@inproceedings{oai:jaxa.repo.nii.ac.jp:00014619,
 author = {滝澤, 勇二 and 佐藤, 俊逸 and 安部, 隆士 and Konigorski, Detlev and Takizawa, Yuji and Sato, Shunichi and Abe, Takashi and Konigorski, Detlev},
 book = {宇宙航行の力学シンポジウム　平成16年度, Symposium on Flight Mechanics and Astrodynamics 2004},
 month = {Mar},
 note = {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., 資料番号: AA0048089012},
 pages = {45--48},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {大気圏再突入流れ場における印加磁場の干渉効果},
 year = {2005}
}