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10.1002/mma.9220

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CHRISTOV et al.

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, , ,

Nonlinear Einstein paradigm of Brownian motion and localization property of solutions

Ivan C. Christov    Isanka Garli Hevage    Akif Ibraguimov    Rahnuma Islam \orgdivSchool of Mechanical Engineering, \orgnamePurdue University, \orgaddressWest Lafayette, \stateIndiana 47907, \countryUSA \orgdivDepartment of Mathematics & Statistics, \orgnameTexas Tech University, \orgaddressLubbock, \stateTexas 79409, \countryUSA \orgdivOil and Gas Research Institute, \orgnameRussian Academy of Sciences, \orgaddressMoscow, \countryRussia [email protected] [email protected] [email protected] [email protected]    I. C. Christov    I. Garli Hevage    A. Ibraguimov    R. Islam
(2022; ; 2023)
Abstract

[Summary]We employ a generalization of Einstein’s random walk paradigm for diffusion to derive a class of multidimensional degenerate nonlinear parabolic equations in non-divergence form. Specifically, in these equations, the diffusion coefficient can depend on both the dependent variable and its gradient, and it vanishes when either one of the latter does. It is known that solutions of such degenerate equations can exhibit finite speed of propagation (so-called localization property of solutions). We give a proof of this property using a De Giorgi–Ladyzhenskaya iteration procedure for non-divergence-from equations. A mapping theorem is then established to a divergence-form version of the governing equation for the case of one spatial dimension. Numerical results via a finite-difference scheme are used to illustrate the main mathematical results for this special case. For completeness, we also provide an explicit construction of the one-dimensional self-similar solution with finite speed of propagation function, in the sense of Kompaneets–Zel’dovich–Barenblatt. We thus show how the finite speed of propagation quantitatively depends on the model’s parameters.

\jnlcitation\cname

, , , and (\cyear2023), \ctitleNonlinear Einstein paradigm of Brownian motion and localization property of solutions, \cjournalMath. Meth. Appl. Sci., doi:10.1002/mma.9220.

keywords:
Degenerate parabolic equations, Diffusion processes, Localization property of solutions, Gradient-dependent diffusivity
articletype: Research Article

1 Introduction

A number of physical processes are governed by nonlinear parabolic partial differential equations (PDEs), specifically ones in which the coefficient of the highest-order spatial derivative (identified as the diffusion coefficient in the case of a parabolic PDE) can vanish 1, 2. These degenerate parabolic equations can exhibit finite speed of propagation, i.e., initial conditions of compact support expand the length of their support in time at a finite speed (see, e.g., §1.9 of Straughan’s book 3). This property is in contrast to the case of linear parabolic equations, for which initial data “propagates” instantaneously throughout the domain, leading to the so-called paradox of heat conduction 4. More generally, compact (localized) solutions are but one example of traveling waves in nonlinear diffusion-convection-reaction equations 5.

In physics and in engineering, nonlinear degenerate diffusion equations have been derived to describe the flow and spreading of compressible fluids (gases) through porous media 6, 7. The evolution of the thickness of thin liquid films on solid surfaces 8, determined by the balance of viscous flow forces, surface tension, and van der Waals interactions, is also governed by a degenerate nonlinear parabolic equation, now of higher order 9, 10. High-temperature phenomena, such as shock waves in ionized gases, can also be described by nonlinear degenerate diffusion equations, in which the thermal diffusivity vanishes at a certain temperature 11. In these previous examples, the diffusion coefficient may only depend on (and vanish with) the dependent variable (say, gas concentration, fluid film height, or temperature). Interestingly, there are also physics and engineering problems in which the diffusivity can also vanish when the gradient of the dependent variable vanishes. One example is pre-Darcy flow in saturated porous media 12. Another example is the spreading of confined layers of non-Newtonian fluids 13, 14, for which the complex rheology of the fluid leads to a degenerating gradient-dependent diffusivity (unlike the Newtonian case 8); see also the review by Ghodgaonkar and Christov 15. Indeed, degenerate equations with gradient-dependent diffusivity are traditionally associated with problems of non-Newtonian filtration through a porous medium (see, e.g., the discussion by Kalashnikov16).

In the present work, we reconsider all of the above models, and their governing nonlinear parabolic PDEs, from the point of view of Einstein’s random walk paradigm 17, 18 for diffusion in a continuous medium. Specifically, we show how to derive a generic degenerate nonlinear parabolic equation, in non-divergence form, with the diffusivity depending on both the dependent variable and its gradient. This approach can be interpreted as a complementary conceptual derivation of the governing equation for the physical situations mentioned above, but without appealing to Fick’s (or Darcy’s or Fourier’s) law (see, e.g., Ch. 1 of the book by Cunningham 19), the continuity (conservation of mass) equation, and the thermodynamic closures that relate the various system variables (such as density, mass, and concentration) to each other.

To this end, this paper is organized as follows. In Section 2, we introduce the Einstein random-walk paradigm and its generalization used for the present derivations. In Section 3, we prove a maximum principle for the solution of the multidimensional nonlinear parabolic equation derived, taking into account its degeneracy with respect to the dependent variable and its gradient. To accomplish this task, we regularize the degeneracy of the PDE, proving the maximum principle for a smooth viscosity solution, then we take the limit. Next, in Section 4, we strengthen our result by proving the localization property of solutions using a De Giorgi–Ladyzhenskaya iteration procedure, without the need for explicitly constructing a barrier function. Again, we work with the regularized problem and in terms of the viscosity solution, for convenience, but the final estimate is independent of the (small) regularization parameter. In Section 5, for the case of one spatial dimension, we develop transition formulas to map the non-divergence form of the PDE (discussed in earlier sections) to the more traditional divergence-form case. Beyond showing a fundamental equivalence of the two forms of the PDE, the latter is more convenient for numerical simulation, since we have previously developed and validated a finite-difference scheme for divergence-form nonlinear degenerate PDEs 15. Then, in Section 6 again for the special case of one spatial dimension, we construct explicit self-similar solutions with finite speed of propagation and perform simulations of the divergence-form degenerate PDE to illustrate and verify our main mathematical result from Section 4. Finally, Section 7 discusses the broader context of our results and avenues for future work.

2 Einstein paradigm for diffusion

2.1 Setup and preliminaries

In the celebrated work of Einstein 17, Brownian motion was explained using a mathematical model based on a thought experiment. Since then, the stochastic interpretation of this approach has been applied to many transport processes arising in physics, chemistry, and engineering (see, e.g., §1.2.1 of Gardiner’s book 20).

To formulate the PDE model (following our earlier work 21), consider a collection of “particles,” which here stands for any discrete physical object and some physics governing its motion with respect to nearby particles. The particles may be actual particles, or molecules, or physical agents or even animals 22, depending on the physical process under consideration. The modeling approach under the Einstein paradigm is generic.

To begin, first we require that there exists a time interval τ\tau such that (s.t.), during two consecutive intervals τ\tau, the motions performed by individual particles in the system are mutually independent (uncorrelated) events. The interval τ\tau is “sufficiently small” compared to the time scale tt of observation of the physical process, but not so small that the motions become correlated.

Now, we will extend the traditional one-dimensional Einstein model of Brownian motion to the dd-dimensional real Euclidean space d\mathbb{R}^{d}. Let xdx\in\mathbb{R}^{d} and u(x,t):d×[0,)u(x,t):\mathbb{R}^{d}\times[0,\infty)\to\mathbb{R}. We assume that the number of particles per unit volume at point xx at time tt can be represented by (i.e., it is proportional to) the concentration, which is the scalar function u(x,t)u(x,t). {assumption} We assume the following extension of the axioms formulated by Einstein 17, 18:

  1. 1.

    Consider a particle (PP) of particular type moving through the medium of interest. Let (τ)\mathbb{P}(\tau) be the set of vectors with non-colliding jumps of PP during the time interval τ\tau. We call Δ=(Δ1,,Δd)\vec{\Delta}=\big{(}\Delta_{1},\ldots,\Delta_{d}\big{)}^{\top} the “vector of free jumps of particle PP” if Δ(τ)\vec{\Delta}\in\mathbb{P}(\tau).

  2. 2.

    The interactions of particles during the time interval τ\tau can occur via absorption (or reaction) through the surrounding medium, via collisions with other particles, and possibly via the spatial domain’s boundaries. In general, this key quantity τ\tau can depend on the concentration of particles uu, its gradient u\nabla u, and possibly also xx and tt.

  3. 3.

    The time interval of free jumps τ\tau, the vector of expected free jump lengths Δe\vec{\Delta}^{e}, and the scalar probability density function φ(Δ)\varphi(\vec{\Delta}) of free jumps Δ\vec{\Delta} are the quantities that characterize the generalized Brownian process under the Einstein paradigm. Here, the free jumps in each coordinate direction are denoted Δi\Delta_{i} for i=1,2,,di=1,2,\ldots,d.

  4. 4.

    During the time interval [t,t+τ][t,t+\tau] in the unit volume around the particle PP located at the observation point xx, it is possible absorption and/or reaction with other particles (or with the suspending medium) occurs. This effect is represented by the integral

    tt+τ𝒜(u(x,s),s)𝑑s,\int_{t}^{t+\tau}\mathcal{A}\big{(}u(x,s),s\big{)}\,ds, (1)

    where 𝒜(u,t)\mathcal{A}(u,t) is a potentially nonlinear function that can be positive or negative, depending on the physics considered.

Axiom 1 (Whole universe axiom).
(τ)φ(Δ)𝑑Δ=1,\int_{\mathbb{P}(\tau)}\varphi(\vec{\Delta})\,d\vec{\Delta}=1, (2)

where dΔ\triangleqdΔ1dΔ2dΔdd\vec{\Delta}\triangleq d\Delta_{1}d\Delta_{2}\cdots d\Delta_{d}.

Note that, in a view of the definition of the set (τ)\mathbb{P}(\tau), if Δ(τ)\vec{\Delta}\notin\mathbb{P}(\tau), then φ(Δ)=0\varphi(\vec{\Delta})=0.

Let us define the vector of expected free jumps:

Δe\triangleq(Δ1e,Δ2e,,Δde),whereΔie\triangleq(τ)Δiφ(Δ)𝑑Δ,\vec{\Delta}^{e}\triangleq(\Delta^{e}_{1},\Delta^{e}_{2},\ldots,\Delta^{e}_{d})^{\top},\quad\text{where}\quad\Delta^{e}_{i}\triangleq\int_{\mathbb{P}(\tau)}{\Delta_{i}}\varphi(\vec{\Delta})\,d\vec{\Delta}, (3)

and the matrix of standard (co-)variances of free jumps:

σij2\triangleq(τ)(ΔiΔie)(ΔjΔje)φ(Δ)𝑑Δ.\sigma_{ij}^{2}\triangleq\int_{\mathbb{P}(\tau)}\left({\Delta_{i}}-{\Delta}^{e}_{i}\right)\left({\Delta_{j}}-{\Delta}^{e}_{j}\right)\varphi(\vec{\Delta})\,d\vec{\Delta}. (4)

Evidently Δe(x,t)\vec{\Delta}_{e}(x,t) and σij(x,t)\sigma_{ij}(x,t) depend on space xx and time tt. Next, considering Section 2.1 and the above, we state the generalized Einstein paradigm axiom for the number of particles found at time t+τt+\tau in an infinitesimal control volume dvddv\subset\mathbb{R}^{d} containing the point xx:

Axiom 2 (Einstein conservation law).
u(x,t+τ)dv=((τ)u(x+Δ,t)φ(Δ)𝑑Δfree jumps+tt+τ𝒜(u(x,s),s)𝑑sabsorption/reaction)dv.u(x,t+\tau)\cdot dv=\Bigg{(}\,\underbrace{\int_{\mathbb{P}(\tau)}u\big{(}x+\vec{\Delta},t\big{)}\varphi(\vec{\Delta})\,d\vec{\Delta}}_{\text{free jumps}}+\underbrace{\int_{t}^{t+\tau}\mathcal{A}\big{(}u(x,s),s\big{)}\,ds}_{\text{absorption/reaction}}\Bigg{)}\cdot dv. (5)

The Einstein conservation law (Axiom 2) is illustrated schematically in Fig. 1.

Refer to caption
Figure 1: Schematic illustrating the notation and jump process, from tt to t+τt+\tau, for the proposed generalized Einstein random walk paradigm for x=(x1,x2)2x=(x_{1},x_{2})\in\mathbb{R}^{2}.

Assuming that u(x,t)𝒞x,t2,1u(x,t)\in\mathcal{C}^{2,1}_{x,t} (i.e., uu is twice continuously differentiable in xx and once in tt) and using the multidimensional analog of the Caratheodory Theorem 23 and arguments from our previous work 21, Einstein’s conservation equation (5) can be reduced to a generic advection-reaction-diffusion equation:

Lu=τut+Δeudrift/advectioni,j=1dai,j2uxixjdiffusion+τ𝒜(u(x,t),t)absorption/reaction=0.Lu=\tau\frac{\partial u}{\partial t}+\underbrace{\vec{\Delta}^{e}\cdot\nabla u}_{\text{drift/advection}}-\underbrace{\sum_{i,j=1}^{d}a_{i,j}\frac{\partial^{2}u}{\partial x_{i}\partial x_{j}}}_{\text{diffusion}}+\underbrace{\tau\mathcal{A}\big{(}u(x,t),t\big{)}}_{\text{absorption/reaction}}=0. (6)
Remark 2.1.

Equation 6 is applicable in the general case of an anisotropic medium with vector Δe(x,t)\vec{\Delta}^{e}(x,t) of expected values of free jumps in the dd spatial directions, and symmetric matrix (ai,j)\left(a_{i,j}\right) of coefficients

ai,j\triangleq{12σi,i2,ifi=j,σi,j2,ifij,a_{i,j}\triangleq\begin{cases}\frac{1}{2}\sigma_{i,i}^{2},&\quad\text{if}\quad i=j,\\ \sigma_{i,j}^{2},&\quad\text{if}\quad i\neq j,\end{cases} (7)

which are defined in terms of the corresponding (co-)variances σi,j\sigma_{i,j} of the free jump distribution φ\varphi, given in Eq. 4.

2.2 Nonlinear PDE under the Einstein paradigm

For the remainder of this paper, we assume there is no absorption or reaction (meaning no creation or annihilation of particles), so 𝒜(u)0\mathcal{A}(u)\equiv 0. Next, we specialize the model to a dd-dimensional domain in d\mathbb{R}^{d} under the assumption that the medium in which the diffusion process occurs is homogeneous and isotropic. By the homogeneity assumption, the frequency distribution φ\varphi is a scalar function of the vector Δe\vec{\Delta}^{e}, and the vector of expected values is simply Δe=(Δe,,Δe)\vec{\Delta}^{e}=(\Delta^{e},\ldots,\Delta^{e}). In other words, the expected values of jumps in the random walk are the same in all coordinate directions, and equal to the same given constant value Δe\Delta^{e}. It follows that ai,j=σ22δi,ja_{i,j}=\tfrac{\sigma^{2}}{2}\delta_{i,j}, where σ2\sigma^{2} is the now-constant variance of the jump distribution, and δi,j\delta_{i,j} is the Kronecker-δ\delta symbol.

Now, we further motivate how the model equation, derived in Section 2.1 under the generalized Einstein paradigm, can be used to obtain a nonlinear parabolic diffusion equation, in non-divergence form, for a Brownian-like process.

{assumption}

[Time interval in nonlinear Einstein paradigm] Under the Einstein paradigm, τ\tau, Δe\Delta^{e}, and φ\varphi characterize the Brownian process. In general, they could be functions of both the spatial and time variables, xx and tt, and properties of the medium. But, more importantly, they can be functions of the dependent variable, such as the concentration of particles u0u\geq 0 and its derivatives, via a power-law relation (Remarks 2.3 and 2.4 motivate this functional form):

τ=τ0uγ|u|β,\tau=\frac{\tau_{0}}{u^{\gamma}|\nabla u|^{\beta}}, (8)

where τ0>0\tau_{0}>0 is a suitable dimensional consistency constant, and γ,β\gamma,\beta\in\mathbb{R} do not have to be integers (though their ranges will be further restricted below for the proofs). Here, the earlier assumption of a homogeneous isotropic medium rules out an explicit dependence of τ\tau on xx or tt.

Remark 2.2 (Classical Einstein paradigm).

Observe that τ0\tau_{0} (i.e., τ\tau for γ=β=0\gamma=\beta=0) in Section 2.2 coincides with the time interval between jumps in the special case of Einstein’s classical derivation 17, 18.

Remark 2.3 (uu dependence of τ\tau).

In ionized gases, the mean free path (between collisions) of molecules is directly proportional to a non-integer power of the temperature (see, e.g., Ch. X§2 of the book by Zel?dovich and Raizer 11), with the power depending on the level of ionization. Therefore, kinematics implies that the time interval between collisions is also proportional to the temperature (because the “agitation” and kinetic energy of molecules increases with temperature). Translated to the context of concentration and particles: the length of free jumps, and therefore the time during which the free jumps occur, must be inversely proportional to some power of the concentration. That is, the more particles there are nearby, the more likely they are to collide, thus reducing the time interval during which the free jumps occur (i.e., the time interval during which the motion is uncorrelated). This physical situation is a special case of Section 2.2 (β=0\beta=0).

Remark 2.4 (u\nabla u dependence of τ\tau).

Similar arguments can also be made for the case of β0\beta\neq 0 to justify that the time interval between collisions can also depend upon some (possibly non-integer) power of the gradient’s magnitude |u||\nabla u|. For example, Kruckels 24 argued that if a particle has more neighbors on one “side” (versus another), then a gradient effect arises because the preferentially large number of particles on one side will make it more likely for a collision to occur. In turn, this again reduces the time interval during which the free jumps occur, along the lines of Remark 2.3. The power-law form of this gradient dependence has been further motivated by appealing to Eyring’s theory of rate processes 24, 19.

Under the above assumptions, on a general domain UdU\subset\mathbb{R}^{d}, Eq. 6 becomes

Lu=τ0ut+uγ|u|βΔei=1duxiσ22uγ|u|βΔu=0inU×(0,T],UdLu=\tau_{0}\frac{\partial u}{\partial t}+u^{\gamma}|\nabla u|^{\beta}\Delta^{e}\sum_{i=1}^{d}\frac{\partial u}{\partial x_{i}}-\frac{\sigma^{2}}{2}u^{\gamma}|\nabla u|^{\beta}\Delta u=0\quad\text{in}\;\;U\times(0,T],\;\;U\subset\mathbb{R}^{d} (9)

subject to an initial and boundary condition:

u(x,t)=h(x,t)0 on Γ(UT).u(x,t)=h(x,t)\geq 0\quad\text{ on }\ \Gamma(U_{T}).\ (10)

Above, Γ(UT)\Gamma(U_{T}) is the parabolic boundary of UT=U×(0,T]U_{T}=U\times(0,T].

Equation 9 is sometimes called a doubly nonlinear parabolic equation because it degenerates when u=0u=0 and/or |u|=0|\nabla u|=0.

3 Maximum principle on a bounded domain

In this section, we prove a maximum principle for the solutions of Eq. 9, following 25, 26, 21. In addition to d\mathbb{R}^{d} as above, we also consider the (d+1)(d+1)-dimensional space d+1\mathbb{R}^{d+1}, in which the spatial coordinates are augmented by time: d+1(x,t)=(x1,x2,,xd,t)\mathbb{R}^{d+1}\ni(x,t)=(x_{1},x_{2},\ldots,x_{d},t). Again, let UdU\subset\mathbb{R}^{d} be bounded, and t>0t>0. We define the cylindrical region UT\triangleqU×(0,T]d+1U_{T}\triangleq U\times(0,T]\subset\mathbb{R}^{d+1}, its parabolic boundary Γ(UT)\triangleq(U×{t=0})(U×(0,T])\Gamma(U_{T})\triangleq(U\times\{t=0\})\cup(\partial U\times(0,T]), and the layer Hd+1(0,T]H\subset\mathbb{R}^{d+1}\cap(0,T].

As above, 𝒞x,t2,1(UT)\mathcal{C}^{2,1}_{x,t}(U_{T}) denotes the class of continuous functions on UT¯\overline{U_{T}} that have two continuous derivatives in xx and one continuous derivative in tt inside the domain UTU_{T}.

Remark 3.1.

Note that Eq. 9 degenerates when u=0u=0 or |u|=0|\nabla u|=0, therefore its solution u(x,t)u(x,t) does not belong to 𝒞x,t2,1(UT)\mathcal{C}^{2,1}_{x,t}(U_{T}), strictly speaking. To prove our result, we introduce a “viscous” regularization. Specifically, we regularize the operator LL as LϵL_{\epsilon} via

Lϵuϵ=τ0uϵt+(uϵ+ϵ)γ(|uϵ|β+ϵ)Δei=1duϵxiσ22(uϵ+ϵ)γ(|uϵ|β+ϵ)Δuϵ=0inU×(0,T],Ud.L_{\epsilon}u_{\epsilon}=\tau_{0}\frac{\partial u_{\epsilon}}{\partial t}+(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\Delta^{e}\sum_{i=1}^{d}\frac{\partial u_{\epsilon}}{\partial x_{i}}-\frac{\sigma^{2}}{2}(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\Delta u_{\epsilon}=0\;\;\text{in}\;\;U\times(0,T],\;\;U\subset\mathbb{R}^{d}. (11)

In all major estimates for the solution of the initial-boundary-value problem (IBVP) for Lϵuϵ=0L_{\epsilon}u_{\epsilon}=0 in this article, the constants do not depend on ϵ\epsilon. All dependence on the regularization parameter ϵ\epsilon appears as separate terms in the respective estimates, and they do not depend on the solution uϵu_{\epsilon} or its derivatives. This observation allows us to pass to the limit in the final estimates, and conclude the localization property for the limiting function:

u(x,t)=limϵ0uϵ(x,t),u(x,t)=\lim_{\epsilon\to 0}u_{\epsilon}(x,t), (12)

which is considered as a weak passage to the limit 27. Thus, we define the weak viscosity solution from Eq. 12 as a partial limit with respect to the norm that will be induced by Eq. 31 in Section 4. This solution may not be unique, and we will assume a priori, in Section 4, that the limiting function u(x,t)u(x,t) has certain properties.

Next, in this section, we prove a maximum principle, which evidently will not depend on the parameter ϵ\epsilon, therefore the limiting function is bounded. In this article, we assume that this limit exists. Then, the obtained localization property will extend from the estimates on uϵu_{\epsilon} to the weak solution uu.

Lemma 3.2 (Weak maximum principle).

For a given function uϵ𝒞x,t2,1u_{\epsilon}\in\mathcal{C}^{2,1}_{x,t}, if Lϵuϵ>0L_{\epsilon}u_{\epsilon}>0 in UTU_{T}, then uϵminΓ(UT)uϵu_{\epsilon}\geq\min_{\Gamma(U_{T})}u_{\epsilon} in UTU_{T}.

Proof 3.3.

Let us suppose there is a point (x0,t0)UT(x_{0},t_{0})\in U_{T} s.t. minUT¯uϵ=uϵ(x0,t0)<minΓ(UT)u\min_{\overline{U_{T}}}u_{\epsilon}=u_{\epsilon}(x_{0},t_{0})<\min_{\Gamma(U_{T})}u, then the minimum of uϵ(x,t)u_{\epsilon}(x,t) attained at (x0,t0)UT(x_{0},t_{0})\in U_{T}, for x0Ux_{0}\in U and t0Tt_{0}\leq T. Therefore, at the point (x0,t0)(x_{0},t_{0}), uϵ=0\nabla u_{\epsilon}=0, uϵt0\frac{\partial u_{\epsilon}}{\partial t}\leq 0 and Δuϵ0\Delta u_{\epsilon}\geq 0.

Consequently, Lϵuϵ0L_{\epsilon}u_{\epsilon}\leq 0 at the point (x0,t0)(x_{0},t_{0}), which is a contradiction.

Theorem 3.4 (Strong maximum principle).

For a given function uϵ𝒞x,t2,1u_{\epsilon}\in\mathcal{C}^{2,1}_{x,t}, if Lϵuϵ0L_{\epsilon}u_{\epsilon}\geq 0 in UTU_{T}, then uϵminΓ(UT)uϵu_{\epsilon}\geq\min_{\Gamma(U_{T})}u_{\epsilon} in UTU_{T}.

Proof 3.5.

Consider the function w(x,t)=Kt+uϵ(x,t)w(x,t)=Kt+u_{\epsilon}(x,t) for (x,t)UT(x,t)\in U_{T} and t<Tt<T, K>0K>0. Then for given uϵu_{\epsilon},

L~ϵw\triangleqτ0wt+(uϵ+ϵ)γ(|uϵ|β+ϵ)Δewσ22(uϵ+ϵ)γ(|uϵ|β+ϵ)Δw=Kτ0+τ0uϵt+(uϵ+ϵ)γ(|uϵ|β+ϵ)Δeuϵσ22(uϵ+ϵ)γ(|uϵ|β+ϵ)Δuϵ=Kτ0+Lϵuϵ>0.\begin{split}\tilde{L}_{\epsilon}&w\triangleq\tau_{0}\frac{\partial w}{\partial t}+(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\vec{\Delta}^{e}\cdot\nabla w-\frac{\sigma^{2}}{2}\cdot(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\Delta w\\ &=K\tau_{0}+\tau_{0}\frac{\partial u_{\epsilon}}{\partial t}+(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\vec{\Delta}^{e}\cdot\nabla u_{\epsilon}-\frac{\sigma^{2}}{2}\cdot(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\Delta u_{\epsilon}\\ &=K\tau_{0}+L_{\epsilon}u_{\epsilon}\\ &>0.\end{split} (13)

Since Luϵ0Lu_{\epsilon}\geq 0, it follows LϵwKτ0>0L_{\epsilon}w\geq K\tau_{0}>0, therefore, we obtain w(x,t)minΓ(UT)ww(x,t)\geq\min_{\Gamma(U_{T})}w in UTU_{T}, for some Kτ0>0K\tau_{0}>0, by Lemma 3.2. Consequently, Kt+uϵ(x,t)minΓ(UT)uϵKt+u_{\epsilon}(x,t)\geq\min_{\Gamma(U_{T})}u_{\epsilon} in UTU_{T}, which implies KT+uϵ(x,t)minΓ(UT)uϵKT+u_{\epsilon}(x,t)\geq\min_{\Gamma(U_{T})}u_{\epsilon} in UTU_{T} for KK. Taking K0K\to 0, uϵminΓ(UT)uϵu_{\epsilon}\geq\min_{\Gamma(U_{T})}u_{\epsilon}.

4 Proof of the localization property (finite speed of propagation)

The standard method 28 of proving the finite speed of propagation (localization property of solutions) is based on the construction of an appropriate “Barenblatt-type” barrier function, then applying the maximum principle (Section 3). This method has advantages for equations in non-divergence form. The proof was revisited by Tedeev and Vespri 29 in the framework of equations in divergence form by applying the powerful machinery of De Giorgi 1 for estimation of the oscillation of the solution via integral fluxes, obviating the need to construct a barrier function.

In this section, motivated by the approach of Tedeev and Vespri 29, we prove the localization property of solutions using the De Giorgi–Ladyzhenskaya iteration procedure 30, for the non-divergence form Eq. 9. Let uϵ0u_{\epsilon}\geq 0 be a classical solution of the following IBVP:

uϵt+Δea(uϵ+ϵ)γ(|uϵ|β+ϵ)i=1duϵxiσ22a(uϵ+ϵ)γ(|uϵ|β+ϵ)Δuϵ=0,\displaystyle\frac{\partial u_{\epsilon}}{\partial t}+\frac{\Delta^{e}}{a}(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\sum_{i=1}^{d}\frac{\partial u_{\epsilon}}{\partial x_{i}}-\frac{\sigma^{2}}{2a}(u_{\epsilon}+\epsilon)^{\gamma}(|\nabla u_{\epsilon}|^{\beta}+\epsilon)\Delta u_{\epsilon}=0, (14)
uϵ(x,0)=u0(x)+ϵ,\displaystyle u_{\epsilon}(x,0)=u_{0}(x)+\epsilon, (15)
uϵ(x,t)|U×(0,T)=ϵ.\displaystyle u_{\epsilon}(x,t)|_{\partial U\times(0,T)}=\epsilon. (16)

Here, |u|=i=1d|u/xi|2|\nabla u|=\sqrt{\sum_{i=1}^{d}|\partial u/\partial{x_{i}}|^{2}}. Observe that Eq. 14 is Eq. 9 with a=τ0a=\tau_{0}. In this section, we use τ\tau as a generic (“dummy”) integration variable, not to be confused with τ\tau from Section 2.

Assume that suppu0BR0(0)\operatorname{supp}u_{0}\subset B_{R_{0}}(0) and UdU\subset\mathbb{R}^{d} are bounded, and consider the sequence of rn=2r(11/2n+1)r_{n}=2r\left(1-1/2^{n+1}\right) for n=0,1,2,n=0,1,2,\ldots with r>2R0r>2R_{0}. Let r¯n=(rn+rn+1)/2\overline{r}_{n}=(r_{n}+r_{n+1})/{2}, Un=UBrn(0)U_{n}=U\setminus B_{r_{n}}(0), and U¯n=UBr¯n(0)\overline{U}_{n}=U\setminus B_{\overline{r}_{n}}(0). We define ηn\eta_{n} to be a sequence of cut-off functions s.t.

ηn(x)={0, for xBrn(0),1, for xU¯n,|ηn|c2nr, otherwise.\eta_{n}(x)=\begin{cases}0,&\text{ for }x\in B_{r_{n}}(0),\\ 1,&\text{ for }x\in\overline{U}_{n},\\ |\nabla\eta_{n}|\leq\frac{c2^{n}}{r},&\text{ otherwise.}\end{cases} (17)

Here, c>0c>0 is a constant.

Lemma 4.1.

Assume that γ>0\gamma>0, β0\beta\geq 0, and σ2>0{\sigma^{2}}>0. Let θ1\theta\geq 1 and Δe,p\Delta^{e},p\in\mathbb{R} be s.t.

β+2p<(θ+γβ+1)2|Δe|σ2.\displaystyle\beta+2\leq p<\left(\frac{\theta+\gamma}{\beta+1}\right)-\frac{2|\Delta^{e}|}{\sigma^{2}}. (18)

Then, for any t>0t>0, there exist constants c0c_{0} and ν\nu such that

sup0<τ<tUn+1uϵθ+1𝑑x+C0tUn+1uϵθ+γ1|uϵ|β+2𝑑x𝑑τDn0tUnuϵθ+γ+β+1𝑑x𝑑τ+c0ϵνt,\sup_{0<\tau<t}\int_{U_{n+1}}u_{\epsilon}^{\theta+1}\,dx+C\int_{0}^{t}\int_{U_{n+1}}u_{\epsilon}^{\theta+\gamma-1}|\nabla u_{\epsilon}|^{\beta+2}\,dxd\tau\leq D_{n}\int_{0}^{t}\int_{U_{n}}u_{\epsilon}^{\theta+\gamma+\beta+1}\,dxd\tau+c_{0}\epsilon^{\nu}t, (19)

where we have introduced the definitions

C\displaystyle C \triangleq(θ+1)2a[σ2(θ+γ1+β)2|Δe|σ2p],\displaystyle\triangleq\frac{(\theta+1)}{2a}\left[{\sigma^{2}}\left(\frac{\theta+\gamma}{1+\beta}\right)-{2|\Delta^{e}|}-{{\sigma^{2}}p}\right], (20)
Dn\displaystyle D_{n} \triangleq(θ+1)2a[σ2p(c2nr)β+2+2|Δe|].\displaystyle\triangleq\frac{(\theta+1)}{2a}\left[{{\sigma^{2}}p}\left(\frac{c2^{n}}{r}\right)^{\beta+2}+2{|\Delta^{e}|}\right]. (21)
Proof 4.2.

Let tTt\leq T, multiply both sides of Eq. 14 by ηnpuϵθ\eta_{n}^{p}u_{\epsilon}^{\theta} and integrate over Ut\triangleqU×(0,t)U_{t}\triangleq U\times(0,t) to obtain:

1θ+1Utηnpuϵθ+1𝑑x+ΔeaUtηnpuϵθ+γ|uϵ|βi=1duϵxidxdτ+σ22a(β+1)Ut(ηnpuϵθ+γ)|uϵ|βuϵdxdτ=0.\frac{1}{\theta+1}\int_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+1}\,dx+\frac{\Delta^{e}}{a}\iint_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma}|\nabla u_{\epsilon}|^{\beta}\sum_{i=1}^{d}\frac{\partial u_{\epsilon}}{\partial x_{i}}\,dxd\tau+\frac{\sigma^{2}}{{2a}(\beta+1)}\iint_{U_{t}}\nabla\left(\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma}\right)|\nabla u_{\epsilon}|^{\beta}\nabla u_{\epsilon}\,dxd\tau=0. (22)

Compute (ηnpuϵθ+γ)\nabla\left(\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma}\right), then Eq. 22 yields

1θ+1Utηnpuϵθ+1𝑑x|Δe|aUtηnpuϵθ+γ|uϵ|β+1𝑑x𝑑τ+σ22a(θ+γβ+1)Utηnp|uϵ|β+2uϵθ+γ1𝑑x𝑑τσ22apUtηnp1|ηn||uϵ|β+1uϵθ+γ𝑑x𝑑τ.\frac{1}{\theta+1}\int_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+1}\,dx-\frac{|\Delta^{e}|}{a}\iint_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma}|\nabla u_{\epsilon}|^{\beta+1}\,dxd\tau+\frac{\sigma^{2}}{2a}\left(\frac{\theta+\gamma}{\beta+1}\right)\iint_{U_{t}}\eta_{n}^{p}|\nabla u_{\epsilon}|^{\beta+2}u_{\epsilon}^{\theta+\gamma-1}\,dxd\tau\\ \leq{\frac{\sigma^{2}}{2a}p}\iint_{U_{t}}\eta_{n}^{p-1}|\nabla\eta_{n}||\nabla u_{\epsilon}|^{\beta+1}u_{\epsilon}^{\theta+\gamma}\,dxd\tau. (23)

Apply Young’s inequity:

ηnp1|ηn||uϵ|β+1uϵθ+γηn(p1)(β+2)β+1|uϵ|β+2uϵθ+γ1+|ηn|β+2uϵθ+γ+β+1.\eta_{n}^{p-1}{}|\nabla\eta_{n}||\nabla u_{\epsilon}|^{\beta+1}u_{\epsilon}^{\theta+\gamma}\leq\eta_{n}^{\frac{(p-1)(\beta+2)}{\beta+1}}|\nabla u_{\epsilon}|^{\beta+2}u_{\epsilon}^{\theta+\gamma-1}+|\nabla\eta_{n}|^{\beta+2}u_{\epsilon}^{\theta+\gamma+\beta+1}. (24)

Note that

|uϵ|β+1uϵθ+γ|uϵ|β+2uϵθ+γ1+uϵθ+γ+β+1.|\nabla u_{\epsilon}|^{\beta+1}u_{\epsilon}^{\theta+\gamma}\leq|\nabla u_{\epsilon}|^{\beta+2}u_{\epsilon}^{\theta+\gamma-1}+u_{\epsilon}^{\theta+\gamma+\beta+1}. (25)

Then, the estimate (23) becomes

1θ+1Utηnpuϵθ+1𝑑x|Δe|aUtηnpuϵθ+γ1|uϵ|β+2+ηnpuϵθ+γ+β+1dxdτ+σ22a(θ+γβ+1)Utηnp|uϵ|β+2uϵθ+γ1𝑑x𝑑τσ22apUtηn(p1)(β+2β+1)uϵθ+γ1|uϵ|β+2+uϵθ+γ+β+1|ηn|β+2dxdτ.\frac{1}{\theta+1}\int_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+1}\,dx-\frac{|\Delta^{e}|}{a}\iint_{U_{t}}\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma-1}|\nabla u_{\epsilon}|^{\beta+2}+\eta_{n}^{p}u_{\epsilon}^{\theta+\gamma+\beta+1}\,dxd\tau+\frac{\sigma^{2}}{2a}\left(\frac{\theta+\gamma}{\beta+1}\right)\iint_{U_{t}}\eta_{n}^{p}|\nabla u_{\epsilon}|^{\beta+2}u_{\epsilon}^{\theta+\gamma-1}\,dxd\tau\\ \leq{\frac{\sigma^{2}}{2a}p}\iint_{U_{t}}\eta_{n}^{{(p-1)}({\frac{\beta+2}{\beta+1}})}u_{\epsilon}^{\theta+\gamma-1}|\nabla u_{\epsilon}|^{\beta+2}+u_{\epsilon}^{\theta+\gamma+\beta+1}|\nabla\eta_{n}|^{\beta+2}\,dxd\tau. (26)

Rearranging the above inequality, we obtain

[σ22a(θ+γβ+1)|Δe|a]ηnp>σ22apηn(p1)(β+2β+1)\left[\frac{\sigma^{2}}{2a}\left(\frac{\theta+\gamma}{\beta+1}\right)-\frac{|\Delta^{e}|}{a}\right]\eta_{n}^{p}>{\frac{\sigma^{2}}{2a}p}\eta_{n}^{{(p-1)}\left({\frac{\beta+2}{\beta+1}}\right)} (27)

by Eq. 18. Note that Un+1U¯nUnUU_{n+1}\subset\overline{U}_{n}\subset U_{n}\subset U. So, the inequality (26) becomes

1θ+1Un+1uϵθ+1𝑑x+0tUn+1[σ22a(θ+γβ+1)|Δe|aσ22ap]uϵθ+γ1|uϵ|β+2𝑑x𝑑τσ22apUnU¯nuϵθ+γ+β+1(c2nr)β+2𝑑x𝑑τ+|Δe|aUnuϵθ+γ+β+1𝑑x𝑑τ.\frac{1}{\theta+1}\int_{U_{n+1}}u_{\epsilon}^{\theta+1}\,dx+\int_{0}^{t}\int_{U_{n+1}}\left[\frac{\sigma^{2}}{2a}\left(\frac{\theta+\gamma}{\beta+1}\right)-\frac{|\Delta^{e}|}{a}-{\frac{\sigma^{2}}{2a}p}\right]u_{\epsilon}^{\theta+\gamma-1}|\nabla u_{\epsilon}|^{\beta+2}\,dxd\tau\\ \leq{\frac{\sigma^{2}}{2a}}p\iint_{U_{n}\setminus{\overline{U}_{n}}}u_{\epsilon}^{\theta+\gamma+\beta+1}\left(\frac{c2^{n}}{r}\right)^{\beta+2}\,dxd\tau+{\frac{|\Delta^{e}|}{a}}\iint_{{U}_{n}}u_{\epsilon}^{\theta+\gamma+\beta+1}\,dxd\tau. (28)

Thus, we have

sup0<τ<tUn+1uϵθ+1𝑑x+C0tUn+1uϵθ+γ1|uϵ|β+2𝑑x𝑑τDn0tUnuϵθ+γ+β+1𝑑x𝑑τ.\sup_{0<\tau<t}\int_{U_{n+1}}u_{\epsilon}^{\theta+1}\,dx+C\int_{0}^{t}\int_{U_{n+1}}u_{\epsilon}^{\theta+\gamma-1}|\nabla u_{\epsilon}|^{\beta+2}\,dxd\tau\leq D_{n}\int_{0}^{t}\int_{U_{n}}u_{\epsilon}^{\theta+\gamma+\beta+1}\,dxd\tau. (29)

Now, let us define the mapping

w\trianglequϵ(θ+γ+β+1)/(β+2),w\triangleq u_{\epsilon}^{{(\theta+\gamma+\beta+1)}/{(\beta+2)}}, (30)

and, for any n=0,1,2,n=0,1,2,\ldots, define

In(t)\triangleqsup0<τ<tUn+1wq𝑑x+0tUn+1|w|β+2𝑑x𝑑τ,I_{n}(t)\triangleq\sup_{0<\tau<t}\int_{U_{n+1}}w^{q}\,dx+\int_{0}^{t}\int_{U_{n+1}}|\nabla w|^{\beta+2}\,dxd\tau, (31)

where q\triangleq(θ+1)(β+2)/(θ+γ+β+1)q\triangleq{(\theta+1)(\beta+2)}/{(\theta+\gamma+\beta+1)}.

Lemma 4.3 (Iteration lemma).

Let uϵ(x,t)0u_{\epsilon}(x,t)\geq 0 be a classical solution of IBVP (14)–(16). Then CL>0\exists\;C_{L}>0, bL>1b_{L}>1, cc, a>0a>0 and ν>0\nu>0 s.t. for given n=1,2,n=1,2,\ldots,

Inϵ(t)t1ζCLbL(n1)(In1ϵ(t))1+ϵ0+cϵνta,I_{n}^{\epsilon}(t)\leq t^{1-\zeta}C_{L}b^{(n-1)}_{L}\left(I_{n-1}^{\epsilon}(t)\right)^{1+\epsilon_{0}}+c\epsilon^{\nu}t^{a}, (32)

where

ϵ0\displaystyle\epsilon_{0} \triangleq(1ζ)(β+2q1),\displaystyle\triangleq(1-\zeta)\left(\frac{\beta+2}{q}-1\right), (33)
ζ\displaystyle\zeta \triangleqγ+βγ+β+d(β+2)(θ+1).\displaystyle\triangleq\frac{\gamma+\beta}{\gamma+\beta+d(\beta+2)(\theta+1)}. (34)
Proof 4.4.

The inequality (29) becomes

sup0<τ<tUn+1wq𝑑x+0tUn+1|w|β+2𝑑x𝑑τDnK0tUnwβ+2𝑑x𝑑τ,\sup_{0<\tau<t}\int_{U_{n+1}}w^{q}\,dx+\int_{0}^{t}\int_{U_{n+1}}|\nabla w|^{\beta+2}\,dxd\tau\leq\frac{D_{n}}{K}\int_{0}^{t}\int_{U_{n}}w^{\beta+2}\,dxd\tau, (35)

where K=min{1,C[q/(θ+1)]β+2}K=\min\left\{1,C[q/(\theta+1)]^{\beta+2}\right\}.

Applying the Gagliardo–Nirenberg–Sobolev inequality on the function w(x,t)w(x,t), one can obtain

Unwβ+2𝑑xcG(Un|w|β+2𝑑x)ζ(Unwq𝑑x)(1ζ)(β+2)q\int_{U_{n}}w^{\beta+2}\,dx\leq c_{G}\left(\,\int_{U_{n}}|\nabla w|^{\beta+2}\,dx\right)^{\zeta}\left(\,\int_{U_{n}}w^{q}\,dx\right)^{\frac{(1-\zeta)(\beta+2)}{q}} (36)

for some constant cGc_{G}. Integrating the above inequality over time, we get

0tUnwβ+2𝑑x𝑑τcG0t(Un|w|β+2𝑑x)ζ𝑑τ(sup0<τ<tUnwq𝑑x)(1ζ)(β+2)q.\int_{0}^{t}\int_{U_{n}}w^{\beta+2}\,dxd\tau\leq c_{G}\int_{0}^{t}\left(\,\int_{U_{n}}|\nabla w|^{\beta+2}\,dx\right)^{\zeta}d\tau\left(\sup_{0<\tau<t}\int_{U_{n}}w^{q}\,dx\right)^{\frac{(1-\zeta)(\beta+2)}{q}}. (37)

By applying Hölder’s inequality in the last result, we have

0tUnwβ+2𝑑x𝑑τcGt1ζ(0tUn|w|β+2𝑑x𝑑τ)ζ(sup0<τ<tUnwq𝑑x)(1ζ)(β+2)q.\int_{0}^{t}\int_{U_{n}}w^{\beta+2}\,dxd\tau\leq c_{G}t^{1-\zeta}\left(\int_{0}^{t}\int_{U_{n}}|\nabla w|^{\beta+2}\,dxd\tau\right)^{\zeta}\left(\sup_{0<\tau<t}\int_{U_{n}}w^{q}\,dx\right)^{\frac{(1-\zeta)(\beta+2)}{q}}. (38)

Using Eq. 38 in Eq. 35, the quantity defined in Eq. 31 is bounded as

In(t)DnKcGt1ζIn1ζ+(1ζ)(β+2)q.I_{n}(t)\leq\frac{D_{n}}{K}c_{G}t^{1-\zeta}I_{n-1}^{\zeta+\frac{(1-\zeta)(\beta+2)}{q}}. (39)

Note that ζ+(1ζ)(β+2)q=1+ϵ0{\zeta+\frac{(1-\zeta)(\beta+2)}{q}}=1+\epsilon_{0}. Moreover, by Eq. 18, we obtain

Dn(θ+1)[|Δe|a+(c2R0)σ22a(θ+γ)]2nβ+2n.D_{n}\leq(\theta+1)\left[\frac{|\Delta^{e}|}{a}+\left(\frac{c}{2R_{0}}\right)\frac{\sigma^{2}}{2a}(\theta+\gamma)\right]2^{{n\beta}+2n}. (40)

Therefore, from Eq. 39, we have the following iterative relation

Int1ζCLbLn1In11+ϵ0I_{n}\leq t^{1-\zeta}C_{L}b^{n-1}_{L}I_{n-1}^{1+\epsilon_{0}} (41)

with CL={(θ+1)[|Δe|a+(c2R0)σ22a(θ+γ)]cGK2β+2}C_{L}=\left\{(\theta+1)\left[\frac{|\Delta^{e}|}{a}+\left(\frac{c}{2R_{0}}\right)\frac{\sigma^{2}}{2a}(\theta+\gamma)\right]\frac{c_{G}}{K}2^{{\beta}+2}\right\} and bL=2β+2b_{L}=2^{\beta+2}.

Finally, the main inequality of Lemma 4.3 follows from Eq. 41. It is not difficult to show that μ>0\exists~{}\mu>0 depending on the parameters of the model s.t. for the integral

I~nϵ=sup0<τ<tUn+1uϵμ𝑑x,\tilde{I}_{n}^{\epsilon}=\sup_{0<\tau<t}\int_{U_{n+1}}u_{\epsilon}^{\mu}\,dx, (42)

the corollaries follow.

Corollary 4.5.

There exist constants ν>0\nu>0, μ>0,\mu>0, aa, and cc independent from ϵ\epsilon s.t. for any given nn,

I~nϵbntϵ0(I~n1ϵ)1+ϵ0+ctaϵν.\tilde{I}_{n}^{\epsilon}\leq b^{n}t^{\epsilon_{0}}\left(\tilde{I}_{n-1}^{\epsilon}\right)^{1+\epsilon_{0}}+ct^{a}\epsilon^{\nu}. (43)
Corollary 4.6.

Let uu be a weak viscosity solution in the sense of weak convergence of the sequence regularized solutions uϵu_{\epsilon} and

I~n=sup0<τ<tUn+1uμ𝑑x,\tilde{I}_{n}=\sup_{0<\tau<t}\int_{U_{n+1}}u^{\mu}\,dx, (44)

then

I~nbntϵ0(I~n1)1+ϵ0.\tilde{I}_{n}\leq b^{n}t^{\epsilon_{0}}\left(\tilde{I}_{n-1}\right)^{1+\epsilon_{0}}. (45)

Finally, via the Ladyzhenskaya iterative Lemma 31, the following theorem is established.

Theorem 4.7.

Assume the weak viscosity solution u(x,t)u(x,t) is s.t.

I~0(T)CL1ϵ02(β+2ϵ02)T(θ+1γ+β).\tilde{I}_{0}(T)\leq C_{L}^{-\frac{1}{\epsilon_{0}}}2^{-\left(\frac{\beta+2}{\epsilon_{0}^{2}}\right)}T^{-\left(\frac{\theta+1}{\gamma+\beta}\right)}. (46)

Then,

I~n(T)0 as n.\tilde{I}_{n}(T)\rightarrow 0\text{ as }n\rightarrow\infty. (47)
Corollary 4.8 (Localization property of solutions).

Since Un+1UnU_{n+1}\subset U_{n}, it follows from Theorem 4.7 and the maximum principle that, for any initial data with compact support in the ball B2r(0)B_{2r}(0), there exists TT s.t. the weak viscosity solution

u(x,t)=0 a.e.  in UB2r(0) for any tT.u(x,t)=0\quad\text{ a.e. }\quad\text{ in }\quad U\setminus{B_{2r}(0)}\quad\text{ for any }\quad t\leq T. (48)

5 Mapping of the non-divergence form equation to divergence form

The physical models in which nonlinear degenerate diffusion equations arise, which were discussed in Section 1, generically lead to divergence form equations. On the other hand, however, the Einstein paradigm, introduced in Section 2, generically leads to a PDE in non-divergence form. To connect these two formulations, in this section, we present a transition formula between them, which is often convenient in the analysis of degenerate parabolic PDE 32.

As it was pointed out in Section 1, the solution of the degenerate parabolic PDE arising from the Einstein paradigm for Brownian motion may not be smooth. So, our estimates and localization property did not rely on smoothness. To be clear, however, we worked with the so-called viscosity solution 27, and obtained a qualitative result. In this section, we are assuming that the solution of both the divergent and non-divergent form equation is smooth enough to prove a mapping formula between them. We believe that it will not difficult to show that the weak viscosity solution will obey such a mapping as well. However, this is not a result needed for the upcoming illustrations of the finite speed of propagation (localization) property, so we leave this detail for future work.

Since all our semi-analytic solutions and numerical simulations, which follow in Section 6, will be performed on a 1D spatial domain without drift, we henceforth assume that xx\in\mathbb{R} and Δe=0\Delta^{e}=0. The key mathematical result of this section is to connect solutions of a generalized degenerate Einstein equation in non-divergence form Eq. 49 to solutions of a corresponding Eq. 52 in divergence form.

Theorem 5.1 (Mapping of solutions).

Let 0γ<1.0\leq\gamma<1. Assume that u(x,t)𝒞x,t2,1u(x,t)\in\mathcal{C}^{2,1}_{x,t}, u0u\geq 0, and it solves

Lu=utσ22uγ|ux|β2ux2=0.Lu=\frac{\partial u}{\partial t}-\frac{\sigma^{2}}{2}u^{\gamma}\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial^{2}u}{\partial x^{2}}=0. (49)

Let

α=γ1γγ=α1+α.\alpha=\frac{\gamma}{1-\gamma}\quad\Leftrightarrow\quad\gamma=\frac{\alpha}{1+\alpha}. (50)

Define a uu-vv mapping via

v\trianglequ1α+1.v\triangleq u^{\frac{1}{\alpha+1}}. (51)

Then, v(x,t)0v(x,t)\geq 0 is the solution of

L^v=vtq0x(vγ0|vx|βvx)=0,\hat{L}v=\frac{\partial v}{\partial t}-q_{0}\frac{\partial}{\partial x}\left(v^{\gamma_{0}}\left|\frac{\partial v}{\partial x}\right|^{\beta}\frac{\partial v}{\partial x}\right)=0, (52)

where

q0=σ22(α+1)βandγ0=α(β+1).q_{0}=\frac{\sigma^{2}}{2}(\alpha+1)^{\beta}\qquad\text{and}\qquad\gamma_{0}=\alpha(\beta+1). (53)
Proof 5.2.

We proceed as follows.

  1. 1.

    Since we have assumed that xx\in\mathbb{R}, then |v|=(v/x)2|\nabla v|=\sqrt{(\partial v/\partial x)^{2}}. Additionally, for any function v𝒞x1v\in\mathcal{C}^{1}_{x} with γ0\gamma_{0} given in Eq. 53, it is straightforward to show that

    1(α+1)1+β|(vα+1)x|β(vα+1)x=vγ0|vx|βvx,\frac{1}{(\alpha+1)^{1+\beta}}\left|\frac{\partial(v^{\alpha+1})}{\partial x}\right|^{\beta}\frac{\partial(v^{\alpha+1})}{\partial x}=v^{\gamma_{0}}\left|\frac{\partial v}{\partial x}\right|^{\beta}\frac{\partial v}{\partial x}, (54)

    where we have used the fact that v0v\geq 0.

  2. 2.

    From the above, it follows that, for some constant C1C_{1},

    L0v=vtC1x(vγ0|vx|βvx)=vtC11(α+1)1+βx(|(vα+1)x|β(vα+1)x).\begin{split}L_{0}v&=\frac{\partial v}{\partial t}-C_{1}\frac{\partial}{\partial x}\left(v^{\gamma_{0}}\left|\frac{\partial v}{\partial x}\right|^{\beta}\frac{\partial v}{\partial x}\right)\\ &=\frac{\partial v}{\partial t}-C_{1}\frac{1}{(\alpha+1)^{1+\beta}}\frac{\partial}{\partial x}\left(\left|\frac{\partial(v^{\alpha+1})}{\partial x}\right|^{\beta}\frac{\partial(v^{\alpha+1})}{\partial x}\right).\end{split} (55)
  3. 3.

    Multiplying Eq. 55 by vαv^{\alpha} and using the mapping (51), we obtain

    vαL0v=vαvtC11(α+1)1+βvαx(|(vα+1)x|β(vα+1)x)=1(α+1)utC11(α+1)1+βuα1+αx(|ux|βux).\begin{split}v^{\alpha}L_{0}v&=v^{\alpha}\frac{\partial v}{\partial t}-C_{1}\frac{1}{(\alpha+1)^{1+\beta}}v^{\alpha}\frac{\partial}{\partial x}\left(\left|\frac{\partial(v^{\alpha+1})}{\partial x}\right|^{\beta}\frac{\partial(v^{\alpha+1})}{\partial x}\right)\\ &=\frac{1}{(\alpha+1)}\frac{\partial u}{\partial t}-C_{1}\frac{1}{(\alpha+1)^{1+\beta}}u^{\frac{\alpha}{1+\alpha}}\frac{\partial}{\partial x}\left(\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial u}{\partial x}\right).\end{split} (56)

    Introducing γ\gamma from Eq. 50 into Eq. 56:

    (α+1)vαL0v=utC11(α+1)βuγx(|ux|βux).(\alpha+1)v^{\alpha}L_{0}v=\frac{\partial u}{\partial t}-C_{1}\frac{1}{(\alpha+1)^{\beta}}u^{\gamma}\frac{\partial}{\partial x}\left(\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial u}{\partial x}\right). (57)
  4. 4.

    Observe that

    x(|ux|βux)=(1+β)|ux|β2ux2.\frac{\partial}{\partial x}\left(\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial u}{\partial x}\right)=(1+\beta)\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial^{2}u}{\partial x^{2}}. (58)
  5. 5.

    Substituting Eq. 58 into Eq. 57, we obtain

    (α+1)vαL0v=utC1(1+β)(α+1)βuγ|ux|β2ux2.(\alpha+1)v^{\alpha}L_{0}v=\frac{\partial u}{\partial t}-C_{1}\frac{(1+\beta)}{(\alpha+1)^{\beta}}u^{\gamma}\left|\frac{\partial u}{\partial x}\right|^{\beta}\frac{\partial^{2}u}{\partial x^{2}}. (59)
  6. 6.

    Suppose that L0v=0L_{0}v=0 and let C1=q01+βC_{1}=\frac{q_{0}}{1+\beta}, then we obtain the desired result.

Remark 5.3.

We can remove the coefficient q0q_{0} from Eq. 52 by letting (x,t)=(x,q0t)(x^{\prime},t^{\prime})=(x,q_{0}t), where q0q_{0} is given in Eq. 53.

6 Numerical examples of the localization property of solutions

6.1 Preliminaries

In light of Remark 5.3, let us relabel xxx^{\prime}\leftrightarrow x and ttt^{\prime}\leftrightarrow t for simplicity. Now, based on Eq. 52 and the above deliberations, consider the 1D problem:

vtx(vγ0|vx|mvx)=0,\frac{\partial v}{\partial t}-\frac{\partial}{\partial x}\left(v^{\gamma_{0}}\left|\frac{\partial v}{\partial x}\right|^{m}\frac{\partial v}{\partial x}\right)=0, (60)

where the sign of mm is not fixed. The results from Section 4 apply for the case of m=β>0m=\beta>0. In this section, we will discuss some cases (beyond the scope of our earlier results) that do not assume m>0m>0, hence the change in notation.

Equation 60 is subject to the compact initial condition (IC):

v(x,0)=v0(x)={34x0[1(xx0)2],|x|x0,0,|x|>x0.v(x,0)=v_{0}(x)=\begin{cases}\displaystyle\frac{3}{4x_{0}}\left[1-\left(\frac{x}{x_{0}}\right)^{2}\right],&\quad|x|\leq x_{0},\\ 0,&\quad|x|>x_{0}.\end{cases} (61)

Take x0=1x_{0}=1 without loss of generality. Note that we do not take a “box” function because then |dv0/dx||dv_{0}/dx| would be undefined as |x|x0|x|\to x_{0}, which would cause numerical difficulties. Instead, we take a “mound” function (inverted parabola) of unit area.

We solve Eq. 60 subject to (61) on a finite length domain, x[xmax,+xmax]x\in[-x_{\mathrm{max}},+x_{\mathrm{max}}] subject to “natural” (Neumann) boundary conditions (BCs) at the endpoints:

vx|x=±xmax=0t[0,T].\left.\frac{\partial v}{\partial x}\right|_{x=\pm x_{\mathrm{max}}}=0\qquad\forall t\in[0,T]. (62)

The interval [xmax,+xmax][-x_{\mathrm{max}},+x_{\mathrm{max}}] is chosen to be large enough, so that the imposed BCs at x=±xmaxx=\pm x_{\mathrm{max}} have no influence whatsoever on the nonlinear diffusion process of a localized initial condition, during the time interval (0,T](0,T] of interest.

6.2 Explicit construction of the Kompaneets–Zel’dovich–Barenblatt-type barrier function

Given the localization property proved in Section 4, finite speed of expansion of the compact support of the initial condition is expected under generic conditions without the need to explicitly construct a barrier function. However, for a class of 1D PDEs arising from our nonlinear Einstein paradigm, it is also possible to explicitly construct the spreading self-similar solutions with compact support.

Therefore, for completeness and to illustrate our general mathematical result, in this subsection, we construct solutions with finite speed of propagation explicitly using the Kompaneets–Zel’dovich–Barenblatt self-similarity approach 11, 33, 34. This calculation, of course, is only explicit for the 1D model considered in this section, i.e., Eq. 60 subject to v(x,0)=δ(x)v(x,0)=\delta(x) (point source, or fundamental, solution).

To this end, let the support of the solution increase as [xf(t),+xf(t)][-x_{f}(t),+x_{f}(t)] for some moving front function xf(t)x_{f}(t) to be determined. The point-source initial condition together with the localization property of the solution imposes a “finite mass” constraint on vv:

xf(t)+xf(t)v(x,t)𝑑x=1t0.\int_{-x_{f}(t)}^{+x_{f}(t)}v(x,t)\,dx=1\quad\forall t\geq 0. (63)

Next, assume that v(x,t)=Vtςf(ξ)v(x,t)=Vt^{-\varsigma}f(\xi), where VV is a constant, ξ\triangleqη/ηf\xi\triangleq\eta/\eta_{f} is the normalized similarity variable, with η\triangleqxtς\eta\triangleq xt^{-\varsigma} and ηf\eta_{f} being the (constant) value of η\eta at x=xf(t)x=x_{f}(t) (i.e., ηf=xf(t)tς\eta_{f}=x_{f}(t)t^{-\varsigma}). Here, VV, ς\varsigma and ηf\eta_{f} must be determined from the PDE (60) and any initial/boundary condition(s) to ensure the self-similarity assumption that v(x,t)=Vtςf(ξ)v(x,t)=Vt^{-\varsigma}f(\xi) holds. Substituting this transformation into Eq. 60, it is easy to show that such a solution exists if the following ordinary differential equation (ODE) is satisfied:

ς(f+ξf)+(fγ0|f|mf)=0,ξ(1,+1),\varsigma\left(f+\xi f^{\prime}\right)+(f^{\gamma_{0}}|f^{\prime}|^{m}f^{\prime})^{\prime}=0,\qquad\xi\in(-1,+1), (64)

with

ς=1γ0+2m+2,V=ηf(m+2)/(γ0+m).\varsigma=\frac{1}{\gamma_{0}+2m+2},\qquad V=\eta_{f}^{(m+2)/(\gamma_{0}+m)}. (65)

Here, prime denotes differentiation with respect to the argument of ff, i.e., d/dξd/d\xi. By the localization property of the solution, f(±1)=0f(\pm 1)=0. Finally, ηf\eta_{f} is determined by transforming Eq. 63:

ηf=[1+1f(ξ)𝑑ξ](γ0+m)/(γ0+2m+2),\eta_{f}=\left[\int_{-1}^{+1}f(\xi)\,d\xi\right]^{-(\gamma_{0}+m)/(\gamma_{0}+2m+2)}, (66)

having used the expression for VV from Eq. 65.

Next, observe that the left-hand side of the ODE (64) is a product rule, hence a first integral exists:

ςξf+fγ0|f|mf=0,\varsigma\xi f+f^{\gamma_{0}}|f^{\prime}|^{m}f^{\prime}=0, (67)

where the constant of integration is set to zero by requiring ξξ\xi\leftrightarrow-\xi symmetry. Symmetry also allows us to deal with the absolute value in Eq. 67 by restricting to ξ0\xi\geq 0. The simulations to be discussed in Section 6.3 suggest that f(ξ)f(\xi) is monotonically decreasing on [0,1][0,1], so we can set |f|=f|f^{\prime}|=-f^{\prime}. Then, the first integral (67) of the ODE becomes

f(γ01)/(m+1)f=(ςξ)1/(m+1).f^{(\gamma_{0}-1)/(m+1)}f^{\prime}=-\left(\varsigma\xi\right)^{1/(m+1)}. (68)

Now, using f(1)=0f(1)=0 and ς\varsigma from Eq. 65, the solution to the ODE (64) is

f(ξ)=[(γ0+mm+2)(γ0+2m+2)1m+1(1ξm+2m+1)]m+1γ0+m,ξ[0,1].f(\xi)=\left[\left(\frac{\gamma_{0}+m}{m+2}\right)(\gamma_{0}+2m+2)^{\frac{-1}{m+1}}\left(1-\xi^{\frac{m+2}{m+1}}\right)\right]^{\frac{m+1}{\gamma_{0}+m}},\quad\xi\in[0,1]. (69)

From the constraint (66) it follows that

ηf=(m+2γ0+m)m+1γ0+2m+2(γ0+2m+2)1γ0+2m+2[12(m+2m+1)Γ(m+1m+2+m+1m+γ0+1)Γ(m+1m+2)Γ(m+1m+γ0+1)]γ0+mγ0+2m+2,\eta_{f}=\left(\frac{m+2}{\gamma_{0}+m}\right)^{\frac{m+1}{\gamma_{0}+2m+2}}(\gamma_{0}+2m+2)^{\frac{1}{\gamma_{0}+2m+2}}\left[\frac{1}{2}\left(\frac{m+2}{m+1}\right)\frac{\Gamma\left(\frac{m+1}{m+2}+\frac{m+1}{m+\gamma_{0}}+1\right)}{\Gamma\left(\frac{m+1}{m+2}\right)\Gamma\left(\frac{m+1}{m+\gamma_{0}}+1\right)}\right]^{\frac{\gamma_{0}+m}{\gamma_{0}+2m+2}}, (70)

where Γ(z)\Gamma(z) is the Gamma function. See also the works by Eggers and Fontelos 35 (Exercise 3.5, p. 59 therein) or Pattle 36 for the (classical) special case of m=0m=0.

Motivated by Barenblatt 6, 37, we observe that the behavior of the gradient ff^{\prime}, as ξ0\xi\to 0 or ξ1\xi\to 1, depends on γ0\gamma_{0} and mm. From the self-similar solution (69), we compute

f(ξ)=(γ0+2m+2)1m+1ξ1m+1[(γ0+m)(m+2)(γ0+2m+2)1m+1(1ξm+2m+1)]1γ0γ0+mf^{\prime}(\xi)=-(\gamma_{0}+2m+2)^{\frac{-1}{m+1}}\xi^{\frac{1}{m+1}}\left[\frac{(\gamma_{0}+m)}{(m+2)(\gamma_{0}+2m+2)^{\frac{1}{m+1}}}\left(1-\xi^{\frac{m+2}{m+1}}\right)\right]^{\frac{1-\gamma_{0}}{\gamma_{0}+m}} (71)

to understand the possible scenarios. In Section 4, it was assumed that m>0,γ00m>0,\gamma_{0}\geq 0. Here, let us consider all possibilities instead. From Eq. 71, it follows that the behavior of f(ξ)f^{\prime}(\xi) is regular as ξ0\xi\to 0 and f(0)=0f^{\prime}(0)=0 γ0\forall\gamma_{0} if m>1m>-1 and singular with |f(ξ)||f^{\prime}(\xi)|\to\infty as ξ0+\xi\to 0^{+} if m<1m<-1. The special case of m=1m=-1, if it is of interest, appears to be problematic and requires more careful analysis. Meanwhile, as ξ1\xi\to 1^{-}, f(ξ)f^{\prime}(\xi) is regular and f(1)=0f^{\prime}(1)=0 if (1γ0)/(γ0+m)>0(1-\gamma_{0})/(\gamma_{0}+m)>0 and singular with f(ξ)f^{\prime}(\xi)\to-\infty as ξ1\xi\to 1^{-} if (1γ0)/(γ0+m)<0(1-\gamma_{0})/(\gamma_{0}+m)<0. The special case of γ0=1\gamma_{0}=1 is interesting because then f(1)=(2m+2)1m+1<0f^{\prime}(1)=-(2m+2)^{\frac{-1}{m+1}}<0, assuming m>1m>-1.

These observations also highlight that the self-similar solution is only a weak solution of the original PDE (60) (see, e.g., Ref. 38 and related literature).

Next, we numerically verify the localization property of solutions (i.e., the main mathematical result on finite speed of propagation), as well as the predictions from this section based on the self-similarity analysis.

6.3 Numerical results

The self-similar solution v(x,t)=Vtςf(ξ)v(x,t)=Vt^{-\varsigma}f(\xi) based on Eq. 69, satisfying the normalization condition (63), is strictly speaking the fundamental solution 39, and it is not the exact solution for the initial data (61). However, from the principle of intermediate asymptotics 33, 34, we know that a solution of Eq. 60 subject to (61) eventually converges (for large tt\to\infty) to the point-source self-similar solution, as the initial data is “forgotten.” That is, the self-similar solution from Section 6.2 is, in a sense, an attractor. Hence, the support of the solution v(x,t)v(x,t) starting from the compactly supported initial condition (61) remains compact for t>0t>0. In other words, v(|x|xf(t),t)=0v\big{(}|x|\geq x_{f}(t),t\big{)}=0 while v(|x|<xf(t),t)0v\big{(}|x|<x_{f}(t),t\big{)}\neq 0 (given the xx-symmetry of the problem). Importantly, from the principle of intermediate asymptotics, we know that the compact support of this non-fundamental solution will (for large tt) expand with the same finite speed of propagation as the fundamental (self-similar) solution.

Next, to verify these claims, we use the strongly-implicit finite-difference scheme in conservative form developed and benchmarked by Ghodgaonkar and Christov 15. This scheme is well suited for the types of gradient-degenerate diffusion equations (60) considered in this work. We ensured that the reported numerical results are grid and time-step independent. After obtaining the numerical solution of the PDE (60) subject to (61), we found xf(t)x_{f}(t) s.t. v(x=±xf(t),t)=0v\big{(}x=\pm x_{f}(t),t\big{)}=0. This quantity can then be compared to the prediction of the self-similarity analysis. Specifically, xf(t)t1/(γ0+2m+2)x_{f}(t)\sim t^{1/(\gamma_{0}+2m+2)}, or logxf(t)1γ0+2m+2logt\log x_{f}(t)\sim\frac{1}{\gamma_{0}+2m+2}\log t, based on Section 6.2.

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Figure 2: Example numerical simulations showing finite speed of propagation of initially compact solutions of the PDE (60) from the initial condition (61) (shown as dash-dotted curves in left panels), for different choices of nonlinearity exponents γ0\gamma_{0} and mm, up to t=T=10t=T=10. The speed of propagation, as predicted by the analysis in Section 6.2, is represented by the slope of the dashed trendlines in the right panels. Note that (b) is the special case corresponding to the “Barenblatt solution” of the porous medium equation. The time evolution in the left panels is in the direction of the arrow from dark to light colored curves. The plots in the right panels are on a log-log scale.

The numerical results are shown in Fig. 2. We confirm the finite speed of propagation of the solution at the speed predicted by self-similarity analysis.

Also, observe the sharp crest of the solution at x=0x=0 for m=1m=1 in Fig. 2(a,c). Indeed, Eq. 71 suggests that v/xsgn(x)|x|1/2\partial v/\partial x\sim\operatorname{sgn}(x)|x|^{1/2} as |x|0|x|\to 0, hence there’s a curvature singularity at x=0x=0 leading to the sharp crest. Additionally, as discussed in Section 6.2, v/x0\partial v/\partial x\to 0 as |x|xf(t)|x|\to x_{f}(t) if γ00\gamma_{0}\neq 0 (Fig. 2(a)), but v/xsgn(x)const.\partial v/\partial x\to\operatorname{sgn}(x)const. as |x|xf(t)|x|\to x_{f}(t) in the special case of γ0=1\gamma_{0}=1 (Fig. 2(b,c)).

7 Discussion on the localization property

The early references on the localization property for parabolic equations link to the work of Zel’dovich. The localization property was then proved by Barenblatt by constructing the “Barenblatt type” of barrier function for the corresponding degenerate nonlinear PDE. They understood that, if the diffusivity degenerates with respect to the solution, then the solution exhibits finite speed of propagation, which can provide a more realistic interpretation of physical observations typically understood via a Darcy/Fourier/Fick-type law. Specifically, with degenerate PDEs, the localization property of the solution of the evolutionary equation is called, in some publications, a “dead zone." In other words, a non-negative solution of the steady-state evolutionary equation, if it exists, must be zero outside of some compact support. Independently, this property of solutions of elliptic equations with nonlinear absorption (dependent on the solution only) was investigated by Landis 26, 40 using his method of lemma of the growth of a narrow domain. This approach leads to a very different perspective on the localization property of solutions.

In the recent work by Tedeev and Vespri 29, a method based on De Giorgi’s iteration (see also the Ladyzhenskaya iterative process) was employed to prove this essential feature for a class of degenerate parabolic equation in divergence form. We used the Tedeev and Vespri approach as our groundwork, but we provided a proof of the localization property (Section 4) for degenerate parabolic equation in non-divergence form, which we derived from a generalized Einstein Brownian motion paradigm (Section 2), giving the non-divergence form equations a new physical interpretation. It is appropriate to mention that Landis used his method to provide an alternative proof of De Giorgi’s celebrated theorem on Hölder continuity of the solution of elliptic equation of second order 41. We believe that, by employing the Landis method, in future work we can significantly widen the class of equations for which the localization property holds. In this way, we can also extend the present results by keeping the absorption term in Eq. 6. Importantly, when starting from the non-divergence form of the equation under the Einstein paradigm, we do not require the smoothness of coefficients, which was assumed in previous works.

Refer to caption
Figure 3: Schematic illustrating of the location of the points on the xx-axis.

Finally, we sketch the arguments that underlay Landis’ machinery for proving the localization property of solutions to the 1D degenerate Einstein model. As it was explained above, for the time interval of free jumps in the most basic nonlinear model Einstein, one can assume that τ=τ0uγ\tau=\tau_{0}u^{-\gamma} (τ0\tau_{0} can be absorbed into tt and scaled out). Here, 0γ<10\leq\gamma<1 and u0u\geq 0. Then, one can rewrite the model as follows:

L0u=u1γt2ux2=0 in the domain  0<x<2L, for  0<t<,\displaystyle L_{0}u=\frac{\partial u^{1-\gamma}}{\partial t}-\frac{\partial^{2}u}{\partial x^{2}}=0\;\text{ in the domain }\;0<x<2L,\;\text{ for }\;0<t<\infty, (72)
u(x,0)=u0(x)>0 for  0<x<L2,\displaystyle u(x,0)=u_{0}(x)>0\ \text{ for }\ {0<x<\frac{L}{2}}, (73)
u(x,0)=0 for L2x<2L,\displaystyle u(x,0)=0\;\text{ for }\;{\frac{L}{2}\leq x<2L}, (74)
ux(0,t)=ux(2L,t)=0 for  0<t<.\displaystyle\frac{\partial u}{\partial x}(0,t)=\frac{\partial u}{\partial x}(2L,t)=0\;\text{ for }\;0<t<\infty. (75)

It will be convenient to use the notation introduced in the diagram in Fig. 3. Let ln=L2nl_{n}=L-2^{-n} and In={x:2L>x>ln}I_{n}=\{x:2L>x>l_{n}\} and Jn=InIn+1J_{n}=I_{n}\setminus I_{n+1}. In the layers Jn1J_{n-1} and Jn2J_{n-2} introduce auxiliary points ξnJn1\xi_{n}\in J_{n-1} and cnJn2c_{n}\in J_{n-2}, which will be specified later. First observe that, due to initial and boundary conditions, the function v(x)=0Tu(x,τ)𝑑τv(x)=\int_{0}^{T}u(x,\tau)\,d\tau satisfies a maximum principle: v(cn)v(ξn)v(c_{n})\geq v(\xi_{n}) for any points cn<ξnc_{n}<\xi_{n}. After integration by parts in the domain I~n=In{x>ξn}\tilde{I}_{n}=I_{n}\cap\{x>\xi_{n}\} and using the Lagrange mean value theorem with ξn\xi_{n} as a mean point, one can easily get the following inequality from maximum principle for the function v(x)v(x):

max0<τ<TIn+1u1γ(x,τ)𝑑xInu1γ(x,T)𝑑x2n0Tu(ξn,τ)𝑑τ.\max_{0<\tau<T}\int_{I_{n+1}}u^{1-\gamma}(x,\tau)\,dx\leq\int_{I_{n}}u^{1-\gamma}(x,T)\,dx\leq 2^{n}\int_{0}^{T}u(\xi_{n},\tau)\,d\tau. (76)

One more application of the maximum principle for v(x)v(x) on the domain I~n=In2{x>cn}\tilde{I}_{n}=I_{n-2}\cap\{x>c_{n}\} and selecting cn=cnc_{n}=c_{n}^{*} as an intermediate value point from the integral mean value theorem for the function u1γu^{1-\gamma}, and using arguments as in Lemma 7.1 with b=ln3b=l_{n-3} and a=ln2a=l_{n-2}, we obtain

Inu1γ(x,T)𝑑x2n2n0T(Jn2u1γ(x,τ)𝑑x)11γ𝑑τ.\int_{I_{n}}u^{1-\gamma}(x,T)\,dx\leq 2^{n}\cdot 2^{n}\int_{0}^{T}\left(\,\,\int_{J_{n-2}}u^{1-\gamma}(x,\tau)\,dx\right)^{\frac{1}{1-\gamma}}\,d\tau. (77)

Then, due to Eq. 76:

max0<τ<TIn+1u1γ(x,τ)dx4nTmax0<τ<T(In2u1γ(x,τ)dx)1+ϵ0,ϵ0=γ1γ.\max_{0<\tau<T}\int_{I_{n+1}}u^{1-\gamma}(x,\tau)\,dx\leq 4^{n}\cdot T\max_{0<\tau<T}\left(\,\,\int_{I_{n-2}}u^{1-\gamma}(x,\tau)\,dx\right)^{1+\epsilon_{0}},\qquad\epsilon_{0}=\frac{\gamma}{1-\gamma}. (78)

From the above inequality follows an iterative estimate similar to the one that we obtained in the iterative inequality in Eq. 41 above. Consequently, we can conclude the localization property holds for the non-negative classical solution of the IBVP (72)–(75) with compact support of the initial data.

Namely, if initial data in the IBVP (72)–(75) with 0γ<10\leq\gamma<1 are s.t.

max0<τ<T02Lu1γ(x,τ)𝑑xT1/ϵ041/ϵ02,\max_{0<\tau<T}\int_{0}^{2L}u^{1-\gamma}(x,\tau)\,dx\leq T^{-1/{\epsilon_{0}}}4^{-1/{\epsilon_{0}^{2}}}, (79)

then

u(x,t)0, for all x[L,2L] during the time interval t[0,T].u(x,t)\equiv 0,\text{ for all }x\in[L,2L]\text{ during the time interval }t\in[0,T]. (80)
Lemma 7.1.

Let u(x,t)0u(x,t)\geq 0 be a continuous function on [a,b]×[0,T][a,b]\times[0,T], and δ>0\delta>0. For any T>0T>0 there exists a<c<ba<c^{*}<b, s.t.

0Tuδ(c,τ)𝑑τTbamax0tTabuδ(x,t)𝑑x.\int_{0}^{T}u^{\delta}(c^{*},\tau)\,d\tau\leq\frac{T}{b-a}\max_{0\leq t\leq T}\int_{a}^{b}u^{\delta}(x,t)\,dx. (81)
Proof 7.2.

Proof follows from the argument. For any T>τ>0T>\tau>0, there exists a<c(τ)<ba<c(\tau)<b s.t.

uδ(c(τ),τ)=1baabuδ(x,τ)𝑑xmax0tT1baabuδ(x,t)𝑑x.u^{\delta}\big{(}c(\tau),\tau\big{)}=\frac{1}{b-a}\int_{a}^{b}u^{\delta}(x,\tau)\,dx\leq\max_{0\leq t\leq T}\frac{1}{b-a}\int_{a}^{b}u^{\delta}(x,t)\,dx. (82)

Acknowledgments

We thank Prof. J. R. Walton for insightful questions about the behavior of the slope of the self-similar solution at the moving front.

Author contributions

Ivan C. Christov — Conceptualization, Investigation, Project administration, Software, Writing – original draft. Isanka Garli Hevage — Formal analysis, Investigation, Methodology, Writing – original draft. Akif Ibraguimov — Conceptualization, Formal analysis, Methodology, Project administration, Supervision, Writing – original draft. Rahnuma Islam — Formal analysis, Investigation, Methodology, Writing – original draft.

Financial disclosure

None reported.

Conflict of interest

The authors declare no potential conflicts of interest.

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