论文标题

用于Hall推进器建模的广义减少粒子中的粒子中的粒子中:轴向齐路构型中的概念和深入验证

Generalized reduced-order particle-in-cell scheme for Hall thruster modeling: concept and in-depth verification in the axial-azimuthal configuration

论文作者

Reza, Maryam, Faraji, Farbod, Knoll, Aaron

论文摘要

还原粒子中的粒子(PIC)方案是一种新型的建模方法,可实现等离子的计算有效的静电动力学模拟。在我们以前的出版物中,我们证明了该图片方案的初步实施的潜力,以在大厅推进器中以接近传统的多维图片模拟的方式解决多维等离子体过程。在这项工作中,我们首先引入了一种数学上成熟的公式,以降低泊松方程的尺寸,从而实现了广义的“准摩尔蒂二维”图片方案。我们提供了一个证据,即尺寸降低了泊松方程在极限中会收敛到多维的方程。然后,对于一般的2D泊松问题,验证了结合了降低降低性降低配方的减少量度泊松求解器。接下来,我们介绍使用广义还原静电PIC方案进行的几个准2D轴向齐路模拟的结果。我们表明,减少顺序PIC的配方的改进显着增强了其预测能力,从而可以在几种情况下使用2D问题的低阶近似值在几种条件下准确地重现参考完整2D PIC模拟的结果。此外,高阶近似值使我们能够在文献中恢复有关霍尔推进器中方位角不稳定性中报告的相同特征和行为,并通过模拟降低了计算成本的几个因素。最后,我们讨论了一系列灵敏度分析,包括阴极边界条件的影响以及方位角域的长度对准2D模拟的预测。因此,我们在结论中概述了降低订单方案的持续活动,用于对霍尔推进器物理学的成本效益的三维研究。

Reduced-order particle-in-cell (PIC) scheme is a novel modeling approach that enables computationally efficient electrostatic kinetic simulations of plasma. In our previous publications, we demonstrated the potentials of a preliminary implementation of this PIC scheme to resolve the multi-dimensional plasma processes in a Hall thruster in a manner close to traditional multi-dimensional PIC simulations. In this work, we first introduce a mathematically mature formulation for the dimensionality reduction of Poisson's equation, which enables the generalized "quasi-multi-dimensional" PIC scheme. We present the proof that the dimensionally reduced Poisson's equation converges to the multi-dimensional one in the limit. A reduced-dimension Poisson solver incorporating the dimensionality-reduction formulation is then verified for general 2D Poisson problems. Next, we present the results of several quasi-2D axial-azimuthal simulations performed using the generalized reduced-order electrostatic PIC scheme. We show that the improvements in the formulation of the reduced-order PIC notably augments its predictive capability, enabling the approach to reproduce quite accurately the results from reference full-2D PIC simulations in several conditions using low-order approximations of the 2D problem. Moreover, higher order approximations allow us to recover the same characteristics and behaviors reported in the literature regarding the azimuthal instabilities in Hall thrusters with simulations offering several factors reduction in computational cost. Finally, we discuss a series of sensitivity analyses, including the influence of the cathode boundary condition and the azimuthal domain length on the quasi-2D simulations' predictions. Accordingly, we outline in the conclusions the ongoing activities on the reduced-order scheme toward cost-effective three-dimensional studies of Hall thrusters' physics.

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