@inproceedings{oai:jaxa.repo.nii.ac.jp:00037727,
 author = {山田, 仁 and 石垣, 博 and 望月, 宗和 and Yamada, Hitoshi and Ishigaki, Hiroshi and Mochizuki, Munekazu},
 book = {航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集, Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics},
 month = {Dec},
 note = {航空宇宙技術研究所 10-12 Jun. 1992 東京 日本, National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan, 真直ぐな入口および出口部分をもつ正方形断面S字ダクトの中の発達する層流を有限容積法に基づいて数値的に調べた。ディーン数は299、曲率比は7で、S字ダクト角は22.5度である。計算結果をTaylorらによる実験データと比較し、良好な一致をみた。, Developing laminar flow in a S-curved square duct with an inlet and outlet straight region, is studied numerically by using a finite volume method. In this study, Dean number is 299 and curvature ratio is 7 and S-curved duct angle is 22.5 degrees respectively. Calculated results are compared with the experimental data by Taylor et al.. The calculated results showed good agreements with the experimental data., 資料番号: AA0004168041, レポート番号: NAL SP-19},
 pages = {225--228},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {S型ベンドの流れの数値解析},
 volume = {19},
 year = {1992}
}