@inproceedings{oai:jaxa.repo.nii.ac.jp:00006452,
 author = {Li, Dong and Menshov, Igor and 中村, 佳朗 and Li, Dong and Menshov, Igor and Nakamura, Yoshiaki},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004},
 month = {Mar},
 note = {Detached-Eddy Simulation is applied to three airfoils with different stall types. The method combines the strong points of Reynolds-averaged Navier-Stokes and Large Eddy Simulation approaches. Spalart-Allmaras Model is basically used, which reduces to a RANS formulation near a solid surface and to a subgrid model away from the wall. LU-SGS implicit scheme is employed to solve the model in time. Compared with experiment data, it is found that stall angle can be reasonably predicted by the present method., 資料番号: AA0048469012, レポート番号: JAXA-SP-04-012},
 pages = {75--81},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Detached-Eddy Simulation of massively separated flows around airfoil},
 volume = {JAXA-SP-04-012},
 year = {2005}
}