@inproceedings{oai:jaxa.repo.nii.ac.jp:00004404,
 author = {杉浦, 裕樹 and Sugiura, Hiroki},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, Wind tunnel test model is generally sting-mounted and forces acting on the model are measured using internal force sensors. In order to avoid any interference of the support on the flow field, magnetic suspension and balance system (MSBS) suspends the model magnetically. Six components of the forces can be measured simultaneously by calculating from coil currents required for the levitation. MSBS also enables to measure unsteady forces while the model is moving dynamically in space. JAXA's Fluid Dynamcs Group started MSBS research on 1986, independently developed the present system, and succeeded in the world's first full 6 degree-of-freedom (DOF) control and simultaneous 6-DOF force measurement. It has the world's largest test section and has been in practical use since 2000., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207032, レポート番号: JAXA-SP-11-015},
 pages = {187--188},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {磁力支持風洞試験データベース},
 volume = {JAXA-SP-11-015},
 year = {2012}
}