电力推进数值模拟研究进展

Sai Vigness Ramasamy, L. Bazyma
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引用次数: 0

摘要

自20世纪60年代初以来,电力推进技术得到了发展,其在卫星、轨道平台和行星际探测器上的应用在21世纪显著增加。为了更详细地了解工作物理和更准确地评估性能以创造创新设计,刺激了几种数值模拟代码的发展。对特定推力器建模方法的选择应根据装置中流动的物理特性和模拟所需的精度水平来决定。不同类型的推进器有不同的条件。这意味着必须为每一种不同的推进器开发不同的方法和计算机代码。成功地发展物理精确的数值方法来模拟电推进推进器中的气体和等离子体流动,可以显著改善这些装置的设计过程。近年来,数值模拟越来越有利于对电动推进器的基本认识和工程优化。这是由于几个并发的贡献:计算机硬件的进化使得多维几何和多尺度现象的表示成为可能;实施复杂的新算法和数值诊断工具;以及新的碰撞和表面相互作用数据的可用性。今后的工作主要有两个方向,即继续改进电动推进器的数值模拟。首先,数值方法本身必须在物理精度和计算速度方面得到改进。改进模拟的第二个主要方向包括更精确地确定数值公式所要求的物理参数。本文概述了开发各种电力推进概念模型的努力,从90年代初的第一次尝试到最新的复杂多维模拟。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Progress in electric propulsion numerical simulation
Electric propulsion has been developed since the early 1960s, and its use onboard satellites, orbiting platforms, and interplanetary probes have increased significantly in the 21st century. The need for a detailed understanding of the working physics and a more accurate assessment of performance to create innovative designs has stimulated the development of several numerical simulation codes. The choice of method for modelling a specific thruster should be dictated by the physical characteristics of the flow in the device, and by the level of accuracy required from the simulation. There are various conditions in different types of thrusters. This means that different methods and computer codes must be developed for each of the different thrusters. The successful development of physically accurate numerical methods for simulating gas and plasma flows in electric propulsion thrusters can significantly improve the design process of these devices. In recent years, numerical simulations have increasingly benefited the basic understanding and engineering optimization of electric thrusters. This is due to several concurrent contributions: the evolution of computer hardware that has allowed the representation of multidimensional geometries and multiscale phenomena; implementation of sophisticated new algorithms and numerical diagnostic tools; and availability of new collisional and surface interaction data. There are two main directions for future work to continue to improve the numerical modelling of electric thrusters. First, the numerical methods themselves must be improved in terms of their physical accuracy and computational speed. The second main direction for improvement in the simulations involves more accurate determination of physical parameters that are required by the numerical formulations. This paper outlines efforts to develop models of various electrical propulsion concepts, from the first attempts in the early 90s to the latest sophisticated multidimensional simulations.
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