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	Simulation analysis of ion thruster plume thermal effect [离子推力器羽流热效应仿真分析]
	Zhang, J.; Li, J.; You, F.; Zheng, H.
刊名	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
	2018
卷号	44页码:2028-2034
关键词	Computer simulation Electric propulsion Flow fields Flow measurement Flowmeters Heat transfer Ion propulsion Ions Monte Carlo methods Numerical methods Space flight Thermal effects Direct simulation Monte Carlo method Measuring points Particle in cell method PIC-DSMC method Plume Sensitive materials Simulation analysis Thermal deformation Plasma simulation
ISSN号	10015965
DOI	10.13700/j.bh.1001-5965.2017.0802
URL标识	查看原文
收录类别	CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5929627
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Zhang, J.,Li, J.,You, F.,等. Simulation analysis of ion thruster plume thermal effect [离子推力器羽流热效应仿真分析][J]. Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,2018,44:2028-2034.
APA	Zhang, J.,Li, J.,You, F.,&Zheng, H..(2018).Simulation analysis of ion thruster plume thermal effect [离子推力器羽流热效应仿真分析].Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics,44,2028-2034.
MLA	Zhang, J.,et al."Simulation analysis of ion thruster plume thermal effect [离子推力器羽流热效应仿真分析]".Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 44(2018):2028-2034.

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