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Dynamics of transport barrier relaxations in tokamak edge plasmas P - - PowerPoint PPT Presentation

CNRS UNIVERSITE DE PROVENCE ASSOCIATION EURATOM CEA Dynamics of transport barrier relaxations in tokamak edge plasmas P . Beyer, S. Benkadda, G. Fuhr-Chaudier Laboratoire PIIM, Equipe Dynamique des Syst` emes Complexes CNRS


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CNRS – UNIVERSITE DE PROVENCE ASSOCIATION EURATOM – CEA

Dynamics of transport barrier relaxations in tokamak edge plasmas

P . Beyer, S. Benkadda, G. Fuhr-Chaudier Laboratoire PIIM, Equipe Dynamique des Syst` emes Complexes CNRS – Universit´ e de Provence, Marseille, France

  • X. Garbet, Ph. Ghendrih, Y. Sarazin

Association Euratom – CEA, CEA/DSM/DRFC CEA Cadarache, France

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Introduction

  • The operational regime of future fusion

reactors is characterized by – an edge transport barrier, – relaxation oscillations of the barrier (Edge Localized Modes, ELMs).

  • Explanations for relaxations are usually

based on MHD instability,

q=2 q=2.5 q=3 50 100 150 minor radius mean pressure

with barrier w/o barrier

– analysis of linear stability properties, no dynamics.

  • Most existing dynamical models are phenomenological,

– not based on 1st principles, i.e. turbulence simulations.

  • Frequency, crash time and energy release are central issues.

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Outline

  • Overview of existing reduced dynamical models

for transport barrier relaxations.

  • 3D fluid turbulence simulations.
  • Subsequent reduced 1D model.
  • Systematic reduction
  • 0D model.

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Reduced models for barrier dynamics: not straightforward

  • simple model (1D):

transport eqn. coupled to instability amplitude eqn. at plasma edge

∂t ¯ p

=

  • ∂x

χ0 ¯ π

χ1

ξ

2 ¯

π

  • Γ

∂tξ

=

γ0

¯ π

  • αc

ξ

ν0∂2

¯ π

  • ∂x ¯

p ¯ p: pressure profile, ξ: perturbation ampl., Γ: incoming energy flux, x: minor radius

x p Γ

  • no oscillations, stable fixed point, robust property

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Possible modifications to obtain oscillations or relaxations

  • Introduction of S–curve

– for dependency of flux vs gradient (due to ExB shear flow), – in dynamical eqn. for perturbation amplitude (explosive instability), – in dynamical eqn. for ExB shear flow (multiple states: L–H).

  • Introduction of characteristics of ideal MHD eigenmodes

– vanishing growth rate below threshold, – radial shape of global modes.

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S–curve for flux vs gradient produces relaxations

  • Introduce ambient turbulent flux Γturb

due to drift waves, etc.

  • ˜

Φ

¯ π

✝ ✞

Γturb

¯ π

✝ ✂

χ0 ¯ π : S-curve due

to turb. stabilization by ExB shear flow.

∂t ¯ p

  • ∂x
  • ˜

Φ

¯ π

✝ ✂

χ1

ξ

2 ¯

π

  • Γ

∂tξ

γ0

¯ π

  • αc

ξ

ν0∂2

¯ π

  • ∂x ¯

p

  • Relaxations, frequency
✂ ✂ ✂

with power.

  • More sophisticated models available.

p

¯ π

Lebedev, Diamond, PoP 95

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Explosive instability

  • Account for non-linear terms in amplitude equation:

first is destabilizing, second is stabilizing.

∂t ¯ p

=

  • ∂x

χ0 ¯ π

χ1

ξ

2 ¯

π

  • Γ

∂tξ

=

γ0

¯ π

  • αc

ξ

µξ2

  • νξ3

¯ π

  • ∂x ¯

p

  • Dynamics close to Van der Pol oscillations.

Cowley, Wilson, PPCF 03

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Multiple states for shear flow

  • L–H transition: multiple states for ExB shear flow ¯

u

¯ π

, and: effective flux χeff

¯ u

¯ π depends on shear flow. ∂t ¯ p

=

  • ∂x
  • χeff

¯ u

¯ π

  • Γ

∂t ¯ u

=

¯ π

  • αc
  • µ1 ¯

u3

µ2 ¯ u

ν∂2

x ¯

u ¯ π

  • ∂x ¯

p

  • Ginzburg–Landau type, limit cycle oscillations.
  • No perturbation amplitude, more appropriate for “dithering”.
  • Generalization to ELMs available.

Itoh, Itoh, PRL 91, PRL 95

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Linear ideal MHD instability model

  • Linear ideal MHD eigenmodes:

– growth rate

  • 0 below threshold,

– global mode structure.

  • Modeled by

– Heaviside funct. H on growth rate, – Gaussian shape G in eff. diffusivity

∂tξ

γ0

¯ π

  • αc

H

¯ π

  • αc

ξ

  • ν

ξ

  • ξ0

+ transp. code with χeff ∝

ξ

2G

x

  • Relaxations, frequency
✂ ✂ ✂

with power.

  • More sophisticated models (peeling).

  • nnroth, Parail, PPCF 04

B´ ecoulet, Huysmans, EPS 03

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State of the art

  • Most existing models are phenomenological.
  • Difficult to reproduce relaxations with frequency
  • with power.
  • Turbulence simulations of relaxations exist,

based on turbulent ExB flow generation, no barrier.

  • Need for 1st principles based model, i.e. 3D turbulence simulations,

reproducing i) transport barrier ii) complete relaxation cycle.

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3D edge turbulence simulations with transport barrier

  • turbulence model: resistive ball. modes,

reduced MHD equations

∂t∇2

  • φ
✂ ✁

φ

∇2

  • φ
✄ ✞
  • ∇2

φ

  • Gp

ν∇4

  • φ

∂t p

✂ ✆

φ

p

✝ ✞

δcGφ

χ

∇2

p

χ

  • ∇2
  • p

S

  • 3D toroidal geometry at plasma edge
  • driven by incoming flux Γin
✞ ✞

r rmin Sdr

,

  • press. profile evolves self-consistently
  • barrier generated by imposed flow U,

locally sheared, ωEext

✞ ✆

∂rU

max

0rmin rq=2 rq=2.5 rq=3 rmax S(r)

radial profile of source S

rmin rq=2 rq=2.5 rq=3 rmax U(r)

radial profile of imposed flow U

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Strong local ExB shear

  • formation of barrier

q=2 q=2.5 q=3 10 20 30 rayon flux turbulent

ωEext=7.3 ωEext=5.5 ωEext=3.7 ωEext=0

q=2 q=2.5 q=3 200 400 600 rayon pression moyenne

ωEext=7.3 ωEext=5.5 ωEext=3.7 ωEext=0

turbulent flux profile time averaged pressure profile

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Barrier relaxation oscillations appear

0.5 1 normalized pressure gradient 5 10 15 normalized turbulent flux 3000 5000 7000 9000 −0.6 −0.4 −0.2 normalized velocity shear fluctuations time

1.

∂x ¯ p

Γin

  • χ
  • 2. Γturb
  • Γin

3.

ωE

  • ωEext
  • ωEext
  • all evaluated at barrier center
  • bserved in a range of Γin, ωEext
  • robust property

scenario:

  • turb. state

relaxations

quiescent st.

ωE

no barrier

barrier

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Fixed input power: frequency decreases with shear

5 10 15 normalized turbulent flux

ωE = 14

5 10 15

ωE = 12

5 10 15

ωE = 10

5 10 15

ωE = 8

3000 6000 9000 12000 5 10 15 time

ωE = 6

input power: Γ

36

shear layer width: 28.8%

2 4 6 8 10 12 400 800 1200 1600 2000 # time lag time lag ωE = 12 ωE = 10 ωE = 8 ωE = 6

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Fixed input power: frequency decreases with shear

10 20 normalized turbulent flux

ωE = 14

10 20

ωE = 12

10 20

ωE = 10

10 20

ωE = 7.3

10 20

ωE = 5.5

3 8 13 18 10 20 time / 103

ωE = 3.7

input power Γ

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shear layer width: 34.4%

4 8 12 16 400 800 1200 1600 2000 # time lag time lag ωE = 12 ωE = 10 ωE = 7.3 ωE = 5.5 ωE = 3.7

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Fixed flow shear: frequency increases with power

2 4 normalized turbulent flux

Γ = 12

2 4

Γ = 11

2 4

Γ = 10

3 8 13 18 2 4 time / 103

Γ = 9

flow shear: ωE

2

shear layer width: 34.4%

4 8 12 16 400 800 1200 1600 # time lag time lag Γ = 12 Γ = 11 Γ = 10 Γ = 9

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Frequency dependence: two opposite trends

freq.

✂ ✂ ✂

with Γin for ωE fixed (ωE

  • 2)

9 10 11 12 2 4 6 Γ (time lag)−1 × 103 9 10 11 12 250 500 Γ standard deviation of time lag

freq.

  • with ωE for Γin fixed (Γin
  • 36)

4 8 12 2 4 6 shear layer width ωE (time lag)−1 × 103 0.288 0.313 0.344 4 8 12 250 500 ωE standard deviation of time lag

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Frequency dependence: two opposite trends

if ωE increases fast enough with Γin

  • frequency decreases with Γin.

0.5 1 normalized pressure gradient 3 8 13 18 2 4 normalized turbulent flux time/103

Γin

  • 10
  • ωE
  • 2

0.4 0.8 1.2 normalized pressure gradient 3 8 13 18 5 10 15 20 normalized turbulent flux time / 103

Γin

  • 36
  • ωE
  • 12

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Possible mechanisms excluded

  • Relaxations persist even if ExB

shear flow is frozen

  • mechanism

turbulent shear flow generation.

  • No significant variation of modes

localized outside barrier

  • mechanism

toroidal mode coupling.

  • All fluctuations die out when sup-

pressing curvature

  • Kelvin–Helmholtz stable.

Γin

  • 36
  • ωE
  • 8

0.5 1 normalized pressure gradient 5 10 15 normalized turbulent flux 3000 5000 7000 9000 −0.6 −0.4 −0.2 normalized velocity shear fluctuations time

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Relaxation governed by mode at barrier center

snapshots of potential fluctuations between relaxations during relaxation

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1D model for central mode amplitude ˜

p

  • x

t

˜ p

  • x

t

˜ p

  • x

t

& profile ¯

p

  • x

t

¯ p

  • x

t

¯ p

  • x

t

∂t ¯ p

  • 2γ0∂x

˜ p

2

χ

  • ∂2

x ¯

p

S ∂t ˜ p

γ0

  • ∂x ¯

p

  • α0

˜ p

Ex ˜

p

  • χ
✟ ☎

x2 ˜ p

χ

  • ∂2

x ˜

p x

r

  • r0: radial dist. from barrier center

m: poloidal wavenumber of central mode

  • reproduces relaxation oscillations
  • ExB shear ω

E

ωEm

  • r0
  • nonlinear short-term dynamics.
  • Not described by linear modes

(long-term dynamics).

0.5 1 normalized pressure gradient 3 6 9 12 15 10 20 normalized turbulent flux time / 103

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Description by linear modes is not appropriate

For ∂x ¯

p

  • α, evolution equation for ˜

p is linear: ∂t ˜ p

γ0

α

  • α0

˜ p

Ex ˜

p

  • χ
✟ ☎

x2 ˜ p

χ

  • ∂2

x ˜

p

  • most unstable eigenmode:

˜ peimθ

  • exp
  • x2

2σ2

imθ

Ex

2 χ

✁ ✂

χ

with σ2

☎ ✆

χ

✝ ✞

χ

✟ ✠
  • growth rate:

γ

γ0

α

  • α0
  • ω

2 E

✁ ✂
  • χ
  • χ
✟ ☎
  • when iω

Ex term replaced by shift of

instability threshold

  • no oscillations

−20 20 −20 20 (r − r0) / ξ r0 θ′ / ξ

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Time delay in stabilization by ExB shear flow

  • Short term dynamics of initial pulse

˜ p

x

t

✞ ✝

∝ δ

x

with

  • ∂x ¯

p

α and χ

✟ ☎

term neglected.

  • Solution :

˜ p ∝ exp

  • γ

0t

  • t3

3τ3

D

✝ ✁

γ

✟ ✞

γ0

α

  • α0

, τD

✞ ✁

1 4χ

  • ω

2 E

  • 1

3

.

  • Transient growth before stabilization.
  • τD large for small χ
  • (barrier) and low m.
  • Clearly observed in simulations (— curve).

10 20 10 20 30 40 time mode amplitude

  • - - curve

γ

✟ ✞ ✂

42 τD

10

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0D model reproduces oscillations Radial mode structure

linear mode

  • From 1D model
  • relevant radial structures: ˜

pR

x

, ˜

pI

x

, ¯

p0

x

✝ ✂

linear mode in case ∂x ¯

p

const: ˜

plin

˜ pR

i ˜ pI

  • Projection: ˜

p

x

t

✝ ✞

aRpR

iaIpI

¯ p

x

t

✝ ✞
  • αx

a0 ¯ p0

  • Amplitude equations:

˙ aR

✞ ✆

Γ

  • δ1a0

aR

Ω1

aR

  • aI

˙ aI

✞ ✆

Γ

  • δ2a0

aI

  • Ω2

aI

  • aR

˙ a0

  • γ0a0

2δ1a2

R

2δ2a2

I Γ

  • γ0

α

  • α0
  • γs
  • γE

γ2

s

  • χ
✁ ✂

χ

Ω1

Ω2

2γEe

γE

γs

γE

  • ω

E 2

✁ ☎

✁ ✂ ✆

400 800 1200 −2 2 Time aR

γE/γs = 0.20 γE/γs = 0.70 γE/γs = 1.24

  • same frequency dependence on ExB shear as in 3D simulations

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Conclusions

  • 3D nonlinear turbulence simulations based on 1st principles show

– onset of transport barrier, – barrier relaxation oscillations.

  • Mechanism based on effective time delay for stabilization by ExB shear,

no obvious S–curve, no global mode.

  • Mean features are reminiscent of type III ELMs:

– frequency dependence, – resistive ballooning mode model (low temperature plasma), – sensitivity to shear flow.

  • turb. state

relaxations

quiescent st.

ωE

no barrier

barrier

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