@inproceedings{oai:jaxa.repo.nii.ac.jp:00004741,
 author = {名古屋, 靖一郎 and 木野, 由也 and 相曽, 秀昭 and Nagoya, Seiichiro and Kino, Yuya and Aiso, Hideaki},
 book = {宇宙航空研究開発機構特別資料: 第42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2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42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2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, The aim of this paper is to discuss the applicability of data assimilation methods for numerical calculation of flow around wing. We mainly adopt the particle filter to solve the maximum problem of likelihood which is consisted of difference between CFD and EFD. Effectiveness of the adjoint method is also discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967034, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {翼周計算におけるデータ同化手法の適用性について},
 volume = {JAXA-SP-10-012},
 year = {2011}
}