Communications in Physics, Vol. 26, No. 1 (2016), pp. 11-18<br />
DOI:10.15625/0868-3166/26/1/7790<br />
<br />
RIPPLON MODES OF TWO SEGREGATED BOSE-EINSTEIN<br />
CONDENSATES IN CONFINED GEOMETRY<br />
TRAN HUU PHAT<br />
Vietnam Atomic Energy Commission, 59 Ly Thuong Kiet, Hanoi, Vietnam<br />
HOANG VAN QUYET†<br />
Department of Physics, Hanoi Pedagogical University No. 2, Hanoi, Vietnam<br />
† E-mail:<br />
<br />
hoangvanquyetsp2@gmail.com<br />
<br />
Received 20 February 2016<br />
Accepted for publication 12 April 2016<br />
<br />
Abstract. The ripplon modes of two segregated Bose-Einstein condensates (BECs) confined by<br />
one and two hard walls are respectively studied by means of the hydrodynamic approach within<br />
the Gross-Pitaevskii (GP) theory. For the system at rest we find that due to the spatial restriction<br />
the dispersion relations are of the form ω ∼ k2 in low momentum limit for both cases, while for<br />
the system in motion parallel to the interface the dispersion relations for both cases are ω ∼ k at<br />
low momentum limit and, furthermore, the system becomes unstable.<br />
Keywords: Bose-Einstein condensates, hydrodynamic approach, ripplon modes, Kelvin-Helmholtz<br />
instability, Bernoulli equation.<br />
Classification numbers: 03.75.Fi, 05.30.Jp, 67.60.- g.<br />
<br />
I. INTRODUCTION<br />
The phase separation in binary mixtures of Bose-Einstein condensates was theoretically<br />
predicted [1, 2] and observed later in experiments [3–8]. Since then many works have been devoted to explore the statics, the dynamics and the ripplon modes of two segregated BECs [9–25].<br />
However, most of them concerned with the systems in infinite space, while all experimental realizations have been carried out in restricted regions of space with spatial structure being more and<br />
more complicated. In this respect, the present paper deals with the problem: how ripplon modes<br />
are influenced by the spatial restriction when a system of two segregated BECs is confined by one<br />
or two hard walls and the method we use to tackle the problem is the hydrodynamic approach. To<br />
c<br />
2016<br />
Vietnam Academy of Science and Technology<br />
<br />
12<br />
<br />
TRAN HUU PHAT AND HOANG VAN QUYET<br />
<br />
begin with, let us start from the GP Lagrangian<br />
<br />
<br />
−r P + P − g |ψ |2 |ψ |2 ,<br />
£ = ∫ d→<br />
1<br />
2<br />
12 1<br />
2<br />
Pj = i¯hψ ∗j<br />
<br />
2 g j j 4<br />
∂ψj<br />
h¯ 2 <br />
ψ j ,<br />
∇ψ j −<br />
+<br />
∂t<br />
2m j<br />
2<br />
<br />
(1a)<br />
(1b)<br />
<br />
with m j being the atomic mass of the j component. The intra-s and inter-species interaction coupling constants are defined as<br />
<br />
<br />
−1<br />
g jk = 2π h¯ 2 a jk m−1<br />
+<br />
m<br />
,<br />
j<br />
k<br />
where a jk is the scattering length between the atoms in components j and k. In the following we<br />
assume that two BECs are separated g212 > g11 g22 .<br />
From the Lagrangian (1) the GP equations are deduced straightforwardly<br />
<br />
<br />
∂ ψ1<br />
h¯ 2 2<br />
2<br />
2<br />
i¯h<br />
= −<br />
∇ + g11 |ψ1 | + g12 |ψ2 | ψ1 ,<br />
(2a)<br />
∂t<br />
2m1<br />
<br />
<br />
∂ ψ2<br />
h¯ 2 2<br />
2<br />
2<br />
i¯h<br />
= −<br />
∇ + g22 |ψ2 | + g12 |ψ1 | ψ2 .<br />
(2b)<br />
∂t<br />
2m2<br />
This paper is organized as follows. The main body of the work is presented in Sec. II where<br />
the Bernoulli equation is established and the ripplon modes are derived. The conclusion and<br />
discussion are given in Sec. III.<br />
II. RIPPLON MODES<br />
First of all let us establish the Bernoulli equation for the system of two BECs separated by<br />
the interface which is represented by the equation z = z0 + η (σ ) , σ = (kx x + ky y − ωt) and located<br />
at z = z0 . Assume that the component 1 (component 2) resides in the region z > z0 (z < z0 ). Then<br />
the Lagrangian (1a) is approximated by<br />
η+z<br />
<br />
+∞<br />
0<br />
£ = 2π ∫ dxdy ∫ dzP2 + ∫ dzP1 − αS,<br />
(3)<br />
−∞<br />
<br />
η+z0<br />
<br />
where α is the interface tension and the interface area S is given by<br />
Z<br />
<br />
S=<br />
<br />
<br />
<br />
∂η<br />
dxdy[1 +<br />
∂x<br />
<br />
2<br />
<br />
<br />
<br />
∂η<br />
+<br />
∂y<br />
<br />
2<br />
<br />
1<br />
2<br />
<br />
] ≈<br />
<br />
Z<br />
<br />
<br />
<br />
<br />
<br />
1 ∂η 2 1 ∂η 2<br />
+<br />
],<br />
dxdy[1 +<br />
2 ∂x<br />
2 ∂y<br />
<br />
for interface with negligible thickness. From (3) and (4) we arrive at the Bernoulli equation<br />
2<br />
<br />
∂<br />
∂2<br />
P1 (x, y, z = z0 + η,t) − P2 (x, y, z = z0 + η,t) = α<br />
+<br />
,<br />
∂ x 2 ∂ y2<br />
<br />
(4)<br />
<br />
(5)<br />
<br />
which corresponds to the classic Bernoulli equation in hydrodynamics [26, 27]. Next , we proceed<br />
to the GP equations in linear approximation as made in Ref. [17] writing<br />
q<br />
ψ j (x, y, z, t,) = n j (x, y, z, t)eiφ j (x,y,z,t) ,<br />
(6)<br />
<br />
RIPPLON MODES OF TWO SEGREGATED BOSE-EINSTEIN CONDENSATES IN CONFINED GEOMETRY<br />
<br />
13<br />
<br />
in which the particle number density and phase, n j (x, y, z,t) and φ j (x, y, z,t), are decomposed as<br />
n j (x, y, z,t) = n j0 + δ n j (x, y, z,t) ,<br />
(7a)<br />
g j j n j0<br />
φ j (x, y, z,t) = −<br />
t + δ φ j (x, y, z,t) .<br />
(7b)<br />
h¯<br />
Inserting (6) and (7) into (2) and taking only the first order of δ n j , δ φ j we are led to the approximate equations<br />
−<br />
∇→<br />
v = 0,<br />
(8a)<br />
j<br />
<br />
∂<br />
δ φj + g j j δ nj = 0,<br />
(8b)<br />
∂t<br />
assuming that the relative density changes following fluid particles are small compared to the<br />
velocity gradient [28]. The velocity ~v j in (8a) is defined as<br />
h¯<br />
<br />
<br />
<br />
h¯<br />
→<br />
−<br />
v j = ~∇δ φ j ,<br />
mj<br />
<br />
(9)<br />
<br />
Eq. (8a) tells that in the approximation under consideration the condensates are incompressible<br />
fluid.<br />
Based on the approximate equations (8) and (9) the pressure given in (1b) takes the form<br />
1<br />
(10)<br />
Pj = g j j n2j0 + g j j n j0 δ n j .<br />
2<br />
To solve (8a) and (9) we adopt the ansatz<br />
δ φ j (x) = ϕ j (z) χ j (σ ) ,<br />
from which we get the equations<br />
<br />
d2<br />
2<br />
−<br />
k<br />
ϕ j (z) = 0,<br />
dz2<br />
2<br />
<br />
∂<br />
∂2<br />
2<br />
+<br />
+ k χ j = 0,<br />
∂ x 2 ∂ y2<br />
<br />
<br />
(11a)<br />
(11b)<br />
<br />
with<br />
k2 = kx2 + ky2 .<br />
The Bernoulli equation together with the solutions to Eqs. (11) are the basic ingredients for<br />
calculating the ripplon modes in the following two subsections.<br />
A- One hard-wall case<br />
Assume that the hard-wall is located at z = - h as depicted in Fig. 1.<br />
The geometrical configuration of the system suggests that the reasonable conditions to be<br />
imposed on the two condensates are<br />
<br />
∂ ϕ2 (z) <br />
= 0,<br />
∂z <br />
z=−h<br />
<br />
ϕ1 (z) → 0 as z → +∞,<br />
which lead to<br />
δ φ1 = (A1 cos σ + B1 sin σ ) exp (−kz) ,<br />
<br />
14<br />
<br />
TRAN HUU PHAT AND HOANG VAN QUYET<br />
<br />
Fig. 1. The interface is located at z = z0 and the hard wall at z = −h.<br />
<br />
δ φ2 = (A2 cos σ + B2 sin σ ) cosh [k(z + h) ] ,<br />
where A j , B j are small parameters.<br />
For simplicity let us restrict to the case<br />
δ φ1 = A1 exp (−kz) cos σ ,<br />
<br />
(12a)<br />
<br />
δ φ2 = A2 cosh [k(z + h) ] cos σ .<br />
<br />
(12b)<br />
<br />
Note that the results to be obtained later remain unchanged if cos σ in (12) is replaced by sin σ .<br />
The kinetic condition at the interface reads<br />
<br />
<br />
<br />
<br />
∂ η (σ )<br />
h¯ ∂ δ φ1<br />
h¯ ∂ δ φ2<br />
=<br />
=<br />
.<br />
(13)<br />
∂t<br />
m1<br />
∂ z z=z0 m2<br />
∂ z z=z0<br />
Inserting (12) into (13) yields<br />
−ω<br />
<br />
dη (σ )<br />
h¯ k<br />
h¯ k<br />
= −A1<br />
exp (−kz0 ) cos σ = A2<br />
sinh [k(z0 + h) ] cos σ .<br />
dσ<br />
m1<br />
m2<br />
<br />
(14)<br />
<br />
The solution to Eqs. (14) provides immediately<br />
η (σ ) = η0 sinσ ,<br />
<br />
(15)<br />
<br />
and<br />
η0 m1 ω exp(kz0 )<br />
,<br />
h¯ k<br />
η0 m2 ω<br />
A2 = −<br />
.<br />
h¯ k sinh [k(z0 + h)]<br />
A1 =<br />
<br />
(16a)<br />
(16b)<br />
<br />
Eqs. (14) are justified for |kη0 | 1.<br />
Substituting (10) , (12) , (15) , (16) into the Bernoulli equation (5) we arrive at<br />
ω2 =<br />
<br />
αk3<br />
,<br />
ρ2 coth [k(z0 + h)] + ρ1<br />
<br />
here ρ1 = m1 n10 (z0 + 0), ρ2 = m2 n20 (z0 − 0).<br />
As h tends to infinity Eq. (17) turns out to be<br />
r<br />
ω=<br />
<br />
α<br />
k3/2 ,<br />
ρ1 + ρ2<br />
<br />
(17)<br />
<br />
RIPPLON MODES OF TWO SEGREGATED BOSE-EINSTEIN CONDENSATES IN CONFINED GEOMETRY<br />
<br />
15<br />
<br />
which is the well known formula for dispersion relation of ripplon in classic hydrodynamics [26,<br />
27]. At the low momentum limit Eq. (17) behaves like<br />
α (h + z0 ) 4<br />
k ,<br />
(18)<br />
ω2 ≈<br />
ρ2<br />
which is the main result of this subsection.<br />
In order to get a deeper insight into the issue let us extend to the case when condensates flow with<br />
velocity ~V j parallel to the interface. Then the corresponding stationary state is also represented in<br />
the form (7b) with<br />
g j j n j0<br />
mj →<br />
− →<br />
φj = −<br />
t+<br />
V j .−r ⊥ + δ φ j ,<br />
h¯<br />
h¯<br />
where δ φ j is given by Eqs. (12). In this case the kinetic condition at the interface (13) is modified<br />
as<br />
<br />
<br />
<br />
<br />
h¯ ∂ δ φ j<br />
∂ →<br />
− ∂<br />
+ Vj −<br />
η=<br />
.<br />
(19)<br />
∂t<br />
mj<br />
∂ z z=z0<br />
∂ r→<br />
⊥<br />
Substituting (12) and (15) into (19) gives<br />
<br />
<br />
η0 m1 ω − ~V1~k exp(kz0 )<br />
A1 =<br />
,<br />
(20a)<br />
h¯ k<br />
<br />
η0 m2 ω − ~V2~k<br />
A2 = −<br />
.<br />
(20b)<br />
h¯ k sinh [k(z0 + h)]<br />
After inserting (20) into (5) we are led to the equation<br />
<br />
2<br />
<br />
2<br />
ρ1 ω − ~V1~k + ρ2 coth [k (z0 + h)] ω − ~V2~k = αk2 ,<br />
yielding<br />
k<br />
ω± = Vc k ± √<br />
ρ1 + ρ2<br />
here<br />
Vc =<br />
<br />
r<br />
ρ1 ρ2 2<br />
αk −<br />
V<br />
ρ1 + ρ2 r<br />
<br />
(21)<br />
<br />
ρ1V1 cos θ1 + ρ2 coth [k (z0 + h)]V2 cos θ2<br />
,<br />
ρ1 + ρ2 coth [k (z0 + h)]<br />
<br />
\<br />
with θ j = ~V j ,~k .<br />
It is easily seen that as h tends to infinity (21) turns out to be<br />
s<br />
αk3<br />
ρ1 ρ2Vr2 k2<br />
ω± = Vc k ±<br />
−<br />
,<br />
ρ1 + ρ2 (ρ1 + ρ2 )2<br />
<br />
(22)<br />
<br />
which is a well known result.<br />
The small-k behavior of (21) reads<br />
r<br />
ρ1<br />
ω ≈ V2 cos θ2 k ± − (h + z0 )Vr k3/2 .<br />
ρ2<br />
<br />
<br />
<br />
<br />
Eq. (23) indicates that the Kelvin-Helmholtz instability always occurs for Vr = ~V1 − ~V2 > 0.<br />
Next let us go over to the two hard-wall case.<br />
<br />
(23)<br />
<br />