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Research article

Edge-fault-tolerant strong Menger edge connectivity of bubble-sort graphs

  • This paper studies the edge-fault-tolerant strong Menger edge connectivity of n-dimensional bubble-sort graph Bn. We give the values of faulty edges that Bn can tolerant when Bn is strongly Menger edge connected under two conditions. When there are (n3) faulty edges removed from Bn, the Bn network is still working and it is strongly Menger edge connected. When the condition of any vertex in Bn has at least two neighbors is imposed, the number of faulty edges that can removed from Bn is (2n6) when Bn is also strongly Menger edge connected. And two special cases are used to illustrate the correctness of the conclusions. The conclusions can help improve the reliability of the interconnection networks.

    Citation: Yanling Wang, Shiying Wang. Edge-fault-tolerant strong Menger edge connectivity of bubble-sort graphs[J]. AIMS Mathematics, 2021, 6(12): 13210-13221. doi: 10.3934/math.2021763

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  • This paper studies the edge-fault-tolerant strong Menger edge connectivity of n-dimensional bubble-sort graph Bn. We give the values of faulty edges that Bn can tolerant when Bn is strongly Menger edge connected under two conditions. When there are (n3) faulty edges removed from Bn, the Bn network is still working and it is strongly Menger edge connected. When the condition of any vertex in Bn has at least two neighbors is imposed, the number of faulty edges that can removed from Bn is (2n6) when Bn is also strongly Menger edge connected. And two special cases are used to illustrate the correctness of the conclusions. The conclusions can help improve the reliability of the interconnection networks.



    This paper concerns a one-dimensional model of solid-fluid interaction:

    {tu+xf(u)=Kk=1λk(hk(t)u)δ(xhk(t)),(x,t)R×(0,T):=ΠT,mkhk(t)=λk(u(hk(t),t)hk(t)),t(0,T),k=1,,K,u(x,0)=u0(x),(hk(0),hk(0))=(hk,0,vk,0),k=1,,K. (1.1)

    Here f(u)=u2/2, and δ(x) denotes the Dirac delta measure concentrated at x=0. The function u=u(x,t) models the velocity of the fluid, hk(t) models the location of the kth solid particle at time t, λk>0 is a drag coefficient associated with the kth particle, and mk>0 is the mass of the kth particle. Study of the single-particle version of (1.1) was initiated in [11], and has been the subject of a number of additional papers.

    The fluid velocity is governed by the inviscid Burgers equation ut+f(u)x=0, and the particle-fluid coupling is due to friction, more specifically the drag terms λk(uhk) which appear in both the PDE and the ODEs in (1.1). Since there is no viscosity, the velocity u(x,t) admits entropy weak solutions, meaning that shock waves occur. This leads to complex interactions between the resulting shock wave and the particles. When multiple particles are present there are interesting features of the solutions that include particles drafting and passing by one another; see Figure 4 or Figure 5.

    Figure 4.  Example 8.3. Particle trajectories using basic scheme (upper plot) and MUSCL (lower plot). Both the true (thick line) and approximate (thin line) trajectories are plotted. For the MUSCL scheme (lower plot) the true and approximate trajectories are visually indistinguishable at this level of discretization. Δx=1.95×105, μ=.25, 102401 time steps.
    Figure 5.  Example 8.4. Basic scheme (left) and MUSCL (right). The horizontal axis represents x, and the vertical axis represents t. Top level plots: Δx1=3.75×104. Middle level plots: Δx2=12Δx1. Bottom level plots: Δx3=14Δx1. μ=.125 for all plots.

    There are some difficulties associated with (1.1), in addition to the well-known ones associated with a nonlinear conservation law. The source terms on the right side of the first equation are nonconservative products of distributions; their meaning is not immediately clear. The differential equations appearing in the second line are coupled to the conservation law. Due to discontinuities in u the meaning of the right side of the DE's is also not readily apparent. There are related difficulties in designing practical numerical algorithms.

    Notwithstanding these difficulties there has been much progress on the single-particle version of (1.1). A notion of solution has been developed, well-posedness has been proven, and numerical algorithms have been designed whose approximations are known to converge to the unique solution. In this paper we focus on the multiple-particle problem, which has not been studied as thoroughly. We propose a notion of entropy solution suitable for multiple particles, present a Lax-Friedrichs difference scheme for the multiple-particle problem, and prove that the resulting approximations converge to an entropy solution. This is accomplished under the assumption that the particle paths do not intersect except possibly at a set of times whose Lebesgue measure is zero.

    Reference [4] developed a unifying framework for the jump conditions that hold across a spatial flux discontinuity for a conservation law with discontinuous flux, using the theory of L1-dissipative (L1D) admissibility germs. The relevant L1D admissible germ for the problem discussed here is G(λ,c), which was identified in [7].

    Definition 1.1 (the germ G(λ,c), [7]] The germ G(λ,c) is the subset of R2 defined by

    G(λ,c)=(c,c)+{(a,b)R2|b=aλ}{(a,b)R2|a0,b0,λa+bλ}. (1.2)

    Reference [6] gives a definition of entropy solution for the single-particle version of (1.1). The following is a direct generalization of that definition to the multiple-particle problem.

    Definition 1.2 (entropy solution).

    (ⅰ) Given hkW1,([0,T],R), k=1,,K, let Γ=Kk=1{(hk(t),t)):t[0,T)}. A function u is a solution of the first equation of (1.1) with initial data u0 if uL(ΠT)C([0,T]);L1loc(R)), if u is a Kružkov entropy solution in ΠTΓ of the Burgers equation with initial data u0, and if for a.e. t(0,T) the one-sided traces of u at each particle position satisfy

    (u(hk(t),t),u(hk(t)+,t))G(λk(t),hk(t)),k=1,,K. (1.3)

    (ⅱ) A function hk is a solution of the second equation of (1.1) with initial data (hk,0,vk,0) if hkW2,([0,T]), if hk(0)=hk,0, hk(0)=vk,0, and if given given u a Kružkov entropy solution of the Burgers equation in ΠTΓ we have for a.e. t(0,T)

    mkhk(t)=(12u(hk(t),t)2hk(t)u(hk(t),t))(12u(hk(t)+,t)2hk(t)u(hk(t)+,t)). (1.4)

    (ⅲ) With the notation h=(h1,,hK), a pair (u,h) satisfying (ⅰ) and (ⅱ) above is an entropy solution of the system (1.1).

    Remark 1. Definition 1.2 requires strong one-sided traces u(hk(t)±,t) along each path x=hk(t). Assuming that the particle trajectories do not intersect except possibly on a subset of (0,T) having Lebesgue measure zero, the results of [13] guarantee existence of the required traces. This is due to the regularity of the paths x=hk(t) and the fact that u is a Kružkov entropy solution of the Burgers equation in ΠTΓ.

    Assumption 1.1. The initial data satisfies u0BV(R).

    Above we have used the notation BV(R) to denote the set of functions of bounded variation on R, i.e., those functions ρ:RR for which

    TV(ρ):=sup{Mi=1|ρ(ξi)ρ(ξi1)|}<,

    where the sup extends over all M1 and all partitions {ξ0<ξ1<<ξM} of R.

    Theorem 1.3 (Main theorem). The Lax-Friedrichs scheme described in Section 2 produces approximations that converge as the mesh size approaches zero, along a subsequence, to a pair (u,h) where uL(ΠT)C([0,T];L1loc(R)) and hkW2,([0,T]), k=1,,K. If the particle trajectories hk(t) do not intersect except possibly on a subset of (0,T) having Lebesgue measure zero, then (u,h) is an entropy solution in the sense of Definition 1.2.

    As mentioned above, there has been significant progress on the single-particle version of (1.1) [1,5,6,7,11]. The study of (1.1) started with reference [11]. Among other things the authors completely solved the Riemann problem for K=1, and described the asymptotic behavior of solutions.

    In reference [5], the authors introduce two finite volume methods for computing approximate solutions. One is a Glimm-like scheme, and the other is a well-balanced scheme that uses nonrectangular space-time cells near the interface. These methods employ random sampling for placing the particle at a mesh interface at each time step. The nonconservative source term is handled by using a certain well-balanced scheme that was analyzed in [7]. They avoid the use of a moving mesh, and also avoid the use of a Riemann solver for the full model. The case of multiple particles is addressed, and is handled via a splitting method.

    Reference [14] presents a finite volume scheme that is based on the well-balanced scheme of [5,7], but uses an adaptive stencil as an alternative to using a moving grid. The multiple-particle case is handled by splitting.

    Reference [7] proves well-posedness for the problem

    ut+(u2/2)x=λuδ(x),u(x,0)=u0(x). (1.5)

    This is a simplification of (1.1), but its analysis provides an important step in analyzing the full problem. As mentioned above the germ G(λ,c), which is required for the correct defintion of entropy solution, was identified in [7].

    Reference [6] proves well-posedness of the model (1.1) for K=1, assuming that the initial data is of bounded variation. Approximate solutions are generated via a wave-front tracking algorithm. Definition 1.2 is a direct generalization of the definition for K=1 appearing in [6].

    Reference [1] presents a class of finite volume schemes for (1.1) when K=1. The schemes are similar to those in [5], but a moving grid is used, which keeps the particle located at a fixed cell boundary. The approximations are shown to converge to the unique entropy solution.

    References [2] and [3] concern a generalized version of (1.1) (again, for K=1), where the fluid is governed by the inviscid compressible Euler equations.

    Reference [10] specifically deals with a multiple-particle problem. The authors prove well-posedness for a version of (1.1) where the particle paths hk(t) are given, i.e., the second equation of (1.1) does not appear.

    Let H() denote the Heaviside function, i.e., the characteristic function of [0,). The system (1.1) has the following equivalent formulation [5,11]:

    {tu+x(u2/2)=Kk=1λk(hk(t)u)xwk,(x,t)ΠT,twk+hk(t)xwk=0,(x,t)ΠT,k=1,,K,mkhk(t)=λk(u(hk(t),t)hk(t)),t(0,T),k=1,,K,u(x,0)=u0(x),(hk(0),hk(0))=(hk,0,vk,0),k=1,,K,wk(x,0)=H(xhk,0),k=1,,K. (1.6)

    Although the splitting approach for multiple particles used in [5] and [14] gives good numerical results, extending the convergence analysis from the single-particle to the multiple-particle problem seems difficult. Various bounds required for convergence are not preserved by the splitting steps. The numerical schemes in those papers are based on the model (1.1). In this paper we instead discretize (1.6), using Lax-Friedrichs differencing for each of the PDEs. The advantage of this approach is that the case of multiple particles is accommodated without splitting. This makes it possible to obtain a number of estimates which taken together give a convergence proof for the multiple-particle model. On the other hand, while the schemes of [1], [5], and [14] give very sharply resolved shocks at the particle locations, our Lax-Friedrichs method results in a substantial amount of smearing. With this in mind, we additionally propose a higher resolution version of the scheme, based on MUSCL processing.

    The rest of the paper is organized as follows. In Section 2 we describe the Lax-Friedrichs scheme mentioned above. In Section 3 we prove convergence, modulo a subsequence, of the approximations for u, as well as the approximations for hk. In Section 4 we prove convergence of the approximations for wk. In Section 5 we verify that the subsequential limit u is a Kružkov entropy solution in ΠTΓ and satisfies the jump condition (1.3). In Section 6 we prove that the limit hk satisfies the differential equation (1.4). Section 6 concludes with the proof of Theorem 1.3. Section 7 describes the MUSCL processing mentioned above. Section 8 presents the results of some numerical experiments.

    We use a uniform spatial mesh size Δx, and temporal step size Δt. Define

    xj=jΔx,jZ,tn=nΔt,0nN, (2.1)

    where the integer N is such that NΔt[T,T+Δt). Define Ij=[xjΔx/2,xj+Δx/2), In=[tn,tn+1). Let χj(x) denote the characteristic function of Ij, and χn(t) the characteristic function of In We denote by Unj the finite difference approximation of u(xj,tn), Unju(xj,tn). Similarly Wnk,jwk(xj,tn). Let {Qnj} be a grid-defined function such as {Unj} or {Wnk,j}. We will use the following notational abbreviations:

    Δ+Qnj=Qnj+1Qnj,ΔQnj=QnjQnj1,ˆQnj=12(Qnj1+Qnj+1),Qnmin=infjZQnj,Qnmax=supjZQnj,Qn=supjZ|Qnj|. (2.2)

    Let v0(x) denote the initial data u0(x) or H(xhk,0). The data v0(x) is discretized via V0j=1ΔxIjv0(x)dx, implying that

    infxIjv0(x)V0jsupxIjv0(x),andjZχj(x)V0jv0(x)inL1loc(R)asΔx0. (2.3)

    With the notation v0min=infyRv0(y), v0max=supyRv0(y), we have <v0min, v0max<. Due to our method of discretizing v0, v0minV0min, V0maxv0max, V0v0, and jZ|Δ+V0j|TV(v0).

    We extend {Unj} and {Wnk,j} from grid-defined functions to functions defined on all of ΠT via

    uΔ(x,t)=Nn=0jZχj(x)χn(t)Unj,wΔk(x,t)=Nn=0jZχj(x)χn(t)Wnk,j. (2.4)

    Similarly,

    cΔk(t)=Nn=0χn(t)cnk,hΔk(t)=Nn=0χn(t)(hnk+(ttn)cnk), (2.5)

    where cnkhk(tn) and hnkhk(tn), with the initialization (h0k,c0k)=(hk,0,vk,0)

    Let μ=Δt/Δx. The algorithm that we propose discretizes the first two equations of (1.6) via the Lax-Friedrichs scheme, the third equation using Euler's method:

    {Un+1j=UnjμΔˉfnj+1/2+Kk=1λkμ2(cnkˆUnj)(Wnk,j+1Wnk,j1),Wn+1k,j=Wnk,jμΔˉgnk,j+1/2,cn+1k=cnk1mkjZΔtλk2(cnkˆUnj)(Wnk,j+1Wnk,j1),hn+1k=hnk+cnkΔt. (2.6)

    Here

    ˉfnj+1/2=ˉf(Unj+1,Unj)=12((Unj+1)2/2+(Unj)2/2)q2μ(Unj+1Unj),ˉgnk,j+1/2=12(cnkWnk,j+1+cnkWnk,j)q2μ(Wnk,j+1Wnk,j), (2.7)

    where q is a parameter. For our purposes q(0,1/2]. The numerical fluxes in (2.7) result by applying the Lax-Friedrichs flux [12] to f(u)=u2/2 and gnk(w)=cnkw.

    Remark 2. The scheme (2.6) preserves solutions where the fluid velocity and particle velocities are equal to the same constant: Unj=v for all jZ, cnk=v for k=1,,K.

    Remark 3. Some explanation of the third equation of (2.6) is in order. Based on the third equation of (1.6), the third equation of (2.6) should be (approximately) equivalent to

    cn+1k=cnk1mkΔtλkcnk+1mkΔtλk˜u(hk(tn),tn),

    where ˜u(hk(tn),tn)u(hk(tn),tn). To see that the third equation of (2.6) is actually of this form, note that since Wnk,jH(xjhk(tn)), the grid function {(1/2)(Wnk,j+1Wnk,j1)/Δx} approximates δ(xhk(tn)), a delta function concentrated at x=hk(tn). In particular, we expect (1/2)jZ(Wnk,j+1Wnk,j1)1 (in fact this holds with ``'' replaced by ``=''; this follows from (3.5) of Lemma 3.1), and so we can write the third equation of (2.6) in the form

    cn+1k=cnk1mkΔtλkcnk+1mkΔtλk(1/2)jZˆUnj(Wnk,j+1Wnk,j1).

    Thus, by defining

    ˜u(hk(tn),tn):=(1/2)jZˆUnj(Wnk,j+1Wnk,j1)Ru(x,tn)δ(xhk(tn))dx,

    we have the desired approximation ˜u(hk(tn),tn)u(hk(tn),tn). Clearly there are other, possibly simpler, methods of discretizating the third equation of (1.6). The reason for choosing this particular approximation is to ensure the discrete conservation of momentum property discussed below.

    From the first two equations of (1.1) it follows that, at least formally, the total momentum of the system is conserved:

    ddt(Ru(x,t)dx+Kk=1mkhk(t))=0. (2.8)

    The scheme (2.6) enforces a discrete version of (2.8).

    Proposition 1. Assume that there is a 0<JZ such that Unj=0 for |j|>J, and that Un<. Define the discrete momentum:

    Mn=ΔxjZUnj+Kk=1mkcnk. (2.9)

    The discrete momentum is conserved: Mn+1=Mn for 0nN.

    Proof. Multiplying by Δx and summing the first equation of (2.6) over jZ gives

    ΔxjZUn+1j=ΔxjZUnj+jZKk=1λkΔt2(cnkˆUnj)(Wnk,j+1Wnk,j1). (2.10)

    Multiplying the third equation of (2.6) by mk and then summing over k gives

    Kk=1mkcn+1k=Kk=1mkcnkKk=1jZΔtλk2(cnkˆUnj)(Wnk,j+1Wnk,j1). (2.11)

    The proof is completed by adding (2.10) and (2.11).

    Define

    Znj=Unj+Kk=1λkWnk,j,zΔ(x,t)=Nn=0jZχj(x)χn(t)Znj. (2.12)

    Lemma 2.1. Znj satisfies the following (equivalent) evolution equations:

    Zn+1j=ZnjμΔˉf(Znj+1,Znj)+μ2Kk=1λkˆWnk,j(Znj+1Znj1), (2.13)
    Zn+1j=Znj+12(qμˆUnj)Δ+Znj12(q+μˆUnj)ΔZnj. (2.14)

    Remark 4. From (1.6) and the definition z=u+Kk=1λkwk, one can derive (formally) the PDE

    tz+xf(z)=Kk=1λkwkxz. (2.15)

    Evidently (2.13) is a discretization of (2.15).

    Remark 5. It is clear by inspection of either (2.13) or (2.14) that the scheme (2.6) preserves solutions of the form Znj=constant.

    Proof. Using (2.12) and (2.6) we find that

    Zn+1j=UnjμΔˉfnj+1/2+Kk=1λkμ2(cnkˆUnj)(Wnk,j+1Wnk,j1)+Kk=1λk(Wnk,jμΔˉgnk,j+1/2)=ZnjμΔˉfnj+1/2+Kk=1λkμ2(cnkˆUnj)(Wnk,j+1Wnk,j1)μKk=1λkΔˉgnk,j+1/2. (2.16)

    Next we use

    Δˉfnj+1/2=12ˆUnj(Unj+1Unj1)q2μΔ+ΔUnj,Δˉgnk,j+1/2=12cnk(Wnk,j+1Wnk,j1)q2μΔ+ΔWnk,j. (2.17)

    Substituting (2.17) into (2.16) and canceling (μ/2)Kk=1λkcnk(Wnk,j+1Wnk,j1), the result is

    Zn+1j=Znjμ2ˆUnj(Unj+1Unj1)+q2Δ+ΔUnjμ2ˆUnjKk=1λk(Wnk,j+1Wnk,j1)+q2Kk=1λkΔ+ΔWnk,j=Znjμ2ˆUnj(Znj+1Znj1)+q2Δ+ΔZnj=Znjμ2ˆUnj(Δ+Znj+ΔZnj)+q2(Δ+ZnjΔZnj). (2.18)

    The identity (2.14) is immediate from (2.18).

    For the proof of (2.13), we start from the second equality of (2.18) and substitute ˆUnj=ˆZnjKk=1λkˆWnk,j, which results in

    Zn+1j=Znjμ2(ˆZnjKk=1λkˆWnk,j)(Znj+1Znj1)+q2Δ+ΔZnj=Znjμ2ˆZnj(Znj+1Znj1)+μ2(Kk=1λkˆWnk,j)(Znj+1Znj1)+q2Δ+ΔZnj=Znjμ2(f(Znj+1)f(Znj1))+q2Δ+ΔZnj+μ2(Kk=1λkˆWnk,j)(Znj+1Znj1). (2.19)

    The identity (2.13) now follows directly from (2.19).

    Let Δ=(Δx,Δt). For our convergence analysis we will assume that Δ0 with μ fixed, and satisfying the following CFL condition:

    μmax(max1kK|c0k|,z0+Kk=1λk,u0+Kk=1λk)q1/2. (3.1)

    Additionally we assume that

    Δtmk/λk,k=1,,K, (3.2)

    which will be satisfied automatically for Δ sufficiently small.

    Define z0(x)=u0(x)+Kk=1λkH(xhk(0)). Due to the method of discretizing u0 and H(xhk(0)), it follows from from (2.12) that Z0j=1ΔxIjz0(x)dx. Using the notation z0min=infyRz0(y), z0max=supyRz0(y), we have <z0min, z0max<, and z0minZ0min, Z0maxz0max, and Z0z0.

    Lemma 3.1. The following properties hold:

    z0minZnjz0max,Znz0, (3.3)
    u0minKk=1λkUnju0max+Kk=1λk,Unu0+Kk=1λk, (3.4)
    Wnk,j[0,1],Δ+Wnk,j0,jZΔ+Wnk,j=1, (3.5)
    |cnk|max(|c0k|,u0+Kk=1λk). (3.6)

    Proof. The proof is by induction on n. Clearly all of (3.3), (3.4), (3.5), and (3.6) hold at n=0. Assume that those assertions hold at time step n. From (3.1) and the induction hypothesis it follows that

    μ(Zn+Kk=1λk)q,μ|cnk|q,k=1,,K. (3.7)

    To prove that (3.3) holds at time step n+1 we rewrite (2.14) using incremental coefficients:

    Zn+1j=Znj+Cnj+1/2Δ+ZnjDnj1/2ΔZnj, (3.8)

    where

    Cnj+1/2=12(qμˆUnj),Dnj1/2=12(q+μˆUnj). (3.9)

    Using ˆUnj=ˆZnjKk=1λkˆWnk,j, and ˆWnk,j[0,1] we see that Cnj+1/20, Dnj1/20 due to (3.7). At the same time Cnj+1/2+Dnj1/2=q1/2. Next we rewrite (3.8):

    Zn+1j=(1Cnj+1/2Dnj1/2)Znj+Cnj+1/2Znj+1+Dnj1/2Znj1. (3.10)

    From (3.10) it is clear that Zn+1j is a convex combination of Znj+1, Znj, Znj1, implying that ZnminZn+1jZnmax. Invoking the induction hypothesis then completes the proof of (3.3) for n+1.

    Next we prove that (3.5) holds for n+1. We rewrite the second equation of (2.6):

    Wn+1k,j=(1αnkβnk)Wnk,j+αnkWnk,j+1+βnkWnk,j1, (3.11)

    where

    αnk=12(qμcnk),βnk=12(q+μcnk). (3.12)

    By (3.7) we have αnk0, βnk0, and (3.1) implies αnk+βnk=q1/2. Thus Wn+1k,j is a convex combination of Wnk,j1,Wnk,j,Wnk,j+1, implying that Wn+1k,j[0,1] after invoking the induction hypothesis. By differencing (3.11) we get

    Δ+Wn+1k,j=(1αnkβnk)Δ+Wnk,j+αnkΔ+Wnk,j+1+βnkΔ+Wnk,j1. (3.13)

    Invoking the induction hypothesis again yields Δ+Wn+1k,j0. Finally, summing (3.13) over j and then applying the induction hypothesis yields jZΔ+Wn+1k,j=1.

    To prove (3.4) holds at n+1, we employ the result of the previous two paragraphs. Recalling (2.12), the proven bound on Zn+1j is equivalent to

    z0minKk=1λkWn+1k,jUn+1jz0maxKk=1λkWn+1k,j. (3.14)

    It is readily verified that u0minz0min and z0maxu0max+Kk=1λk. Replacing z0min and z0max in (3.14), the result is

    u0minKk=1λkWn+1k,jUn+1ju0max+Kk=1λkKk=1λkWn+1k,j. (3.15)

    Recalling that λk>0 and Wn+1k,j[0,1], it is clear that (3.4) holds.

    To verify that (3.6) holds for n+1, we start with the third formula of (2.6), from which it is evident that

    cn+1k=(1Δtλk2mkjZ(Wnk,j+1Wnk,j1))cnk+Δtλk2mkjZ(Wnk,j+1Wnk,j1)ˆUnj. (3.16)

    The induction hypothesis yields jZ(Wnk,j+1Wnk,j1)=2, and so after taking absolute values, and applying (3.2), equation (3.16) becomes

    |cn+1k|(1Δtλkmk)|cnk|+Δtλk2mkjZ(Wnk,j+1Wnk,j1)|ˆUnj|(1Δtλkmk)|cnk|+Δtλk2mkjZ(Wnk,j+1Wnk,j1)(u0+Kk=1λk)=(1Δtλkmk)|cnk|+Δtλkmk(u0+Kk=1λk)(1Δtλkmk)max(|c0k|,u0+Kk=1λk)+Δtλkmk(u0+Kk=1λk), (3.17)

    from which the desired inequality follows readily.

    Lemma 3.2. Unj and Znj satisfy spatial variation bounds:

    jZ|Δ+Znj|TV(u0)+Kk=1λk, (3.18)

    and

    jZ|Δ+Unj|TV(u0)+2Kk=1λk. (3.19)

    Proof. We claim that the scheme is a so-called Total Variation Decreasing (TVD) scheme with respect to the variable Znj, i.e.,

    jZ|Δ+Zn+1j|jZ|Δ+Znj|. (3.20)

    To prove the claim we use (3.8). We have shown that Cnj+1/2,Dnj+1/20. It suffices by a standard result [12,p. 116] to show that Cnj+1/2+Dnj+1/21. Using (3.9) we find that

    Cnj+1/2+Dnj+1/2=qμ4(Unj+1+Unj1)+μ4(Unj+2+Unj)q+μUnq+μ(u0+Kk=1λk)2q. (3.21)

    Here we have used (3.1) to get the last inequality. The desired bound then results by recalling that q1/2. Then by induction it follows from (3.18) that

    jZ|Δ+Znj|jZ|Δ+Z0j|TV(z0). (3.22)

    It is readily verified using (2.12) that

    jZ|Unj+1Unj|Kk=1λkjZ|Znj+1Znj|jZ|Unj+1Unj|+Kk=1λk. (3.23)

    Then (3.18) follows from (3.22) and the n=0 version of (3.23), along with the fact that jZ|Δ+U0j|TV(u0). Finally, (3.19) results from (3.18) and (3.23).

    Lemma 3.3. The following time continuity estimate holds:

    jZ|Un+1jUnj|B, (3.24)

    where the constant B is independent of Δ.

    Proof. Rearranging the first equation of (2.6), and using (2.17) to rewrite Δˉfnj+1/2 yields

    Un+1jUnj=12(qμˆUnj)Δ+Unj12(q+μˆUnj)ΔUnj+μ2Kk=1λk(cnkˆUnj)(Wnk,j+1Wnk,j1). (3.25)

    After taking absolute values, applying the triangle inequality, then using the bounds on cnk and ˆUnj provided by Lemma 3.1, we sum over jZ. The result is

    jZ|Un+1jUnj|B1jZ|Δ+Unj|+B2Kk=1jZ|Wnk,j+1Wnk,j1|, (3.26)

    where B1 and B2 are Δ-independent constants. The proof is completed by invoking Lemma 3.2, along with the observation that jZ|Wnk,j+1Wnk,j1|=2, which follows from (3.5).

    Lemma 3.4. The particle velocity approximations satisfy the following bound:

    |cn+1kcnk|λkΔtmk(max(|c0k|,u0+Kk=1λk)+u0+Kk=1λk). (3.27)

    Proof.

    We start with the third formula of (2.6). Subtracting cnk from both sides, taking absolute values, and then using the triangle inequality, the result is

    |cn+1kcnk|1mkjZΔtλk2|cnkˆUnj|(Wnk,j+1Wnk,j1)1mkjZΔtλk2(|cnk|+Un)(Wnk,j+1Wnk,j1)=Δtλkmk(|cnk|+Un). (3.28)

    The proof of (3.27) is completed using (3.4) and (3.6).

    Lemma 3.5. The approximations uΔ converge boundedly a.e. and in L1loc(ΠT) as Δ0, along a subsequence, to some uL(ΠT)C([0,T];L1loc(R)). For each k{1,,K} the sequence hΔk converges (along the same subsequence) in W1,([0,T]) to some hkW2,([0,T]), and cΔk converges (also along the same subsequence) to hk in L1loc((0,T)).

    Proof. The proof is a standard argument (e.g., the proof of Proposition 2.4 of [1]) using Lemmas 3.1, 3.2, and 3.3 for the u portion, and Lemmas 3.1 and 3.4 for the hk portion.

    Remark 6. In Sections 5 and 6 we will assume that the particle trajectories do not intersect except possibly on a subset of (0,T) having Lebesgue measure zero. The convergence result above holds without any assumptions about particle path intersections.

    In what follows (u,h) refers to a fixed subsequential limit of the type whose existence is guaranteed by Lemma 3.5. When taking the limit as Δ0 it is understood to be along this fixed subsequence.

    Lemma 4.1. Wnk,j satisfies a spatial variation bound and a time continuity estimate for each k{1,,K}:

    jZ|Δ+Wnk,j|=1,jZ|Wn+1k,jWnk,j|1/2. (4.1)

    Proof. The first part of (4.1) is evident from (3.5). For the second part of (4.1), we write (3.11) in the form

    Wn+1k,jWnk,j=αnkΔ+Wnk,jβnkΔWnk,j. (4.2)

    Taking absolute values, and recalling from the proof of Lemma 3.1 that αnk,βnk[0,1] yields

    |Wn+1k,jWnj|αnk|Δ+Wnk,j|+βnk|ΔWnk,j|. (4.3)

    Then summing over jZ and using jZ|Δ+Wnk,j|=1, αnk+βnk1/2, gives the second part of (4.1)

    Lemma 4.2. As Δ0, wΔk(x,t)H(xhk(t)) boundedly a.e. and in L1loc(ΠT) for each k{1,,K}.

    Proof. Lemma 4.1 along with Wnk,j[0,1] (Lemma 3.1) guarantees that wΔk converges along a subsequence in L1loc(R+×R) and boundedly a.e. to some wkL(ΠT)C([0,T];L1loc(R)).

    A standard Lax-Wendroff calculation [9] proves that wk is a weak solution of

    twk+hk(t)xwk=0,wk(x,0)=H(xhk(0)). (4.4)

    One such weak solution is wk(x,t)=H(xhk(t)). We will show that this is the only weak solution and the proof will be complete. Assume that wk and ˜wk are both weak solutions of (4.4). This implies that for every ϕC0(R×[0,T]),

    T0R(˜wkwk){ϕt+hk(t)ϕx}dxdt=T0(˜wkwk)ϕ(x,T)dt. (4.5)

    Fix ψC0(R×[0,T]). Let

    ϕ(x,t)=tTψ(xhk(t)+hk(σ),σ)dσ. (4.6)

    It is readily verified that ϕt+hk(t)ϕx=ψ, ϕ(,T)=0. Substituting into (4.5), we have

    T0R(˜wkwk)ψ(x,t)dxdt=0. (4.7)

    Since (4.7) holds for any ψC0(R×[0,T]), we conclude that w=˜w a.e.

    The following lemma is a direct consequence of (2.12), Lemma 3.5, and Lemma 4.2.

    Lemma 4.3. Define z(x,t)=u(x,t)+Kk=1λkH(xhk(t)). As Δ0, zΔ(x,t)z(x,t) boundedly a.e. and in L1loc(ΠT).

    In this section we verify that the subsequential limit u is a Kružkov entropy solution in ΠTΓ and satisfies the jump condition (1.3).

    Here and in Section 6 we will employ the test function 0ψδ(x)C0(R), δ>0, such that ψδ(0)=1, supp(ψδ)=[δ,δ], and

    ψδ(x)={ηδ(x+δ/2),x0,ηδ(xδ/2),x0, (5.1)

    where ηδ denotes the standard C(R) mollifier:

    supp(ηδ)=[δ/2,δ/2],ηδ(x)0xR,Rηδ(x)dx=1. (5.2)

    Assumption 5.1. Assume that the particle trajectories do not intersect except possibly on a subset F(0,T) having Lebesgue measure zero.

    Remark 7. The set F has the form F=ijFi,j, where

    Fi,j:={t(0,T)|hi(t)=hj(t)}.

    Since each of the particle paths thk(t) is continuous, each Fi,j is closed, and thus F is also a closed subset of (0,T). There are no particle path intersections in the open set E:=(0,T)F. E is a countable disjoint union of open intervals, E=Mm=1(am,bm), where 1M and each (am,bm)(0,T). By Assumption 2, E is of full measure, meas((0,T)E)=0.

    Lemma 5.1. Define U=[u0minKk=1λk,u0max+Kk=1λk]. Referring to (2.6), let G(Unj+1,Unj,Unj1)=UnjμΔˉfnj+1/2. Then G is nondecreasing with respect to each of Unj+1,Unj,Unj1 if Unj+1,Unj,Unj1U. Referring to (2.13),Zn+1j is nondecreasing with respect to each of Znj+1,Znj,Znj1 if Znj+1,Znj,Znj1[z0min,z0max].

    Proof. The partial derivatives of G are

    GUnj=1q,GUnj+1=μ2Unj+1+q2,GUnj1=μ2Unj1+q2. (5.3)

    Clearly G/Unj0 since q1/2. For Un+1j/Unj±1,

    GUnj±112(qμUn)12(qμ(u0+Kk=1λk)). (5.4)

    In view of (5.4) and (3.1) it is clear that G/Unj±10.

    For Zn+1j we use (2.13) to compute

    Zn+1jZnj=1q,Zn+1jZnj+1=q2μ2Znj+1+μ2Kk=1λkˆWnk,j,Zn+1jZnj1=q2+μ2Znj1μ2Kk=1λkˆWnk,j. (5.5)

    It is readily verified that each of these partial derivatives is nonnegative using (3.1) and the fact that ˆWnk,j[0,1].

    The following lemma is a straightforward consequence of (3.5) and Lemma 4.2.

    Lemma 5.2. Define

    Snj=Kk=1λkˆWnk,j,SΔ(x,t)=Nn=0jZχj(x)χn(t)Snj. (5.6)

    Snj has the following properties:

    0SnjKk=1λk,Δ+Snj0,jZΔ+Snj=Kk=1λk, (5.7)

    and as Δ0, SΔ(x,t)Kk=1λkH(xhk(t)) boundedly a.e. and in L1loc(ΠT).

    Lemma 5.3. The following discrete entropy inequalities hold for all κ[z0min,z0max]:

    Zn+1jκZnjκμΔˉf(Znj+1κ,Znjκ)+μ2Snj(Znj+1κZnj1κ),Zn+1jκZnjκμΔˉf(Znj+1κ,Znjκ)+μ2Snj(Znj+1κZnj1κ). (5.8)

    Proof. Writing (2.13) in the form Zn+1j=P(Znj+1,Znj,Znj1), it is readily apparent that P(κ,κ,κ)=κ. Using this observation the proof is a standard calculation [8,9], using the fact that P is a nondecreasing function of all three arguments (Lemma 5.1).

    Lemma 5.4. The limit solution u satisfies the jump condition (1.3) for a.e. t(0,T) and each k1,,K.

    Proof. We start with the first inequality in (5.8), and use the identity

    Aj(Bj+1Bj1)=Δ+(AjBj)Bj+1Δ+Aj+Δ(AjBj)Bj1ΔAj. (5.9)

    This results in

    Zn+1jκZnjκμΔ(ˉf(Znj+1κ,Znjκ)12Snj+1(Znj+1κ)12Snj(Znjκ))μ2((Znj+1κ)Δ+Snj+(Znj1κ)ΔSnj). (5.10)

    Since Δ±Snj0, we have

    (Znj+1κ)Δ+SnjκΔ+Snj,(Znj1κ)ΔSnjκΔSnj, (5.11)

    and so we can replace (5.10) by

    Zn+1jκZnjκμΔ(ˉf(Znj+1κ,Znjκ)12Snj+1(Znj+1κ)12Snj(Znjκ))μκ2(Snj+1Snj1). (5.12)

    Following the proof of the Lax-Wendroff theorem [9], let ϕ be a nonnegative test function with ϕ(x,0)=0, and ϕnj:=ϕ(xj,tn). We multiply (5.12) by ϕnjΔx, and then sum over jZ, n0. After summation by parts the result is

    ΔxΔtjZn0(Zn+1jκ)ϕn+1jϕnjΔt+ΔxΔtjZn0(ˉf(Znj+1κ,Znjκ)12Snj(Znjκ)12Snj+1(Znj+1κ))Δ+ϕnjΔx+ΔxΔtκjZn0SnjΔ+ϕnjΔx0. (5.13)

    Letting Δ0 and recalling zΔz, SΔKk=1λkH(xhk(t)) yields

    T0R(zκ)ϕtdxdt+T0R(f(zκ)Kl=1λlH(xhl(t))(zκ))ϕxdxdt+κT0RKl=1λlH(xhl(t))ϕxdxdt0. (5.14)

    After simplifying the last integral the result is

    T0R(zκ)ϕtdxdt+T0R(f(zκ)Kl=1λlH(xhl(t))(zκ))ϕxdxdtκKl=1λlT0ϕ(hl(t),t)dt0. (5.15)

    A similar calculation starting from the second inequality of (5.8) yields

    T0R(zκ)ϕtdxdt+T0R(f(zκ)Kl=1λlH(xhl(t))(zκ))ϕxdxdtκKl=1λlT0ϕ(hl(t),t)dt0. (5.16)

    Recalling Assumption 5.1 and Remark 7, fix an interval Im:=(am,bm)(0,T) where there are no path intersections, and fix a particle path, indexed by k. For this calculation we will use the abbreviations z±(t)=z(hk(t)±,t) and ck(t)=hk(t). The ordering of the particles does not change in Im, so we can assume that the particles are labeled so that

    h1(t)<h2(t)<<hk(t)<<hK(t),tIm. (5.17)

    Let ϕ(x,t)=ψδ(xhk(t))ρ(t), where 0ρC0(Im). Letting δ0 in (5.15) yields

    Im{f(zκ)ck(zκ)(f(z+κ)ck(z+κ)λk(z+κ))γk(zκz+κ)λkκ}ρ(t)dt0, (5.18)

    where γk=l<kλl, and we have abbreviated z±=z±(t), ck=ck(t). Another such test function calculation, this time with (5.16) results in

    Im{f(zκ)ck(zκ)(f(z+κ)ck(z+κ)λk(z+κ))γk(zκz+κ)λkκ}ρ(t)dt0. (5.19)

    Continuing with the abbreviation z±=z±(t), ck=ck(t), for a.e. tIm we have

    f(zκ)ck(zκ)(f(z+κ)ck(z+κ)λk(z+κ))γk(zκz+κ)λkκ0, (5.20)
    f(zκ)ck(zκ)(f(z+κ)ck(z+κ)λk(z+κ))γk(zκz+κ)λkκ0. (5.21)

    Fix a time tIm where (5.20), (5.21) hold. If z=z+ then (5.20) and (5.21) are satisfied. So assume for now that zz+. Substituting zκz+ into (5.20) and then (5.21) gives

    zκz+{f(z+)f(κ)(λk+˜ck)(z+κ),f(z)f(κ)˜ck(zκ). (5.22)

    where ˜ck=ck+γk. Repeating this calculation with z+κz, we find that

    z+κz{f(z+)f(κ)(λk+˜ck)(z+κ),f(z)f(κ)˜ck(zκ). (5.23)

    Plugging κ=z into the first inequality of (5.22) and then into the first inequality of (5.23), and recalling f(z)=z2/2, yields

    z++z2(λk+˜ck). (5.24)

    The second inequality of (5.22) (for z<z+) or the second inequality of (5.23) (for z>z+) implies that in either case

    z˜ck. (5.25)

    Substituting κ=z+ into the second inequalities of (5.22) and (5.23) yields

    z++z2˜ck. (5.26)

    Finally, with ϵ>0, we substitute κ=z+ϵ into the first inequality of (5.22), and κ=z++ϵ into the first inequality of (5.23). Sending ϵ0 results in

    z+λk+˜ck. (5.27)

    Thus either z+=z or all of (5.24), (5.25), (5.26), (5.27) hold. Let u±=u(hk(t)±,t). Substituting z=u+γk, z+=u++γk+λk into these relationships we have shown that either

    u+ck=uckλk, (5.28)

    or

    uck0,u+ck0,λk(uck)+(u+ck)λk. (5.29)

    Recalling Definition 1.1, and that ck=hk(t), it is evident from (5.28), (5.29) that

    (u,u+)G(λk,ck)=G(λk,hk(t)), (5.30)

    and this holds for a.e. tIm. The proof is completed by repeating this argument for each k{1,,K} and each m{1,,M}.

    Lemma 5.5. The following discrete entropy inequality holds for each κR:

    |Un+1jκ||Unjκ|μΔˉF(Unj+1,Unj)+μ2Kk=1λk|cnkˆUnj|(Wnk,j+1Wnk,j1), (5.31)

    where \bar{F}\left(U_{j+1}^{n},U_j^{n} \right) = \bar{f}(U_{j+1}^n \vee \kappa,U_{j}^n \vee \kappa) - \bar{f}(U_{j+1}^n \wedge \kappa,U_{j}^n \wedge \kappa) .

    Proof. First assume that \kappa \in \mathcal{U} = [ u^0_{\min}-\sum_{k = 1}^K \lambda_k, u^0_{\max} + \sum_{k = 1}^K \lambda_k] . We write the first equation of (2.6) in the form

    \begin{equation} U_j^{n+1} = G(U_{j+1}^n,U_j^n,U_{j-1}^n) +Q_j^n, \end{equation} (5.32)

    where

    \begin{equation} \begin{split} &V_j^{n+1}: = G(U_{j+1}^n,U_j^n,U_{j-1}^n) = U_j^n - \mu \Delta_- \bar{f}^n_{ j+1/2}, \\ &Q_j^n = {{\mu}\over 2}\sum\limits_{k = 1}^K \lambda_k \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right). \end{split} \end{equation} (5.33)

    Invoking the monotonicity of G (Lemma 5.1), a standard calculation [8,9] yields

    \begin{equation} \left|{V_j^{n+1} - \kappa}\right| \le \left|{U_j^{n} - \kappa}\right| - \mu \Delta_- \bar{F}\left(U_{j+1}^{n},U_j^{n} \right), \end{equation} (5.34)

    for \kappa \in \mathcal{U} . Substituting V_j^{n+1} = U_j^{n+1} - Q_j^n , and using the triangle inequality yields (5.31), assuming \kappa \in \mathcal{U} .

    Now take the case where \kappa \notin \mathcal{U} , say \kappa < u^0_{\min} - \sum_{k = 1}^K \lambda_k . In that case (5.31) reduces to

    \begin{equation} U_j^{n+1} \le U_j^n -\mu \Delta_- \bar{f}^n_{ j+1/2} + \left|{Q_j^n}\right|. \end{equation} (5.35)

    which, recalling the first equation of (2.6), is clearly satisfied. The case where \kappa > u^0_{\max} + \sum_{k = 1}^K \lambda_k is handled similarly.

    Lemma 5.6. The limit u is a Kružkov entropy solution in \Pi_T \setminus \Gamma of the Burgers equation with initial data u_0 .

    Proof. Define F(a,b) = f(a\vee b)-f(a\wedge b) = \operatorname*{sgn}(a-b)(a^2/2 - b^2/2) . We must show that u satisfies

    \begin{equation} \int_0^T \int_{ \mathbb{R}} \left(\left|{u-\kappa}\right|\phi_t + F(u,\kappa) \phi_x \right) \,dx \,dt + \int_R \left|{u_0 - \kappa}\right| \phi(x,0) \,dx \ge 0 \end{equation} (5.36)

    for every \kappa \in \mathbb{R} and every nonnegative test function \phi \in C_0^{\infty}\left( \mathbb{R} \times [0,T) \setminus \Gamma \right) .

    The proof is based on the discrete entropy inequality (5.31). Due to the bounds on U_j^n and c_k^n (Lemma 3.1), we have for some B>0 which independent of \Delta ,

    \begin{equation} {{\mu}\over 2}\sum\limits_{k = 1}^K \lambda_k \left|{c_k^n-\hat{U}_j^n}\right| \left(W_{k,j+1}^n - W_{k,j-1}^n \right) \le {{ \mu}\over 2}B \sum\limits_{k = 1}^K \lambda_k \left(W_{k,j+1}^n - W_{k,j-1}^n \right). \end{equation} (5.37)

    Substituting into (5.31) the result is

    \begin{equation} \left|{U_j^{n+1} - \kappa}\right| \le \left|{U_j^{n} - \kappa}\right| - \mu \Delta_- \bar{F}\left(U_{j+1}^{n},U_j^{n} \right) + {{\mu}\over 2}B\sum\limits_{k = 1}^K \lambda_k \left(W_{k,j+1}^n - W_{k,j-1}^n \right). \end{equation} (5.38)

    Multiplying by \phi_j^n = \phi(x_j,t^n) and then summing by parts we find that

    \begin{equation} \begin{split} & \Delta x \Delta t\sum\limits_{n = 0}^N \sum\limits_{j \in \mathbb{Z}} \left\{\left|{U_j^{n+1} - \kappa}\right| (\phi_j^{n+1}- \phi_j^n)/ \Delta t +\bar{F}\left(U_{j+1}^{n},U_j^{n} \right) (\phi_{j+1}^{n}- \phi_j^n)/ \Delta x \right\}\\ &-B\sum\limits_{k = 1}^K \lambda_k \Delta x \Delta t\sum\limits_{n = 0}^N \sum\limits_{j \in \mathbb{Z}} W_{k,j}^n {1\over 2}(\phi_{j+1}^{n}- \phi_{j-1}^n)/ \Delta x + \Delta x \sum\limits_{j \in \mathbb{Z}} \left|{U_j^{0} - \kappa}\right|\phi_j^0 \,dx \ge 0. \end{split} \end{equation} (5.39)

    Letting \Delta \rightarrow 0 , and using u^{ \Delta} \rightarrow u , w_k^{ \Delta} \rightarrow H(x-h_k(t)) , results in

    \begin{equation} \begin{split} &\int_0^T \int_{ \mathbb{R}} \left(\left|{u-\kappa}\right| \phi_t + F(u,\kappa)\phi_x \right) \,dx \,dt - B\sum\limits_{k = 1}^K \lambda_k \int_0^T \int_{ \mathbb{R}} H(x-h_k(t)) \phi_x \,dx \,dt \\ &+ \int_{ \mathbb{R}} \left|{u_0(x) - \kappa}\right| \, dx \ge 0. \end{split} \end{equation} (5.40)

    The proof is finished by observing that \int_{ \mathbb{R}} H(x-h_k(t)) \phi_x \,dx = 0 , since \phi(h_k(t),t) = 0 .

    In this section we prove that the limit h_k satisfies the differential equation (1.4). This section also contains the proof of Theorem 1.3. Assumption 5.1 (restriction on particle intersections) remains in effect in this section.

    Lemma 6.1. The limit h_k(t) satisfies the differential equation (1.4) for each k \in {1,\ldots,K} and a.e. t \in (0,T) . Also, (h_k(0),h_k'(0)) = (h_{k,0},v_{k,0}) .

    Proof. Fix a particle with index k , 1\le k \le K . Let a_k^n = (c_k^{n+1}-c_k^n)/\Delta t . The third equation of (2.6) yields

    \begin{equation} m_k a_k^n = -\sum\limits_{j \in \mathbb{Z}} {{ \lambda_k}\over 2}\left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right). \end{equation} (6.1)

    Define \psi_j^n = \psi_{\delta}(x_j - h_k(t^n)) , where \psi_{\delta} is defined by (5.1). Let \xi(t) \in \mathcal{C}^{\infty}_0((0,T)) and define \xi^n = \xi(t^n) . We re-write (6.1) in the form

    \begin{equation} \begin{split} m_k a_k^n & = -{{\lambda_k}\over{2}}\sum\limits_{j\in \mathbb{Z}} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) \psi_j^n\\ &\quad - {{\lambda_k}\over{2}}\sum\limits_{j\in \mathbb{Z}} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) (1-\psi_j^n). \end{split} \end{equation} (6.2)

    Next we multiply by \xi^n \Delta t and sum over n:

    \begin{equation} \begin{split} m_k \Delta t \sum\limits_{n\ge 0} a_k^n \xi^n & = - {{\lambda_k}\over{2}}\Delta t \sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) \psi_j^n \xi^n\\ &- {{\lambda_k}\over{2}} \Delta t\sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) (1-\psi_j^n) \xi^n. \end{split} \end{equation} (6.3)

    We solve for \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) in the first equation of (2.6),

    \begin{equation} \begin{split} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right)& = {2 \over {\lambda_k \mu}}\left( U_j^{n+1}-U_j^n + \mu \Delta_- \bar{f}^n_{ j+1/2}\right)\\ &-{1 \over{\lambda_k}} \sum\limits_{l\neq k} \lambda_l \left(c_l^n - \hat{U}_j^n \right) \left(W^n_{l,j+1}-W^n_{l,j-1} \right), \end{split} \end{equation} (6.4)

    and substitute into the first sum on the right side of (6.3). The result is

    \begin{equation} \begin{split} m_k \Delta t\sum\limits_{n\ge 0} a_k^n \xi^n & = -\underbrace{\Delta x\sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \left(U_j^{n+1}-U_j^n + \mu \Delta_- \bar{f}^n_{ j+1/2}\right) \psi_j^n \xi^n}_{ \mathcal{S}_1}\\ +& \underbrace{{1\over 2} \Delta t \sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \sum\limits_{l\neq k}\lambda_l\left(c_l^n - \hat{U}_j^n \right) \left(W^n_{l,j+1}-W^n_{l,j-1} \right) \psi_j^n \xi^n }_{ \mathcal{S}_2}\\ - &{{\lambda_k}\over{2}} \underbrace{\Delta t \sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \left(c_k^n - \hat{U}_j^n \right) \left(W^n_{k,j+1}-W^n_{k,j-1} \right) (1-\psi_j^n) \xi^n}_{ \mathcal{S}_3}.\\ \end{split} \end{equation} (6.5)

    Summing the left side of (6.5) by parts, we find that

    \begin{equation} m_k \Delta t\sum\limits_{n\ge 0} a_k^n \xi^n = -m_k \Delta t \sum\limits_{n \ge 0} c_k^{n+1} {{\xi^{n+1}-\xi^n}\over{ \Delta t}}. \end{equation} (6.6)

    Letting \Delta \downarrow 0 in (6.6), and using c_k^{ \Delta} \rightarrow h_k' , the result is

    \begin{equation} m_k \Delta t \sum\limits_{n\ge 0} a_k^n \xi^n \rightarrow -m_k \int_0^T h_k'(t) \xi'(t) \, dt, \end{equation} (6.7)

    and for \mathcal{S}_1 , summation by parts followed by sending \Delta \rightarrow 0 yields

    \begin{equation} \mathcal{S}_1 \rightarrow \int_0^T \int_{ \mathbb{R}} \left\{u\, \partial_t \left(\psi_{\delta}(x-h_k(t)) \xi(t)\right) + f(u) \,\partial_x \left(\psi_{\delta}(x-h_k(t)) \xi(t)\right) \right\} \,dx \,dt. \end{equation} (6.8)

    We next estimate \mathcal{S}_2 . Fix l \ne k . It suffices to estimate \mathcal{S}_{2,l} , where

    \begin{equation} \mathcal{S}_{2,l} = {1\over 2} \Delta t \sum\limits_{n\ge 0}\sum\limits_{j\in \mathbb{Z}} \lambda_l\left(c_l^n - \hat{U}_j^n \right) \left(W^n_{l,j+1}-W^n_{l,j-1} \right) \psi_j^n \xi^n. \end{equation} (6.9)

    Since c_l^n and \hat{U}_j^n are bounded (Lemma 3.1), and \left(W^n_{l,j+1}-W^n_{l,j-1} \right) \ge 0 , \psi_j^n \ge 0 ,

    \begin{equation} \left|{ \mathcal{S}_{2,l}}\right| \le B \Delta t\sum\limits_{n\ge 0} \left|{\xi^n}\right|\sum\limits_{j\in \mathbb{Z}} \left(W^n_{l,j+1}-W^n_{l,j-1} \right) \psi_j^n \end{equation} (6.10)

    where B is some positive number independent of \delta and \Delta . Summation by parts yields

    \begin{equation} \begin{split} \sum\limits_{j\in \mathbb{Z}} \left(W^n_{l,j+1}-W^n_{l,j-1} \right) \psi_j^n & = \sum\limits_{j \in \mathbb{Z}}\left(W^n_{l,j+1}\psi_{j+1}^n - W^n_{l,j-1}\psi_{j-1}^n\right)\\ &- \sum\limits_{j \in \mathbb{Z}} \left(W^n_{l,j+1}+W^n_{l,j} \right)\Delta_+ \psi_{j}^n. \end{split} \end{equation} (6.11)

    The first sum on the right is telescoping and is equal to zero. Thus, referring back to (6.10) we have

    \begin{equation} \begin{split} \left|{ \mathcal{S}_{2,l}}\right| &\le - B \Delta t \sum\limits_{n\ge 0} \left|{\xi^n }\right| \sum\limits_{j \in \mathbb{Z}} \left(W_{l,j+1}+W_{l,j} \right)\Delta_+ \psi_{j}^n\\ & = - 2B \Delta x \Delta t \sum\limits_{n\ge 0} \left|{\xi^n }\right| \sum\limits_{j \in \mathbb{Z}} {1\over2}\left(W_{l,j+1}+W_{l,j} \right)\Delta_+ \psi_{j}^n/ \Delta x. \end{split} \end{equation} (6.12)

    Letting \Delta \rightarrow 0 yields

    \begin{equation} \limsup\limits_{ \Delta \rightarrow 0} \left|{ \mathcal{S}_{2,l}}\right| \le - 2B \int_0^T \left|{\xi(t)}\right| \int_{ \mathbb{R}}w_l(x,t) \partial_x \psi_{\delta}(x-h_k(t)) \, dx \, dt. \end{equation} (6.13)

    Recalling that w_l(x,t) = H(x-h_l(t)) , we find that

    \begin{equation} \begin{split} \int_{ \mathbb{R}}w_l(x,t) \partial_x \psi_{\delta}(x-h_k(t)) \, dx & = \int_{x = h_l(t)}^{\infty} \partial_x \psi_{\delta}(x - h_k(t)) \, dx = - \psi_{\delta}(h_l(t)-h_k(t)).\\ \end{split} \end{equation} (6.14)

    Substituting into (6.13) yields the desired estimate of \mathcal{S}_{2,l} :

    \begin{equation} \limsup\limits_{ \Delta \rightarrow 0} \left|{ \mathcal{S}_{2,l}}\right| \le 2B\int_0^T \left|{\xi(t)}\right| \psi_{\delta}(h_l(t)-h_k(t)) \, dt. \end{equation} (6.15)

    We claim that \mathcal{S}_3 \rightarrow 0 . Since c_k^n and \hat{U}_j^n are bounded (Lemma 3.1), and \psi_j^n \le 1 , W^n_{k,j+1}-W^n_{k,j-1} \ge 0 ,

    \begin{equation} \left|{ \mathcal{S}_3}\right| \le B \Delta t\sum\limits_{n\ge 0} \left|{\xi^n}\right|\sum\limits_{j\in \mathbb{Z}} \left(W^n_{k,j+1}-W^n_{k,j-1} \right) (1-\psi_j^n). \end{equation} (6.16)

    where B is some positive number independent of the mesh size \Delta . Using the formula (6.11) with 1-\psi_j^n replacing \psi_j^n ,

    \begin{equation} \begin{split} \sum\limits_{j\in \mathbb{Z}} \left(W^n_{k,j+1}-W^n_{k,j-1} \right) (1-\psi_j^n) & = \sum\limits_{j \in \mathbb{Z}}\left(W^n_{k,j+1}(1-\psi_{j+1}^n) - W^n_{k,j-1}(1-\psi_{j-1}^n)\right)\\ &+ \sum\limits_{j \in \mathbb{Z}} \left(W^n_{k,j+1}+W^n_{k,j} \right)\Delta_+ \psi_{j}^n. \end{split} \end{equation} (6.17)

    In the second term on the right side we have used \Delta_+(1-\psi_{j}^n) = -\Delta_+\psi_{j}^n . The first sum on the right is telescoping and is equal to 2 . Thus, referring back to (6.16) we have

    \begin{equation} \begin{split} \left|{ \mathcal{S}_3}\right| &\le 2 B \Delta t\sum\limits_{n\ge 0} \left|{\xi^n}\right| + B \Delta t \sum\limits_{n\ge 0} \left|{\xi^n }\right| \sum\limits_{j \in \mathbb{Z}} \left(W_{k,j+1}+W_{k,j} \right)\Delta_+\psi_{j}^n\\ & = 2 B \Delta t\sum\limits_{n\ge 0} \left|{\xi^n}\right| + 2B \Delta t \Delta x\sum\limits_{n\ge 0} \left|{\xi^n }\right| \sum\limits_{j \in \mathbb{Z}} {1\over2}\left(W_{k,j+1}+W_{k,j} \right)\Delta_+\psi_{j}^n/ \Delta x. \end{split} \end{equation} (6.18)

    Letting \Delta \rightarrow 0 yields

    \begin{equation} \limsup\limits_{ \Delta \rightarrow 0} \left|{ \mathcal{S}_3}\right| \le 2 B \int_0^T \left|{\xi(t)}\right|\, dt + 2B \int_0^T \left|{\xi(t)}\right| \int_{ \mathbb{R}}w_k(x,t) \partial_x \psi_{\delta}(x-h_k(t) \, dx \, dt. \end{equation} (6.19)

    Substituting w_k(x,t) = H(x-h_k(t)) , and using \psi_{\delta}(0) = 1 , the result is

    \begin{equation} \begin{split} \int_{ \mathbb{R}}w_k(x,t) \partial_x \psi_{\delta}(x-h_k(t)) \, dx & = \int_{x = h_k(t)}^{\infty} \partial_x \psi_{\delta}(x-h_k(t)) \, dx = -1. \end{split} \end{equation} (6.20)

    Plugging (6.20) into (6.19) completes the proof of the claim.

    Combining \mathcal{S}_3 \rightarrow 0 with (6.7), (6.8), and (6.15) we have

    \begin{equation} \begin{split} & -m_k \int_0^T h_k'(t) \xi'(t) \, dt = \\ & \int_0^T \int_{ \mathbb{R}} \left\{u (\psi_{\delta}(x-h_k(t)) \xi(t))_t + f(u) (\psi_{\delta}(x-h_k(t)) \xi(t))_x \right\} \,dx \,dt\\ &+\int_{ \mathbb{R}} u_0(x) \psi_{\delta}(x-h_k(0)) \xi(0) \, dx +R_k, \end{split} \end{equation} (6.21)

    where

    \begin{equation} \left|{R_k}\right| \le 2B \sum\limits_{l\neq k} \int_0^T \left|{\xi(t)}\right| \psi_{\delta}(h_l(t)-h_k(t)) \, dt. \end{equation} (6.22)

    Next we consider the limit when \delta \rightarrow 0 in (6.21), (6.22). Due to Assumption 5.1 (restriction on particle intersections), if l \neq k then \left|{h_l(t)-h_k(t)}\right|>0 for a.e. t \in (0,T) and thus

    \begin{equation} {\psi_{\delta}(h_l(t)-h_k(t)) \rightarrow 0{\rm{\;for\;a.e.\;}}t \in (0,T)}, \end{equation} (6.23)

    with the result that R_k \rightarrow 0. Let

    \begin{equation} \begin{split} & \left[u(h_k(t),t)\right] = u(h_k(t)^+,t)-u(h_k(t)^-,t), \\ & \left[f(u(h_k(t),t))\right] = f(u(h_k(t)^+,t))-f(u(h_k(t)^-,t)). \end{split} \end{equation} (6.24)

    A straightforward calculation using (5.1), (5.2) gives

    \begin{equation} \begin{split} &\int_0^T \int_{ \mathbb{R}} \left\{u (\psi_{\delta}(x-h_k(t)) \xi(t))_t + f(u) (\psi_{\delta}(x-h_k(t)) \xi(t))_x \right\} \,dx \,dt \\ &\quad \quad \rightarrow \int_0^T\left\{h_k'(t) [u(h_k(t),t)] - [f(u(h_k(t),t))]\right\} \xi(t) \, dt, \end{split} \end{equation} (6.25)

    and

    \begin{equation} \int_{ \mathbb{R}} u_0(x) \psi_{\delta}(x-h_k(0)) \xi(0) \, dx \rightarrow 0. \end{equation} (6.26)

    The result is that (6.21) becomes

    \begin{equation} \begin{split} & -m_k \int_0^T h_k'(t) \xi'(t) \, dt \\ & \qquad \qquad \qquad \qquad = \int_0^T\left\{h_k'(t) [u(h_k(t),t)] - [f(u(h_k(t),t))]\right\} \xi(t) \, dt. \end{split} \end{equation} (6.27)

    After integrating the left side by parts the result is

    \begin{equation} \int_0^T\left\{m_k h_k''(t) - [u(h_k(t),t)]h_k'(t) - [f(u(h_k(t),t))]\right\} \xi(t) \, dt = 0, \end{equation} (6.28)

    implying that (1.4) holds for a.e. t \in [0,T] .

    The observation that for all \Delta >0 , h^{ \Delta}_k(0) = h_{k,0} and c^{ \Delta}_k(0) = v_{k,0} proves the assertion that (h_k(0),h_k'(0)) = (h_{k,0},v_{k,0}) .

    Proof of the main theorem.

    Proof. Lemma 3.5 provides the convergence portion of Theorem 1.3. That the limit (u,\vec{h}) is an entropy solution results from Lemmas 5.4, 5.6, and 6.1.

    Remark 8. For the single-particle case, Theorem 8 of [6] states that Definition 1.2 is sufficient for uniqueness. Thus if K = 1 , the Lax-Friedrichs approximations (u^{ \Delta}, h_1^{ \Delta}) converge to the unique entropy solution, and convergence is along the entire computed sequence, not just a subsequence.

    It is possible to somewhat reduce the excessively diffusive nature of Lax-Friedrichs differencing without adding too much complexity by using the MUSCL approach. Our incorporation of MUSCL processing is standard [12]. Let \mathcal{M}(\cdot,\cdot) denote the minmod function:

    \begin{equation} \mathcal{M}(a,b) = {1\over 2}\left( \operatorname*{sgn}(a)+ \operatorname*{sgn}(b) \right)\min(\left|{a}\right|,\left|{b}\right|). \end{equation} (7.1)

    We replace the numerical fluxes \bar{f}^n_{ j+1/2} , \bar{g}^n_{k, j+1/2} in (2.7) by

    \begin{equation} \begin{split} &\tilde{f}^n_{ j+1/2} = {1\over 2}\left( \left(U_{j+1}^{n,-} \right)^2/2 + \left(U_{j}^{n,+} \right)^2/2\right) - {q \over{2\mu}}\left(U_{j+1}^{n,-} -U_{j}^{n,+} \right),\\ &\tilde{g}^n_{k, j+1/2} = {1\over 2}\left( c_k^n W_{k,j+1}^{n,-} + c_k^n W_{k,j}^{n,+} \right) - {q \over{2\mu}}\left(W_{k,j+1}^{n,-} -W_{k,j}^{n,+} \right), \end{split} \end{equation} (7.2)

    where

    \begin{equation} \begin{split} &U_{j}^{n,\pm} = U_j^n \pm {1\over 2}\mathcal{M}(\Delta_+ U_j^n, \Delta_- U_j^n), \\ &W_{k,j}^{n,\pm} = W_{k,j}^n \pm {1\over 2}\mathcal{M}(\Delta_+ W_{k,j}^n, \Delta_- W_{k,j}^n). \end{split} \end{equation} (7.3)

    We do not presently have any convergence results or even stability estimates for the resulting scheme with MUSCL processing incorporated. A moderate amount of numerical experience indicates that the algorithm produces approximations that converge to the same solution as the basic algorithm of Section 2.

    Following are a few numerical examples. We refer to the scheme of Section 2 as the basic scheme, and the modified scheme of Section 7 as the MUSCL scheme. We used q = 1/2 in all examples.

    Example 8.1. This is a single-particle Riemann problem, with

    \begin{equation} (u_L,u_R) = (.15, -.15), \quad (h(0),h'(0)) = (0,.65), \quad \lambda = .5, \quad m = 2. \end{equation} (8.1)

    The exact solution is available for comparison, using the results of [11]. See Figure 1. The approximations appear to improve when the mesh size is halved, as expected. It is also apparent that the MUSCL scheme is more accurate than the basic one.

    Figure 1.  Example 8.1. Top: Fluid velocity u at t = 1 . Exact solution is solid line, with sharp corners. Bottom: Particle position error vs. time. Basic scheme (left plots) and MUSCL scheme (right plots). \Delta x = .0025 (dashed line), and \Delta x = .00125 (solid line). Both approximations used \mu = .25 .

    The sharp transition at x\approx 0.8 is a shock that is collocated with the particle. With our Lax-Friedrichs scheme there is some smearing of the shock. We must rely on a very small mesh size, even with the MUSCL version, to obtain a very sharp transition. The schemes of [1], [5], and [14] resolve this type of shock (i.e., the shock is collocated with the particle) with no smearing.

    Example 8.2. This is another single-particle Riemann problem with

    \begin{equation} (u_L,u_R) = (.25, .75),\quad (h(0),h'(0)) = (0,.65),\quad \lambda = .5,\quad m = 1. \end{equation} (8.2)

    As in the previous example the exact solution is available via [11]. This example displays a spurious kink, see Figure 2, that appears in some cases where a particle's velocity h_k'(t) lies between u(h_k^-(t),t) and u(h_k^+(t),t) . The kink is probably due to the large numerical viscosity of the Lax-Friedrichs scheme. The size of the kink diminishes, as expected, when the mesh shrinks. Also the MUSCL approximation has a smaller kink than the basic approximation.

    Figure 2.  Example 8.2. Fluid velocity u at t = 1 . Basic scheme (left plots) and MUSCL scheme (right plots). Exact solution (dashed line) and approximate solution (solid line). Top plots used \Delta x = .005 , bottom plots used \Delta x = .000625 . All approximations used \mu = .25 . A spurious kink is visible. Its magnitude diminishes with grid refinement.

    Example 8.3. This is a two-particle example with z(x,t) = \rm{constant} = \hat{z} . It is possible to explicitly solve this type of problem. With z(x,t) = \hat{z} , we have u(x,t) = \hat{z} - \lambda_1 H(x-h_1(t)) - \lambda_2 H(x-h_2(t)) . Thus the problem reduces to determining the particle paths h_1(t) and h_2(t) . This can be accomplished using the differential equations (1.4), which become

    \begin{equation} h_k'' + {{\lambda_k}\over{m_k}} h_k' = \sigma_k(t), \quad k = 1,2. \end{equation} (8.3)

    Here

    \begin{equation} \sigma_k(t) = {{\lambda_k \hat{z} - \lambda_k^2/2}\over {m_k}} + p_k(t), \end{equation} (8.4)

    where

    \begin{equation} p_1(t) = \begin{cases} 0, &\quad h_1(t) < h_2(t),\\ -{{\lambda_1 \lambda_2}\over{m_1}}, &\quad h_1(t) > h_2(t), \end{cases} \quad p_2(t) = \begin{cases} -{{\lambda_1 \lambda_2}\over{m_2}}, &\quad h_1(t) < h_2(t),\\ 0, &\quad h_1(t) > h_2(t). \end{cases} \end{equation} (8.5)

    Assume that the particle trajectories do not intersect except for a finite set of times \tau_\nu with 0<\tau_1< \ldots< \tau_M < T . Define \tau_0 = 0 , \tau_{M+1} = T , and let r_k = \lambda_k/m_k . The solution of (8.3), (8.4), (8.5) can be expressed piecewise. For t \in (\tau_\nu,\tau_{\nu+1}) the solution is

    \begin{equation} h_k(t) = h_k(\tau_\nu) +{{h_k'(\tau_\nu)}\over{r_k}}(1-\exp(-r_k(t-\tau_\nu))) -{{\sigma_k}\over{r_k^2}}(1-\exp(-r_k(t-\tau_\nu))) +{{\sigma_k}\over{r_k}}(t - \tau_\nu). \end{equation} (8.6)

    The parameters used in this example are

    \begin{equation} \begin{split} &m_1 = .025, m_2 = .02, (h_1(0),h_1'(0)) = (.2,1.2), (h_2(0),h_2'(0)) = (.3,0.9),\\ & \lambda_1 = .75, \lambda_2 = .5, \hat{z} = .5. \end{split} \end{equation} (8.7)

    See Figures 3 and 4. From Figure 3 it appears that the MUSCL scheme is more accurate than the basic scheme, as expected. We also see that the discrete L^1 error in u decreases as we decrease the mesh size. Figure 4 shows the approximate and exact particle trajectories. At the level of discretization shown, the particle trajectories produced by the basic scheme do not quite agree with the exact trajectories. This discrepancy diminishes when the mesh size is decreased (not shown), but convergence is slow. For the MUSCL scheme the resolution is better; the exact and computed trajectories are not visually distinguishable at this level of grid refinement.

    Figure 3.  Example 8.3. Solution u using basic scheme at t = .125 (upper left), and using MUSCL (upper right). True solution (dashed line) and approximate solution (solid line). Both upper plots computed with \Delta x = .00325 , \mu = .25 . The lower plots show the error in u in discrete L^1 norm as a function of time using the basic scheme (lower left) and MUSCL scheme (lower right). Uses \Delta x = .00325 and \Delta x = .001625 , \mu = .25 .

    Example 8.4. This is another two-particle example. This time the particles are initially heading toward each other, and the fluid is initially at rest. Unlike the previous example the true solution is not known. In Figure 5 we show the particle trajectories at three levels of grid refinement. It appears that the particle trajectories are converging as the mesh size is refined. The MUSCL scheme is better able to resolve the fine details of the trajectory, especially after the first crossing of trajectories.

    The initial fluid velocity is zero, u_0(x) = 0 . The other parameters of the problem are

    \begin{equation} m_1 = .04, m_2 = .02, (h_1(0),h_1'(0)) = (.1,-2), (h_2(0),h_2'(0)) = (-.1,4), \lambda_1 = \lambda_2 = 1. \end{equation} (8.8)

    The author thanks an anonymous referee for providing the now improved version of Assumption 5.1, and sharing ideas about how to weaken Assumption 5.1 for future efforts to address much more general particle interaction scenarios.



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