@inproceedings{oai:jaxa.repo.nii.ac.jp:00005534,
 author = {池田, 友明 and 黒滝, 卓司 and 住, 隆博 and 高木, 正平 and Ikeda, Tomoaki and Kurotaki, Takuji and Sumi, Takahiro and Takagi, Shohei},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第40回, JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition},
 month = {Feb},
 note = {Karman-vortex shedding induced by wake instability behind a 2-D airfoil is of interest at relatively low Reynolds numbers, to understand how a vortex street develops in the wake region, and also how an aeolian tone is generated therefrom; this is supposed to show a different flow mechanism from a high-Reynolds number flow that exhibits more complicated viscous-flow phenomena. In this study, we performed numerical simulations of a 2-D laminar flow past an NACA0012 airfoil. The computation was run on the simulation code being developed to predict an aero-acoustic problem by using a highly accurate numerical method. For the verification of our code, the results are compared with the experimental data obtained in a similar flow configuration and also with an available numerical study. The detailed flow visualization is presented to understand the mechanism of the wake instability that results in vortex shedding., 資料番号: AA0063908013, レポート番号: JAXA-SP-07-026E},
 pages = {41--44},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Numerical simulations of flow past a 2-D airfoil at a low Reynolds number},
 volume = {JAXA-SP-07-026E},
 year = {2008}
}