IMECH-IR  > 等离子体与燃烧中心(2009-2011)
Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster
Wang HX; Jia SX; Chen X; Pan WX(潘文霞)
Source PublicationISCM II and EPMESC XII, PTS 1 and 2, AIP Conference Proceedings
2010
Volume1233Issue:1Pages:209-212
AbstractModeling studies are preformed to investigate the plasma and heat transfer characteristics of a low power argon arcjet thruster. Computed temperature, velocity, static pressure, and Mach number distribution in arcjet thruster under typical operating condition are presented in this paper. It shows that the performance data from numerical modeling results are basically consistent with the experimental measured values.
Subject Area电磁流体力学和等离子体动力学
Indexed ByEI
Language英语
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43290
Collection等离子体与燃烧中心(2009-2011)
Corresponding AuthorWang HX
Recommended Citation
GB/T 7714
Wang HX,Jia SX,Chen X,et al. Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster[J]. ISCM II and EPMESC XII, PTS 1 and 2, AIP Conference Proceedings,2010,1233(1):209-212.
APA Wang HX,Jia SX,Chen X,&潘文霞.(2010).Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster.ISCM II and EPMESC XII, PTS 1 and 2, AIP Conference Proceedings,1233(1),209-212.
MLA Wang HX,et al."Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster".ISCM II and EPMESC XII, PTS 1 and 2, AIP Conference Proceedings 1233.1(2010):209-212.
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