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Electric propulsion plume simulations using parallel computer

机译:使用并行计算机进行电推进羽流模拟

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A parallel, three-dimensional electrostatic PIC code is developed for large-scale electric propulsion simulations using parallel supercomputers. This code uses a newly developed immersed-finite-element particle-in-cell (IFE-PIC) algorithm designed to handle complex boundary conditions accurately while maintaining the computational speed of the standard PIC code. Domain decomposition is used in both field solve and particle push to divide the computation among processors. Two simulations studies are presented to demonstrate the capability of the code. The first is a full particle simulation of near-thruster plume using real ion to electron mass ratio. The second is a high-resolution simulation of multiple ion thruster plume interactions for a realistic spacecraft using a domain enclosing the entire solar array panel. Performance benchmarks show that the IFE-PIC achieves a high parallel efficiency of ≥90%.
机译:开发了一个并行的三维静电PIC代码,用于使用并行超级计算机进行的大规模电推进仿真。该代码使用了新开发的浸入式有限元单元内粒子(IFE-PIC)算法,该算法可精确处理复杂的边界条件,同时保持标准PIC代码的计算速度。领域分解既用于现场求解,又用于粒子推送,以将计算结果划分到各个处理器之间。进行了两次仿真研究,以证明代码的功能。第一个是使用实际离子质量比电子对质量的近推力羽流的全粒子模拟。第二个是使用包围整个太阳能电池板的区域对现实航天器进行的多个离子推进器羽流相互作用的高分辨率模拟。性能基准表明,IFE-PIC的并行效率高达90%以上。

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