of 32
POTENTIAL SINGULARITY OF THE AXISYMMETRIC EULER
EQUATIONS WITH
C
α
INITIAL VORTICITY FOR A LARGE
RANGE OF
α
. PART I: THE
3
-DIMENSIONAL CASE
THOMAS Y. HOU
AND
SHUMAO ZHANG
Abstract.
In Part I of our sequence of 2 papers, we provide numerical evidence for a potential
finite-time self-similar singularity of the 3D axisymmetric Euler equations with no swirl and with
C
α
initial vorticity for a large range of
α
. We employ an adaptive mesh method using a highly effective
mesh to resolve the potential singularity sufficiently close to the potential blow-up time. Resolution
study shows that our numerical method is at least second-order accurate. Scaling analysis and
the dynamic rescaling formulation are presented to quantitatively study the scaling properties of
the potential singularity. We demonstrate that this potential blow-up is stable with respect to the
perturbation of initial data. Our study shows that the 3D Euler equations with our initial data
develop finite-time blow-up when the H ̈older exponent
α
is smaller than some critical value
α
.
By properly rescaling the initial data in the
z
-axis, this upper bound for potential blow-up
α
can
asymptotically approach 1
/
3. Compared with Elgindi’s blow-up result in a similar setting [15], our
potential blow-up scenario has a different H ̈older continuity property in the initial data and the
scaling properties of the two initial data are also quite different.
Key words.
3D axisymmetric Euler equations, finite-time blow-up
AMS subject classifications.
35Q31, 76B03, 65M60, 65M06, 65M20
1. Introduction.
The three-dimensional (3D) incompressible Euler equations
in fluid dynamics describe the motion of inviscid incompressible flows and are one
of the most fundamental equations in fluid dynamics. Despite their wide range of
applications, the question regarding the global regularity of the Euler equations has
been widely recognized as a major open problem in partial differential equations
(PDEs) and is closely related to the Millennium Prize Problem on the Navier-Stokes
equations listed by the Clay Mathematics Institute [16]. In 2014, Luo and Hou [35,
36] considered the 3D axisyemmtric Euler equations with smooth initial data and
boundary, and presented strong numerical evidences that they can develop potential
finite time singularity. The presence of the boundary, the symmetry properties and
the direction of the flow in the initial data collaborate with each other in the formation
of a sustainable finite time singularity. Recently, Chen and Hou [6] provided a rigorous
justification of the Luo-Hou blow-up scenario.
In 2021, Elgindi [15] showed that given appropriate
C
α
initial vorticity with
α >
0
sufficiently small, the 3D axisymmetric Euler equations with no swirl can develop
finite-time singularity. In Elgindi’s work, the initial data for the vorticity
ω
have
C
α
H ̈older continuity near
r
= 0 and
z
= 0. When
α
is small enough, Elgindi
approximated the 3D axisymmetric Euler equations by a fundamental model that
develops a self-similar finite-time singularity. The blow-up result obtained in [15] has
infinite energy. In a subsequent paper [13], the authors improved the result obtained
in [15] to have finite energy blow-up.
In this work we study potential finite time singularity of the 3D axisymmetric
Euler equations with no swirl and
C
α
initial vorticity for a large range of
α
. Define
ω
=
∇×
u
as the vorticity vector, and then the 3D incompressible Euler equations
Department of Computing and Mathematical Sciences, California Institute of Technology,
Pasadena, CA (hou@cms.caltech.edu).
Department of Computing and Mathematical Sciences, California Institute of Technology,
Pasadena, CA (shumaoz@caltech.edu).
1
arXiv:2212.11912v1 [math.AP] 22 Dec 2022
2
THOMAS Y. HOU AND SHUMAO ZHANG
can be written in the vorticity stream function formulation:
(1.1)
ω
t
+
u
·∇
ω
=
ω
·∇
u,
−∇
ψ
=
ω,
u
=
∇×
ψ,
where
ψ
is the vector-valued stream function. Let us use
x
= (
x
1
,x
2
,x
3
) to denote a
point in
R
3
, and let
e
r
,
e
θ
,
e
z
be the unit vectors of the cylindrical coordinate system
e
r
=
1
r
(
x
1
,x
2
,
0)
, e
θ
=
1
r
(
x
2
,
x
1
,
0)
, e
z
= (0
,
0
,
1)
,
where
r
=
x
2
1
+
x
2
2
and
z
=
x
3
. We say a vector field
v
is axisymmetric if it admits
the decomposition
v
=
v
r
(
r,z
)
e
r
+
v
θ
(
r,z
)
e
θ
+
v
z
(
r,z
)
e
z
,
namely,
v
r
,
v
θ
and
v
z
are independent of the angular variable
θ
. Denote by
u
θ
,
ω
θ
, and
ψ
θ
the angular velocity, vorticity and stream function, respectively. The axisymmetric
condition can then simplify the 3D Euler equations (1.1) to [38]:
u
θ
t
+
u
r
u
θ
r
+
u
z
u
θ
z
=
1
r
u
r
u
θ
,
(1.2a)
ω
θ
t
+
u
r
ω
θ
r
+
u
z
ω
θ
z
=
2
r
u
θ
u
θ
z
+
1
r
u
r
ω
θ
,
(1.2b)
ψ
θ
rr
ψ
θ
zz
1
r
ψ
θ
r
+
1
r
2
ψ
θ
=
ω
θ
,
(1.2c)
u
r
=
ψ
θ
z
, u
z
=
1
r
ψ
θ
+
ψ
θ
r
.
(1.2d)
In the case of no swirl, i.e.
u
θ
0, the axisymmetric Euler equations are further
simplified into:
ω
θ
t
+
u
r
ω
θ
r
+
u
z
ω
θ
z
=
1
r
u
r
ω
θ
,
(1.3a)
ψ
θ
rr
ψ
θ
zz
1
r
ψ
θ
r
+
1
r
2
ψ
θ
=
ω
θ
,
(1.3b)
u
r
=
ψ
θ
z
, u
z
=
1
r
ψ
θ
+
ψ
θ
r
.
(1.3c)
When the initial condition for the angular vorticity
ω
θ
is smooth, it is well known that
the 3D axisymmetric Euler equations with no swirl (1.3) will not develop finite-time
blow-up [47]. Therefore, we consider (1.3) when the initial condition for the angular
vorticity
ω
θ
is
C
α
H ̈older continuous for a large range of
α
. By using an effective
adaptive mesh method, we will provide convincing numerical evidences that the 3D
axisymmetric Euler equations with no swirl and
C
α
initial voriticity with 0
< α <
1
/
3
develop potential finite-time self-similar blow-up.
We perform scaling analysis and use the dynamic rescaling formulation [21, 5, 8] to
study the behavior of the potential self-similar blow-up. An operator splitting method
is proposed to solve the dynamic rescaling formulation and the late time solution from
the adaptive mesh method is used as our initial condition for the dynamic rescaling
formulation. We observe rapid convergence to a steady state, which implies that this
potential singularity is self-similar. We will demonstrate that this potential blow-up is
POTENTIAL SINGULARITY OF THE AXISYMMETRIC EULER EQUATIONS, PART I
3
stable with respect to the perturbation of initial data, suggesting that the underlying
blow-up mechanism is generic and insensitive to the initial data. By introducing a
parameter
δ
to control the stretching of the physical domain and the initial data in
the
z
-axis, we find that the 3D Euler equations with
C
α
initial vorticity can develop
potential finite-time blow-up when the H ̈older exponent
α
is smaller than some
α
.
This upper bound
α
can asymptotically approach 1
/
3 as
δ
0. This result supports
Conjecture 8 of [13].
We choose the following
C
α
initial data for
ω
θ
with a stretching parameter
δ >
0:
ω
θ
0
=
12000
r
α
(
1
r
2
)
18
sin(2
πδz
)
1 + 12
.
5 cos
2
(
πδz
)
.
Note that the initial condition is a smooth and periodic function in
z
and is
C
α
in
r
.
The velocity field
u
becomes
C
1
continuous. We further introduce the new variables:
ω
1
(
r,z
) =
1
r
α
ω
θ
(
r,z
)
, ψ
1
(
r,z
) =
1
r
ψ
θ
(
r,z
)
,
(1.4)
to remove the formal singularity in (1.3) near
r
= 0. In terms of the new variables
(
ω
1
1
), the 3D axisymmetric Euler equations with no swirl have the following equiv-
alent form
ω
1
,t
+
u
r
ω
1
,r
+
u
z
ω
1
,z
=
(1
α
)
ψ
1
,z
ω
1
,
(1.5a)
ψ
1
,rr
ψ
1
,zz
3
r
ψ
1
,r
=
ω
1
r
α
1
,
(1.5b)
u
r
=
1
,z
, u
z
= 2
ψ
1
+
1
,r
.
(1.5c)
The above reformulation is crucial for us to perform accurate numerical computation
of the potential singular solution and allow us to push the computation sufficiently
close to the singularity time.
It is important to note that the initial condition for the rescaled vorticity field
ω
1
is a smooth function of
r
and
z
. Using the above reformualtion enables us to resolve
the potential singular solution sufficiently close to the potential singularity time. If
we solve the original 3D Euler equations (1.3a)–(1.3c), it is extremely difficult to
resolve the H ̈older continuous vorticity even with an adaptive mesh, especially for
small
α
. For this reason, we have not been able to compute the finite time singularity
in Elgindi’s work [15] since such a reformulation is not available for his initial data.
Compared with Elgindi’s blow-up result [15], our potential blow-up scenario has
very different scaling properties. The scaling factor
c
l
in our scenario increases with
α
and tends to infinity as
α
approaches
α
. In contrast, the scaling factor
c
l
in Elgindi’s
scenario is 1
, which decreases with
α
and tends to infinity as
α
approaches 0.
Another difference is that Elgindi’s initial vorticity is
C
α
in both
ρ
=
r
2
+
z
2
and
z
, while our initial vorticity is
C
1
continuous in
ρ
, but smooth in
z
.
There has been a number of theoretical analysis of the 3D Euler equations. The
Beale-Kato-Majda (BKM) blow-up criterion [2, 17] gives a necessary and sufficient
condition for the finite-time singularity for the smooth solutions of the 3D Euler
equations at time
T
if and only if
T
0
ω
(
·
,t
)
L
d
t
= +
. In [10], Constantin,
Fefferman and Majda asserted that there will be no finite-time blow-up if the velocity
u
is uniformly bounded and the direction of vorticity
ξ
=
ω/
|
ω
|
is sufficiently regular
(Lipschitz continuous) in an
O
(1) domain containing the location of the maximum
vorticity. Inspired by the work of [10], Deng-Hou-Yu developed a more localized
non-blow-up criterion using a Lagrangian approach in [12].
4
THOMAS Y. HOU AND SHUMAO ZHANG
There have been a number of numerical attempts in search of the potential finite-
time blow-up. The finite-time blow-up in the numerical study was first reported by
Grauer and Sideris [19] and Pumir and Siggia [41] for the 3D axisymmetric Euler
equations. However, the later work of E and Shu [14] suggested that the finite-time
blow-up in [19, 41] could be caused by numerical artifact. Kerr and his collaborators
[24, 3] presented finite-time singularity formation in the Euler flows generated by a
pair of perturbed anti-parallel vortex tubes. In [22], Hou and Li reproduced Kerr’s
computation using a similar initial condition with much higher resolutions and did
not observe finite time blow-up. The maximum vorticity grows slightly slower than
double exponential in time. Later on, Kerr confirmed in [25] that the solutions from
[24] eventually converge to a super-exponential growth and are unlikely to lead to a
finite-time singularity.
In [4, 45], Caflisch and his collaborators studied axisymmetric Euler flows with
complex initial data and reported singularity formation in the complex plane. The
review paper [18] lists a more comprehensive collection of interesting numerical results
with more detailed discussions.
Due to the lack of stable structure in the potentially singular solutions, the pre-
viously mentioned numerical results remain inconclusive. In [35, 36], Luo and Hou
reported that the 3D axisymmetric Euler equations with a smooth initial condition
developed a self-similar finite time blow-up in the meridian plane on the boundary
of
r
= 1, see also [37]. The Hou-Luo blow-up scenario has generated a great deal of
interests in both the mathematics and fluid dynamics communities, and inspired a
number of subsequent developments [28, 27, 26, 9, 7, 5, 8, 6].
The rest of this paper is organized as follows. In Section 2, we briefly introduce
the numerical method. We present the evidence of the potential self-similar blow-
up in Section 3, and provide the resolution study and scaling analysis. In Section
4 we use the dynamic rescaling method to provide further evidence of the potential
blow-up for the case of
α
= 0
.
1. In Section 5, we consider the potential finite-time
blow-up in the general case of the H ̈older exponent
α
, and introduce the anisotropic
scaling parameter
δ
. The sensitivity of the potential blow-up to the initial data is
considered in Section 6, and the comparison of our potential blow-up scenario with
Elgindi’s scenario in [15] is discussed in Section 7. Some concluding remarks are made
in Section 8.
2. Problem set up and numerical method.
In this section, we give details
about the setup of the problem, the initial data, the boundary conditions, and some
basic properties of the equations, and our numerical method.
2.1. Boundary conditions and symmetries.
We consider (1.5) in a cylinder
region
D
cyl
=
{
(
r,z
) : 0
r
1
}
,
We impose a periodic boundary condition in
z
with period 1:
ω
1
(
r,z
) =
ω
1
(
r,z
+ 1)
, ψ
1
(
r,z
) =
ψ
1
(
r,z
+ 1)
.
(2.1)
In addition, we enforce that (
ω
1
1
) are odd in
z
at
z
= 0:
ω
1
(
r,z
) =
ω
1
(
r,
z
)
, ψ
1
(
r,z
) =
ψ
1
(
r,
z
)
.
(2.2)
And this symmetry will be preserved dynamically by the 3D Euler equations.
At
r
= 0, it is easy to see that
u
r
(0
,z
) = 0, so there is no need for the boundary
condition for
ω
1
at
r
= 0. Since
ψ
θ
=
1
will at least be
C
2
-continuous, according
POTENTIAL SINGULARITY OF THE AXISYMMETRIC EULER EQUATIONS, PART I
5
to [32, 33],
ψ
θ
must be an odd function of
r
. Therefore, we impose the following pole
condition for
ψ
1
ψ
1
,r
(0
,z
) = 0
.
(2.3)
We impose the no-flow boundary condition at the boundary
r
= 1:
ψ
1
(1
,z
) = 0
.
(2.4)
This implies that
u
r
(1
,z
) = 0. So there is no need to introduce a boundary condition
for
ω
1
at
r
= 1.
Due to the periodicity and the odd symmetry along the
z
direction, the equations
(1.3) only need to be solved on the half-periodic cylinder
D
=
{
(
r,z
) : 0
r
1
,
0
z
1
/
2
}
.
The above boundary conditions of
D
show that there is no transport of the flow across
its boundaries. Indeed, we have
u
r
= 0
on
r
= 0 or 1
,
and
u
z
= 0
on
z
= 0 or 1
/
2
.
Thus, the boundaries of
D
behave like “impermeable walls”.
Fig. 1
.
3D profiles of the initial value
ω
1
and
ψ
1
.
Fig. 2
.
The initial data for the angular vorticity
ω
θ
.
2.2. Initial data.
Inspired by the potential blow-up scenario in [20], we propose
the following initial data for
ω
1
in
D
,
ω
1
=
12000
(
1
r
2
)
18
sin(2
πz
)
1 + 12
.
5 cos
2
(
πz
)
.
(2.5)
6
THOMAS Y. HOU AND SHUMAO ZHANG
Later we will see in Section 6 that the self-similar singularity formation has some
robustness to the choice of initial data. We solve the Poisson equation (1.5b) to get
the initial value
ψ
1
of
ψ
1
.
Fig. 3
.
Initial velocity fields
u
r
and
u
z
.
Fig. 4
.
A heuristic diagram of the hyperbolic flow.
The 3D profiles of (
ω
1
1
) can be found in Figure 1. Since most parts of
ω
1
and
ψ
1
are negative, we negate them for better visual effect when generating figures. In
Figure 2, we show the 3D profile and pseudocolor plot of the angular vorticity
ω
θ
at
t
= 0. We can see that there is a sharp drop to zero of
ω
θ
near
r
= 0, which is due
to the H ̈older continuous of
ω
θ
at
r
= 0.
We plot the initial velocity field
u
r
and
u
z
in Figure 3. We can see that
u
r
is primarily positive near
z
= 0 and negative near
z
= 1
/
2 when
r
is small, and
u
z
is mainly negative when
r
is small. Such a pattern suggests a hyperbolic flow
near (
r,z
) = (0
,
0) as depicted in the heuristic diagram Figure 4, which will extend
periodically in
z
.
2.3. Self-similar solution.
For nonlinear PDEs, people are particularly inter-
ested in studying self-similar blow-up solutions. A self-similar solution is when the
local profile of the solution remains nearly unchanged in time after rescaling the spa-
tial and the temporal variables of the physical solution. For example, for (1.5), the
POTENTIAL SINGULARITY OF THE AXISYMMETRIC EULER EQUATIONS, PART I
7
self-similar profile is the ansatz
(2.6)
ω
1
(
x,t
)
1
(
T
t
)
c
ω
(
x
x
0
(
T
t
)
c
l
)
,
ψ
1
(
x,t
)
1
(
T
t
)
c
ψ
Ψ
(
x
x
0
(
T
t
)
c
l
)
,
for some parameters
c
ω
,
c
ψ
,
c
l
,
x
0
and
T
. Here
T
is considered as the blow-up time,
and
x
0
is the location of the self-similar blow-up. The parameters
c
ω
,
c
ψ
,
c
l
are called
scaling factors.
It is also important to notice that the 3D Euler equations (1.1) enjoy the following
scaling invariant property: if (
u,ω,ψ
) is a solution to (1.1), then (
u
λ,τ
λ,τ
λ,τ
) is
also a solution, where
u
λ,τ
(
x,t
) =
λ
τ
u
(
x
λ
,
t
τ
)
, ω
λ,τ
(
x,t
) =
1
τ
ω
(
x
λ
,
t
τ
)
, ψ
λ,τ
(
x,t
) =
λ
2
τ
ψ
(
x
λ
,
t
τ
)
,
and
λ >
0,
τ >
0 are two constant scaling factors. In the case of the axisymmetric 3D
Euler equations with no swirl (1.5), the scaling invariant property can be equivalently
translated to: if (
ω
1
1
) is a solution of (1.5), then
{
1
λ
α
τ
ω
1
(
x
λ
,
t
τ
)
,
λ
τ
ψ
1
(
x
λ
,
t
τ
)}
(2.7)
is also a solution.
If we assume the existence of the self-similar solution (2.6), then the new solutions
in (2.7) should also admit the same ansatz, regardless of the values of
λ
and
μ
. As a
result, we must have
c
ω
= 1 +
αc
l
, c
ψ
= 1
c
l
.
(2.8)
Therefore, the self-similar profile (2.7) of (1.5) only has one degree of freedom, for
example
c
l
, in the scaling factors. In fact,
c
l
cannot be determined by straightforward
dimensional analysis.
As a consequence of the ansatz (2.6) and the scaling relation (2.8), we have
ω
θ
(
x,t
)
L
1
T
t
,
ψ
1
,z
(
x,t
)
L
1
T
t
,
(2.9)
which should always hold true regardless of the value of
c
l
.
2.4. Numerical method.
Although the initial data are very smooth, the so-
lutions of Euler equations quickly become very singular and concentrate in a rapidly
shrinking region. Therefore, we use the adaptive mesh method to resolve the singular
profile of the solutions. A detailed description of the adaptive mesh method can be
found in [21, 37, 48]. Here we briefly introduce the idea behind the adaptive mesh
method. The specific parameter setting used for the experiments in this work can be
found in the appendix of [48].
The Euler equations (1.5) are originally posted as an initial-boundary value prob-
lem on the computational domain (
r,z
)
[0
,
1]
×
[0
,
1
/
2]. To capture the singular
part of the solution, we introduce two variables (
ρ,η
)
[0
,
1]
×
[0
,
1], and the maps
r
=
r
(
ρ
)
, z
=
z
(
η
)
,