Phase Space Instability with Frequency Sweeping

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1 Phase Space Instability with Frequency Sweeping H. L. Berk and D. Yu. Eremin Institute for Fusion Studies Presented at IAEA Workshop

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Phase Space Instability with Frequency Sweeping. H. L. Berk and D. Yu. Eremin Institute for Fusion Studies Presented at IAEA Workshop Oct. 6-8 2003. “Signature” for Formation of Phase Space Structure (single resonance). Berk, Breizman, Pekker. - PowerPoint PPT Presentation

Transcript of Phase Space Instability with Frequency Sweeping

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Phase Space Instability with Frequency Sweeping

H. L. Berk and D. Yu. Eremin

Institute for Fusion Studies

Presented at IAEA Workshop

Oct. 6-8 2003

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“Signature” for Formation of Phase Space Structure (single resonance)

Explosive response leads to formation of phase space structure

Berk, Breizman, Pekker

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Simulation:N. Petviashvili

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“BGK” relation•Basic scaling obtained even by neglecting effect of directfield amplitude •Examine dispersion with a structure in distribution function(e.g. hole)

0 = ε(ω,k) =1 +ω p

2

kdv∫

∂f (v)

∂vω − kv

≈2(ω −ω p )

ω p

+ω p

2

kdv∫

∂[ f (v) − f0(v)]

∂vω − kv

0 ≈ω − ωp

ω(1−

γ L

ωb

); thus γ L ≈ ωb

v

ωb

k

f (v) - f0 (ω0

k)

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Power Transfer by Interchange in Phase Space

Ideal Collisionless Result

ωb =163π 2 γ L ; δω =

π

2 2

γ d

γ L

⎛ ⎝ ⎜

⎞ ⎠ ⎟

1/ 2

ωb3/2t1/2

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TAE modes in MAST

(Culham Laboratory, U. K. courtesy of Mikhail Gryaznevich)

IFS numerical simulation Petviashvili [Phys. Lett. (1998)]

L linear growth without dissipation; for spontaneous hole formation; L d.

ω =(ekE/m)1/2 0.5L

With geometry and energeticparticle distribution known internalperturbing fields can be inferred

Predicted Nonlinear Frequency Sweeping Observed in Experiment

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Study of Adiabatic EquationsStudy begins by creating a fully formed phase spacestructure (hole) at an initial time, and propagate solutionusing equations below.

∂f (J, t)

∂t−ν eff

3 ∂

∂J(∂J

∂EJ

∂f (J, t)

∂J) = 0 (in trapped particle region),

δωωb2 =

4γ L

π 2 ∂f0(ω0)

∂ω

dE[ f (J (E), t) − f0−ω b2

ω b2

∫ (ω0 +δω)]dφ

[2(E + ωb2 cosφ)]1/ 20

φ max

γ dωb4 = −

γ L

dδω

dt

π∂f0 (ω0 )

∂ω

dJ[ f (J, t) − f00

Jsep

∫ (ω0 + δω)]

J =dϕ

2π∫ p =2

πdφ

0

φmac

∫ [2(E(J) +ωb2 cosφ)]1/2, E ≡ energy in local wave frame

Note: If ν eff = 0, ωb(δω, t) depends only on δω(t)

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Results of Fokker-Planck Code

sweeping terminates why?

sweeping goes tocompletion

δ ˆ ω ≡δων eff

3/ 2

ωbi(γ dγ L2 )1/ 2

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Normalized Adiabatic Equation, eff=0Dimensionless variables:

δωδω0

→ Ω, ωbi → 1, ωb → Ωb , Jsep → Ω b1, J → Ωb I, f (J) → GT (Ωb I)

Ωb =1− 1

ΩdIGT(IΩb)Q(I)

0

1

I = (2 2)−1 dφ[E'+cosφ]1/20ϕ max

∫ , Q(I) =3 dφcosφ /[E'+cosφ]1/2

0ϕ max

∫dφ /[E' +cosφ]1/2

0ϕ max

“BGK” Equation

Take derivative with with respect to Ωb

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Propagation Equation;Difficulties

dΩdΩb

=ΩHT (Ω,Ω b)

1− Ω b

HT(Ω,Ω b ) = 1+ (ΩΩ b )−1 dIIdGT (IΩ b )

dI0

1

∫ Q (I)

Problems with propagation

a. HT (Ω Ω ) = 0, termination of frequency sweepingb. 1- Ω = HT (Ω Ω ) = 0; singularity in equation, unique solution cannot be obtained

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Instability AnalysisBasic equation for evolving potential in frame of nonlinear wave (extrinsic wave damping neglected), 1= P(t) cos x + Q(t) sinx; Ω Ω Ω

dQ

dt+ ΔΩP = −β dΓf cos(x)∫

dP

dt− ΔΩQ = β dΓ f sin(x∫ )

f satisfies Vlasov equation for:

f ( x,v, t) = F (E ) +δ ˆ f (E, x)exp(−iω t)

Spatial solutions are nearly even or odd

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Analysis (continued)

F(J)-F0(Ω ) ΩGT

Ω ΩJ

Find equilibrium in wave frame:

E = (v − Ω2 ) / 2 − Ω b2 cos x, J = ΩbI ; solve for Ωb = 1− dIGT (IΩb )Q(I)

0

1

∫ Linearization:

φ=[δP cos x + δQsin x]exp(−iω t); lowest order δQ = 0 + ϑ (Ω b / ΔΩ)

Perturbed distribution function

δf (E, x) = −∂GT (E )

∂EδPe −iωt[cosx − iω dt'e− iωt ' cos x(t ')( )

−∞

0

∫ ]

cos x(t)( ) = < cos x >2n cos4πn

T (E )t −τ (E, x)( )

⎣ ⎢

⎦ ⎥

n=1

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Dispersion Relation

HT'

2≡ 1− β dE

∂GT (E)∂E−Ω b

2

Ω b2

∫ T (E )[< cos2 x > 0 − < cos x > 02]

= 2β dE-Ω b

2

Ω b2

∫n=1

∑∂GT (E)

∂ET (E )

ω2 < cos x > 2n2

2n2π

T (E) ⎛ ⎝ ⎜

⎞ ⎠ ⎟2

−ω 2

ω <<Ω b ⏐ → ⏐ ⏐ σΩ2, σ > 0

Identity

Instability Arises if H T' < 0

HT' = HT =1 +

1Ωb

dIIdG(Ωb I)

dI0

1

∫ Q(I)

Consequence: Adiabatic SweepingTheory “knows”about linear instability criterion for both types of Breakdown: (a)sweeping termination (b) singular point

Onset of instability necessitates non-adiabatic response

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Comparison of Adiabatic Code and Simulation

Ωb0 =1.16, γ L

ωbi

=1.85, γ d

ωbi

= .093, I* = 0.8, ΔΩ

ωbi

= 9.26

(passing particle distribution flat)

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Evolution of Instability

Trapping frequency,ωb ωbiSpectral Evolution, δωL

slope in passing particle distribution

Indication that Instability Leads to Sideband Formation

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Side Band Formation During Sweeping

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Summary1. Ideal model of evolution of phase structure has beentreated more realistically based on either particle adiabatic invariance or Fokker-Planck equation 2. Under many conditions the adiabatic evolution of frequency sweeping reaches a point where the theory cannot make a prediction (termination of frequency sweeping or singularity in evolution equation)3. Linear analysis predicts that these “troublesome” points are just where non-adiabatic instability arises4. Hole structure recovers after instability; frequency sweeping continues at somewhat reduced sweeping rate5. Indication the instability causes generation of side-bandstructures

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Finis

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Linear Dispersion Relation

HT(Ω,Ω b ) / 2 = −σ γ 2, if γ 2 << Ω b2 , σ > 0

Linear Instability if HT < 0

Hence HT(ΩΩb) =0 is marginal stability conditionof linear theory. Adiabatic theory breakdown due tofrequency sweeping termination, or reaching singularpoint is indicative of instability. Then there is an intrinsic non-adiabatic response of this particle-wave system

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