Abstract
Numerical computations in viscoelasticity show the failure of many numerical schemes when the Weissenberg number is beyond a critical value Keunings (J Non-Newtonian Fluid Mech 20:209–226, 1986, [6]). The existence of singularities in the continuum model could be the way to explain instability appearing in numerical simulations. We consider here a 2D Oldroyd-B type model at high Weissenberg number, and we show the existence of the so-called splash singularities (namely, points where the free boundary remains smooth but self-intersects). In our case, we assume physically realistic boundary conditions given by the static equilibrium of all the force fields acting at the interface. Our strategy is based on local existence and stability results applied to a family of smooth suitable initial configurations, we show they will evolve into a self-intersecting configuration, and then necessarily there exists a positive time \(t=t^*\), where the configuration has a splash singularity. To prove local existence and stability, we first apply a conformal transformation to the 2D domain, in order to separate the contact point with splash, and then we pass into Lagrangian coordinates to fix our domain, inspired by a Thomas Beale’s paper on the initial value problem for the Navier–Stokes equations with a free surface.
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Keywords
1 Introduction
In this paper, we study a viscoelastic fluid model of Oldroyd-B type at high Weissenberg number. The goal of this paper is to study the existence of splash singularity for the following system:
with appropriate boundary conditions, which will be explained later.
Incompressible viscoelastic fluids are described classically by the following momentum balance equations:
where \(\tau =\nu _s(\nabla u+\nabla u^T)+\tau _p\) denotes the stress, \(\nu _s\) is the solvent viscosity, and \(\tau _p\) is the stress related to the elastic part. From now on, we assume \(\bar{\rho }=1\).
The stress tensor satisfies the well-known Oldroyd-B model
where
-
\(\partial _t^{uc}\tau =\partial _t\tau + (u\cdot \nabla )\tau -\nabla u^T \tau -\tau \nabla u\) denotes the upper convective time derivative,
-
\(\nu _0=\nu _s+\nu _p\) denotes the material viscosity, \(\nu _s\) the solvent viscosity, and \(\nu _p\) the polymeric viscosity, respectively,
-
\(\lambda \) the relaxation time, and
-
\(\lambda _s=\frac{\nu _s}{\nu _0}\lambda \).
By separating the solvent and the polymeric contributions to the stress, we get that the stress \(\tau _p\) satisfies
Moreover, combining the equations for the stress together with the equations for the mass and the momentum balance, it follows
In the study of this type of non-Newtonian fluids, an important role is played by the relaxation time \(\lambda \), which in our case turns out to be proportional to the Weissenberg number \(\text {We}\), a number which measures the ratio between the viscous and the elastic forces, see [11]. For very high Weissenberg number \((\text {We}\rightarrow \infty )\), the system (3) reduces to the following one:
Let us denote with \(\alpha \in \mathbb {R}^2\) the Lagrangian coordinate and let \(X(t,\alpha )\) be the flux associated with the velocity u. Then, by applying the chain rule, the deformation gradient \(F(t,X)=\frac{\partial X}{\partial \alpha }\) satisfies the following transport equation:
If the initial condition \(\tau _p(0,X)=\tau _0(X)\) is positive definite, then \(\tau _p(t,X)=F\tau _0 F^T\) is also positive definite and satisfies the equation
This allows us to solve the system (1), instead of (4). By imposing that the physical boundary conditions are given by the static equilibrium of the force fields at the interface, the free-boundary problem for the system (1) is
We also assume \(\text {div}F_0=0\), therefore \(\text {div}F=0\), for all t. The variable domain \(\varOmega (t)\subset \mathbb {R}^2\) denotes the region occupied by the fluid. Our main result is stated in the following theorem.
Theorem 1.
There exists a time \(t^*\in [0,T]\) such that the interface \(\partial \varOmega (t^*)\) self-intersects in one point.
Similar results for the Navier–Stokes equations are obtained by Castro, Córdoba, Fefferman, Gancedo and Gómez-Serrano in [2] and by Coutand and Shkoller in [3]. In our paper, the main problem is the presence of the elastic components, which could prevent the development of splash singularity. We prove that this is not the case.
One of the important ingredients in the proof is the use of a conformal map that has been introduced for this specific problem in [2]. The map \(P(z)=\tilde{z}\), for \(z\in \mathbb {C} \setminus \varGamma \), is defined as a branch of \(\sqrt{z}\), where \(\varGamma \) is a line, passed through the splash point. We take \(z\in \mathbb {C} \setminus \varGamma \) in order to make \(\sqrt{z}\) an analytic function. The key idea, to prove our theorem is to make the analysis into the Lagrangian framework, in order to have a fixed boundary, as done in the paper of Beale [1] to analyze the free boundary of the Navier–Stokes equations. The geometric ideas behind the proof are inspired from the construction in [2]. The main steps are explained below with the help of Fig. 1.
-
Let the initial domain \(\varOmega _0\) be a non-regular domain as (b); for this reason, we use the conformal map P and by projection we get \(\tilde{\varOmega }_0\), a non-splash domain.
-
If \(\{\tilde{\varOmega }_0, \tilde{u}(0,\cdot ), \tilde{p}(0,\cdot ), \tilde{F}(0,\cdot )\}\) are smooth, we can prove the existence of a local solution \(\{\tilde{\varOmega }(t), \tilde{u}(t,\cdot ), \tilde{p}(t,\cdot ), \tilde{F}(t,\cdot )\}\), \(t\in [0,T]\).
-
By a suitable choice of the initial velocity, in particular \(\tilde{u}(0,\tilde{z}_1)\cdot n>0,\) \(\tilde{u}(0,\tilde{z}_2)\cdot n>0\) such that there exists \(\bar{t}>0\) and \(P^{-1}(\tilde{\varOmega }(\bar{t}))\) is as (c). This solution lives in the tilde complex plane and cannot be transformed, by \(P^{-1}\), into a solution in the non-tilde complex plane.
-
To solve the problem in the non-tilde domain, we take a one-parameter family \(\{\tilde{\varOmega }_{\varepsilon }(0),\tilde{u}_{\varepsilon }(0), \tilde{F}_{\varepsilon }(0)\}\), with \(\tilde{\varOmega }_{\varepsilon }(0)=\tilde{\varOmega }_0+\varepsilon b\) and \(|b|=1\), such that \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(0))\) is regular, and there exists a local in time smooth solution \( \{\tilde{\varOmega }_{\varepsilon }(t), \tilde{u}_{\varepsilon }(t,\cdot ), \tilde{p}_{\varepsilon }(t,\cdot ), \tilde{F}_{\varepsilon }(t,\cdot )\}\), which can be inverted in the non-tilde complex plane.
-
By stability we get
$$\text {dist}(\partial \tilde{\varOmega }_{\varepsilon }(\bar{t}),\partial \tilde{\varOmega }(\bar{t}))\le C\varepsilon $$hence \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(\bar{t}))\sim P^{-1}(\tilde{\varOmega }(\bar{t}))\) and so \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(\bar{t}))\) self-intersects.
-
Since \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(0))\) is regular of type (a) and \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(\bar{t}))\) is self-intersecting domain of type (c), and then there exists a time \(t^*\) such that \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(t^*))\) has a splash singularity.
2 Conformal and Lagrangian Transformations
The free-boundary incompressible viscoelastic fluid model in Eulerian coordinates that we intend to study is given in (5). Because of the geometrical singularity induced by the self-intersection point, to start with an initial domain \(\varOmega _0\) which is a splash domain, as in Fig. 1b, we use the conformal transformation \(P(z)=\sqrt{z}\) to set our problem inside a regular domain. The new velocity field is defined as follows
The same for the deformation gradient F
Remark 1.
Defining \(J^P_{kj}=\partial _{X_j}P_k(P^{-1}(\tilde{X}))\), we have the following derivation formulas:
The system in \(\tilde{\varOmega }\) takes the following form:
The next step is to move form Eulerian into Lagrangian coordinates so that we transform a free-boundary problem into a fixed boundary problem. Then, the equation for the flux becomes
Therefore, the Lagrangian variables are given by
The new system in \( [0,T]\times \tilde{\varOmega }_0\) that we are going to study becomes
where \(\tilde{\zeta }=(\nabla \tilde{X})^{-1}\) and \(\nabla _{\varLambda }\tilde{X}=-\varLambda \nabla \tilde{X}\varLambda \), with \(\varLambda =\left( \begin{matrix} 0 &{} -1 \\ 1&{} 0\end{matrix}\right) \), since \(\tilde{n}=-\varLambda J^P_{|\partial \tilde{\varOmega }(t)}\varLambda n\).
3 Local Existence of Smooth Solutions
The idea to prove the local existence is based on a fixed point argument. The iteration will separate the equation in \(\tilde{v}\) from the equation in \(\tilde{G}\). In particular, \(\tilde{G}\) satisfies an ODE, and then it will not interfere in the boundary conditions.
3.1 Iterative Scheme
The iterative scheme is given by the following two steps:
STEP 1
STEP 2
where
The system regarding the flux \(\tilde{X}\) is given by
thus \(\tilde{X}^{(n+1)}\) satisfies
3.2 Analysis of the System (9)
As we mentioned before, we will analyze the linearized system related to STEP 2 by means of the techniques introduced by T. Beale in [1] and their improvements in [2]. Namely, we study
where the compatibility conditions for the initial data are as follows:
We are going to use the following functional spaces:
Therefore on the linearized problem, we recall the following result obtained by Beale, used later on in order to prove the local existence.
Theorem 2.
Let \(2<s<\frac{5}{2}\) and let \(L: X_0\rightarrow Y_0\) be the operator associated with the system (12), then L is invertible and the norm of the inverse is uniformly bounded for any \(0<T<\bar{T}\).
3.3 The Fixed Point Argument
In order to apply Theorem 2 and hence to get bounds independent of T, we need \(\tilde{v}_{|t=0}=0\) and \(\partial _t\tilde{v}_{|t=0}=0\). For this reason, we replace the initial condition \(\tilde{v}_0\) as follows:
where \(\tilde{q}_{\phi }\) is chosen in such a way that for all n, \(\partial _t\tilde{v}^{(n)}_{|t=0}=\partial _t\phi _{|t=0}=0\). The velocity is defined by
Therefore, we can rewrite the system (9) in the following way:
Our main local existence result is then equivalent to show the following theorem.
Theorem 3.
Let \(2<s<\frac{5}{2}\) and \(1<\gamma <s-1\). If \((\tilde{v}(0), \partial _t\tilde{v}(0))=(0,0)\) and \((\tilde{q}(0),\tilde{f}(0),\tilde{g}(0),\partial _t\tilde{g}(0), \tilde{h}(0))=(0,0,0,0,0)\), moreover \(\tilde{G}(0)=\tilde{G}_0\in H^s\), then there exist T (sufficiently small) and a solution \(\{\tilde{X}(\cdot ), \tilde{v}(\cdot ), \tilde{q}(\cdot ), \tilde{G}(\cdot )\}\in \mathscr {F}^{s+1,\gamma }\times \mathscr {K}^{s+1}\times \mathscr {K}^s_{pr}\times \mathscr {F}^{s,\gamma -1}\) on [0, T].
In order to prove this theorem, we need the following technical results.
Proposition 1.
-
1.
Let \(\tilde{G}^{(n)}-\tilde{G}_0\in \mathscr {F}^{s,\gamma -1}\), \(\tilde{X}^{(n)}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }\), and \(\tilde{w}^{(n)}\in \mathscr {K}^{s+1}\) and such that
-
(i)
\(\displaystyle \tilde{G}^{(n)}-\tilde{G}_0\in \left\{ \tilde{G}-\tilde{G}_0\in \mathscr {F}^{s,\gamma -1}\right. :\)
$$\left. \left\| \tilde{G}-\tilde{G}_0-\int _0^t J^P\nabla \phi \tilde{G}_0\,d\tau \right\| _{\mathscr {F}^{s,\gamma -1}} \le \left\| \int _0^t J^P\nabla \phi \tilde{G}_0\,d\tau \right\| _{\mathscr {F}^{s,\gamma -1}}\right\} \equiv B, $$ -
(ii)
\(\left\| \tilde{w}^{(n)}\right\| _{\mathscr {K}^{s+1}}\le N.\)
Then, for \(T>0\) small enough, depending only on \(N, \tilde{v}_0, \tilde{G}_0\),
$$\tilde{G}^{(n+1)}-\tilde{G}_0\in B.$$ -
(i)
-
2.
Let \(\tilde{G}^{(n)}-\tilde{G}_0\), \(\tilde{G}^{(n-1)}-\tilde{G}_0\in \mathscr {F}^{s,\gamma -1}\), with \(\tilde{X}^{(n)}-\tilde{\alpha }\), \(\tilde{X}^{(n-1)}-\tilde{\alpha }\in \mathscr { F}^{s+1,\gamma }\) and \(\tilde{w}^{(n)}, \tilde{w}^{(n-1)} \in \mathscr {K}^{s+1}\) and such that
-
(i)
\(\left\| \tilde{w}^{(n)}\right\| _{\mathscr {K}^{s+1}}\le M\), \(\left\| \tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}\le M\),
-
(ii)
\(\left\| \tilde{X}^{(n)}-\tilde{\alpha }\right\| _{\mathscr { F}^{s+1,\gamma }}\le M\), \(\left\| \tilde{X}^{(n-1)}-\tilde{\alpha }\right\| _{\mathscr { F}^{s+1,\gamma }}\le M\),
-
(iii)
\(\left\| \tilde{G}^{(n)}-\tilde{G}_0\right\| _{\mathscr {F}^{s,\gamma -1}}\le M\), \(\left\| \tilde{G}^{(n-1)}-\tilde{G}_0\right\| _{\mathscr {F}^{s,\gamma -1}}\le M,\)
for some \(M>0\). Then
$$\begin{aligned} \left\| \tilde{G}^{(n+1)}-\tilde{G}^{(n)}\right\| _{\mathscr {F}^{s,\gamma -1}}\le CT^{\delta }&\left( \left\| \tilde{G}^{(n)}-\tilde{G}^{(n-1)}\right\| _{\mathscr {F}^{s,\gamma -1}}+\left\| \tilde{w}^{(n)}-\tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}\right. \\&\left. +\left\| \tilde{X}^{(n)}-\tilde{X}^{(n-1)}\right\| _{\mathscr { F}^{s+1,\gamma }}\right) , \end{aligned}$$for a suitable \(\delta >0\).
-
(i)
Proof.
The proof is given in [4].
Proposition 2.
-
1.
Let \(\tilde{X}^{(n)}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }\), \(\tilde{w}^{(n)}\in \mathscr {K}^{s+1}\) and such that
-
(i)
\(\displaystyle \tilde{X}^{(n)}-\tilde{\alpha }\in \left\{ \tilde{X}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }: \left\| \tilde{X}-\tilde{\alpha }-\int _0^t J^P\phi \,d\tau \right\| _{\mathscr {F}^{s+1,\gamma }}\le \right. \left. \left\| \int _0^t J^P\phi \,d\tau \right\| _{\mathscr {F}^{s+1,\gamma }}\right\} \equiv B_{J^P\phi } \),
-
(ii)
\(\Vert \tilde{w}^{(n)}\Vert _{\mathscr {K}^{s+1}}\le N.\)
Then, for \(T>0\) small enough, depending only on N and \(\tilde{v}_0\),
$$\tilde{X}^{(n+1)}-\tilde{\alpha }\in B_{J^P\phi }.$$ -
(i)
-
2.
Let \(\tilde{X}^{(n)}-\tilde{\alpha }, \tilde{X}^{(n-1)}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }\), with \(\tilde{w}^{(n)}, \tilde{w}^{(n-1)}\in \mathscr {K}^{s+1}\) and such that
-
(i)
\(\left\| \tilde{w}^{(n)}\right\| _{\mathscr {K}^{s+1}}\le M\), \(\left\| \tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}\le M\),
-
(ii)
\(\left\| \tilde{X}^{(n)}-\tilde{\alpha }\right\| _{\mathscr {F}^{s+1,\gamma }}\le M\), \(\left\| \tilde{X}^{(n-1)}-\tilde{\alpha }\right\| _{\mathscr {F}^{s+1,\gamma }}\le M\)
for some \(M>0\). Then
$$\begin{aligned} \left\| \tilde{X}^{(n+1)}-\tilde{X}^{(n)}\right\| _{\mathscr {F}^{s+1,\gamma }}&\le CT^{\delta }\left( \left\| \tilde{X}^{(n)}-\tilde{X}^{(n-1)}\right\| _{\mathscr {F}^{s+1,\gamma }}+\left\| \tilde{w}^{(n)}-\tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}\right) , \end{aligned}$$for a suitable \(\delta >0\).
-
(i)
Proof.
The proof of this theorem is given in [2].
Proposition 3.
-
1.
Let \(\tilde{X}^{(n)}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }\), \(\tilde{q}_w^{(n)}\in \mathscr {K}^s_{pr}\) and \(\tilde{w}^{(n)}\in \mathscr {K}^{s+1}\), and such that
-
(i)
\(\Vert \tilde{X}^{(n)}-\tilde{\alpha }\Vert _{\mathscr {F}^{s+1,\gamma }}\le N\),
-
(ii)
\(\Vert \tilde{G}^{(n)}-\tilde{G}_0\Vert _{\mathscr {F}^{s,\gamma -1}}\le N\),
-
(iii)
\((\tilde{w}^{(n)},\tilde{q}_w^{(n)})\in \left\{ (\tilde{w},\tilde{q})\in \mathscr {K}^{s+1}\times \mathscr {K}^s_{pr}: \tilde{w}_{|t=0}=0, \partial _t\tilde{w}_{|t=0}=0,\right. \)
$$\begin{aligned}&\left. \Vert (\tilde{w},\tilde{q})-L^{-1}(\tilde{f}_{\phi }^L,\tilde{g}_{\phi }^L,\tilde{h}_{\phi }^L)\Vert _{\mathscr {K}^{s+1}\times \mathscr {K}^s_{pr}}\le \Vert L^{-1}(\tilde{f}_{\phi }^L,\tilde{g}_{\phi }^L,\tilde{h}_{\phi }^L)\Vert _{\mathscr {K}^{s+1}\times \mathscr {K}^s_{pr}}\right\} \\&\quad \equiv B_{L^{-1}(\tilde{f}_{\phi }^L,\tilde{g}_{\phi }^L,\tilde{h}_{\phi }^L)}. \end{aligned}$$
Then
$$(\tilde{w}^{(n+1)},\tilde{q}_w^{(n+1)})\in B_{L^{-1}(\tilde{f}_{\phi }^L,\tilde{g}_{\phi }^L,\tilde{h}_{\phi }^L)}.$$ -
(i)
-
2.
Let \(\tilde{X}^{(n)}-\tilde{\alpha }, \tilde{X}^{(n-1)}-\tilde{\alpha }\in \mathscr {F}^{s+1,\gamma }\), \(\tilde{G}^{(n)}-\tilde{G}_0,\tilde{G}^{(n-1)}-\tilde{G}_0\in \mathscr {F}^{s,\gamma -1}\), \(\tilde{w}^{(n)}, \tilde{w}^{(n-1)}\in \mathscr {K}^{s+1}\), with \(\tilde{w}^{(n)}_{|t=0}=\tilde{w}^{(n-1)}_{|t=0}=0\), \(\partial _t \tilde{w}^{(n)}_{|t=0}=\partial _t \tilde{w}^{(n-1)}_{|t=0}=0\), \(\tilde{q}_w^{(n)}, \tilde{q}_w^{(n-1)}\in \mathscr {K}^s_{pr}\), and such that
-
(i)
\(\left\| \tilde{w}^{(n)}\right\| _{\mathscr {K}^{s+1}}\le M\), \(\left\| \tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}\le M\),
-
(ii)
\(\left\| \tilde{X}^{(n)}-\tilde{\alpha }\right\| _{\mathscr {F}^{s+1,\gamma }}\le M\), \(\left\| \tilde{X}^{(n-1)}-\tilde{\alpha }\right\| _{\mathscr {F}^{s+1,\gamma }}\le M\),
-
(iii)
\(\left\| \tilde{G}^{(n)}-\tilde{G}_0\right\| _{\mathscr {F}^{s,\gamma -1}}\le M\), \(\left\| \tilde{G}^{(n-1)}-\tilde{G}_0\right\| _{\mathscr {F}^{s,\gamma -1}}\le M\),
-
(iv)
\(\Vert \tilde{q}_w^{(n)}\Vert _{\mathscr {K}^{s}_{pr}},\le M\), \(\Vert \tilde{q}_w^{(n-1)}\Vert _{\mathscr {K}^{s}_{pr}},\le M.\)
for some \(M>0\). Then
$$\begin{aligned}&\left\| \tilde{w}^{(n+1)}-\tilde{w}^{(n)}\right\| _{\mathscr {K}^{s+1}}+\left\| \tilde{q}_w^{(n+1)}-\tilde{q}_w^{(n)}\right\| _{\mathscr {K}^{s}_{pr}} \le CT^{\delta }\left( \left\| \tilde{X}^{(n)}-\tilde{X}^{(n-1)}\right\| _{\mathscr {F}^{s+1,\gamma }}\right. \\&\left. +\left\| \tilde{w}^{(n)}-\tilde{w}^{(n-1)}\right\| _{\mathscr {K}^{s+1}}+ \left\| \tilde{q}_w^{(n)}-\tilde{q}_w^{(n-1)}\right\| _{\mathscr {K}^{s}_{pr}} + \left\| \tilde{G}^{(n)}-\tilde{G}^{(n-1)}\right\| _{\mathscr {F}^{s,\gamma -1}}\right) , \end{aligned}$$for a suitable \(\delta >0\).
-
(i)
Proof.
For the proof of this theorem, we will use Theorem 2.
By putting together the results of Proposition 1, Proposition 2 and Proposition 3 and by applying the contraction mapping principle we get the proof of Theorem 3.
4 Stability
In this section, we want to prove what we described in the Introduction. So we pick a one-parameter family \(\tilde{\varOmega }_{\varepsilon }(0)=\tilde{\varOmega }_0+\varepsilon b\), where \(|b|=1\) and such that \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(0))\) is a regular domain as in Fig. 1a. We take the difference between the solution \((\tilde{w},\tilde{q},\tilde{X},\tilde{G})\) and the perturbed solution \((\tilde{w}_{\varepsilon },\tilde{q}_{\varepsilon },\tilde{X}_{\varepsilon },\tilde{G}_{\varepsilon })\), which is as follows:
The main estimates we prove, for a suitable \(\delta >0\) and for \(2<s<\frac{5}{2}\), are
5 Existence of Splash Singularity (Proof of Theorem 1)
From the stability estimates above, we obtain
by choosing \(0<T<\frac{1}{(3C)^{\frac{1}{\delta }}}\).
The main arguments to prove the existence of splash singularity are the stability results and the choice of the initial velocity. As stated in the Introduction, we choose \(\tilde{u}_0\cdot n>0\), and then we get a domain \(\tilde{\varOmega }(\bar{t})\) such that, by the inverse mapping, \(P^{-1}(\tilde{\varOmega }(\bar{t}))\) is a self-intersecting domain, for \(\bar{t}>0\). By using (17), it follows that \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(\bar{t}))\) is also a self-intersecting domain. In conclusion, we have that \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(0))\) is a regular domain of type (a) and \(P^{-1}(\tilde{\varOmega }_{\varepsilon }(\bar{t}))\) is a self-intersecting domain of type (c), for some \(\bar{t}\in (0,T]\), then there exists a time \(t^*\in (0,\bar{t})\) such that \(P^{-1}(\tilde{\varOmega }(t^*))\) self-intersects in one point, so it forms a splash singularity. Thus, Theorem 1 holds.
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Appendix
Appendix
The spaces we used in our proof are of the type
For our purposes, we shall always take \(r=\frac{s}{2}\), and we introduce the following notations:
with
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Di Iorio, E., Marcati, P., Spirito, S. (2018). Splash Singularity for a Free-Boundary Incompressible Viscoelastic Fluid Model. In: Klingenberg, C., Westdickenberg, M. (eds) Theory, Numerics and Applications of Hyperbolic Problems I. HYP 2016. Springer Proceedings in Mathematics & Statistics, vol 236. Springer, Cham. https://doi.org/10.1007/978-3-319-91545-6_38
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