INTERNATIONAL JOURNAL OF LATEST TECHNOLOGY IN ENGINEERING,  
MANAGEMENT & APPLIED SCIENCE (IJLTEMAS)  
ISSN 2278-2540 | DOI: 10.51583/IJLTEMAS | Volume XIV, Issue XI, November 2025  
MHD Flow Over A Rotating Vertical Porous Plate with  
Exponentially Accelerating Velocity, Temperature, and Mass in the  
Presence of Hall Current and Heat Source  
Dr D. Lakshmikaanth1, M. Krishnakumari2  
1Department of Mathematics, College of Fish Nutrition & Food Technology (CFNFT), Tamilnadu Dr. J.  
Jayalalithaa Fisheries University (TNJFU), Chennai-600051, India  
2 Department of Mathematics, Mahalashmi Women’s College of Arts and Science , No.!,Mahalashmi  
Received: 29 November 2025; Accepted: 05 December 2025; Published: 24 December 2025  
ABSTRACT:  
This study analyzes exponentially accelerating fluid through vertically porous plate with a heat source. The  
effects of rotation, porosity, and Thermal Radiation on velocity (Speed), temperature (Warmth), and  
concentration(accumulation) profiles are investigated. Results indicate that velocity rises with heat source  
increase but decreases with radiation and rotation. Temperature increases with heat generation raises while  
concentration drops with higher Schmidt numbers. Also, Skin friction, Nusselt & Sherwood values tabulated.  
Keywords: Exponential, Sherwood, Generation, Plate, Concentration.  
INTRODUCTION  
Heat sources are used a lot in the processing of chemicals and polymers, like film coating, extrusion, and drying,  
because they speed up reaction and production rates. In the food industry, heat sources are used in processes like  
pasteurisation, and film coating. Controlled heating speeds up reactions, improves texture, and makes products  
more stable. [1] Kota et al. studied transient MHD flow across a vertically speeding permeable plate with viscous  
heating and warmth generation. [2] A. Selvaraj and E. Jothi looked into how the temperature of the plate rises  
in a straight line over time, with the highest values happening close to the surface of the plate. [3]-[4] Nath and  
Deka compared the behaviour of nanofluids with two stratifications to that without any stratification without and  
with Chemical reaction. [5] Rakesh Rabha and Rudra K. Deka analyzed the flow with and without stratification,  
observing that steady state(independent of time) is reached faster in the presence of stratification. [6] K.Balu  
and his collegue examines MHD across rapidly sloped plate and concentrating on the region adjacent to the  
plate. [7] Pratibha P. Ubale Patil et al. found that axial skin friction goes down as water permeability goes up,  
changes in an irregular way in air, and oscillates in both fluids when a heat source is present.[8]-[11] D.  
Lakshmikanth and his team looked into how a heat source with and without rotation, as well as the Dufour effect,  
affected a vertically accelerated isothermal plate that was undergoing chemical reaction and radiation.[12] R.  
Muthukumaraswamy and a coworker used MATLAB to make graphs of skin friction, temperature,  
concentration, and velocity profiles for different thermophysical parameters. [13]-[14] Hetnarski introduces an  
algorithm for the formulas of inverse Laplace transforms.  
Mathematical Formulation  
We are looking at a non-conductive vertical plate at = 0, with a viscous incompressible conducting fluid  
flowing past it. The plate is vertical and the axis is normal to it. The velocity, temperature and concentration  
all are eat at t=0. The velocity components make the flow characteristics when there is constant pressure across  
flow and continuity is met. Taking these assumptions into account, the governing equations for the transient flow  
are written like this:  
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2
2
2
~
~
~
~
~
B  
u
m v  
u  
u  
~
~
~
~
u
~
0
1
2u    
gT T gC C  
1
~
2
2
~
t  
K
1
z  
1m  
1
2
2
2
~
~
~ ~  
~
B m u v  
v  
v  
v  
~
0
1
2v    
2
~
2
2
~
t  
K
1
z  
1m  
1
~
~
2
  
1    
~
~
R  Q  
3
   
~
2
~
t  
Pr  
z  
~
~
2
C  
1 C  
4
~
2
~
t  
Sc  
z  
The conditions are  
~
~
~
~
~
~
~
~
t 0: u v 0,T T ,C C ,z 0,  
~
~
~
~
~
~
at  
~
~
~
t 0: u u  
e
, v 0,T T C C 0z 0,  
5
0
~
~
~
~
~
~
~
t 0: u 0, v 0,T T ,C C as z  ,  
The consequent dimensionless aggregate is  
~
~
~
~
~
2
0
~
~
u
zu  
tu  
T T  
C C  
0
Z   
, t   
,U   
,   
,C     
~
~
~
~
u
T T  
C
C  
o
w
w
1/ 3  
~
~
~
~
2
gT T  
g  
C
C  
B  
o
2
w
w
Gr   
,Gc   
,M   
6
3
3
2
u
u
u
o
o
o
1/ 3  
Cp  
2
Pr   
,K K  
,Sc   
1
k
D
u
o
(1)+ i×(2) and putting velocity q = u+iv we get ,  
2
2
q  
t  
q  
q
M
G   G C   
mq   
where m   
2i  
r
c
2
K
1hi  
z  
1
2
  
t  
1    
P
r
R  Q  
2
z  
2
C  
1 C  
2
t  
S
c
z  
With conditions  
q 0,   C 0 for all z,t 0  
at  
at  
at  
q e ,   e  
,C e  
for all z,t 0  
q 0,   0 ,C 0 as z  .  
RESULTS & DISCUSSION  
Solving Using Inverse technique of Laplace we have  
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at  
e
2atSc  
z atSc  
C  
e
erfcSc ate  
erfcSc at  
2   
at  
42P atRtQt  
42P aRQ  
t
e
2
2
r
r
  
e
erfc P at Rt Qt e  
erfc P at Rt Qt  
r
r
2
1
1
2
2
ma 4t  
ma 4t  
at  
e
t
t
k1  
k1  
q   
e
erfc mt   
at e  
erfc mt   
at  
2
k
k
1
1
t
2
mt at 4  
t
k1  
e
erfc mt   
at  
at  
k
e
1
2
t
2
mt at 4  
t
k1  
e  
erfc   mt   
at  
k
1
G
1
r
P 1 a b  
t
2
r
mt bt 4  
t
k1  
e
erfc   
mt   
bt  
k
bt  
1
e
2
t
2
mt bt 4t  
t
k1  
   
e  
erfc   
mt   
bt  
   
k
1
   
t
2
mt at 4  
t
k1  
e
erfc   
mt   
at  
k
at  
e
1
2
t
2
mt at 4  
t
k1  
e  
erfc    
mt   
at  
k
1
   
G
1
c
S 1 a c  
c
t
2
mt ct 4  
t
k1  
e
erfc    
mt   
ct  
k
ct  
1
e
2
t
2
mt at 4  
t
k1  
e  
erfc    
mt   
ct  
k
1
   
R Qa4t2 Pr  
2
e
erfc Pr Rt Qt at  
at  
e
R Qa4t2 Pr  
2   
2
e  
erfc Pr Rt Qt at  
G
1
r
R Qb4t2 Pr  
P 1 a b  
r
   
2
e
erfc Pr Rt Qt bt  
bt  
e
R Qb4t2 Pr  
2   
   
2
e  
erfc Pr Rt Qt bt  
at  
e
2atSc  
2atSc  
ct  
e
erfcSc ate  
erfcSc at  
G
1
2
c
S 1 a c  
c
e
2ctSc  
2ctSc  
e
erfcSc cte  
erfcSc ct  
2
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1
1
m   
R QPr  
m   
k
z
k
1
1
where    
b   
,
,
c   
Pr1  
Sc 1  
2 t  
Skin  
Friction  
1
(Sk)  
1
mt t  
at  
q  
1  
1
k1  
at  
e  
e  
1erfc  
mt t  
at  
m   
a  
z  
k
k
1
t  
1
z0  
1
mt t  
at  
1
1
1
k1  
at  
e
e
1erfc  
mt t  
at  
m   
a  
k
k
1
t  
1
G
r
P 1a b  
1
r
mt t  
bt  
1
1
1
k1  
bt  
e  
   
e  
1erfc  
mt t  
bt  
m   
b  
k
k
1
t  
1
1
mt t  
at  
1
1
1
k1  
at  
e
e
1erfc  
mt t  
bt  
m   
a  
k
k
1
t  
1
G
c
  
Sc 1a c  
1
mt t  
ct  
1
1
1
k1  
bt  
e  
e
1erfc  
mt t  
bt  
m   
c  
k
k
1
t  
1
Pr  
at  
RtQtat  
e
   
e  
1erfcRt Qt at  
R Q aPr  
t  
G
r
P 1a b  
Pr  
r
bt  
RtQtbt  
e  
e
1erfcRt Qt bt  
R Q bPr  
t  
Nusselt  
G
Sc  
Sc  
at  
at  
bt  
bt  
c
e
e
1erfc at  
aSc e  
e
1erfc bt  
bSc  
Sc 1a c  
t  
t  
  
Pr  
at  
Rt Qtat  
e  
e
1erfcRt Qt at  
R PrQPra Pr  
Number (Nu)  
z  
t  
z0  
Sherwood Number (Sh)  
C  
Sc  
at  
eat  
e
1erfcat  
aSc  
z  
t  
z0  
Nusselt Number (Nu)  
R
Q
Pr  
t
Nu  
2.0  
2.0  
2.0  
7.0  
7.0  
7.0  
0.4  
0.4  
0.4  
-3.4646  
-5.0003  
-6.2683  
3.0  
5.0  
7.0  
R
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5.0  
5.0  
5.0  
5.0  
5.0  
5.0  
5.0  
5.0  
7.0  
7.0  
7.0  
0.71  
7.0  
7.0  
7.0  
7.0  
0.4  
0.4  
0.4  
0.4  
0.4  
0.1  
0.2  
0.4  
-5.9710  
-5.0003  
-3.4646  
-1.5925  
-5.0003  
-6.1739  
-5.3226  
-5.0003  
0.5  
2.0  
4.0  
2.0  
2.0  
2.0  
2.0  
2.0  
Q
Pr  
T
Sherwood Number (Sh)  
Sc  
t
Sh  
0.4  
0.4  
0.4  
0.1  
0.2  
0.4  
-0.5287  
-0.7478  
-1.3686  
-2.5804  
-1.8611  
-1.3686  
0.3  
0.6  
Sc  
2.01  
2.01  
2.01  
2.01  
t
Skin Friction ( )  
Gr  
Gc  
R
Q
k1  
M
hc  
w
25.0  
25.0  
25.0  
10.0  
18.0  
25.0  
25.0  
25.0  
25.0  
25.0  
5.0  
5.0  
5.0  
5.0  
5.0  
5.0  
2.0  
3.0  
5.0  
5.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
0.5  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
0.7275  
1.7715  
2.6849  
1.5370  
2.1493  
2.6849  
3.4668  
3.1615  
2.6849  
2.4134  
10.0  
18.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
Gr  
Gc  
R
Q
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25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
25.0  
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  
1.0  
1.0  
0.5  
1.0  
4.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.0  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
2.5  
3.0  
1.5  
1.5  
1.5  
1.5  
1.5  
1.5  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
3.0  
0.25  
1.0  
3.0  
3.0  
3.0  
3.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
3.0  
4.0  
2.6849  
3.1615  
-1.7834  
2.6849  
6.1627  
2.6849  
1.3032  
0.2148  
0.9419  
1.9332  
2.6849  
2.6849  
-0.3271  
-4.7847  
2.0  
4.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
2.0  
k1  
M
Hc  
Ω
Geometrical Representation  
Figure 1  
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Fig 1 :The buoyancy force induced by the difference in temperature stronger as the thermal Grashof number  
(Gr) goes up. This higher buoyancy makes the fluid move faster, which speeds up the flow.  
Figure 2  
Fig 2 It shows that when the Mass Grashof number (Gc) goes up the velocity (speed) goes up also. This is  
because a bigger mass-concentration differential makes buoyancy forces greater, which pushes the fluid faster  
and raises the flow speed.  
Figure 3  
Fig 3: It discovers that the speed of the fluid rises as the heat source (Q) gets greater. This is because more  
heating increases the buoyancy force, which pushes the fluid faster.  
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Figure 4 In Fig 4 As radiation(R) rises, the velocity (speed) drops because more radiation takes heat out from  
the fluid, which lowers the buoyancy force and slows down the flow.  
Figure 5 In Fig 5 As the rotation (w) speeds up, the velocity (speed) down. This is because higher rotational  
effects create Coriolis and centrifugal forces, which slow down the flow by resisting the fluid motion.  
Figure 6 In Fig 6 As the Hall current (hc)goes up, the speed (velocity) goes up also. This is because the Hall  
effect makes the electromagnetic force stronger in the fluid, which speeds up the motion and raises the flow  
speed.  
Figure 7In Fig 7 The speed (velocity) goes up when permeability(k1) goes up. This is because increased  
permeability makes it easier for the fluid to move through the medium, which lowers resistance and speeds up  
flow.  
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Figure 8 In Fig 8 As the Prandtl number (Pr) goes up, the velocity (speed) goes down. This is because a higher  
Prandtl number indicates that momentum spreads out quicker than heat, which slows down the fluid motion and  
stops the thermal boundary layer from growing.  
Figure 9 In Fig 9 As radiation (R) rises, the temperature drops. This is because increased radiation takes heat out  
from the fluid, lowering its thermal energy and lowering the temperature.  
Figure 10 In Fig. 10, the temperature goes up because greater Heat source (Q) contributes more thermal energy  
to the fluid, which makes it hotter.  
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Figure 11  
In Fig 11 The Schmidt number (Sc) goes up, which means that mass diffusion is slower than  
momentum. This slows down the flow and diminishes the fluid motion.  
CONCLUSION  
The fast isothermal flow over a inclined vertical plate is the focus of this easy-to-use and interesting framework  
for computer research. This has to do with HMT. These computations allow for the deduction of several crucial  
relationships:  
(i) Velocity increases when the Heat Source increases, whereas velocity decreases with raise in permeability and  
Hall Current  
(ii)Temperature drops as radiation levels rise whereas the Heat Source raises, the temperature raises.  
(iii)The concentration of the species involved tends to decline as the rate of the schmidth raises.  
(iv)The Skin friction decreases as Prandtl, Hartmaann, Permeability, Radiation and Hall Current Values  
increases whereas skin friction increases when Rotation, Heat Source, Thermal Grashof and Mass Grashof values  
increases.  
REFERENCES  
1. Santhi Kumari Dharani Kota, Venkata Subrahmanyam Sajja, and Perugu Mohana Kishore. “Transient  
MHD Flows Through an Exponentially Accelerated Isothermal Vertical Plate with Viscous Dissipation  
and Heat Source Embedded in a Porous Medium.” Journal of Advanced Research in Fluid Mechanics  
and Thermal Sciences 106, no. 2 (July 18, 2023): 15366. https://doi.org/10.37934/arfmts.106.2.153166.  
2. Selvaraj, A., and E. Jothi. “Heat Source Impact on MHD and Radiation Absorption Fluid Flow Past an  
Exponentially Accelerated Vertical Plate with Exponentially Variable Temperature and Mass Diffusion  
through  
a
Porous  
Medium.”  
Materials  
Today:  
Proceedings  
46  
(2021):  
3490–94.  
3. Nath, Rupam Shankar, and Rudra Kanta Deka. “Thermal and Mass Stratification Effects on MHD  
Nanofluid Past an Exponentially Accelerated Vertical Plate through a Porous Medium with Thermal  
Radiation and Heat Source.” International Journal of Modern Physics B 39, no. 07 (April 3, 2024).  
4. Nath, Rupam Shankar, and Rudra Kanta Deka. “Theoretical Study of Thermal and Mass Stratification  
Effects on MHD Nanofluid Past an Exponentially Accelerated Vertical Plate in a Porous Medium in  
Presence of Heat Source, Thermal Radiation and Chemical Reaction.” International Journal of Applied  
and Computational Mathematics 10, no. 2 (April 2024). https://doi.org/10.1007/s40819-024-01721-9.  
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ISSN 2278-2540 | DOI: 10.51583/IJLTEMAS | Volume XIV, Issue XI, November 2025  
5. Rabha, Rakesh, and Rudra K. Deka. “Influence of Mass Transfer and Chemical Reaction on MHD Flow  
Through a Porous Medium Past an Exponentially Accelerated Vertical Plate With Thermal Stratification  
and Radiation.” Heat Transfer 54, no. 5 (April 14, 2025): 3208–19. https://doi.org/10.1002/htj.23353.  
6. Balu, K. “Heat And Mass Transfer on MHD Flow Past an Exponentially Accelerated Vertical Plate  
Through Porous Medium.” Interantional Journal of Scientific Research in Engineering and Management  
07, no. 09 (September 1, 2023). https://doi.org/10.55041/ijsrem25575.  
7. Pratibha P. Ubale Patil, V. B. Kulkarni, R. M. Lahurikar “Effect of Heat Source on the Rotatory Flow  
Past an Accelerated Infinite Vertical Plate through Porous Medium.”  
Journal of Intelligent Systems and Applications  
International  
Engineering, 2024.  
in  
8. Lakshmikaanth, D., A. Selvaraj, P. Selvaraju, and S. Dilip Jose. “Hall and Heat Source Effects of Flow  
Past a Parabolic Accelerated Isothermal Vertical Plate in the presence of Chemical Reaction and  
Radiation.”  
JP  
Journal  
of  
Heat  
and  
Mass  
Transfer,  
July  
14,  
2023,  
105–26.  
9. Lakshmikaanth, D., Selvaraj, A., Selvaraju, P., & Jose, S. D. (2023). Heat Source effects of flow past a  
parabolic accelerated isothermal vertical plate in the presence of Hall Current , Chemical reaction ,  
Rotation and Radiation. Eur. Chem. Bull. 2023,12(4), 3354-3374.  
10. D, lakshmikaanth, Selvaraj A., and Bhavani S. “Exploration of the Impacts of Hall Effect, Dufour Effect,  
and Heat Source on Parabolic Flow over an Infinite Vertical Plate in the Presence of Rotation, Chemical  
Reaction, and Radiation in a Porous Medium.” CFD Letters 17, no. 1 (August 31, 2024): 6077.  
11. Jose, S. Dilip, K. Selvaraj, P. N. Sudha, P. Geetha, and D. Lakshmikaanth. “Heat and Mass transfer  
Effects on parabolic flow past an accelerated Isothermal Vertical plate in the Presence Of Chemical  
Reaction and Hall Current.” JP Journal of Heat and Mass Transfer 35 (September 15, 2023): 55–74.  
12. Muthucumaraswamy, R., and C. Santhana Lakshmi. “Mass and Heat transfer Effects on MHD Fluid  
Flow of an Exponentially Accelerated Isothermal vertical Plate with variable mass diffusion.” Advances  
and  
Applications  
in  
Fluid  
Mechanics  
18,  
no.  
1
(May  
8,  
2015):  
3149.  
13. Hetnarski, Richard B. “An Algorithm for Generating Some Inverse Laplace Transforms of Exponential  
Form.” Zeitschrift Für Angewandte Mathematik Und Physik ZAMP 26, no. 2 (March 1975): 24953.  
14. Hetnarski, R. “On Inverting the Laplace Transforms Connected with the Error Function.” Applicationes  
Mathematicae 7, no. 4 (1964): 399405. https://doi.org/10.4064/am-7-4-399-405.  
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