@inproceedings{oai:jaxa.repo.nii.ac.jp:00004401,
 author = {名古屋, 靖一郎 and 木野, 由也 and 平口, 雪乃 and 相曽, 秀昭 and Nagoya, Seiichiro and Kino, Yuya and Heiguchi, Yukino and Aiso, Hideaki},
 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, Data assimilation techniques in the calculation around a wing are attempted using FaSTAR, fast aerodynamics solver. The particle filter is mainly used as data assimilation techniques. The adjoint problem of fluid equations is FaSTAR code is considered in this article., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207029, レポート番号: JAXA-SP-11-015},
 pages = {171--176},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {FaSTARを用いた翼周りデータ同化計算の試み},
 volume = {JAXA-SP-11-015},
 year = {2012}
}