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ERO code development. A. Kirschner M. Airila, D. Borodin, S. Droste, C. Niehoff. The ERO code ERO code management Modelling of CH 4 puffing in ASDEX Modelling of CH 4 puffing in JET. The ERO code. 3- dimensional (at present 2D for divertor), Monte Carlo - PowerPoint PPT Presentation
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ERO code development
A. Kirschner
M. Airila, D. Borodin, S. Droste, C. Niehoff
The ERO code
ERO code management
Modelling of CH4 puffing in ASDEX
Modelling of CH4 puffing in JET
The ERO code
3-dimensional (at present 2D for divertor), Monte Carlo
Various experimental geometries are possible(at the moment: TEXTOR, ASDEX, JET, ITER, PISCES, MAGNUM)
Plasma-wall-interaction:
- physical sputtering, chemical erosion (CH4 or higher hydrocarbons)
- C-deposition from background, re-deposition of eroded particles Local particle transport:
- ionisation, recombination, dissociation
- Ehrhardt/Langer or Janev data for CH4 reaction chain
- friction (Fokker-Planck), thermal force, Lorentz force, diffusion D
ERO code management (1)
Several users and developers: version controlling necessary
CVS (Concurrent Versions System) – server at FZJ
Variety of versions
ERO.LIM
ERO.DIV
ERO.LINEAR
“Main line of
development”CVS parallelisation
ERO code management (2)
Development of user friendly interface (“JERO”)
in combination with ERO internet webpage
Modelling of 13CH4 puffing in ASDEX (1)
-1.2
-1.1
-1
-0.9
-0.8
-0.7
-0.6
-0.5
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9
R [m]
Z [m]
ERO simulationvolume
80° rotation
B2-Eirene grid of divertor region
ERO simulation volume (outer divertor):
0
40
80
120
160
-160 -120 -80 -40 0 40 80 120 160
distance along outer target [mm]
r [m
m]
separatrix
Modelling of 13CH4 puffing in ASDEX (2)
Modelling of 13CH4 puffing in ASDEX (3)
Plasma parameter (L mode) from B2-Eirene (D. Coster)
separatrix
Modelling of 13CH4 puffing in ASDEX (4)
CH4 CH2 CH
CH+ C C+
0 80 mm
80mm
0CH4
Transport of injected CH4 into outer divertor @ s=48mm:
sticking assumption for hydrocarbons S = 0
C-Deposition from injected CH4 (@ 48mm) into outer divertor:
sticking assumption for hydrocarbons S = 0
local deposition: ~70%, losses to PFR: ~30%
0
0.2
0.4
0.6
0.8
1
-160 -120 -80 -40 0 40 80 120 160
distance along outer plate [mm]
de
po
sit
ion
[a
.u
.]
PFR
SEP
SOL
Modelling of 13CH4 puffing in ASDEX (5)
Modelling of 13CH4 puffing in ASDEX (6)
Injection of CH4 (@ 48mm and 88mm) into outer divertor:
Puff @ 48 mm Puff @ 88 mm
S = 0 S = 1 S = 0 S = 1
Deposition at target 70% 96% 89% 99.4%
Puffing location deeper in SOL: high local re-deposition even if with S = 0!!!
Further 13C transport modelling in ASDEX:
in co-operation with M. Airila
(Helsinki University of Technology)
Modelling of 13CH4 puffing in ASDEX (7)
Modelling of CH4 puffing in JET (1)
MkIIA: Standard gas fuelled ELMy H-mode, 12 MW (#44029)
ne [cm-3]
240230 250 260220
-170
-160
-150
-140
-130
-180
RC [cm]
ZC [cm]
240230 250 260220
-170
-160
-150
-140
-130
-180
RC [cm]
ZC [cm] Te [eV]
• Zero sticking of hydrocarbons CDy, Ehrhardt-Langer• Location of injection: strike point
Profiles of re-deposition for various incoming ion fluxes:
Amount ofre-deposition:
88%
89%
87%
vertical plate
base plate
0.0E+00
2.0E+12
4.0E+12
6.0E+12
8.0E+12
1.0E+13
1.2E+13
0 50 100 150 200 250 300 350 400x along plates [mm]
par
ticl
es/a
rea
[a.u
.] (0.5ne, 2Te)
(ne, Te)
(2ne, 0.5Te)
Modelling of CH4 puffing in JET (2)
Modelling of CH4 puffing in JET (3)
Amount ofre-deposition:
76%
72%
66%
0.0E+00
1.0E+12
2.0E+12
3.0E+12
4.0E+12
5.0E+12
0 50 100 150 200 250 300 350 400x along plates [mm]
par
ticl
es/a
rea
[a.u
.] (0.5ne, 2Te)
(ne, Te)
(2ne, 0.5Te)
vertical plate
base plate
• Zero sticking of hydrocarbons CDy, Ehrhardt-Langer• Location of injection: center of base plate (SOL)
Profiles of re-deposition for various incoming ion fluxes:
Summary: re-deposition of injected CD4 and C2D4
Injection at strike point: Injection at center of base plate (SOL):
0
20
40
60
80
100
0.5 0.75 1 1.25 1.5Incoming Ion Flux [a.u.]
amo
un
t [%
]
0
20
40
60
80
100
CD4
C2D4
(0.5ne / 2Te) (ne / Te) (2ne / 0.5Te)
0
20
40
60
80
100
0.5 0.75 1 1.25 1.5Incoming Ion Flux [a.u.]
0
20
40
60
80
100
CD4
C2D4
(0.5ne / 2Te)(2ne / 0.5Te)(ne / Te)
• No significant difference in re-deposition of puffed CD4 and C2D4
• Puffing at strike point: no significant dependence on flux
• Puffing at center of base plate (SOL): decreasing re-deposition with increasing flux
Modelling of CH4 puffing in JET (4)