JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64967034.pdf1.16 MB
Other TitleApplicability of Data Assimilation for Numerical Calculation of Flow around Wing
Author(jpn)名古屋, 靖一郎; 木野, 由也; 相曽, 秀昭
Author(eng)Nagoya, Seiichiro; Kino, Yuya; Aiso, Hideaki
Author Affiliation(jpn)アーク情報システム; アーク情報システム; 宇宙航空研究開発機構
Author Affiliation(eng)ARK Information Systems; ARK Information Systems; Japan Aerospace Exploration Agency (JAXA)
Issue Date2011-02-28
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication titleJAXA special publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010
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
Publication date2011-02-28
AbstractThe 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.
DescriptionOriginal contains color illustrations
Meeting Information: 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan
形態: カラー図版あり
会議情報: 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)
Document TypeConference Paper
JAXA Category特別資料
Report NoJAXA-SP-10-012

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