Ray Tracing and Full-wave Simulation of KSTAR LH Wave

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Ray Tracing and Full-wave Simulation of KSTAR LH Wave 2016 KO-JA Workshop on Physics and Technology of Heating and Current Drive Presented by Young-soon Bae NFRI a W. Namkung, a M.H. Cho, b S. Shiraiwa, c S.C. Kim, c Y.S. Hwang a POSTECH, b MIT, c SNU

Outline LH wave accessibility and Landau damping Off-midplane and inside launching Ray tracing study of outside midplane launcher Full-wave simulation for wave coupling and propagation Summary

Understanding of LH wave accessibility condition and Landau damping is important for desirable launcher design /m 3 ] 20 1 0.8 0.6 Accessibility (red dash) and Landau Damping zone (white solid) 3.7 3.6 3.39 3.49 3.17 3.28 High n 2.96 //acc 3.07 2.75 3.16 2.85 2.54 3 kev 2.64 2.32 2.43 2.74 4 kev 2.24 KSTAR 6 kev The wave propagation is proved to closely depend on the LH wave accessibility condition, by which maximum wave phase velocity parallel to magnetic field in the plasma is determined And wave is absorbed through the Landau damping ne(0) [10 0.4 0.2 5 kev 2.45 2.07 7 kev 2.22 1.83 2 2.11 1.9 Low n //acc 1.79 10 kev 1.94 8 kev 1.73 1.69 nn,aaaaaa = 1 ωω 2 pppp ωω 2 + ωω 2 pppp 2 + ωω pppp ωω cccc vv ppp = vv = 3~5 vv ttt nn LLLL = 5.4/ TT ee ωω cccc 1.8 2 2.2 2.4 2.6 2.8 3 Bt [T] n //acc < n // < n LD

Wave accessibility and Landau damping for H- mode density profile Inside Outside (Outboard) Inside launch : higher field increases the window for accessibility and strong LD allowing lower n // to penetrate, which improves efficiency since η ~ 1/n // 2

The off-midplane launch has a benefit of significant upshift on the evolution n // Off-midplane launch Robust accessibility and off-axis current drive avoiding wave interactions in SOL region (PDI, power spectrum splitting, collisional damping, etc) Y.S. Bae et al, PPCF 58 (2016) 075003

Outside midplane launcher in KSTAR 5 GHz LHCD Conventional grill waveguide launcher To be replaced by steady state launcher (PAM)

Ray tracing and Fokker Planck calculation for KSTAR outside midplane LH launcher using GENRAY/CQL3D code Plasma density and temperature profile - Theoretical H-mode pedestal profile near rho = 0.9 LCFS Midplane launcher: 4-row 5.8 cm height waveguide grills launcher 2-cm behind LCFS For simplicity, only main forward peak is considered in GENRAY/CQL3D simulations - total launched power of 1.5 MW loaded to forward power

Multiple reflections in 2 T case even with high n // = 2.5 2T 2.5T ne=3e19/m3, Te=5keV

LH-drive current profile is strongly dependent upon temperature and density profiles both for n // = 2.0 and 2.5 Temperature Density B0= 2.5 T, n // =2.0 B0= 2.5 T, n // =2.5

Current drive efficiency for Bt = 2.0 T Current drive dependency on the density for various Te(0) and n // (2.0, 2.2, 2.5) for ne(0)=7x10 19 /m 3, 80~150kA/MW and η = 1~2.8x10 19 Am -2 W -1 for Te(0)=3-10keV η = ne*r*icd/pabs

Current drive efficiency for Bt = 2.5 T ~20% enhancement than Bt=2T Current drive dependency upon density for various Te(0) and n // 100~250kA/MW and η = 1.5~2.7x10 19 Am -2 W -1 for ne(0)=7x10 19 /m 3

Current drive efficiency for Bt = 3.0 T Similar CD efficiency as Bt=2.5T Current drive dependency upon density for various Te(0) and n // 120~200kW/MW and η = 1.5~3.0x10 19 Am -2 W -1 for ne(0)=7x10 19 /m 3

Effect of fast electron diffusion Confinement time of fast electron τ F /τ E ~ γ α α = 3~4 In Cylindrical geometry, χ F a 2 /(6τ F ) If 100 kev, γ = 1.1956; For KSTAR, τ F = τ E γ α 0.1 s x 1.1956 3 ~ 0.2 s χ F ~ 0.2 m 2 /s ne(0)=5x10 19 /m 3 Te(0)=7 kev I CD decreases by ~20%

Reversed spectrum from the launcher with forward to reverse power loading, 70:30% results in reduced current drive by ~ 40% 7:3 Only main peak With reversed spectrum n // = φφ + 22ππmm, mm = llll, ll = 00, ±11, ±22, kk 00 pp NNkk 00 pp p is period N is number of active waveguide in each PAM module ϕ=270deg l=0, n//=-2.5 (main lobe) l=-2, n//=4.2 (opposite lobe) With reversed spectrum I CD = 180 ka With only main peak I CD = 320 ka

Multiple side lobes results in much smoother spectral gap filling Multiple high n tor side lobes are predicted by theoretical calculation of power spectrum from the grill launcher - 3 high n tor peaks are included for n 0 = 2.5 - Different from customary approach with the only main peak, which tends to result in poorer spectral phase space filling

Proposed configuration of KSTAR 3 MW PAM launcher using 8 x 0.5 MW klystrons K1 X 8 3-dB hybrid splitter 2 way x 4 way x 4 active x 8 klys = 256 active wgs (32 toroidal x 8 poloidal) n// = φφ kk 00 pp + δδδδ 111111 NN wwww kk 00 pp 111111/ππ =2.5 7mm 5 mm 3 mm ~600 mm 55 mm A P A P ϕ=270deg 250kW CW BeO window 4 active x 4 passive 180deg N wg = 4 p = 18mm 4-way splitter Power flux 3MW/256/(58mmx7mm) = 28.8MW/m 2 ITER design: 33 MW/m 2 Tore Supra: 25 MW/m 2 (2.7 MW during 78 s) to be increased to > 30 MW/m 2 K n-1 δϕ=180deg K n

RF power reflection calculation in PAM launcher from the edge plasma using FEM-based full-wave simulation Perfect Matched Layer (PML) Plasma with high conductivity Plasma Bt COMSOL Multiphysics model 16 active and 17 passive waveguides With ba = 7 mm, bp = 7 mm (5 mm), e = 3mm (2mm) Wave equation kk kk EE kk 0 2 εε rr ii σσ ωωεε 0 EE = 0 Plasma model: Dielectric tensor in Stix s frame εε rr = SS iiii 0 iiii SS 0 0 0 PP

Wave propagation from the PAM grill waveguides shows two main lobes of the radiation spectrum Nwg = 16 n main = -2.5; n opp = 4.1 Directivity = 55 % Fourier Transform of Ex near the launcher ba=7mm,bp=7mm, e=2mm ne(0)=0.6x10 18 /m 3 ba=7mm,bp=5mm, e=3mm ne(0)=0.6x10 18 /m 3

Power reflection as a function of edge density (n e_edge ) and density gradient (n e / n e ) Reflection changes significantly with density gradient at the low density regime, but less effect at high density regime ba=7mm, bp= 7 mm, e = 2 mm ba=7mm, bp=5mm, e=3 mm

LH wave propagation inside tokamak using FEM-based full-wave simulation Collaboration with MIT Conventional PDE solved by COMSOL Convolution integral done in LiveLink Matlab

Stix s dielectric tensor should be rotated with two angles defined by 3D equilibrium magnetic field data (Bx, By, Bz) Dielectric tensor in Stix s frame KSTAR εε = SS iiii 0 iiii SS 0 0 0 PP iiεε EEEEEE Rotation of dielectric tensor R(θ, φ) ε R(-θ, -φ) θ and φ is defined with Bx, By, Bz

Summary Using GENRAY/CQL3D code, the wave ray tracing and its current drive are studied for KSTAR outside midplane launcher. The simulation results show that high toroidal magnetic field or high launched n // is recommended according to accessibility condition and strong Landau damping. A significant LH wave current drive could be obtained for the wave spectrum with peak value n // = 2.5 if a toroidal magnetic field B t = 2.5 ~ 3.0 T is applied. Further studies in full wave simulation is planned for the investigation of the of LH wave non-linear interaction in SOL region and edge region. Proposed off-midplane (top launcher) for strong single pass absorption hence high CD efficiency in KSTAR LHCD is being considered for future upgrade

Next time, I hope to see you again in Hokkaido (?) with another topic of top launcher of ECH

Lower hybrid wave penetration and absorption Lower hybrid wave frequency in tokamak Density limit (related to PDI) ωω > 5ωω LLLL Accessibility ωω LLLL = ωω pppp 2 ωω pppp 1 + 2 ωω cccc 1/2 n e (0) = 1 x 10 20 /m 3, B t = 2 T nn 1 = 1 + ωω 2 pppp 2 1 ωω ccccωω cccc ωω cccc ωω 2 + ωω pppp ωω cccc 2 ωω GGGG = ωω cccc ωω cccc Landau damping Linear Quasi Linear nn 2 = nn 2 = 30 TT ee (kkkkkk) vv ppp = vv = 3vv ttt 49 TT ee (kkkkkk) vv ppp = vv = 2.3vv ttt 24