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Pure Mathematics

An accelerated numerical computation for singularly perturbed Robin-type parabolic problems with small parameters

ORCID Icon & ORCID Icon | (Reviewing editor:)
Article: 2354536 | Received 06 Nov 2023, Accepted 08 May 2024, Published online: 22 May 2024

ABSTRACT

This study presents a computational method for solving singularly perturbed Robin-type parabolic problem with two perturbation parameters. The fitted operator method in the space direction and the implicit Euler approach in the time direction are used to discretize the problem on a uniform mesh. Furthermore, the new fitted operator method is used to discretize the Robin boundary conditions. The linear order of parameter-uniform convergence has been investigated in both the time and space variables. The application of the Richardson extrapolation approach enhanced the accuracy and rate of convergence of the present method from linear to quadratic order. On the computations of two numerical examples, the theoretical and computational results agreed upon.

1. Introduction

Differential equations, which consider small positive parameters, are often used to describe real-world engineering and applied mathematics problems. Many scientists, researchers, and engineers investigated differential equations with a single parameter ε(0<ε1) multiplied to the highest derivative in the equation. This type of equation is a singularly perturbed differential equation with one-parameter. Several studies published in the literature explore asymptotic, analytical, and numerical solutions to ordinary and partial differential equations with one-parameter. Asymptotic and numerical solutions to two-parameter singularly perturbed differential equations have received relatively little study in comparison to their one-parameter counterparts. It is generally understood that the existence of small parameters in differential equations creates boundary and/or interior layers to appear in the solution. O’Malley (Citation1967a, Citation1967b, Citation1969) and Chen and O’Malley (Citation1974) proposed singularly perturbed problems with two small parameters and investigated their asymptotic solutions.

Various numerical approaches were developed subsequently that improved the accuracy of the asymptotic approaches proposed by O’Malley and his co-workers. Patidar (Citation2008) was the first scholar to design a robust fitted operator finite difference approach for a two-parameter singular perturbation ordinary differential equations. The numerical solution of two-parametric singularly perturbed parabolic partial differential equations with non-smooth data was studied in Chandru et al (Citation2018, Citation2019). Various researchers proposed parameter-uniform numerical methods for solving two-parameter singularly perturbed parabolic problems, see in O’Riordan et al. (Citation2006), Kadalbajoo and Yadaw (Citation2012), Das and Mehrmann (Citation2016), Jha and Kadalbajoo (Citation2015), Munyakazi (Citation2015), Gupta et al. (Citation2019), Mekonnen et al (Citation2020, Citation2021). Bullo et al (Citation2021b, Citation2021b, Citation2022) and Sumit et al. (Citation2020). All of the preceding works dealt with singularly perturbed two-parameter parabolic problems with initial and Dirichlet boundary conditions. Some parameter-robust numerical methods are developed by Hailu et al (Citation2022b, Citation2022a), Daba et al. (Citation2022), Hassen et al. (Citation2023) and Duressa et al. (Citation2023) to solve different kinds of singularly perturbed problems. However, different numerical treatments have been reported for one-parameter singularly perturbed problems of convection-diffusion and reaction-diffusion types with initial and Robin boundary conditions in Hemker et al. (Citation2002), Das and Natesan (Citation2013a), Selvi and Ramanujam (Citation2017), Mbroh et al. (Citation2020), Janani Jayalakshmi and Tamilselvan (Citation2020), Das et al. (Citation2020), Sunil et al. (Citation2021), Gelu et al (Citation2021, Citation2022a, Citation2022b, Citation2022, Citation2023b, Citation2023a), Saini et al (Citation2023, Citation2024) and Srivastava et al. (Citation2023), S. Kumar et al. (Citation2023).

The Haar wavelet method for space direction on a Shishkin mesh and the implicit Euler method for time direction on a uniform mesh are used to solve the problem under consideration by D. Kumar and Deswal (Citation2022). They determined the maximum residual errors since the double mesh approach cannot be used to solve all kinds of problems approximated using the Haar wavelet scheme. Despite the fact that they claimed their method is robust, no one can observe a stable and parameter-uniform convergence from their numerical output. Motivated by this work, we construct an efficient, stable and parameter-uniform numerical method that is based on a uniform mesh and combines the fitted operator finite difference method in space direction with implicit Euler method in time direction. The proposed method leads to the linear order of convergence in time and space directions. The use of Richardson extrapolation improved the accuracy by increasing the order of convergence from linear to quadratic. Two test examples are used to verify the appilcability of the present method. The results we obtain indicate that the method provides stable and parameter-uniform convergence irrespective of ɛ and µ. The problem considered is the following two-parameter singularly perturbed parabolic problem

(1) Lε,μw(x,t)∂w∂tε2wx2μa(x,t)∂w∂x+b(x,t)w(x,t)=g(x,t), (x,t)Ω,(1)

along with the initial condition and Robin boundary conditions

(2) {w(x,0)=φ(x),0x1,Bl,εw(0,t)β1(0,t)w(0,t)εβ2(0,t)∂w(0,t)∂x=η(t),0<tT,Br,εw(1,t)λ1(1,t)w(1,t)+ελ2(1,t)∂w(1,t)∂x=θ(t),0<tT,(2)

where ε (0<ε1) and μ (0μ1) are the small perturbation parameters and Ω=(0,1)×(0,T]. The functions a(x,t),b(x,t),g(x,t) in Ω¯; β1(0,t),β2(0,t),\allowbreakλ1(1,t),λ2(1,t),η(t),θ(t) for 0<tT and φ(x)for0x1 are assumed to be smooth and bounded such that a(x,t)α>0, b(x,t)ζ>0, (x,t)Ω¯. Moreover, we assume that the constants β1,β2,λ1,λ2 given in Robin boundary conditions satisfy the conditions (Mbroh et al., Citation2020)

β1(0,t), β2(0,t)>0, β1(0,t)+β2(0,t)>0,λ1(1,t), λ2(1,t)0, λ1(1,t)+λ2(1,t)>0.

Furthermore, we define γ=max(x,t)Ω¯b(x,t)a(x,t). If µ = 0, then (Equation1) is called a singularly perturbed parabolic reaction-diffusion problem which exhibits boundary layers of width O(ε) at x = 0 and x = 1. If µ = 1, then (Equation1) is well-known singularly perturbed parabolic convection-diffusion-reaction problem showing parabolic boundary layer of width O(ε) appear near x = 0 (O’Riordan et al., Citation2006). Depending on the order of the parameters, two possibilities arise. Firstly, when we assume εμ20 as μ0, a layer of width O(εμ) and O(μ) appear in the vicinity of x = 0 and x = 1, respectively. Secondly, when we suppose μ2ε0 as ε0, boundary layers of width O(ε) appear in the vicinity of the boundary x = 0 and x = 1.

The existence and uniqueness for the solution to EquationEq. (1)-(Equation2) can be established under the assumption that the data are Ho¨lder continuous and satisfy an appropriate compatibility conditions at the corner points (0, 0) and (1, 0). The boundary functions η(t),θ(t)Ck([0,T]),φ(x)C(1,k)([0,1]) should satisfy the kth order compatibility condition for the initial function if

ktk(β1(0,0)φ(0)εβ2(0,0)∂φ(0)∂x)=dkη(0)tk,ktk(λ1(1,0)φ(1)+ελ2(1,0)∂φ(1)∂x)=dkθ(0)tk,∂η(0)∂tε2φ(0)x2μa(0,0)∂φ(0)∂x+b(0,0)φ(0)=g(0,0),∂θ(1)∂tε2φ(1)x2μa(1,0)∂φ(1)∂x+b(1,0)φ(1)=g(1,0).

Now, we introduce the regularity of the solutions to the time-dependent problems in some spaces. To guarantee the existence of the unique solution of problem (Equation1)-(Equation2), we need to assume that the coefficients of the considered problem are Ho¨lder continuous in both x and t with exponent λ, where λ(0,1). A function u(x,t) is said to be Ho¨lder continuous with respect to exponent λ if,

|u(x,t)u(x,t)|C(|xx|2+|tt|)λ/2.

for all (x,t)Ω. Assume that the coefficient of the parabolic PDE and the initial boundary condition in (Equation1)–(Equation2) are sufficiently smooth, and satisfy the necessary compatibility conditions. Then, the problems (Equation1)–(Equation2) have unique solution u(x,t)Cλ4(Ω¯), where the space of all functions having Ho¨lder continuous derivatives is defined as

Cλ4(Ω)=min{u:i+juxitjCλ0(Ω)}

for all non negative integers i,j with 0i+2j4 and here Cλ0(Ω) is the set of Ho¨lder continuous functions with exponent λ.

The mathematical models related to two-parameter singularly perturbed problem of type (Equation1) arise in transport phenomena in chemistry, biology, chemical reactor theory (Vasil’eva, Citation1963), lubrication theory (DiPrima, Citation1968) and dc motor theory (Bigge & Bohl, Citation1985) and flow through unsaturated porous media (Bhathawala & Verma, Citation1975). In two-parameter singular perturbation problems, the diffusion and convection terms are multiplied by the perturbation parameters.

This article is divided as follows. Section 2 outlines the analytical properties of the continuous problem. Section 3 discuss about fully discrete numerical scheme. Section 4 demonstrates the stability and convergence analysis of a fully discretized problem. Section 4 gives the numerical results and discussions. The paper ends with conclusion in Section 6.

2. Analytical properties

In this section, we put a priori bounds for the solution and its corresponding derivatives. The assumptions given for (Equation1) and (Equation2) ensure that the differential operator Lε,μ satisfies the following maximum principle.

Lemma 2.1.

Assume that Φ(x,t) be smooth function satisfying Φ(x,0)0 on x(0,1), Bl,εΦ(0,t)0, Br,εΦ(1,t)0 on t(0,T]. If Lε,μΦ(x,t)0,(x,t)Ω, then Φ(x,t)0, (x,t)Ω¯.

Proof.

Let an arbitrary smooth function Φ takes its minimum value at the point (ξ,ς)Ω¯ such that Φ(ξ,ς)=min(x,t)Ω¯Φ(x,t) and assume that Φ(ξ,ς)<0. This implies that (ξ,ς) is not on the boundary.

Case (i): For (ξ,ς){0}×(0,T], we have Φ∂x(0,ς)0. Hence, Bl,εΦ(0,ς)=β1(0,t)Φ(0,ς)εβ2(0,t)Φ∂x(0,ς)<0, which contradicts the assumption.

Case (ii): For (ξ,ς){1}×(0,T], we have Φ∂x(0,η)0. Hence, Br,εΦ(1,ς)=λ1(1,t)Φ(1,ς)+λ2(1,t)Φ∂x(1,ς)<0, which contradicts the assumption.

Case (iii): For (ξ,ς)Ω, as it attains minimum at (ξ,ς), we have Φ∂t(ξ,ς)=0, Φ∂x(ξ,ς)=0 and 2Φx2(ξ,ς)0. Hence,

Lε,μΦ(ξ,ς)=Φ∂t(ξ,ς)ε2Φx2(ξ,ς)μa(ξ,ς)Φ∂x(ξ,ς)+b(ξ,ς)Φ(ξ,ς)<0,

which contradicts the supposition Lε,μΦ(x,t)0 implying that Φ(ξ,ς)0 and thus Φ(x,t)0,(x,t)Ω¯.

The following Lemma proves the stability estimate to obtain unique solution.

Lemma 2.2.

The solution w(x,t) to the continuous problem in (Equation1)-(Equation2) satisfy the following bound

|w(x,t)|max{|φ(x)|,|η(t)|,|θ(t)|}+gα.

Proof.

To prove this lemma, the barrier functions ϑ± are defined as follows

ϑ±(x,t)=max{|φ(x)|,|η(t)|,|θ(t)|}+gα±w(x,t).

Evaluating the barrier functions at the initial condition and boundary conditions together with Lemma (2.1), the required stability bound is achieved.

The ε,μconvergence analysis of the numerical scheme which we propose requires that we use bounds on the solution and its derivatives. For the discrete analysis, we use the characteristic equation for problem (Equation1) in space direction only is

εΨ2(x)μa(x)Ψ(x)+b(x)=0.

The two solutions for the characteristic equations are Ψ0(x)<0 and Ψ1(x)>0 which are used to describe the boundary layers at x = 0 and x = 1, respectively. The quantity Ψ0(x) is associated with the boundary layer at x = 0 and Ψ1(x) with the boundary layer at x = 1. We define the following to bound the solution and its derivatives

ψ0=max[0,1]Ψ0(x)  and  ψ1=max[0,1]Ψ1(x).

The next theorem gives the ε,μ-uniform bounds for the derivatives of the solution u, which we will use in the discrete problem convergence analysis.

Theorem 2.3

For 0i4 and any real constant 0<p<1, we have the following space derivative bound

|iw(x)xi|Ω¯C(1+ψ0iepψ0x+ψ1iepψ1(1x)).

Proof.

For the details of the proof, see Kadalbajoo and Yadaw (Citation2012).

3. Fully discrete problem

On the space domain [0,1], we introduce the equidistant meshes with uniform mesh length h such that x0=0,xi=x0+ih,i=1,M1,h=1M=xixi1,xM=1, where M is the number of mesh points in the space direction. Similarly, we divide the time interval [0,T] into N equal sub-intervals with uniform mesh size Δt, defined by t0=0,tn=nΔt,n=1,,N1,Δt=TN,tN=T, where M denotes the number of mesh points in time direction. The notation W(xi,tn)Win is used as the approximation of w(xi,tn)win. Both the space and time discretizations are on a uniform mesh. Now, we fully discretize (Equation1) in space direction using the non-standard finite difference method and time direction using implicit Euler method to get the discrete problem in the form

(3) Lε,μM,ΔtWin+1ε(Wi1n+12Win+1+Wi+1n+1ϕi2)μain+1(Wi+1n+1Win+1h)+(bin+1+1Δt)Win+1=gin+1+WinΔt.(3)

for i=1,,M1,n=0,,N. According to Mickens (Citation1994, Citation2005), the concept of sub-equations is the major tool to derive the denominator function for a partial differential equation. From (Equation3), we take the homogeneous form of the constant coefficient sub-equation as

(4) ε(Wi1n+12Win+1+Wi+1n+1ϕi2)ρ(Wi+1n+1Win+1h)+κWin+1=0,(4)

where ρ=μain+1 and κ=bin+1+1Δt. EquationEquation (4) has two linearly independent analytical solutions, namely, exp(τ1x) and exp(τ2x), where

(5) τ1,2=ρ±ρ2+4εκ2ε(5)

Following the technique of Mickens’ (Mickens, Citation2005), we construct the second-order difference equation for (Equation4) as follows

(6) |Wi1W1,i1W2,i1WiW1,iW2,iWi+1W1,i+1W2,i+1|=|Wi1exp(τ1xi1)exp(τ2xi1)Wiexp(τ1xi)exp(τ2xi)Wi+1exp(τ1xi+1)exp(τ2xi+1)|=0.(6)

Simplifying the determinant in (Equation6), we get

(7) exp(ρh2ε)Wi12cosh(hρ2+4εκ2ε)Wi+exp(ρh2ε)Wi+1=0,(7)

which is the exact scheme for (Equation4) in the sense that (Equation7) has the same general solution

(8) Wi=C1exp(τ1xi)+C2exp(τ2xi)(8)

as (Equation4). It is noted that to construct the non-standard finite difference method, we need to find a suitable denominator function which replaces h2. To this end, the extraction of the denominator function from (Equation7) is not straightforward. However, the fact that the layer behaviors of the solution of (Equation1) and that of the (Equation4) in the case when κ0 are similar (CitationPatidar Citation2008). Thus, for the latter case, that is, κ0, we have the exact scheme of the form (Equation7). Multiplying both sides of (Equation7) by exp(ρh2ε), and incorporating the term Wi+1n+1Win+1, we obtain

(9) Wi1n+12Win+1+Wi+1n+1+(Wi+1n+1Win+1)(exp(ρhε)1)=0,(9)

EquationEquation (9) can be written as

(10) εWi1n+12Win+1+Wi+1n+1ϕ2ρWi+1n+1Win+1h=0,(10)

where the denominator function is given by

(11) ϕ2(h,ε,μ)ϕ2=ρ(exp(ρhε)1).(11)

Adopting the denominator function for the variable coefficient, we can write as

(12) ϕi2(h,ε,μ)ϕi2=hεμain+1(exp(μain+1hε)1).(12)

Thus, we get the following fully discrete problem

(13) Lε,μM,ΔtWin+1WinΔtεWi1n+12Win+1+Wi+1n+1ϕi2μain+1(Wi+1n+1Win+1h)+bin+1Win+1=gin+1,(13)

where the denominator function is given in (Equation12). We use forward and backward finite differences to approximate the first derivative in the left and right boundary conditions, respectively as given below. To find the denominator function in the boundary conditions, we use the concept of the theory of non-standard difference method by taking the homogeneous form of the boundary equation while keeping the time variable t continuous as

β1,0W(x)εβ2,0W(x)=0,        λ1,MW(x)+ελ2,MW(x)=0.

Solving the above equations, we have

W(x)=β1,0εβ2,0W(x),        W(x)=λ1,Mελ2,MW(x).

with solution of the form

{W(x)=exp(β1,0εβ2,0x),W(x)=exp(λ1,Mελ2,Mx).

Discretizing (Equation2) by using forward and backward finite difference approximations, we have

{β1,0Wiεβ2,0(Wi+1Wiϕ0)=0,λ1,MWi+ελ2,M(WiWi1ϕM)=0.

Following Micken’s technique in Mickens (Citation2005), we construct a difference equation for the left boundary condition

|WiW1,iWi+1W1,i+1|=|Wiexp(β1,0εβ2,0xi)Wi+1exp(β1,0εβ2,0xi+1)|=0.

Simplifying the above determinant gives

exp(β1,0εβ2,0xi+1)Wiexp(β1,0εβ2,0xi)Wi+1=0.

Since xi+1=xi+h and exp(β1,0εβ2,0xi)0, we have

Wi+1=exp(β1,0hεβ2,0)Wi.

Substituting this last result into left boundary condition, we have

β1,0Wiεβ2,0(exp(β1,0hεβ2,0)WiWiϕ0)=0,

Since Wi0, we must have

ϕ0=εβ2,0β1,0(exp(β1,0hεβ2,0)1).

This is a fitting factor for the left boundary condition. Similarly, following Micken’s technique in Mickens (Citation2000), the fitting factor for the right boundary condition is

ϕM=ελ2,Mλ1,M(1exp(hλ1,Mελ2,M)).

We have the discrete initial and boundary conditions as

(14) {Wi0=φi,xiΩ¯,β1,0n+1W0n+1εβ2,0n+1(W1n+1W0n+1ϕ0)=η(tn+1),tn[0,T],λ1,Mn+1WMn+1+ελ2,Mn+1(WMn+1WM1n+1ϕM)=θ(tn+1),tn[0,T],(14)

where the denominator functions in the boundary conditions in (Equation14) are given by

(15) {ϕ0=εβ2,0n+1β1,0n+1(exp(hβ1,0n+1εβ2,0n+1)1),i=0,ϕM=ελ2,Mn+1λ1,Mn+1(1exp(hλ1,Mn+1ελ2,Mn+1)),i=M.(15)

The discrete scheme in (Equation13) and the discrete conditions in (Equation14) together with the denominator functions in (Equation12) and (Equation15) can be written in matrix form as

(16) AW=ϝ,i=1,2,,M1,n=0,,N,(16)

where W and ϝ are column vectors of M +1 and the matrix A is a tri-diagonal matrix of (M+1)×(M+1). The entries of the coefficient matrix A are given by

(17) {A0,0=1+εϕ0,A0,1=εϕ0,Ai,i1=εϕi2,i=1,,M1,Ai,i=2εϕi2+μain+1h+bin+1+1Δt,i=1,,M1,Ai,i+1=εϕi2μain+1h,i=1,,M1,AM,M1=εϕM,AM,M=1+εϕM.(17)

The entries of column vectors ϝ and W are given as follows

(18) {ϝ0n+1=η(tn+1),ϝin+1=gin+1+WinΔt,i=1,,M1,ϝMn+1=θ(tn+1).(18)

4. Analysis of the discrete problem

We prove some useful attributes the discrete problem. The discrete operator Lε,μM,Δt in (Equation13) satisfies the following discrete maximum principle.

Theorem 4.1

Assume that Lε,μM,Δt be discrete operator given in (Equation13) and Θin be any mesh function satisfying Lε,μM,ΔtΘin0, (i,n)ΩM,Δt, initial condition Θi00,0iM and Robin boundary conditions

η(tn+1)β1,0n+1Θ0n+1εβ2,0n+1Θ1n+1Θ0n+1ϕ00,0nN,θ(tn+1)λ1,Mn+1ΘMn+1+ελ2,Mn+1ΘMn+1ΘM1n+1ϕM0,0nN.

If Lε,μM,ΔtΘin+10, (xi,tn)ΩM,Δt, then Θin+10 for all (xi,tn)Ω¯M,Δt.

Proof.

Let s and k be indices such that Θsk+1=min(i,n)Ω¯M,ΔtΘin+1 for Θin+1Ω¯M,Δt. Assume that Θsk+1<0. Then, (s,k){1,,M1}×{1,,N}. It follows that Θs+1k+1Θsk+10,Θsk+1Θs1k+10 and Θsk+1Θsk0. Now on the domain ΩM,Δt

Lε,μM,ΔtΘsk+1Θsk+1ΘskΔtεϕs2(Θs+1k+12Θsk+1+Θs1k+1)μask+1h(Θs+1k+1Θsk+1)+bsk+1Θsk+1,Θsk+1ΘskΔtεϕs2[(Θs+1k+1Θsk+1)(Θsk+1Θs1k+1)]μask+1h(Θs+1k+1Θsk+1)+bsk+1Θsk+1,<0,

which contradicts the assumption. The discrete boundary condition becomes

β1,0k+1Θ0k+1εβ2,0k+1ϕ0(Θ1k+1Θ0k+1)<0  andλ1,Mk+1ΘMk+1+ελ2,Mk+1ϕM(ΘMk+1ΘM1k+1)<0,

which contradicts the assumption Θkk+1<0, (s,k). Therefore, Θsk+1>0 implies that Θin+10 in Ω¯.

Now, we prove the uniform stability analysis of the discrete problem.

Lemma 4.2.

Let Win+1 be the discrete solution. Then, we have the following bound

Win+11αmax(i,n)Ω¯|Lε,μM,ΔtWin+1|+max(i,n)Ω¯{|φi|,η(tn+1),θ(tn+1)}.

Proof.

Let Z=1αmax(i,n)Ω¯|Lε,μM,ΔtWin+1|+max(i,n)Ω¯{|φi|,η(tn+1),θ(tn+1)} and define the two barrier functions (Ψ±)in+1 by (Ψ±)in+1=Z±Win+1. At the initial condition, we get (Ψ±)i0=Z±Wi0=Z±φi0. At the boundary points, we have (Ψ±)0n+1=Z±W0n+1=Z±η(tn+1)0, and (Ψ±)Mn+1=Z±WMn+1=Z±θ(tn+1)0. On the discretized domain 1iM1, we have

Lε,μM,Δt(Ψ±)in+1(Z±Win+1)(Z±Win)Δtεϕi2((Z±Wi1n+1)2(Z±Win+1)+(Z±Wi+1n+1))μain+1h((Z±Wi+1n+1)(Z±Win+1))+bin+1(Z±Win+1),=bin+1Z±Lε,μM,ΔtWin+1,=bin+1Z±gin+1,0,

where bin+1ζ>0 and from Theorem (4.1), we get (Ψ±)in+10,(xi,tn)Ω¯.

4.1. Convergence analysis

We use the following lemma to prove the uniform convergence analysis of the discrete problem.

Lemma 4.3.

For all positive integers k on a fixed mesh, we have

limε 0max1<i<N1exp(Cxiε)εk2=0andlimε 0max1<i<N1exp(C(1xi)ε)εk2=0,

where xi=ih,h=1M,∀i=1,,M1.

Proof.

For the proof, see Patidar and Sharma (Citation2006).

The truncation error of the proposed method is given by

(19) Lε,μM,Δt(Win+1win+1)=Lε,μM,ΔtWin+1Lε,μM,Δtwin+1,=gin+1Lε,μM,Δtwin+1,=Lε,μwin+1Lε,μM,Δtwin+1,=(wt)in+1ε(wxx)in+1μain+1(wx)in+1[win+1winΔtε(wi+1n+12win+1+wi1n+1ϕi2)μain+1(wi+1n+1win+1h)].(19)

Taylor’s expansions of the terms win+1,wi+1n+1 and wi1n+1 are give as following

wi+1n+1=win+1+h(wx)in+1+h22(wxx)in+1+h36(wxxx)in+1+h424(wxxxx)in+1+wi1n+1=win+1h(wx)in+1+h22(wxx)in+1h36(wxxx)in+1+h424(wxxxx)in+1+win+1=win+Δt(wt)in+Δt22(wtt)in+

From the above Taylor’s expansion, we deduce the following

(20) wi+1n+12win+1+wi1n+1=h2(wxx)in+1+h412(wxxxx)in+1+wi+1n+1win+1=h(wx)in+1+h22(wxx)in+1+win+1winΔt=(wt)in+Δt2(wtt)in+(20)

Substituting EquationEquations (20) into their respective positions into (Equation19) and rearranging, we obtain

(21) Lε,μM,Δt(Win+1win+1)=Δt2(wtt)inε(wxx)in+1+μh2ain+1(wxx)in+1++εϕi2(h2(wxx)in+1+h412(wxxxx)in+1+)+(21)

Using a truncated Taylor’s expansion of the denominator function Munyakazi (Citation2015)

1ϕi2=1h2μain+12εh+(μain+1)212ε2

in (Equation21) and after some manipulation, we obtain

(22) Lε,μM,Δt(Win+1win+1)=(12(wtt)in)Δt+(μain+1(wxx)in+1)h+((μain+1)212ε(wxx)in+1+ε12(wxxxx)in+1)h2+(μain+124(wxxxx)in+1)h3+((μain+1)2144ε(wxxxx)in+1)h4(22)

Following nyakazi (Citation2015) for the bounds on derivatives in Theorem (4.1) together with Lemma (4.3) and using the fact that as ε0, both the terms ψ0iepψ0xi and ψ1iepψ1(1xi) approach zero for all i{0,1,2,,}. Applying the relation h>h2>h3>h4 in (Equation22), the discrete problem satisfy the following bound

|Lε,μM,Δt(Win+1win+1)|C(h+Δt),

where C is constant independent of the perturbation parameters and mesh sizes and given by C=C1+C2=(12(wtt)in)+(μain+1(wxx)in+1). Invoking the uniform stability in Lemma (4.2), we get the result

|Win+1win+1|C(h+Δt).

The error bound at the left boundary x0 is estimated as follows

W0n+1w0n+1=β1,0n+1w0n+1εβ2,0n+1(wx)0n+1η(tn+1)[β1,0n+1w0n+1εβ2,0n+1ϕ0(w1n+1w0n+1)η(tn+1)]=εβ2,0n+1(wx)0n+1+εβ2,0n+1ϕ0(w1n+1w0n+1)

Taylor series expansion of the term w1n+1 in the above expression yields

W0n+1w0n+1=εβ2,0n+1(wx)0n+1+εβ2,0n+1ϕ0(w0n+1+h(wx)0n+1+h22(wxx)0n+1+w0n+1)

Appropriate truncated Taylor series expansion of the denominator function ϕ01 yields

1ϕ0=1hβ1,0n+12εβ2,0n+1.

Using this in the above expression and simplifying gives

W0n+1w0n+1=εβ2,0n+1(wx)0n+1+(εβ2,0n+1hβ1,0n+12)(h(wx)0n+1+h22(wxx)0n+1+)

Further simplification yields

W0n+1w0n+1=(εβ2,0n+12(wxx)0n+1β1,0n+12(wx)0n+1)h+(β1,0n+14(wxx)0n+1)h2.

Using the relation h>h2 and applying the bound in Theorem (2.3), we get

|W0n+1w0n+1|Ch.

In similar way, we can find the error bound at the right boundary xM as

|WMn+1wMn+1|Ch.

Combining the error bound at the two boundaries and that of the interior mesh points leads us to the following main theorem to prove the uniform convergence of the fully discretized scheme.

Theorem 4.4

Let win+1 be the continuous solution and Win+1 be the discrete solution. Then, the overall error bound satisfies

(23) sup0<ε1 max0iM;0nN|Win+1win+1|C(h+Δt),(23)

where C is a constant independent of ɛ and the mesh lengths h and Δt.

From the above theorem, we deduce that the developed method is first-order convergent, independent of the parameters ɛ and µ both in space and time directions.

Next, we develop the Richardson extrapolation technique to improve the method’s accuracy and rate of convergence.

4.2. Richardson extrapolation

Richardson extrapolation is a technique used to accelerate the accuracy and rate of convergence of the proposed method. Some Richardson extrapolation is addressed for non-uniform meshes in (Das, Citation2018; Das & Natesan, Citation2013b). From (Equation23), we have

(24) |Win+1win+1|C(h+Δt),(24)

where win+1 and Win+1 are continuous and numerical solutions, respectively, C is a constant independent of the perturbation parameters ε,μ and mesh sizes h and Δt. Assume ΩM,ΔtΩ2M,Δt/2 where ΩM,Δt is the mesh obtained from the mesh intervals h and Δt and Ω2M,Δt/2 is the mesh obtained by bisecting the mesh intervals h and Δt. Denoting the numerical solution obtained with the mesh points Ω2M,Δt/2 by W~in+1. From (Equation24), it clear that for the mesh (xi,tn)ΩM,Δt

(25) Win+1win+1=C(h+Δt)+RM,Δt,(25)

Now, we construct another mesh Ω~2M={0=x~0<x~1<<x~2M=1} which is obtained by bisecting the mesh ΩM. Let us define the step size as h~=x~ix~i1. Then, x~ix~i1=h~=h2 for x~iΩ2M. Similarly, another time mesh is constructed as 0=t~0<t~1<<t~Δt/2=1 which is obtained by bisecting the original time mesh Δt/2. Hence, the time step size on this new mesh is t~nt~n1=Δt2. Then, t~nt~n1=Δ~t=Δt2 for t~nΩΔt/2. For the mesh (x~i,t~n)Ω2M,Δt/2, we have

(26) W~in+1win+1=C(h2+Δt2)+R2M,Δt/2,(26)

where RM,Δt and R2M,Δt/2 are the remainder terms of the truncation error with O(h2+Δt2). Subtracting (Equation26) from (Equation25) gives

(27) Win+1win+1(2W~in+1win+1)=RM,Δt2R2M,Δt/2.(27)

Dropping the error term in (Equation27) and rearranging, we have the following extrapolation formula at the interior points

(28) (Win+1)ext=2W~in+1Win+1.(28)

In similar way, we use the extrapolation formulas at the boundary points x0 and xM

(29a) (W0n+1)ext=2W~0n+1W0n+1.(29a)
(29b) (WMn+1)ext=2W~Mn+1WMn+1.(29b)

The error bound for extrapolated solutions can now be reported in the theorem below.

Theorem 4.5

Let win+1 be the solution to the continuous problem and (Wext)in+1 be the extrapolated solution. Then, the new error bound takes the form

sup0<ε1,0μ1 max0iM;0nN|(Wext)in+1win+1|C(h2+Δt2),

where C is a constant independent of ɛ and the mesh lengths h and Δt.

Therefore, using Richardson extrapolation, first-order parameter-uniformly convergent method is altered into second-order parameter-uniformly convergent method. Thus, the proposed method is second-order convergent. Now, we illustrate the theoretical findings in the previous sections in practice via numerical computations.

5. Numerical illustrations and discussions

In this section, we carry out numerical experiments to confirm the effectiveness of the proposed method in accordance with the theoretical findings covered in the sections above.

Example 5.1.

Consider the singularly perturbed two-parameter parabolic problem

{∂w∂tε2wx2μ(1+xt)∂w∂x+(1+t)w=et2(x+5),(x,t)(0,1)×(0,1],w(x,0)=sin(πx),x[0,1],w(0,t)ε∂w(0,t)∂x=επ,t[0,1],w(1,t)+ε∂w(1,t)∂x=επ,t[0,1].

Example 5.2.

Consider the singularly perturbed two-parameter parabolic problem

{∂w∂tε2wx2μ(1+x)∂w∂x+w=x2+1,(x,t)(0,1)×(0,1],w(x,0)=1x2,x[0,1],w(0,t)ε∂w(0,t)∂x=1+t+ε,t[0,1],w(1,t)+ε∂w(1,t)∂x=2ε,t[0,1].

Since the exact solution for the Examples (5.1) and (5.2) are not available, we use the double mesh principle to calculate maximum point-wise errors. For each (ε,μ), we calculate the maximum point-wise errors for different values of mesh points and ε,μ using

Eε,μM,Δt=max0iM;0nN|WM,Δt(xi,tn)W2M,Δt/2(xi,tn)|,

before extrapolation and after extrapolation, we use the formula

Eε,μ,extM,Δt=max0iM;0nN|WextM,Δt(xi,tn)Wext2M,Δt/2(xi,tn)|,

where WM,Δt(xi,tn) is the numerical solution with mesh sizes (h,Δt) and W2M,Δt/2(xi,tn) is the numerical solution with (h2,Δt2) mesh points before extrapolation. The numerical solutions after extrapolation are WextM,Δt(xi,tn) with mesh sizes (h,Δt) and Wext2M,Δt/2(xi,tn) with mesh sizes (h2,Δt2). The (ε,μ)-uniform errors before and after extrapolation were calculated using the following formulas, respectively

EM,Δt=maxε,μEε,μM,ΔtandEextM,Δt=maxε,μEε,μ,extrM,Δt.

The (ε,μ)-uniform rate of convergence before and after extrapolation were calculated using the following formulas, respectively

RM,Δt=maxε,μRε,μM,ΔtandRextM,Δt=maxε,μRε,μ,extM,Δt.

Numerical results in Tables for an equal number of mesh points confirm that the present method before extrapolation has been improved after extrapolation for Example (5.1)-(5.2), respectively. Numerical simulation for Examples (5.1)-(5.2) is displayed in Figures , respectively. From these figures, we observe that the formation of twin boundary layers at x = 0 and x = 1 were demonstrated as ɛ and µ goes very small. For a visual understanding of the theoretical order of convergence graphically, the maximum point-wise errors for Examples (5.1)-(5.2) are plotted using log-log scale as can be seen in Figures , respectively showing the (ε,μ)-uniform convergence.

Table 1. Values of Eε,μ,extM,Δt,EextM,Δt,RextM,Δt, Eε,μM,Δt, EM,Δt,RM,Δt for μ=1010 fcple (5.1)

Table 2. Values of Eε,μ,extM,Δt,EextM,Δt,RextM,Δt, Eε,μM,Δt, EM,Δt,RM,Δt for μ=1010 for example (5.2)

Figure 1. Mesh plot of the numerical solution for example (5.1) at M=32=1Δt.

Figure 1. Mesh plot of the numerical solution for example (5.1) at M=32=1Δt.

Figure 2. Log-log plot of the maximum errors at μ=1010 for example (5.1).

Figure 2. Log-log plot of the maximum errors at μ=10−10 for example (5.1).

Figure 3. Mesh plot of the numerical solution for example (5.2) at N=64=1Δt.

Figure 3. Mesh plot of the numerical solution for example (5.2) at N=64=1Δt.

Figure 4. Log-log plot of the maximum errors at μ=1010 for example (5.2).

Figure 4. Log-log plot of the maximum errors at μ=10−10 for example (5.2).

6. Conclusion

From the table of values, we deduce that when the mesh points increase, the maximum point-wise errors decrease. The developed method is first-order uniformly convergent independent of small parameters ε,μ. To boost the accuracy, we applied the Richardson extrapolation. Thus, the proposed method is accurate and converges uniformly with order of convergence O(M1+Δt) before extrapolation and O(M2+Δt2) after extrapolation. The numerical solutions displayed in Tables show that the present method is (ε,μ)-uniformly convergent of second-order and it agrees with the theoretical order of convergence. When ɛ and µ are small, one can see that the proposed method produces smaller errors in Tables than in Tables . Graphs were plotted for the considered Examples by taking various values of the parameters ɛ and µ to demonstrate the suitability of the proposed method.

Table 3. Values of Eε,μ,extM,Δt,EextM,Δt,RextM,Δt, Eε,μM,Δt, EM,Δt,RM,Δt for ε=102 for example (5.1)

Table 4. Values of Eε,μ,extM,Δt,EextM,Δt,RextM,Δt, Eε,μM,Δt, EM,Δt,RM,Δt for ε=102 for example (5.2)

Public Interest Statement

Asymptotic and numerical solutions to two-parameter singularly perturbed differential equations have received relatively little study in comparison to their one-parameter counterparts. Various numerical approaches for solving singularly perturbed parabolic two-parameters problems with initial-Dirichlet boundary conditions have recently been developed. In this study, a non-standard fitted operator method in the space direction and implicit Euler method in the time direction are used to discretize a singularly perturbed parabolic two-parameters problems with initial-Robin boundary conditions. Furthermore, the new fitted operator method is used to discretize the Robin boundary conditions. The present method with Richardson extrapolation gives more accurate, stable, and uniformly convergent numerical solutions.

Supplemental material

Acknowledgements

The authors are thanks the anonymous reviewers for their constructive comments and suggestions aimed at improving the quality of the manuscript.

Disclosure statement

No potential conflict of interest was reported by the author(s).

Funding

The authors received no direct funding for this research work.

Supplementary Material

Supplemental data for this article can be accessed online at https://doi.org/10.1080/27684830.2024.2354536

Additional information

Notes on contributors

Fasika Wondimu Gelu

Fasika Wondimu Gelu received his M.Sc. and Ph.D. degrees from the Department of Mathematics, Jimma University, Ethiopia. Since 2016 he has been a lecturer at Dilla University, Ethiopia. He is the author of (13) thirteen articles published in different national and international journals. The authors of this research work have focused on numerical solution of singularly perturbed problems of ODEs and PDEs with one-parameter and two-parameters.

Gemechis File Duressa

Gemechis File Duressa received his M.Sc. degree from Addis Ababa University, Ethiopia, and a Ph.D. degree from National Institute of Technology, Warangal, India. He is presently working at Jimma University as a full Professor of Mathematics and Vice President, administrative and development, Jimma University, Ethiopia. He is the author of more than 185 research papers published in different national and international journals. He is working as a referee for several reputable international journals. The authors of this research work have focused on numerical solution of singularly perturbed problems of ODEs and PDEs with one-parameter and two-parameters.

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