@inproceedings{oai:jaxa.repo.nii.ac.jp:00006588,
 author = {齊藤, 健一 and 菊池, 孝男 and 神田, 淳 and 玉山, 雅人 and 中道, 二郎 and Saito, Kenichi and Kikuchi, Takao and Kanda, Atsushi and Tamayama, Masato and Nakamichi, Jiro},
 book = {宇宙航空研究開発機構特別資料: 第67回　風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting},
 month = {Mar},
 note = {In a design of the Non-powered Supersonic Experimental Airplane, three kinds of flutter modes were focused; aileron with one degree of freedom, a first bending mode of a main wing and a rocket fin first torsion mode coupled with control surface motion. Therefore three types of model for each flutter test were made and tested in wind tunnels, in order to confirm analytical results. The results of the tests are described in this paper., 資料番号: AA0047429004, レポート番号: JAXA-SP-03-004},
 pages = {19--24},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {SSTロケット実験機模型フラッタ試験},
 volume = {JAXA-SP-03-004},
 year = {2004}
}