@inproceedings{oai:jaxa.repo.nii.ac.jp:00006453,
 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: 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 = {In this paper, flow computations around a 3D high-lift configuration with three-element (slat-main-flap) wing were performed on structured and unstructured meshes. The results were used to analyze and improve the accuracy and reliability of the aerodynamic analyses for high-lift system. Computed lift and drag coefficients both on structured and unstructured meshes showed good agreement with the experimental data. In the computations, it was also shown that further mesh refinement should be used to improve the resolution for slat wake, wing tip, and trailing edge for more accurate prediction by detail comparison with wind tunnel test data and computational data., 資料番号: AA0048469013, レポート番号: JAXA-SP-04-012},
 pages = {82--86},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {非構造格子法を用いた航空機高揚力装置周りの流れ場解析の精度検証},
 volume = {JAXA-SP-04-012},
 year = {2005}
}