東京大学 大学院
宇宙科学研究所
宇宙科学研究所
Eur. Aeronautic Defence and Space Co.
著者所属（英）
University of Tokyo Graduate School
Institute of Space and Astronautical Science
Institute of Space and Astronautical Science
European Aeronautic Defence and Space Co.
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
宇宙航行の力学シンポジウム 平成16年度
雑誌名(英)
Symposium on Flight Mechanics and Astrodynamics 2004
ページ
45 - 48
発行年
2005-03
抄録（英）
Experimentally examined is the effect of applied magnetic field on a weakly ionized Argon plasma supersonic flow around a body around which the magnetic field is generated. To analyze the flow, applied is the absorption spectroscopic technique which enables determination of the translational temperature and the flow velocity. Based on the translational temperature distribution, combined with the electron excitation temperature distribution previously determined, the effect of the applied magnetic field on the behavior of the shock layer is discussed and it is confirmed that the applied magnetic field of which interaction parameter is 0.34 can affect the shock layer behavior and enhance the shock stand-off distance.
大気圏再突入流れ場における印加磁場の干渉効果
