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Particle and fluid models for streamers: comparison and spatial coupling Li Chao 1 in cooperation with: W.J.M. Brok 2, U. Ebert 1,2, W. Hundsdorfer 1, and J.J.A.M. van der Mullen 2 1. Centrum voor Wiskunde en Informatica (CWI) A’dam 2. Eindhoven University of Technology (TU/E) Eindhoven
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Streamers in laboratory [ Talk: Exploring streamer variability in experiments. T.M.P. Briels] Understand streamer dynamics. Here: electron dynamics in ionization front. For simplicity: Negative streamer in N 2 electronsnet charge Streamers in numerical simulation [Talk: Efficient fluid streamer simulations in 2D and 3D: methods and results. A. Luque]
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Simulation models: advantages and disadvantages Fluid model Particles : electrons and ions Deterministic free flight between Monte Carlo Collisions Particle model Efficient computations in continuum approximation. Full physics : correct energies run away electrons perturbations for branching discrete particles in low density region but too many particles for CPU Compare and combine models! DriftDiffusion Ionization reaction E
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Particle swarm experiments generate µ(E), D(E), α(E), and ε(E). Fluid model Particles : electrons and ions Deterministic free flight between Monte Carlo Collisions. Particle model DriftDiffusion Ionization reaction
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Planar front in particle model: E=E + E=0 Periodic boundary condition Charge layer with charge: Streamer front planar approximation z E=E + E=0 Periodic boundary condition Charge layer with charge: Streamer front planar approximation z
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Particle planar front simulation at 100 kV/cm E=E + E=0 Periodic boundary condition Charge layer with charge: Streamer front planar approximation z
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1.The speeds are almost same. 2.The densities differ by 20%. Planar front simulation results comparison at 100 kV/cm Comparison of particle model with re-derived fluid model:
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1.The speeds are almost same. 2.The densities differ by 20%. Planar front simulation results comparison at 100 kV/cm Comparison of particle model with re-derived fluid model:
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higher energy larger ionization rate in front density discrepancy behind position of the model interface Energy overshoot
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z t1t1 t2t2 t3t3 Constant field E Swarm experiments: Energy overshoot because density decay length is similar to energy relaxation length. Field gradient is not important. avalanche front Same leading edge [C. Li et al. J. Appl. Phys. 2007 ]
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z (mm)
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[C. Li et al., submitted (2007)] at 100 kV/cm
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Improve fluid approximation: Adjust definition of mobility: 1.By mean displacement of swarm avalanche ZZ1Z1 Z2Z2 [N L Aleksandrov and I V Kochetov, J. Phys. D. 29 (1996) 1476-1483.] [G V Naidis, Tech. Phys. Lett. 23(6) (1997) 493.]
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Adjust definition of mobility: 1.By mean displacement of swarm avalanche 2.By mean displacement of initially present particles ZZ1Z1 Z2Z2 Z2Z2 Improve fluid approximation: [N L Aleksandrov and I V Kochetov, J. Phys. D. 29 (1996) 1476-1483.] [G V Naidis, Tech. Phys. Lett. 23(6) (1997) 493.]
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Adjust definition of mobility: 1.By mean displacement of swarm avalanche 2.By mean displacement of initially present particles 3.By averaging the local fluxes μ 1 ≥ μ 2 = μ 3 Improve fluid approximation: [N L Aleksandrov and I V Kochetov, J. Phys. D. 29 (1996) 1476-1483.] [G V Naidis, Tech. Phys. Lett. 23(6) (1997) 493.]
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First VersionImproved version
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Conclusion and outlook Conclusion The fluid approximation is valid, except in the leading edge of the ionization front. Spatial coupling of fluid and particle model realized in 1D. Result: relevant particle physics kept: a) correct energies b) run away electrons c) perturbations for branching d) discrete particles in low density region but computational efficiency largely improved. Outlook 1.Incorporate in 3D computations. 2.Include photo-ionization etc.
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