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. 2025 Mar 25;192(4):45. doi: 10.1007/s10955-025-03437-6

A Non-inertial Model for Particle Aggregation Under Turbulence

Franco Flandoli 1,, Ruojun Huang 2
PMCID: PMC11937112  PMID: 40151767

Abstract

We consider an abstract non-inertial model of aggregation under the influence of a Gaussian white noise with prescribed space-covariance, and prove a formula for the mean collision rate R, per unit of time and volume. Specializing the abstract theory to a non-inertial model obtained by an inertial one, with physical constants, in the limit of infinitesimal relaxation time of the particles, and the white noise obtained as an approximation of a Gaussian noise with correlation time τη, up to approximations the formula reads RτηΔau2a·n2 where n is the particle number per unit of volume and Δau2 is the square-average of the increment of random velocity field u between points at distance a, the particle radius. If we choose the Kolmogorov time scale τηνε1/2 and we assume that a is in the dissipative range where Δau2ενa2, we get Saffman–Turner formula for the collision rate R.

Keywords: Particle coalescence, Turbulent fluid, Cell equation, Scaling limit, Saffman–Turner formula

Introduction

The Abstract Mathematical Model and the Main Results

We consider non-inertial particles x1Nt,...,xNNt in R3, subject to the dynamics

dxiNtdt=σtWϵ/ξxiNt,t+σ0dBitdt 1

where Bit are R3-valued independent Brownian motions, ξ,σ,σ0 are positive real numbers, Wx,t is a Gaussian R3-valued random field, Brownian in time

EWix,tWjy,s=Ci,jx-yts

for i,j=1,2,3, where the covariance matrix Cx is described in Sect. 1.2 below (hence tWx,t is a white noise in time) and Wϵ/ξx,t=Wξxϵ,t.

The parameter ϵ is linked to N by the relation

Nϵ=1 2

which describes a specific degree of sparseness of the system (finite mean free path, in the Brownian case), described below in Sect. 1.4.1. When we take the limit as N, hence ϵ0, the noise covariance is rescaled with ϵ; hence, mathematically speaking, there would be no reason to rescale the noise by ϵ/ξ instead of just ϵ (it is a matter of redefining the covariance). But ϵ, in the example described below in Sects. 1.31.4, is linked to the particle radius, hence the viewpoint in the scaling limit (2) is that the particle radius goes to zero meanwhile the number of particles goes to infinity (roughly speaking, particles occupy a bounded region, independently of N). The fact that also the noise scaling parameter ϵ/ξ goes to zero is a subsequent main assumption, not the structural link between the particles and the domain. We believe that for the interpretation of the results it is important to think that we discuss a scaling limit of a particle system, with a link (2) between number of particles and radius of interaction (a local interaction), in which there is an additional element, a turbulent fluid, with certain scaling properties related to the particle size.

When two particles xiN,xjN, ij, are sufficiently close, they may disappear, in a Markovian way, with rate

R0Nϵ-dθϵ-1xiN-xjN 3

where θ is a smooth compact support probability density function. Therefore ϵ is linked to the interaction radius of the particles. The positive number R0 modulates the pairwise interaction rate; perhaps the most interesting regime is when R0 is very large, case where the final average collision rate does not diverge to infinity with R0 but converges to finite value [thanks to the assumption (2)].

We prove that the empirical distribution of the particle system converges to a function fx,t, weak solution of the equation

tf=12σ2+σ02Δf-R¯f2. 4

The quantity R¯ is the key one to capture the average collision rate but it is important to notice, in connection with real applications, that what is usually called average collision rate, say R, in Physics, namely the number of collisions per unit of time and volume, is linked to R¯ by the formula

R=R¯Nn2 5

where N is the total number of particles in the system and n is the average number of particles per unit of volume. Indeed, f is the limit of a normalized empirical distribution, hence the Nf corresponds to n, then Eq. (4) gives us (up to the redistribution term 12σ2+σ02Δf), tn-R¯Nn2. In the abstract development of the theory we shall call R¯, sometimes, collision rate, but the correct transformation rule is (5).

In itself, Eq. (4) is a general form of quadratic limit equations, valid also under different scaling limits than 2 and different dimensions. For instance, we get the same equation if we perform a purely mean field limit with long range interaction and then send to zero the range in the final PDE. But the main feature of the scaling limit assumption 2, discovered by [13] (for the model above without the term σtWϵ/ξxiNt,t) is that R¯ is given by a non-trivial formula much different from the mean field case. One has

R¯=R0θx1+uxdx

where u is the unique vanishing at infinity solution of class C2 of the equation

σ02Δux+σ2divωξxux=R0θ1+u 6

where

ωx=I3-Cx.

Getting explicit information from this equation is not easy. But, in the limit as R0, one also has

R¯R¯=CapKθ,A

where Kθ is the support of θ and

Ax=σ02I3+σ2ωξx.

The capacity CapKθ,A is defined as the infimum of

R3ϕTxAxϕxdx

over all smooth functions ϕx, vanishing at infinity, that are larger than 1 on a neighbor of Kθ. This characterization is more suitable for quantitative information (see Sect. 1.5). The limit as R0 is a very natural one, corresponding to ask for a certain coalescence, when particles meet. In the sequel and in Sect. 1.5 we shall always only use this characterization.

It is not easy to summarize in a sentence the intuition behind this result. A key of interpretation could be that Eq. (4) contains the infinitesimal generator of the “1-particle motion”, while the differential operator on the left-hand-side of (6) is like the infinitesimal generator of the difference in position between two particles. Therefore Eq. (6) contains information about the mutual behavior of different particles.

With this remark, we may explain a deep fact that, at the beginning and with the wrong eye, may even look counter-intuitive. First, notice that minimizing a quadratic form like R3ϕTλ2I3ϕdx produces a result of the form Cλ2. Therefore the capacity CapKθ,A is (roughly speaking) linear in the size of A. Therefore, in the case of the matrix function Ax=σ02I3+σ2ωξx, it may look strange that it increases linearly with σ02, namely with the noise term σ0dBitdt, and not linearly with the covariance σ2Cξx, corresponding to the other noise term; it increases with the opposite, ωξx=I3-Cξx. The deep reason stands in the “two-particle motion” of the Eq. (1). Two different particles xiNt,xjNt, ij, are driven by two independent Brownian motions σ0dBitdt and σ0dBjtdt and by the “common noise” σtWϵ/ξx,t, just evaluated at the two positions xiNt,xjNt. If the correlation of the common noise at those positions is very small, it also behaves like two independent Brownian motions, hence its effect is similar to the one of σ0dBitdt and σ0dBjtdt. And indeed, ωξxI3. If the space-correlation of the common noise, on the contrary, was very strong, it should not contribute to change the distance of the two particles; and in this case ωξx0. Therefore it is ωξx, not Cξx, which should be directly proportional to the collision rate. In a sense, the term σ02I3 in Ax is there because of the independence of the “internal” Brownian motions of particles, which is like a common noise with infinitesimal space correlation.

In Eq. (4), on the contrary, we have the infinitesimal generator 12σ2+σ02Δ of one-particle motion, where Cξx|x=0 plays a role. Equation (4) describes the particle density, in a sense the probability that a single particle is here or there and alive, hence governed by the one-particle motion.

The motivation of the study of this paper comes from the physical theory of aggregation of particles in turbulent fluids, see for instance [1, 5, 7, 8, 2023, 26]. However, in such a theory, particles are inertial, inertia being quantified by means of the Stokes number St (defined as the ratio between the relaxation time of the particle over the relaxation time of a turbulent eddy). When inertia is large, particles feel turbulence like a light pollutant feels molecules and thus perform a Brownian motion with damping; more inertia, less collisions. On the other side of the “inertial scale of the particle”, when inertia is almost zero, particles move almost adhese to the fluid, which again leads to few collisions. It is only in the intermediate range, when inertia is still small-moderate but starts to show up, that we observe more collisions.

Our results, being based on a non-inertial model (but obtained from an inertial one by an approximation procedure, hence preserving most physical constants), meets necessarily only the case of small Stokes numbers; more precisely, the Stokes number formally disappears from the model and appears a link between two space-scales, the radius of the particle and the Kolmogorov scale. The final results will be expressed in these terms. One of the results, which shows the correctness of some approximations, is that we recover Saffman–Turner formula [25] in the case when the particle radius falls in the dissipation range of the fluid.

We complete the introduction by means of several subsections devoted mostly to physical interpretations of the model and of the results. First, we describe the covariance function Cx and the noise W above, Sect. 1.2. Then we describe the inertial model often considered in the literature, driven by a certain model of turbulent fluid, Sect. 1.3. In that section, we deviate from our main purpose and show briefly how Abrahamson theory arises, summary that may help to clarify that we have no chance to get such a result when we neglect inertia, see Subsect. 1.3.1. Then we describe how we derive, heuristically, a non-inertial model from the inertial one, Sect. 1.4. Finally, we interpret the main theoretical results of this paper (those summarized above), in the case of the non-inertial model with parameters ξ,σ,σ0 coming from the reduction from inertial to non-inertial, which contains some Physics; see Sect. 1.5.

Let us also stress that the limit (4) is deterministic in spite of the presence of an environmental noise. Systems with environmental noise attracted a lot of attention in recent years, in particle systems scaling limit, mean field games and other theories. Usually the macroscopic dynamics is stochastic, the environmental noise is not averaged out by the scaling limit, opposite to the case of independent noise on each particle; see for instance [10] for an example in aggregation phenomena. But here we assume that the environmental noise has a scaling structure in the number of particles such that, in the limit, it behaves like independent noise on each particle—still preserving the covariance structure in the cell equation, since it is an equation for the two-point motion! An example of similar result for point vortices was obtained in [11], inspired by a comment in [12].

Space Covariance and Noise

Let us start with the main building block (see for instance [19, Section 1.1] for more details). We assume to have a covariance matrix function C:R3R3×3 having Fourier transform

C^z=gzI3-zzz2

for a non-negative real valued function g bounded, integrable, smooth, depending only on z; here I3 is the identity matrix in R3. For technical reasons hopefully eliminable in future more advanced works, we assume C compact support, a property that can be translated into a property of analyticity and growth of g by a Paley–Wiener–Schwartz theorem. To this covariance matrix function C, it is associated a Gaussian vector valued process Wx,tR3, with divWx,t=0, that is Brownian in time and has space-covariance C: denoting by E the expected value with respect to the randomness,

EWix,tWjy,s=Ci,jx-yts.

Its time derivative tWx,t is a solenoidal vector valued white noise (formally speaking, the covariance of tWx,t is Cx-yδt-s).

One way to construct Wx,t from C, relevant for the mathematical analysis below and possibly for numerical simulations, is the following one. To C we associate the covariance operator C in the space Ls2R3,R3 of solenoidal vector fields on R3; this operator is positive selfadjoint and compact, hence it has a spectral decomposition Cv=k=0λkv,ekL2ek, vLs2R3,R3, where ekkN is a complete orthonormal system of Ls2R3,R3 and λk0 for every kN. Taken a sequence WktkN of independent scalar Brownian motions, we define

Wx,t=k=0λkekxWkt. 7

From the assumption on the Fourier transform of C, one can prove that xWx,t is an isotropic random field. In particular Cx is a function of x only; and one has C0=13gL1I3 where gL1=R3gxdx. We assume 13gL1=1, hence

C0=I3.

Inertial Model

Behind the non-inertial model of this paper there is an inertial one that we describe now. We use new notations, to avoid confusion.

Consider N particles in R3, with positions and velocities x1Nt,v1Nt,..., xNNt,vNNt, subject to a turbulent fluid by Stokes law:

dxiNtdt=viNtdviNtdt=-1τPviNtu(xiN(t),t)+uPτPdBitdt

where ux,t is a space-time stationary Gaussian vector random field, divergence free, with

Euix,tujy,s=e-t-sτηPijx-y

for i,j=1,2,3. With this first identity we have specified the relaxation time τη of the turbulent fluid. Then we want to specify, by a proper choice of Px, that the fluid is very correlated when x-yη, interpreted as Kolmogorov scale (below which dissipation dominates and the velocity field ux,t is smooth and mildly varying), then less and less correlated as x-y increases above η. One way, accepting moreover isotropy and other idealizations, is to assume

Px=uη2CLηx

where uη2 is a measure of the turbulent kinetic energy, Cx, ek,λkkN and Wx,t are as in the previous section and L is a macroscopic length scale. For simplicity (although it is not mandatory) we choose uη=ητη. If Kolmogorov scale is adopted, we may use the formulae η=ν3ε1/4, τη=νε1/2, uη=νε1/4, where ν is the kinematic viscosity of the fluid and ε the average dissipation energy rate.

Let us also introduce the matrix

Dx=uη2I3-CLηx.

One has

Dijx-y=uη2δij-Pijx-y=12Euix,t-uiy,tujx,t-ujy,t

so it is related to the second order structure function, in particular to the quantity Δx-yu2 anticipated in the Abstract, defined as the square-average of the increment of random velocity field u between points at distance x-y:

Δx-yu2=2TrDx-y.

One way to “realize” such field ux,t is by taking ux,t=uηZηx,t where Zηx,t is a stationary solution of

tZηx,t=-1τηZηx,t+1τηtWη/Lx,t.

One can easily show that

EZηix,tZηjy,s=e-t-sτηCi,jLηx-y. 8

The process Zηx,t has the same space-covariance as Wη/Lx,t, but it is stationary with time-correlation τη. We keep the notation η/L for Wη/L for comparison with Wϵ/ξ of Sect. 1.1, but drop L from all other notations like uη,τη,Zη for simplicity of notations.

This completes the description of the fluid velocity field. Concerning the particles, we have assumed in the model above that they have an inertial motion, with relaxation time τP and Stokes law -1τPviNt-uηZηxiNt,t linking them to the fluid motion, plus a very small “internal” noise uPτPdBitdt, phenomenologically taking into account particle geometry and internal degrees of freedom interacting with the environment in a complex way. Neglecting the fluid, the standard deviation of viNt would be proportional to uP, providing a phenomenological interpretation of the parameter uP; that we shall assume much smaller than all other contributions, just needed to mathematical reasons of “diffusion regularization”.

Particles have an interaction radius a: when the centers have distance less or equal to 2a, they undergo a collision which may produce coalescence of the particles, with a certain rate of collision (since we do not develop the full inertial theory, we skip the precise description of the rate). We assume to work in a fluid-particle regime where η and a are roughly comparable, maybe differing multiplicatively by a large or small length-scale ratio

ξ0=aη

but not being different infinitesimal orders when we take the limit a0. Therefore we assume ξ finite in the limit a0 and we can write the covariance CLηx of the noise in the form

Cξ0Lax.

This model, heuristically speaking, captures a number of properties of aggregation in turbulent fluids, the we describe in the following three cases 1iner,2iner,3iner (certainly non exhausting the important informations on the problem, but useful for the conceptualizations made later on).

1iner: Case τPτη. In this case, particles are almost adhese to the fluid and thus do not collide so often. This case is classically covered by Saffman–Turner law R¯a3 (up to constants involving the factor εν1/2) [25].

2iner: Case τPτη (up to finite constants). In this case, particles are less adhese, with some (but not large) inertia. More collisions are observed.

3iner: Case τPτη. In this case inertia dominates more and more as St increases; the behavior of particles is similar to independent Brownian motions, but with inertia. More inertia produces less collisions, hence the mean collision rate decreases with St. See Subsect. 1.3.1 below for additional informations (like Abrahamson law uηSt).

In this paper the condition τP1 is essential for the non-inertial approximation. Although a priori this could still allow us to consider τPτη, mathematically the information about τP is lost and our results do not cover such a case. Our paper is restricted to cases 1iner and 2iner.

However, even with the restriction to 1iner and 2iner, we do not fully recover the rapid increase of mean collision rate happening at some Stokes level, when we pass from 1iner to 2iner. Our theory gives only a relatively smooth transition from 1iner to 2iner. We presume it is due to the homogeneous Gaussian approximation of the velocity field, which lacks very important concentration effects of the density of particles.

The Case τPτη

Let us expand this case for comparison, case unfortunately not covered by the theory of this paper.

In this case, from the observational viewpoint of a particle, Zηx,t is like a white noise, say of the form τηdβit (see (10) below), hence the velocity viNt behaves like the solution of a damped Langevin equation with double noise:

dviNtdt=-1τPviNt+uητητPdβitdt+uPτPdBitdt.

For notational and conceptual simplicity, let us neglect the very small contribution uPτPdBitdt and rewrite the main coefficient as

dviNtdt=-1τPviNt+1τPuηStdβit 9

where the Stokes number is defined as

St=τPτη.

For large St, the inertia dominates the picture and collisions are not so frequent. To see this from Eq. (9), first let us assume that, for two different particles ii, βit and βjt are independent Brownian motions; this is a reasonable approximation, using the rough argument that a strong order between the time scales τPτη corresponds also to a strong order between the length scales aη. Hence, for the difference vijNt=viNt-vjNt we have exactly the same Eq. (9), just with a factor 2 in front of the noise. The standard deviation of a stationary solution is proportional to uηSt, hence (up to a multiplicative factor) we infer that the average collision rate is uηSt. This is the famous Abrahamson law [1]. Unfortunately, this law is lost in the non-inertial approximation below (in spite of several attempts; it seems an intrinsic weakness of the non-inertial model, for the obvious reason that it corresponds to an approximation around τP=0). Similarly, we lose the change of monotonicity which is known from theories and experiments, namely the decrease of the average collision rate in St for large St, after its increase for smaller St.

Reduction to a Non-inertial Model

The model above, suitable for numerical simulations, is too difficult at present for a rigorous mathematical investigation of the limit as N. We apply two simplifications, based on the fact that both τP and τη are very small in practical examples. We have a first approximation

Zηx,tdtτηtWη/Lx,t 10

coming from the equation

-τηtZηx,t=Zηx,t-τηtWη/Lx,t

as τη0; and a second approximation

viNtuηZηxiNt,t+uPτPdBitdt

coming from the equation

-τPdviNtdt=viNt-uηZηxiNt,t-uPτPdBitdt

as τP0. Inserting further the first approximation in the second one, we get

viNtuητηtWη/LxiNt,t+uPτPdBitdt.

Substituting this into the first equation we get

dxiNtdt=uητηtWη/LxiNt,t+uPτPdBitdt 11

which is a closed equation. Understanding the degree of these approximations and their relative importance is very difficult and much beyond the scope of this paper.

Concerning coalescence, first we oversimplify certain aspects of the problem (to focus on difficult others) and therefore assume that particles, after coalescence, “exit the system”. Namely we focus only on the number of particles of radius a and neglect not only what happens to the result of coalescence but also the important fact that, in reality, larger particles produced by coalescence usually may coalesce also with the smaller particles of radius a, contributing to the decrease of their number. But all these elements may be accounted for by the formalism of Smoluckowski equations, which we omit here. By the way, with the present simplified formalism the model may be applied to fragmentation too.

Concerning the collision rate between two particles xiN and xjN, ij, in the case of the non-inertial model a natural choice is the form

R0Na-3θ0a-1xiN-xjN 12

where R0 has dimension L3T-1 to give dimension T-1 to the rate. Here θ0 is a smooth non negative function, with θ0xdx=1, roughly equal to 34π in the ball B0,1, and equal to zero outside.

Before we close this section, let us mention heuristically what the previous non-inertial model may hope to tell us.

We mention this fact, along with the next one, to say that the general formula (14) or the previous ones of this section, more precise and rigorous, are only a first step based on an alternative methodology, still far from providing a good understanding of the small-to-moderate range of particle radius. Particles, just described by their position xiNt, are driven only by two Brownian sources, Wη/LxiNt,t and Bit. Thus xiNt behaves roughly like a Brownian motion (not precisely, since Wη/LxiNt,t depends on the particle position). Particles will collide, because of the random motion, with intensity increasing with the coefficient uητη (also with uPτP, but we assume uP much smaller than all other constants).

1non-iner: case aη. The process Wη/Lx,dt is very correlated below the Kolmogorov scale η, hence particles which have radius a much smaller than the Kolmogorov scale and are very close each other, feel the same random impulses, thus the random strength of Wη/Lx,t on them is very reduced, it does not put them closer; they travel parallely, so to speak. Therefore aggregation, which increases with uητη, is depleted if particles have a radius a much smaller than η.

2non-iner: case aη. Both obstructions discussed in 1non-iner are progressively relaxed when a increases to η. Therefore the mean collision rate should monotonically increase, when aη.

Let us now make precise the scaling between N and a chosen here, which is a critical issue. We separate it into a subsection for the reader’s convenience.

The Mean Free Path Regime

We assume the initial positions of the particles located in a unitary volume, approximately, so the same is true in a finite time interval approximately. Therefore, if we increase N, particles are more packed together, not just distributed in a larger volume; and their radius a is assumed to go to zero, if we increase N towards infinity, to get a sharp mathematical result. The link between N and a will be a finite number (finite in the limit when N and a0).

Na=ρ0. 13

Here ρ0 is a given positive number with dimension L: It is a “volume-occupation-constant”: the volume occupied by the balls of radius a centered at the particle positions is

volumeofparticles4π3Na3=4π3ρ0a2

hence the volume of particles linearly increases with ρ0.

Since a is small, this volume is very small, hence we are talking about a very sparse regime. The intuition then is of a very sparse collection of droplets. However, they perform, roughly speaking, Brownian motions (mostly due to the turbulent contribution uητηtWη/LxiNt,t), hence each one of their centers explores in unitary time a subset of R3 which has Hausdorff dimension 2 (with 2-dimensional Hausdorff measure zero). Hence, a ball of radius a centered at such a point, explores a set AR3 (called the Brownian sausage) having volume roughly of size a, up to multiplication by the parameters of the Brownian motion. During the excursion performed in a unit of time, the particle meets all particles that (with their radius) intersect A. If the particles are roughly uniformly distributed, then the number of particles which intersect A is of order N·Vol(A), namely Na, which is a finite number ρ0. This implies that each particle has a finite number of encounters in the unit of time. This is the so-called mean free path regime.

This is the only regime where we can find non trivial limit results. Indeed, when Na we have a mean field result, since each particle would meet infinitely many others in a unit of time; one can show that the result is simply

R¯=R0

which is a trivial and physically wrong result. On the contrary, for Na0, we would not observe sufficient interactions in the scaling limit; the average collision rate R¯ would vanish.

Therefore we investigate a non-mean-field regime, and the mathematical correction in the final formulae coming from this choice is essential.

Application of Our Results and Their Physical Interpretation

Conversion of the Notations

Let us first summarize the notation of the concrete example of Sect. 1.4 in comparison with the abstract notations of Sect. 1.1. The concrete dynamics of particles is given by equation (11), the rate of collision by (12) and the scaling regime by (13). In the abstract formulation of Sect. 1.1 the dynamics is given by (1), the rate of collision by (3) and the scaling by (2). Therefore the conversion table is (on the left the abstract notations, on the right those of the concrete example:

ϵ=aρ0θx=ρ0-3θ0ρ0-1xσ=uητησ0=uPτPξ=Lρ0aη

and recall

Px=uη2CLηx=uη2Cξ0LaxDx=uη2I3-CLηxR=R¯Nn2

(the first identity comes from comparison of the scaling limit assumption; then the second identity from comparison of the collision rates; the last identity is chosen in order to have Wϵ/ξ=Wη/L, recall the definition Wϵ/ξx,t=Wξϵx,t from Sect. 1.1 and Wη/Lx,t=WLηx,t from Sect. 1.4).

The Result in the Notations of Sect. 1.4

The normalized empirical measure of the particle system converges to a density f satisfying

tf=12uη2τη+uP2τPΔf-R¯f2

where

R¯=R0ρ0-3θ0ρ0-1x1+uxdx

where u is the unique vanishing at infinity solution of class C2 of the equation

uP2τPΔux+uη2τηdivI3-CLρ0aηxux=R0ρ0-3θ0ρ0-1x1+u

namely

uP2τPΔux+τηdivDaρ0xux=R0ρ0-3θ0ρ0-1x1+u.

In the limit as R0, one has

R¯R¯=CapKθ0ρ0-1·,A=CapB0,ρ0,A

where Kθ0ρ0-1·=B0,ρ0 is the support of θ0ρ0-1·, A is the matrix function Ax=uP2τPI3+τηDaρ0x and the capacity CapB0,ρ0,A is defined as the infimum of R3ϕTxAxϕxdx over all smooth functions ϕx, vanishing at infinity, that are larger than 1 on a neighbor of B0,ρ0.

A very heuristic computation in spherical coordinates, for the simplified example of minimizing B0,ρ0cϕTxI3ϕxdx over all smooth functions ϕx, vanishing at infinity, equal to 1 on B0,ρ0, shows that the minimizer is not so different from the radial function linearly decaying to zero on rρ0,2ρ0, with derivative modulus 1ρ0. The minimal value is roughly equal to ρ0, up to a constant (this is the well known result on the electric capacity of a sphere). If, in place of Ax=I3 we take a slowly varying function with radial symmetry, a rough approximation of the infimum is 13TrAρ0ρ0, since A matters only when rρ0,2ρ0. Therefore, the infimum in our case of interest can be approximated by

13TrAρ0ρ0=uP2τPρ0+τη13TrDaρ0=uP2τPρ0+τη16Δau2ρ0

that (to simplify the formulae) we replace by

τηΔau2ρ0

since uP2 is very small and we have also missed other multiplicative constants like 16.

Therefore, taking into account R=R¯Nn2 and Na=ρ0, we get

RτηΔau2a·n2 14

as stated in the Abstract. Then, in particular, if we accept Kolmogorov time scale τηνε1/2 and we assume that a is in the dissipative range where

Δau2u2a2=ενa2

(because of the balance relation νu2=ε), we get Saffman–Turner formula

Rνε1/2ενa2a·n2=εν1/2a3·n2.

The Saffman–Turner regime was already well accepted in the Physical literature, hence we just confirm the result in a more complex way than the original paper [25]. Part of our procedure is rigorous, but many steps were hand waving approximations (very reasonable), hence we cannot claim that we have rigorously proved Saffman–Turner result from first principle. We have only provided an alternative derivation.

The final formula (14), besides being correct in the dissipation range, provides a new view on the behavior for slightly larger a. We should however remember that we took a limit as τP0, hence larger a compared to η are meaningful only in few physical examples, precisely when the density of a particle in much less than the density of the fluid, which is not true for rain droplets in air or small dust clusters in star dust; maybe it may find more applications in fragmentation processes. If τP0 by a is in the inertial range, where

Δau2ε2/3a2/3

according to K41 theory (otherwise one should include intermittent corrections) one get (with the same arguments above)

Rν1/2ε1/6a5/3·n2

which is not a common result and not of easy interpretation. More generally, even if we do not use the Kolmogorov scaling law of structure function, it is clear that Δau2, which starts as a2 for very small a, tends to saturate for larger a, providing an “S-shape”. This is very reasonable. It is a monotone behavior with saturation. There is no chance however to see changes of monotonicity, with the given approximations.

Remark 1

Even if limited to small Stokes numbers, in principle it should be possible to incorporate in a precise mathematical model some ingredient which produces particle concentration, a phenomenon that is observed and is among those responsible for a strong increase of collision rate, when certain parameters increase with respect to Saffman–Turner regime. This remains an open problem in our framework, perhaps the most interesting one. See [4] for results in this direction.

Statement of Main Result

In this section, we start by recapping our model with additional details (that were omitted in the Introduction due to their technical nature), and then we state our main Theorem 6.

About the covariance function C(x), recall that by construction this function is radially symmetric, C(0)=I3 and ω(x)=I3-C(x) is nonnegative definite. The latter property is due to ω(x)=12kN(ek(0)-ek(x))2. We also have

C(x-y)=kNλkekxλkeky, 15

where we recall that our Gaussian random field W(xdt) can be written as a series (7). Henceforth, we will write

Cϵ(x)=C(xϵ),ekϵ(x)=ek(xϵ).

By the series representation of Wϵ/ξ(x,dt), we can rewrite the dynamics of the particle system (1) as

dxiN(t)=σkNλkekϵξxiN(t)dWk(t)+σ0dBi(t),iN(t), 16

where denotes Stratonovich integration. We make this choice in accordance with Wong-Zakai principle. Due to ekϵ being divergence free, it turns out that in our setting it coincides with Itô integration, since the Stratonovich-to-Itô corrector is zero. N(t){1,2,...,N}=N(0) is the (random) index set of active particles at time t.

Let us formally state our model: Given a probability space (Ω,F,P), for every NN, we consider a system of initially N particles evolving in R3, whose positions xi(0) at time t=0 are independent and identically distributed (i.i.d) with probability density f0(x). Particles are enumerated from i=1,2,...,N at the beginning, and their indices are fixed once and for all. As long as a particle i{1,2,...,N} is alive, its spatial position xiN(t)R3 follows (16). Any pair of distinct particles (ij), ij, may coalesce and both disappear, with a stochastic rate (3) which we denote by rijN. When a particle is no longer active, we assign it a “cemetery” state which is absorbing, and thus the cardinality of active particles in the system at t>0 are less or equal than N and non-increasing in time.

We impose the following assumption on the initial density f0(x) of an individual particle.

Condition 2

There exist finite constants L0 and Γ such that f0 is supported in (the Euclidean ball of radius L0 around the origin) B(0,L0)R3, and f0(x)Γ for all xR3. In particular, f0L1L(R3;R+).

The probability space is endowed with the canonical filtration

Gt:=σ{Wk(s)}kN,{Bi(s)}i=1,st,{xi(0)}i=1,t0.

Denoting by ζ a generic configuration of the particle system, i.e. ζ=(x1,x2,...,xN)R3{}N, and by ζtN the configuration of the particle system at time t, (ζtN)t0 is a Markov process with infinitesimal generator

LNF(ζ)=LDNF(ζ)+LJNF(ζ) 17
LDNF(ζ):=12σ2kNi,jN(ζ)λk2ekϵ(ξxi)·xi(ekϵ(ξxj)xjF(ζ))+12σ02iN(ζ)ΔxiF(ζ)=12σ2kNi,jN(ζ)λk2xi·(ekϵ(ξxi)ekϵ(ξxj)xjF(ζ))+12σ02iN(ζ)ΔxiF(ζ) 18
=12σ2i,jN(ζ)xi·(Cϵ(ξ(xi-xj))xjF(ζ))+12σ02iN(ζ)ΔxiF(ζ)LJNF(ζ):=12iN(ζ)jN(ζ):jirijNF(ζ-ij)-F(ζ). 19

Here, F:R3{}NR is a functional on the configuration space, xi denotes partial gradient with respect to variable xiR3 and similarly xi· denotes partial divergence. We denote the index set of active particles in ζ by

N(ζ):={i:xiζ,xi}{1,2,...,N},

whereas ζ-ij is a configuration obtained from ζ by setting its i-th and j-th slots to , and keeping other slots unchanged. The 1/2 in (19) is due to double counting in the double sum of an annihilation event. We have used the fact that ekϵ(x) are divergence free when calculating LDN at step (18). Our assumptions actually imply [see (49)] that LDNF(ζ) can be equivalently written as non-divergence form

LDNF(ζ)=12σ2i,jN(ζ)TrCϵ(ξ(xi-xj))xixj2F(ζ)+12σ02iN(ζ)ΔxiF(ζ).

Remark 3

LDN accounts for the diffusion part of the dynamics, describing the diffusive movement of the particles between two consecutive annihilation events. The annihilation events happen at isolated times, which are sudden jumps in the particle configuration {ζtN}t0, and are described by the jump part of the generator LJN. While the form of LDN follows by an application of Itô’s formula to (16), the jump operator (19) can be written in terms of the jump rates rijN in a way that is familiar in interacting particle systems [16]. The total generator LN is then the sum of the two. The Itô–Dynkin formula states that tF(ζtN)-F(ζ0N)-0tLNF(ζsN)ds is a Gt-martinagle. Naturally this martingale can be decomposed into two parts, one due to diffusion and the other one due to jump.

For the kernel function θ:R3R+ that regulates the coalescence rate (3), it is enough to assume that it is Hölder continuous Cα(R3) for some α(0,1), compactly supported in the unit ball B(0,1)R3 with θ(x)=θ(-x), R3θ(x)dx=1, and θ(0)=0. Throughout, we denote its rescaled version by

θϵ(x):=ϵ-3θ(ϵ-1x),

which has compact support in a ball B(0,ϵ) of radius ϵ. With this notation, the coalescence rate can be written as

rijN=R0Nθϵ(xi-xj). 20

Denote the process of empirical measure of the active particles by

μtN(dx):=1NiN(ζtN)δxiN(t)(dx)D[0,);M+,1(R3),t0, 21

where M+,1(R3) denotes the space of sub-probability measures over R3 endowed with the weak topology, and D[0,);M+,1(R3) denotes the Skorohod space of càdlàg processes taking values in M+,1(R3) endowed with the Skorohod topology.

We introduce the limiting pde with unknown f(t,x):[0,T]×R3R+:

tf(t,x)=12σ02+σ2Δf(t,x)-R¯f(t,x)2,f(0,x)=f0(x), 22

where R¯R+ is given by

R¯=R3R0θ(x)1+u(x)dx. 23

and u:R3R solves the auxiliary pde

σ02Δu(x)+σ2·(ω(ξx)u(x))=R0θ(x)(1+u(x)). 24

We will comment later that (24) has a C2,α(R3) solution that satisfies u(x)[-1,0] for all xR3, see (74) and Lemma 15, and is unique under the constraint that |u(x)|0 as |x|.

Remark 4

An alternative expression for R¯ is

R¯:=σ02+σ2R3Δu(x)dx, 25

and it is in this form that our proof will yield. It can be seen from integration by parts in (24); indeed since ω(x)=I3-C(x) and C has compact support, we have

(σ02+σ2)R3Δu(x)dx=σ2R3·(C(ξx)u(x))dx+R3R0θ(x)(1+u(x))dx=R3R0θ(x)(1+u(x))dx.

Solutions to (22) are understood in the following weak sense.

Definition 5

Assume f0L1L(R3;R+). We say that fL[0,T];L1(R3;R+) is a weak solution to (22) if

R3f(t,x)ϕ(x)dx=R3f0(x)ϕ(x)dx+12(σ02+σ2)0tR3f(s,x)Δϕ(x)dxds-R¯0tR3ϕ(x)f(s,x)2dxds

holds for any t[0,T] and all test function ϕCc2(R3).

One can show that such weak solutions are unique, for a proof in a very similar context see [9, Section 3]. The main result of this article is as follows.

Theorem 6

Assume that the initial density f0 satisfies Condition 2 and the scaling relation (2) holds. Then for every T<, the empirical measure (μtN(dx))t[0,T] (21) of the particle system converges in probability as N, in the space D([0,T];M+,1(R3)), to a limit {μ¯t(dx)}t[0,T]. The limit is deterministic, absolutely continuous with respect to Lebesgue measure for every t, i.e. μ¯t(dx)=f(t,x)dx, where the density f(tx) is the unique weak solution of the pde (22), in the sense of Definition 5.

This result, in particular the form of the average coalescence rate R¯, is a variant of [13]. Compared to that work, we have simplified the model by focusing only on particles of the same mass, but we have introduced a random environment to model the turbulent fluid. In our previous model [10] in a random environment, we have chosen the dense particle scaling ϵ3N=1 which, in the framework studied here, would lead to R¯=R0.

Sketch of Proof

Since the proof of our main result is somewhat technical, we will first provide a general sketch in this section.

Our goal is to show that the empirical measure process, (μtN(dx))t[0,T], which is a measure-valued stochastic process, converges to the unique weak solution of the pde (22). Granted that we have relative compactness of this sequence, we need to show that any subsequential limit is a weak solution of the pde. Since weak formulation of the pde is in terms of integration against test functions ϕ, it is natural and standard to look at the real-valued stochastic process

μtN,ϕ

for any fixed ϕ, and show that asymptotically it satisfies the weak formulation of the pde with test function ϕ.

At the level of fixed N, by applying Itô–Dynkin formula to μtN,ϕ, we can readily get that it satisfies a so-called semimartingale equation. Such equation is still random, with fluctuation terms present, and it only partially looks like the limit pde. In Sect. 3, we will show that the fluctuation terms (they are martingales) vanish in the limit N in a probabilistic sense, so that the limit is deterministic and not a stochastic pde. We will also see that all the other terms, but one of them (31), are in the form of the empirical measure μtN integrated against certain test function. These are terms linear in the empirical measure, and will converge to corresponding linear terms of the pde, just because the empirical measure converges weakly (along subsequences).

There is however one term (31) which is not linear in the empirical measure. The desired limit for this term is quadratic in the pde solution, with a particular multiplicative constant R¯, but it is not at all clear if and how this stochastic term will converge. This difficulty is common in the theory of interacting particle systems, see [16], namely the main work is always concentrated on proving that the nonlinear terms converge. For particle systems evolving on lattices, there are methods bearing the name of “replacement lemma” that deal with such issues, but that requires detailed knowledge of invariant measures of the particle system. Lacking such knowledge in our setting of interacting diffusions in the continuum, we instead rely on a very special technique due to Hammond–Rezakhanlou [13]. We call it Itô–Tanaka trick, with roots in Tanaka’s formula in stochastic calculus; this is developed in Sects. 46 of our paper. The key statement to prove here is Proposition 11, which directly dictates the form of the multiplicative constant R¯ in the limit pde, see the argument following it, (43). However, we do not have enough intuitive or physical understanding of what this proposition means. Vaguely, we may say that it is also a sort of replacement lemma. From Proposition 11, it is relatively easy to deduce the desired convergence of the nonlinear stochastic term, because it allows to disentangle ϵ and N by introducing the auxiliary variable z.

The remaining effort is thus concentrated on proving Proposition 11. Let us look back at the nonlinear stochastic term (31), which is in the form of an averaged double-sum involving θϵ(xiN(t)-xjN(t)). Recall that ϵ0 very fast as N, and θϵ is approaching the Dirac delta. Furthermore, the argument of θϵ is the two-point motion that is responsible for coalesence. Due to the singular nature of θϵ, this expression is highly unstable. The idea of Itô–Tanaka trick is that instead of working with θϵ, we can equivalently work with a much more regular function. Note that regularity here should be understood as not for fixed ϵ, but as ϵ0. In Sect. 4, we construct an auxiliary function uϵ, solution of a carefully-chosen, uniformly elliptic, second-order, divergence form pde (35) (the “cell equation”), whose right-hand side contains θϵ. As a result, uϵ is “two derivatives” more regular than θϵ and not a singular function at all. By rescaling the cell equation, we can obtain an ϵ-independent elliptic equation (36) that can be solved using Green’s function. Here, the capacity scaling relation (2) between ϵ and N plays an important role in correctly rescaling the cell equation. Then, in Sect. 5 we consider a new averaged double-sum process (48), similar to the nonlinear term (31) we started with, but now involving the more regular function uϵ. By applying the Itô–Dynkin formula to this new process, and performing substitution using the cell equation, we obtain an identity in which the pre-limit of Proposition 11 appears, together with many other (presumably minor) terms. Now, to show Proposition 11, it is enough to control all these minor terms, since we have an identity in this manouvre. More precisely, we need to prove that all the minor terms are negligible in suitable probabilistic sense. Since they all involve uϵ and uϵ, for which we have enough control through Green’s functions, we can prove their negligibility which is the content of Sect. 6.

The rest of the article is organized as follows. In Sect. 3 we write the equation satisfied by the empirical measure of the particle system, and identify the nonlinear term whose convergence is the main issue. In Sects. 4 and 5 we introduce the cell equation and the Itô–Tanaka trick, main ingredients in the proof of Theorem 6. In Sect. 6 we show the negligibility of all the minor terms coming out of Itô–Tanaka trick. We omit the proof of tightness of the particle system, the existence of limit density and the uniqueness of the limit pde, as they are similar to arguments detailed in our previous works [9, 10, 14]. In Sect. 7 we tie our main theorem with certain facts in potential theory, so as to deduce the dependence of coalesence efficiency on ξ.

Equation Satisfied by the Empirical Measure

Now, we are ready to derive a semimartingale equation for the empirical measure process (21). Fixing T< and any ϕCc2(R3), we apply the Itô–Dynkin formula (with infinitesimal generator given in (17)) to the functional of configurations

F1(ζtN):=μtN,ϕ=1NiN(ζtN)ϕxiN(t),t0,

where we use the shorthand μ,f:=fdμ for pairings between a function and a measure, and we obtain that

μTN,ϕ-μ0N,ϕ 26
=0T1Nσ22iN(ζtN)·(Cϵ(ξ(xiN(t)-xiN(t)))ϕ(xiN(t)))dt 27
+0T1Nσ022iN(ζtN)Δϕ(xiN(t))dt 28
+0T1NσiN(ζtN)ϕxiN(t)·kNλkekϵ(ξxiN(t))dWk(t) 29
+0T1Nσ0iN(ζtN)ϕ(xiN(t))·dBi(t) 30
-0T12R0N2iN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))[ϕ(xiN(t))+ϕ(xjN(t))]dt+MJN(T), 31

where, while (29) and (30) are martinagles associated with diffusion dynamics, MJN(t) is a martingale associated with jumps, that we do not write out explicitly. Since Cϵ(0)=I3, we have

1Nσ22iN(ζtN)·(Cϵ(ξ(xiN(t)-xiN(t)))ϕ(xiN(t)))=σ22μtN,Δϕ.

Also, since we assumed that θ is symmetric, we have

12R0N2iN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))[ϕ(xiN(t))+ϕ(xjN(t))]=R0N2iN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))ϕ(xiN(t)).

It turns out that the convergence of the linear terms (26)–(28) is not an issue (see e.g. [10, 14]), and we will prove in Lemmas 9 and 10 that the martingale terms vanish, as N. The only difficulty is the convergence of the nonlinear term (31).

We introduce a tool that will be useful also for later sections. Consider on the same filtered probability space (Ω,F,{Gt}t0,P) an anxiliary “free” particle system yiϵ(t), iN which start at t=0 with the same initial condition as the true system yiϵ(0)=xi(0), perform the same sde (16) driven by the same collections of Brownian motions {Wk(t)}kN and {Bi(t)}i=1, but here the particles do not interact/annihilate, i.e.

dyiϵ(t)=σkNλkekϵξyiϵ(t)dWk(t)+σ0dBi(t),t0,i=1,2,... 32

with infinite life time. Note that yiϵ still depends on ϵ.

Since the initial conditions and dynamics of the true and auxiliary systems agree, there is an obvious coupling between them under which whenever xiN(t) is alive at time t, its trajectory on the time interval [0, t] coincides with that of yiϵ(t), for every i=1,2,..,N. By construction, the auxiliary system is exchangeable, meaning that the law of (yi1ϵ(t),yi2ϵ(t),...,yiLϵ(t))t0 is unchanged under any permutation of the indices (i1,i2,...,iL) and any finite LN. Now consider a pair (y1ϵ(t),y2ϵ(t)) and it is known classically that it has a joint density ft12,ϵ(y1,y2) that evolves by the forward Kolmogorov equation (or Fokker–Planck equation)

tft12,ϵ(y_)=Lϵft12,ϵ(y_),f012,ϵ(y_)=f0(y1)f0(y2),y_:=(y1,y2)(R3)2,

where Lϵ is a uniformly negative divergence-form operator that acts on functions g:(R3)2R by

Lϵg(y_)=y_·(Aϵ(y_)y_)

where

y_:=(y1,y2),Aϵ(y_):=12σ02I6+12σ2I3Cϵ(ξ(y2-y1))Cϵ(ξ(y1-y2))I3M6.

Although Lϵ depends on ϵ, its matrix coefficient Aϵ are measurable and bounded uniformly in ϵ. Indeed, Cϵ(x)=C(x/ϵ) and C(x) is assumed smooth and compactly supported. By Aronson’s estimate [3, Theorem 1] for fundamental solutions of uniformly parabolic second-order divergence-form operator with measurable bounded coefficients, there exist some finite constants Ki=Kiσ0,σ,CL (depending only on the bounds on the coefficients, hence independent of ϵ), i=1,2, such that

qϵ(t;y_0,y_)K1(2πK2t)3e-|y_-y_0|22K2t,

where qϵ(t;y_0,y_) denotes the fundamental solution of t-Lϵ, and CL:=maxα,β=13CαβL(R3).

This allows to derive exponential tail bounds on ft12,ϵ. Indeed, let Yt denote a Gaussian random vector on (R3)2 with density 1(2πK2t)3e-|y_|22K2t, then

ft12,ϵ(y_)=(R3)2f012,ϵ(y_0)qϵ(t;y_0,y_)dy_0(R3)2f012,ϵ(y_0)K1(2πK2t)3e-|y_-y_0|22K2tdy_0=K1Ef012,ϵ(y_-Yt),

where E acts on the random variable Yt. Since f012,ϵ(y_)=f0(y1)f0(y2) which is uniformly bounded by Γ2 and compactly supported in B(0,2L0) by Condition 2, we have

ft12,ϵ(y_)K1Ef012,ϵ(y_-Yt)K1Γ2P|y_-Yt|2L0K1Γ2P|Yt||y_|-2L02K1Γ2e-|y_|-2L0+24dK2tKe-|y_|2/K,

for any t[0,T] and some finite constant K that depends only on K1,K2,Γ,T,L0, where we used the tail bound for a Gaussian vector.

A similar argument can also show that the joint density ft12...,ϵ(y1,...,y) of an -tuple of free particles (y1ϵ(t),...,yϵ(t)), for any fixed N, also satisfies an exponential decay, uniformly for t[0,T] and ϵ. We will only use =1,2,3,4 in the sequel. That is, we have proven that

Proposition 7

There exists a finite constant C0=C0σ0,σ,CL,Γ,T,L0, such that for any t[0,T] and ϵ(0,1), we have

ft1...,ϵ(y1,y2,...,y)C0e-|y1|2+...+|y|2C0, 33

for =1,2,3,4.

We proceed to show next that the two martingale terms associated with diffusion vanish in L2(P).

Lemma 8

E0T1NiN(ζtN)ϕxiN(t)·kNλkekϵ(xiN(t))dWk(t)2=ON-1+Oϵ3.

Proof

By Itô isometry and the independence between Wk(t), kN,

E0T1NiN(ζtN)ϕxiN(t)·kNλkekϵ(ξxiN(t))dWk(t)2=E0T1N2kNiN(ζtN)ϕxiN(t)·λkekϵ(ξxiN(t))2dt=E0T1N2kNi,jN(ζtN)ϕ(xiN(t))Tλkekϵ(ξxiN(t))λkekϵ(ξxjN(t))ϕ(xjN(t))dt=E0T1N2i,jN(ζtN)ϕ(xiN(t))TCϵ(ξ(xiN(t)-xjN(t)))ϕ(xjN(t))dtTNϕC12+E0T9N2ijN(ζtN)ϕC12Cϵ(ξ(xiN(t)-xjN(t)))dt,

where for a 3×3 matrix A we denote

A:=maxα,β=13|Aαβ|. 34

Recall the auxiliary free particle system (32) just introduced, which is exchangeable in law and coupled to xiN for iN(ζtN) in a natural way, hence we have the bound

E0T1N2i,jN(ζtN)Cϵ(ξ(xiN(t)-xjN(t)))dtE0T1N2ij=1NCϵ(ξ(yiϵ(t)-yjϵ(t)))dtE0TCϵξ(y1ϵ(t)-y2ϵ(t))dt.

By the tail bound on the pair density (33),

T(R3)2Cϵ-1ξ(y1-y2)C0e-|y1|2+|y2|2C0dy1dy2dt=C0TR3Cϵ-1ξy1dy1R3e-|y2|2C0dy2ϵ3R3Cξydy=O(ϵ3),

where the factor ϵ3 comes from change of variables, and the last integral is finite since every component of C is smooth with compact support (hence bounded). This completes the proof.

Lemma 9

E0T1Nσ0iN(ζtN)ϕ(xiN(t))·dBi(t)2=ON-1.

Proof

By Itô isometry, we have

E0T1Nσ0iN(ζtN)ϕ(xiN(t))·dBi(t)2=EiN(ζtN)0T1N2σ02|ϕ(xiN(t))|2dtTσ02N-2ϕC12E|N(η(t))|Tσ02N-1ϕC12,

since |N(η(t))||N(η(0))|=N.

We show next that the martinagle associated with jumps also vanishes in L2(P).

Lemma 10

E|MJN(T)|2=ON-1.

Proof

By the carré-du-champ formula cf. [6, Proposition 8.7], we have

E|MJN(T)|2E0TR02NiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))1N2[ϕ(xiN(t))+ϕ(xjN(t))]2dtE0T2R0ϕL2N3iN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))dt.

On the other hand, we consider the functional F2(ζtN)=|N(ζtN)|, apply the generator (17) to it, and we get

E|N(ηTN)|-E|N(η0N)|=-E20TR02NiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))dt.

Indeed, the diffusion part of the generator does not affect F2(ζtN), only the jump part does. It yields that

E0TR0NiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))dtE|N(η0)|=N.

Therefore we have E|MJN(T)|22ϕL2N-1.

The Cell Problem and the Nonlinear Term

The remaining task is to prove the convergence of the nonlinear term (31). We aim to establish a form of local equilibrium as in Proposition 11 below. For this purpose, we introduce for every fixed ϵ(0,1) an auxiliary equation uϵ(x):R3R (so-called cell problem in the terminology of homogenization):

σ02Δuϵ(x)+σ2·(ω(ξxϵ)uϵx)=R0θϵx(1+uϵxN), 35

which is a rescaling of an ϵ-independent equation (36). Let u(x):R3R be a particular C2,α(R3)-solution given in (74), of

σ02Δu(x)+σ2·(ω(ξx)u(x))=R0θ(x)(1+u(x)), 36

then it can be readily checked, using N=ϵ-1, that the rescaled function

uϵ(x)=ϵ-1uxϵ 37

solves (35). This is the analogous cell equation as used in [13, Eq. (1.7)].

The following proposition will be proved in Sect. 5 using the Itô–Tanaka trick. Note that we have added an extra test function ψ, with respect to (31), to have more localization. It is actually without loss of generality. Indeed, θϵ(x) is compactly supported in B(0,ϵ) and from (35) it can be seen (45) that Δuϵ(x) is compactly supported in B(0,ϵ(1ξ-1)), and we can always assume that |z|1/2, which implies that each summand

R0θϵ(xiN(t)-xjN(t))-σ02+σ2Δuϵ(xiN(t)-xjN(t)+z)

is zero unless |xiN(t)-xjN(t)|1/2+ϵ(1ξ). Since xiN(t)supp(ϕ), this forces xjN(t) to be inside some other compact set K=K(ϕ,ξ)R3. Hence we can choose a compactly supported test function ψ that is identically 1 on K and decays smoothly to 0 outside. Such a ψ(xjN(t)) does not alter (38).

Proposition 11

Let uϵ(x)C2,α(R3) be given by (37) and ϕ,ψCc2(R3) be two test functions, then we have

lim|z|0lim supNE|0T1N2i,jN(ζtN):ji[R0θϵ(xiN(t)-xjN(t))-σ02+σ2Δuϵ(xiN(t)-xjN(t)+z)]ϕ(xiN(t))ψ(xjN(t))dt|=0. 38

We proceed directly to showing that Proposition 11 yields the convergence of the nonlinear term, as in [13, pp. 42–43]. Firstly, we note that we can add the terms with indices i=j into the double summation of (38), without changing its conclusion. Indeed, there are at most N diagonal terms. With θϵ(0)=0, |Δuϵ(z)||z|-3 provided |z|2ϵ by (77), and a factor of 1/N2 in front, we see that as ϵ0 first (and z fixed), the whole contribution of

1N2iN(ζtN)|R0θϵ(xiN(t)-xiN(t))-σ02+σ2Δuϵ(xiN(t)-xiN(t)+z)|N-1|z|-30.

Hence, we can start our subsequent argument with a version of (38) with full double summation:

lim|z|0lim supNE|0T1N2i,jN(ζtN)[R0θϵ(xiN(t)-xjN(t))-σ02+σ2Δuϵ(xiN(t)-xjN(t)+z)]ϕ(xiN(t))ψ(xjN(t))dt|=0. 39

Denote by ζ:R3R+ a fixed smooth probability density function with compact support in B(0, 1) and denote ζδ(x):=δ-3ζ(x/δ) for δ>0. Then, (39) yields that

0TR0θϵ(x1-x2)ϕ(x1)ψ(x2),μtN(dx1)μtN(x2)dt=0Tσ02+σ2(R3)2Δuϵ(x1-x2-z1+z2)ϕ(x1)ψ(x2),μtN(dx1)μtN(dx2)ζδ(z1)ζδ(z2)dz1dz2dt+Err(δ,ϵ), 40

where Err(δ,ϵ) is a stochastic error that vanishes in the following limit:

limδ0lim supϵ0E|Err(δ,ϵ)|=0, 41

and may change from line to line in the sequel. In (40), we have introduced two averaging on variable z1,z2 with compact supports in B(0,δ), hence in view of (39), the rate of convergence of the error term (41) is uniformly controlled by δ.

Next, we shift the argument of ϕ(x1) and ψ(x2) on the right-hand side of (40) to ϕ(x1-z1) and ψ(x2-z2) respectively, causing an error of O(δ), since z1,z2 are in the compact support of the function ζδ. Then, we perform a change of variable w1=x1-z1, w2=x2-z2, and the right-hand side of (40) (in the sequel written without the time integral, to ease notation) now becomes

σ02+σ2(R3)2Δuϵ(w1-w2)ϕ(w1)ψ(w2)ζδ(x1-w1)ζδ(x2-w2),μtN(dx1)μtN(x2)dw1dw2+Err(δ,ϵ). 42

Next, we shift the argument of ζδ(x2-w2) to ζδ(x2-w1) in (42), causing an error on the order of |w2-w1|δ-4 by the mean-value theorem and |ζδ|δ-4, and the argument of ψ(w2) to ψ(w1), causing an error on the order of |w2-w1|, and (42) is equal to

=σ02+σ2(R3)2Δuϵ(w1-w2)ϕ(w1)ψ(w1)ζδ(x1-w1)ζδ(x2-w1),μtN(dx1)μtN(x2)dw1dw2+Err(δ,ϵ)+Err1(δ,ϵ), 43

with an additional error term Err1 that we need to show is also negligible. Indeed, recalling that μtN is a sub-probability, we firstly have

|Err1(δ,ϵ)|σ02+σ2(R3)2|Δuϵ(w1-w2)||ϕ(w1)||ψ(w2)||w1-w2|δ-7dw1dw2+σ02+σ2(R3)2|Δuϵ(w1-w2)||ϕ(w1)||w1-w2|dw1dw2. 44

Then, note by the cell equation (35) and since ω(x)=I3-C¯(x), we have

σ02+σ2Δuϵ(x)=σ2·(Cϵ(ξx)uϵx)+R0θϵx(1+uϵxN). 45

Since Cϵ and θϵ are compactly supported in B(0,ϵ/ξ) and B(0,ϵ) respectively, we have Δuϵ compactly supported in B(0,ϵ(1ξ-1)). Hence, recalling that Δuϵ(x)=ϵ-3Δu(x/ϵ), (44) can be bounded by

|Err1(δ,ϵ)|(R3)2|ϵ-3Δu(w1ϵ)||ϕ(w1+w2)||ψ(w2)||w1|δ-7dw1dw2ϵ(R3)2|ϵ-3Δu(w1ϵ)||ψ(w2)|δ-7dw1dw2ϵR3|Δu(w1)|δ-7dw1=O(ϵδ-7),

where since ΔuCα(R3) and compactly supported in B(0,1ξ-1), it is integrable. Thus, we see that

limδ0lim supϵ0|Err1(δ,ϵ)|=0.

Using the coupling with the auxiliary free system (32), see [10, Sections 5–6] or [14, Section 6] for arguments in similar contexts, it can be shown that the sequence of laws of {μtN}N is weakly compact, and any subsequential limit of these laws is concentrated on those measure-valued processes that are absolutely continuous with respect to Lebesgue measure for every t0, with a density that is uniformly bounded by the right-hand side of (33) with =1 (i.e. by the 1-particle density of the free particle system). Let {μtk}k be such a converging subsequence, and let the limit density be called f(tx). Then for fixed δ we have as Nk (and ϵ(Nk)0),

ζδ(x1-w1)ζδ(x2-w1),μtN(dx1)μtN(x2)(R3)2ζδ(x1-w1)ζδ(x2-w1)f(t,x1)f(t,x2)dx1dx2.

Recall the definition of R¯ (25). Now, taking ϵ0 and then δ0 in (43), the error terms vanish in L1(P) and the main integral tends first to

R¯Rdϕ(w1)ψ(w1)(R3)2ζδ(x1-w1)ζδ(x2-w1)f(t,x1)f(t,x2)dx1dx2dw1,

and then to

R¯R3ϕ(w1)ψ(w1)f(t,w1)f(t,w1)dw1, 46

since ζδ approximates the delta-Dirac (here one needs the apriori fact that f is bounded uniformly by a non-random constant, hence one can apply the dominated convergence theorem). In (46) we have obtained the desired weak formulation (in space) of the nonlinearity of (22).

In Sect. 3 we already saw that in the identity satisfied by the empirical measure, the linear terms converge easily to the desired limiting linear terms (since they are in the form of a measure integrated against a test function) and the martingale terms vanish in L2(P); the only issue is the convergence of the nonlinear term (31). In this section, we saw that provided Proposition 11 is proved, we can also prove the convergence of the nonlinear term to the desired limiting nonlinear term, along every weakly converging subsequence of {μtN}t[0,T]. Thus a quite standard weak convergence argument as in e.g. [9, pp. 636–637] or [14, pp. 26–27] establishes the subsequential convergence in distribution of {μtN}t[0,T] to a weak solution of (22). Since it can be proved (see e.g. [9, Section 3]) that weak solutions to the pde in the sense of Definition 5 is unique hence deterministic, we conclude that the whole sequence {μtN}t[0,T] converges in probability. This is the proof of Theorem 6 (provided Proposition 11 is shown).

Itô–Tanaka Procedure

In order to prove the key Proposition 11, we need to introduce a particular functional on the particle configuration that contains the macroscopic variable z, and by applying the generator to such a functional, we wish to make appear the pre-limit in (38). It is clear only a posteriori that it should contain an auxiliary function vϵ,z(x) (47) that is in the form of a difference of the function uϵ(x), shifted by z.

For every fixed ϵ(0,1) and zR3 with |z|1/2, denote

vϵ,z(x):=uϵ(x+z)-uϵ(x), 47

where uϵ(x) is a C2,α(R3)-solution of the ϵ-dependent cell problem (35), given in (37). In particular, it is regular enough to apply Itô’s formula to. Consider the following functional on configurations

F3(ζtN):=1N2iN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t)),t0, 48

and we proceed to apply the Itô–Dynkin formula (with infinitesimal generator given in (17)) to it. We note the following property of the function C(x):

α=13αCαβ(x)=0,forallβ=1,2,3,xR3. 49

Indeed, by (15) C(x)=kNλkek(x)λkek(0). Since ek(x) is divergence free, for every kN, we have

α=13αCαβ(x)=kNλk2α=13α(ek)α(x)(ek)β(0)=kNλk2α=13α(ek)α(x)(ek)β(0)=kNλk2divek(ek)β(0)=0.

The property (49) effectively implies that all the divergence forms in the expansion (50) below, are also equivalently non-divergence forms.

Remark 12

The formula below is long, so let us first explain how one obtains it. Consider the first part of the diffusion generator LDN (18) (i.e. the part with covariance in it; the second part being more classical). It is in the form of a double sum, hence by linearity one can consider the action of each “sub-generator” 12σ2xi0·(Cϵ(ξ(xi0-xj0))xj0F(η)), for each fixed pair of indices (i0,j0). Note here that i0,j0 may not be distinct. One acts this “sub-generator” on our functional (48). Now, only those terms in (48) that contain either index i0 or j0 (or both) are affected by the action of this “sub-generator”. As we will exhaust all choices of i0,j0, for clarity we prefer to separate the case when i0=j0 from i0j0. By the property Cϵ(0)=I3, in the case i0=j0 we do not see the function Cϵ appear since we have I3. This is how we obtained the first 4 terms on the right-hand side of the explansion (50) below.

Similarly, the jump generator (19) is also a double sum. By linearity, one can consider the action of each “sub-generator” 12ri0j0NF(η-i0j0)-F(η), for each fixed pair of indices (i0,j0) (here they are necessarily distinct). As one acts this “sub-generator” on our functional (48), only those terms that contain either index i0 or j0 (or both) are affected. Here, the effect of the action is that some terms of (48) are removed. A moment’s thought convinces oneself that triple sums may appear, as in the 6th term on the right-hand side of (50).

We get

F3(ηTN)-F3(η0N)=1N20TiN(ζtN)jN(ζtN):jiσ22[xi·(Cϵ(ξ(xiN(t)-xjN(t)))xj(vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))))+xi·(Cϵ(ξ(xiN(t)-xjN(t)))xj(vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))))]dt+1N20TiN(ζtN)jN(ζtN):jiσ02+σ22[Δvϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+Δvϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]dt+1N20TiN(ζtN)jN(ζtN):jiσ02+σ22[vϵ,z(xiN(t)-xjN(t))Δϕ(xiN(t))ψ(xjN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))Δψ(xiN(t))]dt+1N20TiN(ζtN)jN(ζtN):jiσ02+σ2[vϵ,z(xiN(t)-xjN(t))·ϕ(xiN(t))ψ(xjN(t))-vϵ,z(xjN(t)-xiN(t))·ϕ(xjN(t))ψ(xiN(t))]dt-0TiN(ζtN)jN(ζtN):jiR02Nθϵ(xiN(t)-xjN(t))·1N2[vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]dt-0TiN(ζtN)jN(ζtN):jiR02Nθϵ(xiN(t)-xjN(t))·1N2kN(ζtN):ki,j[vϵ,z(xiN(t)-xkN(t))ϕ(xiN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xiN(t))ϕ(xkN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xkN(t))ϕ(xjN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xjN(t))ϕ(xkN(t))ψ(xjN(t))]dt+M~DN(T)+M~JN(T), 50

where M~DN(t) and M~JN(t) are two martingales associated with diffusion and jumps respectively.

With a tedious but straightforward computation (details omitted), we can expand and rewrite the 1st term on the right-hand side of (50) further:

1N20TiN(ζtN)jN(ζtN):jiσ22[xi·(Cϵ(ξ(xiN(t)-xjN(t)))xj(vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))))+xi·(Cϵ(ξ(xiN(t)-xjN(t)))xj(vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))))]dt=1N20TiN(ζtN)jN(ζtN):jiσ2[-xi·(Cϵ(ξ(xiN(t)-xjN(t)))vϵ,z(xiN(t)-xjN(t)))ϕ(xiN(t))ψ(xjN(t))-ϕ(xiN(t))TCϵ(ξ(xiN(t)-xjN(t)))vϵ,z(xiN(t)-xjN(t))ψ(xjN(t))+vϵ,z(xiN(t)-xjN(t))TCϵ(ξ(xiN(t)-xjN(t)))ψ(xjN(t))ϕ(xiN(t))+ϕ(xiN(t))TCϵ(ξ(xiN(t)-xjN(t)))ψ(xjN(t))vϵ,z(xiN(t)-xjN(t))]dt,

in which we have used Cϵ(-x)=Cϵ(x)T and (49).

By the symmetry of θ and the preceding computation, we get the following simplified expansion from the action of generator to F3(ζtN):

F3(ηTN)-F3(η0N) 51
=-σ2N20TiN(ζtN)jN(ζtN):jixi·(Cϵ(ξ(xiN(t)-xjN(t)))vϵ,z(xiN(t)-xjN(t)))ϕ(xiN(t))ψ(xjN(t))dt 52
-σ2N20TiN(ζtN)jN(ζtN):jiϕ(xiN(t))TCϵ(ξ(xiN(t)-xjN(t)))vϵ,z(xiN(t)-xjN(t))ψ(xjN(t))dt 53
+σ2N20TiN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))TCϵ(ξ(xiN(t)-xjN(t)))ψ(xjN(t))ϕ(xiN(t))dt 54
+σ2N20TiN(ζtN)jN(ζtN):jiϕ(xiN(t))TCϵ(ξ(xiN(t)-xjN(t)))ψ(xjN(t))vϵ,z(xiN(t)-xjN(t))dt 55
+σ02+σ2N20TiN(ζtN)jN(ζtN):jiΔvϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))dt 56
+σ02+σ22N20TiN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))[Δϕ(xiN(t))ψ(xjN(t))+ϕ(xjN(t))Δψ(xiN(t))]dt 57
+σ02+σ2N20TiN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))·[ϕ(xiN(t))ψ(xjN(t))-ϕ(xjN(t))ψ(xiN(t))]dt 58
-R0N30TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xiN(t))dt 59
-R0N30TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))·kN(ζtN):ki,j[vϵ,z(xiN(t)-xkN(t))ϕ(xiN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xiN(t))ϕ(xkN(t))ψ(xiN(t))]dt 60
+M~DN(T)+M~JN(T). 61

We look for all the terms that contain the highest (i.e. second) partial derivatives of vϵ,z, which are (56) and (52). In a sense, they are the most dangerous in terms of regularity (not for fixed ϵ but as ϵ0). Their sum

(56)+(52)=1N20TiN(ζtN)jN(ζtN):ji[(σ02+σ2)Δvϵ,z(xiN(t)-xjN(t))-σ2xi(Cϵ(ξ(xiN(t)-xjN(t)))vϵ,z(xiN(t)-xjN(t)))]ϕ(xiN(t))ψ(xjN(t))dt.

Recall definiton of vϵ,z in terms of uϵ (47), and use the cell equation (35) (which we repeat here)

(σ02+σ2)Δuϵ(x)-σ2·Cϵξxuϵx=R0θϵx(1+uϵxN)withx=xiN(t)-xjN(t)

for the terms that involve uϵ(xiN(t)-xjN(t)), while leaving those terms with uϵ(xiN(t)-xjN(t)+z) as they are, gives

(56)+(52)=1N20TiN(ζtN)jN(ζtN):ji[(σ02+σ2)Δuϵ(xiN(t)-xjN(t)+z)-σ2xi(Cϵ(ξ(xiN(t)-xjN(t)))uϵ(xiN(t)-xjN(t)+z))]ϕ(xiN(t))ψ(xjN(t))dt-R0N20TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))(1+1Nuϵ(xiN(t)-xjN(t)))ϕ(xiN(t))ψ(xjN(t))dt.

It turns out, a posteriori (but already noted in [13]), that a term like (59) with the same argument xiN(t)-xjN(t) in both functions θϵ and uϵ is not negligible, whereas if one argument is xiN(t)-xjN(t) and the other is xiN(t)-xjN(t)+z, then such term is negligible [such as (63) and (64)]. Thus, we have to combine the above with the term (59) to “kill” a non-negligible term, and finally obtain

(56)+(52)+(59)=1N20TiN(ζtN)jN(ζtN):ji[(σ02+σ2)Δuϵ(xiN(t)-xjN(t)+z)-R0θϵ(xiN(t)-xjN(t))]ϕ(xiN(t))ψ(xjN(t))dt 62
-σ2N20TiN(ζtN)jN(ζtN):jixi(Cϵ(ξ(xiN(t)-xjN(t)))uϵ(xiN(t)-xjN(t)+z))ϕ(xiN(t))ψ(xjN(t))dt 63
-R0N30TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))uϵ(xiN(t)-xjN(t)+z)ϕ(xiN(t))ψ(xjN(t))dt. 64

The final product of all these manouvres is that in (62), we have made the pre-limit in (38) appear, and on the other hand, we can expect to show that all the rest of the whole Itô-Tanaka expansion, namely (51), (53), (54), (55), (57), (58), (60), (63), (64) as well as (65), (66) and (67) below, are all negligible in L1(P) in the limit first N and then |z|0. This will be done in Sect. 6. Since the whole expansion (51)–(61) is an identity, the negligibility of all these “minor” terms will prove the desired negligibility of the “main” term in (38).

Finally, the martingales (61) should be bounded in L2(P) sense as follows.

M~DN(t):=M~D,1N(t)+M~D,2N(t)M~D,1N(T):=σN20TiN(ζtN)jN(ζtN):ji[vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))-vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]·kNλkekϵ(xiN(t))dWk(t).M~D,2N(T):=σ0N20TiN(ζtN)jN(ζtN):ji[vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))-vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]·dBi(t).

Hence, by Itô isometry we can bound their quadratic variation by

E|M~D,1N(T)|2=σ2N40TkNE|iN(ζtN)jN(ζtN):ji[vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))-vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]·λkekϵ(xiN(t))|2dt. 65
E|M~D,2N(T)|22σ02N4iN(ζtN)0T|jN(ζtN):ji[vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))+vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))-vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xiN(t))ϕ(xjN(t))ψ(xiN(t))]|2dt. 66

Further, we can bound the second moment of the jump part of the martingale by the carré-du-champ formula cf. [6, Proposition 8.7]

E|M~JN(T)|20TiN(ζtN)jN(ζtN):jiR0Nθϵ(xiN(t)-xjN(t))|1N2vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt+0TiN(ζtN)jN(ζtN):jiR0Nθϵ(xiN(t)-xjN(t))|1N2kN(ζtN):ki,j[vϵ,z(xiN(t)-xkN(t))ϕ(xiN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xiN(t))ϕ(xkN(t))ψ(xiN(t))+vϵ,z(xjN(t)-xkN(t))ϕ(xjN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xjN(t))ϕ(xkN(t))ψ(xjN(t))]|2dt=R0N50TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))|vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt+4R0N50TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))·|kN(ζtN):ki,j[vϵ,z(xiN(t)-xkN(t))ϕ(xiN(t))ψ(xkN(t))+vϵ,z(xkN(t)-xiN(t))ϕ(xkN(t))ψ(xiN(t))]|2dt. 67

The Negligibility of Various Terms

We set out to prove that all the terms (51), (53), (54), (55), (57), (58), (60), (63), (64), (65), (66) and (67) are negligible in the order of limits ϵ0 then |z|0 (we refer to it simply as “negligible” in the sequel), which by the Itô–Tanaka identity (51)–(61) of Sect. 5 yields Proposition 38, and in turn Theorem 6.

Recall once more the ϵ-dependent cell equation uϵ:R3R

σ02Δuϵ(x)+σ2·(ω(ξxϵ)uϵx)=R0θϵx(1+uϵxN), 68

and the unscaled cell equation

σ02Δu(x)+σ2·(ω(ξx)u(x))=R0θ(x)(1+u(x)). 69

They are related by uϵ(x)=ϵ-1u(x/ϵ) for any xR3, hence whenever u exists, uϵ also exists. Crucial for our purpose are pointwise estimates of uϵ(x) stated in lemmas below. They are proved in [13, Lemma 3.5] in the case when the elliptic operator is Δ. To generalize those estimates to our case of uniformly elliptic divergence-form operator with variable coefficients, we will derive all estimates for the ϵ-independent u(x), and then transfer them to uϵ(x) by their scaling relation.

Denote the second-order divergence-form operator in the ϵ-independent equation (69) by

Ax:=σ02Δ+σ2·ω(ξx)-R0θ(x)=σ02Δ+σ2Trω(ξx)2-R0θ(x).

(The equivalence between divergence and non-divergence form is due to (49).) It is uniformly elliptic, since for any ξR3 and xR3

ξTσ02I3+σ2ω(ξx)ξσ02|ξ|2,

where the matrix ω(·) is nonnegative definite and σ0>0.

Let us consider the parabolic operator t-Ax, and let p(txy) denote its fundamental solution (i.e. heat kernel). By parabolic regularity theory [15, Theorem 1, p. 483], p(txy) and its first two spatial derivatives satisfy, for a constant M that depends only on σ0,σ,ξ,R0 and the Cα-norm of a and θ (these data are all given and fixed):

p(t;x,y)Mt3/2e-|x-y|2Mt,|xp(t;x,y)|Mt3/2+1/2e-|x-y|2Mt,|x2p(t;x,y)|Mt3/2+1e-|x-y|2Mt. 70

Since we are in R3, the Green function g(x,y)>0 (i.e. fundamental solution) of Ax exists and is related to the heat kernel by

g(x,y)=0p(t;x,y)dt,x,yR3.

Thus, by (70) we have

g(x,y)0Mt3/2e-|x-y|2Mtdt=s=|x-y|2tM0s-1/2e-s/M|x-y|dsM|x-y|-1, 71

for some finite constant M=M(M), since s-1/2e-s/M is integrable at both 0 and . Similarly,

|xg(x,y)|0xp(t;x,y)dt0|xp(t;x,y)|dt0Mt3/2+1/2e-|x-y|2Mtdt=M0e-s/M|x-y|2dsM|x-y|-2, 72
|x2g(x,y)|0x2p(t;x,y)dt0|x2p(t;x,y)|dt0Mt3/2+1e-|x-y|2Mtdt=M0s1/2e-s/M|x-y|3dsM|x-y|-3, 73

since e-s/M and s1/2e-s/M are both integrable at both 0 and .

Since (69) can be written as Axu(x)=R0θ(x), one can find a solution given by

u(x)=-R3g(x,y)R0θ(y)dy,xR3. 74

(The negative sign is just a convention, due to the fact that Ax is a negative operator while we take g(x,y)>0.) By elliptic regularity theory [17, Theorem 4.3.1], since θCα(R3) and coefficients of Ax are symmetric, Cα and bounded, we have u(x)C2,α(R3).

Lemma 13

There exists a finite constant M=M(σ0,σ,ξ,R0,ω,θ) such that for all xR3 and ϵ(0,1), we have

|uϵ(x)|M|x|ϵ-1, 75
|uϵ(x)|M|x|ϵ-2, 76

and for all |x|2ϵ we have

|2uϵ(x)|M|x|-3. 77

Proof

We will first derive the estimate for u(x), then transfer them to uϵ(x). Since u solves Axu(x)=R0θ(x), we can write

u(x)=-R3g(x,y)R0θ(y)dy 78

where g(xy) is the Green function of Ax. Recall that θ is nonnegative and has compact support in B(0, 1). If |x|2, then for any ysupp(θ), |x-y||x|-|y||x|-1|x|/2. Thus, by (71), g(x,y)M|x|-1. Hence, in this case

|u(x)|R3g(x,y)R0θ(y)dyR3M|x|-1R0θ(y)dyMR0|x|-1.

If on the other hand, |x|2, then for any ysupp(θ), x-yB(0,3), and hence

|u(x)|R3g(x,y)R0θ(y)dyR0θLB(0,1)M|x-y|-1dyB(0,3)|y|-1dy1.

Thus, we conclude the estimate

|u(x)|M(|x|1)-1,|uϵ(x)|=ϵ-1|u(x/ϵ)|M(|x|ϵ)-1.

Turning to the gradient estimate of u,

u(x)=-R3xg(x,y)R0θ(y)dy.

Hence, if |x|2 then for any ysupp(θ), |x-y||x|/2, and by (72),

|u(x)|R3|xg(x,y)|R0θ(y)dyR3M|x|-2R0θ(y)dyMR0|x|-2.

If on the other hand, |x|2, then for any ysupp(θ), x-yB(0,3), and hence

|u(x)|R3|xg(x,y)|R0θ(y)dyR0θLB(0,1)M|x-y|-2dyB(0,3)|y|-2dy1.

Thus, we conclude the estimate

|u(x)|M(|x|1)-2,|uϵ(x)|=ϵ-2|u(x/ϵ)|M(|x|ϵ)-2.

Turning to the estimate on the Hessian of u,

2u(x)=-R3x2g(x,y)R0θ(y)dy.

We only consider the case that |x|2, hence for any ysupp(θ), |x-y||x|/2. By (73), we thus have that

|2u(x)|R3|x2g(x,y)|R0θ(y)dyR3M|x|-3R0θ(y)dyMR0|x|-3.

By scaling relation, this yields that for any x such that |x|2ϵ,

|2uϵ(x)|=ϵ-3|u(x/ϵ)|M|x|-3.

Lemma 14

There exists a finite constant M=M(σ0,σ,ξ,R0,ω,θ) such that for all xR3 with |x|2|z|+2ϵ, ϵ(0,1), we have

|uϵ(x+z)-uϵ(x)|M|z||x|-2, 79
|uϵ(x+z)-uϵ(x)|M|z||x|-3. 80

Proof

We will first derive the estimate for u(x), then transfer them to uϵ(x). We consider only the regime |x|2|z|+2. By (78),

u(x+z)-u(x)=-R3g(x+z,y)-g(x,y)R0θ(y)dy

Since

g(x+z,y)-g(x,y)=01sg(x+sz,y)ds=01z·xg(x+sz,y)ds,

we have

|g(x+z,y)-g(x,y)|01|z·xg(x+sz,y)|ds|z|sups[0,1]|xg(x+sz,y)|.

Since |x|2|z|+2, we have for any ysupp(θ) and s[0,1],

|x+sz-y||x|-|sz|-|y||x|/2+|x|/2-|z|-1|x|/2.

Hence, by (72), for some finite constant M,

|g(x+z,y)-g(x,y)|M|z||x|-2.

Hence,

|u(x+z)-u(x)|R3g(x+z,y)-g(x,y)R0θ(y)dyR0M|z||x|-2.

By scaling relations, this implies that for any |x|2|z|+2ϵ,

|uϵ(x+z)-uϵ(x)|=ϵ-1|u(x/ϵ+z/ϵ)-u(x/ϵ)|ϵ-1|z/ϵ||x/ϵ|-2=|z||x|-2,

where |x/ϵ|2|z/ϵ|+2 hence the above bound applies.

Turning to the estimates for the gradient, we have

u(x+z)-u(x)=-R3xg(x+z,y)-xg(x,y)R0θ(y)dy.

Since

xg(x+z,y)-xg(x,y)=01sxg(x+sz,y)ds=01z·x2g(x+sz,y)ds,

we have

|xg(x+z,y)-xg(x,y)|01|z·x2g(x+sz,y)|ds|z|sups[0,1]|x2g(x+sz,y)|.

For |x|2|z|+2, any ysupp(θ) and s[0,1], we have |x+sz-y||x|/2, thus by (73) for some finite constant M, we have

|xg(x+z,y)-xg(x,y)|M|z||x|-3.

Hence,

|u(x+z)-u(x)|R3xg(x+z,y)-xg(x,y)R0θ(y)dyR0M|z||x|-2R0M|z||x|-3.

By scaling, this implies that for any |x|2|z|+2ϵ,

|uϵ(x+z)-uϵ(x)|=ϵ-2|u(x/ϵ+z/ϵ)-u(x/ϵ)|ϵ-2|z/ϵ||x/ϵ|-3=|z||x|-3.

Lemma 15

The C2,α-solution (74) of (69) satisfies -1u(x)0 for all xR3. Hence -Nuϵ(x)0.

Proof

The argument is similar to [13, p. 64, Step 6]. Denote here

A~x:=σ02Δ+σ2·ω(ξx)

and (69) can be written as A~xu(x)=θ(x)(1+u(x)). For each δ(0,1), let χδ:R[0,1] be smooth, identically 1 on (-,-δ), identically 0 on (0,), and decreasing on [-δ,0], and let

ϕδ(r):=(1+r)χδ(1+r),

which is smooth and non-3ecreasing. Further assume that as δ0, χδ1(-,0) in C2-norm. Clearly, we have the property that |ϕδ(r)|2r for r1 and ϕδ(r)0.

Integration by parts in the ball B(0, R), R1, we have

B(0,R)ϕδ(u(x))A~xu(x)du=-BRϕδ(u(x))u(x)Tσ02I3+σ2ω(ξx)u(x)dx+B(0,R)ϕδ(u(x))σ02I3+σ2ω(ξx)u(x)·dn(x),

where n(x) denotes the unit outward normal vector. By (75) and (76),

B(0,R)ϕδ(u(x))σ02I3+σ2ω(ξx)u(x)·dn(x)R-1R-2|B(0,R)|=O(R-1).

Hence taking R, we obtain that

R3ϕδ(u(x))A~xu(x)du=-R3ϕδ(u(x))u(x)Tσ02I3+σ2ω(ξx)u(x)dx0. 81

On the other hand,

R3ϕδ(u(x))A~xu(x)du=R3ϕδ(u(x))θ(x)1+u(x)dx=R3θ(x)1+u(x)2χδ(1+u(x))dx0,

hence in view of (81) the right-hand side is 0. Letting δ0 in (81), since ϕδ1(-,-1) by construction, we get

R31{u(x)-1}u(x)Tσ02I3+σ2ω(ξx)u(x)dx=0.

Since the quadratic form in the above expression is positive unless u(x)=0, we conclude that u(x)=0 on the set {xR3:u(x)-1}. Since u is continuous, we must have u(x)=-1 on this set, and so u(x)-1 for all xR3. Further, by (74) and g(x,y)>0, we have u(x)0 for all xR3.

Now we proceed to bound all terms that are expected to be negligible. We will make extensive use of the auxiliary free particle system {yiϵ}i=1 (32) introduced in Sect. 3. Recall that under a natural coupling, whenever a true particle xiN is active by time t, its trajectory on [0, t] must coincide with that of the free particle yiϵ. We start with the term (64).

Proposition 16

lim|z|0lim supϵ0E|1N30TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))uϵ(xiN(t)-xjN(t)+z)ϕ(xiN(t))ψ(xjN(t))dt|=0. 82

Proof

Since the limit |z|0 is taken only after ϵ0, we can always assume that |z|2ϵ. The pre-limit on the left-hand side of (82) can be bounded from above by

1N3E0TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))|uϵ(xiN(t)-xjN(t)+z)||ϕ(xiN(t))||ψ(xjN(t))|dt.

Since the integrand and summands are nonnegative, we can further bound it above by

1N3E0Tij=1Nθϵ(yiϵ(t)-yjϵ(t))|uϵ(yiϵ(t)-yjϵ(t)+z)||ϕ(yiϵ(t))||ψ(yjϵ(t))|dt.

Using exchangeability of the free particles, we further have that

1NE0Tθϵ(y1ϵ(t)-y2ϵ(t))|uϵ(y1ϵ(t)-y2ϵ(t)+z)||ϕ(y1ϵ(t))||ψ(y2ϵ(t))|dt1N0T(R3)2θϵ(y1-y2)|uϵ(y1-y2+z)|ft12,ϵ(y1,y2)|ϕ(y1)ψ(y2)|dy1dy2dtC0T1N(R3)2θϵ(y1-y2)|uϵ(y1-y2+z)||ϕ(y1)ψ(y2)|dy1dy2,

where ft12,ϵ(y1,y2) denotes the joint density of (y1ϵ(t),y2ϵ(t)) which satisfies the bound (33). Since |y1-y2|ϵ in the support of the function θϵ, and |z|2ϵ, by (75) we have

|uϵ(y1-y2+z)||z|-1.

Further, (R3)2θϵ(y1-y2)|ϕ(y1)ψ(y2)|dy1dy21, N=ϵ-1, hence we have

1N(R3)2θϵ(y1-y2)|uϵ(y1-y2+z)|dy1dy2ϵ|z|-1.

This yields (82).

We continue with (63).

Proposition 17

lim|z|0lim supϵ0E|1N20TiN(ζtN)jN(ζtN):ji·(Cϵ(xiN(t)-xjN(t))uϵ(xiN(t)-xjN(t)+z))ϕ(xiN(t))ψ(xjN(t))dt|=0. 83

Proof

Since the limit |z|0 is taken only after ϵ0, we can always assume that |z|2ϵ. In view of (49), the pre-limit on the left-hand side of (83) can be bounded from above as follows

=E|1N20TiN(ζtN)jN(ζtN):jiα,β=13Cϵαβ(xiN(t)-xjN(t))αβ2uϵ(xiN(t)-xjN(t)+z)ϕ(xiN(t))ψ(xjN(t))dt|1N2E0TiN(ζtN)jN(ζtN):jiα,β=13|Cϵαβ(xiN(t)-xjN(t))||αβ2uϵ(xiN(t)-xjN(t)+z)||ϕ(xiN(t))ψ(xjN(t))|dt1N2E0Tij=1Nα,β=13|Cϵαβ(yiϵ(t)-yjϵ(t))||αβ2uϵ(yiϵ(t)-yjϵ(t)+z)||ϕ(yiϵ(t))ψ(yjϵ(t))|dtE0Tα,β=13|Cϵαβ(y1ϵ(t)-y2ϵ(t))||αβ2uϵ(y1ϵ(t)-y2ϵ(t)+z)||ϕ(y1ϵ(t))ψ(y2ϵ(t))|dtC0T(R3)2α,β=13|Cϵαβ(y1-y2)||αβ2uϵ(y1-y2+z)||ϕ(y1)ψ(y2)|dy1dy2,

using the auxiliary free system, its exchangeability, and that (y1ϵ(t),y2ϵ(t)) has a uniformly bounded density, see Proposition 7. Since we have assumed that Cϵ(x)=C(x/ϵ) for some matrix function C with compact support in B(0,1)R3, we have |y1-y2|ϵ in the support of Cϵαβ in the above display. By (77) and since |z|2ϵ, we have

|αβ2uϵ(y1-y2+z)||z|-3,α,β=1,2,3.

Thus, we have

(R3)2α,β=13|αβ2uϵ(y1-y2+z)||Cϵαβ(y1-y2)||ϕ(y1)ψ(y2)|dy1dy2|z|-3α,β=13|Cϵαβ(y)||ϕ(y+y2)ψ(y2)|dydy2|z|-3α,β=13|Cϵαβ(y)|dy=ϵ3|z|-3α,β=13|Cαβ(y)|dy,

where the factor ϵ3 comes from change of variables. This yields (83) since the function C is smooth and compactly supported.

We continue with (57). There are two terms with similar structure, and it suffices to consider one of them.

Proposition 18

lim|z|0lim supϵ0E|1N20TiN(ζtN)jN(ζtN):ji[uϵ(xiN(t)-xjN(t)+z)-uϵ(xiN(t)-xjN(t))]Δϕ(xiN(t))ψ(xjN(t))dt|=0. 84

Proof

The pre-limit on the left-hand side of (84) can be bounded from above by

1N2E0TiN(ζtN)jN(ζtN):ji|uϵ(xiN(t)-xjN(t)+z)-uϵ(xiN(t)-xjN(t))||Δϕ(xiN(t))ψ(xjN(t))|dt1N2E0Tij=1N|uϵ(yiϵ(t)-yjϵ(t)+z)-uϵ(yiϵ(t)-yjϵ(t))||Δϕ(yiϵ(t))ψ(yjϵ(t))|dtE0T|uϵ(y1ϵ(t)-y2ϵ(t)+z)-uϵ(y1ϵ(t)-y2ϵ(t))||Δϕ(y1ϵ(t))ψ(y2ϵ(t))|dtC0T(R3)2|uϵ(y1-y2+z)-uϵ(y1-y2)||Δϕ(y1)ψ(y2)|dy1dy2=C0T(R3)2|uϵ(y+z)-uϵ(y)||Δϕ(y+y2)ψ(y2)|dydy2,

using the auxiliary free system, its exchangeability, and that (y1ϵ(t),y2ϵ(t)) has a uniformly bounded density, see Proposition 7. By (79) and (75), we have

|uϵ(y+z)-uϵ(y)||z||y|-2,if|y|2|z|+2ϵ,(ϵ|y+z|)-1+(ϵ|y|)-1,forally.

Note that for any y2supp(ψ), y+y2supp(ϕ), we have yK for some compact set K which is determined by the supports of ϕ,ψ. Hence, bounding |Δϕ(y+y2)|ϕC2, we have

K|uϵ(y+z)-uϵ(y)|dyB(0,2|z|+2ϵ)(ϵ|y+z|)-1dy+B(0,2|z|+2ϵ)(ϵ|y|)-1dy+K\B(0,2|z|+2ϵ)|z||y|-2dy2B(0,3|z|+2ϵ)(ϵ|y|)-1dy+K\B(0,2|z|+2ϵ)|z||y|-2dy(3|z|+2ϵ)2+|z|. 85

Then we integrate in |ψ(y2)|dy2 which is finite. This yields (84).

Remark 19

The same proof as above also yields the negligibility of the initial F3(η0N) and terminal F3(ηTN) terms in (51) individually, since each of them also involve the difference of uϵ and the heat kernel estimates are uniform in [0, T]. Thus we omit discussing them.

We continue with (58). There are two terms with similar structure, and it suffices to consider one of them.

Proposition 20

lim|z|0lim supϵ0E|1N20TiN(ζtN)jN(ζtN):ji[uϵ(xiN(t)-xjN(t)+z)-uϵ(xiN(t)-xjN(t))]·ϕ(xiN(t))ψ(xjN(t))dt|=0. 86

Proof

The pre-limit on the left-hand side of (86) can be bounded from above by

1N2E0TiN(ζtN)jN(ζtN):ji|uϵ(xiN(t)-xjN(t)+z)-uϵ(xiN(t)-xjN(t))||ϕ(xiN(t))ψ(xjN(t))|dt1N2E0Tij=1N|uϵ(yiϵ(t)-yjϵ(t)+z)-uϵ(yiϵ(t)-yjϵ(t))||ϕ(yiϵ(t))ψ(yjϵ(t))|dtE0T|uϵ(y1ϵ(t)-y2ϵ(t)+z)-uϵ(y1ϵ(t)-y2ϵ(t))||ϕ(y1ϵ(t))ψ(y2ϵ(t))|dtC0T(R3)2|uϵ(y1-y2+z)-uϵ(y1-y2)||ϕ(y1)ψ(y2)|dy1dy2=C0T(R3)2|uϵ(y+z)-uϵ(y)||ϕ(y+y2)ψ(y2)|dy,

using the auxiliary free system, its exchangeability, and that (y1ϵ(t),y2ϵ(t)) has a uniformly bounded density, see Proposition 7. By (80) and (76), we have

|uϵ(y+z)-uϵ(y)||z||y|-3,if|y|2|z|+2ϵ,(ϵ|y+z|)-2+(ϵ|y|)-2,forally.

Hence, for some r>2|z|+2ϵ to be chosen and a compact set K determined by the supports of ϕ,ψ, we have

K|uϵ(y+z)-uϵ(y)||ϕ(y+y2)|dyB(0,r)(ϵ|y+z|)-2dy+B(0,r)(ϵ|y|)-2dy+K\B(0,r)|z||y|-3dy2B(0,|z|+r)(ϵ|y|)-2dy+K\B(0,r)|z||y|-3dy(|z|+r)+|z|r-3|K|.

Choosing r=4|z|14>2|z|+2ϵ (we can always assume 2ϵ|z|1/2) yields

K|uϵ(y+z)-uϵ(y)||ϕ(y+y2)|dy|z|14. 87

Then we integrate |ψ(y2)|dy2 which is finite. This yields (86).

Remark 21

The same proof for (86) can also yield the negligibility of the terms (53) and (54), since one can simply bound the covariance terms maxα,β=13|Cϵα,β(ξ(xiN(t)-xjN(t))|CL:=maxα,β=13Cα,βL(R3) and then they are in the form of an averaged double sum involving the difference of uϵ. It is not necessary to take advantage of the smallness given by the support of Cϵ. Similarly, the proof given to prove (84) can yield the negligibility of the term (55), since it also involves the difference of uϵ, and one can bound maxα,β=13|Cϵα,β(ξ(xiN(t)-xjN(t))|CL.

We continue with (60). Although there are two terms there, they can be bounded in the same way, hence it suffices to consider one of them.

Proposition 22

lim|z|0lim supϵ0E|1N30Ti,j,kN(ζtN):ji,ki,jθϵ(xiN(t)-xjN(t))·[uϵ(xiN(t)-xkN(t)+z)-uϵ(xiN(t)-xkN(t))]ϕ(xiN(t))ψ(xkN(t))dt|=0. 88

Proof

The pre-limit on the left-hand side of (88) can be bounded from above by

1N3E0Ti,j,kN(ζtN):ji,ki,jθϵ(xiN(t)-xjN(t))|uϵ(xiN(t)-xkN(t)+z)-uϵ(xiN(t)-xkN(t))||ϕ(xiN(t))ψ(xkN(t))|dt1N3E0Ti,j,k=1N1{ji,ki,j}θϵ(yiϵ(t)-yjϵ(t))|uϵ(yiϵ(t)-ykϵ(t)+z)-uϵ(yiϵ(t)-ykϵ(t))||ϕ(yiϵ(t))ψ(ykϵ(t))|dtE0Tθϵ(y1N(t)-y3N(t))|uϵ(y1ϵ(t)-y2ϵ(t)+z)-uϵ(y1ϵ(t)-y2ϵ(t))||ϕ(y1ϵ(t))ψ(y2ϵ(t))|dt,

using the auxiliary free system and its exchangeability. Since the triple (y1ϵ(t),y2ϵ(t),y3ϵ(t)) has a joint density ft123,ϵ(y1,y2,y3) that satisfies the bound (33), we can further bound the previous display by

=0T(R3)3θϵ(y1-y3)|uϵ(y1-y2+z)-uϵ(y1-y2)||ϕ(y1)ψ(y2)|ft123,ϵ(y1,y2,y3)dy1dy2dy3dtC0T(R3)3θϵ(y1-y3)|uϵ(y1-y2+z)-uϵ(y1-y2)||ϕ(y1)ψ(y2)|dy1dy2dy3=c0T(R3)2|uϵ(y1-y2+z)-uϵ(y1-y2)||ϕ(y1)ψ(y2)|dy1dy2=C0T(R3)2|uϵ(y+z)-uϵ(y)||ϕ(y+y2)ψ(y2)|dy,

where θϵ(y1-y3)dy3=1 is used. The last expression is bounded by ϵ2+(3|z|+2ϵ)2+|z| as already analyzed in (85). This yields (88).

We continue with (65). By the elementary inequality (a+b+c)23(a2+b2+c2), it can be seen that it suffices to control two type of terms, which are treated in the next two propositions. Recall that vϵ,z is a shorthand (47).

Proposition 23

lim|z|0lim supϵ01N40TkNE|iN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))·λkekϵ(xiN(t))ψ(xjN(t))|2dt=0. 89

Proof

The pre-limit on the left-hand side of (89) can be expanded as

1N40TkNE|iN(ζtN)jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))·λkekϵ(xiN(t))ψ(xjN(t))|2dt=1N40TkNEimjnvϵ,z(xiN(t)-xmN(t))ψ(xmN(t))ϕ(xiN(t))Tλkekϵ(xiN(t))λkekϵ(xjN(t))·ϕ(xjN(t))ψ(xnN(t))vϵ,z(xjN(t)-xnN(t))dt=1N40TEimjnvϵ,z(xiN(t)-xmN(t))ψ(xmN(t))ϕ(xiN(t))TCϵ(xiN(t)-xjN(t))·ϕ(xjN(t))ψ(xnN(t))vϵ,z(xjN(t)-xnN(t))dt=1N40TEi=jm,nvϵ,z(xiN(t)-xmN(t))ψ(xmN(t))ϕ(xiN(t))Tϕ(xiN(t))ψ(xnN(t))vϵ,z(xiN(t)-xnN(t))dt+1N40TEij,im,jnvϵ,z(xiN(t)-xmN(t))ψ(xmN(t))ϕ(xiN(t))TCϵ(xiN(t)-xjN(t))·ϕ(xjN(t))ψ(xnN(t))vϵ,z(xjN(t)-xnN(t))dt1N40TEi=jm,n|vϵ,z(xiN(t)-xmN(t))||vϵ,z(xiN(t)-xnN(t))|ϕ(xiN(t))2|ψ(xmN(t))ψ(xnN(t))|dt+9N40TEij,im,jn|vϵ,z(xiN(t)-xmN(t))|Cϵ(xiN(t)-xjN(t))·|vϵ,z(xjN(t)-xnN(t))||ϕ(xiN(t))ϕ(xjN(t))ψ(xmN(t))ψ(xnN(t))|dt,

where recall (34) notation for maximum of matrix entries. By the bound (75) and the coupling with the auxiliary free system, we further bound the above by

ϵ-1N40TEim,n|vϵ,z(xiN(t)-xmN(t))|ϕ(xiN(t))2|ψ(xmN(t))ψ(xnN(t))|dt+ϵ-1N40TEij,im,jn|vϵ,z(xiN(t)-xmN(t))|Cϵ(xiN(t)-xjN(t))|ϕ(xiN(t))ϕ(xjN(t))ψ(xmN(t))ψ(xnN(t))|dt1N30TEim,n|vϵ,z(yiϵ(t)-ymϵ(t))|ϕ(yiϵ(t))2|ψ(ymϵ(t))ψ(ynϵ(t))|dt+1N30TEij,im,jn|vϵ,z(yiϵ(t)-ymϵ(t))|Cϵ(yiϵ(t)-yjϵ(t))|ϕ(yiϵ(t))ϕ(yjϵ(t))ψ(ymϵ(t))ψ(ynϵ(t))|dt.

By exchangeability of the free system, we can further write the above as

0TE|vϵ,z(y1ϵ(t)-y2ϵ(t))|ϕ(y1ϵ(t))2|ψ(y2ϵ(t))ψ(y3ϵ(t))|dt+N0TE|vϵ,z(y1ϵ(t)-y3ϵ(t))|Cϵ(y1ϵ(t)-y2ϵ(t))|ϕ(y1ϵ(t))ϕ(y2ϵ(t))ψ(y3ϵ(t))ψ(y4ϵ(t))|dt.

Recall that a -tuple (y1ϵ(t),...,yϵ(t)) of free particles, =3,4, have a uniformly bounded joint density, see (33). Hence we may rewrite the above as

=0T(R3)3|vϵ,z(y1-y2)|ft123,ϵ(y1,y2,y3)ϕ(y1)2|ψ(y2)ψ(y3)|dy1dy2dt+N0T(R3)4|vϵ,z(y1-y3)|Cϵ(y1-y2)ft1234,ϵ(y1,y2,y3,y4)ϕ(y1)ϕ(y2)ψ(y3)ψ(y4)dy1dy2dy3dy4dtC0TK|vϵ,z(y)|dy+C0TNK2|vϵ,z(y3)|C(y2/ϵ)dy2dy3C0TK|vϵ,z(y)|dy+C0TNϵ3K|vϵ,z(y)|dyR3C(z)dz,

where KR3 is a compact set determined by the supports of ϕ,ψ. Note that Nϵ3=ϵ2 and we already analyzed in (85) that K|vϵ,z(y)|dyϵ2+(3|z|+2ϵ)2+|z|. This yields (89).

Proposition 24

lim|z|0lim supϵ01N40TkNE|iN(ζtN)jN(ζtN):jiϕ(xiN(t))vϵ,z(xiN(t)-xjN(t))·λkekϵ(xiN(t))ψ(xjN(t))|2dt=0. 90

Proof

As the in the last proposition, the pre-limit on the left-hand side of (90) can be expanded as

1N40TkNE|iN(ζtN)jN(ζtN):jiϕ(xiN(t))vϵ,z(xiN(t)-xjN(t))·λkekϵ(xiN(t))ψ(xjN(t))|2dt=1N40TEimjnϕ(xiN(t))ψ(xmN(t))vϵ,z(xiN(t)-xmN(t))TCϵ(xiN(t)-xjN(t))·vϵ,z(xjN(t)-xnN(t))ϕ(xjN(t))ψ(xnN(t))dt1N40TEi=jm,n|vϵ,z(xiN(t)-xmN(t))||vϵ,z(xiN(t)-xnN(t))|ϕ(xiN(t))2|ψ(xmN(t))ψ(xnN(t))|dt+1N40TEij,im,jn|vϵ,z(xiN(t)-xmN(t))|Cϵ(xiN(t)-xjN(t))·|vϵ,z(xjN(t)-xnN(t))||ϕ(xiN(t))ϕ(xjN(t))ψ(xmN(t))ψ(xnN(t))|dt,

We bound the two terms separately. First we treat the first term and we divide it further according to m=n or mn. In case i=j, m=n we have

1N40TEi=jm=n|vϵ,z(xiN(t)-xmN(t))||vϵ,z(xiN(t)-xmN(t))|ϕ(xiN(t))2ψ(xmN(t))2dt1N40TEi=jm=n|vϵ,z(yiϵ(t)-ymϵ(t))||vϵ,z(yiϵ(t)-ymϵ(t))|ϕ(yiϵ(t))2ψ(ymϵ(t))2dt1N20TE|vϵ,z(y1ϵ(t)-y2ϵ(t))||vϵ,z(y1ϵ(t)-y2ϵ(t))|ϕ(y1ϵ(t))2ψ(y2ϵ(t))2dtϵ-1N20TE|vϵ,z(y1ϵ(t)-y2ϵ(t))|ϕ(y1ϵ(t))2ψ(y2ϵ(t))2dt,

and we have analysed in (87) that such a term (even without the 1/N factor) is negligible. In case i=j, mn, we have

1N40TEi=jmn|vϵ,z(xiN(t)-xmN(t))||vϵ,z(xiN(t)-xnN(t))|ϕ(xiN(t))2|ψ(xmN(t))ψ(xnN(t))|dt1N40TEi=jmn|vϵ,z(yiϵ(t)-ymϵ(t))||vϵ,z(yiϵ(t)-ynϵ(t))|ϕ(yiϵ(t))2|ψ(ymϵ(t))ψ(ynϵ(t))|dt1N0TE|vϵ,z(y1ϵ(t)-y2ϵ(t))||vϵ,z(y1ϵ(t)-y3ϵ(t))|ϕ(y1ϵ(t))2|ψ(y2ϵ(t))ψ(y3ϵ(t))|dt.

Recall that the joint density of a triple of free particles y1ϵ(t),y2ϵ(t),y3ϵ(t) has the bound (33), hence we have (even without the 1/N factor)

0TE|vϵ,z(y1ϵ(t)-y2ϵ(t))||vϵ,z(y1ϵ(t)-y3ϵ(t))|ϕ(y1ϵ(t))2|ψ(y2ϵ(t))ψ(y3ϵ(t))|dt=0T(R3)3|vϵ,z(y1-y2)||vϵ,z(y1-y3)|ϕ(y1)2|ψ(y2)ψ(y3)|ft123,ϵ(y1,y2,y3)dy1dy2dy3TC0(R3)3|vϵ,z(y1-y2)||vϵ,z(y1-y3)ϕ(y1)2|ψ(y2)ψ(y3)|dy1dy2dy3K|vϵ,z(y)|dy2,

where K is a compact set determined by the supports of ϕ,ψ. Since from (87) we know that K|vϵ,z(y)|dy is negligible, so is the whole term.

To treat the second main term involving the covariance Cϵ, we proceed as in the proof of Proposition 23, using the bound (76) and coupling with the auxiliary system

1N40TEij,im,jn|vϵ,z(xiN(t)-xmN(t))|Cϵ(xiN(t)-xjN(t))·|vϵ,z(xjN(t)-xnN(t))||ϕ(xiN(t))ϕ(xjN(t))ψ(xmN(t))ψ(xnN(t))|dtϵ-2N40TEij,im,jn|vϵ,z(xiN(t)-xmN(t))|Cϵ(xiN(t)-xjN(t))|ϕ(xiN(t))ϕ(xjN(t))ψ(xmN(t))ψ(xnN(t))|dtϵ-20TE|vϵ,z(y1ϵ(t)-y2ϵ(t))|Cϵ(y1ϵ(t)-y3ϵ(t))|ϕ(x1N(t))ϕ(x2N(t))ψ(x3N(t))ψ(x4N(t))|dtϵ-2ϵ3K|vϵ,z(y)|dyR3C(z)dz.

Notice that we have a factor of ϵ and in addition K|vϵ,z(y)|dy is negligible. This completes the proof of (90).

We continue with (66). By the elementary inequality (a+b)22(a2+b2), it suffices to control separately two terms in the following proposition.

Proposition 25

lim|z|0lim supϵ01N4iN(ζtN)0TE|jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt=0.lim|z|0lim supϵ01N4iN(ζtN)0TE|jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt=0. 91

Proof

The proof of the two statements are similar and for brevity we only treat the first one (91). The pre-limit of the left-hand side of (91) can be bounded by

1N4iN(ζtN)0TE|jN(ζtN):jivϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt=1N4iN(ζtN)0TEj,mN(ζtN):j,mivϵ,z(xiN(t)-xjN(t))·vϵ,z(xiN(t)-xmN(t))ϕ(xiN(t))2ψ(xjN(t))ψ(xmN(t))dt1N4iN(ζtN)0TEj,mN(ζtN):j=mi|vϵ,z(xiN(t)-xjN(t))||vϵ,z(xiN(t)-xjN(t))|ϕ(xiN(t))2ψ(xjN(t))2dt+1N4iN(ζtN)0TEj,mN(ζtN):jm,j,mi|vϵ,z(xiN(t)-xjN(t))||vϵ,z(xiN(t)-xmN(t))|ϕ(xiN(t))2ψ(xjN(t))ψ(xmN(t))dt.

However, notice that this type of terms are already treated in the proof of Proposition 24.

We continue with (67). There are two terms and we bound them separately in the next two propositions.

Proposition 26

lim|z|0lim supϵ0E|1N50TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))|vϵ,z(xiN(t)-xjN(t))ϕ(xiN(t))ψ(xjN(t))|2dt|=0. 92

Proof

By (75) and coupling with the auxiliary free system, the pre-limit on the left-hand side of (92) can bounded by

(ϵ-1)21N50TEiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))ϕ(xiN(t))2ψ(xjN(t))2dt1N30TEij=1Nθϵ(yiϵ(t)-yjϵ(t))ϕ(yiϵ(t))2ψ(yjϵ(t))2dt1N0TEθϵ(y1ϵ(t)-y2ϵ(t))ϕ(y1ϵ(t))2ψ(y2ϵ(t))2dt=1N0T(R3)2θϵ(y1-y2)ϕ(y1)2ψ(y2)2ft12,ϵ(y1,y2)dy1dy2dt=O(N-1),

where θϵ=1 is used. This yields (92).

Proposition 27

lim|z|0lim supϵ01N5E0TiN(ζtN)jN(ζtN):jiθϵ(xiN(t)-xjN(t))·|kN(ζtN):ki,jvϵ,z(xiN(t)-xkN(t))ϕ(xiN(t))ψ(xkN(t))|2dt=0. 93

Proof

Th prelimit on the left-hand side of (93) can be bounded by

=1N5E0Tijk,i,jθϵ(xiN(t)-xjN(t))vϵ,z(xiN(t)-xkN(t))vϵ,z(xiN(t)-xN(t))ϕ(xiN(t))2ψ(xkN(t))ψ(xN(t))dtϵ-11N5E0Tij;k,i,jθϵ(xiN(t)-xjN(t))|vϵ,z(xiN(t)-xkN(t))|ϕ(xiN(t))2|ψ(xkN(t))ψ(xN(t))|dt,

where we have used (75). Using the auxiliary free system, its exchangeability, and that (y1ϵ(t),...,y4ϵ(t)) has a uniformly bounded density, see Proposition 7, we further bound the above by

1N40Tij;k,i,jθϵ(yiϵ(t)-yjϵ(t))|vϵ,z(yiϵ(t)-ykϵ(t))|ϕ(yiϵ(t))2|ψ(ykϵ(t))ψ(yϵ(t))|dt0Tθϵ(y1ϵ(t)-y2ϵ(t))|vϵ,z(y1ϵ(t)-y3ϵ(t))|ϕ(y1ϵ(t))2|ψ(y3ϵ(t))ψ(y4ϵ(t))|dt0T(R3)4θϵ(y1-y2)|vϵ,z(y1-y3)ϕ(y1)2|ψ(y3)ψ(y4)|ft1234,ϵ(y1,y2,y3,y4)dtK|vϵ,z(y3)|dy3,

where K is a compact set determined by the supports of ϕ,ψ, and we used that R3θϵ(y1-y2)dy2=1 for any y1. We already analyzed in (85) that K|vϵ,z(y3)|dy3ϵ2+(3|z|+2ϵ)2+|z|. This yields (93).

This completes the verification that all the terms (51), (53), (54), (55), (57), (58), (60), (63), (64), (65), (66) and (67) are negligible in the sense that lim|z|0lim supϵ0E|()|=0, where () stands for each of these terms.

Potential Theory and Consequence for Particle Coalescence

Let us summarize the result of our main theorem by saying that we have introduced a non-inertial model for particle coalescence, driven by a common noise, and we have obtained in the scaling limit a pde for the limit density with a mean coalescence rate R¯ given by

R¯=R¯ξ,σ2,R0:=R0R3θx1+uxdx

where u:R3R solves the auxiliary cell-equation

σ02Δu(x)+σ2·ω(ξx)u(x)=R0θ(x)1+u(x).

Let us develop a few potential theory preliminaries and deduce properties of R¯ξ,σ2,R0.

Given a uniformly elliptic, bounded and C1,α matrix-valued function A:R3R3×3, for some α(0,1), call GAx,y the associated Green kernel. Given a non-negative integrable Cα function θ:R3R with compact support in B(0, 1), for every γ>0 consider the elliptic problem

·Axuγx=γθx1+uγx. 94

There exists a unique C2(R3) solution uγ to (94), in the class of those u with |u(x)|0 as |x|. The proof is a modification of [13, Theorem 6.1]. Here we only repeat the proof of a weaker result, namely uniqueness within the class of those uC2 such that |u(x)|=O(|x|-1) and |u(x)|=O(|x|-2). In (74) we constructed explicitly a solution uγ to (94) that satisfies these decay conditions cf. Lemma 13 (but we use a different Green function there). To prove this claim, consider u1,u2 two solutions of (94) in this class and let u~=u1-u2. Then

·Axu~x=γθxu~x.

Multiplying u~ on both sides and integrating by parts in the ball B(0, R), we get

-B(0,R)u~(x)TA(x)u~(x)dx+B(0,R)u(x)A(x)u~(x)·dn(x)=B(0,R)γθ(x)u~(x)2,

where n(x) denotes the unit outward normal vector. Since A(x) is component-wise bounded, by the decay assumption,

B(0,R)u(x)A(x)u~(x)·dn(x)R-1R-2|B(0,R)|=O(R-1).

By the positive-definiteness of A, taking R we conclude that

R3u~(x)TA(x)u~(x)dx=R3γθ(x)u~(x)2=0

This forces u~(x)=u1(x)-u2(x)=0 for all xR3.

We proceed to define capacity for our divergence-form operator, a generalization of classical capacity in the case of Δ. Given a compact set KR3, consider the problems:

C1K,A:=infR3ψxTAxψxdx;ψxissmooth,ψ1inaneighborhoodofKC2K,A:=supμK;μmeasuresupportedinKs.t.R3GAx,yμdy1forallxR3.

By [2, Theorem 5.5.5 (i), Lemma 5.5.2, Definition 5.4.1] and [18, Theorem 4.1 and Eq. (6.5)], C1K,A=C2K,A and thus both can serve as equivalent definitions of capacity associated with operator A. Call it CapK,A.

Lemma 28

If KθR3 is the support of θ, then

limγγR3θx1+uγxdx=CapKθ,A.

Proof

Using the equivalent definition C2(K,A), the proof is the same as that of [13, Theorem 6.2].

Coming back to the problem of understanding R¯ξ,σ2,R0, the previous results imply:

Corollary 29

For every σ0,σ>0,

limR0R¯ξ,σ2,R0=CapKθ,σ02I3+σ2ωξ·.

Call “hard sphere coalescence” rate the number

R¯ξ,σ2:=CapKθ,σ02I3+σ2ωξ·,

over which we put our main attention.

Remark 30

We call it hard sphere coalescence, since as R0, the microscopic coalescence rate (20) tends to infinity, thus two particles that do interact (i.e. are ϵ-close) surely annihilate. That is, in this limit, our stochastic interaction rule becomes deterministic. This reminds us of deterministic collision as in Boltzmann’s theory of hard spheres. While we do not claim there is any essential connection to that area, see [24] for a study of particle approximation to Boltzmann equation with stochastic collision rate, where a rate similar to (20) appears.

Call CapKθ the classical capacity of Kθ (i.e. the one associated with Δ). Our main result for the theory of turbulent coalescence is:

Theorem 31

limξ0R¯ξ,σ2=σ02CapKθ
limξR¯ξ,σ2=σ02+σ2CapKθ.

Proof

Using the equivalent definition C1(K,A), the claims follow from the monotonicity of quadratic form in terms of the matrix ordering, since limξω(ξx)=I3 and limξ0ω(ξx)=0 for every x.

The first claim says that the coalescence rate becomes very small as the scale ratio ξ tends to zero, since σ02 is assumed very small with respect to the other constants. The second claim is expressed as a limit as ξ, in order to have a sharp mathematical result but from the viewpoint of physical interpretation it must be understood as a property just for non-small ξ. It clearly states that R¯ξ,σ2 increases with σ2, which was the other one of our desired properties.

Acknowledgements

We thank two anonymous referees who provided very insightful comments which allowed us to reach more precise and quantitative results and improve the exposition, and clarify also certain limitations. We thank Andrea Papini, Alessandra Lanotte and Jeremie Bec for important discussions, Francesco Russo and the organizers of the Winter School “Stochastic and deterministic analysis of irregular models”, Luminy 2024 which motivated the development of the result presented here. The research of the first author is funded by the European Union (ERC, NoisyFluid, No. 101053472). Views and opinions expressed are however those of the authors only and do not necessarily reflect those of the European Union or the European Research Council. Neither the European Union nor the granting authority can be held responsible for them. The research of the second author is funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany’s Excellence Strategy EXC 2044-390685587, Mathematics Münster: Dynamics-Geometry-Structure.

Funding

Open access funding provided by Scuola Normale Superiore within the CRUI-CARE Agreement.

Data Availability

Not applicable (no associated data).

Declarations

Conflict of interest

The authors have no relevant financial or non-financial interests to disclose.

Footnotes

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