Startseite Naturwissenschaften Thermal and stability analysis of silver–water nanofluid flow over unsteady stretching sheet under the influence of heat generation/absorption at the boundary
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Thermal and stability analysis of silver–water nanofluid flow over unsteady stretching sheet under the influence of heat generation/absorption at the boundary

  • Nehad Ali Shah , Areej Abdullah Alabduljabbar , Zeeshan und Se-Jin Yook EMAIL logo
Veröffentlicht/Copyright: 10. Juli 2025
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Abstract

The aim of this study is to examine a numerical analysis of nanofluid (NF) containing silver (Ag) nanoparticles using water (H2O) as a host fluid through an unsteady stretching sheet with stability analysis. The thermal performance of the NF is also examined in the present study, which has a significant role in aerodynamics and space sciences. A mathematical framework is created for the Ag nanofluids in terms of partial differential equations (PDEs). Through resemblance variables, the system of PDEs is made dimensionalized in terms of ordinary differential equations and then computed by a boundary-value problem fourth-order algorithm. The impacts of the physical aspects on the flow features are reported via graphs and tables. The findings show that multiple branches occur due to suction and injection. For the confirmation of the stable solution, stability examination is executed and confirms that the first branch is stable. It is reported that both NFs have high thermal efficiency; however, Ag–H2O represents significant thermal efficiencies. The present study is compared with available analyses to confirm the analysis under limited assumptions.

Nomenclature

A 1 = γ l u 0 1

unsteadiness number

f w

suction/injection parameter

k nf

thermal conductivity of nanofluid

ρ nf

density of nanofluid (kg m−3)

HT

heat transfer

NF

nanofluid

F

dimensionless velocity

Pr = v f k f

Prandtl number

T

temperature (T)

( ρ C p ) nf

heat capacity of nanofluid (W m−1 K−1)

μ nf

viscosity of nanofluid (m2 s−1)

u , v

velocities components (m s−1)

η

similarity variable

θ

dimensionless temperature

ϕ

volume friction

1 Introduction

The thermal efficiency of fluids holds critical significance within the aerospace and industrial domains. Numerous engineering and mechanical operations necessitate a considerable degree of heat transfer (HT) in order to be executed effectively. The traditional liquids are unable to provide the necessary heat to complete the operation. The flow and HT capabilities of the host liquid can be increased by suspending nanomaterials in the base fluid. These fluids have highly developed HT properties that pave the way for engineers and industrialists in the current world. The study of aerodynamics, medical research, chips used in computers, paint manufacturing, the production of aircraft parts, and many more fields are among the potential uses of nanofluids (NFs). Elgazery [1] inspected the non-uniform heat generation and absorption of a porous stretched sheet containing NF. The impact of magnetic fields was also investigated in his study. Nasir et al. [2] portrayed the thin-film flow of NF in the porous medium to analyses the heat rate using a time-dependent starching sheet. Using the Taguchi-GRA approach, Raza and Ashfaq [3] examined how to optimize HT in two-phased NF flow across a biaxial sheet. The improvement of the HT rate of a trihybrid NF inserted inside two parallel coaxial tubes using RSM was investigated by Raza et al. [4]. Utilizing a ferromagnetic tetra-hybrid NF, Shutaywi et al. [5] investigated the optimization of heat transport in a channel with extending walls. The improvement of the flow rate of a radiated micropolar NF with sensitivity evaluation was examined by Alahmadi et al. [6]. Bhattacharyya et al. [7] reported magnetized NF heat transmission across a stretched sheet. The numerical consequences were obtained using the RK4 method. It was revealed that HT increased due to the Brownian motion.

The fluid behavior over the stretched sheet was scrutinized by Mansur and Ishak [8]. A numerical solution has been obtained through the RK4 approach, and the results for the emerging factors are obtained through graphs. It was revealed that there is a direct relationship between the heating surface and HT, while the HT declines as the unsteady flow factor is enhanced. Dutta and Roy [9] described the heat flux features of the magnetohydrodynamics (MHD) movement flowing over an elongating surface. Certain assumptions have been considered to model the flow problem and show the outcomes for the stream phenomena. The work is quite interesting, but it absences novelty regarding HT in the NF from a physics point of view, such as chemical processes, thermal radiation, and magnetic fields. The dynamic of viscous fluid flow with HT through an extended surface was described by Cortell [10]. He reported the problem for two different phases: prescribed and uniform sheet temperature. The results were displayed through graphs for each phase. He examined the work only for the host fluid. Furthermore, this work could be extended to numerous NFs models regarding multiple flow geometries. An advanced HT study of 3D MHD NF flow across an expanding sheet including thermal energy and heat sources was studied by Afzal and Kamran [11]. In the study of fluid analysis, viscous dissipation plays a significant role in altering its characteristics. Mahabaleshwar et al. [12] investigated the influence of radiation in laminar flow using a ternary NF via a stretching sheet. Similarly, Mahabaleshwar et al. [13] examined two NF with a viscosity ratio via an accelerated plate. Three-dimensional MHD NF flow over an extended sheet featuring thermal and a heat sink was studied by Kamran et al. [14].

It is well established that the host fluid (the base fluid) has low thermal conductivity and is not a worthy conductor. So, it is necessary to explore the HT mechanism through a time-dependent stretching and contracting sheet. Such a framework has sufficient applications in industrial and mechanical engineering. There is limited investigation into HT via unsteady stretching or shrinking sheets using NFs. The NF containing silver nanoparticles (Ag–H2O) has significant advantages over host fluids regarding its transportation. The implications of bioconvection cross propagation on MHD movement of NFs over three distinct geometries involving melting were examined by Kamran et al. [15]. The magnetized bioconvection movement of Jeffrey NF containing motile bacteria over a stretched sheet was studied by Waqas et al. [16].

Since numerous investigators have found non-unique results in the majority of the studies, the evaluation of stability is crucial to getting a stable solution. The stability investigation in mixed convection flow across a transparent channel was first applied by Merkin [17]. Weidman et al. [18] subsequently utilized this idea to study a flow issue across a rotating plate utilizing stability analysis. The stagnation boundary movement across a porous upward sheet was then investigated by Merrill et al. [19]. Harris et al. [20] added the slip impact to the Merrill et al. [19] suggested model by utilizing the Brinkman flow theory. The interaction between stability and duality in magneto-radiated Casson NF flow across a stretched cylinder was examined by Deebani et al. [21]. The consequences of slip on MHD hybrid ferrofluid movement having acute magnetic attraction on a stretching sheet were investigated by Asghar et al. [22]. The hybrid NF dynamics on an exponentially contracting/extending Riga sheet during radiative heat flow were computationally investigated by Yashkun et al. [23]. The multiple solutions of MHD radiative movement of Casson NF across a contracting/extending cylinder were studied by Soomro et al. [24]. They deduced that the second solution is unstable while the first is reliable (stable).

A thorough survey of the present literature indicates that multiple research projects have been executed to investigate the thermal properties of base liquids that do not utilize advanced thermal enhancement, particularly in water solutions with Ag nanoparticles. In order to fill this novel research need in the area of improving heat transmission using NFs, an investigation has been conducted in this analysis. The originality of the existing analysis lies in examining the NF containing Ag in water-base fluid for heat enhancement and its stability over an elongating and shrinking sheet. The foremost flow equations in terms of partial differential equations (PDEs) are made dimensionless in terms of ordinary differential equations (ODEs) via a similar transformation. The numerical outcomes are achieved via a boundary-value problem fourth-order (bvp4c) scheme using MATLAB software. The impacts of emerging factors on the flowing fluid and heat rate are examined through graphs.

2 Mathematical exploration

Consider the unsteady fluid flow in a two-dimensional overstretching/shrinking sheet containing the Ag nanoparticles. The geometry of the Ag–H2O is represented in Figure 1(a), in which the NF velocities are portrayed by and for the horizontal and vertical directions, respectively.

Figure 1 
               (a) Geometry of Ag-H2O flow. (b) Flow chart of bvp4c.
Figure 1

(a) Geometry of Ag-H2O flow. (b) Flow chart of bvp4c.

The basic flow equations for the considered model are [21,23]

(1) u x + v y = 0 ,

(2) u t + u u x + v u y = μ nf ρ nf 2 u y 2 ,

(3) T t + u T x + v T y = k nf ( ρ C p ) nf 2 T y 2 .

In the above equations, µ nf signifies the viscosity of NF, ρ nf stands for the density of NF, k nf portrays the thermal conductivity of NF, and ( ρ C p ) nf describes the heat capacity of the NF. Furthermore, Table 1 represents the present model and its thermo-physical properties [21]

(4) ( ρ C p ) nf = ( ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ) ( ρ C p ) f ,

(5) ρ nf = ( ( 1 ϕ ) + ϕ ρ s ( ρ f ) 1 ) ρ f ,

(6) μ nf = μ f ( 1 ϕ ) 2.5 ,

(7) k nf = k s ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 .

Table 1

Thermo-physical properties of the present model

Characteristics Density Heat capacity Thermal conductivity Electric conductivity
Silver 10,500 234 425 6.21 × 106
Water 997.1 4,179 0.613 0.005

The conditions at the surface and far from the surface are given below:

(8) u = u 0 ( x l 1 ) ( 1 + γ t ) 1 , v = v w ( t ) , T = T + T 0 ( 1 + γ t ) c ( x n l n ) ( at the surface ) ,

(9) u 0 and T T ( far from the surface ) .

In equations (8) and (9), the reference lengths are represented by l , n , and c , where γ , T , u 0 , and T 0 are positive constant.

The stream function for the present model is represented by the following equations:

(10) φ ( x , y ) = x l 1 ( Re ( 1 + γ t ) 0.5 ) 1 F ( η ) ,

where Re = l 0 ( v f ) 1 and Pr = v f k f .

By introducing the variables of transformation for the present model [21,23], we obtain

(11) η = Re y ( l ( 1 + γ t ) 0.5 ) 1 , T = T + T 0 ( x n l n ) θ ( η ) ( 1 + γ t ) c ,

(12) u = u 0 x F ( η ) ( l ( 1 + γ t ) ) 1 ,

(13) v w = u 0 F ( η ) ( Re ( 1 + γ t ) 0.5 ) 1 .

The given flow model is a time-dependent flow problem, so we compute the atrial derivative for u and v with respect to space and t .

Using equations (12) and (13), we have

(14) u x = u 0 l ( 1 + γ t ) F ( η ) ,

(15) u y = u 0 x Re l 2 ( 1 + γ t ) 3 / 2 F ( η ) ,

(16) 2 u y 2 = u 0 x Re l 3 ( 1 + γ t ) 3 / 2 F ( η ) ,

(17) u t = u 0 x γ ( l ( 1 + γ t ) 2 ) 1 F ( η ) u 0 x γ y Re 2 l 2 ( 1 + γ t ) 5 2 F ( η ) ,

(18) T t = T 0 c x l c γ ( 1 + γ t ) ( c + 1 ) θ ( η ) T 0 x l c γ y Re 2 l ( 1 + γ t ) c + 3 2 θ ( η ) ,

(19) T x = n T 0 x l n 1 l ( 1 + γ t ) c θ ( η ) ,

(20) T y = T 0 x l c Re l ( 1 + γ t ) c + 1 2 θ ( η ) ,

(21) 2 T y 2 = T 0 x l c Re l 2 ( 1 + γ t ) c + 1 θ ( η ) .

In view of equations (14)–(21), the model equations described in equations (2) and (3), for the velocity and temperature profiles turned into dimensionless form as

(22) F + ( 1 ϕ ) 2.5 ( 1 ϕ + ϕ ρ s ρ f 1 ) 1 ( F F F 2 + A 1 ( F + 0.5 η F ) ) = 0 ,

(23) θ + ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 ( Pr A 1 ( c θ + 0.5 η θ ) + Pr ( n θ F + θ F ) ) = 0 .

Here, A 1 = γ l u 0 1 is the unsteadiness number, and Pr = v f k f is the Prandtl number.

The corresponding transformed boundary conditions are

(24) F ( η = 0 ) = f w , F ( η = 0 ) = 1 and F ( η = ) = 0 ,

(25) θ ( η = 0 ) = 1 and θ ( η = ) = 0 .

3 Numerical modeling of bvp4c

In MATLAB software, the bvp4c method solves the simulated highly complex differential problems (22) and (23) that align with the boundary limitations (24) and (25) numerically. This algorithm is implemented in a three-phase collocation technique, as described by Rehman et al. [25]. A homogeneous fourth-order resolution is implemented like solution C1-continuous in an integrated interval with the use of collocation polynomials. A mesh is implemented in the two phase using a collocation strategy to divide the time frame into sub-intervals. The algorithm ensures the assurance of the computational mechanism’s response.

A solver is used to figure out the error across every subinterval. If the required tolerance is not met, the procedure is repeated with a modified mesh. Figure 1(b) shows the bvp4c workflow. First, we use the steps that follow to convert equations (18)–(21) that relate to the border conditions (23) into first-order differential problems.

Phase I: Introducing the new variables to reduce the equations (18)–(21) with corresponding condition (23) to the first order

(26) χ 1 = F , χ 2 = F , χ 3 = F , χ 4 = θ and χ 5 = θ .

Phase II: In view of (26), equations (22)–(26) reduce to the following form:

(27) χ 1 = F , χ 2 = F , χ 3 = F , χ 4 = θ and χ 5 = θ ,

(28) χ 3 = ( 1 ϕ ) 2.5 ( 1 ϕ + ϕ ρ s ρ f 1 ) 1 ( χ 1 χ 3 χ 2 2 + A 1 ( χ 2 + 0.5 η χ 3 ) ) ,

(29) χ 5 = ( ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 ( Pr 1 ( c χ 4 + 0.5 η χ 5 ) ) ( Pr 1 ( c χ 4 + 0.5 η χ 5 ) + Pr ( n χ 4 χ 2 + χ 5 χ 1 ) ) ) .

Phase III: The altered BCs are

(30) ( χ 1 ) a * = f w , ( χ 2 ) a * = 1 , and ( χ 4 ) a * = 1 ,

( χ 2 ) b * = 0 and ( χ 4 ) b * = 0 .

The subscript “a*” in equation (30) indicates the surface position at η = 0 , while the subscript “b*” indicates its distance to the surface at a given value of η . We have selected the range for the present investigation to be 0 η 7 . We establish a dual response for two distinct initial estimations by applying the bvp4c method. The initial answer is obtained by means of an initial prediction that is very ambiguous. The second branch is not always possible to achieve. Until we arrive at a solution that fulfills the boundary requirements at infinity, this iterative procedure is carried out.

4 Stability analysis

We are interested in finding the second branch for various ranges of λ in the current investigation. Finding the problem’s stability assessment that is both stable and physically possible is important for this goal. The technique utilized by Merkin [17], which was recently enhanced by Weidman et al. [18], is also applied to the current problem.

The time-dependent flow characteristics (1)–(6) are given below:

(31) u x + v y = 0 ,

(32) u t + u u x + v u y = μ nf ρ nf 2 u y 2 ,

(33) T t + u T x + v T y = k nf ( ρ C p ) nf 2 T y 2 .

Following Markin [17] and Wiedman et al. [18], the current study uses the following similarity transformations and defines the dimensionless time variable τ as:

(34) η = Re y ( l ( 1 + γ t ) 0.5 ) 1 , T = T + T 0 ( x n l n ) θ ( η ) ( 1 + γ t ) c ,

(35) u = u 0 x F ( η ) ( l ( 1 + γ t ) ) 1 , v w = u 0 F ( η ) ( Re ( 1 + γ t ) 0.5 ) 1 , τ = ct 1 + γ t .

By substituting equation (20) in equations (16)–(19), we obtain

(36) 3 F η 3 + ( 1 ϕ ) 2.5 ( 1 ϕ + ϕ ρ s ρ f 1 ) 1 F 2 F η 2 F η 2 + A 1 F η + η 2 2 F η 2 + F τ = 0 ,

(37) 2 θ η 2 + ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 Pr A 1 c θ + 0.5 η θ η + Pr n θ F η + θ η F + θ τ = 0 .

The boundary conditions are

(38) F ( η , τ ) = f w , F η ( η , τ ) = 1 , θ ( η , τ ) = 1 at η = 0 ,

(39) F η ( η , τ ) = 0 , θ ( η , τ ) = 0 , η .

The stability of the system can be analyzed by perturbed it with disturbance τ, as explained by Marken [17] and Wiedman et al. [18]

F ( η , τ ) = F 0 ( η , τ ) + e γ τ J ( η , τ ) ,

(40) θ ( η , τ ) = θ 0 ( η , τ ) + e γ τ H ( η , τ ) .

In equation (40), γ represents the eigenvalues that will be determined. The stability of the problem can be analyzed using the smallest eigenvalues of γ . F ( η ) and θ ( η ) are small compared to F 0 ( η ) and θ 0 ( η ) . Therefore, the disturbance J ( η , τ ) , and H ( η , τ ) are small [17,18].

In view of equation (40), equations (36)–(39) become

(41) J + ( 1 ϕ ) 2.5 ( 1 ϕ + ϕ ρ s ρ f 1 ) 1 F 0 J ( J ) 2 + A 1 J + η 2 J γ J + J τ = 0 ,

(42) H + ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 Pr A 1 ( c θ 0 + 0.5 η H ) + H τ + Pr ( n θ J + H F 0 ) γ H = 0 .

The boundary conditions are

(43) F 0 ( η , τ ) = f w , J η ( η , τ ) = 1 , θ 0 ( η , τ ) = 1 at η = 0 ,

(44) J η ( η , τ ) = 0 , θ 0 ( η , τ ) = 0 , η .

The steady-state linear eigenvalues problem of equations (41)–(44) is given below:

(45) J + ( 1 ϕ ) 2.5 ( 1 ϕ + ϕ ρ s ρ f 1 ) 1 JJ ( J ) 2 + A 1 J + η 2 J γ J = 0 ,

(46) H + ( 1 ϕ ) + ϕ ( ρ C p ) s ( ρ C p ) f 1 ( ( k s + 2 k f ) 2 ϕ ( k f k s ) ) ( ( k s + 2 k f ) + ϕ ( k f k s ) ) 1 ( Pr A 1 ( cH + 0.5 η H ) + Pr ( nH J + H J ) ) γ H = 0 ,

(47) J ( η , τ ) = f w , J ( η , τ ) = 1 , H ( η , τ ) = 1 at η = 0 ,

(48) J ( η , τ ) = 0 , H ( η , τ ) = 0 , η .

5 Analysis and physical description

The motivation behind this study is to analyze the thermal conductivity of the NF under the effects of heat generation and absorption in a time-dependent boundary layer flow, which is an important area of research in fluid dynamics. The novelty of the existing study is that it aims to inspect the thermal characteristics of the NF for heat enhancement using Ag nanoparticles in water-base fluid across a time-dependent stretching sheet. The flow model is established for Ag–H2O NF in terms of PDEs. The transform variables are used to obtain dimensionless flow equations in terms of ODEs and then solve via the bvp4c approach. For confirmation, the present study is compared with previous work, and good corresponding is established by comparing the values of the skin friction as shown in Table 2. This validation confirmed that the numerical results of the present study are definite.

Table 2

Validation of the present study

A 1 0.6 1.0 1.4
Elbashbeshy and Bazid [26] 1.3321 1.4691 1.7087
Present study 1.3310 1.4683 1.7075

Figure 2 determines the occurrences of duality, i.e., the stable and unstable branches. As a consequence, a reliability analysis is performed to determine which is utmost consistent. The linearized equations (32)–(35) are numerically solved using the bvp4c approach. Figure 2 displays the eigenvalues γ against suction parameter f w when A 1 = 0.5 . Here point to be noted is that the primary and second solutions are connected with the common point called the critical point. It is perceived that the first solutions (solid lines) is stable branch, whereas the second solution (dashed lines) is the unstable branch based on the previous study reported by Merkin [17] and Wiedman et al. [18]. The stability analysis is important and is significantly used for the stable solution when dual solutions exist, which predicts which solution is stable.

Figure 2 
               Smallest eigenvalues 
                     
                        
                        
                           γ
                        
                        \gamma 
                     
                   with suction parameter 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           <
                           0
                           .
                        
                        {f}_{w}\lt 0.
Figure 2

Smallest eigenvalues γ with suction parameter f w < 0 .

It is perceived from Table 3 that the first branch (second branch) is reliable (unstable) as the magnitude of γ is positive (negative). The positive values of γ denote the stable solution, while the negative values of γ signify the unstable solution.

Table 3

The eigenvalues for the numerous values of unsteadiness parameter A 1

A 1 γ
First branch Second branch
−0.1 1.50778 −0.58707
−0.5 0.72587 −2.42025
−1.0 0.66487 −5.10325
−1.5 0.50010 −9.13063

Figures 3 and 4 show the variation of local skin friction f ( 0 ) regarding volume friction parameter and Prandtl number with the variation of injection factor ( f w < 0 ) and unsteadiness number A 1 , respectively. From this analysis, multiple solutions have been observed for f ( 0 ) . The dual solutions occur due to the injection case. Two dissimilar categories of solutions like multiple branches ( f w f wci ) and no branch ( f w > f wci ) for injection factor f w exist. Furthermore, a significant change in ϕ and Pr results boost in f wci and A 1 ci , which realm a separation. It is examined that f ( 0 ) increases in both cases. In Figure 3, it is significant to point out that the critical value for ϕ = 0.01 is f wc 1 = 2.007 , while the critical values for the ϕ = 0.05 and ϕ = 0.1 are f wc 2 = 2.3134 and f wc 2 = 2.3134 , respectively. Similarly, the critical magnitudes for Pr = 5, 3, and 0.5 are A 1 c 1 = 0.2224 , A 1 c 2 = 0.3764 , and A 1 c 3 = 0.4766 , respectively. The behavior is observed as discussed for f wi , i.e., multiple branch ( A 1 A 1 ci ) and no branch ( A 1 > A 1 ci ) for A 1 exist when f w = 1 . It is portrayed that f ( 0 ) increases as the quantities of ϕ and Pr are enhanced. The impression of ϕ , Pr , and n on the skin friction is shown in Figures 57, respectively. The dual solution is observed for these parameters too. It is reported that the HT is a growing function of ϕ and Pr while decreasing with the increasing values of n . The discrepancy in f″(0) becomes dominant against ϕ in the first solution for a fixed value of A 1 , while the setback phenomenon is observed in the second branch.

Figure 3 
               Variation of 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 ″
                              
                           
                           (
                           0
                           )
                        
                        {f}^{^{\prime\prime} }\left(0)
                     
                   
                  via 
                  
                     
                        
                        
                           ϕ
                        
                        \phi 
                     
                  .
Figure 3

Variation of f ( 0 ) via ϕ .

Figure 4 
               Disparity of 
                     
                        
                        
                           f
                           ″
                           (
                           0
                           )
                        
                        f\left^{\prime\prime} \left(0)
                     
                   
                  via 
                  
                     
                        
                        
                           Pr
                           .
                        
                        \Pr .
Figure 4

Disparity of f ( 0 ) via Pr .

Figure 5 
               Disparity of 
                     
                        
                        
                           −
                           θ
                           ′
                           (
                           0
                           )
                        
                        -\theta \left^{\prime} \left(0)
                     
                   
                  via 
                  
                     
                        
                        
                           ϕ
                        
                        \phi 
                     
                  .
Figure 5

Disparity of θ ( 0 ) via ϕ .

Figure 6 
               Variation of 
                     
                        
                        
                           −
                           θ
                           ′
                           (
                           0
                           )
                        
                        -\theta \left^{\prime} \left(0)
                     
                   
                  via 
                  
                     
                        
                        
                           Pr
                        
                        \Pr 
                     
                  .
Figure 6

Variation of θ ( 0 ) via Pr .

Figure 7 
               Variation of 
                     
                        
                        
                           −
                           θ
                           ′
                           (
                           0
                           )
                        
                        -\theta \left^{\prime} \left(0)
                     
                   
                  via 
                  
                     
                        
                        
                           n
                        
                        n
                     
                  .
Figure 7

Variation of θ ( 0 ) via n .

In the above figures, it is interesting to note that the foremost values of injection do not permit tension in moving molecules, and vorticity is not laminar. In the first branch, with larger injection, the decline in wall shear force as well as the rate of heat transmission is noted. In the second branch, the heat transmission is poorer, but the shear force has improved.

Figures 814 show the influence of emerging factors like suction/injection factor and the unsteadiness number on the dimensionless velocity and temperature of NF containing Ag nanoparticles using water-base fluid. The Pr is taken as 6.2 as water is used as a host fluid. Figures 8 and 9 display the influence of suction and injection factors on the fluid velocity field. The impact of unsteadiness number A 1 on the velocity field is depicted in Figures 10 and 11, individually for the dissimilar values of f w . Figures 12 and 13 show the inspiration of suction/injection and unsteadiness factor on the temperature profile. In the above analysis dual solutions has been observed for the injection case.

Figure 8 
               Velocity for suction 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           >
                           0
                           .
                        
                        {f}_{w}\gt 0.
Figure 8

Velocity for suction f w > 0 .

Figure 9 
               Velocity for injection 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           <
                           0
                           .
                        
                        {f}_{w}\lt 0.
Figure 9

Velocity for injection f w < 0 .

Figure 10 
               Velocity for suction 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           =
                           1
                           .
                        
                        {f}_{w}=1.
Figure 10

Velocity for suction f w = 1 .

Figure 11 
               Velocity for suction 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           =
                           −
                           1
                           .
                        
                        {f}_{w}=-1.
Figure 11

Velocity for suction f w = 1 .

Figure 12 
               Temperature for injection 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           <
                           0
                           .
                        
                        {f}_{w}\lt 0.
Figure 12

Temperature for injection f w < 0 .

Figure 13 
               Temperature for suction 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           >
                           0
                           .
                        
                        {f}_{w}\gt 0.
Figure 13

Temperature for suction f w > 0 .

Figure 14 
               Temperature for suction 
                     
                        
                        
                           
                              
                                 f
                              
                              
                                 w
                              
                           
                           =
                           1
                        
                        {f}_{w}=1
                     
                  .
Figure 14

Temperature for suction f w = 1 .

The influence of f w on the velocity of the fluid is shown in Figures 8 and 9. Figure 8 shows that the fluid velocity decreases when the suction influence is increased at the sheet. From a physics point of view, when the suction is increased, more NF molecules are trapped at the sheet surface, due to which the fluid velocity declines. The dual solutions occur due to the injection f w = 1 . From the analysis, it is perceived that the first solution is higher (dashed lines) than the second solution (solid lines). On the other hand, the velocity of the fluid is a growing function of injection factor f w < 0 as shown in Figure 9 in both cases (first and second solutions). Physically, when fluid particles leave the sheet surface due to injection, their momentum increases, which ultimately enhances the fluid motion. Additionally, the internal forces of the molecules reduce, and the thermal boundary layer thickness upsurges continuously in the first and second branches as the magnitude of injection increases.

Figures 10 and 11 depict the influence of A 1 on the NF velocity field for suction and injection, respectively. Mixed variation is examined for the velocity field both first and second solutions. It is perceived that the velocity of the fluid increases with the increasing quantities of A 1 in the range 0 η 1.5 , while the reverse effect is observed in the domain 1.5 < η 7 which satisfy the far-field Bcs asymptotically.

Figures 1214 show the variation of NF temperature for the suction ( f w > 0 )/injection ( f w < 0 ) f w and unsteadiness number A 1 . Two dissimilar categories of solutions, i.e., multiple branch ( f w f wci ) and no branch ( f w > f wci ) for injection factor f w , exist. Similarly, multiple branch ( A 1 A 1 ci ) and no branch ( A 1 > A 1 ci ) for A 1 exist when f w = 1 . It is detected that the temperature regarding first and second solutions enhances for the injection case while decreases for the suction case. It is also perceived that mixture behavior is detected for the variation of the unsteadiness number. The temperature field increases in the domain 0 η 0.9 and decreases in the range 0.9 < η 7 . Physically, suction causes the fluid velocity to rise quickly, increasing the dynamic energy of the fluid atoms. In elevation, kinematic energy causes a spike in particle collisions. The outcome is a dramatic rise in temperature. Due to increased injection effects close to the surface, the temperature rises quickly and vanishes asymptotically a far η 2 .

The volume fraction of the nanoparticles significantly affects thermophysical characteristics that are vital to the NFs’ HT process. Figure 15 shows the results for active density, energetic viscosity, as well as thermal efficiency versus for the tiny fluid under study. Similarly, by increasing the volumetric percentage of the nanomaterial, efficient density and heat capacity increase.

Figure 15 
               Effect of 
                     
                        
                        
                           ϕ
                        
                        \phi 
                     
                   on thermo-physical quantities.
Figure 15

Effect of ϕ on thermo-physical quantities.

The streamlines and thermal conductivity for the present flow study are displayed in Figures 1619 for two different values of A 1 , respectively. It is reported that the streamlines and thermal conductivity are growing function of A 1 . As the quantities of A 1 are augmented from 0.2 to 1.0, a significant increasing change is observed as depicted in Figures 16 to 19, respectively.

Figure 16 
               Streamlines for A
                  1 = 0.2.
Figure 16

Streamlines for A 1 = 0.2.

Figure 17 
               Streamlines for A
                  1 = 1.0.
Figure 17

Streamlines for A 1 = 1.0.

Figure 18 
               Thermal conductivity for A
                  1 = 0.2.
Figure 18

Thermal conductivity for A 1 = 0.2.

Figure 19 
               Thermal conductivity for A
                  1 = 1.0.
Figure 19

Thermal conductivity for A 1 = 1.0.

6 Conclusions

Due to its excellent thermal performance, a new class of conventional liquids known as NFs has gained a lot of attention from scientists and engineers. As a result, a time-dependent sheet is used to organize the investigation of the thermal transport mechanism for Ag–H2O. Such flows may be seen on the surface of bullets, solar thermal airflow, and automobile bonnets. In order to evaluate the effects of various factors on the heat transport process across a time-dependent surface, a flow issue for Ag–H2O NF is studied. According to the investigation, the employed NF is a superior heat conductor than normal liquids, making it useful for engineering and industrial applications. Finally, a statistical assessment is offered to assess the study’s reliability. It found great consistency with earlier research. Additionally, due to suction/injection phenomena, dual solutions occur for some emerging parameters. So, stability exploration is executed to ratify the stable solution. From the analysis, it is originated that the first solution is reliable, while the second is unstable. Two dissimilar categories of solutions, i.e., multiple branch ( f w f wci ) and no branch ( f w > f wci ) for injection factor f w , exist. Similarly, multiple branches ( A 1 A 1 ci ) and no branch ( A 1 > A 1 ci ) for A 1 exist when f w = 1 . A significant change in ϕ and Pr results boost in f wci and A 1 ci , which is a realm of separation. It is portrayed that f ( 0 ) increases as the quantities of ϕ and Pr are enhanced. It is reported that the HT is a growing function of ϕ and Pr while decreasing with the increasing values of n . It is reported that the fluid velocity decreases when the suction influence is increased at the sheet. The temperature field increases in the domain 0 η 0.9 and decreases in the range 0.9 < η 7 . Similarly, by increasing the volumetric percentage of the nanomaterial, efficient density and heat capacity increase. Additionally, the streamlines and the thermal conductivity are increasing functions of A 1 . As the magnitudes of unsteadiness number A 1 are increased from 0.2 to 1.0, a significant increasing change is observed for the streamlines and thermal conductivity.

Acknowledgments

The authors acknowledge the support by the National Research Foundation of Korea (NRF) grant funded by the Korean government (MSIT) (RS-2024-00346834).

  1. Funding information: This work was supported by the National Research Foundation of Korea (NRF) grant funded by the Korea government (MSIT) (RS-2024-00346834).

  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: 2024-12-18
Revised: 2025-03-28
Accepted: 2025-05-12
Published Online: 2025-07-10

© 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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