Abstract
In this paper, the heat transfer effect on the unsteady boundary layer flow of a Casson fluid past an infinite oscillating vertical plate with Newtonian heating is investigated. The governing equations are transformed to a systems of linear partial differential equations using appropriate non-dimensional variables. The resulting equations are solved analytically by using the Laplace transform method and the expressions for velocity and temperature are obtained. They satisfy all imposed initial and boundary conditions and reduce to some well-known solutions for Newtonian fluids. Numerical results for velocity, temperature, skin friction and Nusselt number are shown in various graphs and discussed for embedded flow parameters. It is found that velocity decreases as Casson parameters increases and thermal boundary layer thickness increases with increasing Newtonian heating parameter.
Introduction
Non-Newtonian fluids are widely used in industries such as chemicals, cosmetics, pharmaceuticals, food and oil & gas [1]. Due to their numerous applications several scientists and engineers are working on them. Despite of the fact non-Newtonian fluids are not as easy as Newtonian fluids. It is due to the fact that in non-Newtonian fluids there does not exist a single constitutive relation that can be used to explain all of them. Therefore several constitutive equations or models are introduced to study their characteristics. The different non-Newtonian models include power law [2], second grade [3], Jeffrey [4], Maxwell [5], viscoplastic [6], Bingham plastic [7], Brinkman type [8], Oldroyd-B [9] and Walters-B [10] models. However, there is another model known as Casson model which is recently the most popular one. Casson [11] was the first who introduce this model for the prediction of the flow behavior of pigment oil suspensions of the printing ink type. Later on, several researchers studied Casson fluid for different flow situations and configurations. Amongst them, Mustafa et al. [12] studied the unsteady flow and heat transfer of a Casson fluid past a moving flat plate. Rao et al. [13] considered the thermal and hydrodynamic slip conditions on heat transfer flow of a Casson fluid past a semi-infinite vertical plate. Heat transfer flow of a Casson fluid past a permeable shrinking sheet with viscous dissipation was considered by Qasim and Noreen [14]. Recently, forced convection flow of a Casson fluid past with surface heat flux over a symmetric porous wedge was investigated by Mukhopadhyay and Mandal [15]. Few other attempts for the Casson fluid can also be found in [16]–[21].
In all these studies mentioned above, the Newtonian heating condition was neglected at the boundary. The situation where the heat is transported to the convective fluid via a bounding surface having finite heat capacity is known as Newtonian heating (or conjugate convective flows). This configuration occurs in convection flows set up when the bounding surfaces absorb heat by solar radiation. Merkin [22] in his pioneering work studied the free convection boundary layer flow past a vertical plate with Newtonian heating. He found the asymptotic solution near the leading edge analytically and the full solution along the whole plate for free convection boundary layer over vertical surfaces numerically. On the other hand, the Newtonian heating situation occurs in many important engineering devices, such as heat exchanger and conjugate heat transfer around fins. Therefore, in view of such applications several authors have used the Newtonian heating condition in their convective heat transfer problems and have obtained the solutions either numerically [23]–[26] or analytical forms [27]–[33].
Most of the existing studies on unsteady boundary layer flow and heat transfer with Newtonian heating condition are limited to the Newtonian fluid or they are solved using any numerical or approximate technique. This motivates us to consider the Newtonian heating phenomenon in the present work for non-Newtonian fluids. More exactly, our aim is to investigate unsteady boundary layer flow and heat transfer of a Casson fluid past an infinite oscillating vertical plate with Newtonian heating condition. The equations of the problem are first formulated and then transformed into their dimensionless forms where the Laplace transform method is applied to find the exact solutions for velocity and temperature.
Mathematical Formulation
Let us consider the heat transfer effect on unsteady boundary layer flow in a Casson fluid past an infinite oscillating vertical plate fixed at
, the flow being confined to
, where
is the coordinate axis normal to the plate. Initially, for time
, both plate and fluid are at stationary condition with the constant temperature
. At time
the plate started an oscillatory motion in its plane
according to
| (1) |
where
,
is the amplitude of the motion,
is the unit step function,
is the unit vector in the vertical flow direction and
is the frequency of plate oscillation. At the same time, the heat transfer from the plate to the fluid is proportional to the local surface temperature
. We assume that the rheological equation for an isotropic and incompressible Casson fluid, reported by Casson [11], is
equivalently
![]() |
where
is the shear stress,
is the Casson yield stress,
is the dynamic viscosity,
is the shear rate,
and
is the
component of the deformation rate,
is the product of the component of deformation rate with itself,
is a critical value of this product based on the non-Newtonian model,
the is plastic dynamic viscosity of the non-Newtonian fluid and
the is yield stress of fluid. Under these assumptions the unsteady boundary layer flow with heat transfer is governed by momentum and energy equations:
| (2) |
| (3) |
where
is the Cauchy stress tensor,
is the fluid density,
is the body force, p is the pressure,
is the heat capacity at constant pressure and
is the thermal conductivity. Under the Boussinesq approximation along with the assumption that the pressure is uniform across the boundary layer, we get the following set of partial differential equations:
| (4) |
| (5) |
with following initial and boundary conditions
| (6) |
| (7) |
| (8) |
in which
is the axial velocity,
is the time,
is the kinematic viscosity,
is the Casson fluid parameter,
is the acceleration due to gravity,
is the volumetric coefficient of thermal expansion and
is the heat transfer coefficient. The geometry of the problem is presented in Figure 1.
Figure 1. Physical model and coordinate system.

To reduce the above equations into their non-dimensional forms, we introduce the following non-dimensional quantities
| (9) |
Substituting equation (9) into equations (4) and (5), we obtain the following non-dimensional partial differential equations (* symbols are dropped for simplicity)
| (10) |
| (11) |
The corresponding initial and boundary conditions in non-dimensional form are
| (12) |
| (13) |
| (14) |
where
are the Grashof number, the Prandtl number and the conjugate parameter for Newtonian heating respectively. We note that equation (13) gives
when
corresponding to having
and hence no heating from the plate exists [23], [32].
Method of Solution
In order to obtain the exact solution of the present problem, we will use the Laplace transform technique. Applying the Laplace transforms with respect to time
to the equations (10)–(11), we get
| (15) |
| (16) |
Here,
and
denote the Laplace transforms of
and
, respectively. Using the initial condition (12), we get
| (17) |
| (18) |
The corresponding transformed boundary conditions are
| (19) |
| (20) |
The solutions of equations (17) and (18) subject to the boundary conditions (19) and (20) are
![]() |
(21) |
| (22) |
By taking the inverse Laplace transforms of above equations, we obtain
| (23) |
![]() |
(24) |
The solution for velocity given in equation (24) is not valid, when
and
. In this case, the solution obtained is given by
![]() |
(25) |
where
![]() |
![]() |
, are dummy functions of the dummy variables
.
The dimensionless expression for skin friction evaluated from equation (24) is given by
![]() |
(26) |
where
is the dimensional skin friction. The dimensionless expression of Nusselt number is given by
![]() |
(27) |
Limiting Cases
The solutions obtained here are more general. In this section, we consider some of their limiting cases.
Solution in case of Newtonian fluid
If
, the solution for velocity given in equation (24) reduces to the corresponding solution for Newtonian fluid given by
![]() |
(28) |
It is important to note that the above solution (28) for Newtonian fluid over an impulsively moved plate when
is similar to that obtained by [27].
Solution in the absence of free convection
In the absence of free convection, which is numerically corresponds to
, the equation (24) reduces to
| (29) |
Solution of Stokes first problem
By making
into equation (24), we get the classical solution
![]() |
(30) |
corresponding to the Stokes first problem for Casson fluid over an impulsively motion of the plate.
Graphical Results and Discussion
Exact solutions for the problem of unsteady boundary layer heat transfer flow of an incompressible Casson fluid past an infinite oscillating vertical plate with Newtonian heating condition are obtained. For the physical behavior of embedded parameters such as Casson parameter
, Prandtl number
, Grashof number
, conjugate parameter for Newtonian heating
, time
and phase angle
, these solutions are plotted in graphs (Figures 2–15) and discussed in details.
Figure 2. Velocity profiles for different values of.

when
Figure 15. Nusselt number variation for different values of.

The velocity profiles for different values of Casson parameter
are shown in Figure 2. From this figure, it is observed that velocity decreases with increasing values of
. Further, it is noticed that Casson parameter does not have any influence as the fluid moves away from the bounding surface. The velocity profiles are shown in Figure 3 for different values of Prandtl number
. It is observed that velocity decreases with increasing Prandtl number. This situation is in consistence with the physical observation because fluids with large Prandtl number have high viscosity and small thermal conductivity, which makes the fluid thick and hence causes a decrease in velocity of fluid. In addition, the curves show that velocity of fluid is maximum near the plate and approaches to zero as
(for away from the plate). It is also found from Figures 2 and 3, that the behavior of
and
on the velocity profiles are quite identical with that found in figure 7 and 9, of Rao et al. [13]. The effects of Grashof number
on the velocity profiles are shown in Figure 4. The trend shows that velocity increases with increasing values of
. It is true physically also because the role of Grashof number in heat transfer flow is to increase the strength of the flow. Here
corresponds to the absence of free convection, while
represents to the cooling problem. Moreover, the cooling problem is of great importance and mostly encountered in engineering applications, such as in the cooling of electronic components and nuclear reactors. For different values of conjugate parameter for Newtonian heating
, the velocity profiles are plotted in Figure 5. An increase in conjugate parameter for Newtonian heating may reduce the fluid density and increases the momentum boundary layer thickness, as a result, the velocity increases within the boundary layer. Further, the behavior of Grashof number and conjugate parameter on the velocity profiles are quite identical with that found in figures 7 and 8 of Jain [33]. Figure 6 demonstrates the effect of time
on the velocity profiles. It is found that velocity increases with an increase in
. The velocity profiles for different values of phase angle
are depicted in Figure 7. It is found that the velocity shows an oscillatory behavior. The oscillations near the plate are of great significance; however, these oscillations reduce for large values of the independent variable
and approach to zero as
approaches to infinity. The numerical results for velocity and temperature are computed in Table 1 and Table 2 respectively. Furthermore, Figures 8 and 9 are prepared to show the comparison of the present analytical results for velocity and temperature given by equations (24) and (23) with the numerical results in Table 1 and Table 2. It is found that the analytical results are quite identical with the numerical results.
Figure 3. Velocity profiles for different values of.

when
Figure 7. Velocity profiles for different values of.

when
Figure 9. Comparison of exact solution of temperature with numerical solution, when.

Figure 4. Velocity profiles for different values of.

when
Figure 5. Velocity profiles for different values of.

when
Figure 8. Comparison of exact solution of velocity with numerical solution, when.

Figure 6. Velocity profiles for different values of.

when
Table 1. Numerical results for velocity.
|
|
|
|
|
|
|
|
| 0 | 0.2 | 0.6 | 0.3 | 3 | 0.5 |
|
0.500 |
| 1 | 0.2 | 0.6 | 0.3 | 3 | 0.5 |
|
0.208 |
| 2 | 0.2 | 0.6 | 0.3 | 3 | 0.5 |
|
0.035 |
| 1 | 0.4 | 0.6 | 0.3 | 3 | 0.5 |
|
0.417 |
| 2 | 0.4 | 0.6 | 0.3 | 3 | 0.5 |
|
0.162 |
| 1 | 0.2 | 1.0 | 0.3 | 3 | 0.5 |
|
0.176 |
| 2 | 0.2 | 1.0 | 0.3 | 3 | 0.5 |
|
0.020 |
| 1 | 0.2 | 0.6 | 0.5 | 3 | 0.5 |
|
0.187 |
| 2 | 0.2 | 0.6 | 0.5 | 3 | 0.5 |
|
0.029 |
| 1 | 0.2 | 0.6 | 0.3 | 5 | 0.5 |
|
0.236 |
| 2 | 0.2 | 0.6 | 0.3 | 5 | 0.5 |
|
0.040 |
| 1 | 0.2 | 0.6 | 0.3 | 3 | 1.0 |
|
0.283 |
| 2 | 0.2 | 0.6 | 0.3 | 3 | 1.0 |
|
0.047 |
| 1 | 0.2 | 0.6 | 0.3 | 3 | 0.5 |
|
0.042 |
| 2 | 0.2 | 0.6 | 0.3 | 3 | 0.5 |
|
0.008 |
Table 2. Numerical results for temperature.
|
|
|
|
|
| 0 | 0.2 | 0.3 | 0.5 | 0.656 |
| 1 | 0.2 | 0.3 | 0.5 | 0.140 |
| 2 | 0.2 | 0.3 | 0.5 | 0.016 |
| 0 | 0.4 | 0.3 | 0.5 | 1.155 |
| 1 | 0.4 | 0.3 | 0.5 | 0.396 |
| 0 | 0.2 | 0.5 | 0.5 | 0.379 |
| 1 | 0.2 | 0.5 | 0.5 | 0.020 |
| 0 | 0.2 | 0.3 | 1.0 | 2.827 |
| 1 | 0.2 | 0.3 | 1.0 | 0.893 |
The variation of temperature for different values of Prandtl number
are plotted in Figure 10. It is found that temperature of the fluid decreases with increasing values of
. This is in agreement with the physical fact that with increasing Prandtl number, the viscosity of the fluid increases, the fluid become more thick which reduces the heat transfer. From Figure 11, it is observed that an increase in the conjugate parameter for Newtonian heating increases the thermal boundary layer thickness and as a result the surface temperature of the plate increases. It is also observed that there is a sharp rise in temperature with the increase of conjugate parameter. Note that the variations in temperature due to conjugate parameter are identical to the published work of [31], [33]. It is observed from Figure 12 that the fluid temperature increases with an increase in time
.
Figure 10. Temperature profiles for different values of.

when
Figure 11. Temperature profiles for different values of.

when
Figure 12. Temperature profiles for different values of.

when
On the other hand, variation of skin friction and Nusselt number verses time are plotted in Figures 13–15 for various parameters of interest. It is found from Figure 13 that skin friction increases with increasing value of
whereas it decreases with increasing value of
and
, when
and
are fixed. From Figure 14, it is noticed that the skin friction increases with increasing values of conjugate parameter
, while reverse effect is observed for phase angle
. Finally, the Nusselt number increases as
and
are increased as shown in Figure 15. Finally, for the comparison of the present results with those existing in the literature we have plotted Table 3. It is found that for
, our results are quite identical with those obtained in [32], when
(in the absence of thermal radiation).
Figure 13. Skin-friction variation for different values of.

when
Figure 14. Skin-friction variation for different values of.

when
Table 3. Comparison of skin friction calculated in the present work at
and in [32], when
.
|
|
|
|
|
Present Results | Results of [32] |
| 0.01 | 0.35 | 5 | 1 | 0 | 5.5818 | 5.5818 |
| 0.02 | 0.35 | 5 | 1 | 0 | 3.8620 | 3.8620 |
| 0.01 | 0.50 | 5 | 1 | 0 | 5.5956 | 5.5956 |
| 0.01 | 0.35 | 10 | 1 | 0 | 5.5218 | 5.5218 |
| 0.01 | 0.35 | 5 | 2 | 0 | 5.5027 | 5.5027 |
| 0.01 | 0.35 | 5 | 1 |
|
4.4819 | 4.4819 |
Conclusions
In this paper, exact solutions of unsteady boundary layer flow and heat transfer of a Casson fluid past an oscillating vertical plate with Newtonian heating are obtained using the Laplace transform technique. The results obtained have shown that the effect of number increases the velocity but reduces the skin friction. However, the velocity is decreased when the Casson parameter is increased. Moreover, in the particular case of Newtonian fluid, the analytical results obtained in the present work were compared with those available in the literature, obtaining an excellent agreement with those given in [32]. A significant finding of this study is that flow separation can be controlled by increasing the value of Casson fluid parameter as well as by increasing Prandtl number.
Data Availability
The authors confirm that all data underlying the findings are fully available without restriction. All relevant data are within the paper.
Funding Statement
The authors gratefully acknowledge the financial supports received from the Universiti Malaysia Pahang, Malaysia, through vote numbers RDU121302 and RDU131405. The corresponding author is also grateful to Majmaah University Saudi Arabia for the financial support through research project. The funders had no role in study design, data collection and analysis, decision to publish, or preparation of the manuscript.
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Associated Data
This section collects any data citations, data availability statements, or supplementary materials included in this article.
Data Availability Statement
The authors confirm that all data underlying the findings are fully available without restriction. All relevant data are within the paper.












































