@techreport{oai:jaxa.repo.nii.ac.jp:00043335,
 author = {桜木, 卓也 and 加茂, 圭介 and Sakuragi, Takuya and Kamo, Keisuke},
 month = {Nov},
 note = {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., 資料番号: NALSP0010006, レポート番号: NAL SP-10},
 title = {側壁付きONERA-M6翼まわりの非定常計算},
 year = {1989}
}