
2
ding from the penetrable to impenetrable regime.
The remainder of this paper is organized as follows. In
Sec. II, we describe a theoretical model to study the vor-
tex shedding dynamics in a BEC based on the 2D Gross-
Pitaevskii equation. In Sec. III, we present numerical re-
sults, including a comparison of the shedding dynamics
for penetrable and impenetrable obstacles, and the char-
acterization of the critical vortex dipole state generated
by the moving obstacle at the critical strength. Finally,
in Sec. IV, a summary of this work and the outlooks for
future studies are provided.
II. THEORETICAL MODEL
We consider a situation where an obstacle moves in a
homogeneous BEC with a constant velocity v. In the
mean-field theory, the BEC dynamics is described by the
Gross-Pitaevskii equation (GPE),
i~∂Ψ
∂t =−~2
2m∇2+V(r−vt) + g|Ψ|2−µΨ,(1)
where Ψ(r, t) is the macroscopic wave function of the
BEC, ~is Planck’s constant divided by 2π,mis the atom
mass, V(r) is the obstacle potential, and gis the nonlin-
ear coupling coefficient. Taking the unitary transforma-
tion Ψ(r, t) = exp[−vt·∇]ψ(r, t), Eq. (1) is transformed
into the reference frame moving with the obstacle as
i~∂ψ
∂t =−~2
2m∇2+i~v∂
∂x +V(r) + g|ψ|2−µψ(2)
with v=vˆ
x. The characteristic length and time scales of
the system are given by the healing length ξ=~/√2mµ
and tµ=~/µ, respectively. Using the change in vari-
ables, ˜
r=r/ξ and ˜
t=t/tµ, the equation can be ex-
pressed in a dimensionless form as
i∂˜
t˜
ψ=−˜
∇2+i√2˜v∂˜x+˜
V(˜
r) + |˜
ψ|2−1˜
ψ(3)
with ˜
ψ=n−1/2
0ψ, ˜v=v/cs,˜
∇=ξ∇, and ˜
V=V/µ.
Here n0=µ/g is the particle density of the BEC without
the obstacle and cs=pµ/m is the speed of sound.
In this work, we study the BEC dynamics for a Gaus-
sian obstacle in two dimensions. This is motivated by
the recent experiments using highly oblate atomic sam-
ples [9–12, 23], where the vortex line dynamics along
the tight confining direction is energetically irrelevant.
Hence, the shedding dynamics can be well described in
2D. In a hydrodynamic approximation, the dimensional
reduction is carried out by integrating the wave function
component along the short axis. It effectively modifies
the speed of sound in Eq. (3) [26, 27]. The potential of the
Gaussian obstacle is given by V(r) = V0exp[−2(r2/σ2)],
where r=px2+y2and σis the 1/e2radius of the obsta-
cle. The obstacle is located at the origin of the reference
frame.
We numerically solve Eq. (3) in the xy plane with pe-
riodic boundary conditions, using the pseudo spectral
method [28]. In the simulation of vortex shedding for
v > vc, we set the initial state to be a stationary solution
for a velocity vislightly below vc. Next, we increase the
obstacle speed up to the target velocity vfor an accelera-
tion time ta= 200tµ[29]. The initial stationary solution
is obtained using the imaginary-time method where tis
replaced by −iτ [30, 31]. To realize a constant stream
at the front boundary of the obstacle, we adopt the nu-
merical method described in Ref. [25], where damping
zones with a thickness of 20ξare set at the boundary to
attenuate the wake of the BEC and recover the constant
uniform flow at the front boundary. In the calculation of
a stationary solution using the imaginary-time propaga-
tion method, the damping zone is inactivated.
III. RESULTS AND DISCUSSION
A. Determination of critical velocity
Figures 1(a) and 1(b) display the density distribu-
tions of the BEC, n(x, y) = |ψ|2, at t/tµ= 1200 for
two different velocities, v/cs= 0.25 and 0.28, respec-
tively [29]. The obstacle size and strength are σ/ξ = 20
and V0/µ = 0.8. When the speed is lower than the
threshold value of vc≈0.26cs, no vortices are generated.
The BEC remains stationary [Fig. 1(a)]. By contrast,
when the obstacle velocity increases above the threshold
velocity, vortices are emitted from the obstacle in a pe-
riodic manner [21]. The periodic vortex shedding is also
examined by inspecting the drag force exerted by the
obstacle Fx=−R˜
ψ∗(∂˜x˜
V)˜
ψd2˜
rusing the Ehrenfest re-
lation [25]. We verify that for v > vcthe force oscillates
in time, corresponding to the periodic vortex emission.
For v < vcit is stationary and remains approximately
zero [Fig. 1(c)].
We determine the critical velocity vcfrom the exis-
tence of a stationary ground state solution via the imagi-
nary time propagation method [15]. The imaginary time
method gives a converging stationary solution for v < vc
or an oscillating solution otherwise. In the oscillating
solution, a pair of vortices is created by the obstacle.
They move away from each other along the y-direction
and are annihilated at the system’s boundary due to
the periodic boundary conditions. This process is re-
peated over an imaginary time. In the calculation of
stationary solutions, we employed a spatial domain of
(Lx, Ly) = (400,400)ξwith (Nx, Ny) = (600,600) grids
and took a time step of ∆τ/tµ= 0.04. We decided the
convergence of a solution through its behavior up to the
imaginary time τ/tµ= 4000. The critical velocities de-
termined from our imaginary time method are identical
to the threshold values from the simulation of the real-
time evolution within an error of 0.02cs.
Figure 2displays the numerical results of the critical
velocities over a range of obstacle strength 0.1≤V0/µ ≤