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Initial Value Problem of the Whitham Equations for the Camassa-Holm Equation

Tamara Grava grava@sissa.it V. U. Pierce virgilpierce@gmail.com Fei-Ran Tian tian@math.ohio-state.edu SISSA, Via Beirut 2-4, 34014 Trieste, Italy Department of Mathematics, Ohio State University, 231 W. 18th Avenue, Columbus, OH 43210
Abstract

We study the Whitham equations for the Camassa-Holm equation. The equations are neither strictly hyperbolic nor genuinely nonlinear. We are interested in the initial value problem of the Whitham equations. When the initial values are given by a step function, the Whitham solution is self-similar. When the initial values are given by a smooth function, the Whitham solution exists within a cusp in the xx-tt plane. On the boundary of the cusp, the Whitham solution matches the Burgers solution, which exists outside the cusp.

keywords:
Camassa-Holm equation , Whitham equations , Non-strictly hyperbolic , Hodograph transform
PACS:
02.30.Ik , 02.30.Jr

, , and

1 Introduction

The Camassa-Holm equation

ut+(3u+2ν)uxϵ2(uxxt+2uxuxx+uuxxx)=0,u(x,0;ϵ)=u0(x)u_{t}+(3u+2\nu)u_{x}-\epsilon^{2}(u_{xxt}+2u_{x}u_{xx}+uu_{xxx})=0\ ,\quad u(x,0;\epsilon)=u_{0}(x) (1)

describes waves in shallow water when surface tension is present [2]. Here, ν\nu is a constant parameter. The solution of the initial value problem (1) will develop singularities in a finite time if and only if some portion of the positive part of the initial “momentum” density u0(x)ϵ2u0′′(x)+νu_{0}(x)-\epsilon^{2}u_{0}^{\prime\prime}(x)+\nu lies to the left of some portion of its negative part [10]. In particular, a unique global solution is guarenteed if u0(x)ϵ2u0′′(x)+νu_{0}(x)-\epsilon^{2}u_{0}^{\prime\prime}(x)+\nu does not change its sign. These are the non-breaking initial data that we are interested in throughout this paper.

Although the zero dispersion limit of equation (1) has not been established, some of its modulation equations (i.e., Whitham equations) have been derived. The zero phase Whitham equation is

ut+(3u+2ν)ux=0,u(x,0)=u0(x),u_{t}+(3u+2\nu)u_{x}=0\ ,\quad u(x,0)=u_{0}(x)\ , (2)

which can be obtained from (1) by formally setting ϵ=0\epsilon=0.

The single phase Whitham equations have been found in [1] and they can be written in the Riemann invariant form

uix+λi(u1,u2,u3)uix=0forν<u3<u2<u1,u_{ix}+\lambda_{i}(u_{1},u_{2},u_{3})u_{ix}=0\quad\mbox{for}-\nu<u_{3}<u_{2}<u_{1}\ , (3)

where

λi(u1,u2,u3)=u1+u2+u3+2νIuiI,\lambda_{i}(u_{1},u_{2},u_{3})=u_{1}+u_{2}+u_{3}+2\nu-{I\over\partial_{u_{i}}I}\ , (4)

and

I(u1,u2,u3)=u3u2η+ν(η+ν)(u1η)(u2η)(ηu3)𝑑η.I(u_{1},u_{2},u_{3})=\int_{u_{3}}^{u_{2}}{\eta+\nu\over\sqrt{(\eta+\nu)(u_{1}-\eta)(u_{2}-\eta)(\eta-u_{3})}}\ d\eta\ .

The constraint ν<u3<u2<u1-\nu<u_{3}<u_{2}<u_{1} is consistent with the non-breaking initial data mentioned in the first paragraph of this section. The integral II can be rewritten as a contour integral. Hence, it satisfies the Euler-Poisson-Darboux equations

2(uiuj)2Iuiuj=IuiIuj,i,j=1,2,32(u_{i}-u_{j}){\partial^{2}I\over\partial u_{i}\partial u_{j}}={\partial I\over\partial u_{i}}-{\partial I\over\partial u_{j}}\ ,\quad i,j=1,2,3 (5)

since the integrand does so for each ηui\eta\neq u_{i}. The Hamiltonian structure of the single phase Whitham equations for the Camassa-Holm equation was also obtained in [1] in terms of Abelian integrals. The higher phase Whitham equations can also be derived using this structure.

In this paper we will study the evolution of the Whitham solution from the zero phase to the single phase.

This problem is similar to that of the zero dispersion limit of the KdV equation [7, 8, 17]

ut+6uux+ϵ2uxxx=0,u(x,0;ϵ)=u0(x).u_{t}+6uu_{x}+\epsilon^{2}u_{xxx}=0\ ,\quad u(x,0;\epsilon)=u_{0}(x)\ . (6)

It is known that the zero phase Whitham equation for the KdV equation is

ut+6uux=0,u_{t}+6uu_{x}=0\ , (7)

which is equivalent to (2) for the Camassa-Holm equation. The single phase Whitham equations for the KdV equation are [3, 4, 18]

uix+μi(u1,u2,u3)uix=0,foru3<u2<u1,u_{ix}+\mu_{i}(u_{1},u_{2},u_{3})u_{ix}=0\ ,\quad\mbox{for}\quad u_{3}<u_{2}<u_{1}\ , (8)

where

μi(u1,u2,u3)=2[u1+u2+u3I~uiI~],\mu_{i}(u_{1},u_{2},u_{3})=2[u_{1}+u_{2}+u_{3}-{\tilde{I}\over\partial_{u_{i}}\tilde{I}}]\ ,

and

I~(u1,u2,u3)=u3u21(u1η)(u2η)(ηu3)𝑑η.\tilde{I}(u_{1},u_{2},u_{3})=\int_{u_{3}}^{u_{2}}{1\over\sqrt{(u_{1}-\eta)(u_{2}-\eta)(\eta-u_{3})}}\ d\eta\ .

These equations are also similar to (3) and (4) for the Camassa-Holm equation.

In the KdV case, the evolution from the zero phase to the single phase has been studied in [14]. There, the Euler-Poisson-Darboux equations (5) have played an important role. The same equations have also played a crucial role in the study of the transition from the single phase to the double phase in [5].

Although both the Camassa-Holm equation (1) and the KdV equation (6) are dispersive approximations to the Burgers equation (2) or (7), there are significant differences in the limiting dynamics. The biggest difference is that the Whitham equations (3) for the former equation are non-strictly hyperbolic (cf. (36)) while the Whitham equations (8) for the latter equation are strictly hyperbolic [9]. Non-Strictly hyperbolic Whitham equations have also been found in the higher order KdV flows [11, 12, 13] and the higher order defocusing NLS flows [6]. Self-similar solutions of these Whitham equations have been constructed. They are remarkably different from the self-similar solutions of the KdV-Whitham equations [11, 12] or the NLS-Whitham equations [6], both of which are strictly hyperbolic.

In this paper, we will modify the method of paper [14] so that it can be used to solve the non-strictly hyperbolic Whitham equations (3) when the initial function is a smooth function. We will then study the evolution from the zero phase to the single phase for smooth initial data. When the initial function is a step-like function, we will use the method of paper [6, 11, 12] to study the same evolution.

The organization of the paper is as follows. In Section 2, we will introduce an initial value problem which describes the evolution of phases. We will also discuss how to use the hodograph transform to solve non-strictly hyperbolic Whitham equations. In Section 3, we will study the properties of the eigenspeeds of the single phase Whitham equations. We will study the initial value problem when the initial function u0(x)u_{0}(x) is a step-like function in Section 4 and when u0(x)u_{0}(x) is a smooth decreasing function in Section 5.

2 An Initial Value Problem

We describe the initial value problem for the Burgers equation (2) and Whitham equations (3) as follows (see Figure 1.). Consider a horizontal motion of the initial curve u=u0(x)u=u_{0}(x). At the beginning, the curve evolves according to the Burgers equation (2). The Burgers solution breaks down in a finite time. Immediately after the breaking, the curve develops three branches. Denote these three branches by u1u_{1}, u2u_{2}, and u3u_{3}. Their motion is governed by the Whitham equations (3). As time goes on, the Whitham solution may develop singularities and more branches are created. However, our focus is on the evolution of the solution of the Whitham equations from the one branch regime to the three branch regime.

Refer to caption
Figure 1: Profile of the Burgers and Whitham solutions. The Burgers solution uu of (2) lives in the single value regions while the Whitham solution u1u_{1}, u2u_{2} and u3u_{3} of (3) reside in the multiple value region.

The Burgers solution uu of (2) and the Whitham solution u1u_{1}, u2u_{2}, u3u_{3} of (3) must match on the trailing edge x=x(t)x=x_{-}(t) and leading edge x=x+(t)x=x_{+}(t). We see from Figure 1 that

{u1=uu2=u3\displaystyle\left\{\begin{array}[]{c}u_{1}=u\\ u_{2}=u_{3}\end{array}\right. (11)

must be imposed on the trailing edge, and that

{u1=u2u3=u\displaystyle\left\{\begin{array}[]{c}u_{1}=u_{2}\\ u_{3}=u\end{array}\right. (14)

must be satisfied on the leading edge.

In this paper, we consider the initial function u0(x)u_{0}(x) that is monotone. Since the Burgers solution will not develop any shock if u0(x)u_{0}(x) is an increasing function, we will focus on decreasing initial functions. Denoting the inverse function of u0(x)u_{0}(x) by f(u)f(u), the Burger equation (2) can be solved using the method of characteristics; its solution is given implicitly by a hodograph transform,

x=(3u+2ν)t+f(u).x=(3u+2\nu)t+f(u)\ . (15)

The solution method (15) has been generalized to solve the first order quasilinear hyperbolic equations which can be written in Riemann invariant form and which are strictly hyperbolic

uit+si(u1,,un)uix=0,i=1,2,,n.{\partial u_{i}\over\partial t}+s_{i}(u_{1},\cdots,u_{n}){\partial u_{i}\over\partial x}=0\ ,\quad i=1,2,\cdots,n. (16)

The strict hyperbolicity means that the wave propagation speeds sis_{i}’s do not coincide.

We include Tsarev’s theorem for completeness [14, 16].

Theorem 1

If wi(u1,u2,,un)w_{i}(u_{1},u_{2},\cdots,u_{n})’s solve the linear equations

wiuj=Aij(wiwj){\partial w_{i}\over\partial u_{j}}=A_{ij}(w_{i}-w_{j}) (17)

with

Aij=sjujsisjA_{ij}={{\partial s_{j}\over\partial u_{j}}\over s_{i}-s_{j}} (18)

for i,j=1,2,,ni,j=1,2,\cdots,n and iji\neq j, then the solution (u1(x,t),,un(x,t))(u_{1}(x,t),\cdots,u_{n}(x,t)) of the hodograph transform,

x=si(u1,u2,,un)t+wi(u1,u2,,un)x=s_{i}(u_{1},u_{2},\cdots,u_{n})t+w_{i}(u_{1},u_{2},\cdots,u_{n}) (19)

satisfies equations (16). Conversely, any solution (u1(x,t),,un(x,t))(u_{1}(x,t),\cdots,u_{n}(x,t)) of equations (16) can be obtained in this way in the neighborhood of (x0,t0)(x_{0},t_{0}) at which uixu_{ix} are not all vanishing.

The strict hyperbolicity, i.e., sisjs_{i}\neq s_{j} for iji\neq j, of (16) is assumed to ensure that AijA_{ij}’s of (18) are not singular.

The result is classical when n=2n=2.

The validity of this theorem hinges on two factors. First, the linear equations (17) must have solutions. Secondly, the hodograph transform (19) must not be degenerate, i.e., it can be solved for uiu_{i}’s as functions of xx and tt. One interesting observation is that the Jacobian matrix of (19) is always diagonal on the solution (u1(x,t),,un(x,t))(u_{1}(x,t),\cdots,u_{n}(x,t)).

Corollary 2

At the solution (u1(x,t),,un(x,t))(u_{1}(x,t),\cdots,u_{n}(x,t)) of x=si(u1,u2,,un)t+wi(u1,u2,,un)x=s_{i}(u_{1},u_{2},\cdot,u_{n})t+w_{i}(u_{1},u_{2},\cdots,u_{n}), i=1,2,,ni=1,2,\cdots,n, the partial derivatives

(sit+wi)uj=0\frac{\partial(s_{i}t+w_{i})}{\partial u_{j}}=0

for iji\neq j.

Proof.

(sit+wi)uj\displaystyle\frac{\partial(s_{i}t+w_{i})}{\partial u_{j}} =\displaystyle= siujt+wiuj\displaystyle\frac{\partial s_{i}}{\partial u_{j}}t+\frac{\partial w_{i}}{\partial u_{j}}
=\displaystyle= Aij[(sit+wi)(sjt+wj)]\displaystyle A_{ij}[(s_{i}t+w_{i})-(s_{j}t+w_{j})]
=\displaystyle= 0.\displaystyle 0\ .

Another aspect of Theorem 1 is that it is a local result. Solutions produced by the hodograph transform are, in general, local in nature. However, global solutions can still be obtained if the conditions of the theorem are satisfied globally [5, 14].

The Whitham equations (3) will be shown to be non-strictly hyperbolic, i.e., λi\lambda_{i}’s coincide at some points (u1,u2,u3)(u_{1},u_{2},u_{3}) where 0<u3+ν<u2+ν<u1+ν0<u_{3}+\nu<u_{2}+\nu<u_{1}+\nu. However, Theorem 1 can still be applied to equations (3) since the functions AijA_{ij}’s of (18) are still non-singular for the Whitham equations (3), even at the points of non-strict hyperbolicity.

Lemma 3
Bij:=λiujλiλj=12(λiγ)2(uiuj)(λjγ)(uiuj),ij,B_{ij}:={{\partial\lambda_{i}\over\partial u_{j}}\over\lambda_{i}-\lambda_{j}}={1\over 2}{(\lambda_{i}-\gamma)-2(u_{i}-u_{j})\over(\lambda_{j}-\gamma)(u_{i}-u_{j})}\ ,\quad i\neq j\,,

where γ=u1+u2+u3+2ν\gamma=u_{1}+u_{2}+u_{3}+2\nu.

Proof.

By (4), we calculate

λiλj\displaystyle\lambda_{i}-\lambda_{j} =\displaystyle= IuiIujI(uiI)(ujI)=2I(uiuj)uiuj2I(uiI)(ujI),\displaystyle I{\partial_{u_{i}}I-\partial_{u_{j}}I\over(\partial_{u_{i}}I)(\partial_{u_{j}}I)}=2I{(u_{i}-u_{j})\partial_{u_{i}u_{j}}^{2}I\over(\partial_{u_{i}}I)(\partial_{u_{j}}I)}\ ,
λiuj\displaystyle{\partial\lambda_{i}\over\partial u_{j}} =\displaystyle= 2(uiuj)uiuj2IuiI+Iuiuj2I(uiI)2,\displaystyle{2(u_{i}-u_{j})\partial_{u_{i}u_{j}}^{2}I\over\partial_{u_{i}}I}+{I\partial_{u_{i}u_{j}}^{2}I\over(\partial_{u_{i}}I)^{2}}\ ,

where we have used (5). Hence, we get

Bij\displaystyle B_{ij} =\displaystyle= 2(uiuj)+IuiI2IujI(uiuj)\displaystyle{2(u_{i}-u_{j})+{I\over\partial_{u_{i}}I}\over{2I\over\partial_{u_{j}}I}(u_{i}-u_{j})}
=\displaystyle= 12(λiγ)2(uiuj)(λjγ)(uiuj),\displaystyle{1\over 2}{(\lambda_{i}-\gamma)-2(u_{i}-u_{j})\over(\lambda_{j}-\gamma)(u_{i}-u_{j})}\ ,

where we have used (4) to express I/uiII/\partial_{u_{i}}I. ∎

3 The Single Phase Whitham Equations

In this section, we will summarize some of the properties of the speeds λi\lambda_{i}’s of (4) for later use.

Function II of (4) is a complete elliptic integral; indeed,

I(u1,u2,u3)=2(u3+ν)Π(ρ,s)(u1u3)(u2+ν),I(u_{1},u_{2},u_{3})={2(u_{3}+\nu)\Pi(\rho,s)\over\sqrt{(u_{1}-u_{3})(u_{2}+\nu)}}\ , (20)

where Π(ρ,s)\Pi(\rho,s) is the complete integral of third kind, and

ρ=u2u3u2+ν,s=(u2u3)(u1+ν)(u1u3)(u2+ν).\rho={u_{2}-u_{3}\over u_{2}+\nu}\ ,\quad s=\frac{(u_{2}-u_{3})(u_{1}+\nu)}{(u_{1}-u_{3})(u_{2}+\nu)}\ . (21)

Properties of complete elliptic integrals of the first, second and third kind are listed in Appendix A.

Using the well known derivative formulae (99) and (100), one is able to rewrite λi\lambda_{i} of (4) as [1]

λ1(u1,u2,u3)\displaystyle\lambda_{1}(u_{1},u_{2},u_{3}) =\displaystyle= u1+u2+u3+2ν+2(u1u2)(u3+ν)Π(ρ,s)(u2+ν)E(s),\displaystyle u_{1}+u_{2}+u_{3}+2\nu+2(u_{1}-u_{2})\frac{(u_{3}+\nu)\Pi(\rho,s)}{(u_{2}+\nu)E(s)}\ ,
λ2(u1,u2,u3)\displaystyle\lambda_{2}(u_{1},u_{2},u_{3}) =\displaystyle= u1+u2+u3+2ν+2(u3u2)(1s)Π(ρ,s)E(s)(1s)K(s),\displaystyle u_{1}+u_{2}+u_{3}+2\nu+2(u_{3}-u_{2})\frac{(1-s)\Pi(\rho,s)}{E(s)-(1-s)K(s)}\ , (22)
λ3(u1,u2,u3)\displaystyle\lambda_{3}(u_{1},u_{2},u_{3}) =\displaystyle= u1+u2+u3+2ν+2(u2u3)(u3+ν)Π(ρ,s)(u2+ν)[E(s)K(s)].\displaystyle u_{1}+u_{2}+u_{3}+2\nu+2(u_{2}-u_{3})\frac{(u_{3}+\nu)\Pi(\rho,s)}{(u_{2}+\nu)[E(s)-K(s)]}\ .

Here K(s)K(s) and E(s)E(s) are complete elliptic integrals of the first and second kind.

Using inequalities (105), we obtain

λ1(u1+u2+u3+2ν)\displaystyle\lambda_{1}-(u_{1}+u_{2}+u_{3}+2\nu) >\displaystyle> 0,\displaystyle 0\ , (23)
λ2(u1+u2+u3+2ν)\displaystyle\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu) <\displaystyle< 0,\displaystyle 0\ , (24)
λ3(u1+u2+u3+2ν)\displaystyle\lambda_{3}-(u_{1}+u_{2}+u_{3}+2\nu) <\displaystyle< 0,\displaystyle 0\ , (25)

for u1>u2>u3>νu_{1}>u_{2}>u_{3}>-\nu. In view of (101-104) and (106-107), we find that λ1\lambda_{1}, λ2\lambda_{2} and λ3\lambda_{3} have behavior

(1) At u2u_{2} = u3u_{3},

λ1(u1,u2,u3)=3u1+2ν,λ2(u1,u2,u3)=λ3(u1,u2,u3)=u1+2u3+2ν4(u3+ν)(u1u3)u1+ν.\begin{array}[]{ll}\lambda_{1}(u_{1},u_{2},u_{3})=3u_{1}+2\nu\ ,\\ \lambda_{2}(u_{1},u_{2},u_{3})=\lambda_{3}(u_{1},u_{2},u_{3})=u_{1}+2u_{3}+2\nu-{4(u_{3}+\nu)(u_{1}-u_{3})\over u_{1}+\nu}\ .\end{array} (26)

(2) At u1u_{1} = u2u_{2},

λ1(u1,u2,u3)=λ2(u1,u2,u3)=2u1+u3+2ν,λ3(u1,u2,u3)=3u3+2ν.\begin{array}[]{ll}\lambda_{1}(u_{1},u_{2},u_{3})=\lambda_{2}(u_{1},u_{2},u_{3})=2u_{1}+u_{3}+2\nu\ ,\\ \lambda_{3}(u_{1},u_{2},u_{3})=3u_{3}+2\nu\ .\end{array} (27)
Lemma 4
λ3u3<32λ2λ3u2u3<λ2u2\frac{\partial\lambda_{3}}{\partial u_{3}}<\frac{3}{2}\frac{\lambda_{2}-\lambda_{3}}{u_{2}-u_{3}}<\frac{\partial\lambda_{2}}{\partial u_{2}}

for 0<u3+ν<u2+ν<u1+ν0<u_{3}+\nu<u_{2}+\nu<u_{1}+\nu.

Proof.

Comparing formulae (4) and (22), we use (20) to obtain

Iu2=(u1u3)(u2+ν)(u2u3)(u1u2)[E(1s)K].{\partial I\over\partial u_{2}}={\sqrt{(u_{1}-u_{3})(u_{2}+\nu)}\over(u_{2}-u_{3})(u_{1}-u_{2})}\ [E-(1-s)K]\ . (28)

Differentiating (4) for λ2\lambda_{2} and using (28) yields

λ2u2\displaystyle{\partial\lambda_{2}\over\partial u_{2}} =\displaystyle= Iu2u22I(u2I)2\displaystyle{I\partial^{2}_{u_{2}u_{2}}I\over(\partial_{u_{2}}I)^{2}} (29)
=\displaystyle= (u3+ν)Π(u2+ν)[E(1s)K]2×\displaystyle{(u_{3}+\nu)\Pi\over(u_{2}+\nu)[E-(1-s)K]^{2}}\times
×{[s+u2u3u1u32u1u2u1u3][E(1s)K]+s(1s)K}.\displaystyle\times\left\{[s+{u_{2}-u_{3}\over u_{1}-u_{3}}-2{u_{1}-u_{2}\over u_{1}-u_{3}}][E-(1-s)K]+s(1-s)K\right\}\ .

Using formulae (22) for λ2\lambda_{2} and λ3\lambda_{3}, we obtain

λ2(u1,u2,u3)λ3(u1,u2,u3)=2(u2u3)(u3+ν)ΠM(u1,u2,u3)(u2+ν)(KE)[E(1s)K],\lambda_{2}(u_{1},u_{2},u_{3})-\lambda_{3}(u_{1},u_{2},u_{3})={2(u_{2}-u_{3})(u_{3}+\nu)\Pi M(u_{1},u_{2},u_{3})\over(u_{2}+\nu)(K-E)[E-(1-s)K]}\ , (30)

where

M(u1,u2,u3)=[1+u1u2u1u3]E[u1u2u1u3+(1s)]K.M(u_{1},u_{2},u_{3})=[1+{u_{1}-u_{2}\over u_{1}-u_{3}}]E-[{u_{1}-u_{2}\over u_{1}-u_{3}}+(1-s)]K\ . (31)

We then obtain from (29) and (30) that

λ2u232λ2λ3u2u3\displaystyle{\partial\lambda_{2}\over\partial u_{2}}-{3\over 2}\ {\lambda_{2}-\lambda_{3}\over u_{2}-u_{3}} =(u3+ν)(43s)ΠE2(u2+ν)[KE][E(1s)K]2{(1s)(KE)2\displaystyle=-{(u_{3}+\nu)(4-3s)\Pi E^{2}\over(u_{2}+\nu)[K-E][E-(1-s)K]^{2}}\left\{(1-s)({K\over E})^{2}\right.
2(KE)+4+s43s}>0,\displaystyle\phantom{=}\left.\quad-2({K\over E})+{4+s\over 4-3s}\right\}>0\ ,

where the inequality follows from the negativity of the function in the bracket (c.f. (4.18) of [14]). This proves part of the lemma. The other part can be shown in the same way.

We conclude this section with a few calculations. We use (97) and (98) to calculate the derivative of (31)

M(u1,u2,u3)u2\displaystyle{\partial M(u_{1},u_{2},u_{3})\over\partial u_{2}} =\displaystyle= 12(u1u3){[2+(u1+ν)(u3+ν)(u2+ν)2]K\displaystyle{1\over 2(u_{1}-u_{3})}\ \{[2+{(u_{1}+\nu)(u_{3}+\nu)\over(u_{2}+\nu)^{2}}]K (32)
[2+u1+νu2+ν]E},\displaystyle\phantom{{1\over 2(u_{1}-u_{3})}\ \{}-[2+{u_{1}+\nu\over u_{2}+\nu}]E\}\ ,
2M(u1,u2,u3)u22\displaystyle{\partial^{2}M(u_{1},u_{2},u_{3})\over\partial u_{2}^{2}} =\displaystyle= (u1+ν)[4(u1+ν)2(u2+ν)+(u3+ν)]E4(u1u3)(u1u2)(u2+ν)2.\displaystyle{(u_{1}+\nu)[4(u_{1}+\nu)-2(u_{2}+\nu)+(u_{3}+\nu)]E\over 4(u_{1}-u_{3})(u_{1}-u_{2})(u_{2}+\nu)^{2}}\ . (33)

Finally, we use the expansions (101-102) for KK and EE to obtain

M(u1,u2,u3)\displaystyle M(u_{1},u_{2},u_{3}) =\displaystyle= π2{(u2u3)s2(u1u3)+116(13(u1u2)u1u3)s2\displaystyle{\pi\over 2}\left\{{(u_{2}-u_{3})s\over 2(u_{1}-u_{3})}+{1\over 16}\ (1-{3(u_{1}-u_{2})\over u_{1}-u_{3}})s^{2}\right. (34)
+3128(15(u1u2)u1u3)s3+O(s4)}\displaystyle\phantom{{\pi\over 2}}\left.\quad+{3\over 128}(1-{5(u_{1}-u_{2})\over u_{1}-u_{3}})s^{3}+O(s^{4})\right\}
=\displaystyle= π2{[u2+ν2(u1+ν)+116(13(u1u2)u1u3)]s2\displaystyle{\pi\over 2}\left\{[{u_{2}+\nu\over 2(u_{1}+\nu)}+{1\over 16}\ (1-{3(u_{1}-u_{2})\over u_{1}-u_{3}})]s^{2}\right.
+3128(15(u1u2)u1u3)s3+O(s4)},\displaystyle\phantom{{\pi\over 2}}\left.\quad+{3\over 128}(1-{5(u_{1}-u_{2})\over u_{1}-u_{3}})s^{3}+O(s^{4})\right\}\,,

where we have used formula (21) for ss in the last equality.

4 Step-like Initial Data

In this section, we will consider the step-like initial data

u0(x)={ax<0bx>0,abu_{0}(x)=\left\{\begin{matrix}a&\quad x<0\\ b&\quad x>0\end{matrix}\right.\ ,\ \quad a\neq b (35)

for equation (1). Since the solution of (2) will never develop a shock when aba\leq b, we will be interested only in the case a>ba>b. We classify the initial data (35) into two types:

  • (I) a+ν>4(b+ν)a+\nu>4(b+\nu)  ,

  • (II) a+ν4(b+ν).a+\nu\leq 4(b+\nu)\,.

We will solve the initial value problem for the Whitham equations for these two types of initial data.

4.1 Type I: a+ν>4(b+ν)a+\nu>4(b+\nu)

Refer to caption
Figure 2: Self-Similar solution of the Whitham equations for a=2a=2, b=0b=0 and ν=1/20\nu=1/20 of type I.
Theorem 5

(see Figure 2.) For the step-like initial data u0(x)u_{0}(x) of (35) with 0<b+ν<(a+ν)/40<b+\nu<(a+\nu)/4, the solution of the Whitham equations (3) is given by

u1=a,x=λ2(a,u2,u3)t,x=λ3(a,u2,u3)tu_{1}=a\ ,\quad x=\lambda_{2}(a,u_{2},u_{3})\ t\ ,\quad x=\lambda_{3}(a,u_{2},u_{3})\ t (36)

for (3aν)/4<x/tα(3a-\nu)/4<x/t\leq\alpha and by

u1=a,x=λ2(a,u2,b)t,u3=bu_{1}=a\ ,\quad x=\lambda_{2}(a,u_{2},b)\ t\ ,\quad u_{3}=b (37)

for αtx<(2a+b+2ν)t\alpha t\leq x<(2a+b+2\nu)t, where α=λ2(a,u,b)\alpha=\lambda_{2}(a,u^{*},b) and uu^{*} is the unique solution u2u_{2} of λ2(a,u2,b)=λ3(a,u2,b)\lambda_{2}(a,u_{2},b)=\lambda_{3}(a,u_{2},b) in the interval b<u2<ab<u_{2}<a. Outside the region (3aν)/4<x/t<2a+b+2ν(3a-\nu)/4<x/t<2a+b+2\nu, the solution of the Burgers equation (2) is given by

uax/t(3aν)/4u\equiv a\quad\mbox{$x/t\leq(3a-\nu)/4$} (38)

and

ubx/t2a+b+2ν.u\equiv b\quad\mbox{$x/t\geq 2a+b+2\nu$}\ . (39)

The boundaries x/t=(3aν)/4x/t=(3a-\nu)/4 and x/t=2a+b+2νx/t=2a+b+2\nu are the trailing and leading edges, respectively, of the dispersive shock. They separate the solution into the region governed by the single phase Whitham equations and the region governed by the Burgers equation.

The proof of Theorem 5 is based on a series of lemmas.

We first show that the solutions defined by formulae (36) and (37) indeed satisfy the Whitham equations (3) [16].

Lemma 6
  1. (i)

    The functions u1u_{1}, u2u_{2} and u3u_{3} determined by equations (36) give a solution of the Whitham equations (3) as long as u2u_{2} and u3u_{3} can be solved from (36) as functions of xx and tt.

  2. (ii)

    The functions u1u_{1}, u2u_{2} and u3u_{3} determined by equations (37) give a solution of the Whitham equations (3) as long as u2u_{2} can be solved from (37) as a function of xx and tt.

Proof.

(i) u1u_{1} obviously satisfies the first equation of (3). To verify the second and third equations, we observe that

λ2u3=λ3u2=0\frac{\partial\lambda_{2}}{\partial u_{3}}=\frac{\partial\lambda_{3}}{\partial u_{2}}=0 (40)

on the solution of (36). This follows from Lemma 3.

We then calculate the partial derivatives of the second equation of (36) with respect to xx and tt.

1=λ2u2t(u2)x,0=λ2u2t(u2)t+λ2,1=\frac{\partial\lambda_{2}}{\partial u_{2}}\ t(u_{2})_{x}\ ,\quad 0=\frac{\partial\lambda_{2}}{\partial u_{2}}\ t(u_{2})_{t}+\lambda_{2}\ ,

which give the second equation of (3).

The third equation of (3) can be verified in the same way.

(ii) The second part of Lemma 6 can easily be proved in a similar manner.

We now determine the trailing edge. Eliminating xx and tt from the last two equations of (36) yields

λ2(a,u2,u3)λ3(a,u2,u3)=0.\lambda_{2}(a,u_{2},u_{3})-\lambda_{3}(a,u_{2},u_{3})=0\ . (41)

In view of formula (30), we replace (41) by

M(a,u2,u3)s2=0.{M(a,u_{2},u_{3})\over s^{2}}=0\ . (42)

Therefore, at the trailing edge where u2=u3u_{2}=u_{3}, i.e., s=0s=0, equation (42), in view of the expansion (34), becomes

u3+ν2(a+ν)+116[13(au3)au3]=0,{u_{3}+\nu\over 2(a+\nu)}+{1\over 16}\ [1-{3(a-u_{3})\over a-u_{3}}]=0\ ,

which gives u2=u3=(a3ν)/4u_{2}=u_{3}=(a-3\nu)/4.

Lemma 7

Equation (42) has a unique solution satisfying u2=u3u_{2}=u_{3}. The solution is u2=u3=(a3ν)/4u_{2}=u_{3}=(a-3\nu)/4. The rest of equations (36) at the trailing edge are u1=au_{1}=a and x/t=λ2(a,(a3ν)/4,(a3ν)/4)=(3aν)/4x/t=\lambda_{2}(a,(a-3\nu)/4,(a-3\nu)/4)=(3a-\nu)/4.

Having located the trailing edge, we now solve equations (36) in the neighborhood of the trailing edge. We first consider equation (42). We use (34) to differentiate M/s2M/s^{2} at the trailing edge u1=au_{1}=a, u2=u3=(a3ν)/4u_{2}=u_{3}=(a-3\nu)/4, to find

u2[Ms2]=u3[Ms2]=π8(a+ν),{\partial\over\partial u_{2}}[{M\over s^{2}}]={\partial\over\partial u_{3}}[{M\over s^{2}}]={\pi\over 8(a+\nu)}\ ,

which shows that equation (42) or equivalently (41) can be inverted to give u3u_{3} as a decreasing function of u2u_{2}

u3=A(u2)u_{3}=A(u_{2}) (43)

in a neighborhood of u2=u3=(a3ν)/4u_{2}=u_{3}=(a-3\nu)/4.

We now extend the solution (43) of equation (41) in the region a>u2>(a3ν)/4>u3>ba>u_{2}>(a-3\nu)/4>u_{3}>b as far as possible. We deduce from Lemma 4 that

λ2u2>0,λ3u3<0{\partial\lambda_{2}\over\partial u_{2}}>0\ ,\quad{\partial\lambda_{3}\over\partial u_{3}}<0 (44)

on the solution of (41). Because of (40) and (44), solution (43) of equation (41) can be extended as long as a>u2>(a3ν)/4>u3>0a>u_{2}>(a-3\nu)/4>u_{3}>0.

There are two possibilities: (i) u2u_{2} touches aa before or simultaneously as u3u_{3} reaches bb and (ii) u3u_{3} touches bb before u2u_{2} reaches aa.

It follows from (27) that

λ2(a,a,u3)>λ3(a,a,u3)for bu3<a.\lambda_{2}(a,a,u_{3})>\lambda_{3}(a,a,u_{3})\quad\mbox{for $b\leq u_{3}<a$}\ .

This shows that (i) is impossible. Hence, u3u_{3} will touch bb before u2u_{2} reaches aa. When this happens, equation (41) becomes

λ2(a,u2,b)λ3(a,u2,b)=0.\lambda_{2}(a,u_{2},b)-\lambda_{3}(a,u_{2},b)=0\ . (45)
Lemma 8

Equation (45) has a simple zero in the region b<u2<ab<u_{2}<a, counting multiplicities. Denoting the zero by uu^{*}, then λ2(a,u2,b)λ3(a,u2,b)\lambda_{2}(a,u_{2},b)-\lambda_{3}(a,u_{2},b) is positive for u2>uu_{2}>u^{*} and negative for u2<uu_{2}<u^{*}.

Proof.   We use (30) and (33) to prove the lemma. In equation (30), KEK-E and E(1s)KE-(1-s)K are all positive for 0<s<10<s<1 in view of (105). We claim that

M(a,u2,b)=0for u2=b,M(a,u2,b)<0for u2 near b,M(a,u_{2},b)=0\quad\mbox{for $u_{2}=b$}\ ,\quad M(a,u_{2},b)<0\quad\mbox{for $u_{2}$ near $b$}\ ,

and

M(a,u2,b)>0for u2=a.\quad M(a,u_{2},b)>0\quad\mbox{for $u_{2}=a$}\ .

The equality and the first inequality follow from expansion (34) and a+ν>4(b+ν)a+\nu>4(b+\nu). The second inequality is obtained by applying (103) and (104) to (31).

We conclude from the two inequalities that M(a,u2,b)M(a,u_{2},b) has a zero in b<u2<ab<u_{2}<a. This zero is unique because M(a,u2,b)M(a,u_{2},b), in view of (33), is a convex function of u2u_{2}. This zero is exactly uu^{*} and the rest of the theorem is proven easily. ∎

Having solved equation (41) for u3u_{3} as a decreasing function of u2u_{2} for (a3ν)/4u2u(a-3\nu)/4\leq u_{2}\leq u^{*}, we turn to equations (36). Because of (40) and (44), the second equation of (36) gives u2u_{2} as an increasing function of x/tx/t, for (3aν)/4x/tα(3a-\nu)/4\leq x/t\leq\alpha, where

α=λ2(a,u,b).\alpha=\lambda_{2}(a,u^{*},b).

Consequently, u3u_{3} is a decreasing function of x/tx/t in the same interval.

Lemma 9

The last two equations of (36) can be inverted to give u2u_{2} and u3u_{3} as increasing and decreasing functions, respectively, of the self-similarity variable x/tx/t in the interval (3aν)x/tα(3a-\nu)\leq x/t\leq\alpha, where α=λ2(a,u,b)\alpha=\lambda_{2}(a,u^{*},b) and uu^{*} is given in Lemma 8.

We now turn to equations (37). We want to solve the second equation when x/t>αx/t>\alpha or equivalently when u2>uu_{2}>u^{*}. According to Lemma 8, λ2(a,u2,b)λ3(a,u2,b)>0\lambda_{2}(a,u_{2},b)-\lambda_{3}(a,u_{2},b)>0 for u<u2<au^{*}<u_{2}<a, which, by Lemma 4, shows that

λ2(a,u2,b)u2>0.{\partial\lambda_{2}(a,u_{2},b)\over\partial u_{2}}>0\ .

Hence, the second equation of (37) can be solved for u2u_{2} as an increasing function of x/tx/t as long as u<u2<au^{*}<u_{2}<a. When u2u_{2} reaches aa, we have

x/t=λ2(a,a,b)=2a+b+2ν,x/t=\lambda_{2}(a,a,b)=2a+b+2\nu\ ,

where we have used (27) in the last equality. We have therefore proved the following result.

Lemma 10

The second equation of (37) can be inverted to give u2u_{2} as an increasing function of x/tx/t in the interval αx/t2a+b+2ν\alpha\leq x/t\leq 2a+b+2\nu.

We are ready to conclude the proof of Theorem 5.

The Burgers solutions (38) and (39) are trivial.

According to Lemma 9, the last two equations of (36) determine u2u_{2} and u3u_{3} as functions of x/tx/t in the region (3av)/4x/tα(3a-v)/4\leq x/t\leq\alpha. By the first part of Lemma 6, the resulting u1u_{1}, u2u_{2} and u3u_{3} satisfy the Whitham equations (3). Furthermore, the boundary condition (11) is satisfied at the trailing edge x/t=(3av)/4x/t=(3a-v)/4.

Similarly, by Lemma 10, the second equation of (37) determines u2u_{2} as a function of x/tx/t in the region αx/t2a+b+2ν\alpha\leq x/t\leq 2a+b+2\nu. It then follows from the second part of Lemma 6 that u1u_{1}, u2u_{2} and u3u_{3} of (37) satisfy the Whitham equations (3). They also satisfy the boundary condition (14) at the leading edge x=(2a+b+2ν)tx=(2a+b+2\nu)t.

We have therefore completed the proof of Theorem 5.

A graph of the Whitham solution for the initial data (35) of type I is given in Figure 2. It is obtained by plotting the exact solutions of (36) and (37).

4.2 Type II: a+ν4(b+ν)a+\nu\leq 4(b+\nu)

Refer to caption
Figure 3: Self-Similar solution of the Whitham equations for a=2a=2, b=0.8b=0.8 and ν=1/20\nu=1/20 of type II.
Theorem 11

(see Figure 3.) For the step-like initial data (35) with 0<(a+ν)/4b+ν<a+ν0<(a+\nu)/4\leq b+\nu<a+\nu, the solution of the Whitham equations (3) is given by

u1=a,x=λ2(a,u2,b)t,u3=bu_{1}=a\ ,\quad x=\lambda_{2}(a,u_{2},b)\ t\ ,\quad u_{3}=b (46)

for λ2(a,b,b)<x/t<λ2(a,a,b)\lambda_{2}(a,b,b)<x/t<\lambda_{2}(a,a,b), where λ2(a,b,b)=a+2b+2ν4(ab)(b+ν)/(a+ν)\lambda_{2}(a,b,b)=a+2b+2\nu-4(a-b)(b+\nu)/(a+\nu) and λ2(a,a,b)=2a+b+2ν\lambda_{2}(a,a,b)=2a+b+2\nu. Outside this interval, the solution of (2) is given by

uax/tλ2(a,b,b)u\equiv a\quad\mbox{$x/t\leq\lambda_{2}(a,b,b)$}

and

ubx/tλ2(a,a,b).u\equiv b\quad\mbox{$x/t\geq\lambda_{2}(a,a,b)$}\ .

Proof.

We will give a brief proof, since the arguments are, more or less, similar to those in the proof of Theorem 5.

It suffices to show that λ2(a,u2,b)\lambda_{2}(a,u_{2},b) is an increasing function of u2u_{2} for b<u2<ab<u_{2}<a. Using the inequality (105) to estimate the right hand side of (32), we obtain

dM(a,u2,b)du2\displaystyle{dM(a,u_{2},b)\over du_{2}} >(a+ν)(u2b)E(s)2(2s)(ab)2(u2+ν)2{2(u2+ν)+2(b+ν)\displaystyle>{(a+\nu)(u_{2}-b)E(s)\over 2(2-s)(a-b)^{2}(u_{2}+\nu)^{2}}\left\{2(u_{2}+\nu)+2(b+\nu)-\right.
(a+ν)}>0\displaystyle\phantom{>{(a+\nu)(u_{2}-b)E(s)\over 2(2-s)(a-b)^{2}(u_{2}+\nu)^{2}}}\left.-(a+\nu)\right\}>0

for b<u2<ab<u_{2}<a, where we have used (a+ν)/4b+ν(a+\nu)/4\leq b+\nu in the second inequality. Since M(a,u2,b)=0M(a,u_{2},b)=0 at u2=bu_{2}=b in view of (34), this implies that M(a,u2,b)>0M(a,u_{2},b)>0 for b<u2<ab<u_{2}<a. It then follows from (30) that λ2(a,u2,b)λ3(a,u2,b)>0\lambda_{2}(a,u_{2},b)-\lambda_{3}(a,u_{2},b)>0. By Lemma 4, we conclude that

dλ2(a,u2,b)du2>0{d\lambda_{2}(a,u_{2},b)\over du_{2}}>0

for b<u2<ab<u_{2}<a.

A graph of the Whitham solution for initial data (35) of type II is given in Figure 3. It is obtained by plotting the exact solution of (46).

5 Smooth Initial Data

In this section, we will study the initial value problem of the Whitham equations when the initial values are given by a smooth monotone function u0(x)u_{0}(x). Since the Burgers solution of (2) will never develop a shock when u0(x)u_{0}(x) is an increasing function, we will be interested only in the case that u0(x)u_{0}(x) is a decreasing function.

We consider the initial function u0(x)u_{0}(x) which is a decreasing function and is bounded at x=±x=\pm\infty

limxu0(x)=a,limx+u0(x)=b.\lim_{x\rightarrow-\infty}u_{0}(x)=a\ ,\quad\lim_{x\rightarrow+\infty}u_{0}(x)=b\ . (47)

By Theorem 1 and Lemma 3, we can use the hodograph transform,

x=λi(u1,u2,u3)t+wi(u1,u2,u3),i=1,2,3,x=\lambda_{i}(u_{1},u_{2},u_{3})t+w_{i}(u_{1},u_{2},u_{3})\ ,\quad i=1,2,3, (48)

to solve the Whitham equations (3). Here, wiw_{i}’s satisfy a linear over-determined system of type (17)

wiuj=Bij(wiwj),\displaystyle{\partial w_{i}\over\partial u_{j}}=B_{ij}(w_{i}-w_{j})\ , (49)

where BijB_{ij}’s are given in Lemma 3.

The boundary conditions on wiw_{i}’s are obtained by observing that the hodograph solution (48) of the Whitham equations (3) must match the characteristic solution (15) of the Burgers equation (2) at the trailing and leading edges in the fashion of (11-14). By (26-27), wiw_{i}’s must satisfy the boundary conditions,

{w1(u1,u1,u3)=w2(u1,u1,u3),w3(u1,u1,u3)=f(u3),\displaystyle\left\{\begin{array}[]{l}w_{1}(u_{1},u_{1},u_{3})=w_{2}(u_{1},u_{1},u_{3}),\\ w_{3}(u_{1},u_{1},u_{3})=f(u_{3}),\end{array}\right. (52)
{w1(u1,u3,u3)=f(u1),w2(u1,u3,u3)=w3(u1,u3,u3),\displaystyle\left\{\begin{array}[]{l}w_{1}(u_{1},u_{3},u_{3})=f(u_{1}),\\ w_{2}(u_{1},u_{3},u_{3})=w_{3}(u_{1},u_{3},u_{3}),\end{array}\right. (55)

where f(u)f(u) is the inverse of the initial function u0(x)u_{0}(x).

Analogous to the KdV case [14, 15], equations (49) subject to boundary conditions (52-55) are related to a boundary value problem of a linear over-determined system of Euler-Poisson-Darboux type (cf. (5))

2(uiuj)2quiuj\displaystyle 2(u_{i}-u_{j})\frac{\partial^{2}q}{\partial{u_{i}}\partial{u_{j}}} =\displaystyle= quiquj,i,j=1,2,3,\displaystyle\frac{\partial q}{\partial u_{i}}-\frac{\partial q}{\partial u_{j}}\ ,\quad i,j=1,2,3, (56)
q(u,u,u)\displaystyle q(u,u,u) =\displaystyle= f(u),\displaystyle f(u)\ , (57)

for i,j=1,2,3i,j=1,2,3. The solution is unique and symmetric in u1u_{1}, u2,u3u_{2},u_{3}. It is given explicitly by [14]

q(u1,u2,u3)=122π1111f(1+u21+v2u1+1+u21v2u2+1u2u3)(1u)(1v2)𝑑u𝑑v.\displaystyle q(u_{1},u_{2},u_{3})=\frac{1}{2\sqrt{2}\pi}\int_{-1}^{1}\int_{-1}^{1}\frac{f({1+u\over 2}{1+v\over 2}u_{1}+{1+u\over 2}{1-v\over 2}u_{2}+{1-u\over 2}u_{3})}{\sqrt{(1-u)(1-v^{2})}}dudv\ . (58)
Theorem 12

If q(u1,u2,u3)q(u_{1},u_{2},u_{3}) is a solution of (56) and (57), then wi(u1,u2,u3)w_{i}(u_{1},u_{2},u_{3})’s given by

wi\displaystyle w_{i}\ =[λi(u1,u2,u3)γ]q(u1,u2,u3)ui+q(u1,u2,u3),\displaystyle=[\lambda_{i}(u_{1},u_{2},u_{3})-\gamma]\ {\partial q(u_{1},u_{2},u_{3})\over\partial u_{i}}+q(u_{1},u_{2},u_{3})\ , (59)

where γ=u1+u2+u3+2ν\gamma=u_{1}+u_{2}+u_{3}+2\nu, solve equations (49) and satisfy boundary conditions (52-55).

Proof.

By Lemma 3 and (56), we obtain

[λjγ][quiquj]Bij=(qujqui)+[λiγ]2quiuj.\displaystyle[\lambda_{j}-\gamma]\left[{\partial q\over\partial u_{i}}-{\partial q\over\partial u_{j}}\right]B_{ij}=\left({\partial q\over\partial u_{j}}-{\partial q\over\partial u_{i}}\right)+[\lambda_{i}-\gamma]{\partial^{2}q\over\partial u_{i}\partial u_{j}}\ . (60)

Using (59), we calculate

wiuj\displaystyle{\partial w_{i}\over\partial u_{j}} =\displaystyle= λiujqui+[λiγ]2quiuj+qujqui,\displaystyle{\partial\lambda_{i}\over\partial u_{j}}{\partial q\over\partial u_{i}}+\left[\lambda_{i}-\gamma\right]{\partial^{2}q\over\partial u_{i}\partial u_{j}}+{\partial q\over\partial u_{j}}-{\partial q\over\partial u_{i}}\ ,
wiwj\displaystyle w_{i}-w_{j} =\displaystyle= [λiγ][quiquj]+[λiλj]qui.\displaystyle\left[\lambda_{i}-\gamma\right][{\partial q\over\partial u_{i}}-{\partial q\over\partial u_{j}}]+\left[\lambda_{i}-\lambda_{j}\right]{\partial q\over\partial u_{i}}\ .

Substituting these into (60), we find that wiw_{i}’s satisfy (49).

Finally, we shall check the boundary conditions (52-55). We only consider the leading edge, and the trailing edge can be handled in the same way.

Since q(u1,u2,u3)q(u_{1},u_{2},u_{3}) is symmetric in u1u_{1}, u2u_{2} and u3u_{3}, the first condition of (52) follows from (59) and (27).

For the second condition, it follows from (27) and (59) again that

w3(u1,u1,u3)=2(u3u1)qu3+q.w_{3}(u_{1},u_{1},u_{3})=2(u_{3}-u_{1}){\partial q\over\partial u_{3}}+q\ . (61)

Differentiating this with respect to u1u_{1} yields,

w3u1=2qu3+2(u3u1)[2qu1u3+2qu2u3]+qu1+qu2=0,\displaystyle{\partial w_{3}\over\partial u_{1}}=-2{\partial q\over\partial u_{3}}+2(u_{3}-u_{1})[{\partial^{2}q\over\partial u_{1}\partial u_{3}}+{\partial^{2}q\over\partial u_{2}\partial u_{3}}]+{\partial q\over\partial u_{1}}+{\partial q\over\partial u_{2}}=0\ ,

where we have used (56) in the last equality. Since w3(u1,u1,u3)w_{3}(u_{1},u_{1},u_{3}) is independent of u1u_{1}, we replace u1u_{1} by u3u_{3} in (61) and use (57) to obtain the second condition of (52).

Theorem 12 has been reported in [1] in the case of ν=0\nu=0.

In the rest of this section, we study the hodograph transform (48) with wiw_{i}’s given by (58) and (59). We shall show that the transform can be solved for u1u_{1}, u2u_{2} and u3u_{3} as functions of (x,t)(x,t) within a cusp in the xx-tt plane.

Since tb=[3min(u0(x))]1t_{b}=-[3\min\left(u^{\prime}_{0}(x)\right)]^{-1} is the breaking time of the Burgers solution of (2), the breaking is caused by an inflection point in the initial data. If x0x_{0} is this inflection point, then (xb,tb)(x_{b},t_{b}) is the breaking point on the evolving curve where xb=x0+[3u0(x0)+2ν]tbx_{b}=x_{0}+[3u_{0}(x_{0})+2\nu]t_{b}, and tbt_{b} is the breaking time. Without loss of generality, we may assume xb=0x_{b}=0, tb=0t_{b}=0 and denote u0(0)u_{0}(0) by u^\hat{u}. The effect of these choices is that we are starting at the breaking time, and the evolving curve is about to turn over at the point (0,u^)(0,\hat{u}) in the xx-uu plane. It immediately follows that

f(u^)=f(u^)=f′′(u^)=0,f(\hat{u})=f^{\prime}(\hat{u})=f^{\prime\prime}(\hat{u})=0\ , (62)

where x=f(u)x=f(u) is the inverse function of the decreasing initial data u=u0(x)u=u_{0}(x). On the assumption that x=f(u)x=f(u) has only one inflection point, it follows from the monotonicity of the function f(u)f(u) that

f′′(u)={<0u>u^=0u=u^>0u<u^.f^{\prime\prime}(u)=\left\{\begin{array}[]{ll}<0&\quad u>\hat{u}\\ =0&\quad u=\hat{u}\\ >0&\quad u<\hat{u}\end{array}\right.. (63)

Under a little bit stronger condition than (63), we will be able to show that hodograph transform (48) can be inverted to give u1u_{1}, u2u_{2} and u3u_{3} as functions of (x,t)(x,t) in some domain of the xx-tt plane.

Theorem 13

Suppose u0(x)u_{0}(x) is a decreasing function satisfying (47) with a+ν>b+ν>0a+\nu>b+\nu>0. If, in addition to (62), the inverse function f(u)f(u) satisfies f′′′(u)f^{\prime\prime\prime}(u) << 0 for b<u<ab<u<a, then transform (48) with wiw_{i}’s given by (58) and (59) can be solved for u1u_{1}, u2u_{2} and u3u_{3} as functions of (x,t)(x,t) within a cusp in the xx-tt plane for all t>0t>0. Furthermore, these u1u_{1}, u2u_{2} and u3u_{3} satisfy boundary conditions (52-55) on the boundary of the cusp.

The proof is based on a series of lemmas. The organization is as follows: we eliminate xx from transform (48) to obtain two equations involving u1u_{1}, u2u_{2}, u3u_{3}, and tt. These two equations can be shown, for each fixed time after the breaking, to determine u1u_{1} and u3u_{3} as decreasing functions of u2u_{2} within an interval whose end points depend on tt. Substituting u1u_{1} and u3u_{3} as functions of u2u_{2} into the hodograph transform, we find that, within a cusp in the xx-tt plane, u2u_{2} is a function of (x,t)(x,t), and so, therefore, are u1u_{1} and u3u_{3}.

First, we conclude from formula (58)

Lemma 14

If f(u)f(u) satisfies the conditions of Theorem 13, then q(u1,u2,u3)q(u_{1},u_{2},u_{3}) given by (58) satisfies

3quiujuk<0,i,j,k=1,2,3.\frac{\partial^{3}q}{\partial u_{i}\partial u_{j}\partial u_{k}}<0\ ,\hskip 14.45377pti,j,k=1,2,3\ .

Eliminating xx from (48) yields

(λ1t+w1)(λ2t+w2)\displaystyle(\lambda_{1}t+w_{1})-(\lambda_{2}t+w_{2}) =\displaystyle= 0,\displaystyle 0\ , (64)
(λ2t+w2)(λ3t+w3)\displaystyle(\lambda_{2}t+w_{2})-(\lambda_{3}t+w_{3}) =\displaystyle= 0.\displaystyle 0\ . (65)

Using (59) for w1w_{1} and w2w_{2}, and (22) for λ1\lambda_{1} and λ2\lambda_{2} , we write

(λ1t+w1)(λ2t+w2)\displaystyle(\lambda_{1}t+w_{1})-(\lambda_{2}t+w_{2}) =\displaystyle= (λ1γ)[t+qu1](λ2γ)[t+qu2]\displaystyle(\lambda_{1}-\gamma)[t+{\partial q\over\partial u_{1}}]-(\lambda_{2}-\gamma)[t+{\partial q\over\partial u_{2}}]
=\displaystyle= 2(u1u2)(u3+ν)Π(u2+ν)EF(u1,u2,u3),\displaystyle{2(u_{1}-u_{2})(u_{3}+\nu)\Pi\over(u_{2}+\nu)E}\ F(u_{1},u_{2},u_{3})\ ,

where

F=(t+qu1)+sEE(1s)Ku2+νu1+ν[t+qu2].F=(t+{\partial q\over\partial u_{1}})+{sE\over E-(1-s)K}\ {u_{2}+\nu\over u_{1}+\nu}\ [t+{\partial q\over\partial u_{2}}]\ . (66)

Similarly, we use (59) for w2w_{2} and w3w_{3} to write

(λ2t+w2)(λ3t+w3)\displaystyle(\lambda_{2}t+w_{2})-(\lambda_{3}t+w_{3}) =\displaystyle= (λ2λ3)(t+qu2)+(λ3γ)(qu2qu3)\displaystyle(\lambda_{2}-\lambda_{3})(t+{\partial q\over\partial u_{2}})+(\lambda_{3}-\gamma)({\partial q\over\partial u_{2}}-{\partial q\over\partial u_{3}})
=\displaystyle= 2(u2u3)(u3+ν)Π(u2+ν)[KE][E(1s)K]G(u1,u2,u3),\displaystyle{2(u_{2}-u_{3})(u_{3}+\nu)\Pi\over(u_{2}+\nu)[K-E][E-(1-s)K]}\ G(u_{1},u_{2},u_{3})\ ,

where

G=M(u1,u2,u3)(t+qu2)2(u2u3)[E(1s)K]2qu2u3.G=M(u_{1},u_{2},u_{3})(t+{\partial q\over\partial u_{2}})-2(u_{2}-u_{3})[E-(1-s)K]{\partial^{2}q\over\partial u_{2}\partial u_{3}}\ . (67)

In the derivation, we have used formula (30) for λ2λ3\lambda_{2}-\lambda_{3}, formula (22) for λ3\lambda_{3} and equation (56).

Since (105) implies that K(s)E(s)>0K(s)-E(s)>0 and E(s)(1s)K(s)>0E(s)-(1-s)K(s)>0, equations (64) and (65) are equivalent to

F(u1,u2,u3)=0,G(u1,u2,u3)=0F(u_{1},u_{2},u_{3})=0\ ,\quad G(u_{1},u_{2},u_{3})=0 (68)

for 0<s<10<s<1.

5.1 The trailing edge

We first study the trailing edge. We use (101), (102), and (34) to expand

F\displaystyle F =\displaystyle= t+qu1+2(u2+ν)(u1+ν)(t+qu2)3(u2+ν)4(u1+ν)(t+qu2)s\displaystyle t+{\partial q\over\partial u_{1}}+{2(u_{2}+\nu)\over(u_{1}+\nu)}\ (t+{\partial q\over\partial u_{2}})-{3(u_{2}+\nu)\over 4(u_{1}+\nu)}\ (t+{\partial q\over\partial u_{2}})\ s (69)
3(u2+ν)32(u1+ν)(t+qu2)s2+O(s3),\displaystyle-\ {3(u_{2}+\nu)\over 32(u_{1}+\nu)}(t+{\partial q\over\partial u_{2}})\ s^{2}+O(s^{3})\ ,

and

G\displaystyle G =\displaystyle= π2{[u2+ν2(u1+ν)+116(13(u1u2)u1u3)](t+qu2)\displaystyle{\pi\over 2}\left\{[{u_{2}+\nu\over 2(u_{1}+\nu)}+{1\over 16}\ (1-{3(u_{1}-u_{2})\over u_{1}-u_{3}})](t+{\partial q\over\partial u_{2}})-\right. (70)
(u1u3)(u2+ν)u1+ν2qu2u3}s2\displaystyle\phantom{{\pi\over 2}}\left.-{(u_{1}-u_{3})(u_{2}+\nu)\over u_{1}+\nu}\ {\partial^{2}q\over\partial u_{2}\partial u_{3}}\right\}s^{2}
+π2{3128(15u1u2u1u3)(t+qu2)\displaystyle+{\pi\over 2}\left\{{3\over 128}(1-5{u_{1}-u_{2}\over u_{1}-u_{3}})(t+{\partial q\over\partial u_{2}})-\right.
(u1u3)(u2+ν)8(u1+ν)2qu2u3}s3+O(s4).\displaystyle\phantom{{\pi\over 2}}\left.-{(u_{1}-u_{3})(u_{2}+\nu)\over 8(u_{1}+\nu)}{\partial^{2}q\over\partial u_{2}\partial u_{3}}\right\}s^{3}+O(s^{4})\ .

Taking the limits of F=0F=0 and G/s2=0G/s^{2}=0 as s0s\rightarrow 0 and simplifying the results a bit, we obtain the equations governing the trailing edge

U(u1,u3):=(u1+ν)(t+q(u1,u3,u3)u1)+2(u3+ν)(t+q(u1,u3,u3)u2)=0,U(u_{1},u_{3}):=(u_{1}+\nu)(t+{\partial q(u_{1},u_{3},u_{3})\over\partial u_{1}})+2(u_{3}+\nu)(t+{\partial q(u_{1},u_{3},u_{3})\over\partial u_{2}})=0\,, (71)

and

V(u1,u3):=[(u3+ν)14(u1+ν)](t+qu2)2(u1u3)(u3+ν)2qu2u3=0.V(u_{1},u_{3}):=[(u_{3}+\nu)-{1\over 4}(u_{1}+\nu)](t+{\partial q\over\partial u_{2}})-2(u_{1}-u_{3})(u_{3}+\nu)\ {\partial^{2}q\over\partial u_{2}\partial u_{3}}=0\,. (72)

Solving for tt from (71) and substituting it into (72), we use (56) to simplify the result and get

W(u1,u3)\displaystyle W(u_{1},u_{3}) :=[(u3+ν)14(u1+ν)](u1+ν)2qu1u3\displaystyle:=[(u_{3}+\nu)-{1\over 4}(u_{1}+\nu)](u_{1}+\nu){\partial^{2}q\over\partial u_{1}\partial u_{3}}
+[(u1+ν)+2(u3+ν)](u3+ν)2qu2u3=0.\displaystyle\phantom{:=}\quad+[(u_{1}+\nu)+2(u_{3}+\nu)](u_{3}+\nu){\partial^{2}q\over\partial u_{2}\partial u_{3}}=0\ . (73)

Obviously, equations (71) and (72) are equivalent to equations (71) and (73).

We now solve equation (73) for u3u_{3} as a function of u1u_{1} in the neighborhood of u1=u3=u^u_{1}=u_{3}=\hat{u}. We use formula (58) and the symmetry of qq to write

2q(u1,u3,u3)u1u3\displaystyle{\partial^{2}q(u_{1},u_{3},u_{3})\over\partial u_{1}\partial u_{3}} =\displaystyle= 1162π11f′′(1+μ2u3+1μ2u1)(1μ2)1μ𝑑μ,\displaystyle{1\over 16\sqrt{2}\pi}\int_{-1}^{1}f^{\prime\prime}({1+\mu\over 2}u_{3}+{1-\mu\over 2}u_{1}){(1-\mu^{2})\over\sqrt{1-\mu}}\ d\mu\ , (74)
2q(u1,u3,u3)u2u3\displaystyle{\partial^{2}q(u_{1},u_{3},u_{3})\over\partial u_{2}\partial u_{3}} =\displaystyle= 1642π11f′′(1+μ2u3+1μ2u1)(1+μ)21μ𝑑μ.\displaystyle{1\over 64\sqrt{2}\pi}\int_{-1}^{1}f^{\prime\prime}({1+\mu\over 2}u_{3}+{1-\mu\over 2}u_{1}){(1+\mu)^{2}\over\sqrt{1-\mu}}\ d\mu\ . (75)

For u1=u^u_{1}=\hat{u}, it follows from (63), (74) and (75) that equation (73) has only the solution u3=u^u_{3}=\hat{u} in the neighborhood of u1=u3=u^u_{1}=u_{3}=\hat{u}.

For u1u_{1} which is a little bigger than u^\hat{u}, we will show that there is a unique u3u_{3} such that equation (73) holds. By (63), (74) and (75), we have

W(u^,u~3)>0for some u~3<u^.W(\hat{u},\tilde{u}_{3})>0\quad\mbox{for some $\tilde{u}_{3}<\hat{u}$}\ .

Hence,

W(u1,u~3)>0for u1 a bit larger than u^.W(u_{1},\tilde{u}_{3})>0\quad\mbox{for $u_{1}$ a bit larger than $\hat{u}$}\ .

For each of such u1u_{1}’s, we deduct from (63) and (73) again that

W(u1,u^)<0.W(u_{1},\hat{u})<0\ .

By the mean value theorem, we show that, for each u1u_{1} that is slightly larger than u^\hat{u}, there exists a u3<u^u_{3}<\hat{u} such that (73) holds. It is easy to check the uniqueness of u3u_{3}.

Therefore, (73) determines u3u_{3} as a function of u1u_{1}, u3u_{3} == A(u1)A(u_{1}), for small non-positive u1u_{1} with A(u^)A(\hat{u}) == u^\hat{u}. The smoothness of the function f(u)f(u) and Lemma 14 imply that A(u1)A(u_{1}) is a smooth decreasing function of u1u_{1}.

Next, substituting u3u_{3} == A(u1)A(u_{1}) into (71), it is not hard to show that (71) determines u1u_{1} as a function of tt. We have therefore proved the short time version of the following lemma.

Lemma 15

Under the conditions of Theorem 13, equations (71) and (72) have a unique solution (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)) with u2(t)=u3(t)u_{2}^{-}(t)=u_{3}^{-}(t) for all t \geq 0. The solution has the property that u1(t)u_{1}^{-}(t) >> u2(t)u_{2}^{-}(t) = u3(t)u_{3}^{-}(t) for tt >> 0 and that u1(0)u_{1}^{-}(0) = u2(0)=u3(0)=u^u_{2}^{-}(0)=u_{3}^{-}(0)=\hat{u}.

Proof.   We will now extend the solution (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)) of equations (71) and (72) for all t>0t>0. Before doing this, we need a lemma.

Lemma 16

Under conditions of Theorem 13, the following hold:

2qu1u2=2qu1u3<0,2qu12<0,t+qu1<0,\displaystyle\frac{\partial^{2}q}{\partial u_{1}\partial u_{2}}=\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}<0\ ,\quad\frac{\partial^{2}q}{\partial u_{1}^{2}}<0\ ,\quad t+{\partial q\over\partial u_{1}}<0\ ,

and

t+qu2=t+qu3>0,\quad t+{\partial q\over\partial u_{2}}=t+{\partial q\over\partial u_{3}}>0\,,

at the solution (u1,u3,u3)(u_{1},u_{3},u_{3}) of (73) where u1>u3u_{1}>u_{3}.

Proof.   By (56) and Lemma 14,

2qu1u32qu2u3=u3[qu1qu2]=2(u1u2)3qu1u2u3<0,\displaystyle\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}-\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}=\frac{\partial}{\partial u_{3}}[\frac{\partial q}{\partial u_{1}}-\frac{\partial q}{\partial u_{2}}]=2(u_{1}-u_{2})\frac{\partial^{3}q}{\partial u_{1}\partial u_{2}\partial u_{3}}<0\,, (76)

which when combined with (73) gives

2qu1u3<0\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}<0

as long as 4(u3+ν)(u1+ν)>04(u_{3}+\nu)-(u_{1}+\nu)>0. This inequality holds even when 4(u3+ν)(u1+ν)04(u_{3}+\nu)-(u_{1}+\nu)\leq 0. To see this, suppose the inequality fails at some point, at which u2u32q\partial^{2}_{u_{2}u_{3}}q must vanish because of (73). This would violate (76).

The other inequalities of Lemma 16 are shown in the same way.

We now calculate the partial derivatives of UU and VV at the solution (u1,u3,u3)(u_{1},u_{3},u_{3}) of (71) and (72),

Uu1\displaystyle{\partial U\over\partial u_{1}} =\displaystyle= t+qu1+(u1+ν)2qu12+2(u3+ν)2qu1u3<0,\displaystyle t+{\partial q\over\partial u_{1}}+(u_{1}+\nu){\partial^{2}q\over\partial u_{1}^{2}}+2(u_{3}+\nu){\partial^{2}q\over\partial u_{1}\partial u_{3}}<0\,,
Uu3\displaystyle{\partial U\over\partial u_{3}} =\displaystyle= 2(t+qu3)+2(u1+ν)2qu1u3+8(u3+ν)2qu2u3\displaystyle 2(t+{\partial q\over\partial u_{3}})+2(u_{1}+\nu){\partial^{2}q\over\partial u_{1}\partial u_{3}}+8(u_{3}+\nu){\partial^{2}q\over\partial u_{2}\partial u_{3}}
=\displaystyle= 1u1u3[(u1+ν)(t+qu1)+2(u3+ν)(t+qu3)]=0,\displaystyle{1\over u_{1}-u_{3}}\left[(u_{1}+\nu)(t+{\partial q\over\partial u_{1}})+2(u_{3}+\nu)(t+{\partial q\over\partial u_{3}})\right]=0\,,
Vu3\displaystyle{\partial V\over\partial u_{3}} =\displaystyle= t+qu2+[(8(u3+ν)3(u1+ν)]2qu2u3\displaystyle t+{\partial q\over\partial u_{2}}+[(8(u_{3}+\nu)-3(u_{1}+\nu)]{\partial^{2}q\over\partial u_{2}\partial u_{3}}
2(u1u3)(u3+ν)(3qu22u3+3qu2u32)\displaystyle\phantom{t+}\quad-2(u_{1}-u_{3})(u_{3}+\nu)({\partial^{3}q\over\partial u_{2}^{2}\partial u_{3}}+{\partial^{3}q\over\partial u_{2}\partial u_{3}^{2}})
=\displaystyle= 3(u1+ν)212(u1+ν)(u3+ν)+24(u3+ν)28(u1u3)(u3+ν)(t+qu2)\displaystyle{3(u_{1}+\nu)^{2}-12(u_{1}+\nu)(u_{3}+\nu)+24(u_{3}+\nu)^{2}\over 8(u_{1}-u_{3})(u_{3}+\nu)}\ (t+{\partial q\over\partial u_{2}})
2(u1u3)(u3+ν)(3qu22u3+3qu2u32)>0,\displaystyle-\ 2(u_{1}-u_{3})(u_{3}+\nu)({\partial^{3}q\over\partial u_{2}^{2}\partial u_{3}}+{\partial^{3}q\over\partial u_{2}\partial u_{3}^{2}})>0\,,

where we have used Lemmas 14 and 16 to determine the signs of the derivatives. These show that the Jacobian

(U,V)(u1,u3)0\frac{\partial(U,V)}{\partial(u_{1},u_{3})}\neq 0

on the solution (u1,u3,u3)(u_{1},u_{3},u_{3}) of equations (71) and (72) where u1>u3u_{1}>u_{3}.

Therefore, by the Implicit Function Theorem, equations (71) and (72) can be solved for u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t) = u3(t)u_{3}^{-}(t) for all t0t\geq 0. Furthermore, it is easy to check that u1(t)u_{1}^{-}(t) is an increasing function of tt. ∎

5.2 The leading edge

At the leading edge, u1=u2u_{1}=u_{2}, i.e., s=1s=1, it follows from (103), (104), (66), and (67) that equations (68) turn out to be

t+qu1(u1,u1,u3)=0,t+qu3(u1,u1,u3)=0.t+{\partial q\over\partial u_{1}}(u_{1},u_{1},u_{3})=0\ ,\quad t+{\partial q\over\partial u_{3}}(u_{1},u_{1},u_{3})=0\ .

In the same way as we handle Lemma 15, we can solve the above equations for u1u_{1} and u3u_{3} as functions of tt, leading to the lemma.

Lemma 17

Under the conditions of Theorem 13, system (68) has a unique solution (u1+(t)u_{1}^{+}(t), u2+(t)u_{2}^{+}(t), u3+(t)u_{3}^{+}(t)) with u1+(t)=u2+(t)u_{1}^{+}(t)=u_{2}^{+}(t) for all t0t\geq 0. The solution has the property that u1+(t)=u2+(t)>u3+(t)u_{1}^{+}(t)=u_{2}^{+}(t)>u_{3}^{+}(t) for t>0t>0 and that u1+(0)=u2+(0)=u3+(0)=u^u_{1}^{+}(0)=u_{2}^{+}(0)=u_{3}^{+}(0)=\hat{u}.

5.3 Near the trailing edge

By Lemma 15, (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)) satisfies equations (71) and (72). For each fixed t >> 0, we need to solve equations (68) for u1u_{1} and u3u_{3} as functions of u2u_{2} in the neighborhood of u2(t)u_{2}^{-}(t). This is carried out in

Lemma 18

For each t >> 0, equations (68) can be solved for u1u_{1} and u3u_{3} in terms of u2u_{2} in the neighborhood of (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t))

{u1=M(u2)u3=N(u2)\left\{\begin{array}[]{ll}u_{1}=M(u_{2})\\ u_{3}=N(u_{2})\end{array}\right. (77)

such that u1(t)=M(u2(t))u_{1}^{-}(t)=M(u_{2}^{-}(t)) and u3(t)=N(u2(t))u_{3}^{-}(t)=N(u_{2}^{-}(t)), Moreover, for u2>u2(t)u_{2}>u_{2}^{-}(t),

N(u2)<u2<M(u2).N(u_{2})<u_{2}<M(u_{2})\,. (78)

Proof.   Calculating the first partial derivatives of FF and G/s2G/s^{2} of (69) and (70) at (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)), where u2(t)=u3(t)u_{2}^{-}(t)=u_{3}^{-}(t), and using (56), we find

Fu1\displaystyle{\partial F\over\partial u_{1}} =\displaystyle= 2qu122(u2+ν)(u1+ν)2(t+qu2)+2(u2+ν)u1+ν2qu1u2<0,\displaystyle{\partial^{2}q\over\partial u_{1}^{2}}-{2(u_{2}+\nu)\over(u_{1}+\nu)^{2}}(t+{\partial q\over\partial u_{2}})+{2(u_{2}+\nu)\over u_{1}+\nu}{\partial^{2}q\over\partial u_{1}\partial u_{2}}<0\ ,
Fu2\displaystyle{\partial F\over\partial u_{2}} =\displaystyle= 2qu1u2+[2u1+ν341u1u3](t+qu2)+\displaystyle{\partial^{2}q\over\partial u_{1}\partial u_{2}}+[{2\over u_{1}+\nu}-{3\over 4}{1\over u_{1}-u_{3}}](t+{\partial q\over\partial u_{2}})+
+6(u2+ν)u1+ν2qu2u3=0,\displaystyle\phantom{{\partial^{2}q\over\partial u_{1}^{2}}}+{6(u_{2}+\nu)\over u_{1}+\nu}{\partial^{2}q\over\partial u_{2}\partial u_{3}}=0\ ,
Fu3\displaystyle{\partial F\over\partial u_{3}} =\displaystyle= 2qu1u3+341u1u3(t+qu2)+2(u2+ν)u1+ν2qu2u3=0,\displaystyle{\partial^{2}q\over\partial u_{1}\partial u_{3}}+{3\over 4}{1\over u_{1}-u_{3}}(t+{\partial q\over\partial u_{2}})+{2(u_{2}+\nu)\over u_{1}+\nu}{\partial^{2}q\over\partial u_{2}\partial u_{3}}=0\ ,
(G/s2)u2\displaystyle{\partial(G/s^{2})\over\partial u_{2}} =\displaystyle= π2{19(u1+ν)16(u3+ν)32(u1u3)(u1+ν)(t+qu2)u1u22(u1+ν)2qu2u3}\displaystyle{\pi\over 2}\left\{{19(u_{1}+\nu)-16(u_{3}+\nu)\over 32(u_{1}-u_{3})(u_{1}+\nu)}(t+{\partial q\over\partial u_{2}})-{u_{1}-u_{2}\over 2(u_{1}+\nu)}{\partial^{2}q\over\partial u_{2}\partial u_{3}}\right\}
=\displaystyle= 2(u1+ν)2+9(u1+ν)(u3+ν)8(u3+ν)264(u1u3)(u1+ν)(u2+ν)π(t+qu2)>0,\displaystyle{2(u_{1}+\nu)^{2}+9(u_{1}+\nu)(u_{3}+\nu)-8(u_{3}+\nu)^{2}\over 64(u_{1}-u_{3})(u_{1}+\nu)(u_{2}+\nu)}\ \pi(t+{\partial q\over\partial u_{2}})>0\ ,
(G/s2)u3\displaystyle{\partial(G/s^{2})\over\partial u_{3}} =\displaystyle= π2{[316(u1u3)+3(u1+ν)32(u1u3)(u2+ν)](t+qu2)+\displaystyle{\pi\over 2}\left\{[-{3\over 16(u_{1}-u_{3})}+{3(u_{1}+\nu)\over 32(u_{1}-u_{3})(u_{2}+\nu)}](t+{\partial q\over\partial u_{2}})+\right.
+3(u2+ν)2(u1+ν)2qu2u3(u1u3)(u2+ν)u1+ν3qu2u32}\displaystyle\phantom{{\pi\over 2}}\left.+{3(u_{2}+\nu)\over 2(u_{1}+\nu)}{\partial^{2}q\over\partial u_{2}\partial u_{3}}-{(u_{1}-u_{3})(u_{2}+\nu)\over u_{1}+\nu}{\partial^{3}q\over\partial u_{2}\partial u_{3}^{2}}\right\}
=\displaystyle= π2{3[(u1+ν)24(u1+ν)(u3+ν)+8(u3+ν)2]32(u1u3)(u1+ν)(u2+ν)(t+qu2)\displaystyle{\pi\over 2}\left\{{3[(u_{1}+\nu)^{2}-4(u_{1}+\nu)(u_{3}+\nu)+8(u_{3}+\nu)^{2}]\over 32(u_{1}-u_{3})(u_{1}+\nu)(u_{2}+\nu)}\ (t+{\partial q\over\partial u_{2}})\right.
(u1u3)(u2+ν)u1+ν3qu2u32}>0,\displaystyle\left.\phantom{\pi/2\{}-{(u_{1}-u_{3})(u_{2}+\nu)\over u_{1}+\nu}{\partial^{3}q\over\partial u_{2}\partial u_{3}^{2}}\right\}>0\ ,

where we have used (71) and (72) to simplify the results, and Lemmas 14 and 16 to determine the signs of the derivatives.

These prove the non-vanishing of the Jacobian

(F,G/s2)(u1,u3)\frac{\partial(F,G/s^{2})}{\partial(u_{1},u_{3})}

at (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)). Hence, equations (68) can be solved for

{u1=M(u2)u3=N(u2)\left\{\begin{matrix}u_{1}=M(u_{2})\\ u_{3}=N(u_{2})\end{matrix}\right.

in a neighborhood of u2(t)u_{2}^{-}(t) such that u1(t)u_{1}^{-}(t) = M(u2(t))M(u_{2}^{-}(t)) and u3(t)u_{3}^{-}(t) = N(u2(t))N(u_{2}^{-}(t)). Furthermore, N(u2)N(u_{2}) is a decreasing function of u2u_{2} and so (78) holds. ∎

5.4 The passage from the trailing edge to the leading edge

We shall show that, for each fixed t >> 0, solutions (77) of equations (68) can be further extended as long as N(u2)N(u_{2}) << u2u_{2} << M(u2)M(u_{2}). The Jacobian of system (64) and (65) with respect to (u1,u3)(u_{1},u_{3}) has to be estimated along the extension.

Lemma 19

Under the conditions of Theorem 13, the following inequalities hold for each t>0t>0.

(λ1t+w1)u1<0,(λ2t+w2)u2>0,(λ3t+w3)u3<0\frac{\partial(\lambda_{1}t+w_{1})}{\partial u_{1}}<0,\quad\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}}>0,\quad\frac{\partial(\lambda_{3}t+w_{3})}{\partial u_{3}}<0 (79)

on the solution (u1u_{1}, u2u_{2}, u3u_{3}) of (64) and (65) (or equivalently (68)) in the region 0<u3+ν0<u_{3}+\nu << u2+νu_{2}+\nu << u1+νu_{1}+\nu.

Proof.   Using formulae (59) for w1w_{1}, w2w_{2}, and w3w_{3}, we see that (64) and (65) are equivalent to

[λ1(u1+u2+u3+2ν)](t+qu1)=[λ2(u1+u2+u3+2ν)](t+qu2),[\lambda_{1}-(u_{1}+u_{2}+u_{3}+2\nu)](t+\frac{\partial q}{\partial u_{1}})=[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)](t+\frac{\partial q}{\partial u_{2}})\,, (80)
[λ22(u1+u2+u3+2ν)](t+qu2)=[λ3(u1+u2+u3+2ν)](t+qu3).[\lambda_{2}-2(u_{1}+u_{2}+u_{3}+2\nu)](t+\frac{\partial q}{\partial u_{2}})=[\lambda_{3}-(u_{1}+u_{2}+u_{3}+2\nu)](t+\frac{\partial q}{\partial u_{3}})\,. (81)

By Lemma 16,

2q(u1,u2,u3)u1u2<0,2q(u1,u2,u3)u1u3<0\frac{\partial^{2}q(u_{1},u_{2},u_{3})}{\partial u_{1}\partial u_{2}}<0,\quad\frac{\partial^{2}q(u_{1},u_{2},u_{3})}{\partial u_{1}\partial u_{3}}<0 (82)

at the trailing edge.

We claim that inequalities (82) hold on the solution (u1,u2,u3)(u_{1},u_{2},u_{3}) of (64) and (65) as long as 0<u3+ν0<u_{3}+\nu << u2+νu_{2}+\nu << u1+νu_{1}+\nu.

We justify the claim by contradiction. Suppose otherwise, for instance at some point (u¯1,u¯2,u¯3)(\bar{u}_{1},\bar{u}_{2},\bar{u}_{3}) on the solution of (64) and (65), with 0<u¯3+ν<u¯2+ν<u¯1+ν0<\bar{u}_{3}+\nu<\bar{u}_{2}+\nu<\bar{u}_{1}+\nu,

2qu1u2=0.\frac{\partial^{2}q}{\partial u_{1}\partial u_{2}}=0\ .

In view of (56), this gives

qu1=qu2at (u¯1,u¯2,u¯3),\frac{\partial q}{\partial u_{1}}=\frac{\partial q}{\partial u_{2}}\quad\mbox{at $(\bar{u}_{1},\bar{u}_{2},\bar{u}_{3})$}\ ,

which together with (23), (24), and (80) imply

t+12qu1=t+12qu2=0.t+\frac{1}{2}\frac{\partial q}{\partial u_{1}}=t+\frac{1}{2}\frac{\partial q}{\partial u_{2}}=0\ . (83)

By (24), (25), (81), and (83), we obtain

t+qu3=0,t+\frac{\partial q}{\partial u_{3}}=0\,,

which together with (56) gives

2qu1u2=2qu1u3=0\frac{\partial^{2}q}{\partial u_{1}\partial u_{2}}=\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}=0 (84)

at (u¯1,u¯2,u¯3)(\bar{u}_{1},\bar{u}_{2},\bar{u}_{3}).

On the other hand, by (56) and Lemma 14,

2qu1u22qu1u3=2(u2u3)3qu1u2u3<0\frac{\partial^{2}q}{\partial u_{1}\partial u_{2}}-\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}=2(u_{2}-u_{3})\frac{\partial^{3}q}{\partial u_{1}\partial u_{2}\partial u_{3}}<0

at (u¯1,u¯2,u¯3)(\bar{u}_{1},\bar{u}_{2},\bar{u}_{3}). This contradicts (84) and the claim has been justified.

By (56), we have

2(u1u3)2qu1u3=qu1qu3.2(u_{1}-u_{3})\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}=\frac{\partial q}{\partial u_{1}}-\frac{\partial q}{\partial u_{3}}\,.

Differentiating this with respect to u1u_{1} yields

2qu12=32qu1u3+2(u1u3)3qu12u3<0,\displaystyle\frac{\partial^{2}q}{\partial u_{1}^{2}}=3\frac{\partial^{2}q}{\partial u_{1}\partial u_{3}}+2(u_{1}-u_{3})\frac{\partial^{3}q}{\partial u_{1}^{2}\partial u_{3}}<0\ , (85)

where we have used (82) and Lemma 14 in the last step.

It follows from (82) and (56) that

qu1<qu2,qu1<qu3,\frac{\partial q}{\partial u_{1}}<\frac{\partial q}{\partial u_{2}}\ ,\quad\frac{\partial q}{\partial u_{1}}<\frac{\partial q}{\partial u_{3}}\,,

which when combined with (23), (24), (25), (80) and (81) gives

t+12qu1<0,t+12qu2>0,t+12qu3>0t+\frac{1}{2}\frac{\partial q}{\partial u_{1}}<0,\quad t+\frac{1}{2}\frac{\partial q}{\partial u_{2}}>0,\quad t+\frac{1}{2}\frac{\partial q}{\partial u_{3}}>0 (86)

on the solution (u1u_{1}, u2u_{2}, u3u_{3}) of (64) and (65) in the region 0<u3+ν<u2+ν<u1+ν0<u_{3}+\nu<u_{2}+\nu<u_{1}+\nu.

Therefore, by (59),

(λ1t+w1)u1\displaystyle\frac{\partial(\lambda_{1}t+w_{1})}{\partial u_{1}} =\displaystyle= λ1u1(t+qu1)+[λ1(u1+u2+u3+2ν)]2qu12<0,\displaystyle\frac{\partial\lambda_{1}}{\partial u_{1}}(t+\frac{\partial q}{\partial u_{1}})+[\lambda_{1}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{1}^{2}}<0\ ,

where in the last inequality we have used (23), (85), (86), and

λ1u1=Iuiui2I(uiI)2>0.\frac{\partial\lambda_{1}}{\partial u_{1}}={I\partial^{2}_{u_{i}u_{i}}I\over(\partial_{ui}I)^{2}}>0\ .

This proves the first inequality of (79).

Next we shall prove the rest of Lemma 19. By (56), we have

2(u2u3)2qu2u3=qu2qu3.2(u_{2}-u_{3})\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}=\frac{\partial q}{\partial u_{2}}-\frac{\partial q}{\partial u_{3}}\,.

Differentiating this with respect to u2u_{2} yields

2qu22=32qu2u3+2(u2u3)3qu22u3.\frac{\partial^{2}q}{\partial u_{2}^{2}}=3\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}+2(u_{2}-u_{3})\frac{\partial^{3}q}{\partial u_{2}^{2}\partial u_{3}}\,. (87)

Using (56) to rewrite (81), we obtain

(λ2λ3)[t+qu3]+2[λ3(u1+u2+u3+2ν)]2qu2u3(u2u3)=0(\lambda_{2}-\lambda_{3})[t+\frac{\partial q}{\partial u_{3}}]+2[\lambda_{3}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}(u_{2}-u_{3})=0 (88)

which together with (87) gives

3λ2λ3u2u3(t+qu3)+2[λ2(u1+u2+u3+2ν)]2qu22\displaystyle 3\frac{\lambda_{2}-\lambda_{3}}{u_{2}-u_{3}}(t+\frac{\partial q}{\partial u_{3}})+2[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}^{2}}
=4[λ2(u1+u2+u3+2ν)](u2u3)3qu22u3>0,\displaystyle=4[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)](u_{2}-u_{3})\frac{\partial^{3}q}{\partial u_{2}^{2}\partial u_{3}}>0\ , (89)

where we have used (25) and Lemma 14 in the last inequality.

It follows from (59) that

(λ2t+w2)u2\displaystyle\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}} =\displaystyle= λ2u2(t+qu2)+[λ2(u1+u2+u3+2ν)]2qu22\displaystyle\frac{\partial\lambda_{2}}{\partial u_{2}}(t+\frac{\partial q}{\partial u_{2}})+[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}^{2}}
>\displaystyle> 32λ2λ3u2u3(t+qu2)+[λ2(u1+u2+u3+2ν)]2qu22\displaystyle\frac{3}{2}\frac{\lambda_{2}-\lambda_{3}}{u_{2}-u_{3}}(t+\frac{\partial q}{\partial u_{2}})+[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}^{2}}
=\displaystyle= 32λ2λ3u2u3(t+qu3)+[λ2(u1+u2+u3+2ν)]2qu22\displaystyle\frac{3}{2}\frac{\lambda_{2}-\lambda_{3}}{u_{2}-u_{3}}(t+\frac{\partial q}{\partial u_{3}})+[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}^{2}}
+3(λ2λ3)2qu2u3\displaystyle\phantom{\frac{3}{2}}+3(\lambda_{2}-\lambda_{3})\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}
>\displaystyle> 3(λ2λ3)2qu2u30,\displaystyle 3(\lambda_{2}-\lambda_{3})\frac{\partial^{2}q}{\partial u_{2}\partial u_{3}}\geq 0\ ,

where we have used Lemma 4, (86) in the first inequality, and (89) in the second one. The last inequality is due to the fact that λ2λ3\lambda_{2}-\lambda_{3} and u2u32q\partial^{2}_{u_{2}u_{3}}q have the same sign because of (88).

This proves the second inequality of (79). In the same way, we can prove the last one. ∎

We are ready to conclude the proof of Theorem 13.

Proof of Theorem 13: By Lemma 18, equations (68) can be solved for

{u1=M(u2)u3=N(u2)\left\{\begin{array}[]{ll}u_{1}=M(u_{2})\\ u_{3}=N(u_{2})\end{array}\right.

in the neighborhood of (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)). Furthermore, (78) holds if u2u_{2} >> u2(t)u_{2}^{-}(t). We shall extend the solution in the positive u2u_{2} direction as far as possible. It follows from Corollary 2 and Lemma 19 that, along the extension of (77) in the region u1+ν>u2+ν>u3+ν>0u_{1}+\nu>u_{2}+\nu>u_{3}+\nu>0, the Jacobian matrix of (64) and (65) is diagonal and therefore is nonsingular. Furthermore, equations (64) and (65) determines (77) as two decreasing functions of u2u_{2}.

This immediately guarantees that (77) can be extended as far as necessary in the region u1+ν>u2+ν>u3+ν>0u_{1}+\nu>u_{2}+\nu>u_{3}+\nu>0. Since M(u2)M(u_{2}) is decreasing, (77) stops at some point u2+(t)u_{2}^{+}(t) where, obviously, M(u2+(t))M(u_{2}^{+}(t)) = u2+(t)u_{2}^{+}(t). Therefore, we have shown that (64) and (65) determine u1u_{1} and u3u_{3} as decreasing functions of u2u_{2} over the interval [u2(t),u2+(t)][u_{2}^{-}(t),u_{2}^{+}(t)].

Let

{u1+(t)=M(u2+(t))u3+(t)=N(u2+(t)).\left\{\begin{matrix}u_{1}^{+}(t)=M(u_{2}^{+}(t))\\ u_{3}^{+}(t)=N(u_{2}^{+}(t))\,.\end{matrix}\right.\,

Clearly, (u1+(t),u2+(t),u3+(t))(u_{1}^{+}(t),u_{2}^{+}(t),u_{3}^{+}(t)) solves system (68) at the leading edge u1=u2u_{1}=u_{2}. Hence, these u1+(t)u_{1}^{+}(t), u2+(t)u_{2}^{+}(t) and u3+(t)u_{3}^{+}(t) are exactly the ones appearing in Lemma 17.

Substituting (77) into (48), we obtain

x=λ2(M(u2),u2,N(u2))t+w2(M(u2),u2,N(u2))x=\lambda_{2}(M(u_{2}),u_{2},N(u_{2}))t+w_{2}(M(u_{2}),u_{2},N(u_{2}))

which by Corollary 2 and Lemma 19 clearly determines xx as an increasing function of u2u_{2} over interval [u2(t),u2+(t)][u_{2}^{-}(t),u_{2}^{+}(t)]. It follows that, for each fixed t>0t>0, u2u_{2} is a function of xx over the interval [x(t)x^{-}(t), x+(t)x^{+}(t)], and that therefore so are u1u_{1} and u3u_{3}, where

x±(t)=λ2(u1±(t),u2±(t),u3±(t))t+w2(u1±(t),u2±(t),u2±(t)).\displaystyle x^{\pm}(t)=\lambda_{2}(u_{1}^{\pm}(t),u_{2}^{\pm}(t),u_{3}^{\pm}(t))t+w_{2}(u_{1}^{\pm}(t),u_{2}^{\pm}(t),u_{2}^{\pm}(t))\,. (90)

Thus, (48) can be solved for

u1=u1(x,t),u2=u2(x,t),u3=u3(x,t)\displaystyle u_{1}=u_{1}(x,t)\ ,\quad u_{2}=u_{2}(x,t)\ ,\quad u_{3}=u_{3}(x,t)

within a wedge

x(t)<x<x+(t)fort>0,x(0)=x+(0)=0,\begin{array}[]{ll}x^{-}(t)<x<x^{+}(t)\hskip 36.135ptfor~t>0\ ,\\ x^{-}(0)=x^{+}(0)=0\ ,\end{array} (91)

where we have used (90), Lemma 15, and Lemma 17 in the last equations.

Boundary conditions (11) and (14) can be checked easily. The proof of Theorem 13 would be completed if we can verify that the wedge is indeed a cusp. First we need a lemma.

Lemma 20

At (u1(t)(u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t))u_{3}^{-}(t)),

(λ2t+w2)u2=(λ3t+w3)u3=0,\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}}=\frac{\partial(\lambda_{3}t+w_{3})}{\partial u_{3}}=0\,, (92)

while at (u1+(t)(u_{1}^{+}(t), u2+(t)u_{2}^{+}(t), u3+(t))u_{3}^{+}(t)),

(λ1t+w1)u1=(λ2t+w2)u2=0.\frac{\partial(\lambda_{1}t+w_{1})}{\partial u_{1}}=\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}}=0\,. (93)

Proof.

Using expansions (101) and (102), we obtain from (29) that

λ2u2=6[(u3+ν)14(u1+ν)]u1+ν\frac{\partial\lambda_{2}}{\partial u_{2}}={6[(u_{3}+\nu)-{1\over 4}(u_{1}+\nu)]\over u_{1}+\nu}

at (u1(t)u_{1}^{-}(t), u2(t)u_{2}^{-}(t), u3(t)u_{3}^{-}(t)).

By (59), we have

(λ2t+w2)u2\displaystyle\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}} =\displaystyle= 6[(u3+ν)14(u1+ν)](u1+ν)(t+qu2)\displaystyle{6[(u_{3}+\nu)-{1\over 4}(u_{1}+\nu)]\over(u_{1}+\nu)}(t+\frac{\partial q}{\partial u_{2}})
4(u1u3)(u3+ν)u1+ν2qu22=0,\displaystyle\ -{4(u_{1}-u_{3})(u_{3}+\nu)\over u_{1}+\nu}\ \frac{\partial^{2}q}{\partial u_{2}^{2}}=0\ ,

where we have used (26) in the first equality, and (72) and (87) in the last equality. The proof also applies to the other equation of (92).

To prove (93), we proceed as follows. By (22), (103), and (104), we find

λ2u1=O(K(s))as s1 .\frac{\partial\lambda_{2}}{\partial u_{1}}=O(K(s))\quad\mbox{as $s\rightarrow 1$ \ .} (94)

By Corollary 2 and formula (59), we calculate the derivative on the solution of (64) and (65)

0\displaystyle 0 =\displaystyle= (λ2t+w2)u1\displaystyle\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{1}}
=\displaystyle= λ2u1(t+qu2)+12[λ2(u1+u2+u3+2ν)]2qu1u2+qu1qu2,\displaystyle\frac{\partial\lambda_{2}}{\partial u_{1}}(t+\frac{\partial q}{\partial u_{2}})+\frac{1}{2}[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{1}\partial u_{2}}+\frac{\partial q}{\partial u_{1}}-\frac{\partial q}{\partial u_{2}}\,,

which when combined with (27) and (94) gives

lims1[t+qu2]K(s)=0.\lim_{s\rightarrow 1}[t+\frac{\partial q}{\partial u_{2}}]\ K(s)=0\,. (95)

On the other hand, as in (94), we have

λ2u2=O(K(s))as s1 .\frac{\partial\lambda_{2}}{\partial u_{2}}=O(K(s))\quad\mbox{as $s\rightarrow 1$ \ .} (96)

Therefore, by (59) we see that at (u1+(u_{1}^{+}, u2+u_{2}^{+}, u3+)u_{3}^{+})

(λ2t+w2)u2=λ2u2(t+12qu2)+[λ2(u1+u2+u3+2ν)]2qu22=0,\displaystyle\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}}=\frac{\partial\lambda_{2}}{\partial u_{2}}(t+\frac{1}{2}\frac{\partial q}{\partial u_{2}})+[\lambda_{2}-(u_{1}+u_{2}+u_{3}+2\nu)]\frac{\partial^{2}q}{\partial u_{2}^{2}}=0\ ,

where, by (95) and (96), the first term vanishes, while the second term vanishes because of (27). This proves the second equality of (93). In the same way, we can check the other equality of (93). ∎

Now we continue to finish the proof of Theorem 13. Differentiating (90) with respect to tt, by Corollary 2 and Lemma 20 we obtain

dx+¯(t)dt\displaystyle\frac{dx^{\underline{+}}(t)}{dt} =\displaystyle= (λ2t+w2)u2du2±dt+λ2(u1±,u2±,u3±)\displaystyle\frac{\partial(\lambda_{2}t+w_{2})}{\partial u_{2}}\frac{du_{2}^{\pm}}{dt}+\lambda_{2}(u_{1}^{\pm},u_{2}^{\pm},u_{3}^{\pm})
=\displaystyle= λ2(u1±,u2±,u3±),\displaystyle\lambda_{2}(u_{1}^{\pm},u_{2}^{\pm},u_{3}^{\pm})\,,

which when combined with (26), (27), Lemma 15, and Lemma 17 gives

dx±(t)dt=3u^+2νat t=0.\frac{dx^{\pm}(t)}{dt}=3\hat{u}+2\nu\quad\mbox{at $t=0$}\ .

Therefore, wedge (91) is a cusp. This completes the proof of Theorem 13.

We immediately conclude from Theorem 1 and Theorem 13 the following result on the initial value problem of the Whitham equations.

Theorem 21

For a decreasing initial function u0(x)u_{0}(x) whose inverse function f(u)f(u) satisfying the conditions of Theorem 13, the Whitham equations (3) have a solution (u1(x,t),u2(x,t),u3(x,t))(u_{1}(x,t),u_{2}(x,t),u_{3}(x,t)) within a cusp for all positive time. The Burgers solution of (2) exists outside the cusp. The Whitham solution matches the Burgers solution on the boundary of the cusp in the fashion of (11) and (14).

We close this paper with two observations. First, it is obvious from the proof of Theorem 21 that one should expect local (in time) results if local conditions are assumed. Namely, if the global condition f′′′(u)<0f^{\prime\prime\prime}(u)<0 for all b<u<ab<u<a in Theorem 21 is replaced by a local condition f′′′(u)<0f^{\prime\prime\prime}(u)<0 in the neighborhood of the breaking point u^\hat{u}, the results of Theorem 21 are only true for a short time after the breaking time.

Second, a hump-like initial function can be decomposed into a decreasing and an increasing parts. It is known that the decreasing part causes the Burgers solution of (2) to develop finite time singularities while the increasing part does not. These two pieces of data would not interact with each other for a short time after the breaking of the Burgers solution. As a consequence, a short time result also holds for a hump-like initial function.

Appendix A Complete Elliptic Integrals

In this Appendix, we list some of the well-known properties of the complete elliptic integrals of the first, second and third kind.

These are the derivative formulae

dK(s)ds\displaystyle\frac{dK(s)}{ds} =\displaystyle= E(s)(1s)K(s)2s(1s),\displaystyle\frac{E(s)-(1-s)K(s)}{2s(1-s)}\ , (97)
dE(s)ds\displaystyle\frac{dE(s)}{ds} =\displaystyle= E(s)K(s)2s,\displaystyle\frac{E(s)-K(s)}{2s}\ , (98)
dΠ(ρ,s)dρ\displaystyle\frac{d\Pi(\rho,s)}{d\rho} =\displaystyle= ρE(s)+(sρ)K(s)+(ρ2s)Π(ρ,s)2ρ(1ρ)(ρs),\displaystyle\frac{\rho E(s)+(s-\rho)K(s)+(\rho^{2}-s)\Pi(\rho,s)}{2\rho(1-\rho)(\rho-s)}\ , (99)
dΠ(ρ,s)ds\displaystyle\frac{d\Pi(\rho,s)}{ds} =\displaystyle= E(s)(1s)Π(ρ,s)2(1s)(sρ).\displaystyle\frac{E(s)-(1-s)\Pi(\rho,s)}{2(1-s)(s-\rho)}\ . (100)

K(s)K(s) and E(s)E(s) have the expansions

K(s)\displaystyle K(s) =\displaystyle= π2[1+s4+964s2++(13(2n1)242n)2sn+],\displaystyle\frac{\pi}{2}[1+\frac{s}{4}+\frac{9}{64}s^{2}+\cdots+(\frac{1\cdot 3\cdots(2n-1)}{2\cdot 4\cdots 2n})^{2}s^{n}+\cdots]\ , (101)
E(s)\displaystyle E(s) =\displaystyle= π2[1s4364s212n1(13(2n1)242n)2sn]\displaystyle\frac{\pi}{2}[1-\frac{s}{4}-\frac{3}{64}s^{2}-\cdots-\frac{1}{2n-1}(\frac{1\cdot 3\cdots(2n-1)}{2\cdot 4\cdots 2n})^{2}s^{n}-\cdots] (102)

for |s|<1|s|<1. They also have the asymptotics

K(s)\displaystyle K(s) \displaystyle\approx 12log161s,\displaystyle\frac{1}{2}\log\frac{16}{1-s}\ , (103)
E(s)\displaystyle E(s) \displaystyle\approx 1+14(1s)[log161s1]\displaystyle 1+\frac{1}{4}(1-s)[\log\frac{16}{1-s}-1] (104)

when ss is close to 11. They satisfy the inequalities [14]

11s2<K(s)E(s)<1s21sfor0<s<1.\frac{1}{1-\frac{s}{2}}<\frac{K(s)}{E(s)}<\frac{1-\frac{s}{2}}{1-s}\hskip 36.135ptfor~0<s<1\ . (105)

The complete elliptic integral of the third kind has the following behavior

Π(ρ,s)\displaystyle\Pi(\rho,s) =\displaystyle= π2when ρ=0s=0,\displaystyle{\pi\over 2}\quad\mbox{when $\rho=0$, $s=0$}\ , (106)
Π(ρ,s)K(s)\displaystyle{\Pi(\rho,s)\over K(s)} \displaystyle\approx 11ρwhen s is close to 1.\displaystyle{1\over 1-\rho}\quad\mbox{when $s$ is close to $1$}\ . (107)

Acknowledgments. T.G. was supported in part by the MISGAM program of the European Science Foundation, and by the RTN ENIGMA and Italian COFIN 2006 “Geometric methods in the theory of nonlinear waves and their applications.” V.P. was supported in part by NSF Grant DMS-0135308. F.-R. T. was supported in part by NSF Grant DMS-0404931.

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