22nd International Symposium on Plasma Chemistry July 5-10, 2015; Antwerp, Belgium Computational study of a dielectric barrier discharge in argon Y. Peng1, Y. Zhang2, W. Jiang1 and A. Bogaerts2 1 2 School of Physics, Huazhong University of Science and Technology, Wuhan 430074, China Research group PLASMANT, Department of Chemistry, University of Antwerp, 2610 Antwerpen-Wilrijk, Belgium Abstract: The behaviour of a dielectric barrier discharge in argon at atmospheric pressure has been investigated numerically. In this simulation we considered secondary electron emission from the electrodes, which has a vital importance for maintaining the discharge. The electron and ion density and temperature profiles, the electron energy distribution function (EEDF) and the electric field are calculated for a driving voltage of 500 V. In our simulation, the electron and ion densities are in the glow discharge limit, as the ionization degree is lower than 1%. We also find that in the bulk region the electron temperature is higher than the ion temperature, and the EEDF shows one group distribution, which is consistent with a Druyvesteyn distribution. Keywords: dielectric barrier discharge, particle in cell, Monte Carlo 1. Introduction Dielectric barrier discharges (DBDs) [1], also called silent discharges, can occurs when an alternating high voltage is applied to conductive electrodes, at least one of which is covered with a dielectric layer. A prominent feature of DBDs is the simple scalability from small laboratory reactors to large industrial installations. The first experimental investigations were reported by Siemens [2]. It has been developed more than a century since then and its applications have covered many areas, including ozone generation [1, 3], the treatment of polymers [1, 4-6], thin film deposition [1, 7-8], pollution control [1, 9], high power CO 2 lasers [1, 10], ultraviolet excimer lamps [1, 11], and large area flat plasma displays [1, 12]. As far as industrial applications are concerned, except for the surface discharge CO 2 laser, DBDs are operated in the filamentary mode [13]. In recent years, significant research efforts have been devoted to study atmospheric pressure non-equilibrium plasmas in DBDs. A self-consistent two-dimensional model was presented in [14]. The discharge development was divided into four phases, a Townsend phase, an ionization wave or streamer phase, a cathode layer formation phase, and a decay phase. A DBD generated by flowing helium between two parallel-plate electrodes in an open reactor has been characterized in [15]. The authors found that it is possible to observe a transition from the filamentary mode to an apparently uniform and repeatable discharge mode by adjusting the operation conditions with flowing helium. Surface discharges created in DBD configurations and proposed as actuators for flow control have also been investigated, based on a two-dimensional fluid model [16]. Unfer et al. [17] also developed a two–dimensional self-consistent numerical model in which nanosecond voltage pulses were applied between electrodes in a DBD configuration. However, there is only limited work [18] discussing DBDs using an implicit PIC-MC method and the involved P-II-4-10 physics is still not completely clear, partially due to the time-consuming numerical simulation process. The aim of the present work is to study the discharge characteristics in DBDs with various operation parameters, such as the MD gap size and the pulse voltage. We want to understand the basic phenomena that determine the behaviour of atmospheric pressure DBDs. 2. Description of the model In this work, we have employed a direct implicit PIC-MCC code [19-20]. Our method has been described in detail and tested a number of times before. In this PIC-MCC code scheme, the field equations are obtained from direct summation and extrapolation of the equations of particle motion. After the particle pushing procedure and solving the electric field, a standard MCC procedure is executed to account for elastic, excitation and ionization electron-neutral collisions and for elastic scattering and charge exchange ion-neutral collisions. Coulomb collisions are negligible as the ionization degree is less than 1%. The cross sections used for these reactions are adopted from [21-23]. In this simulation we have considered secondary electron emission (SEE) which is self–consistently coupled in the code. SEE is an Auger electron emission process [24], and Zhang et al. [24] have elucidated that the secondary electrons play an essential role in maintaining the discharge. Here we assume a constant ion impact SEE coefficient of 0.1, which is the same as the one typically used in fluid models [25]. As the electron and ion densities increase rapidly duo to SEE, a particle merging algorithm is used when the particle number exceeds a certain value. This PIC-MC method is stable over a very broad range of physical and numerical parameters. A voltage source with amplitude of 500 V is used to drive the discharge. Argon gas is at a temperature of 300 K. The simulation time-step is fixed at 4x10-12 s 1 and the gap size is divided into 128 cells. The discharge is sustained between two parallel plate electrodes covered with two dielectric layers. All the simulation results, such as the electron temperature, electron and ion densities and current, the electric field and the EEDFs, will be averaged by several thousand time steps at steady state. 3. Results and discussion Fig. 1 shows the electron and ion density profiles for an rf voltage of 500 V. The electron and ion densities are more or less equal to each other, except in the sheaths where the ion density is slightly higher. The electron and ion density profiles show two symmetric peaks near the sheath boundary, which is similar to experimental observations [26] in a SEE sustaining MD and to a computational study [24] in a radio frequency MD. It is clear from the density profiles that the discharge is local (i.e., steep density peak at the sheath boundaries and low density in the bulk). It is because the mean free path of electrons is smaller than the width of the bulk region between the sheath boundaries, so the electrons cannot reach or pass through the bulk region and generate ionization. Fig. 2. Electric field as a function of position, for an rf voltage of 500 V. In order to examine the corresponding electron kinetics, we present the electron and ion temperatures and the electron energy distribution functions (EEDFs) in Figs. 3 and 4, respectively. From figure 3 we can see that the electron temperature is much higher than the ion temperature in the bulk region, which demonstrates that the electrons are effectively heated by the electric field and the energetic electrons produce more electron impact ionization. There are also two little peaks in the sheaths, which is consistent with the peaks of the electric field in Fig. 2. In the sheaths the electrons are accelerated due to the potential drop, which is in agreement with [27]. The EEDFs manifest a Druyvesteyn distribution, which is different from [24]. In that paper, the EEDFs show a three-temperature profile (hybrid mode) and a two-temperature distribution (α mode). Shi et al. [28] have elucidated that secondary electron emission strongly affects the gas ionization in the γ mode, but is of little importance in the α mode, and our calculated EEDFs confirm this. Fig. 1. Electron and ion densities as a function of position, for an rf voltage of 500 V. Fig. 2 presents the time-averaged electric field distributions. It is clear that in the dielectric layers the electric field is almost constant, whereas in the two sheaths there is a peak. This is because the deposition of the electrons on the left dielectric sheet results in a negative field just near the dielectric surface, which will lead to the accumulation of the electrons in the gas gap, and more ion deposition on the right dielectric sheet. In the bulk region the electric field is nearly zero, which can be explained from Fig. 1, where the electron and ion densities are nearly equal to each other. Fig. 3. Electron and ion temperature profiles, for an rf voltage of 500 V. 2 P-II-4-10 [6] [7] [8] [9] [10] [11] Fig. 4. Space-time-averaged electron energy distribution function, for an rf voltage of 500 V. 4. Conclusion A direct implicit PIC-MC method is applied to investigate an argon discharge operating in a dielectric barrier configuration. This implicit method allows us to employ much larger space and time steps, therefore it reduces the computational cost and self-heating. The evolutions of the electron and ion densities and temperatures, the time-averaged electric field, and the space-time-averaged EEDF have been presented. In our simulation, the electron and ion densities are in the glow discharge limit, as the ionization degree is lower than 1%. 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