Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster
Data(s) |
2010
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Resumo |
Modeling 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. |
Identificador | |
Idioma(s) |
英语 |
Fonte |
ISCM II and EPMESC XII, PTS 1 and 2, AIP Conference Proceedings.2010,1233(1):209-212 |
Palavras-Chave | #交叉与边缘领域的力学::电磁流体力学和等离子体动力学 |
Tipo |
期刊论文 |