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Simulation of a Stationary Plasma Thruster using the Space-Time Conservation Method

机译:时空守恒法模拟固定式等离子推进器

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The one-dimensional hydrodynamic model of a stationary plasma thruster (SPT) previously described by Morozov and Savelyev [in Reviews of Plasma Physics, Vol. 21, Consultants Bureau, New York, 2000, pp. 360-369] is solved using the space-time conservation element/solution element (CE/SE) method. The hydrodynamic model consists of three equations describing the mass conservation of ions and neutral particles and the momentum of the ions. These equations are coupled nonlinearly through source terms describing the ionization of neutrals, and a non-local term describing current through the plasma. This model is one of the simplest to produce the low-frequency oscillatory behavior (on the order of 10 kHz) known as the "breathing mode" that is observed in ground testing of SPTs. Numerical solutions to the model are challenging due to the highly coupled, nonlinear nature of the equations. The simulation outlined here was successful, but displays some of the Courant number sensitivity noted in other CE/SE simulations.
机译:固定等离子推进器(SPT)的一维流体动力学模型先前由Morozov和Savelyev [在Plasma Physics,Vol。 21,顾问局,纽约,2000年,第360-369页]是使用时空守恒元素/解元素(CE / SE)方法求解的。流体力学模型由三个方程式组成,这些方程式描述了离子和中性粒子的质量守恒以及离子的动量。这些方程通过描述中性离子电离的源项和描述通过等离子体的电流的非局部项进行非线性耦合。该模型是最简单的产生低频振荡行为(大约10 kHz)的模型之一,被称为“呼吸模式”,在SPT的地面测试中可以观察到。由于方程的高度耦合,非线性性质,该模型的数值解决方案具有挑战性。此处概述的模拟是成功的,但是显示了其他CE / SE模拟中提到的一些Courant数敏感性。

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