@inproceedings{oai:jaxa.repo.nii.ac.jp:00004380,
 author = {野々村, 拓 and 小嶋, 亮次 and 安養寺, 正之 and 大山, 聖 and 藤井, 孝蔵 and Nonomura, Taku and Kojima, Ryoji and Anyoji, Masayuki and Oyama, Akira and Fujii, Kozo},
 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, In this study, aerodynamic characteristics of Ishii airfoil at Reynolds number 23,000 are evaluated by large-eddy simulation. For the computational analysis, sixth-order compact scheme for spatial differencing and second-order backward differencing for temporal integration are adopted. The results show that flow around Ishii airfoil has trailing edge separation at low angles of attack, it has leading edge separation and reattachment at medium angles of attack, and it has only leading edge separation at high angle of attack. This characteristics is almost the same as that of NACA0012 which is previously studied. However, the airfoil characteristics of Ishii airfoil are much better than those of NACA0012. This is because of both enhancement in lift by pressure side camber and reduction in drag by pressure side shape., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207008, レポート番号: JAXA-SP-11-015},
 pages = {43--48},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {LESによる石井翼(Re=23,000)の空力特性評価},
 volume = {JAXA-SP-11-015},
 year = {2012}
}