@inproceedings{oai:jaxa.repo.nii.ac.jp:00003846,
 author = {永田, 靖典 and 山田, 宗平 and 山田, 和彦 and 安部, 隆士 and Nagata, Yasunori and Yamada, Shuhei and Yamada, Kazuhiko and Abe, Takashi},
 book = {宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, In the electrodynamic flow control, a weakly-ionized plasma flow behind the strong shock wave could be controlled by the applied magnetic field around a reentry vehicle. It could be an innovative technology for reentry vehicle design because it will realize an aerodynamic control device without moving part. To demonstrate this technology on the flight condition, a light-weight, compact, and strong magnetic field source must be required, which must be able to be magnetized tesla order. We have developed a prototype magnetic field source which contains a superconducting bulk magnet cooled by solid nitrogen and it was applied to some experiments including HIEST wind tunnel test. However, the prototype model has some problems for the magnetizing and cooling processes, which has significant impact on the flight operation. Therefore, the next model is planned to improve and ease the operation by using a Stirling refrigerator instead of liquid refrigerant., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023011, レポート番号: JAXA-SP-14-010},
 pages = {57--62},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {弱電離プラズマ流制御技術の実証に向けた強磁場源の開発と運用について},
 volume = {JAXA-SP-14-010},
 year = {2015}
}