@inproceedings{oai:jaxa.repo.nii.ac.jp:00005633,
 author = {村山, 光宏 and 山本, 一臣 and Murayama, Mitsuhiro and Yamamoto, Kazuomi},
 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 = {A CFD (Computational Fluid Dynamics) workshop was held in the 44th Aircraft Symposium, October 2006, in order to evaluate domestic CFD technology for civil transport aircrafts in high-lift configurations. JAXA provided an experimental data for comparison obtained in the JAXA large low-speed wind tunnel using a half model equipped with high-lift devices, fuselage, nacelle-pylon, slat tracks and Flap Track Fairings (FTF). This paper briefly presents the experimental model, objectives and test cases of the CFD workshop, summary of comparison, and obtained knowledge and issues on CFD and wind tunnel testing for high-lift configuration., 資料番号: AA0063742027, レポート番号: JAXA-SP-07-016},
 pages = {166--171},
 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ワークショップのまとめ},
 volume = {JAXA-SP-07-016},
 year = {2008}
}