Abstract
We construct mixing solutions to the incompressible porous media equation starting from Muskat type data in the partially unstable regime. In particular, we consider bubble and turned type interfaces with Sobolev regularity. As a by-product, we prove the continuation of the evolution of IPM after the Rayleigh–Taylor and smoothness breakdown exhibited in (Castro et al. in Arch Ration Mech Anal 208(3):805–909, 2013, Castro et al. in Ann Math. (2) 175(2):909–948, 2012). At each time slice the space is split into three evolving domains: two non-mixing zones and a mixing zone which is localized in a neighborhood of the unstable region. In this way, we show the compatibility between the classical Muskat problem and the convex integration method.
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1 Introduction and Main Results
We consider two incompressible fluids with different constant densities \(\rho _{-}\), \(\rho _{+}\) and equal viscosity \(\mu \), separated by a connected curve \(z^\circ =(z_1^\circ ,z_2^\circ )\) inside a 2D porous medium with constant permeability \(\kappa \) (or Hele-Shaw cell [67]) and under the action of gravity \(-g (0,1)\). As we deal with closed and open curves, it is convenient to fix an orientation for \(z^\circ \). For closed curves we fix the clockwise orientation (\(\circlearrowright \)) and for open curves the orientation from \(x_1=-\infty \) to \(+\infty \). Then, we denote \(\Omega _{-}^\circ \) (\(\Omega _{+}^\circ \)) by the domain to the left (right) side of \(z^\circ \). Thus, the initial density will be written as
for \(x=(x_1,x_2)\in {\mathbb {R}}^2\). It is widely accepted that the dynamic of this two-phase flow can be modelled by the Incompressible Porous Media (IPM) system
where \(\rho (t,x)\) \(\equiv \) density, v(t, x) \(\equiv \) velocity field, p(t, x) \(\equiv \) pressure. By normalizing, we may assume w.l.o.g. that \(|\rho _{\pm }|=\mu =\kappa =g=1\).
The investigations on the Muskat problem ([62]) which deals with the interface evolution under the assumption of immiscibility, have been very intense both in the applied community due to the many applications (see e.g. [48, 53, 72, 73]) and in the theoretical side as this constitutes a challenging free boundary problem.
Mathematically, the theory has bifurcated into two regimes, the so-called stable regime and unstable regime. This division arises from the linear stability analysis of the equation for the interface evolution. It is classical (see e.g. [28]) that such linear stability is characterized by the sign of the Rayleigh–Taylor function \(\sigma :=(\rho _{+}-\rho _{-})\partial _{\alpha }z_1^\circ \) as follows:
This simply classifies whether the heavier fluid remains (locally) below the lighter one or not. If the initial interface is a graph, \(z^\circ (\alpha )=(\alpha ,f^\circ (\alpha ))\), the interface evolution is governed by a a nonlinear parabolic equation, which can be linearized as \(\partial _tf=(\rho _{+}-\rho _{-})(-\Delta )^{1/2}f\). Hence, the stability simply depends on the sign of the density jump \(\rho _{+}-\rho _{-}\). Therefore, for \(\rho _{+}>\rho _{-}\) (i.e. the heavier fluid is below \(z^\circ \)) what is called the fully stable regime, the analogy with the heat equation gives hope of well-posedness theory in a suitable Sobolev space \(H^k\). We refer to the corresponding weak solutions to IPM as non-mixing solutions (see [6, 28, 31, 69, 74] for initial results). In the last years there have taken extensive steps to reduce the initial k (see [2, 20, 26, 56, 63]). The current world record is the result of Alazard and Nguyen [3] where they have proved the critical case \(k=3/2\) (see also [4, 5]). For small enough initial data these solutions are global-in-time. Additional results of global well-posedness for medium size initial data can be found in [24, 25] and global solutions with large initial slope in [15, 32, 39].
The instability in the linearization is called Rayleigh–Taylor (or Saffman–Taylor [67]) for the Muskat problem. In the graph case, it corresponds to \(\rho _{+}<\rho _{-}\) (i.e. the heavier fluid is above \(z^\circ \)) what is called the fully unstable regime, and the analogy is now with the backwards heat equation. Therefore, it is to be expected that the problem is ill-posed unless the initial data is real-analytic \(C^\omega \). As a matter of fact, all the techniques available in the stable case catastrophic fail in this situation. Indeed, it can be proved that in the fully unstable regime, \(\sigma (\alpha ) \le 0\) for every \(\alpha \), the Cauchy problem for f is ill-posed in Sobolev spaces (see e.g. [69]). However, practical and numerical experiments show the existence of the so-called mixing solutions, solutions in which there exist a mixing zone where the two fluids mix stochastically (see e.g. [48, 73]). Numerically, it can be seen that small disturbances of an analytic initial interface increases rapidly creating finger patterns at different scales in the unstable region (see e.g. [53, 72] and Fig. 1).
In spite of the fact that the linearized problem is ill-posed and in accordance with what is observed in the experiments, weak solutions to IPM, in the fully unstable case, have been constructed in the last years by replacing the continuum free boundary assumption with the opening of a mixing zone \(\Omega _{\mathrm {mix}}\) where the fluids begin to mix indistinguishably. These mixing solutions \((\rho ,v)\) are recovered by the convex integration method applied in \(\Omega _{\mathrm {mix}}\) to a so-called “subsolution” \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) (cf. Sect. 2). These subsolutions are intended to be a kind of coarse-grained solutions to IPM, with \({\bar{m}}\) representing the relaxation of the momentum \({\bar{\rho }}{\bar{v}}\). The subsolutions are very related to the relaxed solutions appearing in the Lagrangian relaxation approach of Otto [65, 66] (see also [51]).
In the context of large data, an striking result from [17, 18] shows that there exist analytic initial interfaces in the fully stable regime (i.e. a graph) such that part of the curve turns to the unstable regime (i.e. no longer a graph) and later, at some \(T_* > 0\), the interface \(z(T_*)\) is analytic but at a point in the unstable region where it is not \(C^4\). The argument in [17] could be adapted to prove weaker singularities in \(C^k\) where \(k\ge 5\) (i.e. the interface leaves to be \(C^k\) but is still \(C^{k-1}\)). Thus, the Rayleigh–Taylor instability can arise spontaneously and the regularity might break down. After the blow-up time \(T_*\) it is to be expected that the Muskat problem is ill-posed.
Note that at this point of the theory h-principles are available and the task is to find a suitable subsolution. Even for the most simple subsolutions (null density in the mixing zone) the structure of the relaxation of IPM constrains the growth-rate \(c(\alpha )\ge 0\) and the shape of the mixing zone (see Sect. 2.4). This constraint prevents the two fluids from mixing (\(c(\alpha )=0\)) around fully stable points (stable points with zero slope) and it implies an equation of Muskat type in \(\{c(\alpha )=0\}\). In the unstable region, where the interface dynamic is expected to be ill-posed (analogous to the fully unstable case), the creation of mixing (\(c(\alpha )>0\)) is the only mechanism we know to solve IPM. This is in stark contrast with previous constructions of mixing solutions available in the literature: the mixing zone can not include the fully stable points and has to include the unstable part completely. Therefore, a new method is needed to find compatibility between the parabolic analysis in the stable regime and the relaxation approach in the unstable case. We remark that all previous approaches modelling instabilities blow up at some point when \(c(\alpha )=0\) ([16, 58, 64]). Indeed, gluing a solution of IPM in \(\{c(\alpha )=0\}\) with a subsolution in \(\{c(\alpha )>0\}\) becomes really subtle on the boundary of the support of \(c(\alpha )\). Thus, apart from the applications, these issues make the problem challenging. At the end of the intro we explain a number of novelties which allow us to bypass those difficulties.
a, c The initial interface \(z^\circ (\alpha )\) separating two fluids with different constant densities \(\rho _{\pm }=\pm 1\) as in (1.6) (1.7) respectively. b, d At some \(t>0\), the two boundaries of the non-mixing zones \(z_{\pm }(t,\alpha )=z(t,\alpha )\mp tc(\alpha )\tau (\alpha )^\perp \) (light blue) for some pseudo-interface \(z(t,\alpha )\) and growth-rate \(c(\alpha )\), with \(\tau (\alpha )=\frac{\partial _\alpha z^\circ (\alpha )}{|\partial _\alpha z^\circ (\alpha )|}\). Inside the mixing zone \(\Omega _{\mathrm {mix}}(t)\) we plot the Rayleigh–Taylor curve \(z_{\mathrm {per}}(t)\) (dark blue) which starts from a tiny perturbation of \(z^\circ \) (via the vortex-blob method). In all the figures we have added the coarse-grained velocity field \({\bar{v}}(t,x)\) outside \(\Omega _{\mathrm {mix}}\)
The original motivation of this work was to continue the solutions after the breakdown ([17, 18]) described before. However, there are numerous scenarios which are partially unstable. In this work we will concentrate on two of them: The so-called bubble interfaces where the two fluids are separated by a closed chord-arc curve (see [44] for the case with surface tension) and the turned interfaces where the interface is an open chord-arc curve which cannot be parametrized as a graph. We describe both scenarios readily, prior to the statement of the theorems.
The bubble type initial interfaces are described by
with \(\rho _{\pm }=\pm 1\), for some closed chord-arc curve \(z^\circ \in H^{k}({\mathbb {T}};{\mathbb {R}}^2)\) with k big enough (cf. Fig. 1a). Recall that we have taken \(z^\circ \) clockwise oriented (\(\circlearrowright \)) to be consistent with the notation in (1.1).
The turned type initial interfaces are described by
with \(\rho _{\pm }=\pm 1\), for some open chord-arc curve \(z^\circ \) whose turned region \(\{\partial _{\alpha }z_1^\circ (\alpha ) \le 0\}\) has positive measure. Here we consider both the \(x_1\)-periodic case \(z^\circ -(\alpha ,0)\in H^k({\mathbb {T}};{\mathbb {R}}^2)\) and the asymptotically flat case \(z^\circ -(\alpha ,0)\in H^{k}({\mathbb {R}};{\mathbb {R}}^2)\) with k big enough (cf. Fig. 1b).
Now we are ready to state our two main theorems.
Theorem 1.1
For every closed chord-arc curve \(z^\circ \in H^6({\mathbb {T}};{\mathbb {R}}^2)\) there exist infinitely many mixing solutions to IPM starting from (1.1) (1.6) with \(\rho _{\pm }=\pm 1\).
Theorem 1.2
For every open chord-arc curve \(z^\circ \), either \(x_1\)-periodic \(z^\circ -(\alpha ,0)\in H^6({\mathbb {T}};{\mathbb {R}}^2)\) or asymptotically flat \(z^\circ -(\alpha ,0)\in H^{6}({\mathbb {R}};{\mathbb {R}}^2)\), whose turned region \(\{\partial _{\alpha }z_1^\circ (\alpha ) \le 0\}\) has positive measure there exist infinitely many mixing solutions to IPM starting from (1.1) (1.7) with \(\rho _{\pm }=\pm 1\).
The definition of mixing solutions is by now classical and will be rigorously defined in Sect. 2 where the reader is exposed to the convex integration framework.
Remark 1.1
Theorem 1.2 is the first result proving the continuation of the evolution of IPM after the breakdown exhibited in [17, 18].
Remark 1.2
As mentioned above, the h-principle applied to a coarse-grained solution, a subsolution, yields infinitely many weak solutions. This path goes in both directions as, by taking suitable averages of the solutions, the subsolution is essentially recovered [19]. Thus, the relevant macroscopic properties of the solutions are described by the subsolution. Our construction yields piecewise constant subsolutions as in [43] and it is still open whether a continuous subsolution (similar to that in [16]) might be built in the partially unstable regime.
Remark 1.3
As in [16, 43, 64, 71], our mixing zone grows linearly in time around an evolving pseudo-interface. However, in Theorems 1.1 and 1.2 the mixing region must be localized in a neighborhood of the unstable region. Furthermore, this approach reveals the admissible regime for the growth-rate \(c(\alpha )\) of the mixing zone compatible with the relaxation of IPM. This is
which is characterized by the Rayleigh–Taylor function \(\sigma :=(\rho _{+}-\rho _{-})\partial _{\alpha }z_1^\circ \) and the vorticity strength \(\varpi :=-(\rho _{+}-\rho _{-})\partial _{\alpha }z_2^\circ \) along \(z^\circ \) (cf. Sect. 2). Observe that (1.8) prevents the two fluids from mixing wherever the initial interface is stable (\(\sigma (\alpha )>0\)) and there is not vorticity (\(\varpi (\alpha )=0\)).
The proof of the theorems relies on the pioneering adaptation of the convex integration method to Hydrodynamics by De Lellis and Székelyhidi ([35, 36]). The method has turned out to be very robust and flexible and the research on it has been extremely intense in the last decade. We contempt ourselves with describing a few landmarks: It has successfully described several problems related to turbulence as the Onsager’s conjecture (see e.g. [10, 34, 49]), the evolution of active scalars ([11, 30, 47, 50, 52, 68]) and transport equations ([33, 59,60,61]), the compressible Euler equations (see e.g. [1, 21, 22, 42, 54, 55]), the Navier-Stokes equations (see e.g. [9, 13, 14, 23]) and Magnetohydrodynamics ([8, 40, 41]) (see also the surveys [12, 37, 38] and the references therein).
In the context of modeling instabilities in Fluid Dynamics via convex integration, the first result in the IPM context (see also [30]) was proved in [71] where Székelyhidi constructed infinitely many weak solutions to IPM starting from the unstable planar interface. Remarkably, the coarse-grained density (the subsolution in the convex integration jargon) agrees with the Otto’s Lagrangian relaxation of IPM (cf. [65] and also [57]). In [16] the first two authors and Córdoba constructed mixing solutions starting with a non-flat interface. In this work and all the subsequent ones, the mixing zone is described as an envelop of size \(tc(\alpha )\) of a curve \(z(t,\alpha )\) whose evolution is dictated by an operator which is an average of the classical Muskat operator. In [16] the coarse-grained density \({\bar{\rho }}\) is a continuous interpolation between the two fluids, which induces through an adapted h-principle a degraded mixing property ([19]). As a by-product of this version of the h-principle [19], one shows that the subsolution is recovered from the solution by taking suitable averages. Remarkably, if one considers instead piecewise constant coarse-grained densities, the evolution of the pseudo-interface greatly simplifies as was shown in [43] by Förster and Székelyhidi. See also [7, 64] for possible choices of the speed of opening of the mixing zone \(c(\alpha )\).
After the works in IPM, instabilities for the incompressible Euler equations have been successfully modeled with related strategies, e.g. the Rayleigh–Taylor ([45, 46]) and the Kelvin-Helmholtz ([58, 70]) instabilities.
All the previous works deal either with the fully stable or fully unstable regime of the various instabilities and hence new twists should be added to the theory to deal with the partially unstable case. We finish the introduction with some comments on the natural obstructions and a non-technical description of the new view points needed to address them. We believe that it is likely that the ideas from this paper can be adapted and extended to consider different partially unstable scenarios in various problems concerning instabilities in Fluid Dynamics.
Since it is to be expected that the classical Muskat problem is ill-posed in this partially unstable situation, we need to see a way to find compatibility between the parabolic analysis for the stable case and the relaxation approach for the unstable case. In particular, the mixing region needs to envelope the unstable region. That is (recall \(\sigma =(\rho _{+}-\rho _{-})\partial _{\alpha }z_1^\circ \))
As h-principles are by now standard [16, 19, 71], the main issue of the proof relies on building a mixing zone which admits a suitable subsolution \(({\bar{\rho }},{\bar{v}},{\bar{m}})\). We will follow [43] and declare \({\bar{\rho }}\) piecewise constant in the mixing zone. In fact, for the sake of simplicity during the introduction we will assume the simplest case, \({\bar{\rho }}=0\) in \(\Omega _{\mathrm {mix}}\).
At each time slice \(0< t\le T\ll 1\), the mixing zone is the open set in \({\mathbb {R}}^2\) given by
parametrized by the map
where \(\tau (\alpha )\) is an unitary vector field, \(c(\alpha )\) is the growth-rate of the mixing zone and \(z(t,\alpha )\) is the pseudo-interface evolving from \(z^\circ (\alpha )\), that we have to determine.
In order to optimize the speed of opening of the mixing zone, it is convenient to take \(\tau \) as the tangential vector field to \(z^\circ \)
With our ansatz for \({\bar{\rho }}\) as in [43] and this optimal choice for \(\tau \), the admissible regime for \(c(\alpha )\) compatible with the relaxation of IPM becomes
We remark in passing that \(2c(\alpha )\) above can be replaced by \(\frac{2N}{2N-1}c(\alpha )\) for any \(N\ge 1\) as in [43, 64], which yields (1.8) as \(N\rightarrow \infty \) (cf. Sect. 6.2). Observe that this inequality requires \(c(\alpha )=0\) if \(\sigma (\alpha )=|(\sigma (\alpha ),\varpi (\alpha ))|\), or equivalently \(\partial _{\alpha }z_1^\circ (\alpha )=\mathrm {sgn}(\rho _{+}-\rho _{-})|\partial _{\alpha }z^\circ (\alpha )|\) (cf. Remark 1.3). Since in the regimes we are considering there are always such points, we are forced to treat the case where there is no opening in some region, i.e. \(c(\alpha )=0\). An extra difficulty at this level is that our estimates need certain smoothness in c (i.e. the very definition of the velocity) which necessarily creates cusp singularities on \(\Omega _{\mathrm {mix}}\). We deal with this problem by interpreting the mixing zone as a superposition of regular domains (cf. Fig. 2 and Lemma 2.1).
The macroscopic density \({\bar{\rho }}\) (2.26) can be decomposed as the sum of the contribution of \(\rho _+\) on \(\Omega _{+}\cup \Omega _{\mathrm {mix}}\) and \(\rho _-\) on \(\Omega _{-}\cup \Omega _{\mathrm {mix}}\). In this way, the cusp singularities in \(\Omega _{\mathrm {mix}}\) can be understood as the superposition of regular domains
Next we turn to the coarse-grained velocity and the associated Muskat type operator. Here we start from [43] as we have chosen the same ansatz for the coarse-grained density and then explain the new idea. The Förster-Székelyhidi’s velocity is also an average of the classical Muskat velocity as in [16] but only between the two boundaries of the non-mixing zones \(z_\pm =z \mp t c \tau ^\perp \). The associated Muskat type operator is (cf. Sect. 2.1)
where
We remark in passing that, for open curves as in Theorem 1.2, all these integrals are taken with the Cauchy’s principal value at infinity. However, we will focus on the closed case until Sect. 6 for clarity of exposition.
The evolution of z is driven by the operator B. On the one hand, as it is explained in the discussion after (1.13), in the partially unstable case there is always a non-mixing region where we must solve a classical Muskat equation exactly
On the other hand, the flexibility of the notion of subsolution gives some space to define the pseudo-interface ([43, 64]). Namely, in the mixing region it is enough to solve (1.16) approximately
where the error must be small in some sense that shall be specified in Sects. 2.1 and 2.4. Due to the Rayleigh–Taylor instability, it is to be expected that the choice \(\text {error}=0\) above yields an ill-posed equation as in the fully unstable regime. In spite of this, following another clever idea from [43], in the fully unstable regime it is possible to take \(\text {error}=B^{1)}-B+\text {error}\), where \(B^{1)}\) denotes the first order expansion in time of B. This choice yields the following well-defined evolution for z
We remark that, if the error in (1.17) was zero, then the Eqs. (1.16) and (1.17) do not match at \(c(\alpha )=0\). In order to glue these equations we first introduce a partition of the unity \(\{\psi _0,\psi _1\}\) which, as required in (1.9), allows also to open the mixing zone slightly inside the stable region, namely \(\mathrm {supp}\,\psi _0\subset \{\partial _{\alpha }z_1^\circ (\alpha )>0\}\) and \(\mathrm {supp}\,\psi _1=\mathrm {supp}\,c\). That is, we bypass the gluing problem by writing
where the error is supported on \(\{c(\alpha )>0\}.\) Yet the energy inequalities that we obtain for the operator \(\psi _0B\) (or other modifications) yields a factor 1/c which blows up in the region where \(c(\alpha )\) tends to zero. The way out of this vicious circle is to treat the interaction between separate boundaries as a perturbation. In this way, one can write \(B=E+\text {error}\) in such a way that E yields good energy inequalities and the \(\text {error}\) is small in the supremum norm and supported on \(\{c(\alpha )>0\}\). Thus, the perturbation can be absorbed in the relaxation even if its derivatives are badly behaving. Hence, we will solve
for some error term supported on \(\{c(\alpha )>0\}\), where \(E^{1)}\) denotes the first order expansion in time of E. Essentially, \(E=B_{+,+}+B_{-,-}\) as the factor 1/c comes from the terms with \(a\ne b\) in (1.15).
Organization of the Paper We start Sect. 2 by recalling briefly the Classical and the Mixing Muskat problem. After this, we recall also the concepts of mixing solution and subsolution, as well as the h-principle in IPM. Then, we define our ansatz for the subsolution in terms of the mixing zone and derive the conditions for the growth-rate c and the pseudo-interface z under which such subsolution truly exists. The construction of a pair (c, z) satisfying such requirements appears in Sects. 3–5. Finally, we prove in Sect. 6 the Theorems 1.1, 1.2 and the optimal regime for c given in (1.8).
Notation
-
(Complex coordinates) It is convenient to identify the Euclidean space \({\mathbb {R}}^2\) with the complex plane \({\mathbb {C}}\) as usual, \(z=(z_1,z_2)=z_1+iz_2\). Therefore, along the whole paper we will use complex coordinates and subindexes 1, 2 indicate real and imaginary parts for a complex number.
Thus, \(i\equiv (0,1)\) plays the roll both of the standard vertical vector and the imaginary unit. We will denote \(z^*:=(z_1,-z_2)=z_1-iz_2\), \(z^\perp :=(-z_2,z_1)=iz\) and \(z\cdot w:=z_1w_1+z_2w_2=(zw^*)_1\). In this regard, we also have \(\nabla =(\partial _1,\partial _2)=\partial _1+i\partial _2\), and so \(\nabla ^*=\partial _1-i\partial _2\) and \(\nabla ^\perp =i\nabla \).
-
(Function spaces) We will consider the usual Hölder spaces \(C^{k,\delta }\) with norm
$$\begin{aligned} \Vert f\Vert _{C^{k,\delta }}:=\sup _{j\le k}\Vert \partial ^jf\Vert _{L^\infty }+|\partial ^kf|_{C^\delta } \quad \text {with}\quad |g|_{C^\delta }:=\sup _{\alpha ,\beta }\frac{|g(\alpha )-g(\alpha -\beta )|}{|\beta |^\delta }, \end{aligned}$$and also the Sobolev spaces \(H^{k}\) with
$$\begin{aligned} \Vert f\Vert _{H^k}:=\left( \sum _{j=0}^k\Vert \partial ^jf\Vert _{L^2}^2\right) ^{\frac{1}{2}}. \end{aligned}$$ -
(Increments and different quotients) Given a function \(f=f(\alpha )\) and another parameter \(\beta \), it will be handy to use the expressions \(f'=f(\alpha -\beta )\), \(\delta _\beta f=f-f'\) and \(\Delta _\beta =\frac{\delta _\beta }{\beta }\) as in [29, 32].
2 The Mixing Zone and the Subsolution
2.1 The Muskat Problem
The Muskat problem describes IPM under the assumption that there is a time-dependent oriented curve \(z(t,\alpha )\) separating \({\mathbb {R}}^2\) into two complementary open domains
each one occupied by a fluid with different constant densities \(\rho _{-}\) and \(\rho _{+}\) respectively.
The incompressibility condition (1.3) implies that \(v=\nabla ^\perp \psi \) for some stream function \(\psi (t,x)\). Hence, the Darcy’s law (1.4) can be written in complex coordinates as \(\nabla (p+i\psi )=-i\rho ,\) which yields the following Poisson equation (\(\nabla ^*\nabla =\Delta \))
In view of (2.1), the density jump along z implies that
in the sense of distributions. Hence, p and \(\psi \) are recovered from the Poisson equation through the Newtonian potential
Then, p and \(\psi \) are continuous but have discontinuous gradients along z, and indeed \(\Delta (p+i\psi )=(\sigma +i\varpi )\delta _z\) where \(\sigma \) \(\equiv \) Rayleigh–Taylor and \(\varpi \) \(\equiv \) vorticity strength (\(\Delta \psi =\nabla ^\perp \cdot v=\omega \)), which satisfy
The velocity v is recovered from the vorticity through the Biot-Savart law
where we have applied that \(\varpi =-(\rho _{+}-\rho _{-})\partial _{\alpha }z_2\) and the Cauchy’s argument principle in the last equality
It is easy to see that v is bounded, smooth outside z but with tangential discontinuities along z. Its normal component is well-defined and satisfies
where
Observe that the operator B is obtained by adding a suitable tangential term to the velocity (2.3) and then taking the limit \(\Omega _{\pm }(t)\ni x\rightarrow z(t,\alpha )\). We refer to (2.5) as the classical Muskat operator. Let us remark that this operator (2.5) coincides with (1.14) when tc is identically zero. Since it only appears in this Sect. 2.1 and the notation of the paper is heavy enough, we do not give it another name.
Finally, it is easy to check that the conservation of mass equation (1.2) is equivalent to find z satisfying
Thus, the Muskat problem is equivalent to solve this Cauchy problem for the interface z starting from \(z^\circ \) given in (1.16). We remark that because of (2.6), one may add any tangential term to (1.16). This only changes the parametrization and does not modify the geometric evolution of the curve. We refer to (1.16) as the Classical Muskat problem.
Assuming that the interface can be parametrized as a graph, \(z(t,\alpha )=\alpha +if(t,\alpha )\) in complex coordinates, the Eq. (1.16) reads as
which can be linearized as \(\partial _tf=(\rho _{+}-\rho _{-})(-\Delta )^{1/2}f\). In analogy with the heat equation, the fully stable regime (\(\rho _+>\rho _-\)) admits a parabolic analysis through energy estimates.
However, the same strategy for the fully unstable regime (\(\rho _+<\rho _-\)) is not viable. Despite this, mixing solutions to IPM starting from fully unstable Muskat inital data have been constructed in the last years through the convex integration method [16, 43, 64, 71]. In these works, the mixing zone is given as in (1.10) (1.11) but with \(\tau =(-1,0)\) instead of (1.12). More generally, we may consider any unitary vector field \(\tau (\alpha )\) satisfying
Thus, the triplet \((\tau ,c,z)\) parametrizes the mixing zone, which does not exist when \(tc(\alpha )=0\). Here we follow [43, 64], where \({\bar{\rho }}=0\) on \(\Omega _{\mathrm {mix}}\). In this case, the coarse-grained velocity becomes
where \(z_\pm (t,\alpha )=z(t,\alpha )\mp tc(\alpha )\tau (\alpha )^\perp \) are the two boundaries of the non-mixing zones. The admissible regime for \(c(\alpha )\) compatible with the relaxation of IPM is
which agrees with [43, 64] as in this case \(\rho _{\pm }=\mp 1\), \(\partial _{\alpha }z^\circ =(1,\partial _{\alpha }f^\circ )\) and \(\tau =(-1,0)\) (cf. Rem. 2.4). Observe that (2.7) requires \(c(\alpha )=0\) if \(\partial _{\alpha }z_1^\circ (\alpha )=\partial _{\alpha }z^\circ (\alpha )\cdot \tau (\alpha )\). In view of (1.9), this prevents some choices for \(\tau (\alpha )\) as for instance the one from [16, 19, 43]. Thus, we really need to optimize by opening the mixing zone perpendicularly to the curve (this is also the case in [58]). This is why we have chosen \(\tau \) as in (1.12). With such optimal choice for \(\tau \), (2.7) reads as (1.13) (recall (2.2)).
Once \(\tau (\alpha )\) and \(c(\alpha )\) are fixed, we must determine the time-dependent pseudo-interface \(z(t,\alpha )\). Modulo technical details which will be explained in Sect. 2.4, the existence of a relaxed momentum \({\bar{m}}(t,x)\) is reduced to find z satisfying
uniformly in \(\alpha \) as \(t\rightarrow 0\), where
with \(\tau \), c, B and \(B_{a}\) given in (1.10)–(1.15). Observe that \(D\cdot \partial _{\alpha }(c\tau )=0\) for \(\partial _{\alpha }z=(1,\partial _{\alpha }f)\) and \(\tau =(-1,0)\), and thus it does not appear in [43, 64]. Hence, the Eq. (2.8) generalizes both (1.16) and (1.17). As we mentioned in the introduction, we cannot simply glue these evolution equations because they do not match at \(c(\alpha )=0\). In order to interpolate between the two regions, we introduce a partition of the unity \(\{\psi _0,\psi _1\}\) subordinated to \(\{\partial _{\alpha }z_1^\circ (\alpha )>0\}\) and \(\{c(\alpha )>0\}\) respectively. Then, we consider (cf. (4.1))
Here, E should be an extension of B and good for energy inequalities, which justify its name twice.
In view of (1.16) and (1.17), one would be initially tempted to take \(E=B\). However, the terms with \(a\ne b\) in (1.14) introduce a factor \(\partial _{\alpha }\log c(\alpha )\) in the energy estimates which we did not see how to compensate. Thus, we will declare
which equals B on \(tc(\alpha )=0\) and only includes interaction of stable Muskat type.
The error term is localized on the mixing region with order t. This is
where \(D^{(0)}=D|_{t=0}\), \(\kappa =\partial _t(E-B)|_{t=0}\) depends on the initial curvature and \(h=O(t^2)\) is a time-dependent average. As a result, \(D^{(0)}\) and \(\kappa \) only depends on \(z^\circ \) while h(t) depends on z(t) but not on \(\alpha \). This allows to treat the error as a harmless term in the energy estimates.
2.2 Weak Solutions, Subsolutions and the Mixing Zone
Let us start by recalling the rigorous definition of weak solutions, mixing solutions and subsolutions in the IPM context.
Given \(T>0\) and \(\rho ^\circ \) as in (1.1), a weak solution to IPM
satisfies that, for every test function \(\phi \in C_c^1({\mathbb {R}}^3)\) with \(\phi ^\circ :=\phi |_{t=0}\) and \(0<t\le T\):
In addition, a weak solution is a mixing solution if, at each \(0<t\le T\), the space \({\mathbb {R}}^2\) is split into three complementary open domains, \(\Omega _{+}(t)\), \(\Omega _{-}(t)\) and \(\Omega _{\mathrm {mix}}(t)\), satisfying that \((\rho ,v)\) is continuous on the non-mixing zones \(\Omega _\pm \):
while it behaves wildly inside the mixing zone \(\Omega _{\mathrm {mix}}\):
for every open \(\emptyset \ne \Omega \subset \Omega _{\mathrm {mix}}(t)\).
Conversely, we say that \((\rho ,v)\) is a non-mixing solution if \(\Omega _{\mathrm {mix}}=\emptyset \).
In convex integration, a subsolution (a macroscopic solution) is defined in term of a conservation law and a relaxed constitutive relation, which is typically given by the \(\Lambda \)-convex hull. In the IPM context, the hull was computed in [71] (see also [57] for related computations).
Given \(T>0\) and \(\rho ^\circ \) as in (1.1), a subsolution to IPM
satisfies that, for every test function \(\phi \in C_c^1({\mathbb {R}}^3)\) with \(\phi ^\circ :=\phi |_{t=0}\) and \(0< t\le T\):
such that, at each \(0<t\le T\), the space \({\mathbb {R}}^2\) is split into three complementary open domains, \(\Omega _{+}(t)\), \(\Omega _{-}(t)\) and \(\Omega _{\mathrm {mix}}(t)\) satisfying that
In addition, it is required that
Remark 2.1
Notice that the pressure does not appear in (2.11c) (2.14c). For completeness we will show in Lemma A.1 how \(p\in C([0,T]\times {\mathbb {R}}^2)\) is recovered and its relation with \({\bar{p}}\). We are not aware of similar computations for the IPM pressure in the convex integration framework.
Theorem 2.1
(H-principle in IPM) Assume that there exists a subsolution \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) to IPM starting from \(\rho ^\circ \), for some \(T>0\), \(\Omega _\pm \) and \(\Omega _{\mathrm {mix}}\). Then, there exist infinitely many mixing solutions \((\rho ,v)\) to IPM starting from \(\rho ^\circ \), for the same \(T>0\), \(\Omega _{\pm }\) and \(\Omega _{\mathrm {mix}}\), and satisfying \((\rho ,v)=({\bar{\rho }},{\bar{v}})\) outside \(\Omega _{\mathrm {mix}}\).
The proof of this h-principle for the \(L_{t,x}^\infty \) case can be found in [71], and the generalization to \(C_tL_{w^*}^\infty \) in [19]. As noticed in [71], the inequality (2.15b) only provides solutions in \(L^2\). Remarkably, Székelyhidi computed in [71, Prop. 2.4] the additional inequalities which yield solutions in \(L^\infty \). In [57, Lemma 4.3] it is checked that, if \({\bar{v}}\) is controlled as in (2.16), then these additional inequalities are automatically satisfied.
By Theorem 2.1, the construction of mixing solutions as stated in Theorems 1.1 and 1.2 is reduced to constructing suitable subsolutions \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) adapted to \(\Omega _{\mathrm {mix}}\).
As described in the intro, it follows from (1.10)-(1.12) that the mixing zone is prescribed by the growth-rate c and the pseudo-interface z. With this terminology, for bubble interfaces (1.6) we define
and for turned interfaces (1.7)
Thus, \(\Omega _{+}(t)\), \(\Omega _{-}(t)\) and \(\Omega _{\mathrm {mix}}(t)\) are complementary open domains in \({\mathbb {R}}^2\). For each region \(r=+,-,\mathrm {mix}\), we denote \(\Omega _r:=\{(t,x)\,:\,x\in \Omega _{r}(t),\,0\le t\le T\}\).
Remark 2.2
For the sake of simplicity we will consider from now on the closed case (2.17) and go back at Sect. 6 with the open case (2.18). Recall that for closed interfaces we have assumed that \(z^\circ \) is clockwise oriented (\(\circlearrowright \)). In addition, we may assume w.l.o.g. that \(z^\circ \) is the arc-length (\(|\partial _{\alpha }z^\circ |=1\)) parametrization, although z(t) will not be it in general. Thus, we fix \({\mathbb {T}}=[-\ell _\circ /2,\ell _\circ /2]\) where \(\ell _\circ :=\mathrm {length}(z^\circ )\).
For a general pair (c, z) we construct in the next Sect. 2.3 a suitable triplet \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) adapted to \(\Omega _{\mathrm {mix}}\). After this, we derive in Sect. 2.4 conditions for (c, z) under which this \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) becomes a subsolution. Finally, we will prove in Sects. 3–5 the existence of a pair (c, z) satisfying such requirements.
Hipothesis on (c, z). Apart from regularity assumptions, the curve needs to satisfy an angle and a chord-arc condition in a uniform manner. Prior to state the assumptions, let us introduce the angle constant of z w.r.t. \(\tau \)
and recall the definition of a chord-arc curve.
Definition 2.1
A curve \(z\in C({\mathbb {T}};{\mathbb {R}}^2)\) is chord-arc if
Along the rest of this Sect. 2 we will assume the existence of \(\delta ,T>0\) such that
and
satisfying the following equi-angle condition
and the following equi-chord-arc condition
where we recall that \(z_\lambda =z-\lambda tc\tau ^\perp \) with \(\tau =\partial _{\alpha }z^\circ \).
The condition (2.23) controls the angle between the family of curves \(z_\lambda \) w.r.t. \(\tau \). The equi-chord-arc condition (2.24) bounds the singularity due to the denominator of the operators \(B_{a,b}\) (1.15), while the numerator justifies the regularity assumptions (2.21) (2.22). In addition, all they have the following useful consequence.
Remark 2.3
The conditions (2.21)-(2.24) imply that map \((\alpha ,\lambda )\mapsto z_\lambda (t,\alpha )\) is a diffeomorphism from \(\{c(\alpha )>0\}\times (-1,1)\) to \(\Omega _{\mathrm {mix}}(t)\) with Jacobian \(tc(\partial _{\alpha }z_\lambda \cdot \tau )>0\).
In Sect. 3 we will construct a suitable smooth growth-rate c. Once c is fixed, we will still assume (2.22)-(2.24) in Sect. 4. Finally, we will construct a time-dependent pseudo-interface z satisfying such conditions in Sect. 5.
We conclude this subsection by proving an auxiliary lemma which allows to integrate by parts, under certain conditions, on the domain with cusp singularities \(\Omega _{\mathrm {mix}}\).
Lemma 2.1
Fix \(0\le t\le T\). Let \(f\in L^\infty ({\mathbb {R}}^2)\) satisfying that \(f\in C^1\) with \(\nabla \cdot f=0\) outside \(\partial \Omega _{+}(t)\cup \partial \Omega _{-}(t)\) and with well-defined continuous limits
whenever \(z_a(t,\alpha )\in \partial \Omega _{r}(t)\) for \(a=\pm \) and \(r=+,-,\mathrm {mix}\). Then, for every \(\phi \in C_c^1({\mathbb {R}}^2)\),
Proof
First of all we split the integral over \({\mathbb {R}}^2\) into \(\Omega _{+}(t)\), \(\Omega _{-}(t)\) and \(\Omega _{\mathrm {mix}}(t)\). On the one hand, by applying the Gauss divergence theorem on the regular domains \(\Omega _{a}(t)\) for \(a=\pm \), we get
where we have applied that \(\nabla \cdot f=0\) outside \(\partial \Omega _{+}(t)\cup \partial \Omega _{-}(t)\) and that the normal vector to \(\partial \Omega _{a}(t)\) pointing outward is \(a\partial _{\alpha }z_a(t)^\perp \). This concludes the proof for \(t=0\). Now we pay special attention to the cusp singularities in \(\Omega _{\mathrm {mix}}(t)\) for \(0<t\le T\). For any \(\varepsilon >0\) we define
which forms an exhaustion by Lipschitz domains of \(\Omega _{\mathrm {mix}}(t)\). Hence, we can apply first the dominated convergence and then the Gauss divergence theorem on \(\Omega _{\mathrm {mix}}^\varepsilon (t)\) to obtain
where \(f^{\text {mix}}\) denotes the limit of f on \(\partial \Omega _{\mathrm {mix}}^\varepsilon (t)\) and \(n^\varepsilon \) is the unit normal vector to \(\partial \Omega _{\mathrm {mix}}^\varepsilon (t)\) pointing outward. Since \(f\in L^\infty \) it follows that the contribution of the boundary integral on \(c(\alpha )=\varepsilon \), \(\lambda \in (-1,1)\) is zero in the limit \(\varepsilon \rightarrow 0\). Therefore, we deduce that
This concludes the proof. \(\square \)
2.3 The Subsolution
2.3.1 The Density
Following [43, 64] we declare \({\bar{\rho }}=0\) on \(\Omega _{\mathrm {mix}}\):
with \(\Omega _{\pm }(t)\) given in (2.17). As a result, \(\partial _1{\bar{\rho }}(t)\) is a Dirac measure supported on \(\partial \Omega _{+}(t)\cup \partial \Omega _{-}(t)\) with density \((\partial _{\alpha }z_a(t))_2\) on each \(\partial \Omega _a(t)\) for \(a=\pm \).
Lemma 2.2
For every \(\phi \in C_c^1({\mathbb {R}}^2)\) and \(0\le t\le T\),
Proof
It follows from Lemma 2.1 applied to \(f={\bar{\rho }}\) because, in this case, we have \(1\cdot \partial _{\alpha }z_a^\perp =-(\partial _{\alpha }z_a)_2\), \({\bar{\rho }}_a^a=a\) and \({\bar{\rho }}_a^{\mathrm {mix}}=0\). \(\square \)
2.3.2 The Velocity
In view of Lemma 2.2 we define \({\bar{v}}\) by means of the Biot-Savart law (cf. (2.3))
Observe that \({\bar{v}}\) is continuous (indeed \(C_t^1C^\omega \)) outside \(\partial \Omega _+\cup \partial \Omega _-\). Proposition 2.1 shows hat \({\bar{v}}\) satisfies the Eqs. (2.14b) (2.14c), the boundedness condition (2.16) and that has well-defined continuous limits (2.25). Proposition 2.2 shows that the normal component of \({\bar{v}}\) on \(\partial \Omega _+\cup \partial \Omega _-\) is well-defined and continuous. Figure 2 explains why this is not surprising.
Proposition 2.1
Let \({\bar{\rho }}\) be as in (2.26). The unique velocity satisfying (2.14b) (2.14c) which additionally vanishes as \(|x|\rightarrow \infty \) is precisely (2.27). Moreover, \({\bar{v}}\) is uniformly bounded on \([0,T]\times {\mathbb {R}}^2\) and has well-defined continuous limits (2.25).
Proof
Step 1 \({\bar{v}}\) in (2.27) is uniformly bounded and has well-defined continuous limits (2.25). First of all notice that \({\bar{v}}\) is continuous (indeed \(C_t^1C^\omega \)) outside \(\partial \Omega _{+}\cup \partial \Omega _{-}\). Moreover, for any \((t,x)\notin \partial \Omega _{+}\cup \partial \Omega _{-}\) it holds that
that is, \({\bar{v}}\) decays as \(|x|^{-2}\) when \(|x|\rightarrow \infty \).
Let us manipulate the expression (2.27) to help better understand the behavior of \({\bar{v}}\) near the boundary \(\partial \Omega _+\cup \partial \Omega _-\). We will use de index w.r.t. \(z_b(t)\) of points x outside \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\):
Recall that z(t) is clockwise oriented (\(\circlearrowright \)). Hence, the Cauchy’s argument principle yields
In order to compute the limits (2.25), for any x outside \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\) but close enough and \(a=\pm \), we take \(\alpha (x,a)\in {\mathbb {T}}\) minimizing \(|x-z_a(t,\alpha )|\). Then, a straightforward identity of complex numbers yields
On the one hand, the regularity conditions (2.21)–(2.24) allow to apply the dominated convergence theorem on the first term in (2.29) as \(x\rightarrow z_a(t,\alpha )\). On the other hand, the limits \(\Omega _{r}(t)\ni x\rightarrow z_a(t,\alpha )\) in the second term in (2.29) change depending on the region \(r=+,-,\text {mix}\) where x is coming from due to (2.28). Therefore, \({\bar{v}}\) has well-defined continuous limits (2.25)
where
for \((t,\alpha )\in [0,T]\times {\mathbb {T}}\) and \(a,b=\pm \). Finally, it follows that \({\bar{v}}\) is uniformly bounded on \([0,T]\times {\mathbb {R}}^2\).
Step 2 \({\bar{v}}\) satisfies (2.14b) (2.14c). Observe that \({\bar{v}}(t)^*\) is holomorphic outside \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\) for all \(0\le t\le T\). Thus, the Cauchy–Riemann equations imply that \(\nabla \cdot {\bar{v}}(t)=\nabla ^\perp \cdot {\bar{v}}(t)=0\) outside \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\). Notice also that \(z_{+}=z_{-}\) and \(V_{+}=V_{-}\) on \(tc(\alpha )=0\). In particular,
Let \(\phi \in C_c^1({\mathbb {R}}^2)\) and \(0<t\le T\). Then, by applying Lemma 2.1 to \(f={\bar{v}}\) and \({\bar{v}}^\perp \), we deduce that
These identities jointly with Lemma 2.2 imply that \({\bar{v}}\) satisfies (2.14b) (2.14c).
Step 3 Uniqueness Finally, it is easy to check that any solution to (2.14b) (2.14c) has the form \({\bar{u}}={\bar{v}}+f^*\) for some (time-dependent) entire function f. Thus, if \({\bar{u}}\) vanishes as \(|x|\rightarrow \infty \) too, the Liouville’s theorem implies that \(f=0\). \(\square \)
In the next lemma we deal with the normal component of \({\bar{v}}\) at the boundary of the mixing zone \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\). We will use the notation from Lemma 2.1 for the outer an inner limits and the operators \(B,B_a\) defined in the intro (1.14), (1.15).
Proposition 2.2
Let \(a=\pm \) and \(r=+,-\mathrm {mix}\). Then, it holds that
on \([0,T]\times {\mathbb {T}}\). In particular,
Proof
Let x be outside \(\partial \Omega _+(t)\cup \partial \Omega _-(t)\) but close enough. Firstly, using that \((\mathrm {Ind}_{z_b(t)}(x))_2=0\), it follows that the velocity (2.27) can be written as (cf. (2.3) (2.4))
In particular,
where we take \(\alpha \in {\mathbb {T}}\) as in (2.29). Thus, it remains to show that we can take the limit \(x\rightarrow z_a(t,\alpha )\) in the r.h.s. above. By writing \(z_a=z_b-i(a-b)tc\tau \), we split the above integrals into
Analogously to (2.29), the regularity conditions (2.21)–(2.24) allow to apply the dominated convergence theorem on the first term as \(x\rightarrow z_a(t,\alpha )\). Notice that the second term vanishes for \((a-b)tc(\alpha )=0\). Otherwise, we can consider directly \(x\rightarrow z_a(t,\alpha )\). This implies the first statement. As a by-product, we have seen that \(B_{a,b}\) is split into
Finally, the second statement follows from the fact that \(z_+=z_-\) and \(B_+=B_-=B\) on \(tc(\alpha )=0\). \(\square \)
2.3.3 The Relaxed Momentum
In view of the inequality (2.15), it seems suitable to define \({\bar{m}}\) as
in terms of some \(\gamma \in C(\Omega _{\mathrm {mix}};{\mathbb {R}}^2)\) to be determined ([16, 43, 64, 71]). Moreover, for any \(0<t\le T\) we assume that \(\gamma (t)\in C^1(\Omega _{\mathrm {mix}}(t))\) with continuous limits
whenever \(z_a(t,\alpha )\in \partial \Omega _{\mathrm {mix}}(t)\) for \(a=\pm \) and \(c(\alpha )>0\).
2.4 Compatibility Between the Mixing Zone and the Subsolution
In the next proposition we derive the conditions for \((c,z,\gamma )\) under which the corresponding \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) given in (2.26),(2.27) and(2.32) becomes a subsolution.
Proposition 2.3
Assume that (c, z) satisfies (2.21)–(2.24) for some \(T>0\). The triplet \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) given in (2.26), (2.27) and (2.32) defines a subsolution to IPM if and only if the triplet \((c,z,\gamma )\) satisfies the following equations on \(\partial \Omega _a\) for \(a=\pm \)
and the following conditions on \(\Omega _{\mathrm {mix}}\)
Proof
Recall that \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) already satisfies the Eqs. (2.14b) (2.14c) and the conditions (2.15a) (2.16) (see Prop. 2.1). Moreover, it is clear that \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) satisfies the Eq. (2.14a) on \(\Omega _{\mathrm {mix}}\) and the inequality (2.15b) if and only if (2.34) holds. Thus, it remains to analyze (2.14a) outside \(\Omega _{\mathrm {mix}}\).
Let \(\phi \in C_c^1({\mathbb {R}}^3)\) and \(0< t\le T\). On the one hand, since \({\bar{\rho }}=0\) on \(\Omega _{\mathrm {mix}}\) and \({\bar{\rho }}=\pm 1\) on the regular domains \(\Omega _{\pm }(t)\), an integration by parts yields
where \(Z(t,\alpha ):=(t,z(t,\alpha ))\) and \(Z_a(t,\alpha ):=(t,z_a(t,\alpha ))\). On the other hand, notice (2.32) reads as
In particular, \({\bar{m}}\) satisfies the assumptions in Lemma 2.1. Therefore, it follows that
where we have applied Proposition 2.2 in the first two lines above. In summary, we have seen that
This concludes the proof. \(\square \)
We conclude this section by showing that we can construct \(\gamma (t,x)\) satisfying the requirements in Proposition 2.3 provided that (c, z) satisfies certain conditions. Observe that \(\{c(\alpha )>0\}\) is open and thus a (countable) union of disjoint intervals \((\alpha _1,\alpha _2)\). Recall the definition of B and D from (1.14) and (2.9).
Lemma 2.3
Assume that (c, z) satisfies (2.21)–(2.24) for some \(T>0\). Assume further that the following conditions hold uniformly on \(\{c(\alpha )>0\}\)
and
as \(t\rightarrow 0\), for \(a=\pm \) and \(\alpha \in (\alpha _1,\alpha _2)\) connected component of \(\{c(\alpha )>0\}\). Then, there exists \(0<T'\le T\) and \(\gamma (t,\alpha )\) satisfying (2.33b)–(2.34) as long as \(0<t\le T'\).
Proof
Step 1 Analysis of (2.33b)–(2.34). For simplicity we may assume w.l.o.g. that there is one connected component \((\alpha _1,\alpha _2)=\{c(\alpha )>0\}\). Recall that \((\alpha ,\lambda )\mapsto z_{\lambda }(t,\alpha )\) is a diffeomorphism from \((\alpha _1,\alpha _2)\times (-1,1)\) to \(\Omega _{\mathrm {mix}}(t)\) (cf. Rem. 2.3). In particular, since \(\Omega _{\mathrm {mix}}(t)\) is simply-connected, (2.34a) implies that \(\gamma (t)=\nabla ^\perp g(t)\) for some \(g(t)\in C^1(\Omega _{\mathrm {mix}}(t))\) to be determined. Moreover, g can be defined in terms of some G in \((\alpha ,\lambda )\)-coordinates as
where \(Z(t,\alpha ,\lambda ):=(t,z_\lambda (t,\alpha ))\). Notice that (recall \(z_\lambda =z-\lambda tc\tau ^\perp \))
On the one hand, the boundary conditions (2.33b) for \(\gamma \) read as
On the other hand, for (2.34b) notice that
In particular,
![](http://media.springernature.com/lw477/springer-static/image/art%3A10.1007%2Fs40818-022-00121-w/MediaObjects/40818_2022_121_Equ249_HTML.png)
with \(\partial _{\alpha }z^\circ \cdot \tau > 0\) uniformly on \(c(\alpha )>0\) by (2.23). Therefore, assuming that c satisfies (2.35), it is enough to find G satisfying (2.37) and the following growth conditions
uniformly on \(c(\alpha )>0\) as \(t\rightarrow 0\), because in this case (recall \(\tau =\partial _{\alpha }z^\circ \) with \(|\partial _{\alpha }z^\circ |=1\))
Step 2 Ansatz for G. We declare
Hence, it follows that
Notice that (2.37) is satisfied. Finally, assuming that z satisfies (2.36), then (2.39) holds. \(\square \)
Remark 2.4
Following the previous proof, notice that for \(z(t,\alpha )=(\alpha ,f(t,\alpha ))\) and \(\tau =(-1,0)\) as in [43, 64], the admissible regime for \(c(\alpha )\) reads as
which clear is incompatibly with \(c(\alpha )=0\). Remarkably, the authors in [64] achieved that \(c(\alpha )\rightarrow 0\) in the limiting case \(|\alpha |\rightarrow \infty \) for \(\alpha \in {\mathbb {R}}\).
In view of Proposition 2.3 and Lemma 2.3, we need to find a growth-rate \(c(\alpha )\) with certain regularity (2.21) and satisfying the inequality (2.35), and a time-dependent pseudo-interface \(z(t,\alpha )\) satisfying the regularity assumptions (2.22)-(2.24) and the relations (2.33a) (2.36).
3 The Growth-Rate
In this section we declare a suitable growth-rate c, and also a partition of the unity \(\{\psi _0,\psi _1\}\) as discussed in the intro, in terms of \(z^\circ \in C^{1,\delta }({\mathbb {T}};{\mathbb {R}}^2)\). Let us recall what we need. On the one hand, we must construct a regular enough c (2.21) satisfying the inequality (2.35) uniformly on \(\{c(\alpha )>0\}\). At the same time, for the relation (2.36b) it is convenient to control the monotonicity of c near the boundary of \(\{c(\alpha )>0\}\). On the other hand, we shall construct \(\{\psi _0,\psi _1\}\) subordinated to \(\{\partial _{\alpha }z_1^\circ (\alpha )>0\}\) and \(\{c(\alpha )>0\}\) respectively, and satisfying \(\partial _{\alpha }z_1^\circ > 0\) uniformly on \(\mathrm {supp}\,\psi _0\).
In view of Fig. 3, it seems clear that we have enough flexibility to construct such functions. The aim of this section is to make it quantitatively.
A regular growth-rate \(c(\alpha )\ge 0\) (blue) satisfying the inequality \(|2c(\alpha )+\partial _{\alpha } z_1^\circ (\alpha )|<1\) (gray zone) uniformly on \(\{c(\alpha )>0\}\). A partition of the unity \(\{\psi _0,\psi _1\}\) subordinated to \(\{\partial _{\alpha }z_1^\circ (\alpha )>0\}\) and \(\{c(\alpha )>0\}\) respectively, and satisfying \(\partial _{\alpha }z_1^\circ > 0\) uniformly on \(\mathrm {supp}\,\psi _0\)
Let us introduce the following sets \(I_\eta \) which will be very useful for these purposes.
Lemma 3.1
Given \(-1\le \eta \le 1\) we denote
This forms an ascending chain of open subsets of \({\mathbb {T}}\). Furthermore, for any \(-1<\eta _1<\eta _2<1\), we have \(I_{\eta _1}\subset \subset I_{\eta _2}\) with
Proof
First of all notice that \(\partial _{\alpha }z_1^\circ ({\mathbb {T}})=[-1,1]\). Hence, there is \(\alpha _j\in \partial I_{\eta _j}\) for \(j=1,2\), and thus
as we wanted to prove. \(\square \)
In order to interpolate between the Classical and the Mixing Muskat problem, we take a partition of the unity \(\{\psi _0,\psi _1\}\subset C_c^\infty ({\mathbb {T}};[0,1])\) as follows. Firstly, we define the indicator function
in terms of some parameters \(0<\eta ,s<1\) to be determined. With \(\chi _{\eta ,s}\) we declare
where \(\phi _r\) is a standard mollifier, namely \(\phi _r(\alpha ):=\tfrac{1}{r}\phi (\tfrac{\alpha }{r})\) for some fixed \(\phi \in C_c^\infty (-1,1)\) satisfying \(\phi \ge 0\) and \(\int \phi =1\), and \(r>0\) is given in (3.2). Hence,
Among all the possible choices for c, we declare
where \((\partial _{\alpha }z_1^\circ )_-:=-\min (\partial _{\alpha }z_1^\circ ,0)\). This c is smooth with
and satisfies \(c\ge \psi _1\eta /2\) with \(\mathrm {supp}\,c=\mathrm {supp}\,\psi _1\subset {\bar{I}}_\eta \). In the next lemma we show that we can take \(\eta \) and s in such a way that the inequality (2.35) holds.
Lemma 3.2
The growth-rate (3.4) satisfies
Proof
By writing \(f=f_+-f_-\) for \(f=\partial _{\alpha }z_1^\circ \), we split
On the one hand, \(\eta \psi _1\le \eta \) and also \(f_+\le \eta \) on \({\bar{I}}_{\eta }\) \((\supset \mathrm {supp}\,c)\) by (3.1). On the other hand, by (3.2)
This concludes the proof. \(\square \)
Let us assume from now on that \(s<1/3\). In the next lemma we show that \(\partial _{\alpha }z_1^\circ > 0\) uniformly on \(\mathrm {supp}\,\psi _0\) \((\supset \supset {\mathbb {T}}\setminus \mathrm {supp}\,c)\), which will be crucial for the energy estimates in Sect. 5.
Lemma 3.3
It holds that
Proof
Let \(\alpha \in \mathrm {supp}\,\psi _0\). If \(\alpha \notin I_\eta \), simply \(\partial _{\alpha }z_1^\circ (\alpha )\ge \eta \) by (3.1). Assume now that \(\alpha \in I_\eta \). Since \(\psi _1\equiv 1\) on the open set \(I_\eta \setminus {\bar{B}}_{2r}(\partial I_\eta )\) by (3.2) (3.3), necessarily \(\alpha \in {\bar{B}}_{2r}(\partial I_\eta )\). Hence, there is \(\alpha _\eta \in \partial I_\eta \) satisfying \(|\alpha -\alpha _\eta |\le 2r\), and thus
where we have applied (3.2). \(\square \)
Next we turn to the behavior of c inside \(\{c(\alpha )>0\}\). Of course c is monotone in a neighborhood of \(c(\alpha )=0\) and away from zero outside it, but we give bounds for these properties that only depends on \(s,\eta ,\delta \).
Lemma 3.4
Let \(I=(\alpha _1,\alpha _2)\) be a connected component of \(\{c(\alpha )>0\}\) and denote \({\bar{\alpha }}:=\tfrac{1}{2}(\alpha _1+\alpha _2)\). If \(|I|<2r(1/s-1)\), then c is monotone on \([\alpha _1,{\bar{\alpha }}]\) and \([{\bar{\alpha }},\alpha _2]\). Otherwise, c is monotone on each connected component of \(I\cap B_{2r}(\partial I)\), while \(c\ge \eta /2\) on \(I\setminus B_{2r}(\partial I)\). Moreover \(\psi _1\eta /2<c\) everywhere.
Proof
First of all observe that \(\phi _{r}*(\partial _{\alpha }z_1^\circ )_-=0\) (and so \(c=\psi _1\eta /2\)) outside \(B_r(I_0)\).
Case \(|I|<2r(1/s-1)\). Given \(\alpha \in B_r(I_0)\), Lemma 3.1 and (3.2) imply that
Thus, necessarily \(\alpha \notin I\). Then, \(I\cap B_r(I_0)=\emptyset \) and so \(c=\psi _1\eta /2\) with \(\psi _1\) monotone on \([\alpha _1,{\bar{\alpha }}]\) and \([{\bar{\alpha }},\alpha _2]\) by construction (3.2) (3.3).
Case \(|I|\ge 2r(1/s-1)\). Given \(\alpha \in B_{2r}(I_0)\) and \(\beta \in B_r(\partial I)\), Lemma 3.1 and (3.2) imply that
Hence, \(B_{2r}(\partial I)\cap B_r(I_0)=\emptyset \) and so \(c=\psi _1\eta /2\) on \(I\cap B_{2r}(\partial I)\) with \(\psi _1\) monotone on each connected component of \(I\cap B_{2r}(\partial I)\). Finally, \(c\ge \psi _1\eta /2\) with \(\psi _1\equiv 1\) on \(I\setminus B_{2r}(\partial I)\). \(\square \)
Finally, Lemma 3.4 implies the following estimates which will be useful to control (2.36b).
Corollary 3.1
In the context of Lemma 3.4, let us denote
Then, for \(k=0,1\), we have
in terms of \((\eta /|\partial _{\alpha }z_1^\circ |_{C^\delta })^{1/\delta }\), \(1/\eta \) and \(\Vert \partial _{\alpha }^kc\Vert _{L^1}\).
Proof
Case \(|I|<2r(1/s-1)\). For all \(\alpha \in I\), the monotonicity of c on \(I(\alpha )\) implies
with \(|I(\alpha )|\le r(1/s-1)=(1-s)(\eta /|\partial _{\alpha }z_1^\circ |_{C^\delta })^{1/\delta }\le (\eta /|\partial _{\alpha }z_1^\circ |_{C^\delta })^{1/\delta }\).
Case \(|I|\ge 2r(1/s-1)\). For all \(\alpha \in I\cap B_{2r}(\partial I)\), the previous argument works with \(|I(\alpha )|\le 2r\le (\eta /|\partial _{\alpha }z_1^\circ |_{C^\delta })^{1/\delta }\). Finally, for all \(\alpha \in I\setminus B_{2r}(\partial I)\), simply
because \(c(\alpha )\ge \eta /2\). \(\square \)
From now on we fix the parameters \(\eta \) and s satisfying \(\eta (2+s^\delta )<1\) with \(s<1/3\). We remark that they are not necessarily very small (e.g. we can take \(\eta =s=\tfrac{1}{4}\) for \(\delta =1\)).
4 The Pseudo-Interface
We define our pseudo-interface z as the solution of the integro-differential equation
given by the operator
where \(\tau \) is given in (1.12), \(\{\psi _0,\psi _1\}\) is the partition of the unity we fixed in (3.3) and c the growth-rate (3.4). The operator \(E(t,z^\circ ,z)\) extending B outside \(tc(\alpha )=0\) was already introduced in (2.10),
Thus, it expands as
The term \(E^{1)}(t,z^\circ )\) is
where \(E^{(0)}(z^\circ )\) and \(E^{(1)}(z^\circ )\) are
with
The terms \(\kappa (z^\circ )\) and \(D^{(0)}(z^\circ )\) are
The term \(h(t,z^\circ ,z)\) is the time-dependent average defined on each connected component \((\alpha _1,\alpha _2)\) of \(\{c(\alpha )>0\}\) as
where
We notice that, although h is piecewise constant, \(h\psi _1\) is smooth in \(\alpha \) (recall \(\psi _1\lesssim c\) by Lemma 3.1).
As we will see in the next lemmas, \(E^{(0)}=E|_{t=0}\), \(E^{(1)}=\partial _tE|_{t=0}\), \(z_b^{(1)}=\partial _tz_b|_{t=0}\) and \(D^{(0)}=D|_{t=0}\). Thus, \(E^{1)}\) equals to the first order expansion in time of E. In addition, we will see that \(\kappa =\partial _t(E-B)|_{t=0}\).
In the rest of this section we will assume that there exists a solution z of Eq. (4.1) satisfying (2.22)–(2.24) and show that this implies that z satisfies (2.33a) (2.36) as well.
Theorem 4.1
Let \(z^\circ \in H^{k_\circ }({\mathbb {T}};{\mathbb {R}}^2)\) be a closed chord-arc curve with \(k_\circ \ge 6\). Assuming that, for some \(T>0\), there exists \(z\in C_tH^{k_\circ -2}\) with \(\partial _tz\in C_tH^{k_\circ -3}\) solving (4.1) and satisfying (2.23) (2.24), then z satisfies (2.33a) (2.36).
The proof of this theorem relies on the forthcoming Lemmas 4.1–4.5. We start by rewriting some of the terms suitably. Let us observe that, assuming (4.1), the l.h.s. of (2.36a) reads, for \(a=\pm \), as
and for (2.36b) we have
The core of the section is to prove that E remains close to B in \(L^\infty \). In Lemma 4.2 we show that \(E-B_a=O(t(c+|\partial _{\alpha }c|))\). This is sufficient for (2.36a). Indeed, we show in Lemma 4.3 that \(E-B-t\kappa =O(t^2(c+|\partial _{\alpha }c|))\), which is sufficient for (2.36b). In particular, this implies that \(\kappa =\partial _t(E-B)|_{t=0}\) (a similar term appears in [43, 64]). Both estimates are based on a nice technical consequence of the argument principle Lemma 4.1 (a related argument appears in [58, Lemma 4.2]). In Lemma 4.4 we show that \(D-D^{(0)}\partial _{\alpha }z\cdot \partial _{\alpha }z^\circ =O(t)\). The term h has been introduced because (2.36b) reads as
This requires to obtain a cancellation for \(\alpha =\alpha _2\), which is equivalent to (4.4). Finally, we show in Lemma 4.5 that h, \(E-E^{1)}=O(t^2)\). All the ingredients are ready to prove Theorem 4.1.
In the proof of Lemmas 4.1–4.5 all the assumptions in Theorem 5.1 are valid. We start with the technical lemma.
Lemma 4.1
For all \(k\in {\mathbb {N}}\), the function
is uniformly bounded on \(c(\alpha )>0\), \(0<t\le T\) and \(\lambda ,\mu \in [-1,1]\) with \(\lambda \ne \mu \).
Proof
First of all, by adding and subtracting \(\partial _{\alpha }z_{\mu }'/\partial _{\alpha }z_{\mu }\) (recall Sect. 1 Notation) we split
The first term is controlled by \({\mathcal {C}}(c,z)\) and \(\Vert \partial _{\alpha }z_{\mu }\Vert _{C_tC^{0,\delta }}\) (recall (2.24)). The identity (4.8) allows to prove the result by induction on k. For \(k=1\), the second integral in (4.8) is explicit (cf. (2.28))
where we have applied the Cauchy’s argument principle for \(\lambda \ne \mu \) and \(tc(\alpha )>0\). For \(k\ge 2\), an integration by parts yields
where
This \(S_{\lambda ,\mu }^{k-1}\) is controlled by \({\mathcal {C}}(c,z)\) while \(C_{\lambda ,\mu }^{k-1}\) is bounded by induction hypothesis. Furthermore, this recursive formula for \(C_{\lambda ,\mu }^k\) yields (\(S_{\lambda ,\mu }^0=0\))
which is bounded by \({\mathcal {C}}(c,z)\) and \(\Vert \partial _{\alpha }z_{\mu }\Vert _{C_tC^{0,\delta }}\). \(\square \)
Lemma 4.2
For \(0\le t\le T\) it holds that
Proof
Notice that \(E=B=B_+=B_-\) for \(tc(\alpha )=0\). Consider now \(tc(\alpha )\ne 0\). Recall from (2.31) that \(B_{a,b}\) is split into
where \(C_{a,b}^1\) is given in (4.7) and
Then, for \(b=-a\), we have
The last term is \(O(t|\partial _{\alpha }(c\tau )|)\) by Lemma 4.1. For the first term, the fundamental theorem of calculus yields
Let us check that we can apply the Fubini’s theorem. By using the regularity conditions (2.21)–(2.24), then (4.12) can be bounded by
Hence, the Fubini’s theorem allows to interchange the order of integration of \(\lambda \) and \(\beta \) in (4.12). Then, by adding and subtracting \(\beta \partial _{\alpha }^2z_b\) in (4.12), we get
where, by applying the Taylor’s theorem on the first term and Lemma 4.1 on the second one, we see that (4.14) is O(tc) in terms of \({\mathcal {C}}(c,z)\) and \(\Vert \partial _{\alpha }^2z_b\Vert _{C_tC^{0,\delta }}\). \(\square \)
The next lemma shows that indeed \(\kappa =\partial _t(E-B)|_{t=0}\).
Lemma 4.3
For \(0\le t\le T\) it holds that
Proof
Notice that
with \(E-B_a\) given in (4.11). We start with some auxiliary computations. By combining (4.10) and (4.14) we get, for \(b=-a\),
where \(S_{\lambda ,b}^j\) is given in (4.9). Notice that
Furthermore, it is easy to see that \(S_{\lambda ,b}^{j}-S_{\lambda ,0}^{j}=O(t)\) by the regularity conditions (2.21)–(2.24). Then, by writing \(\partial _{\alpha }z_b=\partial _{\alpha }z-itb\partial _{\alpha }(c\tau )\), it follows that
Therefore, analogously to (4.12) (4.13), the fundamental theorem of calculus jointly with the Fubini’s theorem yield (recall (4.11))
For \(I_1\), by adding and subtracting \(c\tau \) and \(\tfrac{1}{2}\beta ^2\partial _{\alpha }^3z\), we split it into
where
The first term of \(I_1\) is \(O((tc)^2)\) by Lemma 4.1 and the commutators are \(O(t^2c)\) in terms of \(\Vert z\Vert _{C_tC^{3,\delta }}\lesssim \Vert z\Vert _{C_tH^4}\). Similarly, by adding and subtracting \(c\tau \) and \(\beta \partial _{\alpha }^2z\) for \(I_2\), we gain commutators of order \(O(t^2c)\), while the remaining term reads as
where we have applied Lemma 4.1. For \(I_3\), (4.10) yields
and thus
Finally, a direct computation shows that
and also for \(I_4\)
in terms of \(\Vert \partial _t z\Vert _{C_tC^{2,0}}\lesssim \Vert \partial _t z\Vert _{C_tH^3}\). \(\square \)
The next lemmas deal with D, h and \(E^{1)}\).
Lemma 4.4
For \(0\le t\le T\) it holds that
Proof
Recall that \(D=-\frac{1}{2}(B_+-B_-)+D^{(0)}\). Then, the statement follows from Lemma 4.2 since
and using that \(\partial _{\alpha }z\cdot \partial _{\alpha }z^\circ =1+O(t)\). \(\square \)
Lemma 4.5
For \(0\le t\le T\) it holds that
Proof
Recall the definition of \(E^{(0)}\) and \(E^{(1)}\) in (4.2). First of all we observe that, in analogy with the Hilbert transform, it follows that \(E^{(0)}\in H^{k_\circ -1}\) and also \(E^{(1)}\in H^{k_\circ -2}\) in terms of the chord-arc constant \({\mathcal {C}}(z^\circ )\) and \(\Vert z^\circ \Vert _{H^{k_\circ }}\). Similarly, by differentiating E in time
Theorem 4.1 provides enough regularity (recall \(k_\circ \ge 6\)) and validity of chord-arc condition to obtain that \(\partial _t E\in C_t H^{k_\circ -4}\) as long as \(0\le t\le T\). In particular, since \(E^{(0)}=E|_{t=0}\), the mean value theorem yields
Hence, recalling the definition of h (4.4) together with Lemmas 4.3 and 4.4, it follows that \(h=O(t)\) as well. Then, by writing
it follows from (4.16) and the regularity of the remaining terms that \( \Vert F-E^{(0)}\Vert _{C_tH^{k_\circ -4}}=O(t). \) As a result from (4.1), (4.2) and (4.15), we have \(\partial _t E-E^{(1)}=O(t)\). Notice this implies \(E^{(1)}=\partial _t E|_{t=0}\). Therefore, by applying the fundamental theorem of calculus
we get \(E-E^{1)}= O(t^2)\). Finally, this is enough to update the estimate for h to \(O(t^2)\) as well. \(\square \)
Proof of Theorem 4.1
Proof of (2.33a). On \(tc(\alpha )=0\) we directly have that \(\partial _tz=E=B.\)
Proof of (2.36). Consider now \(tc(\alpha )>0\). For (2.36a), the expression (4.5) and a direct use of Lemmas 4.2 and 4.5 yield that
For (2.36b), we use the expression (4.6). Then, Lemmas 4.3–4.5 imply that
uniformly on \(c(\alpha )>0\). Firstly, recall that \(\psi _1\lesssim c\) by Lemma 3.1. Secondly, if \(\alpha \) is closer to \(\alpha _1\), Corollary 3.1 controls the integrals \(\int _{\alpha _1}^\alpha c\,\mathrm {d}\alpha '\) and \(\int _{\alpha _1}^\alpha |\partial _\alpha c|\,\mathrm {d}\alpha '\) in terms of \(c(\alpha )\). Hence, the four terms above are \(O(t^2c(\alpha ))\).
If \(\alpha \) is closer to \(\alpha _2\), Corollary 3.1 yields control on \(\int _{\alpha }^{\alpha _2} c \,\mathrm {d}\alpha '\) and \(\int _{\alpha }^{\alpha _2} |\partial _\alpha c| \,\mathrm {d}\alpha '\) in terms of \(c(\alpha )\). However, by (4.4), it holds that
and thus we can integrate on \((\alpha ,\alpha _2)\). Therefore, for all \(\alpha \in (\alpha _1,\alpha _2)\) the full expression is \(O(t^2c(\alpha ))\). Finally, by dividing by \(tc(\alpha )\) we have proven that (2.36b) holds. \(\square \)
5 Existence of z
Theorem 5.1
Let \(z^\circ \in H^{k_\circ }({\mathbb {T}};{\mathbb {R}}^2)\) be a closed chord-arc curve with \(k_\circ \ge 6\). Then, there exists \(z\in C_tH^{k_\circ -2}\) with \(\partial _tz\in C_tH^{k_\circ -3}\) solving (4.1) and satisfying (2.22)–(2.24) for some \(0<T\ll 1\) depending on the chord-arc constant \({\mathcal {C}}(z^\circ )\) and the norm \(\Vert z^\circ \Vert _{H^{k_\circ }}\).
Remark 5.1
The initial regularity required \(k_\circ =6\) is due to the fact that the energy estimates are easier in \(H^4\), some estimates in the proof of Lemmas 4.3–4.5 and that the pseudo-interface loses two derivatives on the mixing region as in [43, 64].
We split the proof of this theorem into two parts. Firstly, we obtain a priori energy estimates for the Eq. (4.1). Secondly, we explain briefly how (4.1) is regularized in order to use the a priori estimates to show the existence of the desired solution z.
5.1 A Priori Energy Estimates
We will take our energy as
where \({\mathcal {A}}(z)\), \({\mathcal {C}}(z)\) are the angle and the chord-arc constants given in (2.19), (2.20) respectively, and
measures the RT-stability of z on \(\mathrm {supp}\,\psi _0\) (recall \(\sigma =(\rho _+-\rho _-)\partial _{\alpha }z_1\) with \(\rho _{\pm }=\pm 1\)). Notice that \({\mathcal {C}}(z^\circ )<\infty \) by hypothesis and that \({\mathcal {A}}(z^\circ )=1\), \({\mathcal {S}}(z^\circ )\ge 2\eta (1-2s)>0\) by construction (recall Lemma 3.3). It turns out that \(\frac{d}{dt}({\mathcal {A}}(z)^{-1}+{\mathcal {C}}(z)+{\mathcal {S}}(z)^{-1})\) is a lower order term w.r.t. \({\mathcal {E}}(z)\). Analogous terms to \({\mathcal {C}}\) and \({\mathcal {S}}\) are rigorously analyzed in [17, 28]. The term \({\mathcal {A}}\) can be treated with a similar technique.
Next, we analyze the Sobolev norm of (5.1). Given \(0\le k\le k_\circ -2\), we split
We claim that the terms I, \(I_\circ \) and \(I_h\) are controlled from above in terms of \(\Vert z^\circ \Vert _{H^{k_\circ }}\), \(\Vert c\Vert _{H^{k_\circ -1}}\), \(\Vert \psi _j\Vert _{H^{k_\circ -2}}\) for \(j=0,1\), \(\Vert z\Vert _{H^{k_\circ -2}}\), \({\mathcal {A}}(z)^{-1}\), \({\mathcal {C}}(z)\) and \({\mathcal {S}}(z)^{-1}\).
The term \(I_\circ \) is controlled because \(\psi _1\), \(E^{1)}\), \(\kappa \), \(D^{(0)}\), c and \(\tau \) only depends on \(z^\circ \). Indeed, it is clear that \(\psi _1\) and c are smooth by definition (3.3) (3.4), while \(\tau \) and \(D^{(0)}\) lose one derivative and \(\kappa \) loses two (recall (1.12) (4.3)). In analogy with the Hilbert transform (recall (4.2)) it follows that \(E^{(0)}\) loses one derivative and similarly \(E^{(1)}\) loses two, namely
in terms of \({\mathcal {C}}(z^\circ )\) and \(\Vert c\Vert _{H^{k_\circ -1}}\), for some \(q\in {\mathbb {N}}\).
The term \(I_h\) is controlled because h(t) does not depend on \(\alpha \). As we saw in Lemmas 4.2–4.5, it follows that \(\Vert h\Vert _{L^\infty }\) is controlled in terms of \(\Vert z\Vert _{H^3}\), \(\Vert z^\circ \Vert _{H^4}\), \({\mathcal {A}}(c,z)^{-1}\) and \({\mathcal {C}}(c,z)\). These quantities (2.23) and (2.24) are controlled by \({\mathcal {A}}(z)^{-1}\) and \({\mathcal {C}}(z)\) for small times (cf. Lemma B.1).
The term I is expected to be controlled because at the linear level
where \(\Lambda :=(-\Delta )^{1/2}\) and \(\sigma _b=(\rho _+-\rho _-)(\partial _{\alpha }z_b)_1\), which satisfies \(\psi _0\sigma _b\ge 0\) for small times as our energy controls \({\mathcal {S}}(z)^{-1}\) (see the next subsection for a detailed explanation).
5.1.1 Analysis of I
As we mentioned in the introduction, the analysis of I is classical for curves in the fully stable regime. In our case, all the terms are treated classically but the most singular one which needs further analysis. Let us present here the estimate for the main term and discuss the rest in the appendix. We will assume w.l.o.g. that \({\mathbb {T}}=[-\pi ,\pi ]\) (\(\ell _\circ =2\pi \)).
The most singular term in I, for each \(b=\pm \), is (recall Sect. 1 Notation)
Since \(z_b=z-ibtc\tau \), the term with \(\partial _{\alpha }^{k+1}\delta _\beta (c\tau )\) is controlled by \({\mathcal {C}}(z)\) and \(\Vert c\tau \Vert _{H^{k+1}}\). For \(\partial _{\alpha }^{k+1}\delta _\beta z\), by adding and subtracting a suitable term, we split it into
where \(\Lambda =(-\Delta )^{1/2}:H^1\rightarrow L^2\) is the operator
and \(\Phi _b\) is the bounded kernel
For \(J_\sigma \) we proceed as follows. Recall that \(\partial _{\alpha }z_1^\circ >0\) uniformly on \(\mathrm {supp}\,\psi _0\). Indeed, this is why we have opened the mixing zone slightly inside the stable regime. Our energy (5.1) allows to assume that \((\partial _{\alpha }z_b)_1>0\) on \(\mathrm {supp}\,\psi _0\) for later times. Hence, using the Córdoba-Córdoba pointwise inequality \(2f\cdot \Lambda f\ge \Lambda (|f|^2)\) (see [27]) and the fact that \(\Lambda \) is self-adjoint, we deduce that
with the first term controlled by \({\mathcal {C}}(z)\) and \(\Vert z_b\Vert _{C^{2,\delta }}\). Notice that, since the evolution of \((\partial _{\alpha }z_b)_1\) is controlled in terms of our energy \({\mathcal {E}}\), the time of positiveness of \((\partial _{\alpha }z_b)_1\) on \(\mathrm {supp}\,\psi _0\) depends just on the initial data \(z^\circ \).
The estimate of \(J_\Phi \) is classical. We present it here for completeness. By writing \(\partial _{\alpha }^{k+1}\delta _\beta z_b =\partial _{\alpha }\partial _{\alpha }^{k}z_b +\partial _{\beta }\partial _{\alpha }^kz_b'\), we split
where we have integrated by parts w.r.t. \(\alpha \) and \(\beta \) for \(L_1\) and \(L_2\) respectively. On the one hand, \(L_1\) is controlled because we can write
which is bounded in \(C^1\) by \({\mathcal {C}}(z)\) and \(\Vert z_b\Vert _{C^{2,\delta }}\). On the other hand, \(L_2\) is controlled because \(\partial _{\beta }\Phi _b\) is bounded in terms of \({\mathcal {C}}(z)\) and \(\Vert z_b\Vert _{C^3}\).
The analysis of the remaining terms is standard (see e.g. [28]). For completeness, we have presented a compact version in Lemma B.2.
5.2 Regularization
In order to be able to apply the Picard’s theorem we regularize the Eq. (4.1) via
in terms of the parameter \(\varepsilon >0\), where
which agrees with F except that E has been replaced by
Let us fix the open set where the Picard’s theorem is applied. Firstly, let \(O_k\) be the open subset of \(H^k\) formed by chord-arc curves
Secondly, given \(z^\circ \in O_{k_\circ }\) and \(k\le k_\circ \), we define the open neighborhood \(O_k(z^\circ )\) of \(z^\circ \) in \(H^k\) as the set of curves \(z\in O_k\) satisfying, for some fixed parameters \(0<A,C,R,S<\infty \),
and also
From left to right, the conditions in (5.4) establish that the angle between \(\partial _{\alpha }z\) and \(\tau \) is uniformly non-perpendicular, which is necessary for our construction of the mixing zone (cf. Rem. 2.3), and that the chord-arc constant and the \(H^k\)-norm of z are uniformly bounded respectively. Since we want \(z^\circ \in O_k(z^\circ )\), necessarily \(A<{\mathcal {A}}(z^\circ )=1\), \(C>{\mathcal {C}}(z^\circ )\) and \(R>\Vert z^\circ \Vert _{H^k}\). The condition (5.5) establishes that z remains uniformly stable on \(\mathrm {supp}\,\psi _0\). By Sect. 3 (cf. Lemma 3.3) we consider \(S<2\eta (1-2s)\).
Lemma 5.1
Assume that there exists \(z^\varepsilon \in C([0,T_\varepsilon ];O_{k_\circ -2}(z^\circ ))\) solving (5.3) for some \(0<T_\varepsilon \ll 1\). Then, there exists \(q\in {\mathbb {N}}\) satisfying
in terms of A, C, R, S and \(\Vert z^\circ \Vert _{H^{k_\circ }}\), but independently of \(\varepsilon \).
Proof
This is totally analogous to the a priori energy estimates of the previous section (see [28]). \(\square \)
Proof of Theorem 5.1
Step 1 Approximation sequence \(z^\varepsilon \). For all \(\varepsilon >0\), a standard Picard iteration yields a time-dependent curve \(z^\varepsilon \in C([0,T_\varepsilon ];O_{k_\circ -2}(z^\circ ))\) satisfying
This \(T_\varepsilon \) is taken in terms of the parameters defining \(O_{k_\circ -2}(z^\circ )\) in such a way that the conditions (B.1) (B.2) hold. Thus, the operators \(B_{a,b}\) (and so h) are well-defined.
As usual, the Gronwall’s inequality applied to (5.6) implies that \(\Vert z^\varepsilon \Vert _{C([0,T_\varepsilon ];H^{k_\circ -2})}\) is uniformly bounded in \(\varepsilon \). Furthermore, \(z^\varepsilon \) satisfies (5.3) with \(\Vert \partial _tz\Vert _{C([0,T_\varepsilon ];H^{k_\circ -3})}\) uniformly bounded in \(\varepsilon \). We notice that our system is not autonomous but smooth in time. All these facts guarantee that the times of existence \(T_\varepsilon \) do not vanish as \(\varepsilon \rightarrow 0\), namely \(T_\varepsilon \ge T> 0\).
Step 2 Convergence to z. By the Rellich–Kondrachov and the Banach–Alaoglu theorems, we may assume (taking a subsequence if necessary) that there exists \(z\in C([0,T];O_{k_\circ -2}(z^\circ ))\) such that \(z^\varepsilon \rightarrow z\) in \(C_tH^{k_\circ -3}\) and also \(\partial _{\alpha }^{k_\circ -2}z^\varepsilon \rightharpoonup \partial _{\alpha }^{k_\circ -2}z\) as \(\varepsilon \rightarrow 0\). Furthermore, \(\partial _tz\in C([0,T];H^{k_\circ -3})\). Finally, it follow that z solves (4.1) and satisfies (2.22)–(2.24). \(\square \)
6 Proof of the Main Results and Generalizations
In this section we glue the several proofs of the previous sections to gain clarity of how the Theorems 1.1 and 1.2 are proved. In addition, we recall how this construction is generalized for piecewise constant coarse-grained densities.
6.1 Proof of Theorems 1.1 and 1.2
First of all we construct the growth-rate c and the partition of the unity \(\{\psi _0,\psi _1\}\) as in (3.4) and (3.3) respectively, in terms of \(z^\circ \) and some small parameters \(\eta ,s\) (e.g. \(\eta =s=\tfrac{1}{4}\), \(\delta =1\)). By Lemma 3.2, this c satisfies the inequality (2.35) and the regularity condition (2.21) (indeed \(c\in C^\infty \)).
Once these functions are fixed, the Theorem 5.1 implies the existence of a time-dependent pseudo-interface z satisfying the Eq. (4.1) and the regularity conditions (2.22)–(2.24) for some \(T\ll 1\). By Theorem 4.1, this z satisfies the growth conditions (2.33a) (2.36).
Next, we construct the mixing zone \(\Omega _{\mathrm {mix}}\) and the non-mixing zones \(\Omega _{\pm }\) by (1.10) (2.17) respectively. Then, we define the triplet \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) by (2.26) (2.27) (2.32). Hence, by Proposition 2.3 and Lemma 2.3, \(({\bar{\rho }},{\bar{v}},{\bar{m}})\) is a subsolution to IPM for some \(0<T'\le T\).
Finally, the h-principle in IPM (Theorem 2.1) yields infinitely many mixing solutions to IPM starting from (1.1) (1.6).
The proof of Theorem 1.2 is analogous to the one of Theorem 1.1. The main difference for the asymptotically flat case is that, since the domain of integration is \({\mathbb {R}}\) instead of \({\mathbb {T}}\), most of the integrals are taken with the Cauchy’s principal value at infinity. In this case, (2.28) reads as
which changes the limits (2.30) but not the result. The proof of Theorem 1.2 in the \(x_1\)-periodic case is even closer to the one of Theorem 1.1. In this case (6.1) holds as well, but we do not have to deal with the infinity since the domain is \({\mathbb {T}}\).
6.2 Piecewise Constant Coarse-Grained Densities
Following [43, 64] we split the mixing zone into several levels \(L=\{\lambda _j\,:\,1\le |j|\le N\}\) for \(N\ge 1\) with
namely we consider
with \(z_\lambda \) defined as in (1.11), which satisfies \(\Omega _{\mathrm {mix}}^1\subset \cdots \subset \Omega _{\mathrm {mix}}^N=:\Omega _{\mathrm {mix}}\). In addition we define \(\Omega _{\pm }\) as in (2.17) (or (2.18)).
Analogously to [43, 64], we define the piecewise constant (coarse-grained) density as (\(|L|=2N\))
for the closed case (1.6), while for asymptotically flat curves (1.7) the definition (6.2) needs to remove the last \(-1\). Observe that \({\bar{\rho }}=\pm 1\) on \(\Omega _{\pm }\) while \({\bar{\rho }}\) approaches the linear profile in [16, 19, 71] inside the mixing zone.
Analogously to (2.27), the Biot-Savart law yields
Analogously to (2.32), we write the relaxed momentum as
in terms of some
with \(g_j(t,x)\) to be determined. Hence, analogously to (2.41), we define \(g_j\) in \((\alpha ,\lambda )\)-coordinates as
where
Finally, using that
the condition \(|\gamma |<\tfrac{1}{2}\) yields the more general regime for c given in (1.8) as \(N\rightarrow \infty \) (cf. (2.40)) . The rest follows analogously to the case \(N=1\) (see [43, 64]).
Change history
14 July 2022
The publisher introduced an error in the last sentence of the proof for Lemma 3.2. Its beginning "The supremum of $\widetilde{W}(LB,UB)$" must be replaced by "The supremum of $\overline{W}(LB,UB)$".
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Acknowledgements
AC, DF and FM are supported by grants SEV2015-0554, CEX2019-000904-S and RED2018-102650-T funded by: MCIN/AEI/ 10.13039/501100011033. AC is supported by grants Europa Excelencia program ERC2018-092824, MTM2017-89976-P and PID2020-114703GB-I00 funded by: MCIN/AEI/ 10.13039/501100011033. DF is partially supported by the Line of excellence for University Teaching Staff between CM and UAM. DF and FM are partially supported by the ERC Advanced Grant 834728 and by the MTM2017-85934-C3-2-P.
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Appendices
The Pressure
Lemma A.1
Let \((\rho ,v)\) be a mixing solution from Theorem 1.1 or 1.2. Then, there exists a pressure p satisfying the Darcy’s law
for every test function \(\Phi \in C_c^2({\mathbb {R}}^3;{\mathbb {R}}^2)\). Observe that (A.1) agrees with (2.11c) for \(\Phi =\nabla ^\perp \phi \).
Moreover, \(v=\nabla ^\perp \psi \) with p and \(\psi \) the continuous functions given by
The first term corresponds to the macroscopic contribution of \({\bar{\rho }}\) (cf. (A.3)). The second one is the fluctuation coming from \(\rho -{\bar{\rho }}\) and vanishes outside \(\Omega _{\mathrm {mix}}\) (cf. (A.2)).
Furthermore, for any fixed \({\mathscr {E}}\in C({\mathbb {R}}_+;{\mathbb {R}}_+)\) with \({\mathscr {E}}(r)>0\) for \(r>0\), we can select these (infinitely many) mixing solutions satisfying
where
Proof
Notice that \({\bar{v}}=\nabla ^\perp {\bar{\psi }}\) by (2.27). In particular,
in the sense of distributions. Following [19, 57, 71] we consider the convex integration sequence \((\rho _k,v_k)\rightarrow (\rho ,v)\) in \(C_tL_{w^*}^\infty \). In fact, \(\rho _k\rightarrow \rho \) in \(C_tL_{\text {loc}}^q\) for all \(1<q<\infty \) (see [57, p. 12]). Let us split \(\rho _k={\bar{\rho }}+\rho _k'\), \(v_k={\bar{v}}+v_k'\) and \(p_k:={\bar{p}}+p_k'\) for some \(p_k'\) to be determined. By construction (see [57, Lemma 3.1]) \((\rho _k',v_k')=(\Delta \varphi _k',-\nabla ^\perp \partial _1\varphi _k')\) for some real-valued function \(\varphi _k'\) which is smooth and compactly supported on \(\Omega _{\mathrm {mix}}\). Notice that \(v_k'=\nabla ^\perp \psi _k'\) for \(\psi _k':=-\partial _1\varphi _k'\). Hence, \(p_k\) satisfies \(\nabla (p_k+i\psi _k)=-i\rho _k\) if and only if \(p_k'\) satisfies
Therefore (\(\Delta =\nabla \nabla ^*\))
for some (time-dependent) entire function \(f_k\). Since \(\varphi _k'\) is compactly supported on \(\Omega _{\mathrm {mix}}\), necessarily \((f_k(t,x))_2\rightarrow 0\) as \(|x|\rightarrow \infty \). Therefore, the Liouville’s theorem (\(e^{if_k(t)}\) is entire and bounded) implies that \(f_k\) equals to a (time-dependent) real constant. Hence, as we are choosing \(p_k'\), we may assume that \(f_k=0\). Finally, the Cauchy-Pompeiu’s formula yields
This concludes the proof by taking the limit \(k\rightarrow \infty \). The inequality (A.2) can be guaranteed by following the proof of the quantitative h-principle in [19]. \(\square \)
Auxiliary Lemmas
Lemma B.1
Let \(z\in C([0,T];C^{1,\delta }({\mathbb {T}};{\mathbb {R}}^2))\). Assume that, for some parameters \(0<A,C,R,S<\infty \),
for all \(0\le t\le T\). Then, there exists \(0<T'(A,C,R,S,\delta ,\Vert c\tau \Vert _{C^{1,\delta }})\le T\) such that the equi-chord-arc condition holds:
for all \(\alpha ,\beta \in {\mathbb {T}}\), \(\lambda ,\mu \in [-1,1]\) and \(0\le t\le T'\), where \(D\equiv 1-\sqrt{1-(A/2)^2}\). In addition,
Proof
First of all notice that \(A<1\), and thus \(D< 1\) as well. In particular, (B.1) holds for \(tc(\alpha )=0\). Henceforth, let \(c(\alpha )>0\) and \(0<t\le T'\) for some \(0<T'\le T\) to be determined. Notice that we can take \(T'\) satisfying (recall Sect. 1 Notation)
We split the proof into two cases, depending on the following parameter
Case \(|\beta |\le r\). By writing,
we split the l.h.s. of (B.1) into
Let us analyze its third term. By our choice of r and using \(|\partial _{\alpha }z|\ge 1/C\), we can take \(T'\) satisfying
Then, by adding and subtracting \(\partial _{\alpha }z/|\partial _{\alpha }z|\), we deduce that (recall (1.11) (1.12))
which implies that
Finally, by applying (B.3) and (B.6) into (B.5), we deduce that
Case \(|\beta |>r\). On the one hand, by applying (B.3) (B.4), the l.h.s. of (B.1) can be bounded from below as
On the other hand, the r.h.s. of (B.1) can be bounded from above as
Thus, it is enough to guarantee that
or equivalently
Since \(D\ll 1\), this holds for all \(|\beta |>r\) by taking \(T'\) small enough.
Finally, it is clear that (B.2) holds for small times. \(\square \)
Lemma B.2
The remaining terms of I from Sect. 5.1.1 are lower order terms.
Proof
By combining the general Leibniz rule applied to \((\psi _0,K_b,\partial _{\alpha }\delta _\beta z_b)\) where
with the Faà di Bruno’s formula applied to the kernel \(K_b\), we split (\(j=(j_0,j_1,j_2)\))
where
with \(\pi _{j_1}:=\{n\in {\mathbb {N}}_0^{j_1}\,:\,n_1+2n_2+\cdots +j_1n_{j_1}=j_1\}\) and
The most singular term \(j=(0,0,k)\) (\(\Rightarrow n=0\)) has been analyzed in Sect. 5.1.1.
Second singular term. Let us consider \(j=(0,k,0)\). If \(n_k=1\) then
By splitting \(\partial _{\alpha }\delta _\beta z_b\) into its real and imaginary part and comparing
we obtain a Hilbert transform acting on \(\partial _{\alpha }^kz_b\) while the commutator is a bounded kernel as in (5.2). If \(n_k=0\), notice that for any \(k\ge 3\) we have \(n_{k-1}\le \frac{k}{k-1}<2,\) that is \(n_{k-1}=0\) or 1 (the case \(k<3<k_\circ -2\) is easier). If \(n_{k-1}=1\) (\(\Rightarrow n_1=1\)) then simply
and for \(n_{k-1}=0\)
Third singular term. Let us consider \(j=(0,1,k-1)\) (\(\Rightarrow n=1\)):
This is analogous to the case (0, k, 0). The case \(j=(1,0,k-1)\) is analogous too. Let us consider now \(j=(0,k-1,1)\). If \(n_{k-1}=1\) then
and so
If \(n_{k-1}=0\) then (B.7) holds. The case \(j=(1,k-1,0)\) is analogous.
Harmless terms. For \(0\le j_1,j_2\le k-2\), simply
This concludes the proof. \(\square \)
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Castro, Á., Faraco, D. & Mengual, F. Localized Mixing Zone for Muskat Bubbles and Turned Interfaces. Ann. PDE 8, 7 (2022). https://doi.org/10.1007/s40818-022-00121-w
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DOI: https://doi.org/10.1007/s40818-022-00121-w