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ORIGINAL RESEARCH article

Front. Phys., 14 December 2022
Sec. Statistical and Computational Physics

Hilbert solution, iterative algorithms, convergence theoretical results, and error bound for the fractional Langevin model arising in fluids with Caputo’s independent derivative

  • 1Department of Basic Sciences, Faculty of Arts and Educational Sciences, Middle East University, Amman, Jordan
  • 2Department of Mathematics, Faculty of Science, Al Balqa Applied University, Salt, Jordan
  • 3Department of Mathematics, Faculty of Science, The University of Jordan, Amman, Jordan

Studying and analyzing the random motion of a particle immersed in a liquid represented in the Langevin fractional model by Caputo’s independent derivative is one of the aims of applied physics. In this article, we will attend to a new, accurate, and comprehensive numerical solution to the aforementioned model using the reproducing kernel Hilbert approach. Basically, numerical and exact solutions of the fractional Langevin model are represented using an infinite/finite sum, simultaneously, in the Σ2Ξ space. The proof has been sketched for many mathematical theorems such as independence, convergence, error behavior, and completeness of the solution. A sufficient set of tabular results and two-dimensional graphs are shown, and absolute/relative error graphs that express the dynamic behavior of the fractional parameters α,β are utilized as well. From an analytical and practical point of view, we noticed that the simulation process and the iterative approach are appropriate, easy, and highly efficient tools for solving the studied model. In conclusion, what we have carried out is presented with a set of recommendations and an outlook on the most important literature used.

1 Introduction

The Langevin equation, in its fractional issue, is a mathematical dynamic model fundamental in Brownian motion applications to characterize the emergence of physical episodes in oscillating mediums. It is a popularization of the conventional model that utilizes a fractional Gaussian procedure formalized by two vertices, which is much more adaptable to the parameterization of the fractal evolution processes [14]. The applications of the FLM can be seen in the stock market, motor control system modeling, photoelectron counting, fluid suspensions, deuteron-cluster dynamics, protein dynamics, evacuation process modeling, financial markets, single-file diffusion, and anomalous transport [58]. Commonly, FDMs have wide applications in the formation of many engineering and fluid physics phenomena. In the second half of the last century, the search for more serious numerical algorithms began to control many of the nonlinear problems that appeared with the emergence of fractional derivatives and their emerging applications. However, many studies came into existence, as in the following literature [913]. To date, effective analytical and numerical schemes have been developed and successfully applied to deal with different classes of FDMs [1420].

Although finding accurate solutions to FDMs of different orders in Brownian particle motion placements is an important problem for understanding the dynamic attitudes of oscillatory environments in trifling media, in this article, we contemplate creating an accurate numerical solution to FLMs utilizing the CFD with appropriate boundary data using a new renewal in the RKHA. Here, we will generate effective and straightforward numerical solutions without imposing any restrictions on the nature of the proposed FLM and obtain sufficient convergence while reducing the computation time by exposure to the following model [18]:

βxαx+μEx=Hx,Ex,(1)

equipped with the posterior boundary condition:

E0E0=0,αxE1E1α=0.(2)

Typically, the FDM (Eqs 1, 2) consists of the posterior parameters, functions, and variable effects as attached:

1) xΞ:0,1 stands for the time-coordinate independent domain.

2) 0α,β1 stands for the rank of fractional derivatives applied.

3) E:0,1R stands for the particle position.

4) γxE:ΞR is the CFD of the rank γ of E and is given as follows:

γxEx=1Γ1γ0xxωγxEωdω,0<γ<1,xEx,γ=1.(3)

6) H:Ξ×RR is a bounded variational map that symbolizes the imposed acting on Brownian particles.

7) μR is a nontrivial parameter that represents the damping or viscosity term.

8) E0,E1αR are nontrivial parameters that represent the initial and terminal positions of the particle simultaneously.

Ordinarily, no conventional schemes produce an accurate prototype solution for FLMs. Thus, there is a great need for the RKHA, which satisfies the purpose, as usual, and has reached the desired and satisfactory numerical results with fully stochastic properties. Here, the relevant theories and facts have been confirmed by numeric emulations, graphical representation, and scale tables for three types of FLMs. However, the tenor of the paper is arranged as follows: Section 1: Presentation: FDMs and CFDs. Section 2: RKHA: Preliminaries and definitions. Section 3: RKHA: Construction and properties. Section 4: RKHA: Solutions and convergence. Section 5: Error: Estimation and bound. Section 6: Justifications: Algorithms, applications, and analyses. Section 7: Outline: Conclusion and outlook.

2 Reproducing kernel: Preliminaries and definitions

The approach of the reproducing kernel is a novel solver built to find solutions to FDMs emerging in physics, waves, statistics, and engineering [2123]. This technique is based on the Gram–Schmidt process and Fourier expansion approach for an arbitrary order and is used for optimizing an orthogonal basis to detect unknown compounds. The RKHA has many motivational aspects and a great ability to handle complicated problems without imposing any restrictions on the style of the models. Therefore, it has been gaining a lot of solicitude and examination lately [2432].

First, a reproducing kernel induced from a given Hilbert space is called the RKHA. Here, CΞ is a set of maps that are continuous absolutely on Ξ. At the outset, some requirements that are necessary to go further in our RKHA scheme will be sought.

Remark 1. [24] The frameworks of Σ0Ξ are as follows:

Σ0Ξ=E:ECΞEL2Ξ,E1x,E2xΣ0=E10E20+ΞE1xE2xdx,EΣ02=Ex,ExΣ0,Πx1s=1+s,sx,x,s>x.(4)

Remark 2. [24] The frameworks of Σ1Ξ are as follows:

Σ1Ξ=E:EoCΞEoL2ΞE0=0,E1x,E2xΣ1=o=01E1o0E2o0+E11E21+ΞE1xE2xdx,EΣ12=Ex,ExΣ1,Πx1s=1120Πs,x,sx,Πx,s,s>x,(5)

with Πs,x=s1201+xxx120246x+10x25x3+x4s+51+xxs31+x2s4.

Definition 1 The framework of Σ2Ξ is as follows:

Σ2Ξ=E:EΣ1ΞαxE1=0.(6)

Here, one can find that Σ2Ξ is a subset in Σ1Ξ and is closed. Next, to generate the kernel function of Σ2Ξ, we put ΛEx=/Exx=1.

Theorem 1. If ΛxΛsΠx1s0, then the framework function of Σ2Ξ is as follows:

Πx2s=Πx1sΛxΠx1sΛsΠx1sΛxΛsΠx1s.(7)

Proof: Because α/sΠ12x=0, Πx2sΣ2Ξ. However, for each Es in Σ2Ξ, one can obtain

Es,Πx2s=Es,Πx1s=Ex,(8)

or Πx2s is the reproducing kernel of Σ2Ξ.

Theorem 2. If EΣ2Ξ, then Ex3.5EΣ2, Ex3EΣ2, and Ex2EΣ2.

Proof: Since E,E,E,ECΞ, applying successive integration from 0 to x for E, E, and E, one can obtain

ExE0=0xEpdp,(9)
ExE0E0x=0x0x1Epdpdx1,(10)
ExE0E0x0.5E0x2=0x0x20x1Epdpdx1dx2.(11)

Taking values and using the fact 0x,x21, we can obtain

ExE0+E0+0.5E0+ΞEpdp.(12)

To complete, one can get E0=E20EΣ2, E0=E02EΣ2, E0=E02EΣ2, and ΞExdxΞEx2dxEΣ2.

3 Reproducing kernel: Construction and properties

Herein, the boundaries in Eq. 2 will first be homogenized to zero to obtain easy-to-access modeling in the proposed Σ2Ξ space. The form of the operator that formulates the required solution will also be determined in addition to some of what is needed for the scheme.

To achieve this, one must first carry out the following:

βxαx+μEx=H¯x,Ex,(13)

equipped with the posterior boundary condition:

E0=0,αxE1=0.(14)

For the briefing, the normalizing modified version in Eqs 13, 14 was obtained from the posterior underlying conversion, taking into account that all the extra terms transformed into H¯x,Ex as

Ex:Ex0.5Γ3αE1αx2+E0,(15)
H¯x,ExΓ3αΓ3αβ+μΓ3αΓ3βxαE1αx2αβ+Hx,Ex0.5Γ3αE1αx2E0.(16)

The conversions in Eqs 15, 16 are needful to insert the equipped boundaries in Eq. 2 inside Σ2Ξ. Indeed, we will denote E to new and old solutions always.

1) Define the map Ƌ such that

Ƌ:Σ2ΞΣ0Ξ.(17)

2) Build the ƋE operator as

ƋExβxαx+μEx.(18)

3) Reframe the FLM problem to solve such that

ƋExH¯x,Ex,E0=0,αxE1=0.(19)

Theorem 3. Ƌ:Σ2ΞΣ0Ξ is a bounded linear operator.

Proof: From Remark 1, one can obtain

ƋExΣ02=ƋEx,ƋExΣ0=ƋE02+ΞƋEx2dx.(20)

Using the reproducing property of Πx2s, one can obtain

Ex=Es,Πx2sΣ2,ƋEox=Es,ƋΠx2osΣ2,o=0,1.(21)

With the use of the Schwarz inequality, one can obtain

ƋEox=Ex,ƋΠx2oxΣ2ƋΠx2oxΣ0EΣ2CoEΣ2,o=0,1.(22)

So ƋEΣ02C02+ΞC12dxEΣ22 or ƋEΣ0C02+C12EΣ2. By picking out a countable dense subset xoo=1 in Ξ, defining ωox=Πxo1x, and setting Θox=Ƌ*ωox, one can fit the orthogonal function system of Σ2Ξ. Furthermore, by the Gram–Schmidt process, one can fit the orthonormal function systems Θ¯oxo=1 on Σ2Ξ as

Θ¯ox=k=1oaokΘkx.(23)

Theorem 4. Θoxo=1 is the complete function system of Σ2Ξ with

Θox=ƋsΠx2ss=xo.(24)

Proof: First, Ƌs indicates that Ƌ applies to a function of s. Certainly,

Θox=Ƌ*ωox=Ƌ*ωos,Πx2sΣ2=ωos,ƋsΠx2sΣ0=ƋsΠx2ss=xo.(25)

So Θox can be written as ƋsΠx2ss=xo in Σ2Ξ. To illustrate more effective properties in Σ2Ξ, the set Πxo2xo=1 is linearly independent as coo=1η agrees well with o=1ηcoΠxo2x=0, and for l=1,2,,η, taking Ekx in Σ2Ξ as Ekxl=δl,k, then

0=Ekx,o=1ηcoΠxo2xΣ2=o=1ηboEkx,Πxo2xΣ2=o=1ηcoEkxo=co,k=1,2,,η.(26)

So Πxo2xo=1η is linearly independent for each η1.

4 Reproducing kernel: Solutions and convergence

This section aims to construct exact and RKHA numeric solutions of Eq. 19, together with some convergence theories, to ensure this analysis is more efficient. Here, CΞ,R and CΞ×R,R indicate a set of continuous maps on the group inside parentheses.

If ECΞ,R and Θ¯oxo=1 are orthonormal, then Ex,Θ¯oxΣ2, o=1,2, are the Fourier maps of E for Θ¯oxo=1 and its Fourier expansion Ex=o=1Ex,Θ¯oxΣ2Θ¯ox, wherein xoo=1 is dense throughout Ξ.

Theorem 5. Suppose that aoko,k=1,1,o are orthogonalization coefficients of Θ¯oxo=1 and a unique solution of Eq. 19 exists, then the posteriors are accomplished:

1) As ϰ, the exact solution, Ex, of Eqs 1, 2 is as follows:

Ex=o=1k=1oaokH¯xk,ExkΘ¯ox.(27)

2) The RKHA numeric solution, Eϰx, of Eqs 1, 2 is as follows:

Eϰx=o=1ϰk=1oaokH¯xk,ExkΘ¯ox.(28)

Proof: For the first side: Through Theorem 4, Θ¯oxo=1 is an orthonormal basis in Σ2Ξ, which is complete. Using o=1Ex,Θ¯oxΣ2Θ¯ox as the Fourier expansion concerning Θ¯oxo=1, one can obtain o=1Ex,Θ¯oxΣ2Θ¯ox< in Σ2. So

Ex=o=1Ex,Θ¯oxΣ2Θ¯ox=o=1Ex,k=1oaokΘkxΣ2Θ¯ox=o=1k=1oaokEx,Ƌ*EkxΣ2Θ¯ox=o=1k=1oaokƋEx,ωjxΣ0Θ¯ox=o=1k=1oaokH¯x,Ex,ωjxΣ0Θ¯ox=o=1k=1oaokH¯xk,ExkΘ¯ox.(29)

For the second side: Because o=1Ex,Θ¯oxΣ2Θ¯ox< and Σ2Ξ are the Hilbert space, one can truncate Eq. 27 using the ϰ-idiom RKHA numeric solution of Ex to generate Eq. 28.

Remark 3. Assume that Eϰ1Σ2< and xoo=1 are dense throughout Ξ. Then, according to Eqs 2728, the portrayal effect can be determined as follows:

Ex=o=1VoΘ¯ox,Vo=k=1oaokH¯xk,Exk.(30)
Eϰx=o=1ϰVoΘ¯ox,Vo=k=1oaokH¯xk,Ek1xk.(31)

Theorem 6. Assume that Eϰ1EΣ20, xϰs as ϰ, Eϰ1Σ2<, and H¯x,ExCΞ×R,R. Then, H¯xϰ,Eϰ1xϰH¯s,Es as ϰ.Proof: It all started where Eϰ1xϰEs as ϰ. Evidently, one can obtain

Eϰ1xϰEs=Eϰ1xϰEϰ1s+Eϰ1sEsEϰ1xϰEϰ1s+Eϰ1sEsEϰ1σxϰs+Eϰ1sEs,(32)

with σ in between xϰ and s. Applying Theorem 2, one can obtain Eϰ1sEs3.5Eϰ1EΣ2 or equivalently Eϰ1sys0 as ϰ and Eϰ1σ3Eϰ1Σ2. Using Eϰ1Σ2< and xϰs, one can obtain equivalently Eϰ1xϰEϰ1s0 as ϰ. By H¯x,ExCΞ×R,R, it gives a glimpse that H¯xϰ,Eϰ1xϰH¯s,us as ϰ.

Theorem 7. One gains EϰxEx as ϰ.Proof: Because Eϰ+1x=Eϰx+ Vϰ+1Θ¯ϰ+1x and the orthogonality of Θ¯oxo=1, one can obtain

Eϰ+1Σ22=EϰΣ22+Vϰ+12=Eϰ1Σ22+Vϰ2+Vϰ+12==E0Σ22+o=1ϰ+1Vo2.(33)

So Eϰ+1Σ2EϰΣ2 and κR such that o=1Vo2=κ or Vo2o=1l2. To get

ExE1xE1xE2xEϰ+1xEϰx,(34)

it is adequate to have for >ϰ that

EEϰΣ22=EE1+E1+Eϰ+1EϰΣ22=EE1Σ22+E1E2Σ22++Eϰ+1EϰΣ22,(35)

with EE1Σ22=V2. However, on the other line, EEϰΣ22=l=ϰ+1Vo20 as ϰ,. Using completeness, EϰxΣ2Ξ such that EϰxEx as ϰ.

Theorem 8. Assume that Eϰ1Σ2< and xoo=1 are dense throughout Ξ. Then, Ex=o=1VoΘ¯ox as ϰ.Proof: Applying limϰ on Eq. 31, one gets Ex=o=1VoΘ¯ox. So

ƋExk=o=1VoƋΘ¯ox,ωkxΣ0=o=1VoΘ¯ox,Ƌ*SkxΣ2=o=1VoΘ¯ox,ΘkxΣ2.,(36)
k=1lalkƋΘxk=o=1VoΘ¯ox,k=1lalkΘkxΣ2=o=1VoΘ¯ox,Θ¯lxΣ2=Vl.(37)

Sequentially, if l=1, then ƋEx1=H¯x1,E0x1, and if l=2, then ƋEx2=H¯x2,E1x2. As a rule, one can obtain ƋExϰ=H¯xϰ,Eϰ1xϰ. By the condition of density, xΞ; xϰqq=1 such that xϰqx as q or equivalently ƋExϰq=H¯xϰq,Eϰq1xϰq. Letting q, one gets ƋEx=H¯E,Ex. Because Θ¯oxΣ2Ξ, Ex fulfills (Eq. 19).

5 Error: Estimation and bound

As a matter of fact, the exact solution of FDMs (Eqs 1, 2) restricted with the CFD depends on α and β. In most cases, this real problem is complicated to be solved traditionally because it lacks an exact solution. This induces us to develop numerical schemes like RKHA that generate approximated realizations of the exact solution depending on the values of α and β.

Here, we will fix T=xoo=1ϰΞ0,1 with x1x2xϰΞ, =max0oϰxo+1xo, =maxxxo,xo+1x, and Ƌ1=sup0EΣ2EΣ01Ƌ1Σ2. Furthermore, we will fix REϰx=ƋEϰxH¯x,Ex to the residual truncated error at xΞ.

Lemma 1. One gains ƋEϰxj=ƋExj, xjT.Proof: Set Πϰ:Σ2Ξj=1ϰbjEjx,bjR. So

ƋEϰxj=Eϰx,ƋxkΠxk2xΣ2=Eϰx,EkxΣ2=ΠϰEx,EjxΣ2=Ex,ΠϰEjxΣ2=Ex,EjxΣ2=Ex,ƋxjΠxj2xΣ2=ƋxjEx,Πxj2xΣ2=ƋxjExj=ƋExj.(38)

In other words, ƋEϰxj=ƋExj.

Lemma 2. Assume that CΞ,R, +1L2Ξ for a fixed 1, and 0 at T with ϰ+1. So Σ0Ξ and a parameter A exist with

Σ0AmaxxΞ+1x.(39)

Proof: Clearly, Σ0Ξ and xxo,xo+1, o=1,2,ϰ, one can obtain

x=xτo=τoxτdτxτomaxxxo,xo+1x,.(40)

On xo,xo+1, applying Roll’s theorem on yields τo=0 with τoxo,xo+1, o=1,2,,ϰ1. So for fixed x, τo such that xτo<2. Similarly, one can write

x=xτo=τoxτdτxτomaxxxo,xo+1x,2.(41)

So x22. Sequentially, a parameter C1 exists with xC1+1+1 and xC1+1. By compiling the previous results, one can obtain

Σ0=02+Ξτ2dτ12AmaxxΞ+1x,(42)

with A=C1+1.

Theorem 9. A parameter B exists with

EoEϰoBmaxxΞREϰ+1x,o=0,1,2.(43)

Proof: Utilizing Lemma 3, one can obtain

REϰW21AmaxxΞREϰ+1x.(44)

However, since REϰx=ƋEϰxH¯E,Ex=ƋEϰxEx, then EEϰ=Ƌ1REϰ and a parameter C2 exists with

EEϰΣ2=Ƌ1REϰΣ2Ƌ1REϰΣ0AC2maxxΞREϰ+1x.(45)

Applying Theorem 2, one can obtain

EoEϰoC3EEϰΣ2AC2C3maxxΞREϰ+1x,o=0,1,2.(46)

In another mode, one can obtain EoEϰoBmaxxΞREϰ+1x, o=0,1,2, where B=AC2C3.Ultimately, one can see that EEϰΣ22 is decreasing for a large ϰ as

EEϰΣ22EEϰ1Σ22=o=ϰ+1Ex,Θ¯oxAΘ¯oxΣ22o=ϰEx,Θ¯oxΣ2Θ¯oxΣ22=o=ϰ+1Ex,Λ¯olΣ22o=ϰEx,Θ¯oxΣ22<0.(47)

However, as o=1Ex,Θ¯oxΣ2Θ¯ox<, one can obtain EEϰΣ220 as ϰ.

6 Justifications: Algorithms, applications, and analyses

To clarify the portability and effectiveness of the presented numeric approach, we need some of the steps, the first of which is to provide sufficient algorithms to demonstrate the mechanism of the solution, the second of which is to present several tangible applications, and then finally to provide several tables, figures, and numeric explanations of the solution procedures. However, all of this is the content of the following sections.

6.1 Algorithms

Next, three used algorithms in our RKHA implementation are given. These algorithms are problem initialization, the Gram–Schmidt process, and RKHA solution steps, simultaneously. However, an expert in the Mathematica platform can interpret these steps in the form of programs.

Stride 1: Set the assumptions.

Ex:Ex12Γ3αE1αx2+E0,(48)
H¯x,ExΓ3αΓ3αβ+μΓ3αΓ3βxαE1αx2αβ+Hx,Ex0.5Γ3αE1αx2E0.(49)

Output: Homogenous FLM.

βxαx+μEx=H¯x,Ex,(50)
E0=0,αxE1=0.(51)

Stride 2: Define a suitable operator.

Ƌ:Σ2ΞΣ0Ξ,(52)
ƋExβxαx+μEx.(53)

Output: Homogenous FLM in the functional form.

ƋExH¯x,Ex,E0=0,αxE1=0.(54)

Algorithm 1. Problem initialization.

Stride 1: At o2 and k=1,2,,o1, evaluate

a11=1Θ1Σ2,aoo=1ΘoΣ22p=1o1Θox,Θ¯pxΣ22,o1aok=1ΘoΣ22p=1o1Θox,Θ¯pxΣ22p=ko1Θox,Θ¯pxΣ2εpj,o>k(55)

Output: aok parameters.

Stride 2: At o=1,2,3,, evaluate

Θ¯ox=j=1oaokΘox.(56)

Output: Θ¯oxo=1 system.

Algorithm 2. Gram–Schmidt process.

Stride I: At fix l,k on Ξ evaluating xo=1/xo and Θox=Ƌ*ωox in o=1,2,,ϰ.

Output: Θox system.

Stride II: Wherein o1 and j=1,2,,o1, evaluate Gram–Schmidt.

Output: aok parameters.

Stride III: Set Θ¯ox=j=1oaokΘox in o=1,2,,ϰ.

Output: Θ¯ox system.

Stride IV: Set E0x0=0 in o=1,2,,ϰ and evaluate

Eoxo=Eo1xo,Vo=k=1oaokH¯xk,Exk,Eϰxo=k=1oVoΘ¯kx.(57)

Output: ϰ-term numeric approximation Eϰxo of Exo.

Algorithm 3. Process of RKHA solutions.

6.2 Applications

Next, three test applications that coincide with the FLM platform are utilized on the basis of the CFD: the first is α,β=1/2,4/5, the second is α,β=1/3,3/4, and the third is α,β=1/4,4/5. Actually, these applications are solved and analyzed using the presented RKHA as utilized in Algorithm 1, Algorithm 2, Algorithm 3.

Application 1: Theorize the posterior and evaluate Eϰxo:

45x12x+1Ex=253Γ15x65+2Γ1710x710,(58)

equipped with the posterior boundary condition:

E0=0,12xE183π=0.(59)

Here, Ex=x2 is the exact smooth solution of Eqs 58, 59 on Ξ.

Application 2: Theorize the posterior and evaluate Eϰxo:

34x13x+1Ex+lnEx=2exΓ14,xΓ14exΓ1112,xΓ1112ex+x,(60)

equipped with the posterior boundary condition:

E0=0,13xE11Γ23,1Γ23e=0.(61)

Here, Ex=ex is the exact smooth solution of Eqs 60, 61 on Ξ.

Application 3: Theorize the posterior and evaluate Eϰxo:

45x14x+μEx+Ex3=253Γ15x65+2Γ3920x1920,(62)

equipped with the posterior boundary condition:

E0=0,14xE13221Γ34=0.(63)

Here, Ex=x1/2+x4/33 is the exact smooth solution of (Eqs 62, 63) on Ξ.

6.3 Analyses

Eventually, to clarify the portability and effectiveness of the presented RKHA, we present and provide several RKHA solution tables, RKHA numeric solution figures, RKHA absolute error figures, and RKHA relative error figures. However, in this section, we used xo=o1/ϰ1 with o=1,2,,ϰ=101 in Eϰxo on Ξ and then executed Algorithm 3 throughout and its related steps.

The tabulated data presenting

xo,Exo,xo,Eϰxo,ρϰxo=ExoEϰxo,σϰxo=ExoEϰxoE1xo,(64)

concerning the features of the memory inherited, are utilized in detail by the RKHA performance of the applications addressed previously, as shown in the included tables (Tables 13).

TABLE 1
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TABLE 1. Associated RKHA scores for application 1 with ϰ=101, when α,β=1/2,4/5.

TABLE 2
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TABLE 2. Associated RKHA scores for application 2 with ϰ=101, when α,β=1/3,3/4.

TABLE 3
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TABLE 3. Associated RKHA scores for application 3 with ϰ=101, when α,β=1/4,4/5.

The 2-D Cartesian plots presenting xo,Exo, concerning the features of the memory inherited, are utilized in detail by the RKHA performance of the applications addressed previously, as shown in the included graphs (Figures 1A–C).

FIGURE 1
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FIGURE 1. 2-D Cartesian plots of the RKHA numeric solution of the FLM platform over Ξ: (A) application 1, when α,β=1/2,4/5; (B) application 2, when α,β=1/3,3/4; and (C) application 3, when α,β=1/4,4/5.

The 2-D Cartesian plots presenting xo,ρϰxo, concerning the features of the memory inherited, are utilized in detail by the RKHA performance of the applications addressed previously, as shown in the included graphs (Figures 2A–C).

FIGURE 2
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FIGURE 2. 2-D Cartesian plots of RKHA absolute errors of the FLM platform over Ξ: (A) application 1, when α,β=1/2,4/5; (B) application 2, when α,β=1/3,3/4; and (C) application 3, when α,β=1/4,4/5.

Ultimately, the 2-D Cartesian plots presenting xo,σϰxo, concerning the features of the memory inherited, are utilized in detail by the RKHA performance of the applications addressed previously, as shown in the included graphs (Figures 3A–C).

FIGURE 3
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FIGURE 3. 2-D Cartesian plots of RKHA relative errors of the FLM platform over Ξ: (A) application 1, when α,β=1/2,4/5; (B) application 2, when α,β=1/3,3/4; and (C) application 3, when α,β=1/4,4/5.

7 Outline: Conclusion and outlook

This research embraced the RKHA to handle a type of well-known FDM called FLM on the basis of the CFD by including three test applications. A detailed presentation of the theories related to the establishment of the solution and the formulation of the approximate was interspersed with the construction of the necessary spaces and the associations’ form of Green’s functions used, with many new results that centered on convergence, error, and independence. Based on the RKHA, Exo, Eϰxo, ρϰxo, and σϰxo have been sketched in 2-D and tabulated for various value parameters of α,β and xo. Conclusively, obtaining analytical solutions for many types of FDMs is not a simple procedure, which motivates us to conduct more studies and scientific research to obtain innovative approximations of FDMs subject to influence the CFD. The RKHA has diverse feasible and favorable benefits. First, the RKHA is appropriate and delicate since the approximation is very closest to the required solution. Second, by utilizing small ϰ terms, we can obtain high accuracy. Third, it is an easy, simple, and soft method to be applied since it does not require sophisticated mathematical tools or an adept professional programmer. Fourth, it is global since it may be utilized to handle different types of fractional complex models. Fifth, the main characteristic of the RKHA is that it may be used with other orthogonal basis sequences. Our outlook study will focus on solving the FLM concerning fuzzy boundaries.

Data availability statement

The original contributions presented in the study are included in the article/Supplementary Material; further inquiries can be directed to the corresponding author.

Author contributions

MA: data curation, investigation, software, methodology, validation, roles/writing—original draft, and writing—review and editing. OA: funding acquisition, investigation, resources, supervision, visualization, and roles/writing—original draft. BM: conceptualization, formal analysis, investigation, project administration, software, and writing—review and editing.

Acknowledgments

The authors are grateful to the Middle East University, Amman, Jordan for the financial support granted to cover the publication fee of this research article.

Conflict of interest

The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Publisher’s note

All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors, and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.

Abbreviations

FLM, fractional Langevin model; RKHA, reproducing kernel Hilbert approach; FDM, fractional differential model; CFD, Caputo’s fractional derivative.

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Keywords: fractional Langevin model, reproducing kernel Hilbert approach, fractional differential model, Caputo fractional derivative MSC2020, 65L10, fluid dynamics

Citation: Aal MA, Arqub OA and Maayah B (2022) Hilbert solution, iterative algorithms, convergence theoretical results, and error bound for the fractional Langevin model arising in fluids with Caputo’s independent derivative. Front. Phys. 10:1072746. doi: 10.3389/fphy.2022.1072746

Received: 17 October 2022; Accepted: 07 November 2022;
Published: 14 December 2022.

Edited by:

Jordan Yankov Hristov, University of Chemical Technology and Metallurgy, Bulgaria

Reviewed by:

Kamal Shah, University of Malakand, Pakistan
Ndolane Sene, Cheikh Anta Diop University, Senegal
Kolade Matthew Owolabi, Federal University of Technology, Nigeria

Copyright © 2022 Aal, Arqub and Maayah. This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.

*Correspondence: Omar Abu Arqub, o.abuarqub@bau.edu.jo

Disclaimer: All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article or claim that may be made by its manufacturer is not guaranteed or endorsed by the publisher.