@inproceedings{oai:jaxa.repo.nii.ac.jp:00005635,
 author = {村山, 光宏 and 横川, 譲 and 山本, 一臣 and 田中, 健太郎 and 上田, 良稲 and Murayama, Mitsuhiro and Yokokawa, Yuzuru and Yamamoto, Kazuomi and Tanaka, Kentaro and Ueda, Yoshine},
 book = {宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集, JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007},
 month = {Feb},
 note = {In this study, three-dimensional flow computations around a realistic landing configuration deploying high-lift devices with a nacelle-pylon tested at JAXA are performed for the JAXA High-Lift Device CFD (Computational Fluid Dynamics) Workshop. Influence on the aerodynamic forces by the turbulent transition of boundary layer is discussed. Importance to consider the transition is shown for better prediction of the aerodynamic forces at high angles of attack. A prediction method for the turbulent transition of boundary layer is also evaluated. The capability is discussed comparing with experimental data. A wind tunnel interference derived from the half-span testing model is also discussed., 資料番号: AA0063742029, レポート番号: JAXA-SP-07-016},
 pages = {178--183},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {JAXA高揚力装置風洞模型を用いたCFD検証解析について},
 volume = {JAXA-SP-07-016},
 year = {2008}
}