Science University of Tokyo Graduate School of Science and Technology
Toyama University Dept. of Mechanical and Intellectual Systems Engineering, Faculty of Engineering
Science University of Tokyo Department of Mechanical Engineering, Faculty of Science and Technology
National Aerospace Laboratory
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory
巻
41
ページ
397 - 402
発行年
1999-02
会議概要（会議名, 開催地, 会期, 主催者等）
航空宇宙技術研究所 24-26 Jun. 1998 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan
Recently, the development of computer power has enabled to make large scale numerical simulation for turbulent flows. In this paper, studies on the simulation of flow around the NACA0012 airfoil without sweep are reported in order to develop the practical DNS (Direct Numerical Simulation) and LES (Large Eddy Simulation) technologies. The Reynolds number Re, based on the uniform inflow velocity and the chord length, is set to be 2.0 x 10(exp 6). Computations are now under going with the high performance parallel supercomputer NWT (Numerical Wind Tunnel) at NAL.
翼まわりの大規模数値シミュレーション
nalsp0041064.pdf
(1.41MB)
