Lecture 2
Vortex knots dynamics and momenta of a tangle:
- Localized Induction Approximation (LIA) and Non-Linear Schrödinger (NLS) equation
- Integrable vortex dynamics and LIA hierarchy - Torus knot solutions to LIA
- Linear and angular momentum in terms of signed area information
Selected references
Maggioni, F, Alamri, SZ, Barenghi, CF & Ricca, RL 2010 Velocity, energy and helicity of vortex knots and unknots. Phys Rev E 82, 26309.
Ricca, RL 1993 Torus knots and polynomial invariants for a class of soliton equations. Chaos 3, 83 [Erratum. Chaos 5, 346].
Ricca, RL 2008 Momenta of a vortex tangle by structural complexity
analysis. Physica D 237, 2223.
Localized induction approximation (LIA) homogeneous
incompressible
inviscid fluid in : in
as
∇ ⋅ u = 0
u = 0 X → ∞ u = u X,t ( )
ω = ∇ × u
R
3R
3Space curve , given by: C
tC
t: X(s,t) := X
t(s) ∈ C
νs∈ [0,L] → R
3Intrinsic reference on , given by:
(Frenet frame) C
tˆ t := ′ X (s,t) = ∂ X
∂ s { ˆ t , ˆ n , ˆ b }
Vortex line on : C
tˆ t
n ˆ
b ˆ
C
tω = ω
0ˆ t ω
0, = constant circulation = constant asymptotic theory: κ
R / a >> 1
X(s,t) = ∂ X
∂ t = ′ X × ′′ X = c ˆb = u
LIA(Da Rios 1906; Hama & Arms 1961 )
Intrinsic equations under LIA and NonLinear Schrödinger (NLS) equation Intrinsic description: , curvature, torsion;
u = (u
t,u
n,u
b)
under LIA: , , . u
LIA= cˆ b u
t= u
n= 0 u
b= c
C
t:= ϕ
t(C)
c = −(c ˙ τ ) − ′ ′ c τ
τ ˙ = c − c ′ ′ τ
2c
′
+ ′ c c
Da Rios 1906 Betchov 1965
NLS eq. via Madelung transform:
c s,t ( ) τ s,t ( )
ψ s,t ( ) = c s,t ( ) e
i 0τ ξ , t( )
d∫
s ξc
τ
ψ R
2C
Intrinsic equations by log-derivative:
let and consider
(Hasimoto 1972)
ℜe ℑm
i ψ + ′′ ψ +
12ψ
2ψ = 0
NLS eq.:
Da Rios- Betchov eqs .
Θ s,t ( ) = ∫
0sτ ξ ( ) ,t d ξ ψ = c e
iΘIntegrable vortex dynamics and LIA hierarchy Integrable vortex dynamics:
: inhomogeneities
(Lakshmanan & Ganesan 1985) β , δ
: non-linear stretching
(Onuki 1985) γ
: axial flow and vorticity
(Fukumoto & Miyazaki 1991)
u = α + βs ( ) cˆ b + γ + δs ( ) t + µ ˆ (
12c
2ˆ t + ′ c ˆ n + cτˆ b )
µ
LIA hierarchy:
u ( )
0= u
LIA(Langer & Perline 1991)
(Nakayama et al. 1992)
NLSE mKdV sine-G … … Hirota class
… … …
ψ ˙ = P
ψ( u
ne
iΘ) + Q
ψ( u
be
iΘ)
integrable class:
u ( )
j+1= ˆt × ˆt + ∫ c s,t ( ) ( u ′
b( )
j+ τ u
n( )
j) ds ˆt = ∑ν =1j+1F ∂ ∂
νu s
ν( )
0 = R u ( ) ( )
0
Stationary solutions: Hasimoto soliton
(Hasimoto 1972)
τ = const.
c s ( ) = 2 sech s ( )
Steady solutions to LIA: torus knots and unknots
T
p, qp > 1 q > 1
Theorem (Ricca 1993). LIA admits torus knot solutions in closed analytic form, given by: T
p, qr = r
0+ ε sin w ( ) ξ α = s
r
0+ ε
wr
0cos w ( ) ξ z = t
r
0+ ε 1− 1 w
21/2
cos w ( ) ξ r
2= F
r( ) J , , . α = F
α( ) E z = F
z( ) Π
. Theorem (Kida 1981). There exists
a class of steady torus knot solutions ( , co-prime integers) to
LIA in terms of incomplete elliptic integrals, given by Look for stationary solutions to LIA in the
shape of torus knots and unknots:
(Da Rios 1933)
Proof. First let’s write LIA in terms of cartesian coordinates
(x, y, z) and cylindrical polar coordinates (r, α , z) .
From
and x = r cos α , y = r sin α , z , by taking time-derivative, we have
u
LIA= X(s,t) = ′ X × ′′ X
and by the last equality of , we have
(∗) (∗∗)
(∗)
.
We now take the arc-length derivative of and substitute in the above, to get LIA in cylindrical polar coordinates: (∗∗)
.
(∗∗∗)
. Small-amplitude perturbations are given by taking
.
By substituting these into and taking first-order terms, we have (∗∗∗)
r = r
0+ ε sin w ( ) ξ α = s
r
0+ ε
wr
0cos w ( ) ξ z = t
r
0+ ε 1− 1 w
21/2
cos w ( ) ξ . By looking for a traveling-wave solution ξ = s– κ t as torus knot, we have
Now let’s consider small-amplitude perturbations. For the vortex ring
we have r = R , and α = s/R , so that previous equations reduce to
Small-amplitude torus knots and unknots under LIA
torus knots
torus unknots
Linear stability of LIA torus knots
(Ricca et al 1999)
T
2, 3w > 1 ( ) T
3, 2w < 1 ( )
Theorem (Ricca 1995). For any given , is linearly stable
iff . w = q / p
w > 1 T
p, qLIA knots and unknots ,
(Maggioni et al. 2010)
T
p,qU
1,mU
m,1Creation and dynamics of trefoil vortex knot in water
(Klecker & Irvine 2013)
Linear and angular momentum by signed area information
Let denote the centreline of a vortex filament with ( ). χ ω = ω
0ˆt ω
0= cst.
Theorem (Ricca 2008). The components of linear and angular
momentum of a vortex filament of circulation Γ , given respectively by
P = (P
x, P
y, P
z) and M = (M
x,M
y,M
z) , can be expressed in terms of signed areas of the projected graph regions:
.
,
- the linear momentum is given by
- the angular momentum is given by
Λ = ˆ ν ( χ ) :
3→
2How to compute ?
For individual components, we have
P
x: Λ
xA
x= A ( ) Λ
xLet denote the vortex axis: ( ) , and ; χ ω = ω
0ˆt ω
0= cst.
X = ˆt = ′ dX ds
, since , we have and
Proof.
X ds = dX ′
and
P
y: Λ
yA
y= A ( ) Λ
yP
z: Λ
zA
z= A ( ) Λ
zand and
where denotes the standard graph projected along the x -axis and the signed area of . Similarly for the y - and z -axis and M
x, M
y, M
z.
. P = 1
2 X × ω d
3X
V ω
( )
∫ = 1 2 Γ ∫
L χ( ) X × ′ X ds = Γ ∫
A χ( ) d
2X
M = 1
3 ∫
V ω( ) X × X × ( ω ) d
3X = 1 3 Γ ∫
L χ( ) X × X × ′ ( X ) ds = 2 3 Γ ∫
A χ( ) d
2X
Computation of signed area of a planar graph
ˆt +1 ρ ˆ
R
χ
To each sub-region of Λ we assign an index that weights the relative contribution from the circulation of neighbouring strands:
R
jwhere according to the r.h.
sign convention of the reference .
3
2
where is the standard area of .
The signed area of Λ is thus given by +1
–1
–2 –1
0
Thus, by the standard definitions of momenta and the observations above we have:
P = 1
2 Γ X × ′ X ds
L χ