利用细胞内粒子将电喷雾发射模型推广到阵列尺度

IF 1.7 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Adler G. Smith, Elaine M. Petro
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引用次数: 0

摘要

我们开发了一种多发射器电喷雾离子源建模的多尺度方法,可将发射场条件传播到可行的空间域,以进行羽流演化模拟。该框架使用 "粒子在单元中 "方法,以保持消费级硬件可行的计算复杂度。单个发射点的源模型由 n 体单发射极模型提供信息。离子群碎裂等分子效应也包括在内。该模型用于预测羽流发散角等阵列级属性,并证明并行模拟多个发射器的计算可行性。该框架用于量化阵列尺寸与空间电荷诱导的光束发散之间的关系。结果表明,对于商用电喷雾推进器,将粒子间作用力纳入羽流扩展会导致羽流半角在发射器电流为 80% 时增加 8.1 度,在发射器电流为 90% 时增加 9.8 度。这些数据表明,在阵列尺度上,空间电荷对羽流演化有重大影响,在分析这些系统时必须加以考虑。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Propagating an Electrospray Emission Model to Array Scales Using Particle-in-Cell
A multiscale approach to multi-emitter electrospray-ion source modeling has been developed to propagate emission site conditions into spatial domains viable for plume evolution simulations. This framework uses the particle-in-cell method to maintain a feasible computational complexity for consumer-grade hardware. Source models for individual emission sites are informed by an n-body single-emitter model. Molecular effects such as ion-cluster fragmentation are included. This model is used to predict array-level properties such as plume divergence angle, and to demonstrate the computational feasibility of modeling many emitters in parallel. This framework is used to quantify the relationship between array dimensions and space-charge- induced beam divergence. It is shown that including interparticle forces in plume expansion results in an increase in plume half angle by 8.1 deg for 80% and 9.8 deg for 90% of the emitter current for a commercial electrospray thruster. These data indicate that, at the array scale, space charge has a significant effect on plume evolution and must be considered in analysis of these systems.
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来源期刊
Journal of Propulsion and Power
Journal of Propulsion and Power 工程技术-工程:宇航
CiteScore
4.20
自引率
21.10%
发文量
97
审稿时长
6.5 months
期刊介绍: This Journal is devoted to the advancement of the science and technology of aerospace propulsion and power through the dissemination of original archival papers contributing to advancements in airbreathing, electric, and advanced propulsion; solid and liquid rockets; fuels and propellants; power generation and conversion for aerospace vehicles; and the application of aerospace science and technology to terrestrial energy devices and systems. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. Papers in these disciplines and the sciences of combustion, fluid mechanics, and solid mechanics as directly related to propulsion and power are solicited.
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