The Institute of Computational Fluid Dynamics
Fuji Heavy Industries Ltd.
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 SP-10
巻
10
ページ
33 - 38
発行年
1989-11
抄録（英）
The major portion of the flow field at high Reynolds number will be unsteady, so turbulent eddy viscosity models are used in simulating such high Reynolds number flow. The steady flow fields obtained by using turbulent eddy viscosity model is expected to be the time-averaged solutions. In this study, we investigated the unsteady solution of the flow over the wing with a side wall. For this purpose, we calculated the time-average of the unsteady flow field without using any turbulent eddy viscosity models. As the number of grid points gets large, the CP-curves of the time-average will become close to the results of the experiment.
側壁付きONERA-M6翼まわりの非定常計算
nalsp0010006.pdf
(303KB)
