@inproceedings{oai:jaxa.repo.nii.ac.jp:00006616,
 author = {秋葉, 公三郎 and 中道, 二郎 and 井上, 隆 and 米澤, 太志 and Akiba, Kosaburo and Nakamichi, Jiro and Inoue, Takashi and Yonezawa, Futoshi},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {This paper presents YSX transonic flutter study and Arrow wing flutter study as NATAS (transonic flutter Analysis code made in NAL) numerical simulation example. The objective of YSX transonic flutter study is to investigate flutter characteristics on WRI (Wing Root Insert) structure. The objective of Arrow wing flutter study is to investigate that reduction of Wash-Out tendency can improve Arrow wing flutter characteristics. In analytical results, reduction of Wash-Out tendency is effective method to improve Arrow wing flutter characteristics., 資料番号: AA0047427015, レポート番号: JAXA-SP-03-002},
 pages = {81--86},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {アローウィングの空力弾性設計},
 volume = {JAXA-SP-03-002},
 year = {2004}
}