In this paper, layer potential techniques are investigated for solving the thermal diffusion problem. We construct the Green function to get the analytic solution. Moreover, by combining Fourier transform some attractive relation between initial heat distribution and the final observation is obtained. Finally iteration scheme is developed to solve the inverse heat conduction problem and convergence results are presented.
Citation: Xiaoping Fang, Youjun Deng, Zaiyun Zhang. Reconstruction of initial heat distribution via Green function method[J]. Electronic Research Archive, 2022, 30(8): 3071-3086. doi: 10.3934/era.2022156
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In this paper, layer potential techniques are investigated for solving the thermal diffusion problem. We construct the Green function to get the analytic solution. Moreover, by combining Fourier transform some attractive relation between initial heat distribution and the final observation is obtained. Finally iteration scheme is developed to solve the inverse heat conduction problem and convergence results are presented.
The thermal diffusion problem has long been studied. Applications can be found in various physical and engineering settings, in particular in hydrology [1], material sciences, heat transfer [2] and transport problems, etc. The inverse problems for determination of initial temperature, thermal conductivity or heat source from final over determination or other additional measurements have been widely considered by lots of researchers (see, e.g., [3,4,5,6,7,8,9,10,11]). In [11], the authors explored the Tikhonov regularization for simultaneous reconstruction of the initial temperature and heat radiative coefficient in a heat conductive system. They used the final observation and temperature in a small region as the additional data. In [9], an exact and analytical representation of the initial heat distribution was given by using only the measurements of temperature and heat flux at one point. In [12], the authors proved the uniqueness of the identification of unknown source locations in two-dimensional heat equations from scattered measurements and presented some numerical methods to identify the locations. Hon and Wei introduced the fundamental solution methods in solving inverse heat conduction problems [6,7]. In recent years a special kind of inverse heat conduction problem called sideways parabolic equations have also been widely studied [13,14,15,16,17]. Various regularization methods are presented to solve the severely ill-posed problem and optimal convergence results are obtained in different stopping rules.
Reconstruction of thermophysical properties such as thermal conductivity and heat capacity is another interesting and meaningful research area. Many theoretical and experimental methods have been developed in the literature, they include, among others, the steady-state method, the probe method [18], the periodic heating method [19], the least-squares method [20] and the pulse heating method. For a steady case, the layer potential technique is widely used for analysis of the solution and reconstruction of the thermal conductivity [21,22]. In [21], the authors construct the Generalized Polarization Tensors based on layer potential method in reconstruction of the shape of the homogeneous conductive body. Besides, layer potential techniques are widely used in wave prorogation problems, including Helmholtz problems, Maxwell problems, Elastic problems and so on (see [23,24,25,26,27,28,29] and there references there in).
In this paper, we shall consider the reconstruction of the initial heat distribution from final observation in the upper half plane. The Dirichlet boundary condition is given. We firstly use the layer potential method to represent the solution of the forward heat conduction problem in an integral form. Then by exploring the Green function, the Dirichlet boundary problem can be solved analytically without knowing the Neumann boundary condition. By using appropriate extension and Fourier transform, we derive a very simple relation between the initial heat distribution and the final observation. The severely ill-posed problem for reconstruction of initial temperature then is done by introducing a new iteration scheme. Convergence results are investigated under both the a priori and a posteriori stopping rules. The main contribution of this paper is to extend the layer potential techniques to the inverse heat diffusion problem and designing of a new iterative scheme in solving the related inverse heat distribution problem, theoretically. We shall consider the numerical implementation in a forthcoming work.
The organization of this paper is as follows. In the second section, we shall introduce the layer potential techniques together with Green's function in representing the integral solution to the heat diffusion problem, while proofs of the main theorems can be found in Appendix A. In Section 3, the attractive relation between initial heat distribution and the final observation shall be derived by making use of the properties of layer potentials. Base on the relation, a new iterative methods is designed in solving the inverse heat distribution problem. We then analyze some properties of the Fourier transform and derived the convergence results by using the aforementioned iterative methods, in Section 4 and 5, respectively. Some conclusions are made in Section 6.}
We shall first consider the forward heat conduction problem in the half plane
{ut=kΔu(x,t)∈R×R+×(0,T),u(x,0)=μ0(x)x∈R×R+,u(x1,0,t)=f(x1,t)(x1,t)∈R×(0,T) | (2.1) |
where R+:=(0,+∞) and x:=(x1,x2). The thermal diffusion coefficient k is supposed to be a positive constant. The initial temperature and boundary temperature are given and denoted by μ0(x1,x2) and f(x1,t), respectively. In this paper, we suppose that μ0(x)∈L2(R×R+) and f(x,t)∈L2(R×(0,T)).
We shall consider the analytic solution to the forward problem (2.1) by using the Green function method. Let Γ(x,t) be the fundamental solution to the heat equation, i.e.,
Γk(x,t)=14πkte−|x|24kt | (2.2) |
which satisfies
{(Γk)t=kΔΓk(x,t)∈R2×R+Γk(x,0)=δ0x∈R2 |
where δ0 is the Dirac function at the origin [31]. To derive the solution to (2.1), we firstly introduce the two well known quantities, single layer potential and double layer potential for heat equation. They are extensions of the classical layer potentials in electrostatic problem [32]. For a domain D, we denote by SkD (if k=1 then we simply denote by SD) the single layer potential
SkD[φ](x,t):=∫t0∫∂DΓk(x−y,t−s)φ(y,s)dσyds,x∈R2∖∂D | (2.3) |
for a density function φ(x,t)∈H−1/2,1(∂D,R+) and denote by DkD (if k=1 then denote by DD) the double layer potential
DkD[ψ](x,t):=∫t0∫∂D∂∂νyΓk(x−y,t−s)ψ(y,s)dσyds,x∈R2∖∂D | (2.4) |
for a density funtion ψ(x,t)∈H1/2,1(∂D,R+). We shall further define a volume potential by
VkD[μ](x,t):=∫DΓk(x−y,t)μ(y)dy,x∈R2 | (2.5) |
for a function μ(x)∈L2(D). Here y=(y1,y2). By using Green's formula, the solution to (2.1) can be written in the form of layer potentials. We state the result in the following theorem, for the sake of convenience to the reader, where proofs can be found in the appendix.
Theorem 2.1. The solution to the heat conduction problem
{ut=kΔu(x,t)∈D×(0,T),u(x,0)=μ0(x)x∈D,u(x,t)=f(x,t)(x,t)∈∂D×(0,T) |
has the following form
u(x,t)=VkD[μ0](x,t)+SkD[k∂u/∂ν](x,t)−kDkD[f](x,t). | (2.6) |
We see from the solution form (2.6) that it contains both Dirichlet and Neumann boundary conditions. Thus, in order to get the solution of (2.1) by using the integral form (2.6), additional Neumann boundary condition is required. In this paper, we shall not use the Neumann boundary measurement thus we need to avoid the appearance of it in the solution form.
If for a bounded smooth domain D, we can introduce the jump formula for layer potentials. For the single layer potential we have on ∂D
∂∂νSD[φ]|±(x,t)=∓12φ(x,t)+K∗D[φ](x,t), | (2.7) |
where the ± signs mean the limits are taken from outside the domain D and inside the domain D, respectively. The integral operator K∗D is the adjoint operator of KD, which is defined by
KD[ψ](x,t)=p.v.∫t0∫∂D∂∂νyΓ(x−y,t−s)ψ(y,s)dσyds, | (2.8) |
where p.v. means the Cauchy principle value of the integral. For the jump formula of double layer potential we have
DD[ψ]|±(x,t)=±12ψ(x,t)+KD[ψ](x,t). | (2.9) |
By taking the trace of the solution u(x,t) and using the jump formulas there holds
SD[g](x,t)=VkD[μ0](x,t)−(I2+KD)[f(⋅,s/k)](x,kt) |
for x∈∂D, where g:=k∂u/∂ν. The above integral equation can be used to solve the Neumann boundary condition g. The equation is a Volterra integral equation of the first kind with kernel Γk(x,t) and uniqueness of solution has been proved in [30].
However, for a unbounded domain D the jump formula for the layer potentials may fail. Besides, it is also not easy and stable to solve the Volterra integral equation of the first kind. In what follows, we seek for the Green function to solve (2.1) without getting involved with the Neumann boundary condition. Denote by G(x,t) the Green function which satisfies
{Gt=ΔG(x,t)∈D×R+G(x,0)=δ0x∈DG(x,t)=0.(x,t)∈∂D×R+. | (2.10) |
With the help of Green's function, solution to heat equation can be written by integral formulation.
Theorem 2.2. Let x∈D=R×R+ then the solution u(x,t) to (2.1) has the form
u(x,t)=∫DG(x−y,kt)μ0(y)dy−∫t0∫∂Dk∂∂νyG(x−y,k(t−s))f(y,s)dσyds. |
The solution form by using Green function method gives us a direct way to compute the solution of (2.1). However, to compute the solution we need first compute the Green's function (2.10), which does not have an explicit form in most cases. However for D=R×R+ we can find the Green function by using the reflection method. We have the following theorem
Theorem 2.3. The solution to (2.1) can be represented by
u(x1,x2,t)=∫∞−∞14kπte−(x1−y1)24kt∫∞0(e−(x2−y2)24kt−e−(x2+y2)24kt)μ0(y1,y2)dy2dy1−y∫t014kπ(t−s)2e−x224k(t−s)∫∞−∞e−(x1−y1)24k(t−s)f(y1,s)dy1ds |
The proofs of Theorem 2.2 and 2.3 can be found in Appendix. We have shown the solution to the forward problem (2.1) with nonhomogeneous boundary condition. The solution is an integral form associated with the Green function. We shall use this solution form to reconstruct the initial temperature distribution from final overdetermination.
The inverse problem we consider in this paper is the reconstruction of the initial temperature distribution μ0(x) and generally the solution u(x,t) from the following problem
{ut=kΔu(x,t)∈R×R+×(0,T),u(x,T)=μT(x)x∈R×R+,u(x1,0,t)=f(x1,t)(x1,t)∈R×(0,T). | (3.1) |
We suppose f(x1,t)∈L2(R×(0,T)) and μT(x)∈L2(R×R+). For convenience to use the Fourier transform we also suppose those functions are in L1 for any fixed time t. Define ‖⋅‖ as the L2 norm with respect to x in R×R+. Denote by GD the operator on L2(R×R+)
GD[μ](x):=∫DG(x,y,kT)μ(y)dy | (3.2) |
where
G(x,y,kT)=14kπTe−(x1−y1)24kT(e−(x2−y2)24kT−e−(x2+y2)24kT.) |
By setting t=T in the solution form in Theorem 2.3 we get
GD[μ0](x)=h(x),x∈R×R+ | (3.3) |
where
h(x)=μT(x)+y∫T014kπ(T−s)2e−x224k(T−s)∫∞−∞e−(x1−y1)24k(T−s)f(y1,s)dy1ds. | (3.4) |
The inverse problem here is to solve the integral equation (3.3) to get the initial temperature distribution μ0(x). We see that GD is an integral operator with the kernel G(x,kT). The following properties on the operator GD is straight forward
Lemma 3.1. The operator GD in (3.3) is a self-adjoint and bounded operator on L2(R×R+).
Proof. Since the kernel of the operator GD is symmetric we immediately get that GD is self-adjoint on L2(R×R+). We shall show the bound of GD on L2(R×R+). Define
μ(x1,x2)={μ0(x1,x2)y>0−μ0(x1,−x2)y<0. |
Then there holds
GD[μ0](x)=14kπT∫R2e−|x−y|24kTμ(y)dy |
where x=(x1,x2). It is easy to see that the right hand side above is a convolution of functions 14kπTe−|x|24kT and μ(x). Thus by Young's inequality we have
‖GD[μ0]‖≤‖14kπTe−|x|24kT‖L1(R2)‖μ‖L2(R2)=2‖μ0‖ |
which completes the proof.
We shall explore a method to solve (3.3). To proceed, we present some preliminary results
Lemma 3.2. There holds the following identities
1√4kπt∫∞−∞y2ne−y24ktdy={1n=0(kt)n(2n)!n!n=1,2,… | (3.5) |
and
1√4kπt∫∞−∞cos(yη)e−y24ktdy=e−η2kt. | (3.6) |
Proof. For n=0 the result is obvious. We assume n≥1. Define
In:=1√4kπt∫∞−∞y2ne−y24ktdy |
then by integral by parts we have
In=121√4kπt∫∞−∞y2n−1e−y24ktdy2=2kt(2n−1)In−1 |
and thus by recursion we obtain
In=(2kt)nn∏j=1(2j−1)I0=(kt)n(2n)!n!. |
Next by Taylor expansion of cos(mπy) we have
∫∞−∞cos(yη)1√4kπte−y24ktdy=∫∞−∞∞∑n=0(−1)n(yη)2n(2n)!1√4kπte−y24ktdy=∞∑n=0(−1)nη2n(2n)!∫∞−∞y2n1√4kπte−y24ktdy=∞∑n=0(−1)nη2n(2n)!(kt)n(2n)!n!=e−η2kt |
which completes the proof.
Lemma 3.3. There holds the following identity
1√4kπt∫∞−∞eiyηe−(x−y)24ktdy=e−η2kteixη | (3.7) |
where i is the imaginary unit.
Proof. By using (3.6) and some elementary calculations we have
1√4kπt∫∞−∞eiyηe−(x−y)24ktdy=1√4kπt∫∞−∞ei(x+y)ηe−y24ktdy=1√4kπt∫∞−∞[cos((x+y)η)+isin((x+y)η)]e−y24ktdy=cos(xη)1√4kπt∫∞−∞cos(yη)e−y24ktdy+isin(xη)1√4kπt∫∞−∞cos(yη)e−y24ktdy=(cos(xη)+isin(xη))e−η2π2kt=eixηe−η2kt. |
With (3.7) on hand, we can get the following result
Theorem 3.1. There holds the following relation
GD[eix0ξsin(y0η)](x,y)=e−(ξ2+η2)kTeixξsin(yη). | (3.8) |
Proof. By using the definition of GD in (3.2) we have
GD[eix0ξsin(y0η)](x,y)=14kπT∫∞−∞e−(x−x0)24kTeix0ξdx0∫∞0(e−(y−y0)24kT−e−(y+y0)24kT)sin(y0η)dy0. |
By using change of variables we have
∫∞0(e−(y−y0)24kT−e−(y+y0)24kT)sin(y0η)dy0=∫∞−∞e−(y−y0)24kTsin(y0η)dy0 |
thus by using (3.7) we finally get
GD[eix0ξsin(y0η)](x,y)=e−ξ2kTeixξe−η2kTsin(yη) |
which completes the proof.
The relation (3.8) inspires us that we can actually use the Fourier transform to solve (3.3). To do this, we shall actually extend the functions μ0(x) and h(x) to R2 by setting
μ0(x1,x2)=−μ0(x1,−x2)h(x1,x2)=−h(x1,−x2)x2<0. |
Under this kind of extension we have
GD[μ0](x)=14kπT∫R2e−(x1−y1)2+(x2−y2)24kTμ0(y1,y2)dy1dy2. | (3.9) |
and
GD[μ0](x)=h(x),x∈R2. | (3.10) |
Define the Fourier transform operator F by
ˆμ(ξ)=F{μ}(ξ)=12π∫R2μ(x)e−ix⋅ξdx | (3.11) |
and the corresponding inverse Fourier transform F−1 by
μ(x)=F−1{ˆμ}(x)=12π∫R2ˆμ(ξ)eix⋅ξdξ | (3.12) |
where ξ=(ξ,η). Then by taking the Fourier transform on both sides of (3.10) and using (3.7) we obtain
F{h}(ξ)=F{GD[μ0]}(ξ)=e−kT|ξ|2ˆμ0(ξ). |
Thus we have
ˆμ0(ξ)=ekT|ξ|2ˆh(ξ) | (3.13) |
and so
μ0(x)=12π∫R2ekT|ξ|2ˆh(ξ)eix⋅ξdξ. |
We mention that to get ˆμ0(ξ) directly from (3.13) is quite unstable especially when the data h(x) is not exactly given. We shall use the iteration schemes to solve this kind of problem when the final over determination μT(x) and the boundary measurement f(x,t) are not exactly given. For the sake of simplicity we denote by hϵ(x) the perturbation of the function h(x) in (3.3) and satisfies
‖hϵ−h‖≤ϵ,ϵ>0 | (3.14) |
where ϵ is a small number which can be treated as the noise level of the measurement. Similar to [13,14], we introduce the following iteration scheme to solve (3.13)
ˆμϵj(ξ)=(1−n√v(ξ))ˆμϵj−1(ξ)+n√v(ξ)v(ξ)χςˆhϵ(ξ), | (3.15) |
where
v(ξ)=e−kT|ξ|2 |
and χς is the characteristic function of ς={ξ| k|ξ|2≤ρ}, that is
χς={1k|ξ|2≤ρ0k|ξ|2>ρ. |
The parameter ρ here is a selective positive number which can be chosen in a flexible way depending on the stopping rule that is used for terminating the iteration scheme. The parameter n is a selective nature number which is used to control the iteration speed. Generally speaking, the lager n is the less iteration steps are required to get an approximate solution. The iterative steps actually decrease exponentially with the parameter n increase normally. However, the error estimation for the solution behaviors badly as n increases as well.
The iteration scheme (3.15) requires us to get the Fourier transform of the perturbation hϵ(x). In fact, the perturbation comes from the noise of the final observation μT and the boundary condition f in (3.4). In this section we consider the Fourier transform of h. To extend h to R2 we only need to extend the final observation μT(x) by
μT(x1,x2)=−μT(x1,−x2),x2<0. |
We observe that (3.4) can be written as follows
h(x)=μT(x)−2k∫T01√4kπ(T−s)∂∂ye−x224k(T−s)∫∞−∞1√4kπ(T−s)e−(x1−y1)24k(T−s)f(y1,s)dy1ds. | (4.1) |
Taking the Fourier transform on both sides of (4.1) and using (3.7) we get
ˆh(ξ)=ˆμT(ξ)−2ikη√2π∫T0e−k|ξ|2(T−s)ˆf(ξ,s)ds | (4.2) |
where by ˆf(ξ,s) we mean the one dimensional Fourier transform of f(x1,s) on x1, i.e.,
ˆf(ξ,s)=1√2π∫∞−∞f(x1,s)e−iξx1dx1 |
and so the inverse one dimensional Fourier transform is
f(x1,s)=1√2π∫∞−∞ˆf(ξ,s)eiξx1dξ. |
In this section, we consider the convergence results of iteration scheme (3.15) by using both the a priori and the a posteriori stopping rules. Before presenting the error estimate of the initial temperature distribution μ0(x), we suppose the a priori bound on μ0(x)
‖μ0‖p≤M, p≥0 | (5.1) |
where
‖μ0‖p:=(∫R2(1+|ξ|2)p|ˆμ0(ξ)|2dξ)12. |
We see that if p=0 then the norm ‖⋅‖p turns to L2 norm.
By using the prior information (5.1) we can design the following stopping rule
j∼⌊(M/ϵ)1/n⌋ | (5.2) |
where ⌊a⌋ denotes the largest integer that is not greater than a. We note that in the stopping rule (5.2), if n increases then the iteration steps j are greatly reduced.
Theorem 5.1. Let μ0(x) be the initial temperature distribution in (3.1).Suppose μϵT(x) is the measured temperature at t=T and fϵ(x1,t) is themeasured boundary condition. Suppose the corresponding function hϵ(x) by (3.4) satisfies(3.14). Let μϵj(x) be the iterates defined by (3.15) withinitial iterate μϵ0(x)=0.If (5.1) is satisfied for M>0, p>0 and we select j∼⌊(M/ϵ)1/n⌋ as the prior stopping rule and
ρ=1Tln(Mδ(lnMδ)−p2) |
then we have the following error estimate
‖μϵj−μ0‖2≤2M2(lnMδ)−p(1+Cn2n+2kpTp(lnMδlnMδ+ln(lnMδ)−p2)p) | (5.3) |
where C is a constant depending on j and n.
Proof. Set α=n√v(ξ) then 0<α≤1. By (3.15) we obtain
ˆμϵj(ξ)=(1−α)ˆμϵj−1(ξ)+α1−nχςˆhϵ(ξ)=j−1∑i=0(1−α)iα1−nχςˆhϵ(ξ). |
Take pj(α)=j−1∑i=0(1−α)i, rj(α)=1−αpj(α)=(1−α)j, we have the following elementary results (cf.[33]):
pj(λ)λm≤j1−m,for all 0≤m≤1, | (5.4) |
rj(λ)λq≤θq(j+1)−q, | (5.5) |
where
θq={10≤q≤1qqq>1. |
From (3.13) we have
ˆμ0(ξ)=α−nˆh(ξ) |
then there holds the estimates
‖ˆμϵj−ˆμ0‖2=‖pj(α)α1−nχςˆhϵ−ˆμ0‖2=‖pj(α)α1−n(χςˆhϵ−ˆh)−rj(α)ˆμ0‖2≤2‖pj(α)α1−n(χςˆhϵ−ˆh)‖2+2‖rj(α)ˆμ0‖2:=2I1+2I2. |
Next we derive the estimates for I1 and I2, respectively.
I1=‖pj(α)α1−n(χςˆhϵ−ˆh)‖2=∫ς|pj(α)α1−n(χςˆhϵ(ξ)−ˆh(ξ))|2dξ+∫R2∖ς|pj(α)α1−n(χςˆhϵ(ξ)−ˆh(ξ))|2dξ≤∫ς|α−n(ˆhϵ(ξ)−ˆh(ξ))|2dξ+∫R2∖ς(1+|ξ|2)−p(1+|ξ|2)p|ˆμ0(ξ)|2dξ. |
By using the definition of ς and the choice of ρ we thus have
I1≤e2ρTϵ2+σpρ−pM2≤(Mϵ)2(lnMϵ)−pϵ2+kpTp(ln(Mϵ(lnMϵ)−p2))−pM2≤M2(lnMϵ)−p(1+kpTp(lnMϵlnMϵ+ln(lnMϵ)−p2)p). |
With similar strategy and (5.2) we estimate I2
I2=‖rj(α)ˆμ0‖2=∫ς|rj(α)ˆμ0(ξ)|2dξ+∫R2∖ς|rj(α)ˆμ0(ξ)|2dξ=∫ς|rk(α)αnv(ξ,t)v(ξ,T)ˆφ1(ξ)|2dξ+∫R2∖ς(1+|ξ|2)−p(1+|ξ|2)p|rj(α)ˆμ0(ξ)|2dξ≤n2n(j+1)−2ne2ρTM2+kpρ−pM2≤Cn2n(Mϵ)2(lnMϵ)−pϵ2+kpTp(ln(Mϵ(lnMϵ)−p2))−pM2≤M2(lnMϵ)−p(Cn2n+kpTp(lnMϵlnMϵ+ln(lnMϵ)−p2)p), |
where (5.5) and the choice of ρ are taken into account and the selection of constant C is only dependent on j and n. We come to the conclusion by combining the estimates of I1 and I2 and using Parseval equality.
The prior stopping rule needs the a priori bound of μ0 to stop the iteration process. However if such bound can not be obtained accurately, the iteration may not stop at a "good time" and thus the result may not be satisfactory. Thus an a posteriori stopping rule is required. We introduce the widely-used "discrepancy principle" due to Morozov [34]. We set the discrepancy principle in the following form
‖ˆhϵ−vˆμϵj∗‖≤τϵ<‖ˆhϵ−vˆμϵj‖,0<j<j∗ | (5.6) |
where k∗ is the first iteration step which satisfies the left inequality of (5.6).
Theorem 5.2. Let μ0(x) be the initial temperature distribution in (3.1).Suppose μϵT(x) is the measured temperature at t=T and fϵ(x,t) is themeasured boundary condition. Suppose the corresponding function hϵ(x) by (3.4) satisfies(3.14). Let μϵj(x) be the iterates defined by (3.15) withinitial iterate μϵ0(x)=0.If (5.1) is satisfied for M>0, p>0 and we select the discrepancy principle (5.6) as the stopping rule and
ρ=1Tln(Mδ(lnMδ)−p2) |
then we have the following error estimate
‖μϵj−μ0‖2≤2M2(lnMδ)−p(1+Cn2n+2kpTp(lnMδlnMδ+ln(lnMδ)−p2)p) | (5.7) |
where C is a constant depending on j and n.
Proof. It sufficient to prove j∗∼(M/ϵ)1/n by Theorem 5.1. We have
‖χςˆhϵ−vˆμϵj‖=‖(1−α)(χςˆhϵ−vˆμϵj−1)‖=‖(1−α)jχςˆhϵ‖≤‖(1−α)j(ˆhϵ−ˆh)‖+‖(1−α)jˆh‖≤ϵ+‖rj(α)αnˆμ0‖≤ϵ+nnj−nM, |
furthermore
‖(1−χς)ˆhϵ‖≤‖(1−χς)(ˆhϵ−ˆh)‖+‖(1−χς)ˆh‖≤ϵ+(∫R2∖ς|v(ξ)ˆμ0(ξ)|2dξ)1/2≤ϵ+e−ρTM≤2ϵ |
thus we obtain
‖ˆhϵ(⋅)−vˆμϵj(⋅,t)‖≤3ϵ+nnj−nM, |
Set τ>3 and according to (5.6) we have (τ−3)ϵ<nnj−nM and thus j∼⌊(Mϵ)1/n⌋.
We remark that although the parameter ρ appears in (3.15) requires the a priori bound on μ0, we do not care much on the choice. In fact the choice of ρ is just for technique setup. We can actually set a very large number M such that it is lager than the sharp upper bound on μ0. By using the discrepancy principle (5.6) as the stopping rule, the convergence rate and reconstruction performance are still ensured.
We have introduced the layer potential technique to get the analytic solution of the heat diffusion problem in the half plane. The Green function has been constructed to avoid the usage of the Neumann boundary condition. We have combined the Fourier transform and the Green function method to get the relation between the initial temperature distribution and the given final observation. We designed an iteration scheme to reconstruct the initial temperature distribution. Although the whole analysis is on two dimensional space heat conduction problem, it can be similar used to analyze higher dimensional problem. The method can also be used to reconstruct the initial heat distribution on any kind of domain and numerical realization of two and three dimensional inverse heat conduction problem will be a forthcoming work.
The work of X. Fang was supported by NSF grant China No. 72001077, Humanities and Social Sciences Foundation of the Ministry of Education No. 20YJC910005, NSF grant of Hunan No. 2021JJ30192. The work of Y. Deng was supported by NSF grant of China No. 11971487 and NSF grant of Hunan No. 2020JJ2038. The work of Z. Zhang was supported by Hunan Provincial Natural Science Foundation of China Grant No. 2021JJ30297 and Research and Innovation team of Hunan Institute of Science and Technology (Grant No. 2019-TD-15).
In this section, we show the main proofs to some Theorems for the sake of convenience to the reader.
Proof of Theorem 2.1 By using the Green's theorem, we have
∫t0∫∂Dk∂∂νyΓ(x−y,k(t−s))u(y,s)−Γ(x−y,k(t−s))k∂∂νyu(y,s)dσyds=∫t0∫DkΔyΓ(x−y,k(t−s))u(y,s)−Γ(x−y,k(t−s))kΔyu(y,s)dyds=∫t0∫DΓt(x−y,k(t−s))u(y,s)−Γ(x−y,k(t−s))us(y,s)dyds=∫t0∫D−Γs(x−y,k(t−s))u(y,s)−Γ(x−y,k(t−s))us(y,s)dyds=∫D−Γ(x−y,k(t−s))u(y,s)|ts=0dy=−u(x,t)+∫DΓ(x−y,kt)u(y,0)dy |
where we have changed the order of integration and used the integral by parts. Thus there holds
u(x,t)=VkD[μ0](x,t)+SkD[∂u/∂ν](x,t)−kDD[f](x,t) |
which completes the proof.
Proof of Theorem 2.2 We first show the relation between G(x,t) and Γ(x,t). If fact, let v(x,t) be the solution to
{vt=Δvin D×R+v(x,0)=0in Dv(x,t)=Γ(x,t)on ∂D×R+ |
then it is easy to see that
G(x,t)=Γ(x,t)−v(x,t). |
By using the Green's formula there holds for u(x,t) and v(x,t)
∫Dv(x−y,kt)μ0(y)dy+∫t0∫∂Dv(x−y,k(t−s))k∂∂νyu(y,s)dσyds−∫t0∫∂Dk∂∂νyv(x−y,k(t−s))u(y,s)dσyds=0 |
By subtracting the above equation from (2.6) and using the fact that
G(x,t)=0,(x,t)∈∂D×R+ |
we immediately get the conclusion.
Proof of Theorem 2.3 Let x=(x1,x2), y=(y1,y2). By using the reflection method, it is easy to find the Green function of (2.10) for D=R×R+
G(x−y,t)=14kπt(e−(x1−x2)2+(y1−y2)24kt−e−(x1−x2)2+(y1+y2)24kt) |
To use the result in Theorem 2.2, we compute
∂∂νyG(x−y,k(t−s))|∂D=−∂∂y0G(x−y,k(t−s))|y0=0=y4k2π(t−s)2e−(x1−y1)2+x224k(t−s). |
By substituting the Green function and the above formula into the solution form in Theorem 2.2 we come to the conclusion.
The authors declare there is no conflict of interest.
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