@inproceedings{oai:jaxa.repo.nii.ac.jp:00005433,
 author = {紀平, 光彦 and 古賀, 光泰 and 舟木, 治郎 and 平田, 勝哉 and Kihira, Mitsuhiko and Koga, Mitsuhiro and Funaki, Jiro and Hirata, Katsuya},
 book = {宇宙航空研究開発機構特別資料: 第40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2008論文集, JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008},
 month = {Feb},
 note = {第40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2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス, Aerodynamic characteristics of airfoils have been researched in higher Reynolds-number ranges more than 10(exp 6), in a historic context closely related with airplanes' developments in the last century. So, in the present study, we investigate such basic airfoils as a NACA0015, a flat plate and the flat plates with modified fore- or after-faces in a Reynolds-number range of 10(exp 2)-10(exp 5), using two- and three-dimensional computations together with wind-tunnel and water-tank experiments., 形態: カラー図版あり, 資料番号: AA0064303031, レポート番号: JAXA-SP-08-009},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {低レイノルズ数での空力特性に及ぼす翼型形状の効果},
 volume = {JAXA-SP-08-009},
 year = {2009}
}