The compressible Euler equations in a physical vacuum: a comprehensive Eulerian approach
Abstract.
This article is concerned with the local well-posedness problem for the compressible Euler equations in gas dynamics. For this system we consider the free boundary problem which corresponds to a physical vacuum.
Despite the clear physical interest in this system, the prior work on this problem is limited to Lagrangian coordinates, in high regularity spaces. Instead, the objective of the present work is to provide a new, fully Eulerian approach to this problem, which provides a complete, Hadamard style well-posedness theory for this problem in low regularity Sobolev spaces. In particular we give new proofs for both existence, uniqueness, and continuous dependence on the data with sharp, scale invariant energy estimates, and continuation criterion.
Key words and phrases:
compressible Euler equations, Moving boundary problems, vacuum boundary.1991 Mathematics Subject Classification:
Primary: 35Q75; Secondary: 35L10, 35Q35.1. Introduction
In this article we study the dynamics of the free boundary problem for a compressible gas. In the simplest form, the gas is contained in a moving domain with boundary , and is described via its density and velocity . The evolution of the Eulerian variables is given by the compressible Euler equations
(1.1) |
with the constitutive law
In the present paper we will consider constitutive laws of the form111Here, for expository reasons, we use rather than as the exponent, as it is more common in the literature.
(1.2) |
Heuristically one can view this system as a coupled system consisting of a wave equation for the pair and a transport equation for . In this interpretation, a key physical quantity is the propagation speed for the wave component. This is called the speed of sound, and is given by
(1.3) |
We consider this system in the presence of vacuum states, i.e. the density is allowed to vanish. The gas is located in the domain , whose boundary is moving. The defining characteristic in the case of a gas, versus the fluid case, is that the density vanishes on the free boundary , which is thus described by
In this context, the decay rate of the sound speed near the free boundary plays a fundamental role both in the gas dynamics and in the analysis. In essence, one expects that there is a single stable, nontrivial physical regime, which is called physical vacuum, and corresponds to the sound speed decay rate
(1.4) |
The property (1.4) will propagate in time for as long as , which will be the case for all solutions considered in this article. We remark that in particular such a bound guarantees a bilipschitz fluid flow.
To provide some intuition for this we note that the acceleration of particles on the free boundary is exactly given by , which is normal to the boundary. Heuristically, because of this, the property (1.4) yields the correct balance which allows the free boundary to move with a bounded velocity and acceleration while interacting with the interior, as follows:
-
•
A faster fallout rate for the sound speed would cause the boundary particles to simply move independently and linearly with the outer particle speed. This can only last for a short time, until the faster waves inside overtake the boundary and likely lead to a more stable regime where (1.4) holds. See for instance the results in this direction in [25], but also the dispersive scenario discussed in [11].
-
•
A slower fallout rate would cause an infinite initial acceleration of the boundary, likely leading again to the same pattern.
A fundamental observation concerning physical vacuum is that the relation (1.4) guarantees that linear waves with speed can reach the free boundary in finite time. Because of this, in the above flow the motion of the boundary is strongly coupled to the wave evolution and is not just a self-contained evolution at leading order.
There are two classical approaches in fluid dynamics, using either Eulerian coordinates, where the reference frame is fixed and the fluid particles are moving, or using Lagrangian coordinates, where the particles are stationary but the frame is moving. Both of these approaches have been extensively developed in the context of the compressible Euler equations, where the local well-posedness problem is very well understood.
By contrast, the free boundary problem corresponding to the physical vacuum has been far less studied and understood. Because of the difficulties related to the need to track the evolution of the free boundary, all the prior work is in the Lagrangian setting and in high regularity spaces which are only indirectly defined.
Our goal in this paper is to provide a new, complete, low regularity approach for this free boundary problem which is fully within the Eulerian framework. In particular, our work contains the following steps, each of which represents original, essential advances in the study of this problem:
-
a)
We prove the uniqueness of solutions with very limited regularity222In an appropriately weighted sense in the case of , see Theorem 1. , . More generally, at the same regularity level we prove stability, by showing that bounds for a certain distance between different solutions can be propagated in time.
-
b)
We develop the Eulerian Sobolev function space structure where this problem should be considered, providing the correct, natural scale of spaces for this evolution.
-
c)
We prove sharp, scale invariant energy estimates within the above mentioned scale of spaces, which show that the appropriate Sobolev regularity of solutions can be continued for as long as we have uniform bounds at the same scale .
-
d)
We give a simpler, more elegant proof of existence for regular solutions, fully within the Eulerian setting, based on the above energy estimates.
-
e)
We devise a nonlinear Littlewood-Paley type method to obtain rough solutions as unique limits of smooth solutions, also proving the continuous dependence of the solutions on the initial data.
At a conceptual level, we also remark that in our approach the study of the linearized problem plays the main role, whereas the energy bounds for the full system are seen as secondary, derived estimates. This is unlike in prior works, where the linearized equation is relegated to a secondary role if it appears at all.
1.1. The material derivative and the Hamiltonian
The derivative along the particle trajectories is called the material derivative and is defined as
With this notation the system (1.1) is rewritten as
(1.5) |
Differentiating once more in the first equation we obtain
which at leading order is a wave equation for with propagation speed , and where can be viewed as a dependent variable.
On the other hand, for the vorticity one can use the second equation to obtain the transport equation
The last two equations show that indeed one can interpret the Euler equations as a coupled system consisting of a wave equation for the pair and a transport equation for .
1.2. The good variables
The pair of variables is convenient to use if . However, for other values of in (1.2) we can make a better choice. To understand that, we compute the sound speed
This should have linear behavior near the boundary. Because of this, it is more convenient to use defined by
which gives
as a good variable instead of .
Written in terms of the equations become
(1.6) |
In our case we have so we rewrite the above system as
(1.7) |
or, using material derivatives,
(1.8) |
We will work with this system for the rest of the paper.
1.3. Energies and function spaces
Given the constitutive law (1.2), the conserved energy is
(1.9) |
Switching to the variables and adjusting constants, we obtain
(1.10) |
This will not be directly useful in solving the equation, but will give us a good idea for the higher order function spaces we will have to employ. Based on this, we introduce the energy space with norm
(1.11) |
for functions defined a.e. within the fluid domain . Importantly, we note that the constants above do not match (1.10), and instead have been adjusted to match the energy functional for the linearized equation, which is discussed in Section 3. The two components of the space as weighted spaces,
For higher regularity, we take our cue from the second order wave equation, which has the leading operator , which is naturally associated to the acoustic metric333Technically one should add a factor here.
(1.12) |
Correspondingly, we define the higher order Sobolev spaces for distributions within the fluid domain to have norms
where is implicitly restricted to . More generally, for all real one can define by interpolation the spaces . These spaces and their properties are further discussed in the next section.
1.4. Scaling and control parameters
The equation (1.7) admits the scaling law
(1.13) |
We use this scaling in order to track the order of factors in multilinear expressions, introducing a counting device based on scaling:
-
i)
and have degree , respectively .
-
ii)
has order and has order .
The order of a multilinear expression is defined as the sum of the orders of each factors. In this way, all terms in each of the equations have the same order. This property remains valid if we either differentiate the equations in , or apply the material derivative .
Corresponding to the above spaces and scaling we identify the critical space where is given by444In general this will not be an integer.
This has the property that its (homogeneous) norm is invariant with respect to the above scaling.
Associated to this Sobolev exponent we introduce the following scale invariant time dependent pointwise control norm
(1.14) |
where is a given nonzero vector. Here can be chosen as for some fixed point where . The motivation for using such an , rather than just , is that the latter is a scale invariant quantity of fixed, unit size. On the other hand the defined above can be harmlessly assumed to be small simply by working in a small neighbourhood of the reference point . Such a localization is allowed in the study of compressible Euler system because of the finite speed of propagation. The control parameter will play a leading role in elliptic estimates at fixed time, and, in order to avoid cumbersome notations, will be implicitly assumed to be small in all of our analysis.
For the energy estimates we will also introduce a second time dependent control norm which is associated with the space , namely
(1.15) |
where the norm is given by
This scales like he norm, but it is weaker in that it only uses one derivative of away from the free boundary.
The role of will be to control the growth rate for our energies, while also allowing for a secondary dependence of the implicit constants on .
1.5. The main results
Our main result is a well-posedness result for the compressible Euler evolution (1.7). However, it is more revealing to break the result down into several components. We begin with the uniqueness result, which requires least regularity.
Theorem 1 (Uniqueness).
For every Lipschitz initial data satisfying the nondegeneracy condition on , the system (1.7) admits at most one solution in the class
(1.16) |
In other words, uniqueness holds in the class of solutions for which remains finite. One can further relax this to . We note that only the spatial regularity is specified in the theorem, as the time regularity can then be obtained from the equations. Also the nondegeneracy condition is only given at the initial time, but it can be easily propagated to later times given our regularity assumptions.
To the best of our knowledge, this is the first uniqueness proof for this problem which applies directly in the Eulerian setting, and also the first uniqueness result at low, scale invariant555Scale invariance corresponds to the assumption . regularity.
Remark 1.1.
Next we consider the well-posedness question. Here we define the phase space
(1.17) |
One should think of this in a nonlinear fashion, as an infinite dimensional manifold, as the norms depend on and thus on . The topology on this manifold is discussed in the next section. Now we can state our main well-posedness result:
Theorem 2 (Well-posedness).
The system (1.1) is locally well-posed in the space for with
(1.18) |
The well-posedness result should be interpreted in a quasilinear fashion, i.e. including:
The last question we consider is that of continuation of the solutions, which is where our control norms are critically used. This is closely related to the energy estimates for our system:
Theorem 3.
For each integer there exists an energy functional with the following properties:
a) Coercivity: as long as666Recall that we can harmlessly assume small. , we have
(1.19) |
b) Energy estimates for solutions to (1.1)
(1.20) |
By Gronwall’s inequality this implies the bound
(1.21) |
Remark 1.2.
These energies are constructed in an explicit fashion only for integer . Nevertheless, as a consequence in our analysis in the last section of the paper, it follows that bounds of the form (1.21) hold also for all noninteger . However, we do this using a mechanism which is akin to a paradifferential expansion, without constructing an explicit energy functional as provided by the above theorem in the integer case.
A consequence of the last result is the following continuation criteria for solutions to (1.1), which holds regardless of whether is an integer:
Theorem 4.
Here we implicitly make a topological assumption and exclude the possibility that two gas bubbles at some point touch each other, or that the free boundary self-intersects. This latter possibility is prohibited at small scales by our result, but certainly not at large scales.
This result is consistent with the standard continuation results for quasilinear hyperbolic systems in the absence of a free the boundary. But for the physical vacuum free boundary problem, this work is the first where anything close to such a continuation result has been proved.
1.6. Historical comments
The study of the compressible Euler evolutions has a long history, and also considerable interest from the physical side. Allowing for vacuum states introduces many added layers of difficulty to the problem, whose nature greatly depends on the behavior of the sound speed near the vacuum boundary. Within this realm, physical vacuum represents the natural boundary condition for compressible gasses. Below we begin with a brief discussion of the broader context, and then we focus on the problem at hand.
1.6.1. Compressible Euler flows
The compressible Euler equations are classically considered as a symmetric hyperbolic system, and as such, local well-posedness has long been known, see e.g. [15], and also the Euler oriented analysis in [21]. The local solutions can be obtained using the energy method, and relying solely on the energy requires initial data local regularity with , with the continuation criteria
By now it is known that these results can be improved by taking advantage of Strichartz estimates for wave equations. In the irrotational case, for instance, the result of [26] applies directly and yields the sharp local well-posedness result, for777Here . . In the rotational case, it is not yet clear what would be the optimal condition on the vorticity which would allow for a similar improvement; see the results in [9] and [29].
1.6.2. Vacuum states in compressible Euler flows
Vacuum states correspond to allowing for the density to vanish in some regions. Here one should think of having a particle region , and a vacuum region, separated by a moving free boundary . There are two major physical scenarios, distinguished by the boundary behaviour of the density , or equivalently of the sound speed :
-
(1)
Fluid flows, where the pressure is constant on the free boundary, describing a balance of forces, and the density and implicitly the sound speed are assumed to have a nonzero, positive limit there.
-
(2)
Gas flows, where the density decay to zero near the free boundary; this is our main focus in this paper.
Both are free boundary problems associated to compressible Euler, but their nature is very different in the two cases. Fluid flows were considered in [4] and [17], and also the incompressible limit was investigated in [18].
Now we turn our attention to our present interest, namely the gas flows. Heuristically one distinguishes several potential scenarios when comparing the sound speed with the distance to the vacuum boundary.
a) Rapid decay corresponds to
In this case the vacuum boundary evolves linearly, and internal waves cannot reach the boundary arbitrarily fast. Thus this geometry persists at least for a short time, and the local well-posedness problem can be even studied using the standard tools of symmetric hyperbolic systems; see for instance [8], [2] and [19], as well as the alternative approach in [22],[1] and the one dimensional analysis in [20]. Thus this case cannot be thought of as a true free boundary problem. Furthermore, after a finite time, the internal waves will reach the boundary [20], and this geometry breaks down.
b) Slow decay,
This is where the problem indeed becomes a genuine free boundary problem, as internal waves can reach the boundary arbitrarily fast, and then the flow of the free boundary becomes strongly coupled with the internal flow. One might think that there might be a range of possible decay rates, for instance like
However, both physical and mathematical considerations seem to indicate that among these there is a single stable decay rate, which corresponds to . This is commonly referred to as physical vacuum. The other values of are expected to be unstable, with the solutions instantly falling into the stable regime; but this is all a conjecture at this point, and likely there will be significant differences between the cases and .
1.6.3. The physical vacuum scenario
We turn now our attention to the problem at hand, i.e. the physical vacuum scenario. The easier one dimensional setting was considered first, in [6] followed by [13]. While some energy estimates are formally obtained in [6] and a procedure to construct solutions is provided, the functional structure there does not provide a direct description of the initial data space. This issue is remedied in [13], which first introduces the Lagrangian counterparts of the scale of spaces we are also using here, and provides both existence and uniqueness results in sufficiently regular spaces.
More recently, the three dimensional case was considered in several papers. Energy estimates for were formally derived in [5]. This was followed by an existence proof proposed in [7], which is based a parabolic regularization. However, the functional setting is similar to their prior one dimensional paper, and some steps are merely claimed rather than proved; for instance the difference bound, which also, as stated, requires additional regularity for the solutions compared to the existence result. Independently, [14] offers an alternative existence and uniqueness proof for arbitrary , this time within the correct scale of weighted Sobolev spaces, using an iterative argument for the existence part, and with a different approach to the energy estimates.
All the results described above are in the Lagrangian setting, and aim to give existence and uniqueness results in sufficiently regular function spaces. In addition to the limitations mentioned above, no attempt is made to provide any continuous dependence results, nor to transfer the results to the physical, Eulerian framework.
By contrast, our results in the present paper are fully developed within the Eulerian setting, at low regularity, in all dimensions and for all . In this context we provide completely new arguments for existence, uniqueness, and continuous dependence of the solutions on the initial data, i.e. a full well-posedness theory in the Hadamard sense. In addition we prove a family of sharp, scale invariant energy estimates, which in particular yield optimal continuation criteria at the level of , consistent with the well-known results for hyperbolic systems in the absence of the free boundary. Despite the fact that we only construct energy functionals corresponding only to integer Sobolev spaces, we nevertheless are able to use these estimates in order to obtain energy estimates in fractional Sobolev spaces as well, nicely completing the theory up to the optimal Sobolev thresholds.
1.7. An outline of the paper
The article has a modular structure, where, for the essential part, only the main results of each section are used later.
1.7.1. Function spaces and interpolation
The starting point of our analysis, in the next section, is to describe the appropriate functional setting for our analysis, represented by the scale of weighted Sobolev spaces. These are associated to the singular Riemannian metric (1.12) under the sole assumption that the boundary is Lipschitz, with as a nondegenerate defining function. A similar scale of spaces was introduced in [14] in the Lagrangian setting, though under more regularity assumptions. However, since in the Eulerian setting the boundary is moving, the corresponding state space for is seen here akin to an infinite dimensional manifold.
We remark on the dual role of , as a defining function of the boundary implicitly as a weight on one hand, and as one of the dynamical variables on the other hand; for our low regularity analysis we carefully decouple these two roles, in order to avoid cumbersome boootstrap loops.
Interpolation plays a significant role in our study. First this occurs at the level of the scale of spaces, and it allows us to work with fractional Sobolev spaces without having to directly prove energy estimates in the fractional setting, using expansions which are akin to paradifferential ones but done at the level of the nonlinear flow. Secondly, we also interpolate between the spaces and the pointwise bounds captured by our control parameters and . It is this last tool which allows us to work at low regularity and to obtain sharp, scale invariant energy estimates.
1.7.2. The linearized equation and transition operators
In Section 3 we consider the linearized equation, which is modeled as a linear evolution in the time dependent weighted space . We view this as the main tool in the analysis of the nonlinear evolution, rather than the direct nonlinear energy estimates as in all prior work (except for [14], to some extent). This later helps us not only to prove nonlinear energy estimates for single solutions, but also to compare different solutions, which is critical both for our uniqueness proof and for our construction of rough solutions as strong limits of smooth solutions. We remark that at the level of the linearized variables there is no longer any boundary condition on the moving free boundary ; this is closely related to the prior comment about uncoupling the roles of .
Next, using the linearized equation, we obtain the transition operators and , which act at the level of the two linearized variables , respectively , and should be though of as the degenerate elliptic leading spatial part of the wave evolution for , respectively . We call them transition operators because they tie the successive spaces and on our scale in a coercive, invertible fashion. These operators play a leading role in both the higher order energy estimates and in the regularization used for our construction of regular solutions.
1.7.3. Difference estimates and the uniqueness result
The aim of Section 4 is to construct a nonlinear difference functional which allows us to track the distance between two solutions roughly at the level of the norm. This is akin to the difference bounds in a weaker topology which are common in the study of quasilinear problems.
This is one of the centerpieces of our analysis, and to the best of our knowledge this is the first time such a construction was successfully carried out in a free boundary setting. The fundamental difficulty is that we are seeking to not only compare functions on different domains, but also to track the evolution in time of this distance. This difficulty is translated into the nonlinear character of our difference functional; some delicate, careful choices are made there, which ultimately allow us to propagate this distance forward in time.
1.7.4. Higher order energy estimates
The aim of Section 5 is to establish energy estimates in integer index Sobolev spaces on our scale. We define the nonlinear energy functionals using suitable vector fields applied to the equation. This energy has two components, a wave component and a transport component, which correspond to the heuristic (partial) decoupling of the evolution into a wave part for and and a transport part for the vorticity . Our proof of the energy estimates is split in a modular fashion into two parts, where we succesively (i) prove the coercivity of our energy functional and (ii) track the time evolution of the energy.
The coercivity bound is obtained inductively in , using the transition operators and as key tools. The main part of the proof of the propagation bound happens at the level of the wave component, where we identify Alihnac style “good variables” , which are shown to solve the linearized equation modulo perturbative source terms.
Our energy functionals are to some extent the Eulerian counterparts of energies previously constructed in [7], [14] in the Lagrangian setting and at higher regularity. They are closer in style to [7], though the coercivity part is largely missing there and as a consequence some of the functional setting is incomplete/incorrect. The analysis in [14], on the other hand, corresponds to combining the two steps above together. This leads to a more comprehensive energy functional, where the coercivity part is relatively straightforward, but instead moves the difficulty to the propagation part, which becomes considerably more complex.
1.7.5. Existence of regular solutions
The aim of Section 6 is to prove the existence theorem in the context of regular solutions. The scheme we propose here is constructive, using a time discretization via an Euler type method to produce good approximate solutions. However a naive implementation of Euler’s method looses derivatives; to rectify this we precede the Euler step by (i) a regularization on a suitable scale, and (ii) a separate transport part888This bit is optional but does simplify the analysis.. The challenge is to control the energy growth at each step of the way. This is more delicate for the regularization, which has has to be done carefully using the elliptic transition operators and .
We note that our construction is very different from any other approaches previously used in analyzing this problem; they all relied on parabolic regularizations. Our construction is simpler and more direct, though not without interesting subtleties. It is also better tailored to the physical structure of the equations, which makes this approach more robust and also successful in the relativistic counterpart of our problem.
1.7.6. Rough solutions as limits of regular solutions
The last section of the paper aims to construct rough solutions as strong limits of smooth solutions. This is achieved by considering a family of dyadic regularizations of the initial data, which generates corresponding smooth solutions. For these smooth solutions we control on one hand higher Sobolev norms , using our energy estimates, and on the other hand the type distance between consecutive ones, which is at the level of the norms. Combining the high and the low regularity bounds directly yields rapid convergence in all spaces below the desired threshold, i.e. for . To gain strong convergence in we use frequency envelopes to more accurately control both the low and the high Sobolev norms above. This allows us to bound differences in the strong topology. A similar argument yields continuous dependence of the solutions in terms of the initial data also in the strong topology, as well as our main continuation result in Theorem 4.
1.8. Acknowledgements
The first author was supported by a Luce Assistant Professorship, by the Sloan Foundation, and by an NSF CAREER grant DMS-1845037. The second author was supported by the NSF grant DMS-1800294 as well as by a Simons Investigator grant from the Simons Foundation.
Both authors thank Marcelo Disconzi for introducing them to this class of problems. In particular, the relativistic counterpart of this problem is considered jointly with him in forthcoming work.
2. Function spaces
The aim of this section is to introduce the main function spaces where we will consider the free boundary problem for the compressible gas. These are Sobolev type spaces of functions inside the gas domain , with weights depending on , or equivalently on the distance to the free boundary. We begin with a more general discussion of weighted Sobolev spaces in Lipschitz domains, and then specialize to the function spaces that are needed in our problem.
2.1. Weighted Sobolev spaces
As a starting point, in a domain with Lipschitz boundary and nondegenerate defining function we introduce a two parameter family of weighted Sobolev spaces (see [27, 28] for a more general take on this):
Definition 2.1.
Let and . Then the space is defined as the space of all distributions in for which the following norm is finite:
(2.1) |
By complex interpolation, one also defines corresponding fractional Sobolev spaces for and . This yields a double family of interpolation spaces.
Some comments are in order here:
-
•
At this point, all we assume about the geometry of the problem is that the boundary is Lipschitz, and that is a non-degenerate defining function for , i.e. proportional to the distance to . Different choices for yield the same space with different but equivalent norms. Without any restriction in generality, we can assume that is Lipschitz continuous.
-
•
The requirement corresponds to the fact that no vanishing assumptions on the boundary are made for any of the elements in our function spaces.
-
•
If then one recovers the classical Sobolev spaces .
-
•
If these are weighted spaces, .
Next, we establish some key properties of these spaces. First, we have the Hardy type embeddings (see the book [16] for a broader view):
Lemma 2.2.
Assume that and with . Then we have
(2.2) |
Proof.
By interpolation and reiteration it suffices to prove the result when , both integers. Thus we will show that
(2.3) |
It suffices to prove the result in dimension ; then all the higher dimensions will follow by considering foliations of with parallel one dimensional lines which are transversal to .
Here is the distance function to the boundary of . Setting , is pointwise equivalent to , and in particular gives
The inclusion follows from the following integration by parts
The boundary term vanishes, and we can now apply Cauchy-Schwartz’s inequality to obtain
∎
As a corollary of the above lemma we have embeddings into standard Sobolev spaces:
Lemma 2.3.
Assume that and . Then we have
(2.4) |
In particular, by standard Sobolev embeddings, we also have Morrey type embeddings into spaces:
Lemma 2.4.
We have
(2.5) |
where the equality can hold only if is not an integer.
2.2. Weighted Sobolev norms for compressible Euler
Our starting point here is the conserved energy for our problem, namely
Even more importantly, in our study of the linearized equation (see Section 3) for linearized variables we use the weighted type energy functional
Based on this, we define our baseline space with norm
In terms of the spaces discussed earlier, or weighted spaces, we have
(2.6) |
Next we define a suitable scale of higher order Sobolev spaces for our problem. To understand the balance between weights and derivatives we consider the leading order operator, if we write the wave part of our system as a second order equation for . At leading order this yields the wave operator
which is naturally associated with the Riemannian metric (1.12) in .
So, to the above type space we need to add Sobolev regularity based on powers of , or equivalently, relative to the metric defined above. Hence we define the higher order Sobolev spaces
of pairs functions defined inside . These form a one parameter family of interpolation spaces. The spaces have the obvious norm if is a nonnegative integer; for instance one can set
(2.7) |
where is also restricted to nonnegative integers.
On the other hand, if is not an integer then the corresponding norms are Hilbertian norms defined by interpolation. Since in the Hilbertian case all interpolation methods yield the same result, for the norm we will use a characterization which is akin to a Littlewood-Paley decomposition, or to a discretization of the method of interpolation. Precisely, we have
Lemma 2.5.
Let . Then can be defined as the space of distributions which admit a representation
(2.8) |
with the property that the following norm is finite:
(2.9) |
and with equivalent norm defined as
(2.10) |
where the infimum is taken with respect to all representations as above.
2.3. The state space .
As already mentioned in the introduction, the state space is defined for (i.e. above scaling) as the set of pairs of functions defined in a domain in with boundary with the following properties:
-
i)
Boundary regularity: is a Lipschitz surface.
-
ii)
Nondegeneracy: is a Lipschitz function in , positive inside and vanishing simply on the boundary .
-
iii)
Regularity: The functions belong to .
Since the domain itself depends on the function , one cannot think of as a linear space, but rather as an infinite dimensional manifold. As time varies in our evolution, so does the domain, so we are interested in allowing the domain to vary in . However, describing a manifold structure for is beyond the purposes of our present paper, particularly since the trajectories associated with our flow are merely expected to be continuous with values in . For this reason, here we will limit ourselves to defining a topology on .
Definition 2.6.
A sequence converges to in if the following conditions are satisfied:
-
i)
Uniform nondegeneracy, .
-
ii)
Domain convergence, .
-
iii)
Norm convergence: For each there exist smooth functions in , respectively in so that
while
We remark that the last condition in particular provides both a uniform bound for the sequence in as well as an equicontinuity type property, which ensures that a nontrivial portion of their norms cannot concentrate on thinner layers near the boundary. This is akin to the the conditions in the Kolmogorov-Riesz theorem for compact sets in spaces.
This definition will enable us to achieve two key properties of our flow:
-
•
Continuity of solutions as functions of with values in .
-
•
Continuous dependence of solutions as functions of the initial data .
2.3.1. Sobolev spaces and control norms
2.3.2. The regularity of the free boundary
Another property to consider for our flow, in dimension , is the regularity of the free boundary, as well as the regularity of the velocity restricted to the free boundary. This is given by trace theorems and the embedding (2.4):
Lemma 2.7.
Suppose that and that is not an even integer. Then has regularity
If in addition is also not an odd integer then the velocity restricted to has class
These properties are provided here only for comparison purposes, and play no role in the sequel. This is because in this problem one cannot view the evolution of the free boundary as a stand alone flow, not even at leading order. In particular, a-priori this velocity does not suffice in order to transport the regularity of ; instead the boundary evolution should be viewed as a part of the interior evolution. Indeed, we will see that there is some interesting cancellation arising from the structure of the equations which facilitates this.
2.4. Regularization and good kernels
An important ingredient in our construction of solutions to our free boundary evolution is to have good regularization operators associated to each dyadic frequency scale , . These operators will need to accomplish two distinct goals:
-
•
Fixed domain regularization. Given , construct regularizations within the same scale of spaces.
-
•
State and domain regularization. Given , where the first component defines a domain , construct regularizations within the scale of spaces, where the regularized domains are defined by , .
We begin with some heuristic considerations and notations. Given a dyadic frequency scale , our regularizations will need to select frequencies with the property that , which would require kernels on the scale
However, if we are too close to the boundary, i.e. , then we run into trouble with the uncertainty principle, as we would have . Because of this, we select the spatial scale and the associated frequency scale as cutoffs in this analysis.
To describe this process, it is convenient to decompose a neighbourhood of the boundary into boundary layers. We denote the dyadic boundary layer associated to the frequency by
(2.13) |
the corresponding full boundary strip by
(2.14) |
and the corresponding interior region by
(2.15) |
We will also use dyadic enlargements of , denoted by
(2.16) |
with a small universal constant , and
(2.17) |
Given a domain with a nondegenerate Lipschitz defining function , and functions in , we will define regularizations associated to the dyadic scale using smooth kernels ,
The heuristic discussion above leads to the following notion of good kernels:
Definition 2.8.
The family of kernels are called good regularization kernels if the following properties are satisfied:
-
i)
Domain and localization:
(2.18) with support properties
(2.19) -
ii)
Size and regularity
(2.20) where is large enough.
-
iii)
Approximate identity,
(2.21) (2.22)
Notably, the first property will allow us to define the regularizations in the extended domain , with dyadic mapping properties as follows:
-
•
For , the regularizations in are determined by also in .
-
•
For the layers, the regularizations in are determined by only in .
Thus our regularization operators use their inputs only outside the boundary layer, but provide outputs in a enlargement of the domain . Such a property is critical in order to have good domain regularization properties.
The role of the third property on the other hand is to ensure that polynomials of sufficiently small degree are reproduced by our regularizations. This will later provide good low frequency bounds for differences of successive regularizations.
Regularization kernels with these properties ca be easily constructed:
Lemma 2.9.
Good regularization kernels exist.
Proof.
We outline the steps in the kernel construction, leaving the details for the reader:
a) We consider a unit vector which is uniformly transversal to the boundary, outward oriented. Such an can be chosen locally, and kernels constructed based on a local choice of can be assembled together using a partition of unity in the first variable.
b) Given such an , we consider a smooth bump function with properties as follows:
-
•
the support of is such that
-
•
its average is :
-
•
and, it has zero moments
c) For each dyadic scale we consider a shifted regularizing kernel
on the scale, which is accurate to any order.
Correspondingly we also consider a partition of unity in ,
where the functions select the region and are smooth on the scale. Given a fixed dyadic scale , we adapt this partition of unity to ,
where the first term can be extended by to the exterior of .
d) We define the regularization kernels
which are still accurate to any order. It is easily verified that these kernels have the desired properties.
∎
Next we prove bounds for our regularizations in spaces:
Proposition 2.10.
The following estimates hold for good regularization kernels whenever is a nondegenerate defining function with :
a) Regularization bound:
(2.23) |
b) Difference bound:
(2.24) |
c) Error bound
(2.25) |
Here we recall that the regularized functions are defined on the larger domain . This is what allows us to measure them with respect to a perturbed domain as long as the two boundaries are within of each other.
Proof.
By interpolation we can assume that and are both integers. Because of the support properties of , we can prove the desired estimate separately in each boundary layer , for , and then separately for . For instance in the case of (2.23) we will show that
(2.26) |
where the domain restricted norms are interpreted as the square integral of the appropriate quantities over the restricted domains999In a standard fashion, we also need to allow the domain on the right to be a slight enlargement of the domain on the left..
The above localization allows us to fix the dependent localization scale for , which becomes akin to a scaling parameter. Even better, we can localize further to a ball and show that
Consider one component of the norm on the left, namely the maximal one, and show that
(2.27) |
To avoid distracting technicalities, consider first the case , where the weights are constant and can be dropped. Then the above inequality becomes
(2.28) |
The difficulty here is that we only have control over the derivatives of (here can be replaced by either or ). We can bypass this difficulty using (a higher order version of) Poincare’s inequality in , which allows us to find a polynomial of degree so that
The property (2.22) shows that , therefore in (2.28) we can replace by , for which we have better control of the lower Sobolev norms. Then the estimate (2.28) easily follows.
Minor adjustments to this argument are needed in . Then , and we can still freeze in the input region to . On the other hand in the output region we have , which still allows us to drop the weight. The Poincare inequality still applies. The only difference is that the weight in the norm on the left might be singular. However, this weight is nevertheless square integrable near the boundary, which suffices due to the fact that in effect in we can obtain pointwise control for .
Now we consider the case (b). There the same localization applies, and the main difference in the proof is that now for a polynomial of degree at most we have
This in turn allows us to also substitute by in (2.28) when is negative. The rest of the argument is identical.
Given a rough state , we can use the above Lemma to construct a regularized state as follows:
-
a)
We define the regularized functions in the larger domain by
-
b)
We restrict to the set101010Here and below we use subscripts for as in to indicate the domain associated to a function , and the superscripts to select various boundary layers. .
Such a strategy works provided that the domain is large enough in order to allow to transition to negative values before reaching the boundary of its domain. We will see that this is indeed true provided that is above the scaling exponent . Our main result is stated below. For better accuracy, we use the language of frequency envelopes to state it.
Proposition 2.11.
Assume that . Then given a state , there exists a family of regularizations , so that the following properties hold for a slowly varying frequency envelope which satisfies
(2.29) |
-
i)
Good approximation,
(2.30) and
(2.31) -
ii)
Uniform bound,
(2.32) -
iii)
Higher regularity
(2.33) -
iv)
Low frequency difference bound:
(2.34)
Proof.
To start with, we will assume that are defined in the larger set using good regularization kernels ,
By Sobolev embeddings we know that
This easily implies the uniform bound for in , as well as the convergence in the same topology to in . It also implies the pointwise bound (2.31). This in turn shows that on the boundary we have , therefore the zero set is within distance from , and thus within . This ensures that restricted to is a well defined state.
Next we consider the bound (2.32). In view of the difference bound (2.31), this is a consequence of (2.23) with and .
It remains to prove (2.33) and (2.34). If we were to replace by on the right, this would also follow from Proposition 2.10. To gain the extra decay associated with a frequency envelope, for the functions we will use the interpolation space representation given by Lemma 2.5 with sufficiently large,
(2.35) |
for which the norm in (2.9) is finite. Accordingly, we can choose a slowly varying frequency envelope so that
(2.36) |
with
The frequency envelope above is the one we will use in the Proposition. The property (2.29) is then automatically satisfied.
iii) Proof of (2.33). Our starting point is again the decomposition (2.35)-(2.36) for , but now we separate the contributions of and .
a) Low frequency components . Using the bounds in Proposition 2.10, the bounds for carry over to , namely
Then by interpolation we have
(2.37) |
b) High frequency components . Here we discard the bound, and instead estimate directly
(2.38) |
v) Proof of (2.34). We follow the same strategy as above, where we still can use all the bounds in Proposition 2.10, but with the difference that now we also have access to the difference bound in (2.24).
Starting with the decomposition (2.35)-(2.36) for , we observe that the bound for suffices in the high frequency case . It remains to consider the low frequency case , where we will have to rely instead on the norm. Precisely, by (2.24) we have
(2.39) |
which again, combined with (2.36), suffices after dyadic summation. ∎
2.5. Interpolation inequalities
Next we consider interpolation type inequalities, which are critical in order to prove our sharp, scale invariant energy estimates.
For clarity and later use we provide a more general interpolation result. Our main result, which applies in any Lipschitz domain with a nondegenerate defining function , is as follows:
Proposition 2.12.
Let and . Define
(2.40) |
and assume that
(2.41) |
Then for we have
(2.42) |
Remark 2.13.
One particular case of the above proposition which will be used later is when , with the corresponding relation in between the exponents of the weights.
As the objective here is to interpolate between the type norm and bounds, we will need the following straightforward consequence of Proposition 2.12:
Proposition 2.14.
Let and
(2.43) |
Define
(2.44) |
Then for we have
(2.45) |
We will also need the following two variations of Proposition 2.14:
Proposition 2.15.
Let and
Define
Then for we have
respectively
Proposition 2.16.
Let and
Define
Then for we have
Here the role of the lower bound on is to ensure that for all intermediate , where the constraint is the strongest.
We will use the last two propositions for , where the pointwise bound comes from the control norms and .
Proof of Proposition 2.12.
We begin with several simplifications. First we note that it suffices to prove the case and . Then the general case follows by reiteration. Indeed the case allows us to compare any three consecutive norms
and then the main estimates (2.42) follows from combining the above bounds.
A second simplification is to observe that we can also reduce the problem to the one dimensional case, which we state in the following lemma:
Lemma 2.17.
Let , and with , so that
and with
Then the following inequality holds
(2.46) |
To see that the -dimensional case reduces to the one dimensional case, we consider a constant vector field which is transversal to the boundary, apply (2.46), with replaced by , on every line in , where denotes the transversal direction. We raise it to the power and integrate in . This yields
where at the second step we have used Hölder’s inequality. The full -dimensional bound is obtained by applying the above estimate for a finite number of vector fields which (i) are transversal to the boundary and (ii) span . It remains to prove the last Lemma 2.17:
Proof of Lemma 2.17.
This interpolation inequality is a weighted Gagliardo–Nirenberg-Sobolev inequality, see[24]. One main ingredient in the original proof given in [24] for the unweighted case, is the following inequality due to P. Ungar:
Proposition 2.18.
On an interval , whose length is denoted by , one has
where ,
The heuristic interpretation of Proposition (2.18) is that the average of the first derivative of a function is controlled by its pointwise values, and its variation is controlled by its second derivative. This observation yields the balance between the parameters , , and in Lemma 2.46. We will use the same result here to prove (2.46).
The first step is to use a dyadic spatial decomposition of , such that the interval in Proposition 2.18 is fully contained in a generic interval , where , and . Using Proposition (2.18), we have
To get from this inequality to (2.46) it would be convenient to know that the last two terms in the above inequality are comparable in size. One can try to achieve this by increasing the size of the interval until this is true. The difficulty is when this it cannot be done without going past the dyadic interval size. So the natural strategy is to consider the dyadic decomposition of interval and compare the and norms in each of these dyadic intervals.
If on any such dyadic interval we get
(2.47) |
then we subdivide this interval into pieces where these two terms are comparable, and complete the proof of (2.46) within this interval.
Unfortunately this may not be the case in all dyadic subintervals. To rectify this we introduce a slowly varying frequency envelopes for and for , so that the following properties hold:
-
•
Control norm
-
•
and summability
-
•
Slowly varying
for small and positive.
Now, we compare again as in (2.47)
(2.48) |
(2.49) |
which holds iff
In the dyadic regions where this holds we finish the proof as discussed above, by subdividing the dyadic intervals and applying Proposition 2.18. To see where the switch happens we observe that is slowly varying whereas the RHS of the inequality above decreases exponentially, as grows. Then we can find a unique where the two are comparable,
(2.50) |
Then (2.49) holds for , which implies that
(2.51) |
It remains to consider the case when , where we are simply going to obtain a pointwise bound for . Selecting a favorable point , i.e. where
(2.52) |
we estimate for with :
Now we estimate using the bound above
(2.53) |
where the integral converges since as the exponents obey the restriction dictated by the scaling in (1.13), and is sufficiently small. To finish the proof we observe that by (2.50) and (2.52), the RHS of (2.53) is comparable to the right hand side of (2.51) when .
This concludes the proof of Lemma2.17. ∎
The proof of the Proposition 2.14 follows as a straightforward consequence. ∎
Proof of Proposition 2.15.
This is largely similar to the proof of Proposition 2.12, so we omit the details and only describe the key differences. The reduction to the case is similar, using also the case of Proposition 2.12, at least if we allow to be arbitrary rather than . The one dimensional reduction is also similar. Thus we are left with having to prove the following analogue of Lemma 2.17
Lemma 2.19.
Let , and with , so that
and with
Then the following inequality holds
(2.54) |
This Lemma is proved using the following analogue of Proposition 2.18, which is a straightforward exercise.
Proposition 2.20.
On an interval , whose length is denoted by , one has
where , .
∎
Proof of Proposition 2.16.
This is also similar to the proof of Proposition 2.12, so we omit the details and only describe the key differences. The reduction to the case uses again the case of Proposition 2.12, and the one dimensional reduction is also similar. Thus we are left with having to prove the following analogue of Lemma 2.17:
Lemma 2.21.
Let , and with , so that
and with
Then the following inequality holds
(2.55) |
This Lemma is proved in the same fashion as Lemma 2.17 using directly Proposition 2.18 for with well chosen constants .
∎
3. The linearized equations
This section is devoted to the study of the linearized equations, which have the form
(3.1) |
Using the material derivative, these equations are written in the form
(3.2) |
Here are functions defined within the time dependent gas domain . Notably, no boundary conditions on are imposed or required on the free boundary .
3.1. Energy estimates and well-posedness
We first consider the question of proving well-posedness and energy estimates for the linearized equations:
Proposition 3.1.
Here we estimate the absolute value of the time derivative of the linearized energy, in order to guarantee both forward and backward energy estimates; these are both needed in order to prove well-posedness.
Proof.
We recall the time dependent weighted norm,
To compute its time derivative, we use the material derivative in a standard fashion. For later reference we state the result in the following Lemma:
Lemma 3.2.
Assume that the time dependent domain flows with Lipschitz velocity . Then the time derivative of the time-dependent volume integral is given by
(3.4) |
Using the above Lemma, we compute
We observe that the last integral is zero. The computations is straightforward and follows from integration by parts:
as the boundary terms vanish on .
The first integral includes the bounded term . It follows right away that the energy norm will indeed control it, and the desired energy estimate (3.3) follows.
The well-posedness result will follow in a standard fashion from a similar estimate for the adjoint equation, interpreted as a backward evolution in the dual space . We identify by Riesz’s theorem, with respect to the associated inner product in :
(3.5) |
Then the adjoint system associated to (3.1), with respect to this duality, is easily computed to be the following:
(3.6) |
Modulo bounded, perturbative terms, this is identical to the direct system (3.2), therefore the backward energy estimate for the adjoint problem (3.6) follows directly from (3.3). ∎
In particular we note that, due to translations in time and space symmetries, the linearized estimate applies to the functions , as well as .
3.2. Second order transition operators
We remark that discarding the terms from the equations we obtain a reduced linearized equation,
(3.7) |
which is also well-posed in . For many purposes it is useful to also rewrite the linearized equation as a second order evolution. We will only seek to capture the leading part, up to terms of order . Starting from the above reduced linearized equation, we compute second order equations where we discard the terms arising from commuting and .
Then for we obtain the reduced second order equation, (which would be exact if were constant)
(3.8) |
which for yields
On the other hand for we similarly obtain
(3.9) |
The operators and will play an important role in the analysis of the energy functionals in the next section. An important observation is that they are symmetric operators in the spaces which occur in our energy functional and in the norm . For a more in depth discussion we separate them:
Lemma 3.3.
Assume that is Lipschitz continuous in the domain , and nondegenerate on the boundary . Then the operator , defined as an unbounded operator in the Hilbert space , with
is a nonnegative, self-adjoint operator.
The proof is relatively standard and is left for the reader. Later in the paper, see Lemma 5.2, we prove that is coercive, and that it satisfies good elliptic bounds, which in particular will allow us to identify the domain of as
which is the first component of the space.
Next we turn our attention to the operator . This is also a symmetric operator, this time in the space , which is the second component of . However, it lacks full coercivity as only controls the divergence of . For this reason, we will match it with a second operator which controls the curl of , namely
so that . Then the operator has the right properties:
Lemma 3.4.
Assume that is Lipschitz continuous in , and nondegenerate on the boundary . Then the operator , defined as an unbounded operator in the Hilbert space , with
is a nonnegative, self-adjoint operator.
Later in the paper, as a consequence of Lemma 5.2, it follows that is coercive, and that it satisfies good elliptic bounds, which in particular will allow us to identify the domain of as
which is the second component of the space.
Remark 3.5.
For the most part, we will think of and in a paradifferential fashion, i.e. with the dependent coefficients localized at a lower frequency than the argument. The exact interpretation of this will be made clear later on.
4. Difference bounds and the uniqueness result
Our aim here is to prove difference bounds for solutions, which could heuristically be seen as integrated111111Along a one parameter family of solutions. versions of the estimates for the linearized equation in the previous section. As a corollary, this will yield the uniqueness result in Theorem 1.
For this we consider two solutions and for our main system (1.7), and seek to compare them. Inspired by the linearized energy estimate, we seek to produce a similar weighted bound for the difference
The first difficulty we encounter is that the two solutions may not have the same domain. The obvious solution is to consider the differences within the common domain,
The domain no longer has a boundary. However, if we assume that the two boundaries and are close in the Lipschitz topology, then still has a Lipschitz boundary which is close to . To measure the difference between the two solutions on the common domain, we introduce the following distance functional121212We do not prove or claim that this defines a metric.
(4.1) |
where throughout the section. We remark that the weight vanishes on only at points where and intersect. Away from such points, both and are nondegenerate; precisely, we have
Since both and are assumed to be uniformly Lipschitz and nondegenerate, it follows that this relation extends to a neighbourhood of ,
Then the first term in yields a nontrivial contribution in this boundary region:
Lemma 4.1.
Assume that and are uniformly Lipschitz and nondegenerate, and close in the Lipschitz topology. Then we have
(4.2) |
One can view the integral in (4.2) as a measure of the distance between the two boundaries, with the same scaling as .
Now we can state our main estimate for differences of solutions:
Theorem 5.
Let and be two solutions for the system (1.7) in , with regularity , , so that are uniformly nondegenerate near the boundary and close in the Lipschitz topology, . Then we have the uniform difference bound
(4.3) |
We remark that
Thus, our uniqueness result in Theorem 1 can be viewed as a consequence of the above theorem.
The remainder of this section is devoted to the proof of the theorem.
4.1. A degenerate difference functional
The distance functional introduced above is effective in measuring the distance between the two boundaries because it is nondegenerate at the boundary. This, however, turns into a disadvantage when we seek to estimate its time derivative. For this reason, in the energy estimates for the difference it is convenient to replace it by a seemingly weaker functional, where the weights do vanish on the boundary. Our solution is to replace the weights in with symmetric expressions in and , which agree to second order with where , and also which vanish on .
Precisely, we will consider the modified difference functional
(4.4) |
where for now the weights and are chosen as follows as functions of and :
-
(1)
They are smooth, homogeneous, nonnegative functions of degree respectively , even in , in the region .
-
(2)
They are connected by the relation .
-
(3)
They are supported in , with in .
For almost all the analysis these conditions will suffice. Later, almost of the end of the section, we will add one additional condition, see (4.26), and show that such a condition can be enforced.
Our objective now is to compare the two difference functionals. Clearly . The next lemma proves the converse.
Lemma 4.2.
Assume that is small. Then
(4.5) |
Proof.
We need to prove the ”” inequality. To do that, we observe that by foliating with lines transversal to , the the bound (4.5) reduces to the one dimensional case. Denoting the distance to the boundary by and the value of on the boundary by , we have the relations
Then
On the other hand,
In the region where we have . Then we can evaluate the first part in the integral by
thereby obtaining the integral in (4.2). Conversely, we have
which gives the desired bound for the missing part of the first term of .
It remains to compare the terms, where we also need to focus on the region . Denote by
for which we can estimate
Then for smaller we can use the Hölder norm to estimate
Hence
as needed. ∎
4.2. The energy estimate
The second step in the proof of Theorem 5 is to track the time evolution of the degenerate energy :
Proposition 4.3.
We have
(4.6) |
In view of Lemma 4.2, the conclusion of the theorem then follows if we apply Gronwall’s inequality.
Proof.
To compute the time derivative of we use material derivatives. But we have two of those, and , and it is essential to do the computations in a symmetric fashion so we will use the averaged material derivative
Using the equations (1.8), we compute difference equations
(4.7) | ||||
(4.8) |
We will also need a symmetrized sum equation
(4.9) |
We use these relations to compute the time derivative of the energy, using Lemma 3.2 with . We have
so the contribution of the term is directly estimated by , and so are the contributions of the first term in (4.7), the first two terms in (4.9), as well as the second term in (4.8). Hence we obtain
where the contributions are as follows:
i) represents the contributions of the averaged material derivative applied to the first factor via the third term (4.9), namely
We separate the two terms,
where
and
ii) represents the contributions of the averaged material derivative applied to the and factors via the third131313The contributions of the first and second terms terms in (4.7) and (4.9) are directly bounded by . terms in (4.7) and (4.9), namely
We also split this into
where
iii) represents the contribution of the averaged material derivative applied to the quadratic factors and via the second and third term in (4.7) and the first term in (4.8).
This is the main term, where we expect to see the same cancellation as in the case of the linearized equation. At this place we need the matching condition between and , namely . Substituting this in and integrating by parts, we obtain an almost full cancellation unless the derivative falls on , namely
where
The above analysis shows that
Hence, in order to prove (4.4), it remains to estimate the error terms,
(4.10) |
A. The bound for . We begin with the bound for , which is simpler and will also be needed later. As in Lemma 4.2, we can reduce the problem to the one dimensional case by foliating with parallel lines nearly perpendicular to its boundary . Denoting again the distance to the boundary by and the value of on the boundary by , we have
Then in order to estimate , it suffices to prove the bound in the following interpolation lemma
Lemma 4.4.
Let and . Then we have the following interpolation bound in :
(4.11) |
The Lemma is applied with . Note that by direct integration the same bound holds in all dimensions. Thus we obtain
Corollary 4.5.
In the context of our problem we have
(4.12) |
The same bound also holds if all norms are restricted to any horizontal cylinder (i.e. transversal to ).
Proof.
We think of this as some version of a Hardy type inequality. The proof is based on similar argument as seen before in Section 2. We interpret as being pointwise equivalent with and get
To get the result we integrate by part and use Hölder’s inequality as follows
Since, we assumed that , we indeed get:
∎
B. The bound for , , , and . We group the like terms and set
where we can express and in the form
with smooth and -homogeneous,
respectively
with smooth and -homogeneous,
Here we have used the fact that is -homogeneous, which yields . Also we remark that vanishes in a conical neighbourhood of , therefore we can also think of the integrand as being at least cubic in .
Heuristically, one might think that after another round of integration by parts one might place the derivative in either on , in which case we get good Gronwall terms, or on , where we just discard it and reduce the problem to estimating an integral of the form
Unfortunately such a strategy works only if ; for larger a problem arises, having to do with potentially large contributions within a thin boundary layer.
Instead, to address the full range of , we will develop the idea of separating a carefully selected boundary layer, where we provide a direct argument, whereas outside this boundary layer we can use the simpler integration by parts idea above.
To understand our choice of the boundary layer, we consider first the much simpler case when and on the boundary, where and
(4.13) |
Then the estimate for above reduces to the one dimensional case, where we can simply argue by Holder’s inequality:
(4.14) | ||||
Unfortunately, in general the bound (4.13) will not hold, and we will separate the region where it holds and the region where it does not hold.
Our boundary layer will depend on , and will roughly be defined as the complement of the region where (4.13) holds, with the additional proviso that it must have thickness at least . For a rigorous definition, we start with the function defined on the boundary of as follows:
(4.15) |
where is a fixed large universal constant. Then we define our boundary layer as
(4.16) |
as well as its enlargement
(4.17) |
Here is a small universal constant.
We want this boundary layer to have a locally uniform geometry. This is insured by a slowly varying type property of the function .
Lemma 4.6.
We have
(4.18) |
Proof.
We consider each of the three components of in (4.15). For the first one we simply use the Lipschitz bound for . For the second one, we use the bound on and to estimate
which suffices. Finally for the last term we have
which is again enough. ∎
This property insures that and are separate:
Lemma 4.7.
There exists a smooth cutoff function in with the following properties:
a) Support: in and in ,
b) Regularity: .
Proof.
For we define the function
so that , are described by
Then we can use the function to describe the separation between and . Precisely, it suffices to show that we can control the Lipschitz constant for in the transition region,
Since is an infimum, it suffices to show the same for each of its defining functions. Equivalently, it suffices to show that if is in the transition region then
Let be the closest point to on the boundary, so that . Then the first relation implies that
Since is small, Lemma 4.6 shows that . Since we are in the transition region, we must also have
as needed. ∎
Finally we verify that we have good control over on the outer region:
Lemma 4.8.
The good bound (4.13) holds outside .
Proof.
Let , and the closest point to on the boundary. Then
Using the bound for along the line, we have
If we use this directly we obtain
If instead we integrate it between and then we obtain
∎
Now we use the cutoff to split each of the above integrals in two, and estimate each of them in turn.
B.1. The estimate in the outer region. Here we insert the cutoff in each of the two integrals , and integrate by parts in . Precisely, the outer part of is
The dependent part of the integrand is
In order to be able to integrate by parts, we define a function in the region of interest by
By definition, is smooth, homogeneous of order three, and satisfies
Then we can write
We substitute this in to obtain
In the first integral we integrate by parts. If the derivative falls on we get a Gronwall term. Else, it falls on , which we discard, or on , where we use Lemma 4.7. Hence we obtain
In view of Lemma 4.8, we can estimate the integral as in (4.14) and conclude.
The argument for is similar but simpler, as no integration by parts is needed.
B.2. The estimate in the boundary layer region. To fix scales, we use the slowly varying property of in Lemma 4.6 to partition into cylinders centered at some point , with radius and similar height, and correspondingly, we partition our integrals using an appropriate locally finite partition of unity,
where each is smooth on the scale. Within this cylinder we will think of as a constant, .
Denoting
and similarly for , our objective will be to show that in each such component we have
(4.19) |
where denotes the integral in but with the added cutoff . After summation over this will give the desired estimate. We will consider separately the cases when is small or large.
As a prerequisite to the proof of (4.19), we consider pointwise difference bounds within . We begin with . By construction, within we have
(4.20) |
In particular this yields
(4.21) |
and the improved pointwise bound
(4.22) |
where we observe that needs not be constant on the boundary within .
Depending on the relative size of and we will distinguish two scenarios:
Lemma 4.9.
One of the following two scenarios applies in :
a) Either , in which case we must have .
b) Or , in which case we must have .
We will refer to the first case as the small case and the second as the large case.
Proof.
We start by comparing with . If , then we must have
and further , which places us in case (b).
If , then we have two nonexclusive possibilities. Either we have
which yields , placing us in case (a). Or, we have
which places us again in case (b). ∎
In addition to bounds for , we also need bounds for . We will show that within the same cylinder we have a good uniform bound for :
Lemma 4.10.
Within we have
(4.23) |
Proof.
Denote by the average of in the region
which represents an interior portion of away from the boundary. We estimate this using the distance , where we observe that within we have . Then we obtain
To obtain the full bound for we combine this with the Lipschitz bound, which yields
within the full cylinder .
∎
B.2.a. The case of large . We recall that in this case we have and . Consider first. We discard the gradient terms, bound by and use Lemma 4.10 for . This yields
On the other hand, a localized version of (4.2) yields
Combining the last two bounds gives
as needed. The arguments for is identical.
B.2.b. The case of small . We recall that this corresponds to and . This is the more difficult case.
The first observation concerning the cylinder is that is large there on average, of size . This is reflected in a bound from below for :
Lemma 4.11.
Assume we are in the small case. Then we have
(4.24) |
Proof.
We approximate near with its linear expansion,
Within this can be simplified to
Now we consider a small interior ball
where we have and , and use to estimate
The integral on the left is easily evaluated, to get
We can compare the constants on the left and the first term on the right. We know that
If the first quantity on the right is larger, then
and we obtain
Choosing with a small constant , the first term on the right is absorbed on the left and we arrive at the desired conclusion.
If the second quantity on the right is larger, then
and we obtain
Hence we can conclude exactly as before. ∎
The above Lemma allows us to slightly improve Lemma 4.10 to
Lemma 4.12.
Assume that is small. Then within we have
(4.25) |
We are now ready to estimate the first integral,
It remains to estimate , which we recall here:
Aside from the obvious cancellation when , we would like to integrate by parts in order to move the derivative away from . To implement this integration by parts, we need an auxiliary function so that
Suppose we have such a function which is smooth, homogeneous of order and supported in . Then integration by parts yields
In the first integral we bound by , and then bound the rest by since in the support of the integrand. The second integral is similar to . Finally in the third integral the gradient of yields an factor, and we can estimate it using Lemma 4.12 and the bound (4.22) for by
where at the last step we bound twice, for the rest of and use Lemma 4.11; the powers of will all cancel, as predicted by scaling considerations.
It remains to show that we can find such a function . This is where a convenient choice of helps. Precisely, we want to be nonnegative, even in , supported in and equal to when . In order to avoid boundary terms in the integration by parts, we will choose with similar support. But we also want to be smooth and homogeneous, and then we will have an issue at , unless we can arrange for to also be supported away from . But this will happen only if
(4.26) |
Lemma 4.13.
There exists a good choice for which satisfies (4.26).
Proof.
We will take advantage of the fact that the function is increasing, as follows. We start with a choice for which is nonincreasing. That would make the integral in (4.26) positive. To correct this we use a nonnegative, compactly supported bump function . Its contribution will be negative, as it can be seen integrating by parts:
Then we choose , with chosen so that the two contributions to the integral in (4.26) cancel. ∎
∎
5. Energy estimates for solutions
Our objective here is to prove Theorem 3. More precisely, we aim to establish uniform control over the norm of the solutions in terms of the similar norm of the initial data, with growth estimated in terms of the control parameters . The key to this is to characterize these norms using energy functionals constructed with suitable vector fields naturally associated to the evolution.
5.1. The div-curl decomposition
A first step in our analysis is to understand the structure of our system of equations. In the nondegenerate case, it is known that at leading order the compressible Euler equations decouple into a wave equation for and a transport equation for . We will show that the same happens here. Of course, algebraically the computations are identical. However, interpreting the coupling terms as perturbative is far more delicate in the present context.
We begin with a direct computation, which yields the following second order wave equation for ,
(5.1) |
with speed of propagation (sound speed)
where corresponds to the (material) velocity
On the other hand for the vorticity we obtain the transport equation
(5.2) |
These two equations are coupled, so it is natural to consider them at matched regularity levels, but we will use different energy functionals to capture their contributions to the energy.
5.2. Vector fields
Our energy estimates will be obtained by applying a number of well chosen vector fields to the equation in a suitable fashion, so that the differentiated fields obtained as the outcome solve the linearized equation with perturbative source terms. We do this separately for the wave component and for the transport part.
a) Vector fields for the wave equation. Here we use all the vector fields which commute with the wave equation at the leading order. There are two such vector fields, which generate an associated algebra:
-
a1)
The material derivative ; this has order .
-
a2)
The tangential derivatives, ; these have order .
We will only use in this article, but note that a similar analysis works for the tangential derivatives.
b) Vector fields for the transport equation. Here we have more flexibility in our choices, again generating an algebra.
-
b1)
The material derivative ; this has order .
-
b2)
All regular derivatives , of order .
-
b3)
The multiplication by , which has order .
In order to avoid negative orders here, one may replace by , which has has order .
5.3. The energy functional
Here we define energy functionals of order , i.e. which involve combinations of vector fields of orders up to . We will set this up as the sum of a wave and a transport component,
(5.3) |
a) The wave energy. Here we want to use operators of the form
applied to the solution . However, we would like to have these defined in terms of the data at each fixed time, rather than dynamically. Algebraically this is easily achieved by reiterating the equation. We define
which should be viewed as discussed above, as nonlinear141414Strictly speaking, at leading order these are linear expressions, so the better terminology would be quasilinear. functions of at fixed time.
One might hope that these functions should be good approximate solutions for the linearized equations. Unfortunately, this is not exactly the case even for . This is because, unlike , does not exactly generate an exact symmetry of the equation. The solution to this difficulty is to work with associated good variables, obtained by adding suitable corrections to them. We denote these good variables by , and define them as follows:
-
i)
.
-
ii)
.
-
iii)
.
-
iv)
:
We now define the wave component of the energy as
(5.4) |
where we recall that defined in (1.11) represents the natural energy functional for the linearized equation. In the sequel we will use these good variables only for even , but for the sake of completeness we have listed them for all .
b) The transport equation. Here we consider a simpler energy, namely
(5.5) |
which at leading order scales in the same way as the wave energy above. One can think of this energy as the outcome of applying vector fields up to and including order to the vorticity .
5.4. Energy coercivity
Our goal here is to prove the equivalence of the energy with the size of .
Theorem 6.
Let be smooth functions in so that is positive in and uniformly nondegenerate on . Then we have
(5.6) |
Proof.
a) We begin with the easier part “”. This is obvious for the vorticity component so it remains to discuss the wave component.
We consider the expressions for . These are both linear combinations of multilinear expressions in and with the following properties:
-
•
They have order , respectively .
-
•
They have exactly derivatives.
-
•
They contain at most , respectively factors of or its derivatives.
These properties suffice in order to be able to distribute the powers of and use the interpolation inequalities in Proposition 2.14. We will demonstrate this in the case of ; the case of is similar. A multilinear expression in has the form
where , ,
and151515Here we allow for or , in which case the corresponding products are omitted.
We seek to split
and correspondingly
so that we can apply our interpolation inequalities from Proposition 2.14, Proposition 2.15. These will give bounds of the form
respectively
where the denominators represent the orders of the expressions being measured, so they add up to as needed.
It only remains to verify that the ’s and the ’s can be chosen in the range where our interpolation estimates apply, which is
respectively
To verify that we can satisfy these conditions we need
But the sum on the left is evaluated by
using . Here equality holds only if , and i.e. for the leading linear case.
b) We continue with the “” part. To do this we will argue inductively, relating with . This is done using the transition operators and introduced earlier.
Lemma 5.1.
For we have a pair of homogeneous recurrence type relations
(5.7) |
where and are also multilinear expressions as above, of order , respectively , but with the additional property that they are non-endpoint, i.e. they contain at least two factors of the form or .
Proof.
We begin with the first relation, for which we first discuss the generic case . We begin expanding the expression of , and then continue calculating the LHS of (5.7). We have
(5.8) |
The LHS expands as follows
(5.9) |
Each of the two terms appearing in the expression above can be further analyzed. For the first term on the RHS in (5.9) we have
(5.10) |
The last two terms already satisfy the non-endpoint property, so we are left to process the first term on the RHS of (5.10) further:
We note that gives at least derivatives, and, for any the claim is obvious, as we have that one material derivative on will produce derivatives. Hence, the more difficult case is when ; we discuss it further:
(5.11) |
We commute the material derivative with the Laplacian using the formula
(5.12) |
and 5.11 gives
(5.13) | ||||
The last term in the expression above gets absorbed in . For the next to last term we have
We distribute and commute all the material derivatives to observe that all but one term are readily in (commuting with , or even better with gives rise to , respectively (5.12) terms, which ensures the non-endpoint property), namely
For this we need commute the material derivatives with :
(5.14) | ||||
The first term above is in and the last term is part of the expression in (5.8).
For the first term in (5.13), we commute with the Laplacian
We observe that the first term on the RHS above is which is one of the terms on the RHS of the expansion in (5.8). The last terms is included in , as the commutator , for , will produce at least one of each terms in .
We now deal with the last term in (5.9)
(5.15) | ||||
For the first term on the RHS of (5.15)we get
where we can, by inspection, see that almost all the terms are in , except for the case , i.e. the term . As before, we have
where the first terms is in and the last one (together with from (5.15)) gives another term in (5.8), namely
(5.16) |
Lastly, we return to the last term in (5.15),
which we rewrite as
This finishes the proof of the (5.7) for the formula in the case : the first term is part of the and the last one appears in (5.8).
The argument for the case is similar. The only difference occurs at the very end, where we collect the contribution of last term in (5.14) (with the corresponding factor) and the expression in (5.16) and rewrite them as follows:
where the last term goes into .
For the there is no difference in the case . The formula we are asked to show is
(5.17) |
As before, we expand the LHS of (5.17) and peel off the terms that belong to , and then inspect that the remaining terms match its RHS
which gives
The commutator terms gets absorbed in . For we note that all but one of the terms have the non-endpoint property, namely , which is part of the RHS of (5.17). Lastly, for the we have
The case gives
the commutator term belongs to , and hence we are left with
which is again part of the RHS of (5.17).
∎
To take advantage of the above recurrence lemma, we will need a pair of elliptic estimates for the operators , . There is one small matter to address, which is that we would like these bounds to depend only on our control parameter , whereas contains second derivatives of in the coefficients. This can be readily rectified by replacing by
(5.18) |
or in coordinates, to avoid ambiguity in notations,
(5.19) |
We note that the difference between and is the expression , whose contribution can be harmlessly placed in in (5.7).
Set
Then we have
Lemma 5.2.
Assume that is small. Then the following elliptic estimates hold:
(5.20) |
respectively
(5.21) |
and
(5.22) |
Remark 5.3.
We note that in essence this estimate has a scale invariant nature. The lower order term added on the right plays no role in the proof, and can be dropped if either are assumed to have small support (by the Poincare inequality), or if we use the corresponding homogeneous norms on the left.
We will in fact need a more general result, where the and operators are replaced by and , respectively, where :
Corollary 5.4.
The results in Lemma 5.2 also hold when and are replaced by and , for , where
This is a direct consequence of the proof of Lemma 5.2, rather than of the Lemma.
Proof of Lemma 5.2.
We first observe that the bound (5.21) is a direct consequence of (5.22) since is a function of . Hence it suffices to prove (5.20) and (5.22).
Before we dwelve fully into the proof, we note that we have the relatively standard weaker elliptic bounds
respectively
For these bounds we only need integration by parts, treating the first order term in both and perturbatively, and using only the pointwise bound for . We leave this straightforward computation to the reader.
Taking the above bounds into account, our bounds (5.20) and (5.22) reduce to the scale invariant estimates
(5.23) |
respectively
(5.24) |
We consider first (5.20), where we proceed using a simple integration by parts. To avoid differentiating twice, we assume that at some point . Then in our domain we have
We compute
which suffices by the Cauchy-Schwarz inequality.
Next we consider the bound (5.21) for the component, where
We use a computation similar to the one before, integrating by parts and using the fact that all the tangential derivatives of are and its normal derivative is ,
We claim that the above expression can be bounded from below by
To see that, we cancel the two terms, and restricting indices below to , we have to show that
(5.25) |
Indeed, we can bound the expression on the left by Cauchy-Schwarz as
If we can establish that the first term on the right admits the equivalent representation
then (5.25) follows by one more application of Cauchy-Schwarz. This last bound, in turn, reduces to the relation
(5.26) |
In the model case , the left hand side is exactly zero, integrating by parts. In the general case, we arrive at almost the same result after a more careful integration by parts:
This concludes the proof of (5.26), and thus the proof of the lemma.
∎
The above set-up suffices in order to prove our coercivity bounds. We will successively establish the estimates
(5.27) |
Concatenating these bounds we get the desired estimates in the theorem, where the errors are absorbed using the smallness condition .
The case follows directly from Lemma 5.2 above, using the interpolation estimates to get smallness for , in the sense that
(5.28) |
The case requires an additional argument. Precisely, we will apply Lemma 5.2 to functions of the form
where is any operator in the right class,
In order to do that we need to have a good relation between and . To achieve this, we apply in (5.7). For this yields
where we need to examine more closely the commutator term. To keep the analysis simple it suffices to argue by induction on , beginning with . All terms in the commutator, where at least one factor gets differentiated twice, are non-endpoint terms, and can be estimated by interpolation. All terms in the commutator where two factors get differentiated are taken care of by the induction in . Finally, all terms where only one term is differentiated are also taken care of by the induction in , unless . Thus if then all commutator terms are estimated either as error terms or via the induction hypothesis.
So the only nontrivial case is when . In this case it is convenient to consider a frame adapted to the free surface, so that
Then all commutators with tangential derivatives are error terms, and the only nontrivial commutator terms are those with . For these, we write modulo good error terms
The contribution of the first term on the right can be included in , akin to a conjugation. The contribution of the second term on the right can be viewed as an induction term if we phrase the argument as an induction in the number of normal derivatives. Then we can write
where
for which we can still apply the analysis in Lemma 5.2.
Finally, we consider the case , where the relation in Lemma 5.1 is not exactly true, but it is essentially true once we differentiate at least twice. Precisely, we compute
Instead of comparing with , we compare with where as before . Here we must have , so we begin with the case and . For tangential derivatives we get modulo error terms
while for normal derivatives
From here on the argument is similar to the case.
The analysis is similar in the case of , which, we recall, has the form
For this we can write a similar conjugation relation, again modulo perturbative and induction terms,
where
Substituting with , we can then apply the elliptic bounds in Corollary 5.4. ∎
5.5. Energy estimates
Here we prove energy estimates in for solutions . We recall the equations.
(5.29) |
or, with :
(5.30) |
We will also use the transport equation for ,
(5.31) |
Now we consider the higher Sobolev norms . For these we will prove the following:
Theorem 7.
The energy functional in has the following two properties:
a) Norm equivalence:
(5.32) |
b) Energy estimate:
(5.33) |
The first part of the theorem, i.e. the coercivity, was proved in the previous subsection. To prove the second part of the theorem we will separately estimate the time derivative of each component in . The first step in that is to derive the equations satisfied by the functions used in the definition of the energy.
I) The wave component. Here we will show that is a good approximate solution to the linearized equation:
Lemma 5.5.
Let . The functions solve the equations
(5.34) |
where and are non-endpoint161616We recall that this means that there is no single factor in , respectively which has order larger that , respectively . Equivalently, each of them has at least two or factors. multilinear expressions in , of order , respectively , with exactly derivatives.
Proof.
The assertions about the order and the number of derivatives are obvious. It remains to show that no single factor in , respectively has order larger that , respectively . In other words, we want to see that each product in , respectively , has at least two factors of the form or .
We begin with :
The first term has a commutator structure involving which yields at least a coefficient. The same happens with in the second term.
We continue with :
Here we are commuting with , which yield at lest a term. The only case when we do not get the desired structure is if the commutator occurs at the level of the last ,
The contribution of the first term is always balanced. However, for the second term we have
Thus we get a possibly an unbalanced contribution if all of applies to . We obtain,
The computation for is similar but simpler, and it is omitted.
∎
II) The transport component. Here the functions whose weighted norms we are trying to propagate are denoted by , and have the form
(5.35) |
For these functions we have
Lemma 5.6.
The functions are approximate solutions for the transport equation
(5.36) |
where are non-endpoint multilinear expressions in , of order with exactly derivatives.
Proof.
We compute the transport equation
where we write schematically
This proves that all terms in are balanced, since all commutators include factors. ∎
To conclude the proof of the energy estimates it remains to bound the time derivative of the linearized energies
by . In view of our energy estimates for the linearized equation, respectively the transport equation, in order to obtain the desired estimate it suffices to bound the source terms , respectively :
Lemma 5.7.
The expressions and above satisfy the scale invariant bounds
(5.37) |
Proof.
This follows using our interpolation inequalities in Propositions 2.14 2.15 and 2.16, following the same argument as in the proof of part (a) of Theorem 6.
The control parameter gives control at degree , i.e. for and , and gives control at degree , i.e. for and .
We consider the factors in each multilinear expression in , and as follows. The factors of order (i.e. the factors are interpreted as weights, and distributed to the other factors. The factors of order in (i.e. factors) are directly estimated in by and discarded. The factors of maximum order are estimated directly by . The intermediate factors can be estimated in norms in two ways, by interpolating the norm with , or by interpolating with .
Overall the product needs to be estimated in , using exactly one factor. Then a scaling analysis shows that we will have to use exactly one norm, i.e. for instance for monomials of order in we have
This is exactly as in the proof of Theorem 6(a); the details are left for the reader.
∎
6. Construction of regular solutions
This section contains the first part of the proof of our well-posedness result; precisely, here we give a constructive proof of existence of regular solutions. The rough solutions will be obtained in the following section as unique limits of regular solutions.
Given an initial data with regularity
where is assumed to be sufficiently large, we will construct a local in time solution with a lifespan depending on the size of the data. Unlike all prior works on this problem, which use parabolic regularization methods in Lagrangian coordinates, here we propose a new approach, implemented fully within the setting of the Eulerian coordinates.
Our novel method is loosely based on nonlinear semigroup methods, where an approximate solution is constructed by discretizing the problem in time. Then the challenge is to carry out a time step construction which, on one hand, is as simple as possible, but where, on the other hand, the uniform in time energy bounds survive. In a classical semigroup approach this would require solving an elliptic free boundary problem, with very precise estimates. At the other extreme, in a pure ode setting one could simply use an Euler type method. The Euler method cannot work here, because it would loose derivatives. A better alternative would be to combine an Euler method with a transport part; this would reduce, but not eliminate the loss of derivatives.
The idea of our approach is to retain the simplicity of the Euler + transport method, while preventing the loss of derivatives by an initial regularization step. Then the regularization step becomes the more delicate part of the argument, because it also needs to have good energy bounds. To achieve that, we carry out the regularization in a paradifferential fashion, but in a setting where we are avoiding the use of complicated classes of pseudodifferential operators. Thus, in a nutshell, our solution is to divide and conquer, splitting the time step into three:
-
•
Regularization
-
•
Transport
-
•
Euler’s method,
where the role of the first two steps is to improve the error estimate in the third step.
To summarize, our approach provides a new, simpler method to construct solutions in the context of free boundary problems. Further, we believe it will prove useful in a broader class of problems.
6.1. A few simplifications
In order to keep our construction as simple as possible, we observe here that we can make a few simplifying assumptions:
i) By finite speed of propagation and Galilean invariance, we can assume that vanishes and is linear outside a small compact set.
ii) Given the reduction in step (i), the coercivity bound (5.22) proved in Lemma 5.2 carries over to the operator . This yields a natural div-curl orthogonal decomposition for in ,
where the first component is a gradient and the second depends only on . In particular, it follows that we have
where we refer the reader to Lemma 6.5 below for the second step. This allows us to make the simplified choice
(6.1) |
for the transport component of the energy.
6.2. Construction of approximate solutions
Given a small time-step and an initial data we will produce a discrete approximate solution , with the following properties:
-
•
(Norm bound) We have
(6.2) -
•
(Approximate solution)
(6.3)
The first property will ensure a uniform energy bound for our sequence. The second property will guarantee that in the limit we obtain an exact solution. There we can use a weaker topology, where the exact choice of norms is not so important.
Having such a sequence of approximate solutions, it will be a fairly simple matter to produce, as the limit on a subsequence, an exact solution on a short time interval which stays bounded in the above topology. The key point is the construction of the above sequence. It suffices to carry out a single step:
Theorem 8.
Let be a large enough integer. Let with regularity
(6.4) |
and . Then there exist a one step iterate with the following properties:
-
(1)
(Norm bound) We have
(6.5) -
(2)
(Approximate solution)
(6.6)
The remainder of this subsection is devoted to the proof of this theorem.
We begin with an obvious observation, namely that a direct iteration (Euler’s method) loses derivatives. A better strategy would be to separate the transport part; this reduces (halves) the derivative loss, but does not fully eliminate it. However, if we precede this by an initial regularization step, then we can avoid the loss of derivatives altogether. In a nutshell, this will be our strategy. We begin with the outcome of the regularization step.
Proposition 6.1.
Given as in (6.4), there exists a regularization with the following properties:
(6.7) |
respectively
(6.8) |
and
(6.9) |
We postpone for the moment the proof of the proposition, and instead we show how to use it in order to prove the result in Theorem 8.
Proof of Theorem 8.
Here we construct starting from given by the last proposition. Naively the remaining steps are the Euler iteration
and the flow transport
(6.10) |
The important point is that these two steps cannot be carried out separately, as each of them taken alone seems to be unbounded. Instead, taken together there is an extra cancellation to be taken advantage of, which is the direct analogue of a similar cancellation in the energy estimates. Using the transport as above, are defined as follows:
(6.11) |
It remain to show that these have the properties in the proposition. We begin by observing that
so these can be used interchangeably as weights. We also have
so the same can be said for the measures of integration.
We successively compute derivatives of in terms of similar derivatives of . We will work with operators of the form . As before, when applied to a data set , these are interpreted as multilinear partial differential expressions, as if they were applied to a solution and then re-expressed, using the equations, in terms of the initial data. In particular, we recall that the expressions and have orders , respectively .
Switching from derivatives in to derivatives in is done by repeated applications of the chain rule, which involves the Jacobian
Thus in this calculation we will not only produce multilinear expressions, but also powers of . To describe errors, we will enhance our standard notion of order by assigning the order to ; this is natural because as a time step, can be thought of as the dual variable to . Such a choice will ensure that the expression has order , and that all our relations below are homogeneous. Then we have
Lemma 6.2.
a) The following algebraic relations hold:
(6.12) |
where and are multilinear expressions in and their derivatives, and also , with the following properties:
-
•
does not appear undifferentiated.
-
•
They have order respectively .
-
•
In addition to powers of , they contain exactly derivatives applied to factors of , or .
-
•
They are balanced, i.e. they contain at least two or factors.
b) Similar relations hold for and its weighted derivatives
(6.13) |
where is as in (5.36) and has the same properties as and above.
Proof.
We prove part (a), as part (b) is similar. As discussed earlier, transcribing the expression in terms of and is based on repeated application of chain rule, which involves the Jacobian
and yields contributions of order zero. Thus one easily obtains
(6.14) |
where and are multilinear expressions in and with added powers of and which have order , respectively , and exactly derivatives applied to factors of or .
It remains to identify the coefficients of the terms, which are
Identifying with time , and redenoting , we have
But by construction the functions solve the equation at , so the desired identification holds. ∎
Returning to the proof of the theorem, we note that the above lemma already gives the bound (6.6) in the uniform topology. It remains to prove the bound (6.5), where we have to compare with . We recall that these energies have the wave component and the curl component. These are treated in a similar way, so we will focus on the wave component which is more interesting. For this we need to compare the type norms of the good variables
The lower order norms also need to be compared, but that is a straightforward matter. Note that these norms are represented as integrals over different domains. However, we identify these domains via (6.10), and we compare the corresponding densities accordingly.
For exact solutions, the good variables solve the linearized equations with source terms (5.34). For our iteration, the above lemma yields a similar relation with additional source terms,
(6.15) |
where are perturbative source terms as in Lemma 5.5, and are as in the lemma above. The terms satisfy the bound (5.37) in Lemma 5.7, which we recall here:
which is what allows us to treat them as perturbative.
In a similar fashion, Lemma 5.7 shows that the expressions satisfy
Since these terms have an factor, the bound (6.9) also allows us to treat them as perturbative.
It remains to estimate the main expression, for which we compute
The second term can be seen to vanish after integrating by parts; this is the same cancellation seen in the proof of the energy estimates for the linearized equation. The third term, on the other hand, can be estimated as an error term via (6.9),
This concludes the proof of the theorem. ∎
Now we return to the proof of our regularization result in Proposition 6.1.
Proof of Proposition 6.1.
We begin with a heuristic discussion, for which the starting point and the first candidate is the regularization already constructed in Proposition 2.11, with the matched parabolic frequency scale . This will satisfy the properties (6.7) and (6.9), but it is not accurate enough for (6.8).
To improve on this and construct a better regularization we need to understand its effect on the energies, and primarily on the leading energy term which is . For this we need to better understand the expressions for . We have seen earlier that we have the approximate relations
so one might expect that we have
However, this is not exactly accurate, as one can see by considering the first relation for . There
whereas
To rectify this discrepancy, we will interpret the operators and in a paradifferential fashion, i.e. decouple the appearing in the coefficients of and from the in the argument of . Instead, the in the coefficients will be harmlessly replaced with a regularized version of itself, call it and correspondingly and will be replaced by , . Then we will be able to write approximate relations of the form
and further
and similarly for .
Based on these considerations, we will construct our regularization as follows:
-
•
Start with the initial state .
-
•
Produce two initial regularizations and of , on scales , with slightly larger domains, and then restrict them to .
-
•
Use the selfadjoint operators and associated to to regularize the high frequency part within below frequency .
-
•
Obtain the scale regularization of in , by adding the low frequency part to the regularized high frequency part.
-
•
Decrease by a small constant and set , in order to ensure that .
1. A formal computation and the good variables. Both in order to motivate the definition of our regularization, and as a tool to prove we have the correct regularization, here we consider the question of comparing the good variables associated to with associated to . The lemma below is purely algebraic, and makes no reference to the relation between and .
Each term in is a multilinear expression of the same order in , so we will view the difference
as a multilinear expression in and . Heuristically we will think of the first expression as the high frequency part of and the second expression as the low frequency part. Since we are working here in high regularity, the intuition is that high-high terms will be better behaved and can be assigned to the error. Explicitly, we write
(6.16) |
where and stand for the differentials of and as functions of . This is akin to a paradifferential expansion of . In this expansion all terms on each line have the same order, which is , respectively , and are at least bilinear in the difference .
The high-high terms will play a perturbative role in our analysis. This leaves us with the terms which are linear in the difference, i.e. the low-high terms involving the two differentials and . We will further simplify this, by observing that the low-high terms where the low frequency factor is differentiated (i.e. has order ) are also favourable. This leaves us only with low-high terms with top order in the high frequency factor in the leading part. These terms are identified in the following lemma:
Lemma 6.3.
We have the algebraic relations
(6.17) |
where the error terms are linear in ,
whose coefficients are multilinear differential expressions in which contain at least one factor with order , i.e. or .
We remark that combining (6.16) and (6.17) we obtain the expansion
(6.18) |
where all terms on each line are multilinear expressions in and of order , respectively , and whose multilinear error terms have either:
-
a)
(high-high) two difference factors, i.e. or
-
b)
(low-high balanced) exactly one difference factor, and at least one nondifference factor with order , i.e. .
One should think of the above expansions as paradifferential linearizations, but implemented without using the paraproduct formalism.
Proof.
Our starting point is provided by the relations (5.7), differentiated with respect to . This yields
Since the expression is balanced, its differential can be included in . Similarly, the second expression on the right also has terms of order in . Thus we get
(6.19) |
Next we turn our attention to the case , where we have
therefore
where the second and forth terms are admissible errors, so we also get (6.19). Then the conclusion of the lemma follows by reiterated use of (6.19). The argument for is similar. ∎
2. Regularizations for . We begin with the dyadic frequency scale matching the time step , in a parabolic fashion, namely . As mentioned earlier, the direct regularization of given by Proposition 2.11 is not a sufficiently accurate regularization, in that it satisfies the properties (6.7) and (6.9), but not necessarily (6.8).
Nevertheless, we will still use Proposition 2.11 to bracket our desired regularization as follows. Starting with the frequency scale we define a lower and a higher frequency scale
where and will be chosen later to satisfy a specific set of constraints. We remark for now that this is a soft choice, in that there is a large range of parameters that will work.
Correspondingly we consider the regularizations given by Proposition 2.11, denoted by
These regularizations are defined on the enlarged domains , respectively . We will use them on the domain . By Proposition 2.11, this domain’s boundary is at distance at most from the original boundary . In order to ensure that are defined on this domain, we will impose the constraint
(6.20) |
We will think of as a “sub”-regularization, which has to be a part of , and of as a “super”-regularization, in that will be a regularization of it. We arrive at in two steps:
-
i)
We define our first regularization as smooth functions in as follows:
(6.21) (6.22) where , with a smooth, positive bump function with values in and the following asymptotics:
(6.23) -
ii)
The functions in are not yet the desired regularizations as does not vanish on the boundary . If it were negative there, we would simply restrict them to . Unfortunately, all we know is that for some large we have
Then we define
(6.24) restricted to as our final regularization.
3. Bounds for the regularization . To start with, we have the bounds for from Proposition 2.11. So here we consider the bounds for .
Lemma 6.4.
Assume that . Then the following estimates hold for in :
(6.25) |
respectively
(6.26) |
Proof.
a) With and similarly for and , we have the obvious bounds
Then (6.25) follows from elliptic bounds for , respectively , which for convenience we collect in the next Lemma:
Lemma 6.5.
Assume that satisfies
and
Then we have the estimates
(6.27) |
respectively
(6.28) |
Proof.
The estimates in (6.27), respectively (6.28) will follow from the bounds
(6.29) |
respectively
(6.30) |
The bounds for and the bounds for are independent of each other. As the arguments are similar, we will prove the bounds for and leave the bounds for for the reader. We begin with (6.29), where we have to estimate
To achieve this we will inductively bound the norms
For the induction step, we need to bound
where is an operator of order . By Lemma 5.2 we have
The commutator has order , but at most derivatives. Hence by Hölder’s inequality and interpolation we can estimate
(6.31) |
Thus we obtain
which concludes the induction step.
It remains to consider the initial case , where we simply take . Here we argue as in the proof of Theorem 6, more precisely the bound (5.27); in an adapted frame we split the derivatives into normal and tangential, , and conjugate
where the remainder has contributions only,
(6.32) |
Applying Lemma 5.2 for we obtain
where the error term on the right can be absorbed on the left.
Turning now our attention to the component of (6.30), the argument is entirely similar, with a slight modification in the commutator bounds (6.31) and (6.32). These are in turn replaced by
(6.33) |
respectively
(6.34) |
The terms in the last bound arise exactly as before when exactly one derivative applies to the factor in . All other contributions have fewer derivatives on , and are estimated by Hölder’s inequality and Sobolev embeddings. The negative powers only arise when more than derivatives apply to the factors in , which means that fewer derivatives apply to . The details are somewhat tedious but routine, and are omitted. ∎
We now return to the proof of Lemma 6.4, and turn our attention to the bound (6.26). We have
Hence, given the properties of , and the above Lemma, we have the bound
∎
3. Comparing the energies for and . Here the first energy is taken in the domain , while the second is taken in . Our objective is to prove the following result:
Lemma 6.6.
Assume that is large enough, and that and are suitably chosen relative to . Then we have
(6.35) |
The proof below consists of several steps, each of which will require various constraints on and . These are then collected at the end of the proof in (6.53). For orientation, one could simply think of the case and with .
Proof.
These energies have two components, the wave energy and the transport energy. We will focus on the wave component in the sequel, as the argument for the transport part is similar but considerably simpler. For the wave component we need to compare the good variables , respectively , associated to , respectively , and their norms,
(6.36) |
We note that in the second expression we are using the norm, as is the defining function for the domain where are defined. As we seek to compare functions on different domains, it is natural to restrict them to a common domain. To understand this choice, we recall that the two free boundaries and are at distance of each other, and the two weights are at a similar distance within the common domain,
In order for the difference of the two weights to only yield errors, we will restrict our comparison to the region , where we have
Outside this region we will simply neglect the contribution to the first norm in (6.36). On the other hand we will seek to make the second norm small in this region. For this to work, we first need to make sure that the neglected region is within the boundary layer, which has width . Thus we require that
But in addition to that, we also want the second norm to be small in this region. Within a fixed layer with this norm is
(6.37) |
which is a consequence of the fact that we are integrating a function which is smooth on the scale, over a thinner region. This is small if
(6.38) |
Hence we obtain
(6.39) |
provided that
(6.40) |
Within we use Lemma 6.3, more precisely its consequence (6.18), in order to compare respectively . There we seek to estimate the errors perturbatively. We begin with :
Lemma 6.7.
Assume that , with size and that are defined as above. Then we have the error bounds
(6.41) |
The proof of this lemma is similar to the proof of Lemma 5.7, using interpolation inequalities, and is omitted. Here the region where we evaluate the norm is less important, and serves only to insure that and are both defined and comparable there. The gain comes from the fact that the difference is small at low frequency, which comes from (6.26) combined with the bounds for the differences in Proposition 2.11. The power requires , but one can gain more if is assumed to be larger.
Next we consider the expressions :
Lemma 6.8.
Assume that , with size and that are defined as above. Then we have the error bounds
(6.42) |
Proof.
We recall that the expressions are balanced multilinear expressions in , respectively , linear in the second component, containing exactly derivatives, and of order , respectively . The fact that they are balanced allows us to estimate them using Hölder’s inequality and interpolation as in Lemma 5.7, by
where respectively , are control parameters associated to , respectively .
Here the first component is localized at frequencies below , while the second is localized at frequencies above . In particular, it follows that are small,
so their contributions go into the second term on the right in (6.42).
On the other hand, and are merely bounded . We split
The first term is localized at frequencies so using the bounds in Proposition 2.10 we have
which can be made smaller than if . The proof of the Lemma is concluded. ∎
Using the above two lemmas together with (6.39), we obtain our first relation between the two energies,
(6.43) |
This is not yet satisfactory, but we can improve it further. We first observe that in the above inner product we can harmlessly replace the operators and by and respectively. Precisely, we have the difference bound
This is a consequence of interpolation inequalities and Hölder’s inequality due the fact that both differences and are concentrated at high frequencies and have small pointwise size. The details are left for the reader. We arrive at
(6.44) |
A second simplification is that we can replace by in the inner product. For this we need to show that
We first insert a cutoff function in the differences on the left, associated to the same boundary layer, which equals further inside and closer to the boundary. This is allowed because the second factor in the inner product is already small in the cutoff region, while the first one is still bounded in in the same region, provided that the cutoff is lower frequency than the frequency,
(6.45) |
One should compare this to (6.20); together these bounds give the allowed range for . With this substitution, we are left with proving that
Since and are self-adjoint, we can move one of them to the right. This becomes
Now the left factor has size and the right factor has size . This yields an gain provided that
(6.46) |
Thus, we can replace by in (6.44), to obtain
(6.47) |
Once this is done, the expression on the left in the inner product is defined on the entire domain , and we can harmlessly extend the inner product to the full region as the expression on the right in the inner product is already small there. We get
(6.48) |
The next step is to apply the expansion (6.18) for the expression on the right in the inner product to write
(6.49) |
By the counterpart of Lemma 6.7 the error terms will be small, so their contribution to (6.48) can be included in the expression .
For the contribution of we integrate by parts one instance of , respectively , to bound it by
Finally, for the contribution of we can integrate again by parts to obtain
provided that
(6.50) |
Thus (6.48) becomes
Now our choice of guarantees that the inner product is positive. Combining the above bound with its counterpart for the transport energy (this is where our choice (6.1) simplifies matters), we further obtain
(6.51) |
where
is still positive. Finally, we use the positivity of to estimate the two remaining terms on the right. Precisely, using the properties (6.23) of the multiplier in the definition of as well as the ellipticity of , respectively in the two components of , we have
Hence, applying the Cauchy-Schwarz inequality in (6.51) we finally obtain
(6.52) |
as desired.
This concludes the proof of (6.35), provided that the scales and were chosen so that the constraints (6.20),(6.40),(6.45),(6.46) are all satisfied. We recall them all here:
(6.53) | ||||
Then the parameters and can be chosen e.g. as follows:
-
(a)
set ,
-
(b)
take large enough so that the second constraint holds,
-
(c)
choose in the range given by the third constraint.
∎
4. Comparing the energies of and . To recall our setting here, the functions are defined in the domain and are localized at frequency scale, but cannot be though of as a state because does not vanish on the boundary . Instead we have
To rectify this, we decrease by a small constant and set
(6.54) |
so that the level set is fully contained within . Then we aim to prove that the energies do not change much:
Lemma 6.9.
We have the energy bound
(6.55) |
Proof.
We separate a boundary layer , with to be chosen later, where we verify directly that the norm on the left is . Outside this layer, we compare directly the associated good variables.
For the first step we use (6.37), which suffices if we impose the constraint (6.38), which we recall here
For the second step, we simply note that the good variables are identical except for the factors, where we replace by . Hence it suffices to ensure that
which yields
These two constraints for are again compatible if is large enough. The proof of the Lemma is concluded.
∎
Combining now the outcomes of Lemma 6.6 and Lemma 6.9, it follows that our final regularization satisfies the bound (6.8). It also satisfies (6.7) and (6.9) due to Lemma 6.4; there one can harmlessly substitute the weight by since are smooth on the scale, which is larger than . Thus the proof of Proposition 6.1 is concluded.
∎
6.3. Construction of regular exact solutions
Here we use the approximate solutions above. Given an initial data so that
applying the successive iterations above we obtain approximate solutions defined at steps, so that
By discrete Gronwall’s inequality, it follows that these approximate solutions are defined uniformly up to a time , with uniform bounds
(6.56) |
On the other hand, in a weaker topology we have
Hence by Arzela-Ascoli we get uniform convergence on a subsequence to a function in a norm, uniformly in . Passing to the limit in the relation (6.6), it follows that solves our equation. Finally, taking weak limits in the norms in (6.56) we also obtain an energy bound on ,
(6.57) |
7. Rough solutions
Our goal in this section is to construct rough solutions as limits of smooth solutions, and conclude the proof of Theorem 2. In terms of a general outline, the argument here is relatively standard, and involves the following steps:
-
(1)
We regularize the initial data,
-
(2)
We prove uniform bounds for the regularized solutions,
-
(3)
We prove convergence of the regularized solutions in a weaker topology,
-
(4)
We prove the convergence in the strong topology by combining the weak difference bounds with the uniform bounds in a frequency envelope fashion.
The main difficulty we face is that our phase space is not linear, and at each stage we have to compare functions on different domains. For a description of the ideas here in a simpler, model setting we refer the reader to the expository paper [12].
7.1. Regularizing the initial data
Given a rough initial data , our first task is to construct an appropriate family of regularized data, depending smoothly of the regularization parameter. Here it suffices to directly use the family of regularizations provided by Proposition 2.11.
7.2. Uniform bounds and the life-span of regular solutions
Once we have the regularized data sets , we consider the corresponding smooth solutions generated by the smooth data . A-priori these solutions exist on a time interval that depends on . Instead, we would like to have a lifespan bound which is independent of . To obtain this, we use a bootstrap argument for our control parameter for , which depends on and .
For a large parameter , to be chosen later, we will make the bootstrap assumption
(7.1) |
The solutions can be continued for as long as this is satisfied. We will prove that we can improve this bootstrap assumption provided that is small enough, , but with independent of . Here is finite but arbitrarily large; its role is simply to ensure that we run the bootstrap argument on finitely many quantities at once.
Our choice of will be quite straightforward,
(7.2) |
In view of our energy estimates in Theorem 3 and Gronwall’s inequality, this guarantees uniform energy bounds for the solutions in all integer Sobolev spaces in .
We remark that the bound (2.32) does not directly propagate unless is an integer. Indeed, in that case one could immediately close the bootstrap at the level of the norm using the embeddings (2.11) and (2.12). The goal of the argument that follows is to establish the bound for noninteger , by working only with energy estimates for integer indices.
Combining Theorem 3 with (2.33) we obtain the higher energy bound in
(7.3) |
Next we consider the bound (2.34), which we reinterpret in a discrete fashion as a difference bound
(7.4) |
This bound we can also propagate by Theorem 5, to obtain, also in , the estimate
(7.5) |
Our objective now is to combine the bounds (7.3) and (7.5) in order to obtain a uniform bound
(7.6) |
To prove this, we would naively like to consider a representation of the form
where we can estimate the successive terms in both and . The difficulty we face is that these functions have different domains. Hence the first step is to use the bounds (7.3) and (7.5) in order to compare these domains.
Lemma 7.1.
Assume that and are nondegenerate, and that (7.5) holds. Then we have
(7.7) |
Proof.
We use the uniform nondegeneracy property for the functions in order to compare these domains. If , then we can find a ball in the common domain so that
Then we obtain
or equivalently
Since , we obtain
∎
Now we return to our expansion for . In order to compare functions which are defined on a common domain, we replace the functions with their regularizations . Their domain includes an additional boundary layer, which by the previous Lemma 6.9 suffices in order to cover the domain for all . Then we write
and claim that this decomposition is as in Lemma 2.5.
The first term is trivial. For the last one we use the boundedness of in and the bound (2.39) integrated in to write
respectively
for a fixed large enough integer , which together suffice in order to place this term into , with norm .
For later use, we state the remaining bound for intermediate as a separate result:
Lemma 7.2.
For any nondegenerate with we have the difference bounds
(7.8) |
(7.9) |
As a corollary of this lemma, we remark that via Sobolev embeddings we also get uniform difference bounds:
Corollary 7.3.
In the region have
(7.10) |
This will serve later in the study of convergence of the regularized solutions.
Proof.
We split
For the first term we use again the boundedness of and then (2.39) to conclude that
and
as needed.
7.3. The limiting solution
Here we show that the limit
(7.11) |
exists, first in a weaker topology and then in the strong topology.
As before, the smooth solutions do not have common domains. However, by Lemma 7.1 the limit
exists, has a Lipschitz boundary , and further we have
For this reason, it is convenient to consider instead the limit
where the functions on the right are all defined in . Indeed, by Lemma 7.2 we see that we have convergence in , and, by interpolation, in for all .
To obtain convergence in , we write
and view the telescopic sum as a generalized Littlewood-Paley decomposition of . Then Lemma 7.2 shows that is in , with norm
(7.12) |
We also see that we have convergence in , namely
(7.13) |
We also show that we have strong convergence of in in the sense of Definition 2.6. Indeed, it suffices to compare it with the constant sequence . Then for we have
(7.14) |
The same relations also show the continuity of in as functions of time.
7.4. Continuous dependence
We consider a sequence of initial data which converges to in in the sense of Definition 2.6, and will show that the corresponding solutions converge to .
The first observation is that the convergence implies uniform boundedness for , which in turn implies a uniform lifespan bound for the solutions as well as a uniform bound in .
Our strategy to prove convergence is to compare this family of solutions with the limit via the regularizations used in the construction of rough solutions. Precisely, denote by respectively the regularized data sets, for which we have the obvious convergence
These are also uniformly bounded in and thus have a uniform lifespan.
Denoting by corresponding frequency envelopes for , we have the difference bounds
To finish the proof we need to establish two facts:
-
•
For each , the frequency envelopes can be chosen so that171717One can do better than that and ensure that the limit is zero, but that is not needed for our argument.
-
•
We have the convergence
(i) Equicontinuity of frequency envelopes. This is easily achieved via the decomposition
which holds for each . The smooth part yields envelopes which are uniformly decreasing, and the error term yields sized envelopes.
(ii) convergence. Here we have uniform bounds for the sequence , as well as weak convergence, in the sense that
The last property implies domain convergence. Then we have convergence away from a boundary layer, which in turn shows convergence of the regularizations in .
7.5. The lifespan of rough solutions
Here we complete the proof of our last result in Theorem 4. Thus, we consider a rough initial data and a corresponding solution in a time interval with the property that
(7.15) |
By the local well-posedness result, in order to prove the theorem it suffices to show that we have a uniform bound
(7.16) |
We consider the regularized data and the corresponding solutions . By the continuous dependence theorem we know that these solutions converge to in , and in particular their lifespans satisfy
What we do not have is a uniform bound for their corresponding control parameters . To rectify this, we consider a large parameter , to be chosen later, and we will show that, for , the solutions persist up to time with uniform bounds
(7.17) |
If that were the case, then by the local well-posedness proof it follows that the solutions remain uniformly bounded in and converge to , thereby concluding the proof.
To establish the bound (7.17) we will run a bootstrap argument. Precisely, we assume that on a time interval with we have a uniform bound
(7.18) |
Then we will show that in effect we must have the better bound
(7.19) |
That would suffice, for then the local well-posedness argument would yield a uniform for in and thus allow us to expand the interval on which the bootstrap assumption holds, uniformly with respect to .
Our goal now is to compare and . Precisely, we aim to show that
(7.20) |
with a universal constant but depending both on the initial data size and on above. This suffices in order to establish (7.19), because we are allowed to choose the threshold sufficiently large, depending on parameters which are fixed in the problem.
The tools we have at our disposal are
(ii) the difference bound (7.5).
The constants in both bounds depend exactly on the norm initial data and on above.
The difficulty we have in comparing and is that the two solutions are supported in different domains respectively . However, the difference bound (7.5) allows us to apply Lemma 7.1 to conclude that the two domains are at distance . Thus, rather than comparing and , it is better to compare their regularizations and , which are defined on enlargements of the domains, which in particular cover the union of and . By a slight abuse of notation, we will identify their domains.
We begin with , for which we have the straightforward bound
(7.21) |
This is where the universal constant appears.
Next we compare and . Here we take a telescopic sum,
Using the difference bound (7.5), we can estimate the successive terms in all norms,
which after summation yields
Now we can use Sobolev embeddings to conclude that181818From Sobolev embeddings we get in effect a bound for the first component.
(7.22) |
Finally, using (7.3), we compare with , estimating also the low frequencies,
Using Sobolev embeddings again, we conclude that
(7.23) |
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