@inproceedings{oai:jaxa.repo.nii.ac.jp:00005637,
 author = {永田, 卓 and 越智, 章生 and 嶋, 英志 and Nagata, Taku and Ochi, Akio and Shima, Eiji},
 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 = {Flow around JAXA HLD (High Lift Devices) wind tunnel model is analyzed by RANS (Reynolds Averaged Navier Stokes) CFD (Computational Fluid Dynamics) method and compared with the experimental data obtained by JAXA. Unstructured mesh with overset technique is used for mesh generation around realistic configuration with small parts such as slat clip. It was shown that the slat clip made a difference in the flowfield especially around the edge of the slat. Baldwin-Barth and Spalart-Allmaras one equation models are used for turbulence model and the former gives better agreement with the experiment., 資料番号: AA0063742031, レポート番号: JAXA-SP-07-016},
 pages = {190--195},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {重合格子を用いたJAXA高揚力装置風洞模型のCFD解析},
 volume = {JAXA-SP-07-016},
 year = {2008}
}