@inproceedings{oai:jaxa.repo.nii.ac.jp:00004008,
 author = {橋本, 敦 and 石田, 崇 and 石向, 桂一 and 青山, 剛史 and Hashimoto, Atsushi and Ishida, Takashi and Ishiko, Keiichi and Aoyama, Takashi},
 book = {宇宙航空研究開発機構特別資料: 第45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2013論文集, JAXA Special Publication},
 month = {Mar},
 note = {第45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2013 (2013年7月4日-5日. タワーホール船堀), 東京, 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan, We show a research plan toward unsteady analysis of high-attack-angle separated flow. Although the separated flow is still a challenging problem for CFD, prediction technology of separation is necessary to improve CFD capability and expand applications in the flight envelope. Our research plan consists of (1) parallel automatic grid generation and (2) highly-accurate unsteady flow analysis with unstructured grid. In this paper, we also review buffet analyses using URANS or RANS/LES hybrid methods and show the current problems to be solved. In addition, the NASA-CRM with high attack angle is computed with steady RANS analysis to know the overall flow field and RANS limitations., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062268008, レポート番号: JAXA-SP-13-011},
 pages = {41--46},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {高迎角剥離流の非定常解析に向けて},
 volume = {JAXA-SP-13-011},
 year = {2014}
}