@inproceedings{oai:jaxa.repo.nii.ac.jp:00006134,
 author = {伊藤, 良三 and 今村, 太郎 and Ito, Ryozo and Imamura, Taro},
 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2005論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005},
 month = {Feb},
 note = {The SST (Shear-Stress Transport) turbulence model has been implemented in UPACS, a CFD platform developed in JAXA. Four test cases with increasing level of difficulty were used to validate the present implementation. Three basic test cases included flat plate, backward-facing step, and transonic airfoil RAE2822. For more practical application, the flow simulation around the DLR-F6 transport aircraft was performed. Validations were carried out by comparing the present numerical results with those of other numerical methods and experimental method. Numerical results obtained from the computations above show that the present implementation is valid. We believe that this effort has extended UPACS's applicability to more complicated flow fields., 資料番号: AA0049212001, レポート番号: JAXA-SP-05-017},
 pages = {11--16},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {UPACSに組み込まれた乱流モデルの検証計算},
 volume = {JAXA-SP-05-017},
 year = {2006}
}