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Water-based hybrid nanofluid flow containing CNT nanoparticles over an extending surface with velocity slips, thermal convective, and zero-mass flux conditions

  • Humaira Yasmin EMAIL logo , Rawan Bossly , Fuad S. Alduais , Afrah Al-Bossly and Anwar Saeed
Published/Copyright: February 13, 2025

Abstract

This study computationally examines the water-based hybrid nanofluid flow with the impacts of carbon nanotubes on an elongating surface. The flow is influenced by velocity slip constraints, zero-mass flux conditions, and thermal convection. Magnetic effects are applied to the flow system in the normal direction. The activation energy and chemical reactivity effects are used in the concentration equation. The modeled equations have been evaluated numerically through the bvp4c technique after conversion to dimensionless form through a similarity transformation approach. It has been discovered in this work that with expansion in magnetic and porosity factors, the velocities declined. Augmentation in the ratio factor has declined the primary flow velocity while supporting the secondary flow velocity. Thermal profiles have intensified with progression in the Brownian motion factor, thermal Biot number thermophoresis factor, and exponential heat source and radiation factors. Concentration distribution has escalated with the activation energy factor and has declined with an upsurge in Schmidt number and chemical reaction factors. The impact of an upsurge in the thermophoresis factor enhances the concentration distribution, while the upsurge in the Brownian motion factor exhibits a reducing impact on concentration distribution. To ensure the validation of this work, a comparative study is conducted in this work with a fine agreement among the current and established datasets.

1 Introduction

The mixing of small-sized particles into a base fluid for the purpose of supplementing its thermal features results in a nanofluid. This idea was floated initially by Choi and Eastman [1] for enhancing the thermal conductance of normal fluid. Nanofluid flow is studied for its potential to enhance rates of thermal transference in various applications, including cooling of electronic devices, automotive and industrial heat exchangers, and biomedical applications as noticed by Anjum et al. [2] and Khan et al. [3]. Hybrid nanofluid flow involves two or more dissimilar kinds of nanoparticles distributed in a pure fluid, combining the benefits of different materials to further enrich the thermal features of the fluid. For instance, a hybrid nanofluid might include a mixture of metallic nanoparticles, such as copper, and non-metallic nanoparticles, such as graphene, to exploit the extraordinary thermal features of copper and the excellent mechanical and thermal properties of graphene as noticed by Sriharan et al. [4]. Analytical evaluation of temperature in living tissues is performed by Hobiny et al. [5] using the TPL bio-heat model, supported by experimental verification. Their study focuses on understanding thermal behavior in biological tissues, integrating theory and practical data. The results of their work validate the model’s accuracy in predicting temperature distributions, crucial for medical applications such as hyperthermia therapy and diagnostics. Alzahrani and Abbas [6] evaluated analytically the active living tissues’ thermal damage subject to laser irradiations. The synergy between different nanoparticles can lead to improved thermal conductivity, stability, and thermal flow management in comparison with single-component nanofluids [7]. Ibrahim et al. [8] observed that the flow behavior and heat transference characteristics of hybrid nanofluids are influenced by the connections between the diverse kinds of nanoparticles, their concentration ratios, and the properties of pure liquid. Applications include more efficient cooling systems in electronics, automotive radiators, and advanced thermal management systems in renewable energy technologies [9]. Both nanofluids and hybrid nanofluids significantly impact heat transfer by enhancing the thermal conductance and convective heat transfer coefficients of pure fluid [10]. This leads to improved efficiency in heat exchangers and cooling systems, allowing for more effective thermal management. The increased thermal conductivity and improved convective heat transfer result in reduced energy consumption and better performance in systems ranging from microelectronics cooling to industrial heat exchangers and renewable energy applications. Marin et al. [11] numerically examined a nonlinear hyperbolic bio-thermal model under various flow conditions to treat tumor cells. The study aimed to understand the interaction between heat transfer and biological tissue in the context of tumor treatment. Their findings contribute to optimizing therapeutic strategies, enhancing the understanding of heat-induced cell damage, and improving treatment protocols for tumors. The investigation of Saeed and Abbas [12] focuses on mathematical models of bio-heat transfer to analyze the transient phenomena in spherical tissue caused by a laser heat source. Their study aims to understand how the tissue responds to the heat over time, considering the impact of the laser on the thermal behavior of the biological material. Hobiny and Abbas [13] examined the nonlinear analysis of the dual-phase lag model of bio-heat in living tissues under laser irradiation. Their work focuses on understanding heat transfer dynamics, accounting for time delays in heat flux and temperature gradient responses, and offering insights into thermal behavior during laser–tissue interactions for medical and scientific applications.

Porous media describe the materials containing pores within their structure, which allow fluids (liquids or gases) to pass through. These materials occur naturally, such as soils, rocks, and biological tissues, or engineered, such as ceramics, foams, and certain types of filters. The pores in porous media vary significantly in size, shape, and distribution, influencing the material’s permeability and porosity. Fluid flow in porous media involves the movement of fluids through materials that contain numerous pores or voids and is primarily governed by Darcy’s law as observed by Yang et al. [14]. Khalil et al. [15] proved that in permeable media, the fluid flow is affected by the porosity and the permeability of the material, as well as the viscosity and density of the fluid. Wang et al. [16] studied the mass and thermal transportations of thin-film flow on a permeable medium with impressions of the Buongiorno model. Pop et al. [17] discussed time-based flow and thermal transference for mono and hybrid nanoparticle flow on a permeable surface and noted that with progression in porosity factor, there has been a decline in velocity distribution while a growth has noted thermal distribution. In practical applications, such as groundwater hydrology, oil recovery, and filtration, the performance of fluid flow in porous media is crucial for heightening the efficacy and effectiveness of a process [18]. The motion of fluid on a permeable media significantly affects thermal and velocity panels within the medium as noted by Ali et al. [19]. For the heterogeneous nature of permeable media, the fluid velocity is not uniform and varies with the pore size and distribution. This non-uniformity leads to complex velocity profiles, where fluid may accelerate through larger pores and slowdown in smaller ones, creating a range of velocities within the medium. Temperature profiles in porous media are also impacted by the flow as noted by Nadeem et al. [20], the thermal conductance of the porous medium, combined with the convective heat transfer of the fluid, determines the temperature distribution.

The key principle of MHD is the relationship between the magnetic fields and the fluid’s electrical conductivity, which induces currents and affects the fluid motion. Governed by the combined principles of fluid dynamics and electromagnetism, MHD finds applications in astrophysics, fusion reactors, and electromagnetic pumps [21,22]. Ahmad et al. [23] studied the significance of multi-slip constraints with impacts of MHD on fluid flow subject of nonlinear radiations thermally and chemically reactivity. Lone et al. [24] discussed a semi-numerical approach for the evaluation of blood-based trihybrid MHD fluid flow on a bi-directional extending sheet with flow slip constraints. In MHD, the existence of a magnetic field considerably influences the velocity and thermal distributions of the conducted fluid as observed by Tarakaramu et al. [25]. Mahesh et al. [26] proved that the Lorentz force, resulting from the interaction between the magnetic field and the induced electric current, acts on the fluid, modifying its flow characteristics. In some cases, MHD also induces secondary flows, such as swirling or rotational movements, subject to the alignment and strength of the magnetic field [27]. Moreover, Lund et al. [28] noted that the occurrence of the magnetic field in a fluid alters the heat transfer mechanisms. However, in some scenarios, it also suppresses convective motion, leading to increased reliance on conduction for heat transfer. Furthermore, as studied by Nawaz et al. [29], MHD can be utilized to control and optimize thermal management in various applications, such as cooling systems in fusion reactors or electromagnetic braking in metallurgy. The overall impact on velocity and thermal distributions depends on factors such as magnetic field strength, fluid properties, and flow conditions, making MHD a versatile tool in engineering and scientific research. Hobiny and Abbas [30] examined experimentally the thermal response of cylindrical tissues subject to laser irradiations. Abbas et al. [31] evaluated analytically the model of bio-heat for spherical tissues using the impacts of laser irradiations.

Brownian motion describes the random movement of particles mixed in a fluid, resulting from collisions of the molecules of fluids. This phenomenon is more pronounced at smaller scales, such as nanoparticles, where thermal fluctuations cause significant particle displacement. Brownian motion affects fluid dynamics by enhancing the mixing and dispersion of particles within the fluid as proved by Madkhali et al. [32]. Thermophoresis is the migration of particles in a fluid for thermal gradient in the flow phenomenon. Particles tend to move from hotter to cooler regions, driven by the imbalance in kinetic energy between particles in different thermal zones. Both thermophoresis and Brownian motion considerably affect heat and concentration transfer in fluid systems [33]. Shahzad et al. [34] studied that the Brownian motion enhances thermal conductance by promoting the uniform distribution of nanoparticles, leading to better heat transfer in nanofluids. Thermophoresis, in contrast, creates a thermal gradient-driven particle movement, which either enhances or inhibits heat transfer subject to the direction of the temperature gradient relative to the desired heat flow [35]. Brownian motion increases particle dispersion, improving the mixing and homogeneity of the solute concentration in the fluid. This leads to more efficient mass transfer and reaction rates in processes such as chemical reactions or pollutant dispersion. Sharma et al. [36] proved that thermophoresis effects contribute to concentration gradients by causing particles to migrate toward cooler regions, affecting the local concentration profiles and potentially enhancing separation processes or creating regions of high particle concentration. Thabet et al. [37] studied thermal augmentation for MHD fluid flow with impacts of Brownian and thermophoretic diffusions. Hanı et al. [38] discussed the impacts of Brownian and thermophoretic diffusions on boundary-layer MHD fluid flow on an elongating surface. Waqas et al. [39] examined computationally the Brownian motion and thermophoretic effects on gyrating nanomaterial fluid flow with activation energy.

Thermal radiation is electromagnetic radiation emitted by a body due to its temperature. It encompasses a range of wavelengths, including infrared, visible, and ultraviolet light, with intensity and wavelength distribution dependent on the body’s temperature. Thermal radiation significantly impacts the thermal characteristics distribution within the fluid and the boundaries it interacts with [40]. This combined heat transfer mechanism is essential in high-temperature environments, such as combustion chambers, solar collectors, and industrial furnaces. Essam and Abedel-AaL [41] proved that thermal radiation enhances heat transfer by providing a surplus mode of energy transfer, supplementing conduction and convection. Pandey et al. [42] studied thermally radiative and mixed convective fluid flow on a surface. Gul et al. [43] discussed the thin flow of carbon nanotubes (CNTs) with magnetic effects on a belt and have proved that pressure profiles, velocity, and thermal transmission have affected more in the case of multi-walled carbon nanotubes (MWCNTs). Alrehili [44] inspected augmentation in heat transfer for nanoparticle fluid flow on a nonlinear elongating surface with thermal radiations. Wang et al. [45] proved that in high-temperature applications, radiative heat transfer dominates, leading to more uniform temperature distributions and improved thermal efficiency. The presence of thermal radiation affects the fluid’s temperature gradients, often resulting in increased heat transfer rates as noted by Goud et al. [46]. Muhammad et al. [47] inspected the slip flow of mixed convective mono/hybrid nanofluids on a curved sheet. In their study, the authors have conducted a comparative analysis to ensure the precision of their results established. This is particularly important in systems where maintaining high thermal performance is critical, such as in the thermal management of electronic devices, high-temperature industrial processes, and energy systems such as solar thermal collectors. By optimizing the role of thermal radiation, engineers can design more efficient thermal systems with improved performance and energy savings. Swain et al. [48] studied computationally 3D Maxwell fluid flow on a stretching surface with impacts of thermal radiations. Hamad et al. [49] discussed the third-grade fluid flow on an inclined elongating surface with magnetic and thermally radiative effects. Hayat et al. [50] studied the Eyring Powell fluid flow with impacts of nanoparticles on exponential elongating sheet. In their work, the authors have conducted a comparative investigation to ensure the validity of the method used for the solution.

Single-walled carbon nanotubes (SWCNTs) are geometrical structures in cylindrical form with a single layer of carbon atoms arranged in a hexagonal lattice. SWCNTs have remarkable electrical, thermal, and mechanical properties due to their unique structure, making them highly conductive and strong. They are used in various applications, including electronics, materials science, and nanotechnology. SWCNTs, with their single-layer structure, offer superior thermal conductivity along their length, making them ideal for applications requiring efficient heat dissipation. They can be used in thermal interface materials and as fillers in composite materials to improve thermal management in electronics and other devices. MWCNTs consist of numerous concentric layers of carbon atoms, forming a series of coaxial cylinders around a central hollow core. MWCNTs are less conductive than SWCNTs due to interlayer interactions. They offer greater mechanical strength and are easier to produce in large quantities. MWCNTs find applications in composite materials, conductive films, and additives to enhance the properties of various materials. MWCNTs, while slightly less efficient than SWCNTs due to interlayer phonon scattering, still provide excellent thermal conductivity. Their larger diameter and multiple layers make them robust and suitable for bulk applications. MWCNTs enhance the thermal conductivity of polymers and other matrices when used as fillers, improving the performance of thermal management systems in various industrial applications. Both types of CNTs are critical in developing advanced materials for efficient heat transfer and thermal regulation. The adoption of convective and zero-mass flux conditions in this analysis is motivated by their practical applications. Convective conditions account for heat exchange between fluid and the surrounding medium, which is critical in systems for improved heat transfer, such as solar collectors, heat sinks, and cooling devices for electronics. In this analysis, single and MWCNT hybrid nanofluid flow is examined on a bi-directional extending sheet. Velocity slips, thermal convective, and zero-mass flux conditions are executed to examine the hybrid nanofluid flow. Also, thermal radiation, exponential heat source, Brownian motion, thermophoresis, chemical reaction, and activation energy effects have been used. In this analysis, the authors are encouraged to investigate how the CNT nanoparticles influence the flow behavior of the water-based hybrid nanofluid flow with numerous constraints, such as velocity slips, thermal convective, and zero-mass flux conditions. How do external factors such as exponential heat source, Brownian motion, thermal radiation, and thermophoresis influence the behavior and efficiency of the water-based hybrid nanofluid flow? What are the effects of the chemical reaction and activation energy on the performance of hybrid nanofluid flow? To answer these questions, the mathematical formulation of the proposed problem is presented in Section 2. The numerical solution of the proposed mathematical model is presented in Section 3. Validation of the present model with published results is presented in Section 4. The present results are discussed in Section 5. The final concluding remarks are shown in Section 6.

2 Problem formulation

A three-dimensional flow of hybrid nanofluid containing SWCNT and MWCNT over an extending sheet using porous media is considered. A Cartesian coordinate system with flow components u , v , w along x , y , z directions is chosen to investigate the hybrid nanofluid flow. Moreover, u w ( x ) = a x and v w ( y ) = b y (with a and b as fixed values) are stretching velocities along x- and y-axes. The z-direction is normal to the xy-plane. The conditions of flow slip ( u slip and v slip ) are also executed in this analysis. The magnetic effect with strength B 0 is employed in a perpendicular direction to the flow system. The working fluid temperature is taken as T f such that ( T f > T w ). The free-stream temperature is denoted by T . The condition of zero-mass flux is applied such that the mass flow at the sheet surface is zero (i.e., C w = 0 ) [51,52,53]. Furthermore, the free-stream concentration is C . Also, the thermal radiation, Brownian motion, exponential heat source, thermophoresis, chemical reaction, and activation energy are used in this work. Following the aforementioned assumptions, the leading equations can be expressed as follows [54,55] (Figure 1):

(1) u x + v y + w z = 0 ,

(2) u u x + v v y + w w z = μ hnf ρ hnf 2 u z 2 μ hnf ρ hnf u K p σ hnf ρ hnf B 0 2 u ,

(3) u v x + v v y + w v z = μ hnf ρ hnf 2 v z 2 μ hnf ρ hnf v K p σ hnf ρ hnf B 0 2 v ,

(4) u T x + v T y + w T z = k hnf ( ρ C p ) hnf + 1 ( ρ C p ) hnf 16 σ T 3 3 k 2 T z 2 + 1 ( ρ C p ) hnf Q e ( T f T ) exp n a ν f z + ( ρ C p ) np ( ρ C p ) hnf D B δ C C z T z + T z 2 D T T ,

(5) u C x + v C y + w C z = D B 2 C z 2 + δ C D T T 2 T z 2 k r 2 ( C C ) T T m E a k B T ,

With physical conditions at boundaries [54]:

(6) u = u w ( x ) + u slip , v = v w ( y ) + v slip , w = 0 , k hnf T z = h f ( T f T ) , D B δ C C z + D T T T z = 0 at z = 0 , u 0 , v 0 , T T , C C as z .

Figure 1 
               Geometrical view of flow problem.
Figure 1

Geometrical view of flow problem.

The velocity slip conditions ( u slip and v slip ) are defined as

(7) u slip = Δ 1 u z , v slip = Δ 2 v z ,

where Δ 1 and Δ 2 are the slip constants.

The effective qualities of mono and hybrid nanofluids are enumerated as follows [53,56] (Table 1):

(8) μ hnf = μ f ( 1 κ 1 ) 2.5 ( 1 κ 2 ) 2.5 , ρ hnf = { ρ f ( 1 κ 1 ) + ρ N 1 κ 1 } ( 1 κ 2 ) + κ 2 ρ N 2 , ( ρ C p ) hnf = { ( ρ C p ) f ( 1 κ 1 ) + ( ρ C p ) N 1 κ 1 } ( 1 κ 2 ) + κ 2 ( ρ C p ) N 2 , k nf k f = k N 1 + 2 k f 2 κ 1 ( k f k N 1 ) k N 1 + 2 k f + κ 1 ( k f k N 1 ) , k hnf k nf = k N 2 + 2 k f 2 κ 2 ( k f k N 2 ) k N 2 + 2 k f + κ 2 ( k f k N 2 ) , σ nf σ f = σ N 1 + 2 σ f 2 ( σ f σ N 1 ) κ 1 σ N 1 + 2 σ f + ( σ f σ N 1 ) κ 1 , σ hnf σ nf = σ N 2 + 2 σ f 2 κ 2 ( σ f σ N 2 ) σ N 2 + 2 σ f + κ 2 ( σ f σ N 2 ) .

(9) u = a f ( ξ ) x , v = a g ( ξ ) x , w = ν f a ( g ( ξ ) + f ( ξ ) ) , θ ( ξ ) = T T T f T , χ ( ξ ) = C C C , ξ = a ν f z .

Table 1

Thermophysical features of SWCNT, MWCNT, and water [57]

Physical property Water SWCNT MWCNT
ρ [ kg m 3 ] 997.1 2,600 1,600
C p [ J kg 1 K 1 ] 4,179 425 796
k [ W m 1 K 1 ] 0.613 6,600 3,000
σ [ S m 1 ] 5.5 × 10‒6 5.96 × 107 2.38 × 106

So, Eq. (1) is satisfied identically, and the remaining equations are as follows:

(10) μ G ρ G f ( ξ ) + f ( ξ ) f ( ξ ) + f ( ξ ) g ( ξ ) f 2 ( ξ ) M σ G ρ G f ( ξ ) K μ G ρ G f ( ξ ) = 0 ,

(11) μ G ρ G g ( ξ ) + f ( ξ ) g ( ξ ) + g ( ξ ) g ( ξ ) g 2 ( ξ ) M σ G ρ G g ( ξ ) K μ G ρ G g ( ξ ) = 0 ,

(12) 1 ( ρ C p ) G ( k g + Rd ) θ ( ξ ) + Pr ( ρ C p ) G × f ( ξ ) θ ( ξ ) + g ( ξ ) θ ( ξ ) + Q Exp exp ( n ξ ) + Nb θ ( ξ ) χ ( ξ ) + Nt θ 2 ( ξ ) = 0 ,

(13) χ ( ξ ) + Nt Nb θ ( ξ ) + Sc f ( ξ ) χ ( ξ ) + Sc g ( ξ ) χ ( ξ ) ScKr ( 1 + β θ ( ξ ) ) N χ ( ξ ) exp E ( 1 + β θ ( ξ ) ) = 0 ,

with related conditions at the boundary as

(14) f ( 0 ) = 0 , f ( 0 ) = 1 + α 1 f ( 0 ) , f ( ) 0 , g ( 0 ) = 0 , g ( 0 ) = λ + α 2 g ( 0 ) , g ( ) 0 , k G θ ( 0 ) = Bi T ( 1 θ ( 0 ) ) , θ ( ) 0 , Nb χ ( 0 ) + Nt θ ( 0 ) = 0 , χ ( ) 0 .

Some emerging factors are encountered in the aforementioned equations that are mathematically described as follows:

(15) μ G = μ hnf μ f , ρ G = ρ hnf ρ f , σ G = σ hnf σ f , k G = k hnf k f , ( ρ C p ) G = ( ρ C p ) hnf ( ρ C p ) f , Sc = ν f D B , Pr = ν f ( ρ C p ) f k f , M = σ f B 0 2 a ρ f , K = μ f a ρ f K p , Rd = 16 σ T 3 3 k k f , Q Exp = Q t a ( ρ C p ) f , Kr = k r a , Bi T = h f k f ν f a , Nb = ( ρ C p ) np D B C δ C ( ρ C p ) f ν f , Nt = ( ρ C p ) np D T ( T f T ) ( ρ C p ) f T ν f , E = E a k B T , β = T f T T , α 1 = Δ 1 a ν f , α 2 = Δ 2 a ν f , Bi T = h f k f ν f a , λ = b a .

The physical description and ranges of these factors are given in Table 2.

Table 2

Symbolic and physical descriptions alongside default values of various factors

Symbol description Physical description Default value
M Magnetic factor 0.5
Rd Radiation factor 0.2
K Porosity factor 0.3
Q Exp Exponential heat source factor 0.2
Pr Prandtl number 6.2
Nb Brownian motion factor 0.2
Bi T Thermal Biot number 0.5
Sc Schmidt number 2.0
K r Chemical reaction factor 1.5
Nt Thermophoresis factor 0.1
λ Ratio factor 0.7
E Activation energy factor 1.0
α 1 Velocity slip factor along the x-direction 0.5
α 2 Velocity slip factor along the y-direction 0.5
β Temperature difference factor 1.0
n , N Power indexes 1.0

The main quantities of interest such as skin friction C f x , Nusselt number Nu x , and Sherwood number Sh x are described as follows:

(16) C f x = τ w x ρ f ( u w ( x ) ) 2 , C f y = τ w y ρ f ( v w ( y ) ) 2 , Nu x = x q w k f ( T f T ) ,

where

(17) τ w x = μ hnf u z z = 0 , τ w y = μ hnf v z z = 0 , q w = k hnf T z z = 0 16 σ 3 k T 4 z z = 0 .

Thus, Eq. (17) reduces as follows:

(18) C f x = μ G f ( 0 ) , C f y = μ G g ( 0 ) , Nu = ( k G + Rd ) ϑ ( 0 ) .

Above C f x = Re x C f x , C f y = Re x C f y , and Nu = Nu x Re x . Furthermore, Re x = u w ( x ) x ν f and Re x = u w ( x ) x ν f are the local Reynolds numbers.

3 Numerical solution

To acquire the numerical solution modeled equations, the bvp4c technique is chosen. This is a powerful technique that can solve highly nonlinear problems. The error tolerance of 10−6 is demarcated in the present case. To implement this technique, we must moderate the higher-order nonlinear problem to a first-order problem. Therefore, we assume that

(19) f = G ( 1 ) , f = G ( 2 ) , f = G ( 3 ) , f = G ( 3 ) , g = G ( 4 ) , g = G ( 5 ) , g = G ( 6 ) , g = G ( 6 ) , θ = G ( 7 ) , θ = G ( 8 ) , θ = G ( 8 ) , χ = G ( 9 ) , χ = G ( 10 ) , χ = G ( 10 ) .

(20) G ( 3 ) = G ( 1 ) G ( 3 ) + G ( 4 ) G ( 3 ) ( G ( 2 ) ) 2 M σ G ρ G G ( 2 ) K μ G ρ G G ( 2 ) μ G ρ G ,

(21) G ( 6 ) = G ( 1 ) G ( 6 ) + G ( 4 ) G ( 6 ) ( G ( 5 ) ) 2 M σ G ρ G G ( 5 ) K μ G ρ G G ( 5 ) μ G ρ G ,

(22) G ( 8 ) = Pr ( ρ C p ) G G ( 1 ) G ( 8 ) + G ( 4 ) G ( 8 ) + Q Exp exp ( n ξ ) + Nb G ( 8 ) G ( 10 ) + Nt ( G ( 8 ) ) 2 1 ( ρ C p ) G ( k g + Rd ) ,

(23) G ( 10 ) = Nt Nb G ( 8 ) + Sc G ( 1 ) G ( 10 ) + Sc G ( 4 ) G ( 10 ) ScKr ( 1 + β G ( 7 ) ) N G ( 9 ) exp E ( 1 + β G ( 7 ) ) ,

with boundary conditions:

(24) G INITAL ( 1 ) 0 , G INITAL ( 2 ) 1 α 1 G INITAL ( 3 ) , G FINAL ( 2 ) 0 , G INITAL ( 4 ) 0 , G INITAL ( 5 ) λ α 2 G INITAL ( 6 ) , G FINAL ( 5 ) 0 , k G G INITAL ( 8 ) + Bi T ( 1 G INITAL ( 7 ) ) , G FINAL ( 7 ) 0 , Nb G INITAL ( 10 ) + Nt G INITAL ( 8 ) 0 , G FINAL ( 9 ) 0 .

where the subscripts INITIAL and FINAL depict the initial as well as boundary conditions respectively.

4 Validation

This section portrays the validation of the current results against the published findings of Hayat et al. [58] and Dawar et al. [54] for variations in ratio, factor ( λ ). The results are compared for a special case of viscous fluid and the effects of magnetic field and porous media are ignored (i.e., M = K = κ 1 = κ 2 = 0 ). Furthermore, the effects of slip conditions are also ignored (i.e., α 1 = α 2 = 0 ). From this analysis, we have confirmed the correctness of the applied method and proposed model by comparing the present and published results (Table 3).

Table 3

Assessment of f ( 0 ) and g ( 0 ) results for variations in λ with published works of Hayat et al. [58] and Dawar et al. [54]

λ 0.0 0.2 0.4 0.6 0.8 1.0
f ( 0 ) Hayat et al. [58] 1.0 1.039495 1.075788 1.109946 1.142488 1.17372
Dawar et al. [54] 1.0 1.039495 1.075788 1.109946 1.142488 1.17372
Present results 1.00000001 1.03949504 1.07578796 1.10994683 1.14248856 1.17372081
g ( 0 ) Hayat et al. [58] 0.0 0.148736 0.349208 0.590528 0.866682 1.17372
Dawar et al. [54] 0.0 0.148736 0.349208 0.590528 0.866682 1.17372
Present results 0.0 0.148737 0.3492088 0.59052911 0.86668307 1.17372081

5 Discussion of results

This section deals with the physical explanation of the obtained results. A numerical investigation of the presented model is carried out by using the bvp4c approach. The obtained results are shown in Tables 4 and 5 and Figures 219. Table 4 shows the variation in C f x and C f y via M , K , λ , α 1 , and α 2 . The greater M enhances C f x and C f y . The higher magnetic factor upsurges both C f x and C f y (skin friction coefficients) due to the fact that the magnetic field induces the Lorentz forces that play a role against the motion of fluid particles, which results in an increase in wall shear stress. This causes a higher velocity gradient near the stretching surface, thus enhancing C f x and C f y . The greater K enhances C f x and C f y . In the presence of porous media, the hybrid nanofluid flow experiences opposing forces resulting in a greater velocity gradient at the sheet surface. This increasing velocity gradient leads to a higher wall shear stress, thus enhancing C f x as well as C f y . The greater λ enhances C f x and C f y . As the values of λ enhance, the velocity gradients along the x and y-axes also enhance. The enhanced velocity gradients increase the wall shear stresses, thus enhancing C f x as well as C f y . Furthermore, the higher slip factors ( α 1 and α 2 ) reduce and C f y . Where there is slip, the velocity gradients at the wall reduce due to the fact the fluid velocity is non-zero at the boundary-layer region. The hybrid nanofluid flow has a finite velocity relative to the stretching wall, reducing the velocity gradient. Table 5 shows the variation in Nu via M , Rd , Q Exp , and Bi T . The greater M enhances Nu . The higher magnetic field escalates the rate of heat transfer by modifying the velocity distribution through Lorentz force, which makes turbulence in the flow pattern, and as a result, the higher temperature gradient is determined. This effect contributes to a greater thermal flow rate in MHD flows. The greater Rd enhances Nu . Thermal radiation factor plays a vital role in heat transfer rate. The radiation factor upsurges the rate of heat transfer by adding an additional model of heat transfer, which upsurges the thermal flow rate at the sheet’s surface. The greater Q Exp enhances Nu . The exponential thermal source upsurges the rate of thermal flow by producing significant internal heat generation leading to a higher Nusselt number. The greater Bi T enhances Nu . The higher thermal Biot number enhances the heat transfer coefficient, which results in a greater rate of heat transfer. Therefore, the higher Bi T enhances Nu .

Table 4

Variation in C f x and C f y via M , K , λ , α 1 , and α 2

M K λ α 1 α 2 C f x C f y
0.1 0.8516042477 0.5763269827
0.2 0.8734369330 0.5931297604
0.3 0.8940778848 0.6089113376
0.4 0.9136374030 0.6237794707
0.1 0.8054190087 0.5403678859
0.2 0.8291931255 0.5589519547
0.3 0.8516042477 0.5763269827
0.4 0.8727793367 0.5926253582
0.1 0.8218044946 0.0710732979
0.2 0.8273012259 0.1467414673
0.3 0.8325488005 0.2263762744
0.4 0.8375798184 0.3094971954
0.1 1.275599036 0.5891556316
0.2 1.130153116 0.5850043243
0.3 1.017139509 0.5816102207
0.4 0.926366307 0.5787628053
0.1 0.863264420 0.8379983743
0.2 0.859535940 0.7503475045
0.3 0.856452974 0.6807050805
0.4 0.853846381 0.6238128749
Table 5

Variation in Nu via M , Rd , Q Exp , and Bi T

M Rd Q Exp Bi T Nu
0.1 0.2218436572
0.2 0.2311341996
0.3 0.2402463468
0.4 0.2492002974
0.1 0.1948013227
0.2 0.2123509435
0.3 0.2296660152
0.4 0.2467670551
0.1 0.1339609864
0.2 0.2123509435
0.3 0.2793823415
0.4 0.3386270997
0.1 0.0589262973
0.2 0.1081643585
0.3 0.1492616108
0.4 0.1835942815
Figure 2 
               Variation in 
                     
                        
                        
                           
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Figure 2

Variation in f ( ξ ) via M .

Figure 3 
               Variation in 
                     
                        
                        
                           
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                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        g^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           M
                        
                        M
                     
                  .
Figure 3

Variation in g ( ξ ) via M .

Figure 4 
               Variation in 
                     
                        
                        
                           
                              f
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        f^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           K
                        
                        K
                     
                  .
Figure 4

Variation in f ( ξ ) via K .

Figure 5 
               Variation in 
                     
                        
                        
                           
                              g
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        g^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           K
                        
                        K
                     
                  .
Figure 5

Variation in g ( ξ ) via K .

Figure 6 
               Variation in 
                     
                        
                        
                           
                              f
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        f^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           λ
                        
                        \lambda 
                     
                  .
Figure 6

Variation in f ( ξ ) via λ .

Figure 7 
               Variation in 
                     
                        
                        
                           
                              g
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        g^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           λ
                        
                        \lambda 
                     
                  .
Figure 7

Variation in g ( ξ ) via λ .

Figure 8 
               Variation in 
                     
                        
                        
                           
                              f
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        f^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           
                              
                                 α
                              
                              
                                 1
                              
                           
                        
                        {\alpha }_{1}
                     
                  .
Figure 8

Variation in f ( ξ ) via α 1 .

Figure 9 
               Variation in 
                     
                        
                        
                           
                              g
                              ′
                           
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        g^{\prime} (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           
                              
                                 α
                              
                              
                                 2
                              
                           
                        
                        {\alpha }_{2}
                     
                  .
Figure 9

Variation in g ( ξ ) via α 2 .

Figure 10 
               Variation in 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \theta (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           
                              
                                 Bi
                              
                              
                                 T
                              
                           
                        
                        {\text{Bi}}_{\text{T}}
                     
                  .
Figure 10

Variation in θ ( ξ ) via Bi T .

Figure 11 
               Variation in 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \theta (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Nb
                        
                        \text{Nb}
                     
                  .
Figure 11

Variation in θ ( ξ ) via Nb .

Figure 12 
               Variation in 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \chi (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Nb
                        
                        \text{Nb}
                     
                  .
Figure 12

Variation in χ ( ξ ) via Nb .

Figure 13 
               Variation in 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \theta (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Nt
                        
                        \text{Nt}
                     
                  .
Figure 13

Variation in θ ( ξ ) via Nt .

Figure 14 
               Variation in 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \chi (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Nt
                        
                        \text{Nt}
                     
                  .
Figure 14

Variation in χ ( ξ ) via Nt .

Figure 15 
               Variation in 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \theta (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           
                              
                                 Q
                              
                              
                                 Exp
                              
                           
                        
                        {Q}_{\text{Exp}}
                     
                  .
Figure 15

Variation in θ ( ξ ) via Q Exp .

Figure 16 
               Variation in 
                     
                        
                        
                           θ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \theta (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Rd
                        
                        \text{Rd}
                     
                  .
Figure 16

Variation in θ ( ξ ) via Rd .

Figure 17 
               Variation in 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \chi (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Sc
                        
                        \text{Sc}
                     
                  .
Figure 17

Variation in χ ( ξ ) via Sc .

Figure 18 
               Variation in 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \chi (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           Kr
                        
                        \text{Kr}
                     
                  .
Figure 18

Variation in χ ( ξ ) via Kr .

Figure 19 
               Variation in 
                     
                        
                        
                           χ
                           
                              
                                 (
                                 
                                    ξ
                                 
                                 )
                              
                           
                        
                        \chi (\xi )
                     
                   
                  via 
                  
                     
                        
                        
                           E
                        
                        E
                     
                  .
Figure 19

Variation in χ ( ξ ) via E .

Figures 2 and 3 show the impact of M on f ( ξ ) and g ( ξ ) . From the obtained results, we observed that higher M diminishes both f ( ξ ) and g ( ξ ) . As the magnetic factor enhances, there exists a Lorentz force that resists the flow of electrically conducting hybrid nanofluid when it moves through a magnetic field. Also, the higher Lorentz force reduces the momentum boundary-layer thickness causing a lessening in the velocity profiles of the hybrid nanofluid. Therefore, the greater magnetic factor reduces both f ( ξ ) and g ( ξ ) .

Figures 4 and 5 depict the effects of K on f ( ξ ) and g ( ξ ) . From the obtained results, we perceived that a greater K diminishes both f ( ξ ) and g ( ξ ) . Actually, the greater porosity factor enhances the skin friction coefficients as shown in Table 4. The greater friction force diminishes the momentum boundary-layer width and causes a decline in the velocity profiles in both directions ( f ( ξ ) , g ( ξ ) ). Therefore, the greater porosity factor reduces both f ( ξ ) and g ( ξ ) .

Figures 6 and 7 depict the effects of λ on f ( ξ ) and g ( ξ ) . From the obtained results, we observed that higher values of λ diminishes f ( ξ ) while upsurges g ( ξ ) . By definition, the ratio parameter has a direct relation with the stretching constant of the y-directional velocity ( λ b ) and inverse relation with the stretching constant of the x-directional velocity ( λ 1 / a ). As the ratio factor enhances, then the y-directional velocity enhances, which results in higher-velocity profile along the y-direction. In contrast, as the ratio factor enhances, then the x-directional velocity reduces, which results reduction in the velocity profile in the x-direction. Therefore, the higher values of λ reduces f ( ξ ) while increases g ( ξ ) .

Figures 8 and 9, respectively, portray the impressions of the velocity slip parameter α 1 (along the x-axis) on primary velocity f ( ξ ) and velocity slip parameter α 2 (along the y-axis) on secondary velocity g ( ξ ) . As α 1 and α 2 increase along both the coordinates axes, it corresponds to a reduction in f ( ξ ) and g ( ξ ) . This phenomenon is physically observed near the boundary layer of a fluid in contact with a surface where slip conditions hold, like in microfluidics or rarefied gas flows. The velocity slips account for the deviation from the normal no-slip boundary condition, indicating that the fluid velocity at the surface is not zero but rather a fraction of the bulk flow velocity. Consequently, this slip reduces the overall momentum transfer from the fluid to the surface, leading to retardation in the primary and secondary flow velocities. These retardations are critical in applications involving high-precision fluid mechanics, as it impacts the efficiency and performance of fluid systems, necessitating careful consideration in the design and analysis of such systems.

Figure 10 depicts the influences of thermal Biot number Bi T on thermal distribution θ ( ξ ) . Clearly, Bi T is a dimensionless parameter that depicts the ratio of interior heat resistance to the exterior heat resistance between the fluid particles and their surroundings. As Bi T increases, it indicates a higher internal resistance to heat transfer compared to the external resistance. Physically, this means that the temperature gradient in the fluid becomes more significant, causing a more prominent thermal distribution. When Bi T is low, the fluid is assumed to have a nearly uniform temperature, as the external heat transfer dominates. Conversely, as Bi T grows, the internal temperature gradients become more substantial, causing variations in temperature throughout the fluid flow. This augmentation in θ ( ξ ) with increasing Biot number is critical in heat transfer analysis, influencing the design and performance of many thermal systems.

Figure 11 depicts the effects of the Brownian motion factor Nb on thermal panels θ ( ξ ) . As Nb increases, there is a corresponding augmentation in θ ( ξ ) within that fluid. Brownian motion refers to the random, movement of fluid particles suspended in a fluid, resulting from collisions with the fluid’s molecules. Physically, as the intensity of Brownian motion grows, the particles facilitate greater heat transfer through their constant movement, effectively spreading thermal energy more evenly throughout the medium. This phenomenon is particularly significant in nanoscale systems and colloidal suspensions, where particle dynamics play a crucial role in heat conduction. The increased thermal distribution due to enhanced Brownian motion is vital for applications in microfluidics, nanotechnology, and biochemical processes, where precise control over temperature and efficient heat dissipation are essential for optimal performance and reliability.

Figure 12 depicts the influences of Brownian motion factor Nb on χ ( ξ ) .The impact of an upsurge in Nb on χ ( ξ ) exhibits a reducing impact. The concentration distribution is reduced because higher Nb arises from the increased nanoparticles movement within the hybrid nanofluid flow, which results in an enhancement in nanoparticle diffusion. This diffusion of nanoparticles smoothens the concentration gradient by redistributing the nanoparticles more uniformly throughout the hybrid nanofluid. As a result, a higher Nb leads to a reduction in the concentration distribution. Therefore, the higher Nb reduces χ ( ξ ) .

Figure 13 depicts the influences of Nt (thermophoresis factor) on thermal distribution θ ( ξ ) with growth in θ ( ξ ) against variations in Nt . Thermophoresis is actually the motion of particles from zones of higher to lower temperatures due to temperature gradients. When thermophoresis factor Nt increases, the force driving the particle movement becomes stronger. Physically, this enhanced movement contributes to a more effective redistribution of particles, which carry thermal energy across the fluid. As these particles move from hot to cold regions, they facilitate a more uniform temperature distribution by transferring heat. Hence, augmentation in Nt causes the corresponding upsurge in θ ( ξ ) as portrayed in Figure 13.

Figure 14 depicts the influences of Nt on concentration distribution χ ( ξ ) . The impact of an upsurge in Nt on χ ( ξ ) exhibits a twofold behavior, characterized by an initial decline followed by an augmentation. On the interval 0 ξ < 0.8 , the enhanced movement of particles from hot to cold regions causes a drop in χ ( ξ ) . This occurs because particles are being driven away from the hot regions at the surface of the bi-directional elongating sheet, creating a weakening zone and increasing concentration gradients. However, as Nt continues to rise into the higher range on the interval 0.8 ξ 1.0 , the particle movement becomes more prominent, and the particles begin to accumulate in the cooler regions. This accumulation leads to an upsurge in χ ( ξ ) as depicted in Figure 14.

The impact of exponential thermal source factor Q Exp on thermal distribution θ ( ξ ) with augmentation in θ ( ξ ) for variations in Q Exp is depicted in Figure 15. Actually, Q Exp represents a heat source whose intensity increases exponentially. Physically, this means that as the thermal source factor grows, the amount of heat being introduced into the system rises rapidly. This rapid increase in heat input enhances the temperature gradients within the medium, leading to a more extensive thermal distribution. The heat spreads more effectively throughout the fluid, creating broader and more prominent temperature profiles θ ( ξ ) . This phenomenon is particularly important in applications involving laser heating, combustion processes, and nuclear reactions where controlling the distribution of heat is crucial for efficiency and safety. The augmented thermal distribution due to the exponential thermal source factor significantly impacts the thermal management, material properties, and overall performance of various industrial and scientific systems.

The impact of thermal radiation factor Rd on thermal distribution θ ( ξ ) with augmentation in θ ( ξ ) against variations in Rd is depicted in Figure 16. Actually, Rd quantifies the effects of thermal radiation, so as this factor increases, the contribution of radiative heat transfer becomes more significant. Physically, this means that more thermal energy is being radiated and absorbed by the fluid, enhancing the overall heat distribution. The radiative heat transfer is particularly effective over larger distances compared to conduction and convection, allowing for a more uniform temperature spread even in less conductive fluid. Hence, growth in the thermal radiation parameter Rd results in augmentation in thermal distribution θ ( ξ ) as depicted in Figure 16.

The influence of Schmidt number Sc on χ ( ξ ) is depicted in Figure 17, where growth in Sc has resulted in retardation in χ ( ξ ) . Actually, the Schmidt number Sc describes the ratio of momentum to mass diffusivity. When Sc upsurges, it specifies that the fluid’s viscosity is high relative to its mass diffusivity, meaning that the fluid’s ability to diffuse momentum is much greater than its ability to diffuse mass. Physically, this results in slower mixing and spreading of species within the fluid. In the scenario of fluid flow on the bi-directionally elongating sheet, this high Schmidt number means that the concentration boundary layer becomes thinner, and mass transfer from the sheet into the fluid is less efficient. The fluid’s high viscosity relative to its mass diffusivity inhibits the dispersion of solute particles, leading to the retardation of χ ( ξ ) . This behavior is crucial in applications involving chemical reactions, separation processes, and coating flows, where precise control over mass transfer and concentration profiles is essential for achieving optimal performance and efficiency.

The influence of chemical reactivity parameter Kr on concentration distribution χ ( ξ ) is depicted in Figure 18, where progression in Kr is resulted in hindrance in χ ( ξ ) . The chemical reactivity factor Kr quantifies the rate at which a chemical species reacts within the fluid. As Kr increases, the rate of reaction becomes faster. Physically, this means that the reactive species are consumed more quickly near the surface of the elongating sheet, reducing their concentration in that region. This rapid consumption creates steep concentration gradients and hinders the spread of the species throughout the fluid. Consequently, χ ( ξ ) becomes more localized and less uniform. In the case of fluid flow on the bi-directionally elongating sheet, the elongation tends to stretch and thin the boundary layer, but the high reactivity exacerbates the reduction of reactants near the surface, leading to further retardation in their distribution. This phenomenon is significant in industrial processes involving catalysis, coating technologies, and material synthesis, where controlling the concentration profiles and reaction rates is essential for optimizing efficiency, product quality, and process stability.

The impacts of activation energy factor E on concentration distribution χ ( ξ ) are depicted in Figure 19, where progression in E has resulted in expansion in χ ( ξ ) . Actually, E characterizes the energy barrier that reactant molecules must overcome to undergo a chemical reaction. As E increases, the activation energy barrier becomes higher, meaning that fewer molecules possess the necessary energy to react. Physically, this leads to a reduction in the rate of chemical reactions near the surface of the elongating sheet, allowing reactants to accumulate more readily in that region. The higher E effectively hinders the alteration of reactants into products, causing an augmentation in their concentration distribution near the sheet’s surface. In the case of fluid flow on bi-directionally elongating sheets, this phenomenon is particularly prominent due to the stretching and thinning of the boundary layer, which enhances the accumulation of reactants. Therefore, growth in E is responsible for augmentation in χ ( ξ ) as portrayed in Figure 19.

6 Conclusions

This work investigates computationally the water-based hybrid nanofluid flow with impacts of CNTs on an elongating surface. The flow is influenced by velocity slip constraints, zero-mass flux conditions, and thermal convection. A magnetic field of specific strength is applied to the flow system in the normal direction. The activation energy and chemical reactivity effects have been used in the concentration equation. The modeled equations have been evaluated numerically through the bvp4c technique after conversion to dimensionless form through the similarity transformation approach. The novelty of this analysis lies in a comprehensive investigation of hybrid nanofluid flow containing CNTs, incorporating velocity slips, and thermal convective and zero-mass flux conditions. The bvp4c solver ensures higher accuracy and consistency in solving the BVPs, with validation achieved through a comparative analysis presenting a robust agreement with the existing studies. A detailed investigation of the work has revealed that:

  • With an upsurge in magnetic and porosity factors, the velocities profiles are declined.

  • Augmentation in ratio factor has declined the primary velocity profile while supported by the secondary velocity profile.

  • Higher values of velocity slip factor along x- and y-axes have retarded both the primary and secondary velocities.

  • Thermal distribution has intensified with progression in Brownian motion factor, thermal Biot number thermophoresis factor, and exponential heat source and radiation factors.

  • Concentration distribution has escalated with the activation energy factor and has declined with the upsurge in Schmidt number and chemical reactivity factor.

  • The impact of an upsurge in the thermophoresis factor enhanced the concentration distribution, while the upsurge in the Brownian motion factor reduced the concentration distribution.

  • To ensure the validation of current work, a comparative study has been conducted in this work with a fine agreement among the current and established datasets.

  • Growth in magnetic, ratio, and porosity factors cause augmentation in the skin frictions along primary and secondary directions.

Acknowledgments

This work was supported by the Deanship of Scientific Research, the Vice Presidency for Graduate Studies and Scientific Research, King Faisal University Saudi Arabia (Grant No. KFU250260). This study was supported via funding from Prince Sattam bin Abdulaziz University Project Number (PSAU/2024/R/1446).

  1. Funding information: This work was supported by the Deanship of Scientific Research, the Vice Presidency for Graduate Studies and Scientific Research, King Faisal University Saudi Arabia (Grant No. KFU250260). This study was supported via funding from Prince Sattam bin Abdulaziz University Project Number (PSAU/2024/R/1446).

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors state no conflict of interest.

  4. Data availability statement: The datasets generated and/or analyzed during the current study are available from the corresponding author on reasonable request.

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Received: 2024-11-07
Revised: 2025-01-02
Accepted: 2025-01-23
Published Online: 2025-02-13

© 2025 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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