Global solutions for the generalized SQG patch equation
Diego C\'ordoba, Javier G\'omez-Serrano, and Alexandru D. Ionescu

TL;DR
This paper proves the global stability of a specific patch solution for the generalized SQG equation with a more singular velocity, marking the first such stability result in this setting.
Contribution
It establishes the first global stability result for patch solutions of the generalized SQG equation with lpha ter 1, extending understanding of stable solutions beyond known rotating V-states.
Findings
Proves global stability of half-plane patch stationary solutions.
First construction of stable global solutions for gSQG patches.
Identifies the velocity's increased singularity for lpha ter 1.
Abstract
We consider the inviscid generalized surface quasi-geostrophic equation (gSQG) in a patch setting, where the parameter . The cases and correspond to 2d Euler and SQG respectively, and our choice of the parameter results in a velocity more singular than in the SQG case. Our main result concerns the global stability of the half-plane patch stationary solution, under small and localized perturbations. Our theorem appears to be the first construction of stable global solutions for the gSQG-patch equations. The only other nontrivial global solutions known so far in the patch setting are the so-called V-states, which are uniformly rotating and periodic in time solutions.
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Global solutions for the generalized SQG patch equation
Diego Córdoba
Instituto de Ciencias Matemáticas
,
Javier Gómez-Serrano
Princeton University
and
Alexandru D. Ionescu
Princeton University
Abstract.
We consider the inviscid generalized surface quasi-geostrophic equation (gSQG) in a patch setting, where the parameter . The cases and correspond to 2d Euler and SQG respectively, and our choice of the parameter results in a velocity more singular than in the SQG case.
Our main result concerns the global stability of the half-plane patch stationary solution, under small and localized perturbations. Our theorem appears to be the first construction of stable global solutions for the gSQG-patch equations. The only other nontrivial global solutions known so far in the patch setting are the so-called V-states, which are uniformly rotating and periodic in time solutions.
Keywords: patches, surface quasi-geostrophic equation, dispersion, modified scattering
The first two authors were supported in part by the grant MTM2014-59488-P (Spain) and ICMAT Severo Ochoa projects SEV-2011-008 and SEV-2015-556. The first author was supported in part by a Minerva Distinguished Visitorship at Princeton University. The second author was supported in part by an AMS Simons Travel Grant. Part of this work was done while some of the authors were visiting ICMAT and Princeton University, to which they are grateful for their support. The last author was supported in part by NSF grant DMS-1600028 and by NSF-FRG grant DMS-1463753.
1. Introduction
1.1. The gSQG equations
In this paper, we consider the generalized surface-quasigeostrophic equations (gSQG):
[TABLE]
where . The case corresponds to the surface quasi-geostrophic (SQG) equation and the limiting case refers to the 2D incompressible Euler equation. The case produces stationary solutions.
These are so-called active scalar equations, which have been originally introduced and studied in the setting of sufficiently smooth solutions . The equations (1.4) have also been analyzed extensively in the natural setting of the so-called -patches, which are solutions for which is a step function
[TABLE]
Here is a regular set given by the initial distribution of , and are constants, and is the evolution of under the induced velocity field.
In this case, the evolution of a patch can be determined by looking just at the evolution of its boundary, thus reducing the problem to a nonlocal one-dimensional equation for the boundary of . More precisely, the evolution equation for the interface of an -patch, which we parametrize as , , can be written as
[TABLE]
Here is an interval (usually in the case of bounded patches or for unbounded patches), the presence of the function has to do with the flexibility in parametrizing the curve, and the normalizing constant is given by
[TABLE]
1.1.1. Local regularity
The local regularity theory for the equations (1.4) and (1.8) is generally well understood, starting with the work of Constantin–Majda–Tabak [12] and Held–Pierrehumbert–Garner–Swanson [30]. As expected, data with sufficient smoothness lead to local in time unique solutions that propagate the regularity of the initial data (see for example Rodrigo [43], Gancedo [23], and Chae–Constantin–Cordoba-Gancedo–Wu [9] for some regularity results of this type).
Weak solutions have also been constructed, starting with the work of Resnick [42] on global weak solutions in in the SQG case . See also [40], [9], and [41] for more general classes of weak solutions. Very recently, Buckmaster–Shkoller–Vicol [4] proved lack of uniqueness of weak solutions for the SQG equation in certain spaces less regular than .
1.1.2. Dynamical formation of singularities
The problem of whether the SQG evolution can lead to finite time singularities is a challenging open problem both in the smooth case (1.4) and in the patch case (1.8).
In the smooth case (1.4), the early numerical simulations in [12] indicated a possible singularity in the form of a hyperbolic saddle closing in finite time. However, Córdoba [13] showed that such a scenario cannot actually lead to singularities, and bounded the growth by a quadruple exponential (see also [14] and [18]). The same scenario was recently revisited with bigger computational power and improved algorithms by Constantin–Lai–Sharma–Tseng–Wu [11], yielding no evidence of blowup and the depletion of the hyperbolic saddle past the previously computed times. More recently, Scott [45], starting from elliptical configurations, proposed a candidate that appears to develop filamentation and, after a few cascades, blowup of .
In the patch case (1.8), numerical simulations looking for singularities of the interface have been performed by different authors. There are at least two scenarios that suggest a possible formation of singularities. The first one (computed by Córdoba–Fontelos–Mancho–Rodrigo [15]), involves the evolution of two patches, and the simulation suggests an asymptotically self-similar singular scenario in which the distance between the two patches goes to zero in finite time while simultaneously the curvature of the boundaries blows up. Scott–Dritschel [46] started from an elliptical patch with a large ratio between its axes and found numerically that it may develop a self-similar singularity with a blowup of the curvature in the case . This is consistent with the rule out of splash singularities by Gancedo–Strain [24].
These recent simulations appear to suggest (convincingly) the possibility of dynamical formation of singularities. However, we emphasize that no rigorous results are known. The best result so far regarding fast growth is due to Kiselev–Nazarov [35], who constructed solutions that started arbitrarily small but grew arbitrarily large in finite time. More recently, Kiselev–Ryzhik–Yao–Zlatos [36] introduced a new gSQG-patch model, with a fixed boundary, and proved the formation of finite time singularities in this model for certain patches that touch the boundary at all times. At this point it is unclear whether such a scenario can lead to singularities in the classical gSQG models considered here.
1.1.3. Global regularity and rotating solutions
The construction of nontrivial global solutions for the gSQG equations is also a challenging problem, both in the smooth and in the patch case. In fact, the only non-stationary global solutions that are known in the patch setting are very special rotating solutions. These solutions, which are periodic in time and evolve by rotating with constant angular velocity around their center of mass, are known as V-states.
Deem–Zabusky [16] were the first to discover the V-states numerically in the patch case. Other authors have later improved the methods and numerically computed larger classes (see for example [49, 22, 39, 44]).
Hassainia–Hmidi [29] have rigorously proved the existence of V-states in the case . They were able to show the existence of convex V-states with boundary regularity. In [5], Castro–Córdoba–Gómez-Serrano were able to prove existence and regularity of convex global rotating solutions for the remaining open cases: for the existence, for the regularity. This boundary regularity was subsequently improved to analytic in [7].
The problem of constructing rotating periodic in time solutions is more challenging in the smooth case (1.4). Such solutions have only been constructed very recently by Castro–Córdoba–Gómez-Serrano [6] who found a smooth 3-fold solution that rotates uniformly (both in time and space) by perturbing from a smooth annular profile. See also [8]. We remark that Dritschel [21] had constructed nontrivial global rotating solutions with regularity.
1.2. The main theorem
Our goal in this paper is to initiate the study of stable global solutions of the equations (1.4) and (1.8). Such stable solutions cannot be periodic in time and their construction requires a different mechanism.
A natural way to look for families of global stable solutions is to perturb around certain explicit stationary solutions of the equation. This approach has been successful to produce nontrivial global solutions for many difficult quasilinear evolutions, such as the Einstein-vacuum equations, plasma models, or water-wave models. In the case of time reversible equations the main mechanism that sometimes leads to global solutions is the mechanism of dispersion.
In our case of the gSQG equations, one could start by perturbing around the trivial solution of the equation (1.4). However, there is no source of dispersion in this case and it is not clear to us how to control the solution beyond the natural time of existence corresponding to data of size .
One could also start from the observation that all radial functions are stationary solutions of the gSQG equations, and look for global solutions that start as small perturbations of radial functions. A natural such problem would be to consider the gSQG-patch equation (1.8), and start with data that is a small perturbation of the characteristic function of a disk. Numerical simulations in this case seem to suggest the existence of long-term (perhaps global) smooth solutions for the gSQG-patch equation (1.8), starting from certain small perturbations of a characteristic function of a ball of radius . So far, however, we have not been able to analyze this scenario rigorously.
In this paper we consider a simpler scenario, namely we perturb around the half-plane stationary solution corresponding to the straight interface
[TABLE]
For simplicity, we will assume that , and . This choice yields the following equation for :
[TABLE]
We will consider solutions that decay at , so the integral in (1.9) is well defined for .
At the linear level, the dynamics of solutions of (1.9) are determined by the equation
[TABLE]
where is the Fourier transform of and is a constant. We notice that this linearized equation has dispersive character, due to the dispersion relation , which is related to the stationary solution we perturb around. Thus one can hope to prove global regularity and decay. This is precisely our main theorem:
Theorem 1.1**.**
Assume , and let and . Then there is a constant such that for all initial-data satisfying the smallness conditions
[TABLE]
there is a unique global solution of the evolution equation (1.9) with . Moreover, the solution satisfies the slow growth energy bounds
[TABLE]
where is the scaling vector-field associated to the linear equation (1.10) and , and the sharp pointwise decay bounds
[TABLE]
where denote the standard Littlewood-Paley projections and .
Our proof provides more information about the global solution as part of the bootstrap argument. In fact, the solution satisfies the main bounds (2.40) in Proposition 2.6. At a qualitative level, the solution remains uniformly bounded in a suitable -norm and undergoes nonlinear (modified) scattering as . See the discussion in subsection 1.3 below.
1.3. Main ideas of the proof
The equation (1.9) is a time reversible quasilinear equation. The classical mechanism to prove global regularity in such a situation has two main steps:
- (1)
Prove energy estimates to propagate control of high order Sobolev and weighted norms;
- (2)
Prove dispersion and decay of the solution over time.
The interplay of these two aspects has been present since the seminal work of Klainerman [37, 38] on nonlinear wave equations and vector-fields, Shatah [47] and Simon [48] on d Klein-Gordon equations and normal forms, Christodoulou-Klainerman [10] on the stability of the Minkowski space-time, and Delort [17] on d Klein-Gordon equations.
In the last few years new methods have emerged in the study of global solutions of quasilinear evolutions, inspired by the advances in semilinear theory. The basic idea is to combine the classical energy and vector-fields methods with refined analysis of the Duhamel formula, using the Fourier transform and carefully constructed “designer” norms. This is the main idea of the “method of space-time resonances” of Germain-Masmoudi-Shatah [25, 26] and Gustafson-Nakanishi-Tsai [28], and of the work on plasma models and water wave models of the last author and his collaborators, in [31, 27, 19, 33, 34, 32, 20].
We describe now in some detail these two main aspects of our proof.
1.3.1. Energy estimates
We would like to control the growth in time of two energy-type quantities: the high order Sobolev norms of our solutions and their weighted norms. More precisely, we would like to prove that the solution satisfies energy bounds with slow growth of the form
[TABLE]
where is the scaling vector-field associated to the linearized equation, and . For this we use a paradifferential reduction, similar to the idea used recently in the study of water-wave models in [1, 2, 3, 32, 20].111Alternatively, one could try to use a change of variables as in [23]. This works well to control the Sobolev norms, but seems to lead to problems in the analysis of the weighted norms involving the vector-field . Because of this we prefer to use here the more robust paradifferential approach. We examine the equation (1.9) and start by rewriting it using paradifferential calculus in the form
[TABLE]
Here is as in (1.10), is an explicit symbol of order , which depends quadratically on , is the paradifferential operator in Weyl quantization (see subsection 2.3 for definitions and simple properties), and is a suitable error term that satisfies cubic bounds in and does not lose derivatives (relative to ).
The formula (1.15) gives a good idea about the structure of the nonlinearity, but is not completely adequate to prove energy estimates. This is because the symbol in not real-valued, thus the operator is not self-adjoint. In fact, can be written in the form
[TABLE]
where and are real-valued symbols of order and , and is a purely imaginary symbol of order . To prove energy estimates we need one more step. Precisely, we define the renormalized variable (the so-called “good variable”) by , for a suitable symbol of order [math]. This symbol is constructed in such a way that the good variable satisfies a better evolution equation of the form
[TABLE]
The resulting error term still satisfies good cubic bounds with no derivative loss.
The equation (1.16) is now suitable to prove energy bounds, first for the good variable , and then for the original variable . The only additional ingredient that is needed to prove the bounds (1.14) is sharp pointwise decay of the solution, i.e an estimate of the form
[TABLE]
This follows from the main bootstrap assumption and linear estimates.
1.3.2. Dispersion and decay
To close the bootstrap argument we need to prove dispersion, in a sufficiently precise way so as to be able to recover the sharp pointwise decay bounds (1.17). Since all the energy estimates have a small loss, this requires an independent argument, which does not rely directly on these energy estimates.
We use the -norm method. More precisely, we define a suitable norm, called the -norm, in such a way that is uniformly bounded as ,
[TABLE]
The precise choice of the -norm is important, since control of the -norm has to complement suitably the energy control proved in the first step. Here we use a type of norms introduced recently in 2D water-wave models by Ionescu–Pusateri [33, 34, 32],
[TABLE]
To prove (1.18) we start by defining the linear profile of the solution . Then we write the Duhamel formula in terms of the profile . The main contribution comes from the cubic nonlinear term
[TABLE]
where and is a suitable multiplier.
This term is not integrable in time, due to the contribution of the space-time resonances. To eliminate these contributions we need to add a nonlinear correction to the profile . More precisely, we define the (modified) nonlinear profile by the formulas
[TABLE]
where is a suitable function (see (4.6) for the precise formulas). Then we show that the nonlinear profile converges in the -norm as , at a suitable rate, and prove the uniform bounds (1.18).
1.4. Organization
The rest of the paper is concerned with the proof of Theorem 1.1. In section 2 we introduce the main notation, define the -norm, prove some important lemmas, and state the main bootstrap Proposition 2.6.
In the remaining two sections we prove Proposition 2.6, along the lines described above. In section 3 we prove the energy estimates, using paradifferential calculus, while in section 4 we prove the dispersive estimates, using the Duhamel formula and Fourier analysis.
2. Preliminaries and the main bootstrap proposition
2.1. Notation and basic lemmas
In this subsection we summarize some of our main notation and recall several basic formulas and estimates. We fix an even smooth function supported in and equal to in , and define
[TABLE]
for any . Let , , and the operators defined by the Fourier multipliers , , and respectively. For any interval let
[TABLE]
For any let
[TABLE]
2.1.1. Multipliers and associated operators
We will often work with multipliers or , and operators defined by such multipliers. We define the class of symbols
[TABLE]
We summarize below some properties of multipliers and associated operators (see [33, Lemma 5.2] for the proof).
Lemma 2.1**.**
(i) We have . If then and
[TABLE]
Moreover, if , is an invertible linear transformation, , and then
[TABLE]
(ii) Assume satisfy , and . Then, for any ,
[TABLE]
In particular, if then
[TABLE]
(iii) More generally, if , satisfy , and then
[TABLE]
where
[TABLE]
and .
Moreover, if are suitable functions defined on and is the scaling vector-field then
[TABLE]
where
[TABLE]
2.1.2. An interpolation lemma
We will use the following simple lemma, see [34, Lemma 4.3] for the proof.
Lemma 2.2**.**
For any , and we have
[TABLE]
2.1.3. A dispersive estimate
The following lemma is our main linear dispersive estimate:
Lemma 2.3**.**
Assume that as before. Then, for any , , and we have
[TABLE]
and
[TABLE]
Proof.
This is similar to the proof of Lemma 4.2 in [34]. For (2.10) it suffices to prove that
[TABLE]
for any and . The left-hand side of (2.12) is clearly bounded by . Therefore in proving (2.12) we may assume .
Let and notice that
[TABLE]
If in the support of the integral in the left-hand side of (2.12) then integrate by parts in to estimate this integral by
[TABLE]
which suffices to prove (2.12), in view of the assumption .
It remains to prove the bound (2.12) when for some with . This is possible only if . Let denote the solutions of the equation , i.e.
[TABLE]
and notice that . We estimate
[TABLE]
where, for any ,
[TABLE]
Clearly
[TABLE]
On the other hand, since in the support of the integral defining , if then we can integrate by parts to estimate
[TABLE]
This suffices to control the sum of over as claimed in (2.12). The full bound (2.12) follows using also (2.14) and (2.15).
To prove the dispersive bound (2.11) we notice that where
[TABLE]
Clearly, . It follows from (2.12) that . The dispersive bound (2.11) follows by considering the two cases and . ∎
2.2. Linearization and expansion of the nonlinearity
Recall the main equation (1.9). To linearize it we write
[TABLE]
where
[TABLE]
and
[TABLE]
We examine first the linear part, and notice that
[TABLE]
An easy calculation shows that where
[TABLE]
Using the formal expansion formula
[TABLE]
where , we write
[TABLE]
where
[TABLE]
Since
[TABLE]
we can symmetrize and rewrite in the Fourier space in the form
[TABLE]
where and
[TABLE]
We will show later, in Lemma 3.3, that the multipliers , , are real-valued, odd, and homogeneous of degree . They also satisfy suitable symbol-type bounds in which allow us to estimate the associated multilinear operators.
2.3. Weyl paradifferential calculus
We will use paradifferential calculus in section 3 to prove high order energy estimates. In this subsection we summarize the results we need, which are all standard. We refer the reader to [20, Appendix A] for the (elementary) proofs.
We recall first the definition of paradifferential operators (Weyl quantization): given a symbol , we define the operator by
[TABLE]
where denotes the partial Fourier transform of in the first coordinate and . We define the Poisson bracket between two symbols and by the formula
[TABLE]
For and we define as the space of symbols defined by the norm
[TABLE]
The index is called the order of the symbol, and it measures the contribution of the symbol in terms of derivatives on . Notice that we have the simple product rule
[TABLE]
An important property of paradifferential operators is that they behave well with respect to products. More precisely:
Lemma 2.4**.**
(i) If and , and then
[TABLE]
(ii) Assume satisfy , , and , are symbols, . Then
[TABLE]
and
[TABLE]
The point of these bounds is the gain of one derivative in (2.30) and the gain of 2 derivatives in the more precise formula (2.31).
With (the scaling vector-field), notice that we have the identities
[TABLE]
We record below some simple properties of paradifferential operators.
Lemma 2.5**.**
(i) If is real-valued then is a bounded self-adjoint operator on . Moreover,
[TABLE]
(ii) For suitable functions defined on and symbols defined on we have
[TABLE]
These properties follow easily from definitions; for (2.34) one uses also the identities (2.32) and integration by parts in .
2.4. The -norm and the main bootstrap proposition
For any function let
[TABLE]
where and . Our main Theorem 1.1 follows, by local existence theory and a continuity argument, from the following main proposition:
Proposition 2.6** (Main bootstrap).**
Assume that ,
[TABLE]
Assume and h\in C\big{(}[0,T]:H^{N_{0}\alpha}\big{)} is a real-valued solution of the system (1.9). Let denote the linear profile of the solution,
[TABLE]
Recall that . Assume that, for any ,
[TABLE]
where . Assume also that the initial data satisfy the stronger bounds
[TABLE]
Then the solution satisfies the improved bounds, for any ,
[TABLE]
We notice that the assumption (2.39) implies the desired bounds (2.40) at time , using also Lemma 2.2. The rest of the paper is concerned with proving the bounds (2.39) at all times . This is done in two steps, in Propositions 3.1 and 4.1.
3. Energy estimates
In this section we prove the following proposition.
Proposition 3.1**.**
With the assumptions in Proposition 2.6, we have, for any ,
[TABLE]
The rest of the section is concerned with the proof of this proposition. We start with two lemmas, concerning pointwise decay of the solution and bounds on the multipliers . The main step is to rewrite the nonlinearity in paradifferential form, in Lemma 3.4. Then we construct a suitable renormalization of the variable and prove the desired energy bounds.
3.1. Two lemmas
We start by proving sharp pointwise decay bounds on .
Lemma 3.2**.**
For any and we have
[TABLE]
Proof.
We may assume and let . We use Lemma 2.3 with to show that
[TABLE]
and
[TABLE]
It follows from (2.38) that
[TABLE]
Therefore
[TABLE]
Since , see (2.36), this is enough to show that
[TABLE]
Combining (3.4), with Lemma 2.2, and (3.5) we see that
[TABLE]
It follows that
[TABLE]
The desired bounds (3.2) follow from (3.6) and (3.7). ∎
We record now some properties of several multipliers that are important in the analysis.
Lemma 3.3**.**
(i) The multipliers defined in (2.24) are real-valued, odd, and homogeneous of degree ,
[TABLE]
(ii) For any and let
[TABLE]
Let and . Then
[TABLE]
for some constant . Moreover, if and then
[TABLE]
(iii) Let
[TABLE]
The multipliers are real-valued and homogeneous of degree , and satisfy the bounds
[TABLE]
Proof.
(i) This is a consequence of the definitions (alternatively, one can use the formula (3.32) derived below).
(ii) We write, using the formula (2.24),
[TABLE]
where is a constant, is the inverse Fourier transform of , and is its derivative. We notice that if and then
[TABLE]
Therefore, using also that ,
[TABLE]
where (here and in the rest of the paper) means that there is a constant such that . This gives the desired bounds (3.10).
To prove (3.11) we notice that differentiation corresponds to multiplication by . Then we notice that if then
[TABLE]
Therefore, estimating as before,
[TABLE]
(iii) We start from the formula
[TABLE]
which follows from (2.19). Therefore
[TABLE]
where . Using (3.15) it follows that
[TABLE]
as desired. ∎
3.2. Paradifferential formulation
The main issue when proving energy estimates is to avoid the potential loss of derivative. We do this here using a paradifferential reduction. Our next lemma is the main step in the proof of Proposition 3.1.
Lemma 3.4**.**
We have
[TABLE]
where
(i) The error term satisfies the bounds
[TABLE]
(ii) The symbol decomposes as
[TABLE]
where , , and are symbols of order , , and given by
[TABLE]
[TABLE]
[TABLE]
where , are defined as in (3.12), and
[TABLE]
The symbols and are real-valued and, see also definitions (2.27) and (2.34),
[TABLE]
Proof.
We use the formulas (2.23). The idea is to extract ”error” terms that can be estimated like in (3.18), and identify the main contributions to the symbols in . Most of the bounds we prove rely on the symbol bounds (3.10) and (3.13), Lemma 2.1, and the bounds on ,
[TABLE]
These bounds follow from the bootstrap assumptions (2.38) and Lemma 3.2.
Step 1. We bound first the contribution when the two highest frequencies are proportional. For we define the multilinear operators by
[TABLE]
Notice that , see (2.23). For let
[TABLE]
Let
[TABLE]
where is the second larger of the numbers . We will show that
[TABLE]
We use (2.6), (3.10), and (3.25). Assuming, for example, that , we estimate
[TABLE]
Thus
[TABLE]
To estimate we use also the identities (2.7)–(2.8). In our case, since is homogeneous, see (3.8), we have
[TABLE]
Estimating as before, with the term containing the vector-field in and the others in , and noticing that we have
[TABLE]
for any . The desired conclusion (3.29) follows.
It remains to control the contribution of . Notice that, by symmetry,
[TABLE]
Step 2. To deal with the contribution of (3.31) we derive first more favorable formulas for the multipliers . Using the mean value theorem
[TABLE]
We recall the following identity for ,
[TABLE]
We use these identities with and , together with (2.24). Thus
[TABLE]
where .
Assume that
[TABLE]
Let . The formula (3.32) gives
[TABLE]
where, with as in (2.19),
[TABLE]
Integrating in we obtain
[TABLE]
We write
[TABLE]
and decompose the multipliers accordingly. Thus let
[TABLE]
[TABLE]
[TABLE]
[TABLE]
where .
Notice that
[TABLE]
The multipliers , , and will essentially generate the symbols , , and in (3.19). The multipliers will only add contributions in the error term .
Step 3. As in (3.26), for we define the multilinear operators by
[TABLE]
We examine the formula (3.31) and define, for ,
[TABLE]
Clearly,
[TABLE]
We have already seen, as a consequence of (3.29), that the contribution of the terms can be incorporated into the error term . The contribution of can also be incorporated into this error term because
[TABLE]
Indeed, these bounds follow as in the proof of (3.29). We only need to notice that the symbols are homogeneous of order and do not lose derivatives, i.e.
[TABLE]
see (3.38), where and .
Step 4. We consider now the leading contributions, corresponding to the functions . We define the symbols and , by
[TABLE]
where, with and defined as in (3.23),
[TABLE]
See also subsection 2.3 for the notation related to paradifferential calculus. We notice that the symbols are real-valued (thus the operators are self-adjoint), but the symbols are not real-valued. Notice also that , compare with (3.20).
We define
[TABLE]
and we will prove that are acceptable errors, i.e.
[TABLE]
Indeed, we start from the formula
[TABLE]
where . This follows from the definitions (3.35), (3.39)–(3.40), and a change of variables. With we notice that we may replace the factor in (3.47) with at the expense of an error , which leads to error terms satisfying (3.46). Thus we may replace with , where
[TABLE]
Finally, we compare the symbols and . Notice that if then
[TABLE]
It is easy to see that
[TABLE]
see definitions (2.27), using the fact that is nontrivial only when at least one the factors of has frequency . The bounds (2.29) and the identities (2.34) show that
[TABLE]
This completes the proof of (3.46).
Step 5. We consider now the contributions corresponding to the functions . We define the symbols by
[TABLE]
where are are defined as in (3.23) and (3.12). The multipliers satisfy the properties summarized in Lemma 3.3 (iii). As in Step 4 it is not hard to see that the error terms satisfy bounds similar to (3.46). In other words, one can replace with at the expense of acceptable errors.
Step 6. We consider the remaining contributions corresponding to the functions . Let
[TABLE]
where is as in (3.44). As in Step 4 the error terms satisfy bounds similar to (3.46), so one can replace with at the expense of acceptable errors.
Finally, we notice that the symbols (defined in (3.43)) and combine to produce the symbols defined in (3.22). The bounds (3.24) follow directly from the definitions (2.27), the pointwise bounds (3.2), and the bootstrap assumptions (2.38). This completes the proof of the lemma. ∎
3.3. The normalized variable
We would like to use Lemma 3.4 to prove energy estimates. To do this directly we would need the operator to be self-adjoint, which is equivalent to the symbol being real-valued. This is true for the symbols and , but not for the symbol . We correct this by introducing the so-called “good variable” .
We define the symbol by the formula
[TABLE]
where the symbols are as in (3.23). Notice that
[TABLE]
Lemma 3.5**.**
Let
[TABLE]
Then we have
[TABLE]
where the symbols and are defined as in (3.20)–(3.21). The functions satisfy the bounds
[TABLE]
and
[TABLE]
Proof.
We apply to the equation (3.17), so
[TABLE]
Notice that , , and are symbols of order [math],
[TABLE]
where . This shows that and are acceptable error terms satisfying (3.55). Moreover, the bounds (3.54) hold, using also (3.25).
To prove the desired identity (3.53) it suffices to show that the term
[TABLE]
is an error type term satisfying (3.55). In view of Lemma 2.4, we may replace the expression above by
[TABLE]
at the expense of acceptable errors. Finally, we notice that the choice of the symbol in (3.52) is such that is a symbol of order [math], satisfying bounds similar to (3.57), so the expression in (3.58) is again a suitable error term. The conclusion of the lemma follows. ∎
3.4. The improved energy bounds
We can now prove the bounds in Proposition 3.1.
Lemma 3.6**.**
With the assumptions in Proposition 2.6, we have, for any ,
[TABLE]
Proof.
We divide the proof in several steps. Let .
Step 1. We prove first suitable bounds for , i.e.
[TABLE]
For this we start from the identities (3.53), written in the form , recall that the operators are self-adjoint, and apply energy estimates,
[TABLE]
Notice that, for ,
[TABLE]
as a consequence of Lemma 2.4 (i), the bootstrap assumptions (2.38), and the symbol bounds. Thus the right-hand side of (3.61) is dominated by . We integrate in time and use the initial-time bound to prove the first inequality in (3.60).
The proof of the weighted bound in (3.60) is similar. Since , it follows from (3.53) that
[TABLE]
As before, we apply the operators , , and derive the identities
[TABLE]
It follows from Lemma 2.4 (i) and the bootstrap assumptions (2.38) that
[TABLE]
and
[TABLE]
for any . Thus the right-hand side of (3.62) is dominated by , and the second bound in (3.60) follows by integration in time.
Step 2. We can prove now the bounds (3.59), using just elliptic estimates. The bounds (3.60), together with the simple identities
[TABLE]
and the symbol bounds (3.24), show that
[TABLE]
The desired conclusions (3.59) follow once we recall that and use (3.57). ∎
Lemma 3.7**.**
With the assumptions in Proposition 2.6, we have, for any ,
[TABLE]
Proof.
Notice that
[TABLE]
using (2.16) and the definition . Notice also that
[TABLE]
which is a simple consequence of the identity . Since we have already proved that , for (3.63) it suffices to show that
[TABLE]
This follows from (3.64) and Lemma 3.4. ∎
4. Modified scattering and pointwise decay
In this section we prove the following:
Proposition 4.1**.**
With the assumptions in Proposition 2.6, we have, for any ,
[TABLE]
The rest of the section is concerned with the proof of this proposition. The analysis is more subtle here, and we need to differentiate between the cubic nonlinearity , which contributes to modified scattering, and the remaining quintic and higher order terms.
4.1. Modified scattering
We rewrite in terms of the profile ,
[TABLE]
using (2.23) and the formula . The formula (3.64) becomes
[TABLE]
where
[TABLE]
In analyzing the formula (4.3), the main contribution comes from the stationary points of the phase function , where
[TABLE]
More precisely, one needs to understand the contribution of the spacetime resonances, i.e., the points where
[TABLE]
In our case, it is easy to see that the only spacetime resonances correspond to . Moreover, the contribution from these points is not absolutely integrable in time, and we have to identify and eliminate its leading order term using a suitable logarithmic phase correction. More precisely, we define
[TABLE]
The formula (4.3) then becomes
[TABLE]
Notice that the phase is real-valued. Therefore, to complete the proof of Proposition 4.1, it suffices to prove the following main lemma:
Lemma 4.2**.**
For any and any , we have
[TABLE]
4.2. Proof of Lemma 4.2
In this subsection we provide the proof of the more technical Lemma 4.2. We first notice that the desired conclusion follows easily for large and small enough frequencies. Indeed, for any and with and
[TABLE]
we can use the interpolation inequality (2.9), the bounds (3.1), and the assumption to obtain
[TABLE]
It remains to prove (4.8) in the intermediate range . For let . For any , let
[TABLE]
Using (2.38) and Lemma 3.2 we know that for any , , and
[TABLE]
whereas, for ,
[TABLE]
Since is real-valued, we have . In view of (4.7), to complete the proof of Lemma 4.2 it suffices to prove the following:
Lemma 4.3**.**
Assume that , , , , and . Then
[TABLE]
Moreover
[TABLE]
4.2.1. Proof of (4.12)
We start with the cubic bound and consider several cases.
Lemma 4.4**.**
The bound (4.12) holds provided that
[TABLE]
Proof.
For we estimate, using Lemma 2.1 (iii) and (3.10),
[TABLE]
for any choice of satisfying . Assume, without loss of generality, that . We set , . Using (4.10)–(4.11) and noticing that we may assume , the right-hand side of (4.15) is dominated by
[TABLE]
Assuming that (4.14) holds, it follows that
[TABLE]
The contribution of the other terms, which contain the symbol , can be estimated easily using the last bounds in (4.10)–(4.11). This suffices to prove the desired conclusion (4.12) in this case. ∎
Lemma 4.5**.**
The bound (4.12) holds provided that
[TABLE]
Proof.
In this case we will show the stronger bound
[TABLE]
Without loss of generality (using changes of variables) we may assume that , . Then
[TABLE]
in the support of the integral. Therefore we can integrate by parts in in the integral expression (4.9) for . This gives
[TABLE]
where
[TABLE]
and
[TABLE]
Using (3.10) and (4.18) it is easy to see that
[TABLE]
We can estimate and as in (4.15), using (4.10)-(4.11) and the bound ,
[TABLE]
A similar estimate shows that . Moreover, using also (3.11),
[TABLE]
and can be bounded similarly. This completes the proof of (4.17) and the lemma. ∎
It remains to consider the case
[TABLE]
Without loss of generality, in proving (4.12) we may assume that , . We decompose the integrals as
[TABLE]
where , , . Notice that . We estimate the remaining contributions in the next two lemmas.
Lemma 4.6**.**
With the hypothesis of Lemma 4.3, and assuming that (4.22) holds, we have
[TABLE]
for .
Proof.
We will only prove the bound for the integral , since the other bounds are similar. We integrate by parts in . The main observation is that
[TABLE]
if . Therefore
[TABLE]
in the support of the integral defining . Due to this lower bound we can integrate by parts in to obtain
[TABLE]
where
[TABLE]
In view of (4.25) we may insert a factor of in the integrals above, for some constant . Let denote the inverse Fourier transform of , so
[TABLE]
It follows that
[TABLE]
We use the estimate, as in (4.15), for and the rapid decay of the function for . Recalling also the constraints (4.22), it follows that, for any ,
[TABLE]
Similar estimates, using also the bounds , see (3.66), show that
[TABLE]
Finally, using the definition (4.6),
[TABLE]
The desired bound follows from (4.26). ∎
Lemma 4.7**.**
With the hypothesis of Lemma 4.3, and assuming that (4.22) holds, we have
[TABLE]
Proof.
We prove only the bound on , since the other two bounds are similar. We examine the integral defining , see (4.23); we would like to show that the main contribution in this integral comes from a suitable neighborhood of the point .
Let denote the smallest integer with the property that . For integers we define the functions by if and if . Then we decompose
[TABLE]
[TABLE]
For (4.28) it suffices to show that
[TABLE]
and
[TABLE]
Proof of (4.31). Since and , we have
[TABLE]
in the support of the integral defining . Moreover, using (3.11),
[TABLE]
Therefore
[TABLE]
For (4.31) it remains to prove that if then
[TABLE]
For this we make the change of variables , . Recalling that we notice that
[TABLE]
in the support of the integral. After changes of variables, and recalling that , see (4.6), for (4.34) it suffices to prove that
[TABLE]
where .
To prove (4.35) we start from the general identity
[TABLE]
Then we estimate, for ,
[TABLE]
Set . Since , using integration by parts either in or in , we have
[TABLE]
Therefore
[TABLE]
and the desired conclusion (4.35) follows. This completes the proof of (4.31).
Proof of (4.32). Without loss of generality we may assume that . We make the change of variables , , thus
[TABLE]
We would like to integrate by parts in . For this we notice that
[TABLE]
in the support of the integral. We integrate by parts in , as in the proof of Lemma 4.5, and estimate
[TABLE]
where, with ,
[TABLE]
and
[TABLE]
We keep fixed and would like to use (2.5). In view of (3.10), if then
[TABLE]
Moreover, using (4.10)–(4.11),
[TABLE]
Therefore, using (2.5),
[TABLE]
A similar argument gives . To bound we also use (2.5), and replace the bounds in (4.40) by
[TABLE]
and the bound in (4.39) by
[TABLE]
It follows that
[TABLE]
This completes the proof of (4.32). ∎
4.2.2. Proof of (4.13)
We estimate now the contribution of the quintic and higher order nonlinearities.
Lemma 4.8**.**
For any we have
[TABLE]
Proof.
It suffices to prove that, for any ,
[TABLE]
for some constant . We use the formula (2.22). We notice that if then
[TABLE]
for any function and . The bootstrap assumptions (2.38) and the pointwise bounds (3.2) show that
[TABLE]
for any (the last bound follows from the estimates and ). The bounds (4.42) follow from (4.43)–(4.44) and the definitions. Indeed, let denote the contribution of in (2.22). For we use the estimate (4.43) with , and estimate one of the factors in and the others in (for the vector-field bound we estimate the factor that carries the vector-field in ). It follows that
[TABLE]
which gives gives the desired bound for the contribution of . The contribution over can be bounded in a similar way: we estimate one of the factors using the bound in (4.43), and the remaining factors using the bound. The bound (4.42) follows. ∎
We turn now to the proof of (4.13). Assume that , , , . We would like to prove that
[TABLE]
Let
[TABLE]
In view of Lemma 2.2, it suffices to prove that
[TABLE]
Since , see the first inequality in (4.41), it suffices to prove that
[TABLE]
To prove (4.47) we write
[TABLE]
where
[TABLE]
Using (4.41) again we have
[TABLE]
Moreover, using integration by parts in and the bound \big{|}\partial_{s}\big{[}e^{iL(\xi_{0},s)}\big{]}\big{|}\lesssim 2^{-9m/10}, see the definition (4.6), we can also estimate . The desired bound (4.47) follows.
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