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Dynamics of a diffusive age-structured HBV model with saturating incidence

  • Received: 01 October 2015 Accepted: 29 June 2018 Published: 01 July 2016
  • MSC : Primary: 35C07, 35K57, 35J61; Secondary: 37B25, 92D30.

  • In this paper, we propose and investigate an age-structured hepatitis B virus (HBV) model with saturating incidence and spatial diffusion where the viral contamination process is described by the age-since-infection. We first analyze the well-posedness of the initial-boundary values problem of the model in the bounded domain ΩRn and obtain an explicit formula for the basic reproductive number R0 of the model. Then we investigate the global behavior of the model in terms of R0: if R01, then the uninfected steady state is globally asymptotically stable, whereas if R0>1, then the infected steady state is globally asymptotically stable. In addition, when R0>1, by constructing a suitable Lyapunov-like functional decreasing along the travelling waves to show their convergence towards two steady states as t tends to ±, we prove the existence of traveling wave solutions. Numerical simulations are provided to illustrate the theoretical results.

    Citation: Xichao Duan, Sanling Yuan, Kaifa Wang. Dynamics of a diffusive age-structured HBV model with saturating incidence[J]. Mathematical Biosciences and Engineering, 2016, 13(5): 935-968. doi: 10.3934/mbe.2016024

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  • In this paper, we propose and investigate an age-structured hepatitis B virus (HBV) model with saturating incidence and spatial diffusion where the viral contamination process is described by the age-since-infection. We first analyze the well-posedness of the initial-boundary values problem of the model in the bounded domain ΩRn and obtain an explicit formula for the basic reproductive number R0 of the model. Then we investigate the global behavior of the model in terms of R0: if R01, then the uninfected steady state is globally asymptotically stable, whereas if R0>1, then the infected steady state is globally asymptotically stable. In addition, when R0>1, by constructing a suitable Lyapunov-like functional decreasing along the travelling waves to show their convergence towards two steady states as t tends to ±, we prove the existence of traveling wave solutions. Numerical simulations are provided to illustrate the theoretical results.


    We consider the following hypersingular integral equation on a circle:

    c+2πc=   f(t)sin2ts2dt=g(s),s(c,c+2π). (1.1)

    Equation (1.1), considered the natural integral equation for harmonic problems, aligns with the form derived by Yu [28,29]. While natural integral equations themselves hold limited direct significance for solving boundary value problems (BVPs), they become instrumental in unbounded domain BVPs [8]. By introducing artificial boundaries such as circles or ellipses and applying corresponding natural integral equations on these boundaries, domain decomposition methods and coupled algorithms can be effectively constructed [29].

    Integrals of this kind possess several definitions and we present our definition as follows:

    c+2πc=   f(t)sin2ts2dt=limϵ0{(sϵc+c+2πs+ϵ)f(t)sin2ts2dt8f(s)ϵ} (1.2)

    and

    c+2πc=   f(t)sin2ts2dt=limϵ0{(sϵc+c+2πs+ϵ)f(t)sin2ts2dt4f(s)cotϵ2}. (1.3)

    The equivalent of (1.2) and (1.3) can be similarly obtained in [32].

    The composite middle rectangle rule remains applicable when the singular point coincides with the midpoint of each subinterval, leading to a superconvergence phenomenon. This allows us to derive the error expansion of the error functional. We leverage these asymptotic expansion results to develop an algorithmic scheme for solving hypersingular integral equations.

    The hypersigular integral defined on the integral

    ba=f(t)(ts)2dt=limε0{sεaf(t)(ts)2dt+bs+εf(t)(ts)2dt2f(s)ε},s(a,b), (1.4)

    has been paid much attention recently.

    Hypersingular integrals frequently arise in boundary element methods and various physical problems, including fracture mechanics, elasticity, acoustics, and electromagnetic scattering [31]. Numerous methods have been devised to handle these integrals, such as Gaussian quadrature [9,10], Newton-Cotes rules [3,12,16,17,19,25,26,27,28], transformation methods [5,7,11], and others [2,4,11,24,30]. These studies rigorously analyze trapezoidal-type quadrature formulas for weakly singular, singular (Cauchy principal value), and hypersingular integrals, providing full asymptotic expansions for error analysis [33,34,35,36,37]. Reference [38] explored product integration using a variant of the generalized Euler-Maclaurin summation formula, while [39] applied this formula to study the convergence of weakly singular Fredholm and Volterra integral equations. Hypersingular integral equations in potential theory was studied in [40], and modal analysis of a submerged elastic disk was studied by [43]. Superconvergence results for the hypersingular integral equation was presented in [41]. Singular integral operators [45], finite-part integrals of highly oscillatory functions [42], and hypersingular integrals [44] have been paid much attention in recent years.

    The extrapolation method[13,21,22] is based on the error function as

    T(h)a0=a1h2+a2h4+a3h6+,

    where T(0)=a0 and aj are constants independent of h. In [14], a generalized trapezoidal rule for numerical computation of hypersingular integrals on intervals was introduced, with asymptotic error expansion proven. In [15], the composite trapezoidal rule for Hadamard finite-part integrals with the hypersingular kernel 1/sin2(xs) was discussed, obtaining the main part of the asymptotic error expansion. In [18], two extrapolation algorithms were presented for hypersingular integrals on intervals, proving their convergence rates, which match those of classical middle rectangle rule approximations. In [20], an extrapolation algorithm for supersingular integrals was introduced.

    Before presenting our main results, we first let

    ϕik(t)={1(ki)!11=Mik(τ,t)(τt)2dτ,|t|<1,1(ki)!11Mik(τ,t)(τt)2dτ,|t|>1, (1.5)

    where τ[1,1] and

    Mik(τ,t)=τi(τt)ki=Fi(τ)(τt)ki. (1.6)

    Set J:=()(1,1)(1,), W:C(J)C(1,1) and let

    Tik(τ):=ϕik(τ)+j=1ϕik(2j+τ)+j=1ϕik(2j+τ), (1.7)

    be the linear operator.

    Compared with Gaussian quadrature and Newton-Cotes rules, the extrapolation method is more effective. In the following, the asymptotic error expansion of the middle rectangle rule for Hadamard finite-part integrals on a circle is given, based on the asymptotic error expansion, and an algorithm to solve the hypersingular integrals equation is presented. The asymptotic error expansion is

    En(f,s)=i=0hi2i+1f(i+1)(s)ai(τ), (1.8)

    where ai(τ) are functions independent of h defined as

    ai(τ)={ik=i1(1)k(k+1)!Tki(τ),i1,12Tki(τ),i=0. (1.9)

    This paper provides the asymptotic error expansion of the middle rectangle rule for Hadamard finite-part integrals on circles. Based on this expansion, an algorithm for solving hypersingular integral equations is proposed. To avoid computing ai(τ), an extrapolation algorithm is suggested for a given τ. A series of sj values approximate the singular point s with mesh refinement. Using extrapolation techniques, we achieve higher-order accuracy and obtain a posteriori error estimates. Additionally, a collocation scheme is constructed to solve hypersingular integral equations via extrapolation methods, with proven convergence rates.

    Let c=t0<t1<<tn1<tn=c+2π be a uniform partition of the interval [c,c+2π] with mesh size h=2π/n and set

    ti=t0+(i1)h,i=1,2,,n, (2.1)
    ˆti=ti+h2,i=1,2,,n. (2.2)

    We define fC(t), the constant interpolation for f(t), as

    fC(t)=f(ˆti),  i=1,,n, (2.3)

    and a linear transformation

    t=ˆti(τ):=(τ+1)(ti+1ti)/2+ti,i=1,,n1,  τ[1,1], (2.4)

    from the reference element [1,1] to the subinterval [ti,ti+1].

    Replacing f(t) in (1.1) with fC(t) produces the composite rectangle rule:

    In(f,s):=c+2πc=   fC(t)sin2ts2dx=ni=1ωi(s)f(ti)=I(f;s)En(f,s), (2.5)

    where ωi(s) denotes the Cotes coefficients given by

    ωi(s)=2cot(ti1s2)2cot(tis2) (2.6)

    and En(f,s) is the error functional.

    Let

    γ(τ)=γ(h,s)=min1in|sti|h=1|τ|2 (2.7)

    and

    In,i(s)={titi1tˆtisin2ts2dt,im,tmtm1=      tˆtmsin2ts2dt,i=m. (2.8)

    We also define

    Fi(τ)=τi (2.9)

    and

    ϕi,i+1(t)={1211  Fi(τ)τtdτ,|t|<1,1211Fi(τ)τtdτ,|t|>1. (2.10)

    If Fi(τ) is replaced by the Legendre polynomial, it is known that ϕi,i+1 defines the Legendre function of the second kind [1]. Let

    ϕii(t)={1211= Fi(τ)(τt)2dτ,|t|<1,1211Fi(τ)(τt)2dτ,|t|>1 (2.11)

    and

    ϕik(t)=1211Fi(τ)(τt)ki2(ki)!dτ,  k>i+1. (2.12)

    Define Ks(t) as

    Ks(t)={(ts)2sin2ts2ts,4,t=s. (2.13)

    Theorem 2.1. Assume f(t)C[c,c+2π]. For the middle rectangle rule In(f;s) defined in (2.5) and ai(τ) defined in (1.9), we have

    En(f,s)=i=0hi2i+1f(i+1)(s)ai(τ) (2.14)

    where s=tm1+(1+τ)h/2,  m=1,2,,n.

    Then the error function can be written as

    En(f,s)=f(s)2a0(τ)+hf(s)22a1(τ)++hi2i+1f(i+1)(s)ai(τ)+ (2.15)

    From the error functional, we know that it is not convergence when the first term is a0(τ). By the first part of a0(τ)=0, we have the convergence rate O(h) which is called the superconvergence phenomenon.

    Define

    Mjik(t,s)=(ttj1/2)i(ts)ki=Fji(t)(ts)ki,  ki, (3.1)

    where

    Fji(t)=(ttj1/2)i. (3.2)

    By (2.4), we have

    Mjik(t,s)=hk+22k+2τi(τcj)ki=hk+22k+2Mik(τ,cj)=hk+22k+2Fi(τ)(τcj)ki, (3.3)

    where

    Mik(τ,cj)=τi(τcj)ki=Fi(τ)(τcj)ki, (3.4)
    cj=2(stj1)/h1 (3.5)

    and Fi(τ) is defined as in(2.9).

    Lemma 3.1. Let Ks(t) be defined as in (2.13). For t(tj1,tj), by linear transformation (2.6), we have

    Ks(t)=Kcj(τ),  τ(1,1) (3.6)

    where

    Kcj(τ)=4+4l=1(τcj)2(τcj2ln)2+4l=1(τcj)2(τcj+2ln)2 (3.7)

    and cj is defined as in (3.5).

    Proof. By the identity in [1],

    π2sin2πt=l=l=1(t+l)2, (3.8)

    and then we get

    1sin2ts2=4(ts)2+4l=11(ts2lπ)2+4l=11(ts+2lπ)2 (3.9)

    and

    (ts)2sin2ts2=4+4l=1(ts)2(ts2lπ)2+4l=1(ts)2(ts+2lπ)2. (3.10)

    Then

    Ks(t)=(ts)2sin2ts2=4+4l=1(τcj)2(τcj4lπ/h)2+4l=1(τcj)2(τcj+4lπ/h)2=4+4l=1(τcj)2(τcj2ln)2+4l=1(τcj)2(τcj+2ln)2=Kcj(τ),

    which completes the proof.

    Lemma 3.2. (See [18, Lemma 3.2]) Let Pn(t),n=0,1,, be the Legendre function [1] defined as

    Pn(t)=12n[n2]r=0(1)r(2n2r)!r!(nr)!(n2r)!tn2r. (3.11)

    For the polynomial tn,n=0,1,, it can be expanded by the Legendre function as

    tn=n!2n[n2]k=0(2n4k+1)Pn2k(t)k!(32)nk, (3.12)

    where (a)n=(a)(a+1)(a+n1).

    Lemma 3.3. Let ϕi,i+1(t) and ϕii(t) be defined as in (2.10) and (2.11), respectively. Then

    ϕi,i+1(t)={i1+1j=1ω2j1Q2j1(t),i=2i1,i1j=0ω2jQ2j(t),i=2i11 (3.13)

    and

    ϕii(t)={Q0(t)+i1j=1ajQ2j(t),i=2i1,Q1(t)+i1j=1bjQ2j1(t),i=2i11, (3.14)

    where

    ωj=2j+1211Fi(τ)Pj(τ)dτ (3.15)

    and

    aj=(4j+1)jk=1ω2k1,
    bj=(4j1)jk=1ω2k2.

    Proof. For i=2i1,

    Fi(τ)=τi

    leads to

    Fi(τ)=i1+1j=1ω2j1P2j1(τ), (3.16)

    where ω2j1 is defined as in (3.15) and Pj(τ) are Legendre polynomials. The first part of (3.13) follows immediately from the definition of ϕi,i+1(τ). Since

    i1+1j=1ω2j1=i1+1j=1ω2j1P2j1(1)=Fi(1)=1,

    then we have

    ϕi,i+1(t)=i1j=1aj4j+1[Q2j+1(t)Q2j1(t)]

    with aj=(4j+1)jk=1ω2k1, which leads to the first part of (3.14) by using the recurrence relation [1].

    Pl+1(t)Pl1(t)=(2l+1)Pl(t),  l=1,2,, (3.17)

    which completed the proof.

    Lemma 3.4. Assume s(tm1,tm), for some m, cj defined as in (3.5). Then, we have

    ψik(cj)={2khk+1tmtm1=      Mjik(t,s)sin2ts2dt,j=m,2khk+1tjtj1Mjik(t,s)sin2ts2dt,jm. (3.18)

    Proof. By the equation of (1.2),

    tmtm1=      Mjik(t,s)sin2ts2dt (3.19)
    =tmtm1=      Fmi(t)Ks(t)(ts)2dt=limε0{sεtm1Fmi(t)Ks(t)(ts)2dt+tms+εFmi(t)Ks(t)(ts)2dt2Fmi(s)Ks(s)ε}=hk+12k+1limε0{(cm2εh1+1cm+2εh)Fi(τ)Ks(τ)(τcm)2dτhFi(cm)Ks(cm)ε}=hk+12k+111= Fi(τ)Ks(τ)(τcm)2dτ=hk+12kψii(cm). (3.20)

    The second identity can be obtained similarly.

    Lemma 3.5. Under the assumption of Lemma 3.4, then we have

    ψik(cj)={2khk+1tmtm1=      Mmik(t,s)sin2ts2dt,j=m,2khk+1tjtj1Mjik(t,s)sin2ts2dt,jm. (3.21)

    Proof. We have:

    tmtm1=      Mmik(t,s)sin2ts2dt=tmtm1       Fmi(t)Ks(t)tsdt=limε0{sεtm1Fmi(t)Ks(t)tsdt+tms+εFmi(t)Ks(t)tsdt}=hk+12k+1limε0{(cmε1+1cm+ε)Fi(τ)Ks(τ)τcmdτ}=hk+12k+111 Fi(τ)Ks(τ)τcmdτ=hk+12kψi,i+1(cm). (3.22)

    The second part of this Lemma 3.4 can be obtained similarly.

    Lemma 3.6. For k>i+1, it holds that

    ψik(cj)=2khk+1tjtj1=   Mjik(t,s)(ki)!sin2ts2dt. (3.23)

    Proof. The proof of (3.23) can be obtained similarly to Lemma 3.4 or Lemma 3.5.

    Lemma 3.7. Suppose f(t)C[c,c+2π]. If stj, for any j=1,2,,n, then it holds that

    f(t)fC(t)=i=0k=i(1)i+1f(k)(s)i!Mjik(t,s)(ki)!. (3.24)

    Proof. By taking the Taylor expansion for f(tj1/2), we have

    f(tj1/2)=f(t)+i=0f(i)(t)i!(tj1/2t)i

    and thus,

    f(t)fC(t)=i=1(1)i+1f(i)(t)i!(ttj1/2)i (3.25)

    and

    f(i+1)(t)=k=if(k)(s)(ts)ki(ki)!. (3.26)

    Combining (3.25) and (3.26) leads to (3.24).

    Define

    Hj(t)=f(t)fC(t)i=0k=i(1)i+1f(k+1)(s)h(i+1)!Mjik(t,s)(ki)!,  t(tj1,tj). (3.27)

    Proof.

    (tm1c+c+2πtm  )f(t)fC(t)sin2ts2dt=nj=1,jmtjtj1f(t)fC(t)sin2ts2dt=i=0k=i(1)i+1f(k+1)(s)h(i+1)!(ki)!nj=1,jmtjtj1Mjik(t,s)sin2ts2dt. (3.28)

    By (3.27) of Hj(t), we have

    tmtm1=      f(t)fC(t)sin2ts2dt=tmtm1=      Hm(t)sin2ts2dt+i=0k=i(1)i+1f(k+1)(s)h(i+1)!(ki)!tmtm1=      Mmik(t,s)sin2ts2dt. (3.29)

    Putting (3.28) and (3.29) together yields

    c+2πc=     f(t)fC(t)sin2ts2dt=i=1k=i(1)i+1hkf(k+1)(s)(i+1)!(ki)!nj=1ψik(τ)=i=0hi2i+1f(i+1)(s)ai(τ) (3.30)

    where

    ai(τ)={ik=i1(1)k+1(k+1)!Tki(τ),i>0,12Tki(τ),i=0. (3.31)

    The proof is complete.

    For i=1,

    a0(τ)=ni=1titi1=   tˆtisin2ts2dt=2hk=1ni=1{sin[k(tis)]+sin[k(ti1s)]}4k=11kni=1{cos[k(tis)]cos[k(ti1s)]}=4hk=1ni=1sin[k(tis)]=4hj=1nsin[nj(t1s)]=8πj=1sin[j(1+τ)π]=4πcot(1+τ)π2=4πtanτπ2, (3.32)

    where

    ni=1sin[k(tis)]={nsin[k(t1s)],k=nj,0,otherwise

    has been used. When τ=0, we get a0(τ)=0 [6]. This is not the same as the case with a singular point located on the interval. The reason is that on the circle each subinterval is equal so we just consider the case of s located at the middle of the interval.

    At last, we suggest the modified composite middle rectangle rule, denoting by ˜In(f,s), defined by

    ˜In(f,s)=In(f,s)4πf(s)tanτπ2. (3.33)

    Following asymptotic expansion,

    En(f,s)=i=0hi2i+1f(i+1)(s)ai(τ). (4.1)

    For the given s and positive integer n0, we have

    m0:=n0(sc)2π.

    First, we partition [c,c+2π] into n0 equal subintervals to get a mesh denoted by Π1 with mesh size h1=2π/n0. Then Π1 is refined to get mesh Π2 with mesh size h2=h1/2. In this way, a series of meshes {Πj}(j=1,2,) is obtained in which Πj is refined from Πj1 with mesh size denoted by hj. The extrapolation scheme is presented in Table 1.

    Table 1.  Extrapolation scheme of T(j)i.
    T(h1)=T(1)1
    T(h2)=T(2)1 T(1)2
    T(h3)=T(3)1 T(2)2 T(1)3
    T(h4)=T(4)1 T(3)2 T(2)3 T(1)4
    T(h5)=T(5)1 T(4)2 T(3)3 T(2)4 T(1)5

     | Show Table
    DownLoad: CSV

    Define

    sj=s+τ+12hj,  j=1,2,, (4.2)

    and

    T(hj)=I2j1n0(f,sj). (4.3)

    The extrapolation algorithm takes the form of:

    Step one: Compute  T(j)1=T(hj),  j=1,,m.
    Step two:Compute  T(j)i=T(j+1)i1+T(j+1)i1T(j)i12i11,  i=2,,m,    j=1,,mi.

    Theorem 4.1. Under the same condition of Theorem 2.1, for a given τ and (4.2), we have

    |I(f,s)T(j)i|Chi (4.4)

    and

    |T(j+1)i1T(j)i12i11|Chi1.

    Proof. By Eq (4.1), we get

    I(f,s)T(hj)=I(f,s)I(f,sj)+I(f,sj)T(hj)=I(f,s)I(f,sj)+i=0hij2iai(τ)f(i+1)(sj). (4.5)
    I(f;sj)=I(f;s)+I(f;s)τ+12hj+I(f;s)(τ+12hj)2++I(l2)(f;s)(τ+12hj)l2+, (4.6)

    and

    f(i+1)(sj)=f(i+1)(s)+f(i+2)(s)τ+12hj+f(i+3)(s)2!(τ+12hj)2++f(l)(s)(li1)!(τ+12hj)li1+. (4.7)

    Putting (4.5)–(4.7) together, we have

    I(f,s)T(hj)=i=0bi(s,τ)hij, (4.8)

    where

    bi(s,τ)=f(i+1)(s)ik=1ak(τ)2k(τ+12)ik1(ik)!(τ+1)i2ii!I(i)(f,s), (4.9)

    where bi(s,τ) is a constant for a given τ. By (4.8), we also have

    I(f,s)T(hj+1)=i=0bi(s,τ)hij+1. (4.10)

    By (4.8) and (4.10), with hj=2hj+1, we have

    I(f,s)=2T(hj+1)T(hj)+i=2bi(s,τ)(12i11)hij+O(hl1j)=T(j)2+i=2bi(s,τ)(12i11)hij, (4.11)

    which implies

    I(f,s)T(j)2=i=2bi(s,τ)(12i11)hij (4.12)

    and

    T(j)2=2T(hj+1)T(hj). (4.13)

    The accuracy O(h3) can be obtained after performing the extrapolation process.

    In order to directly use the error expansion of (4.1), we presented the following the new partition as c=t00<t01<<t0,n1<t0n=c+2π with t0i=ti+h2,i=0,1,,n1 and

    f0C(t)=f(t0i). (4.14)

    Then we have the approximate formula:

    ˜In(f;s):=c+2πc=    f0C(t)sin2ts2dt (4.15)
    =nj=0˜ωj(s)f(tj)=c+2πc=   f(t)sin2ts2dt˜En(f,s), (4.16)

    and get

    ˜ωi(s)={2cot(t0s2)2cot(t01s2),i=0,2cot(t0is2)2cot(t0,i+1s2),0<i<n,2cot(t0ns2)2cot(tn+1s2),i=n, (4.17)

    and then we find the following theorem similarly as with Theorem 2.1.

    Theorem 4.2. Assume f(t)C[c,c+2π]. For the rectangle rule ˜In(f;s) defined in (4.15) and a2i+1(τ) defined in (1.9), independent of h and s, such that

    ˜En(f,s)=c+2πc=     f(t)f0C(t)sin2ts2dt=i=0h2i22i+1f(i+1)(s)a2i+1(τ) (4.18)

    where s=tm1+(1+τ)h/2,  m=1,2,,n.

    Similarly as extrapolation scheme T(hj), new extrapolation scheme is presented in Table 2.

    ˜T(hj)=˜I2j1n0(f,sj). (4.19)
    Table 2.  Extrapolation scheme of ˜T(j)i.
    ˜T(h1)=˜T(1)1
    ˜T(h2)=˜T(2)1 ˜T(1)2
    ˜T(h3)=˜T(3)1 ˜T(2)2 ˜T(1)3
    ˜T(h4)=˜T(4)1 ˜T(3)2 ˜T(2)3 ˜T(1)4
    ˜T(h5)=˜T(5)1 ˜T(4)2 ˜T(3)3 ˜T(2)4 ˜T(1)5

     | Show Table
    DownLoad: CSV

    Theorem 4.3. Under the asymptotic expansion of Theorem 4.2, we have

    |I(f,s)˜T(j)i|Ch2i (4.20)

    and the posteriori asymptotic error estimate is given by

    |˜T(j+1)i1˜T(j)i14i11|Ch2i2.

    The proof of Theorem 4.3 can be similarly obtained as with Theorem 4.1, so we omitted it here.

    Consider

    14π2π0=   f(t)sin2ts2dt=g(s),  s(0,2π), (5.1)

    with

    2π0g(t)dt=0. (5.2)

    As in [29], under the compatibility condition (5.2), there exists a unique solution up to an additive constant for (5.1). With periodical condition

    2π0f(t)dt=0, (5.3)

    there is a unique solution of (5.1).

    Applying ˜In(f,s) to approximate the hypersingular integral in (5.1) and using ˆtk=tk1+h/2(k=1,2,,n) of each subinterval to be a collocation point, we get

    12πnm=1(cotˆtktm2cotˆtktm12)fm=g(ˆtk),  k=1,2,,n, (5.4)

    denoted by

    AnFan=Gen, (5.5)

    where

    An=(akm)n×n,akm=12π(cotˆtkxm2cotˆtkxm12),k,m=1,2,,n,Fan=(f1,f2,,fn)T,Gen=(g(ˆt1),g(ˆt2),,g(ˆtn))T, (5.6)

    and fk=f(ˆtk)(k=1,2,,n). Obviously, An is a circulant matrix and also a symmetric Toeplitz matrix. Since,

    nm=1akm=12πnm=1(cotˆtktm2cotˆtktm12)=0, (5.7)

    we see that An is singular.

    The regularizing factor γ0n (see Reference [23]) in (5.4) is introduced, which leads to

    {γ0n+12πnm=1(cotˆtktm2cotˆtktm12)fm=g(ˆtk),k=1,2,,n,nm=1fm=0, (5.8)

    where γ0n has the form

    γ0n=12πnk=1g(ˆtk)h. (5.9)

    System (5.8) is denoted as

    An+1Fan+1=Gen+1, (5.10)

    where

    An+1=(0eTnenAn),Fan+1=(γ0nFan),Gen+1=(0Gen), (5.11)

    and en=(1,1,,1n).

    Linear system (5.8) can be rewritten as

    {γ0n+12πnm=1fm+1fmhcotˆtktm2h=g(ˆtk),  k=1,2,,n,12πnm=1fm+1fmhh=0, (5.12)

    where f1=fn+1 has been used. Let vm=(fm+1fm)/h, and we get

    {γ0n+12πnm=1cotˆtktm2vmh=g(ˆtk),k=1,2,,n,12πnm=1vmh=0. (5.13)

    The following lemma has been proved in [23].

    Lemma 5.1. ([23, Theorem 6.2.1, §6.2, Chapter 6]) For Eq (5.13), its solution is

    vm=h2πnk=1cottmˆtk2f(ˆtk). (5.14)

    Lemma 5.2. ([6, Lemma 4.2]) Let Bn+1=(bik)(n+1)×(n+1) be the inverse matrix of An+1, defined in (5.10). Then,

    (1) Bn+1 is expressed as

    Bn+1=(b00B1 B2Bn), (5.15)

    where

    B1=(b01,b02,,b0n),B2=(b10,b20,,bn0)T, (5.16)
    bi0=b0i=1n,1in, (5.17)
    bik=h22π[n1m=icotˆtktm21nn1m=1mcotˆtktm2], (5.18)
    1in1,1kn,bnk=h22nπn1m=1mcotˆtktm2,1kn. (5.19)

    (2) Bn is a Toeplitz and also circulant matrix.

    (3) for i=1,2,,n, we have

    nk=1|bik|C. (5.20)

    Circulant matrices have unique advantages in matrix operations, such as matrix multiplication. It can greatly save the calculation time and improve the calculation efficiency. The circular matrix only needs to store the elements of the first row (or the first column) to completely determine the entire matrix, because the remaining row (or column) elements are obtained from the cyclic shift of the first row (or column) elements. Circulant matrices have many good mathematical properties, such as the fact that their eigenvalues and eigenvectors can be calculated analytically, which makes it easier to analyze and deal with circulant matrices than general matrices in solving linear equations and eigenvalue problems.

    We present the main theorem of this section.

    Theorem 5.1. The solution of linear system (5.8) or (5.10)is

    f(ˆti)fi=i=0h2i22i+1f(i+1)(s)a2i+1(τ). (5.21)

    Proof. Let Fen+1=(0,f(ˆt1),f(ˆt2),,f(ˆtn))T be the exact vector. Then, from (5.10), we get

    Fen+1Fan+1=Bn+1(An+1Gen+1Gen+1), (5.22)

    which implies

    f(ˆti)fi=bi0nm=1g(ˆtm)+nk=1bik˜En(f,ˆtk)=12πnm=1g(ˆtm)h+nk=1bik˜En(f,ˆtk), (5.23)

    where {bik} are the entries of Bn+1 and ˜En(f,s) is defined in (4.15).

    For the first part of 12πnm=1g(ˆtm)h of the rectangle rule to compute the definite integral 12π2π0g(t)dt.

    Then we have

    f(ˆti)fi=nk=1bik˜En(f,ˆtk)=nk=1biki=0h2i22i+1f(i+1)(ˆtk)a2i+1(τ)=i=0h2i22i+1a2i+1(τ)nk=1bikf(i+1)(ˆtk). (5.24)

    By (5.24) and (5.20), we obtain

    bik=cn+O(h3)

    and

    nk=1bikf(i+1)(ˆtk)=C+O(h2).

    Then we have

    f(ˆti)fi=i=0h2i22i+1a2i+1(τ),

    where (5.19) and (5.20) has been used.

    Example 6.1. We consider (1.1) with density function f(t)=1+2cos(t)+2cos(2t),c=π,c+2π=π.

    Numerical results are presented in Table 3 for s=t[n/4]+(1+τ)h/2. The right half of Table 3 shows that the accuracy of ˜In(s,f) is always O(h2). However, from the left half, the accuracy is O(h2) if s is located at the superconvergence point (τ=0), and if τ0, the middle rectangle rule is divergent.

    Table 3.  Errors of In(s,f) and ˜In(s,f) with s=t[n/4]+(1+τ)h/2.
    In(f,s) ˆIn(f,s)
    n τ=0 τ=2/3 τ=2/3 τ=2/3 τ=2/3
    32 5.3695e-004 -1.2446e+000 1.0651e+000 1.8350e-003 -7.6074e-004
    64 1.2851e-004 -1.1295e+000 1.0421e+000 4.5684e-004 -1.9980e-004
    128 3.1416e-005 -1.0741e+000 1.0310e+000 1.1397e-004 -5.1140e-005
    512 7.7655e-006 -1.0470e+000 1.0256e+000 2.8464e-005 -1.2933e-005
    1024 1.9303e-006 -1.0336e+000 1.0229e+000 7.1123e-006 -3.2516e-006

     | Show Table
    DownLoad: CSV

    Example 6.2. We still consider f(t)=1+2cos(t)+2cos(2t),c=π,c+2π=π. For s=π/2, and g(s)=5.026548245744136e+001, we use s=t[n/4]+(τ+1)h/2 with τ=0 to compute s=π/2.

    For s=0 and g(s)=7.539822368615504e+01, we also use s=t[n/2]+(τ+1)h/2 with τ=0 to compute s=0.

    In Tables 4 and 6, we present the error of the middle rectangle rule as h2, h4, h6, and h8, respectively. In Tables 5 and 7, the convergence rates h2, h4, and h6 also agree with the theoretic analysis of Theorem 4.2.

    Table 4.  Error estimate of the mid-rectangle rule s=π/2.
    0 h4extra h6extra h8extra
    8 5.0106e+000
    16 1.2820e+000 1.9666 3.9121e-002
    32 3.2236e-001 1.9917 2.4790e-003 3.9801 3.6167e-005
    64 8.0707e-002 1.9979 1.5547e-004 3.9950 5.6990e-007 5.9878 4.8600e-009
    128 2.0184e-002 1.9995 9.7253e-006 3.9988 8.9188e-009 5.9977 1.4339e-011 8.4156
    256 5.0464e-003 1.9999 6.0796e-007 3.9997 1.3873e-010 6.0088 -6.3238e-013 4.0491

     | Show Table
    DownLoad: CSV
    Table 5.  A posteriori estimate of the mid-rectangle rule s=π/2.
    0 h4extra h6extra h8extra
    8
    16 1.2429e+000
    32 3.1988e-001 1.9581 2.4428e-003
    64 8.0551e-002 1.9896 1.5490e-004 3.9791 5.6504e-007
    128 2.0174e-002 1.9974 9.7164e-006 3.9948 8.9044e-009 5.9877 1.9003e-011
    256 5.0458e-003 1.9993 6.0782e-007 3.9987 1.3937e-010 5.9976 5.8710e-014 8.3268

     | Show Table
    DownLoad: CSV
    Table 6.  Error estimate estimate of the mid-rectangle rule s=0.
    0 h4extra h6extra h8extra
    8 -5.6517e+00
    16 -1.4432e+00 1.9694 -4.0361e-02
    32 -3.6271e-01 1.9924 -2.5567e-03 3.9806 -3.6452e-05
    64 -9.0799e-02 1.9981 -1.6033e-04 3.9951 -5.7436e-07 5.9879 -4.8673e-09
    128 -2.2707e-02 1.9995 -1.0029e-05 3.9988 -9.0075e-09 5.9947 -3.3666e-11 7.1899
    256 -5.6773e-03 1.9999 -6.2699e-07 3.9996 -1.6669e-10 5.7493 -2.6361e-11 -

     | Show Table
    DownLoad: CSV
    Table 7.  A posteriori estimate of the mid-rectangle rule sj=s+(τ+1)hj/2.
    0 h4extra h6extra h8extra
    8
    16 -1.4028e+00
    32 -3.6016e-01 1.9616 -2.5203e-03
    64 -9.0638e-02 1.9904 -1.5976e-04 3.9796 -5.6949e-07
    128 -2.2697e-02 1.9976 -1.0020e-05 3.9949 -8.9738e-09 5.9878 -1.8955e-11
    256 -5.6766e-03 1.9994 -6.2682e-07 3.9987 -1.4033e-10 5.9990 -2.8645e-14 9.6078

     | Show Table
    DownLoad: CSV

    In Tables 8 and 10, we present the error of the middle rectangle rule as h, h2, h3, and h4, respectively. In Tables 9 and 11, the convergence rates h, h2, and h3 also agree with the theoretic analysis of Theorem 2.1.

    Table 8.  Error estimate of the mid-rectangle rule s=π/2.
    0 h2extra h3extra h4extra
    32 8.1836e+00
    64 3.7710e+00 1.1178 -6.4164e-01
    128 1.7978e+00 1.0687 -1.7536e-01 1.8714 -1.9940e-02
    256 8.7613e-01 1.0370 -4.5544e-02 1.9450 -2.2699e-03 3.1350 2.5439e-04
    512 4.3227e-01 1.0192 -1.1587e-02 1.9747 -2.6881e-04 3.0779 1.7053e-05 3.8989
    1024 2.1467e-01 1.0098 -2.9214e-03 1.9879 -3.2661e-05 3.0410 1.0752e-06 3.9874

     | Show Table
    DownLoad: CSV
    Table 9.  A posteriori estimate of the mid-rectangle rule sj=s+(τ+1)hj/2.
    0 h2extra h3extra h4extra
    32
    64 4.4126e+00
    128 1.9732e+00 1.1611 -1.5542e-01
    256 9.2167e-01 1.0982 -4.3274e-02 1.8447 -2.5243e-03
    512 4.4386e-01 1.0542 -1.1319e-02 1.9348 -2.8587e-04 3.1425 1.5822e-05
    1024 2.1760e-01 1.0284 -2.8887e-03 1.9702 -3.3736e-05 3.0830 1.0652e-06 3.8927

     | Show Table
    DownLoad: CSV
    Table 10.  Error estimate of the mid-rectangle rule s=π.
    0 h2extra h3extra h4extra
    32 -4.5518e+00
    64 -1.9715e+00 1.2071 6.0874e-01
    128 -9.0311e-01 1.1263 1.6531e-01 1.8807 1.7498e-02
    256 -4.3016e-01 1.0700 4.2802e-02 1.9494 1.9665e-03 3.1535 -2.5230e-04
    512 -2.0964e-01 1.0369 1.0874e-02 1.9768 2.3104e-04 3.0894 -1.6885e-05 3.9013
    1024 -1.0345e-01 1.0190 2.7394e-03 1.9889 2.7950e-05 3.0472 -1.0634e-06 3.9890

     | Show Table
    DownLoad: CSV
    Table 11.  A posteriori estimate of the mid-rectangle rule sj=s+(τ+1)hj/2.
    0 h2extra h3extra h4extra
    32
    64 -2.5803e+00
    128 -1.0684e+00 1.2720 1.4781e-01
    256 -4.7296e-01 1.1757 4.0835e-02 1.8559 2.2188e-03
    512 -2.2051e-01 1.1008 1.0643e-02 1.9400 2.4793e-04 3.1618 -1.5694e-05
    1024 -1.0619e-01 1.0542 2.7115e-03 1.9727 2.9013e-05 3.0951 -1.0548e-06 3.8952

     | Show Table
    DownLoad: CSV

    Example 6.3. In this example, we will not only test our method on a hypersingular integral, but also solve a hypersingular integral equation g(s)=2cos(2s)2sin(2s),c=π,c+2π=π, while the analysis solution is f(t)=cos(2t)+sin(2t). The good numerical results indicate that our quadrature is efficient and accurate, which matches the theoretical analysis.

    In Table 12, we list the numerical results at s=1.45122657606971. Numerical results show that the convergence rate of the hypersingular integral equation has the order O(h2). With extrapolation methods, the order can reach O(h4), O(h6), and O(h8) in Table12.

    Table 12.  Error estimate of a hypersingular integral equation.
    h2 h4extra h6extra h8extra
    16 3.70E-02
    32 9.13E-03 1.67E-04
    64 2.27E-03 1.03E-05 -1.70E-07
    128 5.68E-04 6.39E-07 -2.61E-09 4.19E-11
    256 1.42E-04 3.99E-08 -4.06E-11 1.72E-13

     | Show Table
    DownLoad: CSV

    The article mainly focuses on a class of hypersingular integral equations in the boundary element method. A solution centered on the extrapolation algorithm is proposed, which is based on the asymptotic expansion of the error of the composite rectangle rule. By leveraging the asymptotic characteristics of the error of the composite rectangle rule, an extrapolation algorithm is constructed, providing a new approach to solving hypersingular integral equations. The algorithm is verified through in-depth theoretical and numerical examples. It is confirmed that the main part of the error function of the composite rectangle rule has an asymptotic expansion. Numerical experiments show that special functions significantly affect the convergence rate of the algorithm. This discovery has important guiding significance for subsequent algorithm optimization and improvement of computational efficiency. The adoption of this algorithm has two prominent advantages. First, it can obtain high-precision calculation results, meeting the precision requirements of practical applications; second, it is convenient for deriving a posteriori error estimates.

    ba= — —- —- hypersingular integrals

    ba — —- —- Cauchy principal integral

    In(f;s) — —- —- quadrature for hypersingular integrals

    En(f;s) — —- —- error functional of the quadrature for In(f;s)

    γ(τ) — —- —- distance of a singular point to the mesh point

    η(y) — —- —- distance of singular point s to the boundary point

    ωi(s) — —- —- Cote coefficients of In(f;s)

    ϕik(t) — —- —- special function of En(f;s)

    ai(τ) — —- —- special function in En(f;s)

    γ0n — —- —- the regularization factor

    T(hj) — —- —- extrapolation value

    Hj(t) — —- —- errors of

    Hj(t)=f(t)fC(t)i=0k=i(1)i+1f(k+1)(s)h(i+1)!Mjik(t,s)(ki)!,  t(tj1,tj),

    subinterval [tm,tm+1].

    Qian Ge performed the data analysis; Jin Li performed the formal analysis and wrote the manuscript. All authors have read and approved the final version of the manuscript for publication.

    The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this article.

    The authors gratefully acknowledge the helpful comments and suggestions of the reviewers, which have improved the presentation.

    The work of Jin Li was supported by the Natural Science Foundation of Shandong Province (Grant No. ZR2022MA003).

    The authors declare no conflicts of interest.

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