C^{*}$ 
fluid concentration 
$C_{\infty}$ 
free stream dimensional concentration 
$A$ 
viscoelastic parameter 
$D^{*}$ 
Brownian diffusion coefficient, m^{2}. s^{1} 
$G m$ 
modified Grashof number 
$G r$ 
grashof number 
$K_{\lambda w}$ 
absorption coefficient at wall 
$k^{*}$ 
permeable parameter 
$K$ 
nondimensional porous parameter 
$K_{1}$ 
chemical reaction coefficient 
$K r$ 
chemical reaction parameter 
$M$ 
magnetic parameter 
$n^{*}$ 
constant 
$N u$ 
local Nusselt number 
$P^{*}$ 
pressure, Pa 
$P r$ 
Prandtl number 
$Q_{0}^{*}$ 
dimensional heat sink 
$Q$ 
heat sink parameter 
$R$ 
radiation parameter 
$R^{*}$ 
rate of chemical reactive factor 
$S c$ 
Schmidt number 
$S h$ 
Sherwood number 
$T^{*}$ 
Temperature, K 
$T_{\infty}$ 
surface temperature, K 
$T_{\infty}$ 
free stream dimensional temperature K 
$U$ 
stretching velocity, m. s^{1} 
$U_{0}$ 
reference velocity, m. s^{1} 
$u^{*}, v^{*}$ 
velocity components in $x^{*}, y^{*}$ directions, m. s^{1} 
$u_{p}^{*}$ 
wall dimensional velocity, m. s^{1} 
$x^{*}, y^{*}$ 
Cartesian coordinate in horizontal and vertical directions 
Greek symbols
$v$ 
kinematic viscosity, m^{2}. s^{1} 
$\varepsilon$ 
small value 
$\sigma$ 
electrical conductivity of the fluid, S. m^{1} 
$\rho$ 
fluid density, kg. m^{3} 
$v_{0}$ 
constant suction velocity 
$\tau_{w}$ 
surface shear rate, Pa 
$\beta_{T}$ 
coefficient of thermal expansion 
$\beta_{C}$ 
coefficient of solutal expansion 
$k$ 
thermal conductivity of the fluid, W. m^{1}. k^{1} 
$c_{p}$ 
specific at constant pressure, J.K^{1}.kg^{1} 
Appendix
$m_{1}=\frac{S c+\sqrt{S c^{2}+4 S c K r}}{2}, m_{2}=\frac{S c+\sqrt{S c^{2}+4 S c n_{5}}}{2}$,
$m_{3}=\frac{\operatorname{Pr}+\sqrt{\operatorname{Pr}^{2}+4 \operatorname{Pr} n_{3}}}{2}, m_{4}=\frac{\operatorname{Pr}+\sqrt{\operatorname{Pr}^{2}+4 \operatorname{Pr} n_{4}}}{2}$,
$m_{5}=\frac{1+\sqrt{1+4 n_{1}}}{2}, \quad m_{6}=\frac{1+\sqrt{1+4 n_{1}}}{2}, m_{7}=\frac{1+\sqrt{1+4 n_{2}}}{2}$,
$m_{8}=\frac{1+\sqrt{1+4 n_{2}}}{2}, A_{1}=\frac{A S c m_{1}}{m_{1}^{2}S c m_{1}S c n_{5}}, A_{2}=1A_{1}$,
$A_{3}=\frac{A \operatorname{Pr} m_{3}}{m_{3}^{2}\operatorname{Pr} m 3\operatorname{Pr} n_{4}}, A_{4}=1A_{3}, A_{5}=\frac{G r}{m_{3}^{2}m_{3}n_{1}}$,
$A_{6}=\frac{G m}{m_{1}^{2}m_{1}n_{1}}, A_{7}=u_{p}+A_{5}+A_{6}$,
$A_{8}=\frac{A_{7} m_{5}^{3}}{m_{5}^{2}m_{5}n_{1}}, A_{9}=\frac{A_{5} m_{3}^{3}}{m_{3}^{2}m_{3}n_{1}}, A_{10}=\frac{A_{6} m_{1}^{3}}{m_{1}^{2}m_{1}n_{1}}$,
$A_{11}=A_{10}+A_{9}A_{8}$,
$A_{12}=\frac{A A_{7} m_{5}}{m_{5}^{2}m_{5}n_{2}}, A_{13}=\frac{G r A_{4}}{m_{4}^{2}m_{4}n_{2}}$,
$A_{14}=\frac{G r A_{3}+A A_{5} m_{3}}{m_{3}^{2}m_{3}n_{2}}, A_{15}=\frac{G r A_{2}}{m_{2}^{2}m_{2}n_{2}}$,
$A_{16}=\frac{G m A_{1}+A A_{6} m_{1}}{m_{1}^{2}m_{1}n_{2}}, A_{17}=A_{16}+A_{15}+A_{14}+A_{13}A_{12}$,
$A_{18}=\frac{m_{7}^{3} A_{17}+n A_{17} m_{7}^{2}}{m_{7}^{2}m_{7}n_{2}}, A_{19}=\frac{A A_{11} m_{6}}{m_{6}^{2}m_{6}n_{2}}$,
$A_{20}=\frac{A A_{7} m_{5}^{3}+A A_{8} m_{5}+A_{12} m_{5}^{3}+n A_{12} m_{5}^{2}}{m_{5}^{2}m_{5}n_{2}}$,
$A_{21}=\frac{m_{4}^{3} A_{13}+n A_{13} m_{4}^{2}}{m_{4}^{2}m_{4}n_{2}}$,
$\begin{aligned} A_{22} &=\frac{A A_{5} m_{3}^{3}+A A_{9} m_{3}+A_{14} m_{3}^{3}+n A_{14} m_{3}^{2}}{m_{3}^{2}m_{3}n_{2}} \\ A_{23} &=\frac{m_{2}^{3} A_{15}+n A_{15} m_{2}^{2}}{m_{2}^{2}m_{2}n_{2}} \end{aligned}$,
$\begin{aligned} A_{24} &=\frac{A A_{6} m_{1}^{3}+A A_{10} m_{1}+A_{16} m_{1}^{3}+n A_{16} m_{1}^{2}}{m_{1}^{2}m_{1}n_{2}} \\ A_{25} &=A_{19}A_{18}+A_{24}+A_{23}+A_{22}+A_{21}A_{20} \end{aligned}$.
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